LIBRARY 
 
 OF THE 
 
 UNIVERSITY OF CALIFORNIA. 
 Gats 
 
 GENERAL 
 
THE 
 
 PHYSICAL PAPERS 
 
 OF 
 
 HENRY AUGUSTUS ROWLAND 
 
THE 
 
 PHYSICAL PAPERS 
 
 OF 
 
 HENRY AUGUSTUS ROWLAND 
 
 PH.D., LL. D. 
 
 Professor of Physics and Director of the Physical Laboratory in 
 
 The Johns Hopkins University 
 
 1876-1901 
 
 COLLECTED FOR PUBLICATION BY A 
 COMMITTEE OF THE FACULTY OF THE UNIVERSITY 
 
 BALTIMORE 
 THE JOHNS HOPKINS PRESS 
 1902 
 
Copyright, 1902, by the JOHNS HOPKINS PRESS 
 
 PRINTED BY 
 
 BALTIMORE, RID., U. S. A. 
 
HENRY AUGUSTUS ROWLAND 
 
 Born, Honesdale, Pennsylvania, November 27, 1848 
 Died, Baltimore, Maryland, April 16, 1901 
 
 Doctor of Philosophy (Ph. D.), Johns Hopkins University, 1880. (Hon- 
 oris Causa.) 
 
 Doctor of Laws (LL. D.), Yale University, 1895. 
 Doctor of Laws (LL. D.), Princeton University, 1896. 
 
 Fellow or Member of 
 
 The British Association for the Advancement of Science. 
 
 The Physical Society of London. 
 
 The Philosophical Society of Cambridge, England. 
 
 The Royal Society of London. 
 
 The Royal Society of Gottingen. 
 
 The Gioenian Academy of Natural Sciences, Catania, Sicily. 
 
 The French Physical Society. 
 
 The French Academy of Sciences. 
 
 The Literary and Philosophical Society of Manchester. 
 
 The Royal Lyncean Academy, Rome. 
 
 The Academy of Sciences, Stockholm. 
 
 The Italian Society of Spectroscopists. 
 
 The Royal Society of Edinburgh. 
 
 The Society of Arts, London. 
 
 The Royal Astronomical Society of England. 
 
 The Royal Society of Lombardy. 
 
 The Royal Physiographic Society of Lund. 
 
 The Royal Academy of Sciences, Berlin. 
 
 The Royal Academy of Sciences and Letters, Copenhagen. 
 
 The American Philosophical Society, Philadelphia. 
 
 The American Academy of Arts and Sciences, Boston. 
 
 The National Academy of Sciences, Washington. 
 
 The American Physical Society, its first President. 
 
 The Astronomical and Astrophysical Society of America. 
 
 Delegate of the United States Government to the 
 International Congress of Electricians, Paris, 1881. 
 International Congress for the Determination of Electrical Units, Paris, 
 
 1882. Appointed Officer of the Legion of Honor of France. 
 Electrical Congress, Philadelphia, 1884, President. 
 International Chamber of Delegates for the Determination of Electrical 
 
 Units, Chicago, 1893, President. 
 
 PRIZES AND MEDALS. 
 
 Rumford Medal, American Academy of Arts and Sciences. 
 Draper Medal, National Academy of Sciences. 
 Matteucci Medal. 
 
 Prize awarded by the Venetian Institute in competition for a critical 
 paper on the Mechanical Equivalent, of Heat. 
 
 102497 
 
PREFACE 
 
 Shortly after the death of Professor Rowland in April, 1901, a com- 
 mittee of the Faculty of The 'Johns Hopkins University was appointed 
 by President Gilman to suggest to the Trustees of the University a plan 
 for a memorial of their colleague. The committee, consisting of Pro- 
 fessors Remsen, Welch and Ames decided to recommend that a volume 
 be prepared containing the physical papers and addresses of Professor 
 Rowland, and also a detailed description of the dividing engines which 
 had been designed and constructed by him for the purpose of ruling 
 diffraction gratings, and that this volume be published by the University 
 Press. This recommendation was approved by the Trustees of the 
 University; and the same committee, with the addition of Professor 
 R. W. Wood, was empowered to prepare the volume for publication. 
 The editorial supervision has been mainly undertaken by Professor 
 Joseph S. Ames. 
 
 In deciding upon the scope of the proposed volume, it was thought 
 best to include only the distinctly physical papers, inasmuch as Pro- 
 fessor Rowland himself on several occasions when the question of the 
 collection of his scientific papers was raised, had expressed himself as 
 opposed to the republication of the purely mathematical ones. It was 
 also decided to omit tables of wave-lengths, as these are extremely 
 bulky, and copies can be easily obtained. Professor Rowland left many 
 thousand pages of manuscript notes and outlines of lectures, but none 
 of this material was ready for publication, and the committee were not 
 in a position to undertake the task of its preparation. No attempt has 
 been made to include a biography of Professor Rowland, for this would 
 properly form a volume by itself, and would require much time for its 
 preparation. There was at hand, moreover, the memorial address of 
 Dr. Mendenhall, which tells so well, though briefly, the story of his life. 
 
vi PREFACE 
 
 It was with difficulty, and only after a careful examination of many 
 hundred volumes of scientific journals and transactions, that the com- 
 mittee were able to obtain copies of all of Professor Eowland's numerous 
 and scattered articles; but they are convinced that no paper of import- 
 ance has escaped their notice. In preparing for publication these me- 
 moirs and addresses, no alterations other than typographical have been 
 made. 
 
 For permission to reprint some of the most valuable papers, thanks 
 are due to various publishers. The committee wish especially to express 
 their appreciation of the kindness of Messrs. A. and C. Black, and of 
 The Times (London) for permission to reprint from the Encyclopaedia 
 Britannica the articles on " The Screw " and on " Diffraction Gratings," 
 and of the Engineering Magazine Company, of New York, for permis- 
 sion to reprint the article on " Modern Theories as to Electricity." 
 
 The committee acknowledge their indebtedness also to Mr. 1ST. Mur- 
 ray, Librarian of The Johns Hopkins University, who has personally 
 superintended the details of publication, and whose advice has been 
 often needed. The proofs have been revised by Mr. E. P. Hyde, Fellow 
 in The Johns Hopkins University, who has thus been of the greatest 
 assistance to the committee. 
 
 THE JOHNS HOPKINS UNIVERSITY, 
 
 BALTIMORE, MARYLAND, 
 
 DECEMBER 1, 1902. 
 
CONTENTS 
 
 PAGE 
 
 PREFACE v 
 
 ADDRESS BY DR. T. C. MENDENHALL 1 
 
 SCIENTIFIC PAPERS 19 
 
 PART I. EAKLY PAPERS. 21 
 
 *1. The Vortex Problem 23 
 
 Scientific American XIII, 308, 1865. 
 
 2. Paine's Electro-magnetic Engine 24 
 
 Scientific American XXV, 21, 1871. 
 
 3. Illustration of Resonances and Actions of a Similar Nature 28 
 
 Journal of the Franklin Institute XCIV, 275-278, 1872. 
 
 4. On the Auroral Spectrum 31 
 
 American Journal of Science (3), V, 320, 1873. 
 
 PART II. MAGNETISM AND ELECTRICITY. 33 
 
 5. On Magnetic Permeability, and the Maximum of Magnetism of Iron, 
 
 Steel and Nickel 35 
 
 Philosophical Magazine (4), XL VI, 140-159, 1873. 
 
 6. On the Magnetic Permeability and Maximum of Magnetism of Nickel 
 
 and Cobalt 56 
 
 Philosophical Magazine (4), XLVHI, 321-340, 1874. 
 
 7. On a new Diamagnetic Attachment to the Lantern, with a Note on 
 
 the Theory of the Oscillations of Inductively Magnetized Bodies.. 75 
 American Journal of Science (3), IX, 357-361, 1875. 
 
 8. Notes on Magnetic Distribution 80 
 
 Proceedings of the American Academy of Arts and Sciences, XI, 191, 192, 
 1876. 
 
 9. Note on Kohlrausch's Determination of the Absolute Value of the 
 
 Siemens Mercury Unit of Electrical Resistance 82 
 
 Philosophical Magazine (4), L, 161-163, 1875. 
 
 10. Preliminary Note on a Magnetic Proof Plane 85 
 
 American Journal of Science (3), X, 14-17, 1875. 
 
 * The numbers refer to corresponding ones in the Bibliography, page 681. 
 
viii CONTENTS 
 
 PAGE 
 
 11. Studies on Magnetic Distribution 89 
 
 American Journal of Science (3), X, 325-335, 451-450, 1875. 
 
 Ibid., XI, 17-29, 103-108, 1876. 
 
 Philosophical Magazine (i\ L, 257-277, 348-367, 1875. 
 
 12. On the Magnetic Effect of Electric Convection 128 
 
 American Journal of Science (3), XV, 30-38, 1878. 
 
 13. Note on the Magnetic Effect of Electric Convection 138 
 
 Philosophical Magazine (5), VII, 442-443, 1879. 
 
 14. Note on the Theory of Electric Absorption 139 
 
 American Journal of Mathematics, I, 53-58, 1878. 
 
 15. Eesearch on the Absolute Unit of Electrical Eesistance 145 
 
 American Journal of Science (3), XV, 281-291, 325-336, 430-439, 1878. 
 
 17. On Professors Ayrton and Perry's NeAv Theory of the Earth's Mag- 
 
 netism, with a Note on a New Theory of the Aurora 179 
 
 Philosophical Magazine (5), VIII, 102-106, 1879. 
 Proceedings of the Physical Society, III, 93-98, 1879. 
 
 18. On the Diamagnetic Constants of Bismuth and Calc-spar in Absolute 
 
 Measure. By H. A. Rowland and W. W. Jacques 184 
 
 American Journal of Science (3), XVIII, 360-371, 1879. 
 
 19. Preliminary Notes on Mr. Hall's recent Discovery 197 
 
 American Journal of Mathematics, II, 354-356, 1879. 
 Philosophical Magazine (5), IX, 432-434, 1880. 
 Proceedings of the Physical Society, IV, 10-13, 1880. 
 
 22. On the Efficiency of Edison's Electric Light. By H. A. Rowland and 
 
 G. F. Barker 200 
 
 American Journal of Science (3), XIX, 337-339, 1880. 
 
 27. Electric Absorption of Crystals. By H. A. Rowland and E. L. 
 
 Nichols 204 
 
 Philosophical Magazine (5), XI, 414-419, 1881. 
 Proceedings of the Physical Society, IV, 215-221, 1881. 
 
 28. On Atmospheric Electricity 212 
 
 Johns Hopkins University Circulars Xo. 19, pp. 4, 5, 1882. 
 
 34. The Determination of the Ohm. Extract from a letter to the Inter- 
 
 national Congress at Paris, 1884 217 
 
 Proces-Verbaux, Deuxieme Session, p. 37. Paris, 1884. 
 
 35. The Theory of the Dynamo 219 
 
 Report of the Electrical Conference at Philadelphia in November, 1884, 
 pp. 72-83, 90, 91, 104, 107. Washington, 1886. 
 
 36. On Lightning Protection 236 
 
 Report of the Electrical Conference at Philadelphia in November, 1884, 
 pp. 172-174. 
 
 37. On the Value of the Ohm 239 
 
 La Lumiere Electrique, XXVI, pp. 188, 477, 1887. 
 
CONTEXTS 
 
 PAOE 
 
 38. On a Simple and Convenient Form of Water-battery ............... 241 
 
 American Journal of Science (3), XXXIII, 147, 1887. 
 
 Philosophical Magazine (5), XXIII, 303, 1887. 
 
 Johns Hopkins University Circulars No. 57, p. 80, 1887. 
 
 40. On an Explanation of the Action of a Magnet on Chemical Action. 
 
 By H. A. Rowland and Louis Bell ................................ 242 
 
 American Journal of Science (3), XXXVI, 39-47, 1888. 
 Philosophical Magazine (5), XXVI, 105-114, 1888. 
 
 43. On the Electromagnetic Effect of Convection-Currents. By H. A. 
 
 Kowland and C. T. Hutchinson .................................. 251 
 
 Philosophical Magazine (5), XXVH, 445-460, 1889. 
 
 44. On the Ratio of the Electro-static to the Electro-magnetic Unit of 
 
 Electricity. By H. A. Rowland, E. H. Hall, and L. B. Fletcher. . . 266 
 American Journal of Science (3), XXXVIII, 289-298, 1889. 
 Philosophical Magazine (5), XXVIII, 304-315, 1889. 
 
 47. Notes on the Theory of the Transformer .......................... 276 
 
 Philosophical Magazine (5), XXXIV, 54-57, 1892. 
 
 Electrical World, XX, 20, 1892. 
 
 Johns Hopkins University Circulars No. 99, pp. 104, 105, 1892. 
 
 48. Notes on the Effect of Harmonics in the Transmission of Power by 
 
 Alternating Currents ............................................ 280 
 
 Electrical World, XX, 368, 1892. 
 
 La Lumiere Electrique, XLVII, 42-44, 1893. 
 
 53. Modern Theories as to Electricity ................................. 285 
 
 The Engineering Magazine, VIII, 589-596, 1895. 
 
 60. Electrical Measurement by Alternating Currents .................. 294 
 
 American Journal of Science (4), IV, 429-448, 1897. 
 Philosophical Magazine (5), XLV, 66-85, 1898. 
 
 62. Electrical Measurements. By H. A. Rowland and T. D. Penniman.. 314 
 
 American Journal of Science (4), VIII, 35-57, 1899. 
 
 63. Resistance to Ethereal Motion. By H. A. Rowland, N. E. Gilbert and 
 
 P. C. McJunckin ................................................ 338 
 
 Johns Hopkins University Circulars No. 146, p. 60, 1900. 
 
 PART III. HEAT. 341 
 
 16. On the Mechanical Equivalent of Heat, with Subsidiary Researches 
 on the Variation of the Mercurial from the Air-Thermometer and 
 on the Variation of the Specific Heat of Water ................... 343 
 
 Proceedings of the American Academy of Arts and Sciences, XV, 75-200, 
 
 1880. 
 21. Appendix to Paper on the Mechanical Equivalent of Heat, Contain- 
 
 ing the Comparison with Dr. Joule's Thermometer ............... 469 
 
 Proceedings of the American Academy of Arts and Sciences, XVI, 38-45, 
 
 1881. 
 20. Physical Laboratory; Comparison of Standards ................... 477 
 
 Johns Hopkins University Circulars No. 3, p. 31, 1880. 
 
x CONTENTS 
 
 PAGE 
 
 26. On Geissler Thermometers 481 
 
 American Journal of Science (3), XXI, 451-453, 1881. 
 
 PART IV. LIGHT. 485 
 
 29. Preliminary Notice of the Eesults Accomplished in the Manufacture 
 
 and Theory of Gratings for Optical Purposes 487 
 
 Johns Hopkins University Circulars No. 17, pp. 248, 249, 1882. 
 Philosophical Magazine (4), XIII, 469-474, 1882. 
 Nature, 26, 211-213, 1882. 
 
 30. On Concave Gratings for Optical Purposes 492 
 
 American Journal of Science (3), XXVI, 87-98, 1883. 
 Philosophical Magazine (5), XVI, 197-210, 1883. 
 
 31. On Mr. Glazebrook's Paper on the Aberration of Concave Gratings. 505 
 
 American Journal of Science (3), XXVI, 214, 1883. 
 Philosophical Magazine (5), XVI, 210, 1883. 
 
 33. Screw 506 
 
 Encyclopaedia Britannica, Ninth Edition, Vol. 21. 
 
 39. On the Relative Wave-lengths of the Lines of the Solar Spectrum . . . 512 
 American Journal of Science (3), XXXIII, 182-190, 1887. 
 Philosophical Magazine (5), XXIII, 257-265, 1887. 
 
 41. Table of Standard Wave-lengths 517 
 
 Philosophical Magazine (5), XXVII, 479-484, 1889. 
 
 42. A Few Notes on the Use of Gratings 519 
 
 Johns Hopkins University Circulars No. 73, pp. 73, 74, 1889. 
 
 46. Report of Progress in Spectrum Work 521 
 
 The Chemical News, LXIII, 133, 1891. 
 
 Johns Hopkins University Circulars No. 85, pp. 41, 42, 1891. 
 
 American Journal of Science (3), XLI, 243, 244, 1891. 
 
 49. Gratings in Theory and Practice 525 
 
 Philosophical Magazine (5), XXXV, 397-419, 1893. 
 Astronomy and Astro-Physics, XII, 129-149, 1893. 
 
 50. A New Table of Standard Wave-lengths 545 
 
 Philosophical Magazine (5), XXXVI, 49-75, 1893. 
 Astronomy and Astro-Physics, XII,. 321-347, 1893. 
 
 51. On a Table of Standard Wave-lengths of the Spectral Lines 548 
 
 Memoirs of the American Academy of Arts and Sciences, XII, 101-186, 
 1896. 
 
 52. The Separation of the Rare Earths 565 
 
 Johns Hopkins University Circulars No. 112, pp. 73, 74, 1894. 
 
 57. Notes of Observation on the Rontgen Rays. By H. A. Rowland, N. 
 
 R. Carmichael and L. J. Briggs 571 
 
 American Journal of Science (4), I, 247, 248, 1896. 
 Philosophical Magazine (5), XLI, 381-382, 1896. 
 
CONTENTS xi 
 
 PAGE 
 
 58. Notes on Rontgen Bays. By H. A. Rowland, N. R. Carmichael and 
 
 L. J. Briggs 573 
 
 Electrical World, XXVII, 452, 1896. 
 
 59. The Eontgen Ray and its Relation to Physics 576 
 
 Transactions of the American Institute of Electrical Engineers, XIII, 
 403-410, 430, 431, 1896. 
 
 64. Diffraction Gratings 587 
 
 Encyclopaedia Britannica, New Volumes, III, 458, 459, 1902. 
 
 ADDRESSES 591 
 
 1. A Plea for Pure Science. Address as Vice-President of Section B of 
 
 the American Association for the Advancement of Science, Minne- 
 apolis, August 15, 1883 593 
 
 Proceedings of the American Association for the Advancement of Science, 
 XXXII, 105-126, 1883. 
 
 Science, II, 242-250, 1883. 
 
 Journal of the Franklin Institute, CXVI, 279-299, 1883. 
 
 2. The Physical Laboratory in Modern Education. Address for Com- 
 
 memoration Day of the Johns Hopkins University, February 22, 
 
 1886 614 
 
 Johns Hopkins University Circulars No. 50, pp. 103-105, 1886. 
 
 3. Address as President of the Electrical Conference at Philadelphia, 
 
 September 8, 1884 619 
 
 Report of the Electrical Conference at Philadelphia in September, 1884, 
 Washington, 1886. 
 
 4. The Electrical and Magnetic Discoveries of Faraday. Address at 
 
 The Opening of the Electrical Club House of New York City, 1888 . 638 
 Electrical Review, Feb. 4, 1888. 
 
 5. On Modern Views with Respect to Electric Currents. Address Be- 
 
 fore the American Institute of Electrical Engineers, New York, 
 
 May 22, 1889 653 
 
 Transactions of the American Institute of Electrical Engineers, VI, 342- 
 357, 1889. 
 
 6. The Highest Aim of the Physicist. Address as President of the 
 
 American Physical Society, New York, October 28, 1899 668 
 
 Science, X, 825-833, 1899. 
 
 American Journal of Science (4), VIII, 401-411, 1899. 
 
 Johns Hopkins University Circulars No. 143, pp. 17-20, 1900. 
 
 BIBLIOGRAPHY 679 
 
 DESCRIPTION OF THE DIVIDING ENGINES DESIGNED BY PRO- 
 FESSOR ROWLAND 689 
 
 INDEX. 699 
 
HENRY A. ROWLAND 
 COMMEMORATIVE ADDRESS 
 
 BY 
 
 DR. THOMAS C. MENDENHALL 
 
 [Delivered before an assembly of friends, Baltimore, October 26, 1901.] 
 
 In reviewing the scientific work of Professor Kowland one is most 
 impressed by its originality. In quantity, as measured by printed page 
 or catalogue of titles, it has been exceeded by many of his contem- 
 poraries; in quality it is equalled by that of only a very, very small 
 group. The entire collection of his important papers does not exceed 
 thirty or forty in number and his unimportant papers were few. When, 
 at the unprecedentedly early age of thirty-three years, he was elected 
 to membership in the National Academy of Sciences, the list of his 
 published contributions to science did not contain over a dozen titles, 
 but any one of not less than a half-dozen of these, including what may 
 properly be called his very first original investigation, was of such 
 quality as to fully entitle him to the distinction then conferred. 
 
 Fortunately for him, and for science as well, he liijed during a period 
 of almost unparalleled intellectual activity, and his work was done 
 during the last quarter of that century to which we shall long turn 
 with admiration and wonder. During these twenty-five years the num- 
 ber of industrious cultivators of his own favorite field increased enor- 
 mously, due in large measure to the stimulating effect of his own enthu- 
 siasm, and while there was only here and there one possessed of the 
 divine afflatus of true genius, there were many ready to labor most assid- 
 uously in fostering the growth, development, and final fruition of germs 
 which genius stopped only to plant. A proper estimate of the magni- 
 tude and extent of Eowland's work would require, therefore, a careful 
 examination, analytical and historical, of the entire mass of contribu- 
 tions to physical science during the past twenty-five years, many of 
 his own being fundamental in character and far-reaching in their influ- 
 ence upon the trend of thought, in theory and in practice. But it was 
 1 
 
2 HENRY A. ROWLAND 
 
 quality, not quantity, that he himself most esteemed in any perform- 
 ance; it was quality that always commanded his admiration or excited 
 him to keenest criticism; no one recognized more quickly than he a 
 real gem, however minute or fragmentary it might be, and by quality 
 rather than by quantity we prefer to judge his work to-day, as he would 
 himself have chosen. 
 
 Rowland's first contribution to the literature of science took the 
 form of a letter to The Scientific American, written in the early Autumn 
 of 1865, when he was not yet seventeen years old. Much to his sur- 
 prise this letter was printed, for he says of it, " I wrote it as a kind of 
 joke and did not expect them to publish it." Neither its humor nor 
 its sense, in which it was not lacking, seems to have been appreciated 
 by the editor, for by the admission of certain typographical errors he 
 practically destroyed both. The embryo physicist got nothing but a 
 little quiet amusement out of this, but in a letter of that day he de- 
 clares his intention of some time writing a sensible article for the 
 journal that so unexpectedly printed what he meant to be otherwise. 
 This resolution he seems not to have forgotten, for nearly six years 
 later there appeared in its columns what was, as far as is known, his 
 second printed paper and his first serious public discussion of a scientific 
 question. It was a keen criticism of an invention which necessarily 
 involved the idea of perpetual motion, in direct conflict with the great 
 law of the Conservation of Energy which Rowland had already grasped. 
 It was, as might be expected, thoroughly well done, and received not a 
 little complimentary notice in other journals. This was in 1871, the 
 year following that in which he was graduated as a Civil Engineer from 
 the Rensselaer Polytechnic Institute, and the article was written while 
 in the field at work on a preliminary railroad survey. A year later, 
 having returned to the Institute as instructor in physics, he published 
 in the Journal of the Franklin Institute an article entitled " Illustra- 
 tions of Resonances and Actions of a Similar Nature," in which he 
 described and discussed various examples of resonance or " sympa- 
 thetic " vibration. This paper, in a way, marks his admission to the 
 ranks of professional students of science and may be properly con- 
 sidered as his first formal contribution to scientific literature; his last 
 was an exhaustive article on spectroscopy, a subject of which he, above 
 all others, was master, prepared for a new edition of the Encyclopaedia 
 Britannica, not yet published. Early in 1873 the American Journal of 
 Science printed a brief note by Rowland on the spectrum of the Aurora, 
 sent in response to a kindly and always appreciated letter from Pro- 
 
COMMEMORATIVE ADDRESS 3 
 
 fessor George F. Barker, one of the editors of that journal. It is inter- 
 esting as marking the beginning of his optical work. For a year, or 
 perhaps for several years previous to this time, however, he had been 
 busily engaged on what proved to be, in its influence upon his future 
 career, the most important work of his life. To climb the ladder of 
 reputation and success by simple, easy steps might have contented 
 Eowland, but it would have been quite out of harmony with his bold 
 spirit, his extraordinary power of analysis and his quick recognition of 
 the relation of things. By the aid of apparatus entirely of his own 
 construction and by methods of his own devising, he had made an inves- 
 tigation both theoretical and experimental of the magnetic permea- 
 bility and the maximum magnetization of iron, steel and nickel, a 
 subject in which he had been interested in his boyhood. On June 9, 
 1873, in a letter to his sister, he says: " I have just sent off the results 
 of my experiments to the publisher and expect considerable from it; 
 not, however, filthy lucre, but good, substantial reputation." What 
 he did get from it, at first, was only disappointment and discourage- 
 ment. It was more than once rejected because it was not understood, 
 and finally he ventured to send it to Clerk Maxwell, in England, by 
 whose keen insight and profound knowledge of the subject it was 
 instantly recognized and appraised at its full value. Eegretting that 
 the temporary suspension of meetings made it impossible for him to 
 present the paper at once to the Eoyal Society, Maxwell said he would 
 do the next best thing, which was to send it to the Philosophical Maga- 
 zine for immediate publication, and in that journal it appeared in 
 August, 1873, Maxwell himself having corrected the proofs to avoid 
 delay. The importance of the paper was promptly recognized by 
 European physicists, and abroad, if not at home, Eowland at once took 
 high rank as an investigator. 
 
 In this research he unquestionably anticipated all others in the dis- 
 covery and announcement of the beautifully simple law of the magnetic 
 circuit, the magnetic analogue of Ohm's law, and thus laid the founda- 
 tion for the accurate measurement and study of magnetic permea- 
 bility, the importance of which, both in theory and practice during 
 recent years, it is difficult to overestimate. It has always seemed to 
 me that when consideration is given to his age, his training, and the 
 conditions under which his work was done, this early paper gives a 
 better measure of Eowland's genius than almost any performance of 
 his riper years. During the next year or two he continued to work 
 along the same lines in Troy, publishing not many, but occasional, 
 
4 HENRY A. BOWLAND 
 
 additions to and developments of his first magnetic research. There 
 was also a paper in which he discussed Kohlrausch's determination of 
 the absolute value of the Siemens unit of electrical resistance, fore- 
 shadowing the important part which he was to play in later years in the 
 final establishment of standards for electrical measurement. 
 
 In 1875, having been appointed to the professorship of physics in 
 the Johns Hopkins University, the faculty of which was just then 
 being organized, he visited Europe, spending the better part of a year 
 in the various centres of scientific activity, including several months at 
 Berlin in the laboratory of the greatest Continental physicist of his 
 time, von Helmholtz. While there he made a very important investi- 
 gation of the magnetic effect of moving electrostatic charges, a question 
 of first rank in theoretical interest and significance. His manner of 
 planning and executing this research made a marked impression upon 
 the distinguished Director of the laboratory in which it was done, and, 
 indeed, upon all who had any relations with Eowland during its pro- 
 gress. He found what von Helmholtz himself had sought for in vain, 
 and when the investigation was finished in a time which seemed incred- 
 ibly short to his more deliberate and painstaking associates, the Director 
 not only paid it the compliment of an immediate presentation to the 
 Berlin Academy, but voluntarily met all expenses connected with its 
 execution. 
 
 The publication of this research added much to Eowland's rapidly- 
 growing reputation, and because of that fact, as well as on account of 
 its intrinsic value, it is important to note that his conclusions have 
 been held in question, with varying degrees of confidence, from the day 
 of their announcement to the present. The experiment is one of great 
 difficulty and the effect to be looked for is very small and therefore 
 likely to be lost among unrecognized instrumental and observational 
 errors. It was characteristic of Eowland's genius that with compara- 
 tively crude apparatus he got at the truth of the thing in the very start. 
 Others who have attempted to repeat his work have not been uniformly 
 successful, some of them obtaining a wholly negative result, even when 
 using apparatus apparently more complete and effective than that first 
 employed by Eowland. Such was the experience of Lecher in 1884, 
 but in 1888 Eoentgen confirmed Eowland's experiments, detecting the 
 existence of the alleged effect. The result seeming to be in doubt, 
 Eowland himself, assisted by Hutchinson, in 1889 took it up again, 
 using essentially his original method but employing more elaborate and 
 sensitive apparatus. They not only confirmed the early experiments, 
 
COMMEMORATIVE ADDRESS 5 
 
 but were able to show that the results were in tolerably close agreement 
 with computed values. The repetition of the experiment by Himstedt 
 in the same year resulted in the same way, but in 1897 the genuineness 
 of the phenomenon was again called in question by a series of experi- 
 ments made at the suggestion of Lippmann, who had proposed a study 
 of the reciprocal of the Rowland effect, according to which variations 
 of a magnetic field should produce a movement of an electrostatically 
 charged body. This investigation, carried out by Cremieu, gave an 
 absolutely negative result, and because the method was entirely differ- 
 ent from that employed by Eowland and, therefore, unlikely to be 
 subject to the same systematic errors, it naturally had much weight 
 with those who doubted his original conclusions. Realizing the neces- 
 sity for additional evidence in corroboration of his views, in the Fall 
 of the year 1900, the problem was again attacked in his own laboratory 
 and he had the satisfaction, only a short time before his death, of 
 seeing a complete confirmation of the results he had announced a 
 quarter of a century earlier, concerning which, however, there had 
 never been the slightest doubt in his own mind. It is a further satis- 
 faction to his friends to know that a very recent investigation at the 
 Jefferson Physical Laboratory of Harvard University, in which Row- 
 land's methods were modified so as to meet effectively the objections 
 made by his critics, has resulted in a complete verification of his 
 conclusions. 
 
 On his return from Europe, in 1876, his time was much occupied 
 with the beginning of the active duties of his professorship, and 
 especially in putting in order the equipment of the laboratory over 
 which he was to preside, much of which he had ordered while in Europe. 
 In its arrangement great, many of his friends thought undue, promi- 
 nence was given to the workshop, its machinery, tools, and especially 
 the men who were to be employed in it. He planned wisely, however, 
 for he meant to see to it that much, perhaps most, of the work under 
 his direction should be in the nature of original investigation, for the 
 successful execution of which a well-manned and equipped workshop is 
 worth more than a storehouse of apparatus already designed and used 
 by others. 
 
 He shortly found leisure, however, to plan an elaborate research upon 
 the Mechanical Equivalent of Heat, and to design and supervise the 
 construction of the necessary apparatus for a determination of the 
 numerical value of this most important physical constant, which he 
 determined should be exhaustive in character and, for some time to 
 
6 HENRY A. EOWLAND 
 
 come, at least, definitive. While this work lacked the elements of 
 originality and boldness of inception by which many of his principal 
 researches are characterized, it was none the less important. While 
 doing over again what others had done before him, he meant to do it, 
 and did' do it, on a scale and in a way not before attempted. It was one 
 of the great constants of nature, and, besides, the experiment was one 
 surrounded by difficulties so many and so great that few possessed the 
 courage to undertake it with the deliberate expectation of greatly ex- 
 celling anything before accomplished. These things made it attractive 
 to Eowland. 
 
 The overthrow of the materialistic theory of heat, accompanied as 
 it was by the experimental proof of its real nature, namely, that it is 
 essentially molecular energy, laid the foundation for one of those two 
 great generalizations in science which will ever constitute the glory of 
 the nineteenth century. The mechanical equivalent of heat, the num- 
 ber of units of work necessary to raise one pound of water one degree 
 in temperature, has, with much reason, been called the Golden Number 
 of that century. Its determination was begun by an American, Count 
 Eumford, and finished by Rowland nearly a hundred years later. In 
 principle the method of Eowland was essentially that of Eumford. 
 The first determination was, as we now know, in error by nearly 40 
 per cent; the last is probably accurate within a small fraction of 1 per 
 cent. Eumford began the work in the ordnance foundry of the Elector 
 of Bavaria at Munich, converting mechanical energy into heat by means 
 of a blunt boring tool in a cannon surrounded by a definite quantity 
 of water, the rise in temperature of which could be measured. Eowland 
 finished it in an establishment founded for and dedicated to the in- 
 crease and diffusion of knowledge, aided by all the resources and refine- 
 ments in measurement which a hundred years of exact science had 
 made possible. As the mechanical theory of heat was the germ out 
 of which grew the principle of the conservation of energy, an exact 
 determination of the relation of work and heat was necessary to a 
 rigorous proof of that principle, and Joule, of Manchester, to whom 
 belongs more of the credit for this proof than to any other one man or, 
 perhaps, to all others put together, experimented on the mechanical 
 equivalent of heat for more than forty years. He employed various 
 methods, finally recurring to the early method of heating water by 
 friction, improving on Eumford's device by creating friction in the 
 water itself. Joule's last experiments were made in 1878, and most 
 of Eowland's work was done in the year following. It excelled that of 
 
COMMEMOBATIVE ADDRESS 7 
 
 Joule, not only in the magnitude of the quantities to be observed, but 
 especially in the greater attention given to the matter of thermometry. 
 In common with Joule and other previous investigators, he made use 
 of mercury thermometers, but this was only for convenience, and they 
 were constantly compared with an air thermometer, the results being 
 finally reduced to the absolute scale. By experimenting with water at 
 different initial temperatures he obtained slightly different values for 
 the mechanical equivalent of heat, thus establishing beyond question 
 the variability of the specific heat of water. Indeed, so carefully and 
 accurately was the experiment worked out that he was able to draw 
 the variation curve and to show the existence of a minimum value at 
 30 degrees C. 
 
 This elaborate and painstaking research, which is now classical, was 
 everywhere awarded high praise. It was published in full by the Amer- 
 ican Academy of Arts and Sciences with the aid of a fund originally 
 established by Count Eumford, and in 1881 it was crowned as a prize 
 essay by the Venetian Institute. Its conclusions have stood the test 
 of twenty years of comparison and criticism. 
 
 In the meantime, Rowland's interest had been drawn, largely per- 
 haps through his association with his then colleague, Professor Hast- 
 ings, toward the study of light. He was an early and able exponent 
 of Maxwell's Magnetic Theory and he published important theoretical 
 discussions of electro-magnetic action. Recognizing the paramount im- 
 portance of the spectrum as a key to the solution of problems in ether 
 physics, he set about improving the methods by which it was produced 
 and studied, and was thus led into what will probably always be re- 
 garded as his highest scientific achievement. 
 
 At that time, the almost universally prevailing method of studying 
 the spectrum was by means of a prism or a train of prisms. But the 
 prismatic spectrum is abnormal, depending for its character largely 
 upon the material made use of. The normal spectrum as produced by 
 a grating of fine wires or a close ruling of fine lines on a plane reflect- 
 ing or transparent surface had been known for nearly a hundred years, 
 and the colors produced by scratches on polished surfaces were noted 
 by Eobert Boyle, more than two hundred years ago. Thomas Young 
 had correctly explained the phenomenon according to the undulatory 
 theory of light, and gratings of fine wire and, later, of rulings on glass 
 were used by Fraunhofer who made the first great study of the dark 
 lines of the solar spectrum. Imperfect as these gratings were, Fraun- 
 hofer succeeded in making with them some remarkably good measures 
 
8 HENRY A. ROWLAND 
 
 of the length of light waves, and it was everywhere admitted that for 
 the most precise spectrum measurements they were indispensable. In 
 their construction, however, there were certain mechanical difficulties 
 which seemed for a time to be insuperable. There was no special 
 trouble in ruling lines as close together as need be ; indeed, Nobert, who 
 was long the most successful maker of ruled gratings, had succeeded in 
 putting as many as a hundred thousand in the space of a single inch. 
 The real difficulty was in the lack of uniformity of spacing, and on 
 uniformity depended the perfection and purity of the spectrum pro- 
 duced. Nobert jealously guarded his machine and method of ruling 
 gratings as a trade secret, a precaution hardly worth taking, for before 
 many years the best gratings in the world were made in the United 
 States. More than thirty years ago an amateur astronomer, in New 
 York City, a lawyer by profession, Lewis M. Rutherfurd, became inter- 
 ested in the subject and built a ruling engine of his own design. In 
 this machine the motion of the plate on which the lines were ruled 
 was produced at first by a somewhat complicated set of levers, for which 
 a carefully made screw was afterwards substituted. Aided by the skill 
 and patience of his mechanician, Chapman, Rutherfurd continued to 
 improve the construction of his machine until he was able to produce 
 gratings on glass and on speculum metal far superior to any made in 
 Europe. The best of them, however, were still faulty in respect to 
 uniformity of spacing, and it was impossible to cover a space exceeding 
 two or three square inches in a satisfactory manner. When Rowland 
 took up the problem, he saw, as, indeed, others had seen before him, 
 that the dominating element of a ruling machine was the screw by 
 means of which the plate or cutting tool was moved along. The ruled 
 grating would repeat all of the irregularities of this screw and would 
 be good or bad just as these were few or many. The problem was, 
 then, to make a screw which would be practically free from periodic 
 and other errors, and upon this problem a vast amount of thought and 
 experiment had already been expended. Rowland's solution of it was 
 characteristic of his genius; there were no easy advances through a 
 series of experiments in which success and failure mingled in varying 
 proportions ; " fire and fall back " was an order which he neither gave 
 nor obeyed, capture by storm being more to his mind. He was by 
 nature a mechanician of the highest type, and he was not long in devis- 
 ing a method for removing the irregularities of a screw, which aston- 
 ished everybody by its simplicity and by the all but absolute perfection 
 of its results. Indeed, the very first screw made by this process ranks 
 
COMMEMORATIVE ADDRESS 9 
 
 to-day as the most perfect in the world. But such an engine as this 
 might only be worked up to its highest efficiency under the most favor- 
 able physical conditions, and in its installation and use the most careful 
 attention was given to the elimination of errors due to variation of tem- 
 perature, earth tremors, and other disturbances. Not content, how- 
 ever, with perfecting the machinery by which gratings were ruled, Kow- 
 land proceeded to improve the form of the grating itself, making the 
 capital discovery of the concave grating, by means of which a large 
 part of the complex and otherwise troublesome optical accessories to 
 the diffraction spectroscope might be dispensed with. Calling to his 
 aid the wonderful skill of Brashear in making and polishing plane and 
 concave surfaces, as well as the ingenuity and patience of Schneider, 
 for so many years his intelligent and loyal assistant at the lathe and 
 workbench, he began the manufacture and distribution, all too slowly 
 for the anxious demands of the scientific world, of those beautifully 
 simple instruments of precision which have contributed so much to 
 the advance of physical science during the past twenty years. While 
 willing and anxious to give the widest possible distribution to these 
 gratings, thus giving everywhere a new impetus to optical research, 
 Eowland meant that the principal spoils of the victory should be his, 
 and to this end he constructed a diffraction spectrometer of extra- 
 ordinary dimensions and began his classical researches on the Solar 
 Spectrum. Finding photography to be the best means of reproducing 
 the delicate spectral lines shown by the concave grating, he became at 
 once an ardent student and, shortly, a master of that art. The out- 
 come of this was that wonderful " Photographic Map of the Normal 
 Solar Spectrum," prepared by the use of concave gratings six inches 
 in diameter and twenty-one and a half feet radius, which is recognized 
 as a standard everywhere in the world. As a natural supplement to 
 this he directed an elaborate investigation of absolute wave-lengths, 
 undertaking to give, finally, the wave-length of not only every line of 
 the solar spectrum, but also of the bright lines of the principal ele- 
 ments, and a large part of this monumental task is already completed, 
 mostly by Rowland's pupils and in his laboratory. 
 
 Time will not allow further expositions of the important conse- 
 quences of his invention of the ruling engine and the concave grating. 
 
 Indeed, the limitations to which I must submit compel the omission 
 of even brief mention of many interesting and valuable investigations 
 relating to other subjects begun and finished during these years of 
 activity in optical research, many of them by Eowland himself and 
 
10 HENRY A. KOWLAND 
 
 many of them by his pupils, working out his suggestions and con- 
 stantly stimulated by his enthusiasm. A list of titles of papers ema- 
 nating from the physical laboratory of the Johns Hopkins University 
 during this period would show somewhat of the great intellectual fertil- 
 ity which its director inspired, and would show, especially, his continued 
 interest in magnetism and electricity, leading to his important investi- 
 gations relating to electric units and to his appointment as one of the 
 United States Delegates at important International Conventions for 
 the better determination and definition of these units. In 1883 a com- 
 mittee appointed by the Electrical Congress of 1881, of which Rowland 
 was a member, adopted 106 centimetres as the length of the mercury 
 column equivalent to the absolute ohm, but this was done against his 
 protest, for his own measurements showed that this was too small by 
 about three-tenths of one per cent. His judgment was confirmed by 
 the Chamber of Delegates of the International Congress of 1893, of 
 which Rowland was himself President, and by which definitive values 
 were given to a system of international units. 
 
 Rowland's interest in applied science cannot be passed over, for it 
 was constantly showing itself, often, perhaps, unbidden, an unconscious 
 bursting forth of that strong engineering instinct which was born in 
 him, to which he often referred in familiar discourse, and which would 
 unquestionably have brought him great success and distinction had he 
 allowed it to direct the course of his life. Although everywhere looked 
 upon as one of the foremost exponents of pure science, his ability as an 
 engineer received frequent recognition in his appointment as expert 
 and counsel in some of the most important engineering operations in 
 the latter part of the century. He was an inventor, and might easily 
 have taken first rank as such had he chosen to devote himself to that 
 sort of work. During the last few years of his life he was much occu- 
 pied with the study of alternating electric currents and their applica- 
 tion to a system of rapid telegraphy of his own invention. A year ago 
 his system received the award of a grand prix at the Paris Exposition, 
 and only a few weeks after his death the daily papers published cable- 
 grams from Berlin announcing its complete success as tested between 
 Berlin and Hamburg, and also the intention of the German Postal 
 Department to make extensive use of it. 
 
 But behind Rowland, the profound scholar and original investigator, 
 the engineer, mechanician and inventor, was Rowland the man, and 
 any estimate of his influence in promoting the interests of physical 
 science during the last quarter of the nineteenth century would be 
 
COMMEMORATIVE ADDRESS 11 
 
 quite inadequate if not made from that point of view. Born at Hones- 
 dale, Pennsylvania, on November 27, 1848, he had the misfortune, at 
 the age of 11 years, to lose his father by death. This loss was made 
 good, as far as it is possible to do so, by the loving care of mother and 
 sisters during the years of his boyhood and youthful manhood. From 
 his father he inherited his love for scientific study, which from the very' 
 first seems to have dominated all of his aspirations, directing and con- 
 trolling most of his thoughts. His father, grandfather, and great- 
 grandfather were all clergymen and graduates of Yale College. His 
 father, who is described as one " interested in chemistry and natural 
 philosophy, a lover of nature and a successful trout-fisherman," had 
 felt, in his early youth, some of the desires and ambitions that after- 
 ward determined the career of his distinguished son, but yielding, no 
 doubt, to the influence of family tradition and desire, he followed the 
 lead of his ancestors. It is not unlikely, and it would not have been 
 unreasonable, that similar hopes were entertained in regard to the 
 future of young Henry, and his preparatory school work was arranged 
 with this in view. Before being sent away from home, however, he had 
 quite given himself up to chemical experiments, glass-blowing and other 
 similar occupations, and the members of his family were often sum- 
 moned by the enthusiastic boy to listen to lectures which were fully 
 illustrated by experiments, not always free from prospective danger. 
 His spare change was invested in copper wire and the like, and his first 
 five-dollar bill brought him, to his infinite delight, a small galvanic 
 battery. The sheets of the New York Observer, a treasured family 
 newspaper, he converted into a huge hot-air balloon, which, to the 
 astonishment of his family and friends, made a brilliant ascent and 
 flight, coming to rest, at last, and in flames, on the roof of a neighbor- 
 ing house, and resulting in the calling out of the entire fire department 
 of the town. When urged by his boy friends to hide himself from 
 the rather threatening consequences of his first experiment in aero- 
 nautics, he courageously marched himself to the place where his balloon 
 had fallen, saying, " No ! I will go and see what damage I have done/' 
 When a little more than sixteen years old, in the spring of 1865, he 
 was sent to Phillips Academy at Andover, to be fitted for entering the 
 academic course at Yale. His time there was given entirely to the 
 study of Latin and Greek, and he was in every way out of harmony 
 with his environment. He seems to have quickly and thoroughly ap- 
 preciated this fact, and his very first letter from Andover is a cry for 
 relief. "Oh, take me home!" is the boyish scrawl covering the last 
 
12 HENRY A. ROWLAND 
 
 page of that letter, on another of which he says, " It is simply horrible; 
 I can never get on here." It was not that he could not learn Latin and 
 Greek if he was so minded, but that he had long ago become wholly 
 absorbed in the love of nature and in the study of nature's laws, and 
 the whole situation was to his ambitious spirit most artificial and irk- 
 some. Time did not soften his feelings or lessen his desire to escape 
 from such uncongenial surroundings, and, at his own request, Dr. Far- 
 rand, Principal of the Academy at Newark, New Jersey, to which city 
 the family had recently removed, was consulted as to what ought to- 
 be done. Fortunately for everybody, his advice was that the boy ought 
 to be allowed to follow his bent, and, at his own suggestion, he was 
 sent, in the autumn of that year, to the Eensselaer Polytechnic Institute 
 at Troy, where he remained five years, and from which he was graduated 
 as a Civil Engineer in 1870. 
 
 It is unnecessary to say that this change was joyfully welcomed by 
 young Rowland. At Andover the only opportunity that had offered 
 for the exercise of his skill as a. mechanic was in the construction of a 
 somewhat complicated device by means of which he outwitted some of 
 his schoolmates in an early attempt to haze him and in this he took 
 no little pride. At Troy he gave loose rein to his ardent desires, and 
 his career in science may almost be said to begin with his entrance upon 
 his work there and before he was seventeen years old. 
 
 He made immediate use of the opportunities afforded in Troy and 
 its neighborhood for the examination of machinery and manufacturing 
 processes, and one of his earliest letters to his friends contained a clear 
 and detailed description of the operation of making railroad iron, the 
 rolls, shears, saws, and other special machines being represented in 
 uncommonly well executed pen drawings. One can easily see in this 
 letter a full confirmation of a statement that he occasionally made later 
 in life, namely, that he had never seen a machine, however complicated 
 it might be, whose working he could not at once comprehend. In 
 another letter, written within a few weeks of his arrival in Troy, he 
 shows in a remarkable way his power of going to the root of things 
 which even at that early age was sufficiently in evidence to mark him 
 for future distinction as a natural philosopher. On the river he saw 
 two boats equipped with steam pumps, engaged in trying to raise a 
 half -sun ken canal boat by pumping the water out of it. He described 
 engine?, pumps, etc., in much detail, and adds, "But there was one 
 thing that I did not like about it; they had the end of their discharge 
 pipe about ten feet above the water so that they had to overcome a 
 
COMMEMORATIVE ADDRESS 13 
 
 pressure of about five pounds to the square inch to raise the water so 
 high, and yet they let it go after they got it there, whereas if they had 
 attached a pipe to the end of the discharge pipe and let it hang down 
 into the water, the pressure of water on that pipe would just have 
 balanced the five pounds to the square inch in the other, so that they 
 could have used larger pumps with the same engines and ths have got 
 more water out in a given time." 
 
 The facilities for learning physics, in his day, at the Eensselaer Poly- 
 technic Institute were none of the best, a fact which is made the subject 
 of keen criticism in his home correspondence, but he made the most of 
 whatever was available and created opportunity where it was lacking. 
 The use of a turning lathe and a few tools being allowed, he spent all 
 of his leisure in designing and constructing physical apparatus of var- 
 ious kinds with which he experimented continually. All of his spare 
 money goes into this and he is always wishing he had more. While he 
 pays without grumbling his share of the expense of a class supper, he 
 cannot help declaring that " it is an awful price for one night's pleas- 
 ure; why, it would buy another galvanic battery." During these early 
 years his pastime was the study of magnetism and electricity, and his 
 lack of money for the purchase of insulated wire for electro-magnetic 
 apparatus led him to the invention of a method of winding naked 
 copper wire, which was later patented by some one else and made 
 much of. Within six months of his entering the Institute he had made 
 a delicate balance, a galvanometer, and an electrometer, besides a small 
 induction coil and several minor pieces. A few weeks later he an- 
 nounces the finishing of a Euhmkorff coil of considerable power, a 
 source of much delight to him and to his friends. In December, 1866, 
 he began the construction of a small but elaborately designed steam 
 engine which ran perfectly when completed and furnished power for 
 his experiments. A year later he is full of enthusiasm over an investi- 
 gation which he wishes to undertake to explain the production of 
 electricity when water comes in contact with red-hot iron, which he 
 attributes to the decomposition of a part of the water. Along with all 
 of this and much more he maintains a good standing in his regular work- 
 in the Institute, in some of which he is naturally the leader. He occa- 
 sionally writes: "I am head of my class in mathematics," or "I lead 
 the class in Natural Philosophy," but official records show that he was 
 now and then " conditioned " in subjects in which he had no special 
 interest. As early as 1868, before his twentieth birthday, he decided 
 that he must devote his life to science. While not doubting his ability 
 
14 HENRY A. EOWLAND 
 
 "to make an excellent engineer" as he declares, he decides against 
 engineering, saying, " You know that from a child I have been ex- 
 tremely fond of experiment; this liking instead of decreasing has gradu- 
 ally grown upon me until it has become a part of my nature, and it 
 would be folly for me to attempt to give it up; and I don't see any 
 reason why I should wish it, unless it be avarice, for I never expect 
 to be a rich man. I intend to devote myself hereafter to science. If 
 she gives me wealth, I will receive it as coming from a friend, but if 
 not, I will not murmur." 
 
 He realized that his opportunity for the pursuit of science was in 
 becoming a teacher, but no opening in this direction presenting itself 
 he spent the first year after graduation in the field as a civil engineer. 
 This was followed by a not very inspiring experience as instructor in 
 natural science in a Western college, where he acquired, however, 
 experience and useful discipline. 
 
 In the spring of 1872 he returned to Troy as instructor in physics, 
 on a salary the amount of which he made conditional on the purchase 
 by the Institute of a certain number of hundreds of dollars' worth of 
 physical apparatus. If they failed in this, as afterward happened, his 
 pay was to be greater, and he strictly held them to the contract. His 
 three years at Troy as instructor and assistant professor were busy, 
 fruitful years. In addition to his regular work he did an enormous 
 amount of study, purchasing for that purpose the most recent and most 
 advanced books on mathematics and physics. He built his electro- 
 dynamometer and carried out his first great research. As already 
 stated, this quickly brought him reputation in Europe and what he 
 prized quite as highly, the personal friendship of Maxwell, whose ardent 
 admirer and champion he remained to the end of his life. In April, 
 1875, he wrote, " It will not be very long before my reputation reaches 
 this country," and he hoped that this would bring him opportunity to 
 devote more of his time and energy to original research. 
 
 This opportunity for which he so much longed was nearer at hand 
 than he imagined. Among the members of the Visiting Board at the 
 West Point Military Academy in June, 1875, was one to whom had 
 come the splendid conception of what was to be at once a revelation and 
 a revolution in methods of higher education. In selecting the first 
 faculty for an institution of learning which, within a single decade, was 
 to set the pace for real university work in America, and whose influence 
 was to be felt in every school and college of the land before the end of 
 the first quarter of a century, Dr. Oilman was guided by an instinct 
 
15 
 
 which more than all else insured the success of the new enterprise. 
 A few words about Eowland from Professor Michie, of the Military 
 Academy, led to his being called to West Point by telegraph, and on 
 the banks of the Hudson these two walked and talked, " he telling me," 
 Dr. Oilman has said, " his dreams for science and I telling him my 
 dreams for higher education/' Eowland, with characteristic frank- 
 ness, writes of this interview, " Professor Gilman was very much 
 pleased with me," which, indeed, was the simple truth. The engage- 
 ment was quickly made. Eowland was sent to Europe to study labor- 
 atories and purchase apparatus, and the rest is history, already told and 
 everywhere known. 
 
 Eowland's personality was in many respects remarkable. Tall, erect 
 and lithe in figure, fond of athletic sports, there was upon his face a 
 certain look of severity which was, in a way, an index of the exacting 
 standard he set for himself and others. It did not conceal, however, 
 what was, after all, his most striking characteristic, namely, a perfectly 
 frank, open and simple straightforwardness in thought, in speech and 
 in action. His love of truth held him in supreme control, and, like 
 Galileo, he had no patience with those who try to make things appear 
 otherwise than as they actually are. His criticisms of the work of 
 others were keen and merciless, and sometimes there remained a sting 
 of which he himself had not the slightest suspicion. "I would not 
 have done it for the world," he once said to me after being told that 
 his pitiless criticism of a scientific paper had wounded the feelings of 
 its author. As a matter of fact he was warm-hearted and generous, and 
 his occasionally seeming otherwise was due to the complete separation, 
 in his own mind, of the product and the personality of the author. He 
 possessed that rare power, habit in his case, of seeing himself, not as 
 others see him, but as he saw others. He looked at himself and his own 
 work exactly as if he had been another person, and this gave rise to a 
 frankness of expression regarding his own performance which some- 
 times impressed strangers unpleasantly, but which, to his friends, was 
 one of his most charming qualities. Much of his success as an investi- 
 gator was due to a firm confidence in his own powers, and in the unerring 
 course of the logic of science which inspired him to cling tenaciously 
 to an idea when once he had given it a place in his mind. At a meeting 
 of the National Academy of Science in the early days of our knowledge 
 of electric generators, he read a paper relating to the fundamental 
 principles of the dynamo. A gentleman who had had large experience 
 with the practical working of dynamos listened to the paper, and at the 
 
16 HENRY A. ROWLAND 
 
 end said to the Academy that unfortunately practice directly contra- 
 dicted Professor Rowland's theory, to which instantly replied Rowland, 
 " So much the worse for the practice," which, indeed, turned out to be 
 the case. 
 
 Like all men of real genius, he had phenomenal capacity for concen- 
 tration of thought and effort. Of this, one who was long and intimately 
 associated with him remarks, " I can remember cases when he appeared 
 as if drugged from mere inability to recall his mind from the pursuit 
 of all-absorbing problems, and he had a triumphant joy in intellectual 
 achievement such as we would look for in other men only from the 
 gratification of an elemental passion." So completely consumed was 
 he by fires of his own kindling that he often failed to give due attention 
 to the work of others, and some of his public utterances give evidence 
 of this curious neglect of the historic side of his subject. 
 
 As a teacher his position was quite unique. Unfit for the ordinary 
 routine work of the class room he taught as more men ought to teach, 
 by example rather than by precept. Says one of his most eminent 
 pupils, " Even of the more advanced students only those who were able 
 to brook severe and searching criticism reaped the full benefit of being 
 under him, but he contributed that which, in a University, is above all 
 teaching of routine, the spectacle of scientific work thoroughly done 
 and the example of a lofty ideal." 
 
 Returning home about twenty years ago after an expatriation of 
 several years, and wishing to put myself in touch with the development 
 of methods of instruction in physics and especially in the equipment of 
 physical laboratories, I visited Rowland very soon after, as it happened, 
 the making of his first successful negative of the solar spectrum. That 
 he was completely absorbed in his success was quite evident, but he also 
 seemed anxious to give me such information as I sought. I questioned 
 him as to the number of men who were to work in his laboratory, and 
 although the college year had already begun he appeared to be unable 
 to give even an approximate answer. " And what will you do with 
 them ? " I said. " Do with them ? " he replied, raising the still drip- 
 ping negative so as to get a better light through its delicate tracings, 
 " Do with them ? I shall neglect them." The whole situation was in- 
 tensely characteristic, revealing him as one to whom the work of a drill- 
 master was impossible, but ready to lead those who would be led and 
 could follow. To be neglected by Rowland was often, indeed, more 
 stimulating and inspiring than the closest personal supervision of men 
 lacking his genius and magnetic fervor. 
 
COMMEMORATIVE ADDRESS 17 
 
 In the fulness of his powers, recognized as America's greatest physi- 
 cist, and one of a very small group of the world's most eminent, he died 
 on April 16, 1901, from a disease the relentless progress of which he had 
 realized for several years and opposed with a splendid but quiet courage. 
 
 It was Eowland's good fortune to receive recognition during his life 
 in the bestowal of degrees by higher institutions of learning; in elec- 
 tion to membership in nearly all scientific societies worthy of note in 
 Europe and America; in being made the recipient of medals of honor 
 awarded by these societies; and in the generously expressed words of 
 his distinguished contemporaries. It will be many years, however, be- 
 fore full measure can be had of his influence in promoting the interests 
 of physical science, for with his own brilliant career, sufficient of itself 
 to excite our profound admiration, must be considered that of a host 
 of other, younger, men who lighted their torches at his flame and who 
 will reflect honor upon him whose loss they now mourn by passing on 
 something of his unquenchable enthusiasm, something of his high 
 regard for pure intellectuality, something of his love of truth and his 
 sweetness of character and disposition. 
 
SCIENTIFIC PAPERS 
 
PART I 
 
 EARLY PAPERS 
 
THE VOKTEX PROBLEM 
 
 [Scientific American, XIII, 308, 1865] 
 
 Messrs. Editors: In a late number of your paper an inquiry was 
 made why a vortex was formed over the orifice of an outlet 1 pipe; as, 
 for instance, in a bath tub, when the water is running out. If the 
 water be first started, the explanation will be on the same principle 
 that a ball and string will, if started, wind itself up upon the hand; the 
 ball being attached to the string will, as the string winds up, get nearer 
 the hand, and, consequently, will have less far to go to make one revo- 
 lution, and thus the momentum, though perhaps not great enough to 
 carry it around in the great circle, is still sufficient to make it revolve 
 in the smaller one. 
 
 Therefore, as the string is continually winding up, and the ball con- 
 tinually nearing the hand, it will, if the resistance of the air is not too 
 great, continue to revolve until the string is wound up. Now, in the 
 case of the water, each particle of it will represent the ball, the force 
 of the water rushing toward the outlet will be the string, and, the water 
 running out, and thus causing the particles to come nearer the center 
 at every revolution, will represent the winding-up process. Thus, we 
 see this case is analogous to the preceding, and the same reason that 
 will apply to one will apply to the other. I suppose that some slight 
 motion existing among the particles of the water, united to the motion 
 produced by the outlet, causes the vortex to begin, and, once begun, it 
 will continue until the water is exhausted. 
 
 Such motion could either previously exist, or might be produced by 
 the form * of the vessel, which would cause the water, in running to 
 the outlet, to assume a certain direction. 
 
 H. A. R. 
 
 Troy, N. T., October, 1865. 
 
 '[In the original article this reads "outlet of an orifice," an obvious misprint.] 
 MIn the original article this word is "power," an obvious misprint.] 
 
PAINE'S ELECTRO-MAGNETIC ENGINE 
 
 [Scientific American, XXV, 21, 1871] 
 
 To the Editor of the Scientific American: 
 
 Having noticed several articles in your paper with reference to 
 Paine's electro-magnetic machine, I believe I cannot do better than 
 describe a visit which I paid it about three months ago. 
 
 Entering the office in company with a friend, at about twelve o'clock 
 one day, I was told that the machine was not running then, but would 
 be in operation at one. Proceeding there alone, at about that time, I 
 was, after the formality of sending up my name, conducted by a small 
 boy, through numerous by-ways and passages, to the second story of a 
 back building, where I was met by the illustrious inventor and a few 
 select friends. Mr. Paine began by showing the small model machines, 
 which he set in motion by a battery of four cups, of about a gallon 
 capacity each. These models revolved very well, but apparently with no 
 power, for they could be stopped easily. I then began to reason with 
 him on the absurdity of his position, and adduced in my support the 
 experiments of Joule, Mayer, Faraday and others. He, evidently, had 
 no very high opinion of these, and pronounced the conservation of force 
 an old fashioned idea, which had been overthrown in these enlightened 
 days by his " experiments," though what the latter were I have never 
 determined. 
 
 After conversing some time, to no purpose, he prepared to over- 
 throw me and my authority at one blow, by an exhibition of The 
 Machine. This was standing in front of a chimney, on one side of the 
 room, with the axis of its wheels parallel to the wall. The wheel to 
 which the magnets were attached was, unlike the models, inclosed in a 
 cast iron case, which enveloped it closely above, but spread out into a 
 rectangular base below. The latter rested directly on the floor. The 
 axis of the wheel projected on each side, and, to one end, a pulley was 
 attached, and to the other, the brake for operating the magnets. The 
 machine had the general appearance of a fan blower with an enlarged 
 pulley. The battery was attached to two binding screws, fixed to a 
 
PAINE'S ELECTBO-MAGNETIC ENGINE 25 
 
 standard on the chimney, and the current was supposed to pass from 
 these, along wires, to the break piece, and thence to the magnets. A 
 belt on the pulley connected with a shaft overhead, whence another belt 
 proceeded to the pulley of a small circular saw. 
 
 As soon as the connection was made with the battery, the whole 
 apparatus began to move, and soon the saw attained great velocity, 
 shaking the building with violence. The latter effect was caused by a 
 heavy fly wheel on the saw arbor, which probably was not well balanced. 
 When well in motion, boards were applied and sawed with the greatest 
 ease. To show the excess of power, they were sometimes placed on 
 edge and passed over the saw, so as wholly to envelop it, and the cut 
 made from end to end, without the velocity being at all diminished. 
 On throwing off the belt from the saw, the machine still proceeded at 
 the same velocity, with entire indifference to external resistance. On 
 mentioning this to Mr. Paine, he informed me that when the saw was 
 attached, and the resistance greater, the increased pull on the magnets 
 brought them nearer together, by bending the heavy iron frame; and, 
 as magnetic attraction varies inversely as the square of the distance, it 
 only required a small change of distance to account for the increased 
 power. I clearly indicated that I was skeptical on this point, and sug- 
 gested that it would also work without variation if the power pro- 
 ceeded from some well governed steam engine in the neighborhood. 
 On this he intimated that, if I were not careful, a force might proceed 
 from his body which would act in conjunction with gravitation in 
 causing me to be projected through the window, and strike with vio- 
 lence on the ground below. 
 
 The exhibition being over, on going down stairs in company with the 
 rest, I tried the door of the room below, but found it locked, and the 
 windows covered with papers. I desired to get in, but was met with 
 the assurance that the room was rented by a man who was then absent. 
 
 This, 1 believe, is the last visit paid by an outsider to this wonderful 
 invention. I have been there several times since, but there has been 
 no admittance to me, or to any one else. I have since been to the 
 owner of the building, and find that Mr. Paine rents the room to which 
 I sought admittance, and also rents power in that same room, which is 
 directly below that containing his machine. The engine from which 
 the power comes generally stops work at twelve and starts again at 
 one, but sometimes works all day. 
 
 My visits there have established the following facts: First, That 
 my friend and I were denied admittance at twelve o'clock, but were 
 
26 HENEY A. KOWLAND 
 
 invited to come at one. Second, That the shaft in the room below does 
 not revolve between the hours of twelve and one. Third, That the 
 room below, containing power, was rented by Mr. Paine, but that he 
 kept it carefully locked, and misguided me as to the tenant. Fourth, 
 That the working parts are concealed in an unnecessarily strong case, 
 well adapted to the concealment of another source of power. Fifth, 
 That part of the apparatus is attached to the wall, so that the machine 
 must always occupy the same position on the floor. Sixth, That the 
 models have not a power proportionate to their size. Seventh, That 
 the machine runs at the same velocity, whether producing one horse 
 power or a fraction of a horse power, and this without a governor. 
 
 These are the facts of the case. Where the power of the machine 
 comes from I am unable to say. Is there some secret connection be- 
 tween this machine and the shaft below, and does the battery serve 
 only to make this connection? Or does the battery, when applied, 
 connect the apparatus with a larger battery? I leave these questions 
 to others; but, unless the reasoning and experiments of a host of our 
 greatest men be false, and unless the greatest development of modern 
 science be overthrown, this machine cannot but derive its power from 
 some extraneous source. 
 
 In a late communication to your paper, Mr. Paine sets himself up 
 as the peer of Faraday, Tyndall and others, and gives as the reason, 
 his long devotion to science. He evidently does not consider that to 
 be ranked with such men requires something more than devotion; it 
 requires brains; brains to discriminate between true science and quack- 
 ish nonsense; brains to discover and originate. And pray what fact, 
 among the thousands of science, does Mr. Paine pretend to have proved 
 beyond doubt ? Let him answer. As to Mr. Paine's " science," I 
 assert that it is a tissue of error and ignorance, from beginning to end. 
 Even his vaunted invention of metallic foil, wherewith to envelop his 
 magnets or wire, can operate in no other manner than to the detriment 
 of his machine, as any such metallic coating lengthens the demagneti- 
 zation, which is the very thing to be guarded against. This is due to 
 an induced current, which forms in the coating, and, being in the same 
 direction as the primary current, operates in the same manner to keep 
 up the magnetism. His reason for the machine's keeping at the same 
 velocity also shows great ignorance of the subject. In the first place, 
 the law of magnetic force, under these circumstances, is stated entirely 
 wrong. For this case, the true law is complex, but most nearly ap- 
 proaches to that of inversely as the distance, instead of as the square of 
 
PAINE'S ELECTRO-MAGNETIC ENGINE 27 
 
 the distance. (See Joule, and also Tyndall, in the London, Edinburgh 
 and Dublin Philosophical Magazine for 1850.) And, in the second 
 place, approach of the poles would not necessarily increase the effi- 
 ciency; in this kind of machine there is a distance of maximum effi- 
 ciency; and if the magnets revolve at a distance greater than this, the 
 attraction becomes too small; and if at a less distance, the times of 
 magnetizing and demagnetizing the magnets become too great, and the 
 machine goes too slowly. The distance in this machine is, undoubtedly, 
 within the limit, for Mr. Paine prides himself upon its smallness, and 
 so further reduction, could it take place, can act in no other manner 
 than the opposite of that claimed. But it is my opinion that all the 
 force brought to bear on the magnets could not move them one two- 
 hundredth of an inch, when attached to such a frame. 
 
 As to Mr. Paine's disregard for the conservation of force, I have 
 little to say. His assertions are made directly in the face of this 
 principle, and yet he has never adduced one experiment, or even a plaus- 
 ible reason, to prove what he says. He takes you into a building where 
 shafts are revolving by the vulgar power of steam, and directs you to 
 look while he evokes power from nothing. You must not touch any- 
 thing; you must not enter the room below; you must not be there while 
 the engine next door is at rest; but you must simply look, and by that 
 renowned maxim of fools, that " seeing is believing/' you must believe 
 that the whole structure of science has fallen, and that above its ruins 
 nothing remains but Mr. Paine and his wonderful electro-magnetic 
 
 machine. 
 
 HENRY A. EOWLAND, C. E. 
 
 Newark, N. J. 
 
ILLUSTRATION OF RESONANCES AND ACTIONS OF A 
 SIMILAR NATURE 
 
 [Journal of the Franklin Institute, XCIV, 275-278, 18721 
 
 At the present day, when scientific education is beginning to take 
 its proper place in the public estimation, anything which can help 
 toward imparting a clear idea of any physical phenomenon becomes im- 
 portant. There are a number of these phenomena, of which resonance 
 is one, which play quite an important part in nature, but which as yet 
 have not been illustrated with sufficient clearness in the lecture-room. 
 Among these are the following: A person carrying water may so time 
 his steps as to produce waves which shall rise and fall in unison with 
 the motion of his body; soldiers in crossing a bridge must not keep 
 step, or they may transmit such a vibration to it as to break it down; 
 window-panes are sometimes cracked by sounding a powerful organ- 
 pipe to which they can vibrate ; a tuning-fork will respond to another of 
 equal pitch sounded near it; and others will readily suggest themselves 
 to the reader. In all these cases we have two bodies which can vibrate 
 in equal times, connected together either directly or by some medium 
 which transmits the motion from one to the other. We can, then, 
 readily reproduce the circumstances in the lecture-room. 
 
 The vibrating bodies which I have found most convenient are pendu- 
 lums; they are easily made, are seen well at a distance, and their time 
 of vibration can be easily and quickly regulated. The apparatus can 
 be prepared in the following manner: Fix a board, about a foot long, 
 in a horizontal position; suspend a piece cf small stiff wire, of equal 
 length, beneath its edge, parallel to it, and an inch or two distant, by 
 means of threads. To one end of the board suspend a pendulum, con- 
 sisting of a thread about ten or twenty inches long, to which is attached 
 a ball weighing two or three ounces; join the thread of this pendulum 
 to the horizontal wire by taking a turn of it around the wire, so that 
 when the pendulum oscillates, it causes the wire to move back and 
 forth in unison with it. To complete the apparatus, prepare a number 
 of small pendulums by suspending bullets to threads, and let them have 
 small hooks of wire to hang by. 
 
ILLUSTRATION OF KESONANCES 29 
 
 Having then set the heavy pendulum in motion, hang some of the 
 light ones on the horizontal wire, and note the result: those which are 
 shorter or longer than the heavy one will not be affected, but if any of 
 them are nearly of the same length, they will begin to vibrate to a 
 small extent, but will soon come to rest, after which they will com- 
 mence again, but stop as before ; but if any one happens to be of exactly 
 the proper length, its motion will soon become very great, and im- 
 mensely surpass in amplitude that of the heavy one, although the motion 
 is derived from it. Of course the heavy pendulum must be retarded in 
 giving motion to the light one, but it is hardly perceptible when there is 
 great difference in the weight. In the same manner a tuning-fork will 
 undoubtedly come to rest sooner when producing resonance than when 
 vibrating freely. To show this retardation more clearly, suspend two 
 pendulums, equal in weight and length, to the edge of a horizontal 
 board, and connect their two threads together by a horizontal thread 
 tied to each at a point an inch or two from the top, and drawn so tight 
 as to pull each of the pendulums a little out of plumb. On starting one 
 of these pendulums the other will gradually move, and finally absorb 
 all the motion from the first, and bring it entirely. to rest; the action 
 will then begin anew, and the motion will be entirely given back to the 
 first ball. This experiment differs from that of resonance, inasmuch 
 as in the case of the pendulums all the motion of the first ball is finally 
 stored up in the second; but in the case of resonance the confined air 
 is constantly giving out its motion to the atmosphere in waves of sound. 
 To imitate this to some extent we must attach a rather large piece of 
 paper to the second pendulum, so that it will meet with resistance, and 
 then both balls will come to rest sooner than otherwise. If one of the 
 balls is only two or three times heavier than the other, they will then 
 also interchange motions; but when the heavy ball has the motion, 
 the arc of its vibration will not be so great as that of the other when 
 it vibrates. 
 
 To illustrate the use of Helmholtz resonance globes, or Koenig's 
 apparatus for the analysis of sounds, we can enlarge and modify the 
 first apparatus somewhat. Make the board six or eight feet long, and 
 suspend at one end four or five of the heavy pendulums, and at the 
 other the same number of light ones, each of which corresponds in time 
 of vibration with one of the heavy ones. On now causing any of the 
 heavy pendulums to vibrate, as No. 3, we shall meet with no response 
 from any of the light ones except No. 7. If Nos. 1, 2 and 4 are set 
 going at one time, the wire A will be drawn hither and thither by the 
 
30 
 
 HENKY A. ROWLAND 
 
 conflicting pulls with no seeming regularity, but each of the balls 5, 
 6 and 8 will pick out from the confused motion the vibration due to 
 itself, and will move in unison, but No. 7 will remain quiet. The short 
 pendulums always produce the effect sooner than the long ones. To 
 remedy this to some extent it is well to bend the wire A into the shape 
 shown in the figure. It is not well to make the pendulum more than 
 twenty inches long, if a quick response is wished. There seems to be 
 no limit to the number of pendulums which can be used or the distance 
 to which the effect can be transmitted, though it is more decided when 
 there are but few pendulums and they are near together. It may some- 
 times be more convenient to suspend the pendulums from a wire, 
 
 :wm 
 
 tightly stretched, than from a board. To make the balls visible at a 
 distance, it may be well in some cases to make them of polished steel, 
 and illuminate them by a beam from the electric lamp. 
 
 These experiments have many advantages which recommend them to 
 teachers; they can be performed without purchased apparatus, and 
 can be made to illustrate resonance and the kindred phenomena in all 
 their details. Indeed, any one will be well repaid for spending an hour 
 in performing them, simply for their own beauty. 
 
4 
 
 ON THE AUKORAL SPECTRUM 
 
 I American Journal of Science [3], F, 320, 1873] 
 
 A letter from Henry A. Rowland, at present Instructor in Physics in 
 the Rensselaer Polytechnic Institute at Troy, informs us that he 
 observed the line of wave-length 431 in the auroral spectrum of last 
 October. He says : " The observations were made with an ordinary 
 chemical spectroscope of one prism, in which the scale was read by 
 means of a lamp. Great care was taken in the readings, and after com- 
 pleting them the spectroscope was set aside until morning, when the 
 readings were taken on the lines of comparison without altering the 
 instrument in any way or even regulating the slit. The wave-lengths 
 of the known lines were taken from Watts's * Index of Spectra/ but as 
 he does not give the wave-lengths of lines in the flame spectrum I am 
 not quite certain that they are correct." On the scale of his instru- 
 ment, Li a was at 13.5, Ca a 21, Naa27.5 , Ca/336 , Ca r 95.5, and 
 K/s 110. The aurora lines were as follows: 
 
 Scale-reading. Wave-lengths. 
 
 1 19 628.3 
 
 2 35.5 554.3 
 
 3 95 425 
 
 " The wave-lengths of the auroral lines were obtained by graphical 
 interpolation on such a large scale as to introduce little or no error." 
 
PART II 
 
 MAGNETISM AND ELECTRICITY 
 
ON MAGNETIC PERMEABILITY, 1 AND THE MAXIMUM OF 
 MAGNETISM OF IRON, STEEL, AND NICKEL 
 
 [Philosophical Magazine [4], XL VI, 140-159, 1873] 
 
 More than three years ago I commenced the series of experiments 
 the results of which I now publish for the first time. Many of the 
 facts which I now give were obtained then; but, for satisfactory reasons, 
 they were not published at that time. The investigations were com- 
 menced with a view to determine the distribution of magnetism on 
 iron bars and steel magnets; but it was soon found that little could be 
 done without new experiments on the magnetic permeability of sub- 
 stances. 
 
 Few observations have been made as yet for determining the mag- 
 netic permeability of iron, and none, I believe, of nickel and cobalt, in 
 absolute measure. The subject is important, because in all theories of 
 induced magnetism a quantity is introduced depending upon the mag- 
 netic properties of the substance, and without a knowledge of which 
 the problem is of little but theoretical interest; this quantity has 
 always been treated as a constant, although the experiments on the 
 maximum of magnetism show that it is a variable. However, the form 
 of the function has never been determined, except so far as we may 
 deduce it from the equation of Miiller, 
 
 which, as will be shown, leads to wrong results. The quantities used 
 by different persons are as follows: 
 
 , Neumann's coefficient, or magnetic susceptibility (Thomson). 
 
 Tc, Poisson's coefficient. 
 
 /*, coefficient of magnetization (Maxwell), or magnetic permeability 
 (Thomson). 
 
 ^-, introduced for convenience in the following paper. 
 
 1 The word "permeability" has been proposed by Thomson, and has the same 
 meaning as "conductivity" as used by Faraday ('Papers on Electricity and Magnet- 
 ism,' Thomson, p. 484; Maxwell's 'Electricity and Magnetism,' vol. ii, p. 51.) 
 
36 HEXRY A. ROWLAND 
 
 The relations of these quantities are given by the following equa- 
 tions : 
 
 , _ 
 - 
 
 3k A 
 
 The first determination of the value of any of these quantities was 
 made by Thalen. But more important experiments have been made 
 by Weber, Von Quintus Icilius, and more recently by M. Eeicke and 
 Dr. A. Stoletow. 2 The first three of these in their experiments used 
 long cylindrical rods, or ellipsoids of great length; the last, who has 
 made by far the most important experiments on this subject, has used 
 an iron ring. The method of the ring was first used by Dr. Stoletow 
 in September, 1871; but more than eight months before that, in Jan- 
 uary, 1871, I had used the same method, but with different apparatus, 
 to measure the magnetism. He plots a curve showing the variation of 
 K ; but he plots it with reference to E as abscissa instead of R * , and 
 thus fails to determine the law. His method of experiment is much 
 more complicated than mine, so that he could only obtain results for 
 one ring; while by my method I have experimented on about a dozen 
 rings and on numerous bars, so that I believe I have been enabled to 
 find the true form of the function according to which /* varies with the 
 magnetism of the bar or the magnetizing-force. 
 
 Many experiments have been made on the magnetism of iron without 
 giving the results in absolute measure. Among these are the experi- 
 ments of Muller, Joule, Lenz and Jacobi, Dub, and others. The ex- 
 periments have been made by the attraction of electromagnets, by the 
 deflection of a compass-needle, or, in one case, by measuring the in- 
 duced current in a helix extending the whole length of the bar. By 
 the last two methods the change in the distribution of magnetism over 
 the bar when the magnetism of the bar varies is disregarded, if indeed 
 it was thought of at all : even in a recent memoir of M. Cazin * we have 
 the statement made that the position of the poles is independent of the 
 strength of the current. He does not give the experiment from which 
 he deduces this result. Now it is very easy to show, from the formula 
 
 'Phil. Mag., January, 1873. 
 
 3 Annales de Chimie et de Physique, Feb., 1873, p. 171. 
 
MAGNETIC PERMEABILITY OF IROX, STEEL AND XICKEL 37 
 
 of Green for the distribution of magnetism on a bar-magnet combined 
 with the known variation of K, that this can only be true for short and 
 thick bars; and it has also been remarked by Thomson that this should 
 be the case. 4 An experiment made in 1870 places this beyond doubt. 
 A small iron wire (No. 16), 8 inches long, was wound with two layers of 
 fine insulated wire; a small hard steel magnet inch long suspended by 
 a fibre of silk was rendered entirely astatic by a large magnet placed 
 about 2 feet distant; the wire electromagnet was then placed near it, 
 so that the needle hung H inch from it and about 2 inches back from 
 the end. On now exciting the magnet with a weak current, the needle 
 took up a certain definite position, indicating the direction of the line 
 of force at that point. When the current was very much increased, the 
 needle instantly moved into a position more nearly parallel to the 
 magnet, thus showing that the magnetism was now distributed more 
 nearly at the ends than before. This shows that nearly all the experi- 
 ments hitherto made on bar-magnets contain an error; but, owing to 
 its small amount, we can accept the results as approximately true. 
 
 I believe mine are the first experiments hitherto made on-this subject 
 in which the results are expressed and the reasoning carried out in the 
 language of Faraday's theory of lines of magnetic force ; and the utility 
 of this method of thinking is shown in the method of experimenting 
 adopted for measuring magnetism in absolute measure, for which I 
 claim that it is the simplest and most accurate of any yet devised. 
 Whether Faraday's theory is correct or not, it is well known that its 
 use will give correct results; at the present time the tendency of the 
 most advanced thought is toward the theory 5 ; and indeed it has been 
 pointed out by Sir William Thomson that it follows, from dynamical 
 reasoning upon the magnetic rotation of the plane of polarization of 
 light, that the medium in which this takes place must itself be in 
 rotation, the axis of rotation being in the direction of the lines of 
 force. 8 Some substances must of necessity be more capable of assum- 
 ing this rotary motion than others; and hence arises the notion of 
 magnetic " conductivity '"' and " permeability." 
 
 Thomson has pointed out several analogies which may be used in 
 calculating the distribution and direction of the lines of force under 
 various circumstances. He has shown that the mathematical treatment 
 
 4 Papers on Electricity and Magnetism, p. 512. 
 
 5 "On Action at a Distance," Maxwell, 'Nature,' Feb. 27 and March 6 and 13, 1873. 
 "Thomson's 'Papers on Electricity and Magnetism,' p. 419, note; and Maxwell's 
 
 'Treatise on Electricity and Magnetism,' vol. ii, chap. xxi. 
 
38 HENRY A. EOWLAND 
 
 of magnetism is the same as that of the flow of heat in a solid, as the 
 static induction of electricity, and as the flow of a frictionless incom- 
 pressible liquid through a porous solid. It is evident that to these 
 analogies we may add that of the conduction of electricity. 7 We readily 
 see that the reason of the treatment being the same in each case is that 
 the elementary law of each is similar to Ohm's law. Mr. Webb 8 has 
 shown that this law is useful in electrostatics; and I hope, in a sequel 
 to this paper, to apply it to the distribution of magnetism: I give two 
 equations derived in this way further on. 
 
 The absolute units to which I have reduced my results are those in 
 which the metre, gramme, and second are the fundamental units. The 
 unit of magnetizing-force of helix I have taken as that of one turn 
 of wire carrying the unit current per metre of length of helix, and is 
 4?r times the unit magnetic field. This is convenient in practice, and 
 also because in the mathematical solution of problems in electrodynam- 
 ics the magnetizing-force of a solenoid naturally comes out in this unit. 
 The magnetizing-force of any helix is reduced to this unit by multiply- 
 ing the strength of current in absolute units by the number of coils in 
 the helix per metre of length. These remarks apply only to endless 
 solenoids, and to those which are very long compared with their diam- 
 eter. The unit of number of lines of force I have taken as the number 
 in one square metre of a unit field measured perpendicular to their 
 direction. As my data for reducing my results to these units, I have 
 taken the horizontal force of the earth's magnetism at Troy as 1-641, 
 and the total force as 6-27. 
 
 The total force, which will most seriously affect my results, is well 
 'known to be nearly constant at any one place for long periods of time. 
 
 From the analogy of a magnet to a voltaic battery immersed in water 
 I have obtained the following, on the assumption that // is constant, 
 and that the resistance to the lines of force passing out into the medium 
 is the same at every point of the bar. 
 
 Let R = resistance to lines of force of one metre of length of bar. 
 E' = resistance of medium along 1 metre of length of bar. 
 Q' = lines of force in bar at any point. 
 Q f = lines of force passing from bar along small distance I. 
 e =base of Napierian system of logarithms. 
 x = distance from one end of helix. 
 
 1 Maxwell's 'Treatise on Electricity and Magnetism,' arts. 243, 244 and 245. 
 s "Application of Ohm's Law to Problems in Electrostatics," Phil. Mag. S. 4, vol. 
 xxxv, p. 325 (188). 
 
MAGNETIC PERMEABILITY OF IRON, STEEL AND NICKEL 39 
 
 & = total length of helix. 
 
 s' = resistance at end of helix of the rest of bar and medium. 
 M = magnetizing-f orce of helix. 
 We then obtain 
 
 Ml -A / rx r (-*)-) (l\ 
 
 1M M 1 A 
 
 m - ~ A fe r 4-1 s n e r (-*)^ f9\ 
 
 s' ~f 2R A^- I ( 
 
 IJE 
 
 -VTT 
 
 in which 
 
 and 
 
 for near the centre of an infinitely long bar, where x > and < &, and 
 6=00 , we have 
 
 Q.= 0,and V=%. . .-'. (3) 
 For a ring-magnet, s' = 0; 
 
 .-. & = 0,and Q=X ...... (4) 
 
 And if a is the area of the bar or ring, 
 
 al =B = -ir ori = iSr ..... (5) 
 
 in which A is the same as in the equations previously given. These 
 equations show that we may find the value of ^, and hence the permea- 
 bility, by experimenting either on an infinitely long bar or on a ring- 
 magnet. Equations (4) evidently apply to the case where the diameter 
 of the ring is large as compared with its section. The fact given by 
 these equations can be demonstrated in another and, to some persons, 
 more satisfactory manner. If n is the number of coils per metre of 
 helix and n' the number on a ring-magnet, i the strength of current, 
 and p the distance from the axis of the ring to a given point in the 
 
 Formulae giving the same distribution as this have been obtained by Biot and 
 also by Green. See Biot's Traite de Physique, vol. iii, p. 77, 10 and 'Essay on the Ap- 
 plication of Mathematical Analysis to the Theories of Electricity and Magnetism,' 
 by Green, 17th section. 
 
 IO [In the original paper this was " vol. iv, p. 669." The correction was made later 
 by Professor Rowland.] 
 
40 HENRY A. KOWLAND 
 
 interior of the ring-solenoid, the magnetic field at that point will, as is 
 well known, be 
 
 2n'i - , 
 f> 
 
 and at a point within an infinitely long solenoid 
 
 If the solenoid contain any magnetic material, the field will be for 
 the ring 
 
 and for the infinite solenoid 
 
 4x/ttft, 
 
 Therefore the number of lines of force in the whole section of a ring- 
 magnet of circular section will be, if a is the mean radius of the ring, 
 
 S 
 
 Q'= n' in dx = 
 
 J B a x 
 
 or, since n' = 2 * an and M = in, we have, by developing, 
 
 Qf= ^jfoorj?) (i + \ f + i jr + & c .y . . (6) 
 
 For the infinite electromagnet we have in the same way for a circular 
 section, 
 
 Q' = 4*Mn(*B*) ......... (7) 
 
 When the section of the ring is thin, equation (6) becomes the same 
 as equation (7), and either of them will give 
 
 which is the same as equation (5). 
 
 In all the rings used the last parenthesis of (6) is so nearly unity 
 that the difference has in most cases been neglected, the slightest change 
 in the quality of the iron producing many times more effect on the 
 permeability than this. Whenever the difference amounted to more 
 than -^TT it was not rejected. 
 
 The apparatus used to measure Q' was based upon the fact discovered 
 by Faraday, that the current induced in a closed circuit is proportional 
 to the number of lines of force cut by the wire, and that the deflection 
 of the galvanometer-needle is also, for small deflections, proportional 
 to that number. In the experiments of 1870-71 an ordinary astatic 
 galvanometer was used; but in those made this year a galvanometer was 
 
MAGNETIC PERMEABILITY OF IRON, STEEL AND XICKEL 41 
 
 specially constructed for the purpose. It was on the principle of Thom- 
 son's reflecting instrument, but was modified to suit the case by increas- 
 ing the size of the mirror to of an inch, by adding an astatic needle 
 just above the coil without adding another coil, by loading the needle 
 to make it vibrate slowly, and, lastly, by looking at the reflected image 
 of the scale through a telescope instead of observing the reflection of a 
 lamp on the scale. The galvanometer rested on a firm bracket attached 
 to the wall of the laboratory near its foundation. In most of the ex- 
 periments the needle made about five single vibrations per minute. 
 The astatic needle was added to prevent any external magnetic force 
 from deflecting the needle; and directive force was given by the magnet 
 above. Each division of the scale was 075 inch long; and the extrem- 
 ities of the scale were reached by a deflection of 7 in the needle from 0. 
 The scale was bent to a radius of 4 feet, and was 3 feet from the instru- 
 ment. At first a correction was made for the resistance of the air, &c. ; 
 but it was afterwards found by experiment that the correction was very 
 exactly proportional to the deflection, and hence could be dispensed 
 with. This instrument gave almost perfect satisfaction; and its accu- 
 racy will be shown presently. 
 
 The tangent-galvanometer was also a very fine instrument, and was 
 constructed expressly for this series of experiments. The needle was 
 1*1 inch long, of hardened steel; and its deflections were read on a 
 circle graduated to half degrees, and 5 inches in diameter. The aver- 
 age diameter of the ring was 16^ inches nearly, and was wound with 
 several coils; so that the sensibility could be increased or diminished 
 at pleasure, and so give the instrument a very wide range. The value 
 of each coil in producing deflection was experimentally determined to 
 within at least ^ of 1 per cent by a method which I shall soon publish. 
 The numbers to multiply the tangent of the deflection by, in order to 
 reduce the current to absolute measure, were as follows: 
 
 Number of coils. Multiplier. 
 
 1 -05377 
 
 3 -01800 
 
 9 " . -006007 
 
 27 -002018 
 
 48 " . -001143 
 
 By this instrument I had the means of measuring currents which 
 varied in strength several hundred times with the same accuracy for 
 a large as for a small current. For greater accuracy a correction was 
 
42 HENEY A. ROWLAND 
 
 applied according to the formula of Blanchet and De la Prevostaye for 
 the length of the needle, the position of the poles being estimated; this 
 correction in the deflections used was always less than -6 per cent. To 
 eliminate any error in the position of the zero-point, two readings were 
 always taken with the currents in opposite directions, each one being 
 estimated with considerable accuracy to ^ of a degree. 
 
 The experiments were carried on in the assay laboratory of the 
 Institute, which was not being used at that time; and precautions were 
 taken that the different parts of the apparatus should not interfere 
 with each other. The disposition of the apparatus is represented in 
 Plate II. 
 
 The current from the battery A, of from two to six large Chester's 
 " electropoion " cells No. 2, joined according to circumstances, passed 
 to the commutator B, thence to the tangent-galvanometer C, thence 
 to another commutator D, thence around the magnet E (in this case a 
 ring), and then back through the resistance-coils K to the battery. To 
 measure the magnetism excited in E, a small coil of wire F was placed 
 around it, 11 which connected with the galvanometer H, so that, when 
 the magnetism was reversed by the commutator D, the current induced 
 in the coil F, due to twice cutting the lines of force of the ring, 
 produced a sudden swing of the needle of H. As the needle swung 
 very freely and would not of itself come to rest in ten or fifteen min- 
 utes, the little apparatus 7 was added : this consisted of a small horse- 
 shoe magnet, on one branch of which was a coil of wire ; and by sliding 
 this back and forth, induced currents could be sent through the wire, 
 which, when properly timed, soon brought the needle to rest. This 
 arrangement was very efficient; and without it this form of galvano- 
 meter could hardly have been used. To compare the magnetism of 
 the ring with the known magnetism of the earth, and thus reduce it to 
 absolute measure, a ring G supported upon a horizontal surface was 
 included in the circuit; when this was suddenly turned over, it produced 
 an induced current, due to twice cutting the lines of magnetic force 
 which pass through the ring from the earth's magnetism. The induced 
 current in the case of either coil, F or G, is proportional to the number 
 of the lines of force cut by the coils " and to the number of wires in the 
 coil, which latter is self evident, but may be deduced from the law of 
 Gaugain. 1 * It is evident, then, that if c is the deflection from coil G, 
 
 11 If a bar was used, this coil was placed at its centre. 
 
 12 Faraday's Experimental Researches, vol. iii, series 29. 
 13 Dagnin's Traite de Physique, vol. iii, p. 691. 
 
MAGNETIC PERMEABILITY OF IRON, STEEL AND NICKEL 43 
 
 and h that from helix F, the number of lines of force passing through 
 the magnet E, expressed in the unit we have chosen, will he 
 
 (9) 
 
 where ri is the number of coils in the ring G, n the number in the 
 helix F, R the radius of G, 6- 27 the total magnetism of the earth, and 
 7450' the dip. The quantity 2n'(6-27 sin 7450')^E 2 is constant for 
 the coil, and had the value 14* 15. This is the number of square metres 
 of a unit field which, when cut once by a wire from the galvanometer, 
 would produce the same deflection as the coil when turned over. 
 
 The experiments being made by reversing the magnetism of the bars, 
 a rough experiment was made to see whether they had time to change 
 in half a single vibration of the needle; it was found that this varied 
 from sensibly to nearly 1 second, so that there was ample time. It 
 was also proved that the sudden impulse given to the needle by the 
 change of current produced the same deflection as when the change was 
 more gradual, which has also been remarked by Faraday, though he 
 did not use such sudden induced currents. As a test of the method, 
 the horizontal force of the earth's magnetism was determined by means 
 of a vertical coil; it was found to be 1' 634. while the true quantity is 
 1-641. 
 
 It is sometimes assumed that some of the action in a case like the 
 present is due to the direct induction of the helix around the magnet on 
 the coil F. I think that this is not correct; for when the helix is of 
 fine wire closely surrounding the bar or ring, all the lines of force 
 which affect F must pass through the bar, and so no correction should 
 be made. However, the correction is so small that it will hardly affect 
 
 the result. If it were to be made, -^ (equation 5) should be diminished 
 
 CL 
 
 by 47r/lf ; but, for the above reasons, it has not been subtracted. As a 
 test of the whole arrangement, I have obtained the number of lines of 
 force in a very long solenoid: the mean of two solenoids gave me 
 
 Q' = 12-67 M(xR<); 
 while from theory we obtain, by equation (7) (n 1), 
 
 which is within the limits of error in measuring the diameter of the 
 tubes, &c. 
 
 All the rings and bars with which I have experimented have had a 
 circular section. In selecting the iron, care must be used to obtain a 
 
44 
 
 HEXET A. KOWLAND 
 
 homogeneous bar; in the case of a ring I believe it is better to have it 
 welded than forged solid; it should then be well annealed, and after- 
 wards have the outside taken off all round to about -J of an inch deep in 
 a lathe. This is necessary, because the iron is " burnt " to a consider- 
 able depth by heating even for a moment to a red heat, and a sort of 
 tail appears on the curve showing the permeability, as seen on plotting 
 Table III. To get the normal curve of permeability, the ring must only 
 be used once; and then no more current must be allowed to pass through 
 the helix than that with which we are experimenting at the time. If 
 by accident a stronger current passes, permanent magnetism is given to 
 the ring, which entirely changes the first part of the curve, as seen on 
 comparing Table I with Table II. The areas of the bars and rings were 
 always obtained by measuring their length or diameter across, and then 
 calculating the area from the loss of weight in water. The following 
 is a list of a few of the rings and bars used, the dimensions being given 
 in metres and grammes. In the fourth column " annealed " means 
 heated to a red heat and cooled in open air, " C annealed " means placed 
 in a large crucible covered with sand, and placed in a furnace, where, 
 after being heated to redness, the fire was allowed to die out ; " natural " 
 means that its temper was not altered from that it had when bought. 
 
 Results 
 given in 
 Table. 
 
 Quality of 
 substance. 
 
 How made. 
 
 Temper. 
 
 Spec, 
 grav. 
 
 Weight. 
 
 Mean 
 diam. 
 
 Area. 
 
 State. 
 
 
 
 
 
 
 
 
 0000 
 
 
 M 
 
 "Burden 
 best" iron. 
 
 Welded and 
 turned. 
 
 Annealed. 
 
 17-63 
 
 148-61 
 
 0677 
 
 916 
 
 Normal. 
 
 II. 
 
 u 
 
 11 <{ 
 
 u 
 
 7-63 
 
 148-61 
 
 0677 
 
 916 
 
 Magnetic. 
 
 III. 
 
 It II 
 
 " M 
 
 C an- 
 nealed. 
 
 17-63 
 
 148-01 
 
 0677 
 
 912 
 
 Burnt. 
 
 :v.j 
 
 Bessemer 
 steel. 
 
 Turned from 
 large bar. 
 
 Natural. 
 
 7-84 
 
 38-34 
 
 0420 
 
 371 
 
 Normal. 
 
 M 
 
 Norway 
 iron 
 
 Welded and 
 turned. 
 
 C an- 
 nealed. 
 
 J7-83 
 
 39-78 
 
 0656 
 
 7695 
 
 Magnetic. 
 
 VI. { 
 
 Cast 
 nickel. 14 
 
 Turned from 
 button. 
 
 .... 
 
 8-83 
 
 4-806 
 
 0200 
 
 0869 
 
 Normal. 
 
 VII. | 
 
 Stubs' 
 steel. 
 
 Hard-drawn 
 wire. 
 
 Natural. 
 
 7-73 
 
 
 
 0969 
 
 Normal. 
 
 
 
 The first three Tables are from the same ring. 
 
 Besides these I have used very many other bars and rings ; but most 
 of them were made before I had discovered the effect of burning upon 
 
 14 Almost chemically pure before melting. 
 
MAGNETIC PERMEABILITY OF IKON, STEEL AND NICKEL 45 
 
 the iron, and hence did not give a normal curve for high magnetizing- 
 powers. However, I have collected in Table VIII some of the results 
 of these experiments; but I have many more which are not worked 
 up yet. 
 
 In the following Tables Q= -^ has been measured as previously 
 
 described. It is evident that if, instead of reversing the current, we 
 simply break it, we shall obtain a deflection due to the temporary mag- 
 netism alone. In this manner the temporary magnetism has been 
 measured; and on subtracting this from Q, we can obtain the permanent 
 magnetism. 
 
 The following abbreviations are made use of in the Tables, the other 
 quantities being the same as previously described. 
 
 C.T.G. Number of coils of tangent-galvanometer used. 
 D.T.G. Deflection of tangent-galvanometer. 
 D.C. Deflection from coil G. 
 D.F. Deflection from helix F on reversing the current. 
 
 Q. Magnetic field in interior of bar (total). 
 D.B. Deflection from F on breaking current. 
 
 T. Magnetic field of bar due to temporary magnetism. 
 P. Magnetic field of bar due to permanent magnetism. 
 n. Number of coils in helix F. 
 
 Each observation given is almost always the mean of several. D.T.G. 
 is the mean of four readings, two before and two after the observations 
 on the magnetism; D.C. is the mean of from four to ten readings; D.F. 
 mean of three; D.B. mean of two, except in Table I, where the deflec- 
 tion was read only once. In all these Tables the column containing 
 the temporary magnetism T can only be accepted as approximate, the 
 experiments having been made more to determine Q than T. 
 
 The value of n was generally varied by coiling a wire more or less 
 around the ring, but leaving its length the same. 
 
 The change in the value of D.C. is due to the change in the resist- 
 ance of the galvanometer from change of temperature, copper wire 
 increasing in resistance about 1 per cent for every 2 -60. rise. In 
 Table I the temperature first increased slowly, and then, after remain- 
 ing stationary for a while, fell very fast. 
 
46 
 
 HEXEY A. BOWLAND 
 
 STABLE i. 
 
 " BURDEN BEST" IRON, NORMAL. 
 
 T. 
 M? 
 
 C.T.G. 
 
 D.T.G. 
 
 M. 
 
 B.C. 
 
 71. 
 
 D.F. 
 
 D.F. 
 2n. ' 
 
 D.B. 
 
 n. 
 
 Q. 
 
 A 
 
 A 
 
 Calcu- 
 lated. 
 
 A 
 ^=S- 
 
 T. 
 
 P. 
 
 P. 
 M.' 
 
 3627- 
 
 48 
 
 4-5 
 
 1456 
 
 23-4 
 
 30 
 
 6-6 
 
 1083 
 
 1 
 08 715 
 
 4910 
 
 5845 
 
 390-7 
 
 528 
 
 187- 
 
 1284- 
 
 7080- 
 
 
 16-45 
 
 5501 
 
 
 
 54-6 
 
 910 
 
 59 
 
 6005 
 
 10920 
 
 10885 
 
 868-7 
 
 3894 
 
 2111- 
 
 3838- 
 
 7746- 
 
 
 20-2 
 
 6815 
 
 
 
 87-9 
 
 1-465 
 
 80 
 
 9667 
 
 14180 
 
 14074 
 
 1129 
 
 5280 
 
 4387- 
 
 6437- 
 
 8786- 
 
 
 28-6 ! 1-011 
 
 23-3 
 
 io 
 
 74-2 
 
 3-71 
 
 1-34 
 
 24600 
 
 24330 
 
 24000 
 
 1936 
 
 8882 
 
 15718- 
 
 15550- 
 
 8766- 
 
 
 31-1 
 
 1-119 
 
 
 
 88-2 
 
 4-41 
 
 1-48 
 
 29230 
 
 26120 26050 
 
 2078 
 
 9811 
 
 19419- 
 
 naso- 
 
 8819- 
 
 
 31-9 
 
 1.155 
 
 
 
 92'6 
 
 4-63 
 
 1-53 
 
 30820 
 
 26690} 26660 
 
 2124 10180; 20640' 
 
 17870- 
 
 ?8205- 
 
 
 41-12 
 
 1-623 
 
 
 "z 
 
 28-8 
 
 7-45 
 
 2-0 
 
 49590 
 
 30570 
 
 30740 
 
 2433 13310 36280- 
 
 22370- 
 
 94BO- 
 
 27 
 
 28-35 
 
 1-766 
 
 23-1 
 
 
 32-8 
 
 8-20 
 
 2-5 
 
 54820 
 
 31030 
 
 31050 
 
 2470 
 
 16710 38110- 
 
 21570- 
 
 9517- 
 
 
 29-6 
 
 1-861 
 
 
 
 34-6 
 
 8-65 
 
 2-65 
 
 57820 
 
 31070 
 
 31100 
 
 2472 17710 40110' 
 
 21550- 
 
 8812- 
 
 
 33-4 
 
 2-162 
 
 23-1 
 
 
 39-8! 9-95 
 
 2-85 
 
 66510 
 
 30770 
 
 30776 2448 19050 1 47460- 
 
 21950- 
 
 8115- 
 
 
 37-45 
 
 2-512 
 
 
 
 44-711-18 
 
 3-05 
 
 74730 
 
 29750 
 
 29930 : 2367 20390 
 
 54340- 
 
 21630- 
 
 7985- 
 
 
 44-45 
 
 3-223 
 
 
 
 53-513-38 
 
 3-85 
 
 89430 
 
 27750 27390 ! 2208 25740 
 
 63690- 
 
 19760- 
 
 7674- 
 
 
 52-1 
 
 4-225 
 
 
 
 60-315-08 
 
 4-85 
 
 100800 
 
 23860 24730 : 1899 32420! 67380' 
 
 15950" 
 
 7070- 
 
 '9 
 
 34-65 
 
 6-744 
 
 
 
 73-1 
 
 18-28 
 
 7-10 
 
 122700 
 
 18210 
 
 18410 1448 47680 75020- 
 
 11130- 
 
 6519- 
 
 
 39-8 
 
 8-136 
 
 23-0 
 
 
 77-319-32 
 
 7-90 
 
 129700 
 
 15940 
 
 16130 1 1269 53040 76660- 
 
 9423- 
 
 6403- 
 
 
 44-3 
 
 9-543 
 
 
 "\ 
 
 40-620-30 
 
 9-1 
 
 136300 
 
 14280 
 
 13920 1137 611001 75200' 
 
 7881- 
 
 4666- 
 
 
 55-1 14-04 
 
 
 
 43-521-75 
 
 9-8 
 
 145400 
 
 10360 
 
 10760 
 
 824'1 65510- 79890- 
 
 5690- 
 
 2816- 
 
 '3 
 
 42-95 27-18 
 
 
 
 47-423-70 
 
 11-5 
 
 157700 
 
 5803 
 
 6350 
 
 461-8 
 
 76540; 81160- 
 
 2985- 
 
 2300- 
 
 
 51-3 36-60 
 
 
 
 49-124-55 
 
 12-7 
 
 162700 
 
 4445 
 
 4523 
 
 353.8 
 
 84180! 78520- 
 
 2145- 
 
 1702- 
 
 
 60-15 51-18 
 
 23-4 
 
 
 50-325-15 
 
 13-2 
 
 166000 
 
 3243 
 
 3310 
 
 358.0 
 
 87120, 78880- 
 
 1541- 
 
 
 
 
 00 
 
 
 
 
 
 
 175000 
 
 
 
 
 1 
 
 
 TABLE II. 
 "BURDEN BEST" IRON, MAGNETIC. 
 
 M. 
 
 Q. 
 
 A. 
 
 M. 
 
 M. 
 
 Q. 
 
 A. 
 
 M. 
 
 1456 
 
 426 
 
 2920 
 
 232 
 
 2-930 
 
 82720 
 
 28240 
 
 2247 
 
 5699 
 
 3346 
 
 5987 
 
 476 
 
 4-210 
 
 100900 
 
 23950 
 
 1906 
 
 6962 
 
 5700 
 
 8189 
 
 652 
 
 6-769 
 
 122800 
 
 18140 
 
 1444 
 
 1-080 
 
 24350 
 
 22550 
 
 1795 
 
 7.273 
 
 124300 
 
 17090 
 
 1360 
 
 1-191 
 
 29280 
 
 24580 
 
 1956 
 
 7-626 
 
 127100 
 
 16670 
 
 1326 
 
 1-537 
 
 46150 
 
 30020 
 
 2389 
 
 11-10 
 
 139500 
 
 12570 
 
 1000 
 
 1-590 
 
 49070 
 
 30260 
 
 2408 
 
 13-61 
 
 144700 
 
 10630 
 
 846 
 
 1-933 
 
 59680 
 
 30860 
 
 2456 
 
 22-10 
 
 154600 
 
 6965 
 
 554 
 
 2-377 
 
 71660 
 
 30150 
 
 2399 
 
 
 
 
 
 > TABLE III. 
 BURDEN BEST" IRON, BURNT. 
 
 M. 
 
 Q. 
 
 A. 
 
 M- 
 
 T. 
 
 M. 
 
 Q. 
 
 A. 
 
 M. 
 
 T. 
 
 P. 
 
 P. 
 
 143 
 
 1001 
 
 7039 
 
 560 
 
 1020 
 
 3.810 
 
 116900 
 
 30730 
 
 2446 
 
 
 8 
 
 
 .553 
 
 9395 
 
 16980 
 
 1351 
 
 5115 
 
 4-283 
 
 120200 
 
 28060 
 
 2233 
 
 
 4280- 
 
 
 682 
 
 16550 
 
 24240 
 
 1929 
 
 6835 
 
 4-722 
 
 123900 
 
 26240 
 
 2088 
 
 30830 
 
 9715- 
 
 
 962 
 
 37330 
 
 38780 
 
 3086 
 
 9454 
 
 6.565 
 
 133100 
 
 20270 
 
 1613 
 
 
 27876- 
 
 
 1-070 
 
 42920 
 
 40130 
 
 3194 
 
 10300 
 
 9-326 
 
 141200 
 
 15140 
 
 1200 
 
 3981032620- 
 
 
 1-153 
 
 48830 
 
 42340 
 
 3369 
 
 10530 
 
 11-00 
 
 144400 
 
 13120 
 
 1045 
 
 
 38300- 
 
 
 1-317 
 
 59490 
 
 45180 
 
 3595 
 
 11650 
 
 13-44 
 
 147500 
 
 10970 
 
 873 
 
 44070 
 
 47840- 
 
 103430- 
 
 1-340 
 
 59580 
 
 44450 
 
 3538 
 
 13700 
 
 23-41 
 
 155500 
 
 6642 
 
 529 
 
 51030 
 
 45880- 
 
 104470- 
 
 a 127 
 
 90180 
 
 42400 
 
 3374 
 
 18470 
 
 32-73 
 
 159400 
 
 4870 
 
 387 
 
 
 71710- 
 
 
 2-501 
 
 98560 
 
 39400 
 
 3136 
 
 19920 
 
 32-56 
 
 158400 
 
 48641 387 
 
 
 78640- 
 
 
 2-864 
 
 104000 
 
 36310 
 
 2890 
 
 24600 
 
 51-03 
 
 165800 
 
 3250 
 
 259 
 
 56100 
 
 79400- 
 
 109700- 
 
 3-151 
 
 108200 
 
 34330 
 
 2732 
 
 24610 
 
 
 
 
 
 
 83590- 
 
 
 15 [Columns 1, 15, 16 were added to the original paper by Professor Rowland, 
 after its publication.] 
 
 16 [The last two columns of Tables III, IV, V, VII were added by Professor Row- 
 land after the paper was published.] 
 
MAGNETIC PEEMEABILITY or IKON, STEEL AND XICKEL 47 
 
 STABLE iv. 
 
 BESSEMER STEEL, NORMAL. 
 
 M. 
 
 Q. 
 
 A. 
 
 M- 
 
 T. 
 
 M. 
 
 Q. 
 
 A. 
 
 *. 
 
 T. 
 
 P. 
 
 P. 
 
 1356 
 
 327 
 
 2412 
 
 192 
 
 309 
 
 2-756 
 
 39960 
 
 14500 
 
 1154 
 
 13080 
 
 IS- 
 
 26880- 
 
 2793 
 
 817 
 
 2995 
 
 238 
 
 727 
 
 3-219 
 
 50550 
 
 15700 
 
 1250 
 
 16350 
 
 90- 
 
 34200- 
 
 5287 
 
 1726 
 
 3264 
 
 260 
 
 1471 3-551 
 
 56310 
 
 15860 
 
 1262 
 
 15980 
 
 255- 
 
 40330- 
 
 9398 3833 
 
 4079 
 
 325 3106 
 
 4-469 
 
 71380 
 
 15970 
 
 1271 
 
 18340 
 
 727- 
 
 53040- 
 
 1-421 7702 
 
 5421 
 
 431 
 
 5576 
 
 5-698 
 
 85530, 15010 
 
 1195 
 
 23610 
 
 2126- 
 
 61920- 
 
 1-880 
 
 14080 
 
 7487 596 
 
 8972 
 
 11-44 
 
 119550 10450 
 
 832 
 
 28020 
 
 5108- 
 
 91530- 
 
 1-947 
 
 15420 
 
 7920 
 
 630 
 
 8938 
 
 20-69 
 
 138300 6685 
 
 532 
 
 41360 
 
 6482- 
 
 96940- 
 
 2-300 
 
 24830 
 
 10800 
 
 859 
 
 11320 
 
 38-99 
 
 153700 3942 
 
 314 
 
 52930 
 
 13510- 
 
 100770- 
 
 "TABLE V. 
 NORWAY IRON, MAGNETIC. 
 
 M. 
 
 Q. 
 
 A. 
 
 /* 
 
 T. 
 
 M. 
 
 Q. 
 
 A. 
 
 M. 
 
 T. 
 
 P. 
 
 P. 
 
 1344 
 
 865 
 
 6439 
 
 512 
 
 
 2-290 
 
 105900 
 
 46240 
 
 3680 
 
 35240 
 
 
 70660- 
 
 2673 
 
 2550 
 
 9910 
 
 759 1892 
 
 4-393)134100 
 
 30520 
 
 2429 
 
 54970 
 
 658- 
 
 79130- 
 
 516l! 13000 25200 
 
 2005 5857 
 
 5-910 
 
 142400 
 
 24090 
 
 1917 
 
 62810 
 
 7143- 
 
 79590- 
 
 5572 
 
 15310) 27480 
 
 2187 
 
 8110 
 
 7-874 
 
 149100 
 
 18940 
 
 1507 
 
 68490 
 
 7200- 
 
 80610- 
 
 6725 
 
 30140 44820 
 
 3567 
 
 8921 
 
 13-77 156800 
 
 11390 
 
 906 
 
 77060 
 
 21220- 
 
 79740 
 
 9305 
 
 53800J 57820 4602 
 
 13970 26-84 165800 
 
 6038 
 
 480 
 
 84710 
 
 39830- 
 
 81090- 
 
 1-362 
 
 77700 57110 4545 
 
 21630 
 
 36-86 
 
 168500 
 
 4572 
 
 364 
 
 87860 
 
 56070- 
 
 80740- 
 
 1-788 
 
 93000 
 
 52020 
 
 4140 
 
 28200 
 
 
 
 
 
 
 64800- 
 
 
 TABLE VI. 
 CAST NICKEL, NORMAL. 
 
 M. 
 
 Q. 
 
 A. 
 
 M- 
 
 T. 
 
 M. 
 
 Q. 
 
 A. 
 
 (* 
 
 T. 
 
 1-433 
 
 852 
 
 595 
 
 47-4 
 
 
 13-43 
 
 27100 
 
 2018 
 
 160-6 
 
 11260 
 
 2-904 2377 
 
 819 
 
 65-1 
 
 
 16-53 
 
 31050 
 
 1878 
 
 149-5 
 
 13530 
 
 3-527 
 
 3685 
 
 1070 
 
 85-1 
 
 
 21-02 
 
 34950 
 
 1663 
 
 132-3 
 
 16480 
 
 5-555 
 
 10080 
 
 1815 
 
 144-4 
 
 
 32-17 
 
 41980 
 
 1305 
 
 103-8 
 
 22300 
 
 6-783 
 
 13680 
 
 2017 
 
 160-5 
 
 5120 
 
 33-92 
 
 42650 
 
 1257 
 
 100-0 
 
 23360 
 
 7-401 15270 
 
 2063 
 
 164-2 
 
 5614 
 
 60-91 
 
 50860 
 
 855 
 
 66-4 
 
 29540 
 
 9-273 
 
 19600 
 
 2114 
 
 168-2 
 
 7644 
 
 82-36 
 
 53650 
 
 651 
 
 51.8 
 
 33460 
 
 11.78 24720 
 
 2098 
 
 167-0 
 
 9902 
 
 105-2 
 
 55230 
 
 525 
 
 41-8 
 
 35120 
 
 STABLE vn. 
 
 STUBS' STEEL WIRE, NORMAL. 
 
 M. Q. A. 
 
 M. 
 
 T. 
 
 M. 
 
 Q. 
 
 A. 
 
 /* 
 
 T 
 
 P. 
 
 P. 
 
 1673 159 953 75-9 
 
 
 13-65 
 
 54300 
 
 3978 
 
 316-6 
 
 20900 
 
 
 33400- 
 
 6237 678 1087 86-5 
 
 598 
 
 19-35 
 
 77770 4020 319-9 29480 
 
 80- 
 
 48290- 
 
 1.084 ! 1197 1104 87-9 
 
 1101 
 
 27-43100800 3676 292-6 38590 
 
 96- 
 
 62210- 
 
 2-043 ! 2448 1199 
 
 95-4 
 
 2257 
 
 33-39111300 3335 
 
 265-4 
 
 45110 
 
 191- 
 
 66190- 
 
 2-714 j 3446 1270 
 
 101-0 
 
 3095 
 
 35-58115000 3228 
 
 256-9 
 
 45950 
 
 351- 
 
 69050- 
 
 4-221 i 6278 1487 118-4 
 
 5145 
 
 38-64 
 
 119400 
 
 3092 
 
 246-0 48060 
 
 1133- 
 
 71340- 
 
 10-26 33700 3286 
 
 261 5 
 
 16170 
 
 
 
 
 
 17530- 
 
 
48 HENUY A. EOWLAND 
 
 The best method of studying these Tables is to plot them: one 
 method of doing this is to take the value of the magnetizing-force as 
 the abscissa, and that of the permeability as the ordinate; this is the 
 method used by Dr. Stoletow; but, besides making the complete curve 
 infinitely long, it forms a very irregular curve, and it is impossible to 
 get the maximum of magnetism from it. Another method is to employ 
 the same abscissas, but to use the magnetism of the bar as ordinates; 
 this gives a regular curve, but has the other two disadvantages of the 
 first method; however, it is often employed, and gives a pretty good 
 idea of the action. In Plate II, I have given a plot of Table V with 
 the addition of the residual or permanent magnetism, which shows the 
 general features of these curves as drawn from any of the Tables. It 
 is observed that the total magnetism of the iron at first increases very 
 fast as the magnetizing-force increases, but afterwards more and more 
 slowly until near the maximum of magnetism, where the curve is 
 parallel to the axis of Q. The concavity of the curve at its commence- 
 ment, which indicates a rapid increase of permeability, has been noticed 
 by several physicists, and was remarked by myself in my experiments of 
 January, 1871; it has now been brought most forcibly before the public 
 by Dr. Stoletow, whose paper refers principally to this point. 17 M. 
 Miiller has given an equation of the form 
 
 to represent this curve; but it fails to give any concavity to the first 
 part of the curve. A formula of the same form has been used by M. 
 Cazin ; 18 but his experiments carry little weight with them, on account 
 of the small variation of the current which he used, this being only 
 about five times, while I have used a variation in many cases of more 
 than three hundred times. 
 
 Weber has obtained, from the theory that the particles of the iron 
 are always magnetic and merely turn round when the magnetizing- 
 force is applied, an equation which would make the first part of the 
 curve coincide with the dotted line in Plate II ; 19 and Maxwell, by addi- 
 tion to the theory, has obtained an equation which replaces the first 
 
 17 On the Magnetizing Function of Soft Iron, especially with the weaker decom- 
 posing powers. By Dr. A. Stoletow, of the University of Moscow. Translated in 
 the Phil. Mag., January, 1873. See particularly p. 43. 
 
 18 Annales de Chimie et de Physique, February 1873, p. 182. 
 
 19 This is according to Maxwell's integration of Weber's equation, Weber having 
 made some mistake in the integration. 
 
MAGNETIC PERMEABILITY OF IRON, STEEL AND NICKEL 49 
 
 part of the curve by the broken line. 20 I believe that I have obtained 
 at the least a very close approximation to the true equation of the curve, 
 and will show further on that Q and M must satisfy the equation 
 
 D 
 
 It is very probable that Weber's theory may be so modified as to 
 give a similar equation. 
 
 Space will not permit me to discuss the curves of temporary and 
 permanent magnetism; but I will call attention to the following facts 
 which the Tables seem to establish. 
 
 1. Nearly or quite all the magnetism of a bar is, with weak magnetizing- 
 forces, temporary; and this is more apparent in steel than in soft iron. 
 
 2. The temporary magnetism increases continually with the current. 
 
 3. The permanent magnetism at first increases very fast with the current, 
 but afterwards diminishes as the current increases, when the iron is near 
 its maximum of magnetism. 21 
 
 I have now described the methods of plotting the Tables hitherto 
 used; and I will now describe the third, which is, I believe, new. This 
 is by using the values of the magnetism of the bar as abscissas, and 
 those of the permeability as ordinates. In this way we obtain a per- 
 fectly regular curve, which is of finite dimensions, and from which the 
 maximum of magnetism can be readily obtained. Plate III shows this 
 method of plotting as applied to Table I. If we draw straight lines 
 across the curve parallel to the axis of Q and mark their centres, we 
 find that they always fall very exactly upon a straight line, which is 
 therefore a diameter of the curve. The curve of nickel shown upon 
 the same Plate has this property in common with iron. I have made 
 several attempts to get a ring of cobalt; but the button has always 
 been too porous to use. However, I hope soon to obtain one, and thus 
 make the law general for all the magnetic metals. There are two 
 equations which may be used to express the curve : one is the equation 
 of an inclined parabola; but this fails for the two ends of the curve; 
 the other is an equation of the general form 
 
 (11) 
 
 20 Treatise on Electricity and Magnetism, Maxwell, vol. ii, chap. vi. 
 
 21 The last clause of this sentence cannot be considered yet as entirely settled, 
 though I have other curves than those shown here which show it well. [This note 
 was added to the original paper by Professor Rowland.] 
 
 4 
 
50 HEJSTRY A. ROWLAND 
 
 in which A, H, D, and a are constants depending upon the kind and 
 quality of the metal used. A is the maximum value of X, and gives 
 the height of the curve E D, Plate III; a establishes the inclination of 
 the diameter; H is the line A 0; and D depends upon the line A 0. 
 The following equation, adapted to degrees and fractions of a degree, 
 is the equation from which the values of ^ were found, as given in 
 Table I: 
 
 A = 81-100 sin 
 
 The large curve in Plate III was also drawn from this, and the dots 
 added to show the coincidence with observation; it is seen that this is 
 almost perfect. As X enters both sides of the equation, the calculation 
 can only be made by successive approximations. We might indeed solve 
 with reference to Q ; but in this case some values of ^ as obtained from 
 experiment may be accidentally greater than A, and so give an imagi- 
 nary value to Q. 
 
 By plotting any Table in this way and measuring the distance C, 
 we have the maximum of magnetism. 
 
 I have given in the same Plate the curve drawn from the observations 
 on the nickel ring with Q on the same scale, but ^ on a scale four times 
 as large as the other. The curve of nickel satisfies the equation 
 
 quite well, but not so exactly as in the case of iron. This ring, when 
 closely examined, was found to be slightly porous, which must have 
 changed the curve slightly, and perhaps made it depart from the 
 equation. 
 
 In Table VIII, I have collected some of the values of the constants 
 in the formula when it is applied to the different rings and bars, and 
 have also given some columns showing the maximum of magnetism. 
 When any blank occurs, it is caused by the fact that for some reason 
 or other the observations were not sufficient to determine it. The 
 values of a, H, D, and the value of X, when Q = 0, can in most cases 
 only be considered approximate ; for as they all vary so much, I did not 
 think it necessary to calculate them exactly. For comparison, I have 
 plotted Dr. Stoletow's curve and deduced the results given in the Table, 
 of course reducing them to the same units as mine. 
 
 It will be observed that the columns headed "maximum of mag- 
 netism " contain, besides the maximum magnetic field, two columns 
 
MAGNETIC PERMEABILITY OF IRON, STEEL AND NICKEL 51 
 
 * 
 
 M 
 
 O 
 
 5) (H 
 
 !i 
 
 c 
 
 'S "S 
 
 1=11 
 
 pa x- ^ 
 
 Burnt. 
 
 Normal. 
 Magnetic. 
 Normal. 
 
 ii 
 
 Burnt. 
 
 5 
 
 7. 
 
 Burnt, 
 
 Magnetic. 
 
 o 
 3 
 * 
 
 "* "7? 
 
 O O 
 
 o o o o 
 1-1 T*< e* 
 
 o 
 
 g 
 to 
 
 O O 
 O O 
 
 C5 to <N 
 
 c o 
 
 CO 
 
 
 
 -r 
 
 
 f- 
 
 o 
 o 
 
 o 
 o 
 
 
 > 
 
 o eg 
 
 r-l X CO CO 
 
 So 
 
 cocS 
 
 sg 
 
 i 
 
 00 
 
 
 
 
 ~c 
 
 t- t- 1- > 
 
 t- 
 
 i- i> t- 
 
 I- t- 
 
 i- 
 
 00 
 
 
 
 
 P 
 
 |8 
 
 O C5 
 
 1 1 
 
 o 
 
 1C 
 
 4 
 
 o o 
 
 . 00 35 
 
 
 
 
 o 
 
 1 
 
 
 
 X 
 
 o o 
 
 o o 
 
 
 
 1C CO 
 
 O 
 
 t- 
 
 O O O 
 
 O O 
 O O CO 
 
 O 
 
 o o 
 
 o o 
 
 c 
 
 
 
 = 
 
 
 
 P 
 
 o 
 
 o 
 
 o 
 
 o 
 
 CO 
 
 CO 
 
 
 
 0^00 00 
 
 co 
 
 :i2 
 
 ^ ^ 
 
 S 
 
 
 
 
 i 
 
 
 
 
 
 - 1 
 
 1 
 
 1 
 
 >o 
 
 
 
 b 
 
 - 
 
 5O 1- 1C 35 
 
 I-l 
 
 ^H 1C 00 
 
 i| 
 
 :r. 
 -f 
 
 1 
 
 >c 
 
 o 
 
 CO 
 
 o 
 
 04 
 
 Greatel 
 meabi 
 
 
 
 000 
 o o o 
 
 35 O i-( 35 
 
 CO -J ^-1 O 
 
 o 
 
 o 
 
 o o o 
 
 O O 
 
 
 
 to o 
 
 CM 
 
 O 
 
 
 ?! 
 
 Q 
 
 ?} 
 
 o 
 
 CO 
 OO 
 CO 
 
 O 
 1 1 
 
 t- 
 
 
 |ll 
 
 . O 5 O5 
 
 OO 
 
 iH t~ CO 
 
 
 
 cr. 
 
 to 
 
 oo 
 
 etism. 
 
 o c _ 
 So 
 
 go 
 
 ' I- t- 
 
 rH r-l 
 
 OO 
 H 
 
 CO t- t- 
 
 iH i-l TH 
 
 
 
 Jl 
 
 o* 
 
 o 
 
 00 
 
 i 
 
 e 
 
 S 
 
 3 
 
 Tension of 
 lines in kil. 
 per square 
 centim. 
 
 " i i i 1 
 
 ? 
 
 r-l r-t r-l 
 
 
 
 ? 
 
 1 
 
 
 
 S 
 "K 
 
 5 
 
 O O 
 O O 
 
 .00 
 
 i-H -H 
 
 I 177000 
 
 
 
 o o o 
 
 : 
 
 
 o 
 
 o 
 o 
 o 
 
 s 
 
 o 
 l- 
 
 1-H 
 
 
 Temper. 
 
 <u 
 
 4J ^ ; 2 
 
 C 
 
 a 
 < 
 
 Carefully 
 annealed. 
 
 II 
 
 Natural. 
 
 : = 
 
 i 
 
 C 
 
 
 |s 
 
 S a 
 o ^ 
 
 
 o 
 
 
 ** IT" 
 
 
 
 
 
 " 
 
 "^ 
 
 
 Quality of substanc 
 
 aj O ^ 
 
 "~ ' 
 
 Si 
 
 -3 W 
 1 
 
 s 
 
 a 
 
 " O) 
 
 2 
 
 1 
 
 Nickel 
 
 o 
 
 d 
 ^ 
 
 P 
 
 t 
 
 i 
 
 I 
 
 I ^Q 
 
 if. . if i 
 
 2 S 2 .S 
 
 ) SJD 
 
 III 
 
 PS pa 
 
 r 
 
 = 
 
 bi 
 
 ''2 
 
 '- 
 
 M 
 
 3 
 
52 HENRY A. EOWLAND 
 
 giving the tension of the lines of force per square centimetre and square 
 inch of section of the lines. These have been deduced from the formula 
 
 given by Maxwell ' 3 for the tension per square metre, which is 2C 
 
 &~ 
 
 absolute units of force. 
 This becomes 
 
 24655^00000 kil g rammes P er S( l uare centim > I 
 
 } , (12) 
 
 173240000 Ibs. per square inch, 
 
 from which the quantities in the Table were calculated. 
 
 It is seen that the maximum of magnetism of ordinary bar iron is 
 about 175,000 times the unit field, or 177 Ibs. on the square inch, and 
 for nickel 63,000 times, or 22-9 Ibs. on the square inch. For pure iron, 
 however, I think it may reach 180,000, or go even above that. It is 
 seen that one of the Norway rings gave a very high result; this is 
 explained by the following considerations. All the iron rings were 
 welded except this one, which was forged solid from a bar 2 inches 
 wide and then turned. Even the purest bar iron is somewhat fibrous; 
 and between the fibres we often find streaks of scale lying lengthwise 
 in the bar and so diminishing the section somewhat if the ring be 
 welded from the bar; when, however, it is forged solid, these streaks 
 are thoroughly disintegrated; and hence we find a higher maximum 
 of magnetism for a ring of this kind, and one approaching to that of 
 pure iron. But a ring made in this way has to be exposed to so much 
 heating and pounding that the iron is rendered unhomogeneous, and a 
 tail appears to the curve like that in Table III. It is evident that this 
 tail must always show itself whenever the section of the ring is not 
 homogeneous throughout. 
 
 Hence we may conclude that the greatest weight which can be sus- 
 tained by an electromagnet with an infinite current is, for good but not 
 pure iron, 354 Ibs. per square inch of section, and for nickel 46 Ibs. 
 
 Joule 2 * has made many experiments on the maximum sustaining- 
 power of magnets, and has collected the following Table, which I give 
 complete, except that I have replaced the result with his large magnet 
 by one obtained later. 
 
 It is seen that these are all below my estimate, as they should be. 
 
 23 Treatise on Electricity and Magnetism, vol. ii, p. 256. 
 2* Phil. Mag., 1851. 
 
MAGNETIC PERMEABILITY OF IRON, STEEL AND NICKEL 53 
 
 For comparison, I have added a column giving the values of Q which 
 would give the sustaining-power observed; some of these are as high 
 as any I have actually obtained, thus giving an experimental proof that 
 my estimate of 354 Ibs. cannot be far from correct, and illustrating 
 the beauty of the absolute system of electrical measurement by which, 
 from the simple deflection of a galvanometer-needle, we are able to 
 predict how much an electromagnet will sustain without actually trying 
 the experiment. 
 
 TABLE IX. 
 
 Magnet belonging to 
 
 Least area of 
 section, square 
 inch. 
 
 Weight 
 sustained. 
 
 Weight sus- 
 tained -r 
 least area. 
 
 Q. 
 
 f 1. . 
 
 10. 
 
 2775 
 
 277 
 
 154700 
 
 I 2. . 
 
 196 
 
 49 
 
 250 
 
 147000 
 
 Mr. Joule. ^ * 
 
 0436 
 
 12 
 
 275 
 
 154100 
 
 j 4 
 
 0012 
 
 202 
 
 162 
 
 118300 
 
 Mr. Nesbit 
 
 4-5 
 
 1428 
 
 317 
 
 165500 
 
 Prof. Henry 
 
 3-94 
 
 750 
 
 190 
 
 128200 
 
 Mr. Sturgeon 
 
 196 
 
 50 
 
 255 
 
 148500 
 
 
 
 
 
 
 In looking over the columns of Table VIII, which contain the values 
 of the constants in the formula, we see how futile it is to attempt to 
 give any fixed value to the permeability of iron or nickel; and we also 
 see of how little value experiments on any one kind of iron are. Iron 
 differs as much in magnetic permeability as copper does in electric 
 conductivity. 
 
 It is seen that in the three cases when iron bars have been used, the 
 value of a is negative; we might consider this to be a general law, if I 
 did not possess a ring which also gives this negative. All these bars 
 had a length of at least 120 times their diameter. 
 
 The mathematical theory of magnetism has always been considered 
 one of the most difficult of subjects, even when, as heretofore, fj. is 
 considered to be a constant; but now, when it must be taken as a func- 
 tion of the magnetism, the difficulty is increased many fold. There are 
 certain cases, however, where the magnetism of the body is uniform, 
 which will not be affected. 
 
 Troy, June 2, 1873. 
 
(54) 
 
ON THE MAGNETIC PEEMEABILITY AND MAXIMUM OF 
 MAGNETISM OF NICKEL AND COBALT 
 
 [Philosophical Magazine [4], XL VIII, 321-340, 1874J 
 
 Some time ago a paper of mine on the magnetic permeability of iron, 
 steel, and nickel was published in the Philosophical Magazine (August, 
 1873); and the present paper is to be considered as a continuation of 
 that one. But before proceeding to the experimental results, I should 
 like to make a few remarks on the theory of the subject. The mathe- 
 matical theory of magnetism and electricity is at present developed in 
 two radically different manners, although the results of both methods of 
 treatment are in entire agreement with experiment as far as we can 
 at present see. The first is the German method; and the second is 
 Faraday's, or the English method. When two magnets are placed near 
 each other, we observe that there is a mutual force of attraction or 
 repulsion between them. Now, according to the German philosophers, 
 this action takes place at a distance without the aid of any intervening 
 medium: they know that the action takes place, and they know the 
 laws of that action; but there they rest content, and seek not to find 
 how the force traverses the space between the bodies. The English 
 philosophers, however, led by Newton, and preeminently by Faraday, 
 have seen the absurdity of the proposition that two bodies can act upon 
 each other across a perfectly vacant space, and have attempted to ex- 
 plain the action by some medium through which the force can be trans- 
 mitted along what Faraday has called " lines of force." 
 
 These differences have given rise to two different ways of looking 
 upon magnetic induction. Thus if we place an electromagnet neat" a 
 compass-needle, the Germans would say that the action was due in part 
 to two causes the attraction of the coil, and the magnetism induced in 
 the iron by the coil. Those who hold Faraday's theory, on the other 
 hand, would consider the substance in the helix as merely " conduct- 
 ing " the lines of force, so that no action would be exerted directly on 
 the compass-needle by the coil, but the latter would only affect it in 
 virtue of the lines of force passing along its interior, and so there could 
 be no attraction in a perfectly vacant space. 
 
MAGNETIC PEEMEABILITY OF NICKEL AND COBALT 57 
 
 According to the first theory, the magnetization of the iron is repre- 
 sented by the excess of the action of the electromagnet over that of the 
 coil alone; while by the second, when the coil ia very close around the 
 iron, the whole action is due to the magnetization of the iron. The 
 natural unit of magnetism to be used in the first theory is that quantity 
 which will repel an equal quantity at a unit's distance with a unit of 
 force; on the second it is the number of lines of force which pass 
 through a unit of surface when that surface is placed in a unit field 
 perpendicular to the lines of force. The first unit is 4?r times the 
 second. Now when a magnetic force of intensity & 1 acts upon a mag- 
 netic substance, we shall have 33 = +4-$, in which 33 is the mag- 
 netization of the substance according to Faraday's theory, and is what 
 I formerly called the magnetic field, but which I shall hereafter call, 
 after Professor Maxwell, the magnetic induction. % is the intensity 
 of magnetization according to the German theory, expressed in terms 
 of the magnetic moment of the unit of volume. Now, when the sub- 
 stance is in the shape of an infinitely long rod placed in a magnetic field 
 
 01 
 
 parallel to the lines of force, the ratio 2 ==// is called the magnetic 
 
 
 
 permeability of the substance, and the ratio = K is Neumann's co- 
 efficient of magnetization by induction. Now experiment shows that 
 for large values of Q the values of both n and K decrease, so that 
 we may expect either $ or both 33 and % to attain a maximum value. 
 In my former paper I assumed that 33 as well as $ attain a maxi- 
 mum; but on further considering the subject I see that we have no data 
 for determining which it is at present. If it were possible for 53 to 
 attain a maximum value so that // should approach to 0, K would be 
 negative, and the substance would then become diamagnetic for very 
 high magnetizing forces. 2 This is not contrary to observation; for at 
 present we lack the means of producing a sufficiently intense magnetic 
 field to test this experimentally, at least in the case of iron. To pro- 
 duce this effect at ordinary temperatures, we must have a magnetic field 
 greater than the following for iron 175,000, for nickel 63,500, and for 
 
 1 1 shall hereafter in all my papers use the notation as given in Professor Maxwell's 
 ' Treatise on Electricity and Magnetism ;' for comparison with my former paper I 
 give the following: 
 
 33 in this paper = Q in former one. 
 
 6 " = 4;rM " 
 
 3 " =-M 
 
 'See Maxwell's 'Treatise on Electricity and Magnetism,' art. 844. J. C. M. 
 
58 HENEY A. ROWLAND 
 
 cobalt about 100,000 (?). These quantities are entirely beyond our 
 reach at present, at least with any arrangement of solenoids. Thus, 
 if we had a helix 6 inches in diameter and 3 feet long with an aperture 
 of 1 inch diameter in the centre, a rough calculation shows that, with 
 a battery of 350 large Bunsen cells, the magnetic field in the interior 
 would only be 15,000 or 20,000 when the coils were arranged for*the 
 best effect. We might obtain a field of greater intensity by means of 
 electromagnets, and one which might be sufficient for nickel; but we 
 cannot be certain of its amount, as I know of no measurement of the 
 field produced in this way. But our principal hope lies in heating some 
 body and then subjecting it to a very intense magnetizing-f orce ; for I 
 have recently found, and will show presently, that the maximum of 
 magnetization of nickel and iron decreases as the temperature rises, at 
 least for the two temperatures C. and 220 C. I am aware that iron 
 and nickel have been proved to retain their magnetic properties at high 
 temperatures, but whether they were in a field of sufficient intensity at 
 the time cannot be determined. The experiment is at least worth try- 
 ing by some one who has a magnet of great power, and who will take 
 the trouble to measure the magnetic field of the magnet at the point 
 where the heated nickel is placed. This could best be done by a small 
 coil of wire, as used by Verdet. 
 
 But even if it should be proved that 33 does not attain a maximum, 
 but only $, it could still be explained by Faraday's theory; for we 
 should simply have to suppose that the magnetic induction 33 was 
 composed of two parts the first part, 4 Trig, being due to the magnetic 
 atoms alone, and the second, >, to those lines of force which traversed 
 the aether between the atoms. To determine whether either of these 
 quantities has a maximum value can probably never be done by experi- 
 ment; we may be able to approach the point very nearly, but can never 
 arrive at it, seeing that we should need an infinite magnetizing-force to 
 do so. Hence its existence and magnitude must always be inferred 
 from the experiments by some such process as was used in my first 
 paper, where the curve of permeability was continued beyond the point 
 to which the experiments were carried. Neither does experiment up 
 to the present time furnish any clue as to whether it is 33 or $ which 
 attains a maximum. 
 
 As the matter is in this undecided state, I shall hereafter in most 
 cases calculate both $ and * as well as 33 and //, as I am willing to admit 
 that $ may have a physical significance as well as 33, even on Faraday's 
 theory. 
 
MAGNETIC PEEMEABILITY OF NICKEL AND COBALT 59 
 
 There is a difficulty in obtaining a good series of experiments on 
 nickel and cobalt which does not exist in the case of iron. It is prin- 
 cipally Giving to the great change in magnetic permeability of these 
 substances by heat, and also to their small permeability. To obtain 
 sufficient magnetizing-force to trace out the curve of permeability to a 
 reasonable distance, we require at least two layers of wire on the rings, 
 and have to send through that wire a very strong current. In this way 
 great heat is developed; and on account of there being two layers of 
 wire it cannot escape; and the ring being thus heated, its permeability 
 is changed. So much is this the case, that when the rings are in the 
 air, and the strongest current circulating, the silk is soon burned off the 
 wire; and to obviate this I have in these experiments always immersed 
 the rings in some non-conducting liquid, such as alcohol for low tem- 
 peratures and melted paraffin for high temperatures, the rings being 
 suspended midway in the liquid to allow free circulation. But I have 
 now reason to suspect the efficacy of this arrangement, especially in the 
 case of the paraffin. The experiments described in this paper were 
 made at such odd times as I could command, and the first ones were not 
 thoroughly discussed until the series was almost completed; hence 1 
 have not been so careful to guard against this error as I shall be in the 
 future. This can be done in the following manner namely, by letting 
 the current pass through the ring for only a shirt time. But there is a 
 difficulty in this method, because if the current is stopped the battery 
 will recruit, and the moment it is joined to the ring a large and rapidly 
 decreasing current will pass which it is impossible to measure accu- 
 rately. I have, however, devised the following method, which I will 
 apply in future experiments. It is to introduce into the circuit between 
 the tangent-galvanometer and the ring a current-changer, by which the 
 current can be switched off from the ring into another wire of the same 
 resistance, so that the current from the battery shall always be con- 
 stant. Just before making an observation the current is turned back 
 into the ring, a reading is taken of the tangent-galvanometer by an 
 assistant, and immediately afterward the current is reversed and the 
 reading taken for the induced current; the tangent-galvanometer is 
 then again read with the needle on the other side of the zero-point. 
 The pressure of outside duties at present precludes me from putting this 
 in practice. But the results which I have obtained, though probably 
 influenced in the higher magnetizing-forces by this heating, are still 
 so novel that they must possess value notwithstanding this defect; for 
 they contain the only experiments yet made on the permeability of 
 
60 HENRY A. KOWLAXD 
 
 cobalt at ordinary temperatures, and of iron, nickel, and cobalt at high 
 temperatures. 
 
 The rings of nickel and cobalt which I have used in the experiments 
 of this paper were all turned from buttons of metal obtained by fusing 
 under glass in a French crucible, it having been found that a Hessian 
 crucible was very much attacked by the metal. The crucibles were in 
 the fire three or four hours, and when taken out were very soft from 
 the intense heat. As soon as taken out, the outside of the crucible was 
 wet with water, so as to cool the metal rapidly and prevent crystalliza- 
 tion; but even then the cooling inside went on very slowly. As the 
 physical and chemical properties of these metals exercise great influence 
 on their magnetic properties, I will give them briefly. A piece of nickel 
 before melting was dissolved in HC1; it gave no precipitate with H 2 S , 
 and there were no indications of either iron or cobalt. A solution of 
 the cobalt gave no precipitate with H 2 S, but contained small traces of 
 iron and nickel. After melting the metals no tests have been made up 
 to the present time; but it is to be expected that the metals absorbed 
 some impurities from the crucibles. They probably did not contain 
 any carbon. One button of each metal was obtained, from each of 
 which two rings were turned. The cobalt was quite hard, but turned 
 well in the lathe, long shavings of metal coming off and leaving the 
 metal beautifully polished. The metal was slightly malleable, but fin- 
 ally broke with a fine granular fracture. The rings when made were 
 slightly sonorous when struck; and the color was of a brilliant white 
 slightly inclined to steel-color, but a little more red than steel. The 
 nickel was about as hard. as wrought iron, and was tough and difficult 
 to turn in the lathe, a constant application of oil being necessary, and 
 the turned surface was left very rough; the metal was quite malleable, 
 but would become hard, and finally fly apart when pounded down thin if 
 not annealed. When the rings were struck, they gave a dead sound as 
 if made of copper. In both cases the specific gravity was considerably 
 higher than that generally given for cast metal ; but it may be that the 
 metal to which they refer contained carbon, in which case it would be 
 more easily melted. There is great liability to error in taking the 
 specific gravity of these metals, because they contract so much on cool- 
 ing, and unless this is carried on rapidly crystals may form, between 
 which, as the metal contracts, vacant spaces may be left. As the 
 specific gravity of my rings approaches to that of the pure metals pre- 
 cipitated by hydrogen, I consider it evidence of their purity. The 
 dimensions of the rings and their other constants are as follows: 
 
VNI\ 
 
 MAGNETIC PERMEABILITY OF XICKEL AND COBALT 
 
 61 
 
 King. 
 
 Weight in 
 vacuo, in 
 grammes. 
 
 Loss in water 
 at 4 C.,in 
 grammes. 
 
 Specific 
 gravity. 
 
 Mean dia- 
 meter, in 
 centimetres. 
 
 Nickel No I 
 
 21-823 
 
 2-4560 
 
 8-886 
 
 3-28 
 
 Nickel No II 
 
 
 
 8-887 
 
 
 Cobalt No I 
 
 10-011 
 
 1 1435 
 
 8-7553 
 
 2-48 
 
 Cobalt No. II 
 
 4-681 
 
 5346 
 
 8 7550 
 
 1-81 
 
 
 
 
 
 
 Ring. 
 
 Mean circum- 
 ference, in 
 centimetres. 
 
 Number of 
 coils of wire 
 on ring. 
 
 Coils per 
 metre of cir- 
 cumference. 
 
 Area of sec- 
 tion, in square 
 centimetres. 
 
 Nickel No I 
 
 10 304 
 
 318 
 
 3086 
 
 2384 
 
 Nickel' No. II. 
 
 
 
 
 
 Cobalt, No. I 
 
 7-791 
 
 243 
 
 3119 
 
 1467 
 
 Cobalt No. II 
 
 5-686 
 
 158 
 
 2779 
 
 09403 
 
 
 
 
 
 
 Up to the present time cnly the rings whose dimensions are given 
 have been used. 
 
 The following Tables from the nickel ring No. I leave little to be 
 desired in point of regularity, and confirm the fact proved in my first 
 paper, that the laws deduced for iron hold also for nickel, and also 
 confirm the value given in my other paper for the maximum value of 
 magnetization of nickel. But the most important thing that they show 
 is the effect of heat upon the magnetization of nickel; and Table III 
 contains the first numerical data yet obtained on the effect of heat on 
 the magnetic properties of any substance. 
 
 As all the rings were wound with two layers of wire, a slight correc- 
 tion was made in the value of S) for the lines of inductive force which 
 passed through the air and not through the metal. In all the experi- 
 ments of this paper greater care was used to obtain T than in the first 
 paper. Each value of >, 33, and T is the mean of four readings. In 
 all the Tables I have left the order of the observations the same as that 
 in which they were made, and have also put down the date, as I now 
 have reason to suspect that the leaving of a ring in the magnetized state 
 in which it is after an experiment will in time affect its properties to a 
 small extent. Let me here remark that the time necessary to simply 
 make the observations is only a Very small fraction of that required to 
 prepare for them and to afterwards discuss them. And this, with the 
 small amount of time at my disposal, will account for the late day at 
 which I publish my results. 
 
 The following is the notation used, the measurements being made on 
 that absolute system in which the metre, gramme, and second are the 
 fundamental units. 
 
62 
 
 HENRY A. ROWLAND 
 
 $ is the magnetizing-force acting on the metal. 
 
 23 is the magnetic induction within the metal (see Maxwell's ' Trea- 
 tise on Electricity and Magnetism/ arts. 400, 592, and 604). 
 
 i 
 fj. is the magnetic permeability of the metal s=_=4*-H. 
 
 s? 
 T is the portion of 23 which disappears when the current is broken. 
 
 P is the portion of 33 which remains when the current is broken. 
 
 qa a 
 
 $ is the intensity of magnetization = - 
 
 ow 
 
 ic is Neumann's coefficient of induced magnetization = ^. 
 
 *Q 
 
 TABLE I. 
 
 CAST NICKEL, NOKMAL, AT 15 C. 
 Experiments made November 29, 1873. 
 
 a 
 
 S3 
 
 Ob- 
 served. 
 
 Calcu- 
 lated. 
 
 Error. 
 
 T. 
 
 P. 
 
 3. 
 
 K. 
 
 Ob- 
 served. 
 
 K. 
 
 Calcu- 
 lated. 
 
 Error. 
 
 12-84 
 
 675 
 
 52-6 
 
 46-4 
 
 6-2 
 
 
 
 52-7 
 
 4-10 
 
 3 65 
 
 -45 
 
 26-85 
 
 2169 
 
 80-8 
 
 80-6 
 
 .3 
 
 1263 
 
 906 
 
 170-5 
 
 6-35 
 
 6-27 
 
 08 
 
 45 14 
 
 7451 
 
 165-1 
 
 166-8 
 
 1-7 
 
 2894 
 
 4557 
 
 589-3 
 
 13-06 
 
 13-08 
 
 02 
 
 56-12 
 
 11140 
 
 198-5 
 
 199-1 
 
 6 
 
 3788 
 
 7352 
 
 882-0 
 
 15-72 
 
 15-70 
 
 02 
 
 70-78 
 
 15410 
 
 217-8 
 
 217-5 
 
 -3 
 
 5018 
 
 10392 
 
 1221 
 
 17-25 
 
 17-21 
 
 04 
 
 77-52 
 
 17100 
 
 220-6 
 
 220-6 
 
 
 
 5454 
 
 11646 
 
 1355 
 
 17-47 
 
 17-47 
 
 
 
 90-76 
 
 20180 
 
 222-3 
 
 222-0 
 
 - -3 
 
 6483 
 
 13697 
 
 1599 
 
 17-61 
 
 17-60 
 
 01 
 
 115-4 
 
 25170 
 
 218-2 
 
 214-3 
 
 3-9 
 
 8313 
 
 16857 
 
 1994 
 
 17-28 
 
 16-98 
 
 30 
 
 139-4 
 
 28540 
 
 204-7 
 
 204-3 
 
 -4 
 
 10100 
 
 18440 
 
 2260 
 
 16-21 
 
 16-18 
 
 .03 
 
 172-9 
 
 32460 
 
 187-8 
 
 186-6 
 
 1-2 
 
 12530 
 
 19930 
 
 2569 
 
 14-86 
 
 14-93 
 
 07 
 
 195-3 
 
 34630 
 
 177-3 
 
 179-1 
 
 1-8 
 
 13320 
 
 21310 
 
 2740 
 
 14-03 
 
 14-12 
 
 09 
 
 229-5 
 
 37340 
 
 162-8 
 
 165-5 
 
 2-7 
 
 15720 
 
 21620 
 
 2953 
 
 12-87 
 
 13-02 
 
 15 
 
 275-9 
 
 40860 
 
 148-1 
 
 146-3 
 
 1-8 
 
 17960 
 
 22900 
 
 3230 
 
 11-71 
 
 11-46 
 
 25 
 
 415-2 
 
 46470 
 
 111-9 
 
 112-8 
 
 9 
 
 22560 
 
 23910 
 
 3665 
 
 8-82 
 
 8-77 
 
 05 
 
 727-0 
 
 52690 
 
 72-5 
 
 72-8 
 
 3 
 
 28020 
 
 24670 
 
 4135 
 
 5-69 
 
 5-64 
 
 05 
 
 1042 
 
 55680 
 
 53-4 
 
 52-8 
 
 -6 
 
 30680 
 
 25000 
 
 4344 
 
 4-17 
 
 4-17 
 
 
 
 
 63420 
 
 
 
 
 
 
 
 4940 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 ooo 
 
 = 222 sin 
 
 /"= 
 
 359 
 
 =17 6 sin 
 
 28 
 
 TABLE II. 
 
 CAST NICKEL, MAGNETIC, AT 12 C. 
 Experiments made December 6, 1873. 
 
 6. 
 
 to. 
 
 M. 
 
 T. 
 
 P. 
 
 3- 
 
 K. 
 
 23-25 
 
 1245 
 
 53-55 
 
 
 
 97-2 
 
 4-18 
 
 47-69 
 
 7786 
 
 163-3 
 
 3095 
 
 4691 
 
 615-8 
 
 12-91 
 
 57-78 
 
 11460 
 
 198-3 
 
 3740 
 
 7720 
 
 907-3 
 
 15-70 
 
 73-43 
 
 16040 
 
 218-5 
 
 5032 
 
 11008 
 
 1270-6 
 
 17-30 
 
 88-23 
 
 19790 
 
 224-3 
 
 6554 
 
 13236 
 
 1568 
 
 17-77 
 
 107-3 
 
 23530 
 
 219-2 
 
 7620 
 
 15910 
 
 1864 
 
 17-36 
 
 153-8 
 
 30160 
 
 196-1 
 
 10940 
 
 19220 
 
 2388 
 
 15-52 
 
 206-3 
 
 35880 
 
 174-0 
 
 14030 
 
 21850 
 
 2839 
 
 13-76 
 
 296-4 
 
 41310 
 
 139-4 
 
 18390 
 
 22920 
 
 3264 
 
 11-01 
 
 421-8 
 
 46520 
 
 110-3 
 
 22520 
 
 24000 
 
 3668 
 
 8-70 
 
MAGNETIC PERMEABILITY OF NICKEL AND COBALT 
 
 63 
 
 TABLE III. 
 
 CAST NICKEL, MAGNETIC, AT 220 C. 
 Experiments made December 6, 1873. 
 
 . 
 
 as. 
 
 n- 
 
 T. 
 
 P. 
 
 3- 
 
 K. 
 
 22-60 
 
 4502 
 
 199-2 
 
 2671 
 
 1831 
 
 356-4 
 
 15-77 
 
 45-06 
 
 14000 
 
 310-8 
 
 5470 
 
 8530 
 
 1111 
 
 24-65 
 
 52-96 
 
 16660 
 
 314-6 
 
 6350 
 
 10310 
 
 1322 
 
 24-96 
 
 67-42 
 
 20300 
 
 301-1 
 
 7722 
 
 12578 
 
 1602 
 
 23-88 
 
 80-69 
 
 22540 
 
 279-3 
 
 8914 
 
 13626 
 
 1787 
 
 22-15 
 
 106-4 
 
 26420 
 
 248-3 
 
 11140 
 
 15280 
 
 2094 
 
 19-68 
 
 150-8 
 
 30740 
 
 203-8 
 
 14040 
 
 16700 
 
 2434 
 
 16-14 
 
 191-0 
 
 33530 
 
 175-6 
 
 15940 
 
 17590 
 
 2653 
 
 13-89 
 
 294-8 
 
 38300 
 
 129-9 
 
 20240 
 
 18060 ! 3024 
 
 10-26 
 
 553-6 
 
 42630 
 
 77-0 
 
 24360 
 
 18270 3348 6-05 
 
 789-8 
 
 43900 
 
 55-6 
 
 26060 
 
 17840 
 
 3431 
 
 4-345 
 
 Experiments made December 10, 1873. 
 
 13-00 
 
 1537 
 
 118-2 
 
 
 
 109-2 
 
 9-33 
 
 22-37 
 
 4262 
 
 190-5 
 
 
 
 337-4 
 
 15-08 
 
 25-15 
 
 5337 
 
 212-2 
 
 
 
 422-7 
 
 16-81 
 
 33-19 
 
 94S6 
 
 285-8 
 
 4055 
 
 5431 
 
 752-3 
 
 22-15 
 
 43-28 
 
 13570 
 
 313-6 
 
 5357 
 
 8213 
 
 1076 
 
 24-88 
 
 In Table I are given the results for nickel at about 15 C., together 
 with the values of // and < calculated from the formulae given below the 
 Table. We see that the coincidence is almost perfect in both cases, 
 which thus shows that the formula which we have hitherto used for X 
 and ;j. can also be applied to , at least within the limit of experiments 
 hitherto made, although it must at last depart from one or the other 
 of the curves. The greatest relative error is seen to be in the first 
 line, where ) is small: this does not indicate any departure from the 
 curve, but is only due to the too small deflections Of the galvanometer; 
 and the error indicates that of only a small fraction of a division at the 
 galvanometer. 
 
 In the calculation of /J- and K a method was used which may be of 
 use to others in like circumstances, who have to calculate a large num- 
 ber of values of one variable from a function which cannot be solved 
 with reference to that variable, but can be solved with reference to the 
 other. Thus we have 
 
 which can be solved with reference to S3 but not to //; for we have 
 
 (1) 
 
 (2) 
 
64 HENEY A. ROWLAND 
 
 Suppose we have values of 33, and wish to find the corresponding values 
 of .//. We first calculate a few values of 33 from (2) so that we can plot 
 the curve connecting 33 and [JL. We then from the plot select a value 
 of p which we shall call //, as near the proper value as possible, and 
 calculate the corresponding value of 33, which we shall call 33'. Our 
 problem then is, knowing 33' and //, to find the value of /JL corresponding 
 to 33 when this is nearly equal to 33'. Let 33' receive a small increment 
 J33', so that 33 = 33' + J33' ; then we have, from Taylor's theorem, since 
 ' + J33') and fjf= 
 
 Remembering that the constants in (1) refer to degrees of arc and 
 not to the absolute value of the arc, we have 
 
 &c, 
 
 which is in the most convenient form for calculation by means of 
 Barlow's Tables of squares, &c., and is very easy to apply, being far 
 easier than the method of successive approximation. 
 
 On comparing the magnetic curve Table II with the normal curve 
 Table I, we see that the magnetic curve of nickel bears the same rela- 
 tion to the normal curve as we have already found for iron; that is, 
 the magnetic curve falls below the normal curve for all points before 
 the vertex, but afterwards the two coincide. 
 
 Hence we see that at ordinary temperatures the magnetic properties 
 of nickel are a complete reproduction of those of iron on a smaller scale. 
 But when we come to study the effect of temperature we shall find a 
 remarkable difference, and shall find nickel to be much more susceptible 
 than iron to the influence of heat. 
 
 In Table III we have experiments on the permeability of nickel at 
 a high temperature, the ring being maintained at 220 C. by being 
 placed in a bath of melted paraffin: in this bath the silk covering of 
 the wire remained quite perfect, but after many hours became some- 
 what weak. After completing the experiments on this and the cobalt 
 rings, on unwinding some of them I found the outside layer quite per- 
 fect; but, especially in the smallest ring, the silk on the inside layer 
 was much weaker, although the insulation was still perfect when the 
 wire was in place. I can only account for this by the electric current 
 generating heat in the wire, which was unable to pass outward because 
 
MAGNETIC PERMEABILITY OF NICKEL AND COBALT 
 
 65 
 
 of the outside layer and also of the pieces of paper which were used to 
 separate the layers of wire; hence the ring at high magnetizing-powers 
 must have been at a somewhat higher temperature than the bath, to an 
 amount which it is impossible to estimate. It is probable that it was 
 not very great, however; for at this high temperature continued for 
 hours it requires but little increase of heat to finally destroy the silk. 
 We can, however, tell the direction of the error. 
 
 We see, on comparing Tables I and II with Table III, the great 
 effect of heat on the magnetic properties of nickel. We see that for 
 low magnetization the permeability is greatly increased, which is just 
 opposite to what we might expect; but on plotting the curve we also 
 notice the equally remarkable fact, that the maximum of magnetization 
 
 ZO.OOO 40.000 
 
 eo.ooo 
 
 1. Curve at 15 C. 
 
 2. Curve at 220 C. 
 
 is decreased from 33= 63,400 or 3 = 4940 to 33= 49,000 or $ = 3800. 
 This curious result is shown in the annexed figure, where we see that 
 for low magnetizing-f orces p is increased to about three or four times 
 its value at 15 C., and the maximum value of // is increased from 222 
 to 315. When 33 has a value of 32,000, p is not affected by this change 
 of temperature, seeing that the two curves coincide; but above that 
 point fji is less at 220 C. than at 15 C. In other words, if nickel is 
 heated from 15 C. to 220 C., the magnetization of nickel will increase if 
 the magnetizing-f orce is small, but will decrease if it is large. It is impos- 
 sible to say at present whether increase of temperature above 220 will 
 always produce effects in the same direction as below it or not. 
 
 These remarkable effects of heat, it seems to me, will, when followed 
 
 out, lead to the discovery of most important connections between heat 
 
 and magnetism, and will finally result in giving us much more light 
 
 upon the nature of heat and magnetism, and that equally important 
 
 5 
 
66 HENRY A. EOWLAND 
 
 question of what is a molecule. To accomplish this we must obtain a 
 series of curves for the same ring between as wide limits of temperature 
 as possible. We must then plot our results in a suitable manner; and 
 from the curves thus formed we can find what would probably happen 
 if the temperature were lowered to the absolute zero, or were increased 
 to the point at which nickel is said to lose its magnetism. In such 
 inquiries as these the graphical method is almost invaluable, and little 
 can be expected without its aid. 
 
 In applying the formula to this curve, we do not find so good an 
 agreement as at the lower temperature. I do not consider this conclu- 
 sive that the formula will not agree with observation at this tempera- 
 ture; for I have noticed that the curves of different specimens of iron 
 and nickel seem to vary within a minute range, not only in their 
 elements but also in their form. This might perhaps be accounted for 
 by some small want of homogeneity, as in the case of burning in iron 
 and nickel; but at present the fact remains without an explanation. 
 But the amount of the deviation is in all cases very small when all the 
 precautions are taken to insure good results. The nature of the devia- 
 tion is in this case as follows: when the constants in the formula are 
 chosen to agree with the observed curve at the vertex and at the two 
 ends, then the observed curve falls slightly below the curve of the 
 formula at nearly all other points. In a curve plotted about 5 inches 
 high and broad, the greatest distance between the two curves is only 
 about -^ of an inch, and could be much reduced by changing the con- 
 stants. For the benefit of those who wish to study this deviation, I 
 have calculated the following values, which will give the curve touching 
 the vertex and the two ends of the observed curve of Table III. They 
 are to be used by plotting in connection with that Table. 
 
 K. 
 
 3. 
 
 
 
 140 
 
 3802 
 
 12.75 
 
 205 
 
 2833 
 
 18-75 
 
 455 
 
 2269 
 
 22-5 
 
 703 
 
 1835 
 
 25 
 
 1206 
 
 3 + 25/C + 140 
 
 I have not as yet obtained a complete curve of iron at a high temper- 
 ature; but as far as I have tried, it does not seem to be affected much, 
 at least for high magnetizing-powers. I have, however, found that the 
 maximum of magnetization of iron decreases about 2 per cent by a 
 
MAGNETIC PEEMEABILITY OF NICKEL AND COBALT 
 
 67 
 
 rise of temperature from 15 C. to 222 C., while that of nickel de- 
 creases 22-7 per cent. 
 
 The experiments which 1 have made with cobalt do not seem to be 
 so satisfactory as those made with nickel and iron. There are some 
 things about them which I cannot yet explain; but as they are the only 
 exact experiments yet made on cobalt, they must possess at least a 
 transient value. The difficulties of getting a good cobalt-curve are. 
 manifold, and are due to the following properties (1) its small permea- 
 bility, (2) its sensitiveness to temperature, and (3) its property of having 
 its permeability increased by rise of temperature at all magnetizing- 
 powers within the limits of experiment. The following are the results 
 
 with No. I : 
 
 TABLE IV. 
 
 CAST COBALT, NORMAL, AT 5 C. 
 Experiments made November 27, 1873. 
 
 fi. 
 
 8. 
 
 M. 
 
 T. 
 
 P. 
 
 3- 
 
 K. 
 
 Ob- 
 served. 
 
 K. 
 
 Calcu- 
 lated. 
 
 Error. 
 
 49-33 
 
 4303 
 
 87-24 
 
 3702 
 
 601 
 
 338-5 
 
 6-86 
 
 6-75 
 
 11 
 
 58-83 
 
 5608 
 
 95-32 
 
 4526 
 
 1082 
 
 441-6 
 
 7-51 
 
 7-44 
 
 07 
 
 76-47 
 
 8409 
 
 109-95 
 
 6175 
 
 2234 
 
 663-1 
 
 8-67 
 
 8-79 
 
 12 
 
 93-15 
 
 11623 
 
 124-8 
 
 7826 
 
 3797 
 
 917-5 
 
 9-85 
 
 9-81 
 
 04 
 
 113-0 
 
 14993 
 
 132-7 
 
 9805 
 
 5188 
 
 1193-1 
 
 10-48 
 
 10-44 
 
 04 
 
 129-3 
 
 17439 
 
 134-9 
 
 10580 
 
 6859 
 
 1387-8 
 
 10-66 
 
 10-72 
 
 06 
 
 159-4 
 
 22309 
 
 140-0 
 
 14090 
 
 8219 
 
 1775-3 
 
 11-06 
 
 11-00 
 
 06 
 
 189-0 
 
 26769 
 
 141-6 
 
 16260 
 
 10509 
 
 2130-3 
 
 11-19 
 
 10-97 
 
 22 
 
 219-6 
 
 30580 
 
 139-3 
 
 18200 
 
 12380 
 
 2433-5 
 
 11-01 
 
 10-83 
 
 18 
 
 264-7 
 
 35525 
 
 134-2 
 
 21120 
 
 14405 
 
 2827-0 
 
 10-60 
 
 10-50 
 
 10 
 
 351-1 
 
 43421 
 
 123-7 
 
 25670 
 
 17751 
 
 3455-0 
 
 9-76 
 
 9-73 
 
 03 
 
 400-0 
 
 46640 
 
 116-6 
 
 27830 
 
 18810 
 
 3711-5 
 
 9-20 
 
 9-34 
 
 14 
 
 552-1 
 
 55410 
 
 100-4 
 
 34090 
 
 21320 
 
 4409-0 
 
 7-91 
 
 8-16 
 
 25 
 
 732-1 
 
 63400 
 
 86-6 
 
 39850 
 
 23550 
 
 5045-0 
 
 6-81 
 
 6-93 
 
 12 
 
 999-8 
 
 71800 
 
 71-8 
 
 47310 
 
 24490 
 
 5714-0 
 
 5-63 
 
 5-55 
 
 08 
 
 1471 
 
 80770 
 
 54-9 
 
 55870 
 
 24900 
 
 6430-0 
 
 4-29 
 
 3-98 
 
 31 
 
 
 
 
 
 
 8160 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 c* +190* + 120 
 
 ... -|i ain *y 
 
 46 
 
 TABLE V. 
 
 CAST COBALT, MAGNETIC, AT 5 C. 
 Experiments made November 28, 1873. 
 
 . 
 
 93. 
 
 M. 
 
 T. 
 
 P. 
 
 3- 
 
 K. 
 
 48-47 
 
 3702 
 
 76-37 
 
 3287 
 
 415 
 
 290-8 
 
 6-00 
 
 76-74 
 
 7254 
 
 94-54 
 
 5760 
 
 1494 
 
 571-1 
 
 7-44 
 
 112-8 
 
 14370 
 
 127-5 
 
 9388 
 
 4982 
 
 1134-5 
 
 10-06 
 
 167-6 
 
 24130 
 
 144-0 14490 9640 1907 
 
 11-38 
 
 264-2 
 
 35860 
 
 135 7 
 
 20420 
 
 15440 2833 
 
 10-72 
 
 539-9 
 
 53940 
 
 99-91 
 
 33010 
 
 20930 4249 
 
 7-87 
 
 1473 80760 
 
 54-84 
 
 55920 
 
 24840 
 
 6310 
 
 4-28 
 
 
 
 
 
 
 i 
 
G8 
 
 HENRY A. ROWLAND 
 
 TABLE VI. 
 
 CAST COBALT, MAGNETIC, AT 230 C. 
 Experiments made February 3, 1874. 
 
 ft. 
 
 S3. 
 
 M. 
 
 T. 
 
 P. 
 
 3- 
 
 K. 
 
 13-34 
 
 1357 
 
 101-8 
 
 1165 
 
 192 
 
 107 
 
 8-02 
 
 25-67 
 
 2916 
 
 113-6 
 
 2662 
 
 254 
 
 230 
 
 8-96 
 
 38-55 
 
 4940 
 
 128-2 
 
 4397 
 
 543 
 
 390 
 
 10-12 
 
 55-56 
 
 9400 
 
 169-1 
 
 7440 
 
 I960 
 
 743-5 
 
 13-38 
 
 75-16 
 
 15800 
 
 210-2 
 
 10050 
 
 5750 
 
 1143 
 
 16-65 
 
 101-4 
 
 23920 
 
 235-9 
 
 14260 
 
 9660 
 
 1895 
 
 18-70 
 
 132-7 
 
 31260 
 
 235-5 
 
 17710 
 
 13550 
 
 2475 
 
 18-66 
 
 172-9 
 
 38060 
 
 220-2 
 
 21820 
 
 16240 
 
 3015 
 
 17-44 
 
 281-8 
 
 52520 
 
 186-4 
 
 31160 
 
 21360 
 
 4174 
 
 14-76 
 
 393-6 
 
 63430 
 
 161-2 
 
 39070 
 
 24360 
 
 5039 
 
 12-75 
 
 702-9 
 
 82070 
 
 117-0 
 
 54920 
 
 27150 
 
 6515 
 
 9-27 
 
 989-3 
 
 95600 
 
 96-63 
 
 66750 
 
 28850 
 
 7584 
 
 7-67 
 
 1282 
 
 106200 
 
 82-87 
 
 75820 
 
 30380 
 
 8422 
 
 6-57 
 
 From Table IV we see that at ordinary temperatures cobalt does not 
 offer any exception to the general law for the other magnetic metals 
 that as the magnetization increases, the magnetic permeability first 
 increases and then decreases. We also see that the results satisfy to a 
 considerable degree of accuracy the equation which I have used for the 
 other magnetic metals. The departure from the equation is of exactly 
 the nature that can be accounted for in either of two ways either by 
 the heating of the ring by the current for the higher magnetizing- 
 forces, or by some want of homogeneity in the ring. According to the 
 first explanation, the maximum of magnetization at C. will be some- 
 what lower than the curve indicates; but by the second it must be 
 higher. I, however, incline to the first, that it is due to heating, for 
 two reasons: first, it is sufficient; and secondly, the smaller cobalt ring 
 gives about the same maximum as this. Hence we may take as the 
 provisional value of the maximum of magnetization of cobalt in round 
 numbers 3= 8000, or SB = 100,000. 
 
 We also see from Table IV that, at least in this case, the permeability 
 of cobalt is less than that of nickel, though we could without doubt 
 select specimens of cobalt which should have this quality higher than a 
 given specimen of nickel. The formula at the foot of the Table also 
 shows, by the increased value of the coefficient of K in the right-hand 
 member, that the diameter of the curve is much less inclined to the 
 axis of $ in this case than in the case of nickel or iron. In this re- 
 spect the three metals at present stand in the following order cobalt, 
 nickel, iron. This is the inverse order also of their permeability; but 
 
MAGNETIC PERMEABILITY OF NICKEL AND COBALT 
 
 69 
 
 at present I have not found any law connecting these two, and doubt 
 if any exact relation exists, though as a general rule the value of the 
 constant is greater in those curves where the permeability is least. 
 
 In a short abstract in the ' Telegraphic Journal/ April 1, 1874, of a 
 memoir by M. Stefan, it is stated " that the resistance of iron and 
 nickel to magnetization is at first very great, then decreases to a mini- 
 mum value, which is reached when the induced magnetic moment is 
 become a third of its maximum." This will do for a very rough approx- 
 imation, but is not accurate, as will be seen from the following Table 
 of this ratio from my own experiments : 
 
 Experiments published in Augnst, 1873. 
 
 Iron. 
 Tables I 
 and II. 
 
 Iron. 
 Table III. 
 
 Bessemer Iron 
 Tabfe'iv. j TableV " 
 
 Nickel. 
 Table VI. 
 
 Steel. 
 Table VII. 
 
 1 
 3-02 
 
 1 
 2-64 
 
 1 1 
 
 1 
 3-15 
 
 1 
 2-46 
 
 2-65 2-68 
 
 Experiments of present paper. 
 
 Nickel. 
 Tables I and II. 
 
 Nickel. 
 Table III. 
 
 Cobalt. 
 Tables IV and V. 
 
 1 
 3-23 
 
 1 
 3-14 
 
 1 
 4-2 
 
 The average of these is, if we include Bessemer steel with the iron, as 
 it is more iron than steel: 
 
 Hence the place of greatest permeability will vary with the kind of 
 metal. From these, however, we can approximate to the value of 6 in 
 the formula; for we have 
 
 27,000 f AT- i i ^ 11,000 
 for Iron, b = - ; for Nickel, * = = ; 
 p " 
 
 for Cobalt, b = 26,000. 
 
 In Table V we have the results for cobalt in the magnetic state. 
 We here find the same effect of magnetization as we have before found 
 for iron and nickel. 
 
70 HENRY A. KOWLAND 
 
 In Table VI we have results for cobalt at a high temperature, and 
 see how greatly the permeability is increased by rise of temperature, 
 this being for the vertex of the curve about 70 per cent. But on plot- 
 ting the curve I was much surprised to find an entire departure from 
 that regularity which I had before found in all curves taken from iron 
 and nickel when the metal was homogeneous. At present I am not able 
 to account for this, and especially for the fact that one of the measure- 
 ments of 33 is higher than that which we have taken for the maximum 
 of magnetization, at, however, a lower temperature. The curve is 
 exactly of the same nature as that which I have before found for a 
 piece of nickel which had been rendered unhomogeneous by heating 
 red-hot, and thus burning the outside. The smaller cobalt ring gives 
 a curve of the same general shape as this, but has the top more rounded. 
 I will not attempt without fresh experiments to explain these facts, but 
 will simply offer the following explanations, some one of which may be 
 true. First, it may be due to want of homogeneity in the ring; but it 
 seems as if this should have affected the curve of Table IV more. 
 Secondly, it may be at least partly due to the rise in temperature of the 
 ring at high magnetizing-powers ; and indeed we know that this must 
 be greater in paraffin than in alcohol for several reasons : there is about 
 twice as much heat generated in copper wire at 230 C. as at with 
 the same current; and this heat will not be conducted off so fast in 
 paraffin as in alcohol, on account of its circulating with less freedom; 
 it probably has less specific heat also. Thirdly, it may be due to some 
 property of cobalt, by which its permeability and maximum of magneti- 
 zation are increased by heat and the curve changed. 
 
 The experiments made with the small ring confirm those made with 
 the large one as far as they go; but as it was so small, they do not 
 possess the weight due to those with the larger one. But, curious as 
 it may seem, although they were turned from the same button side by 
 side, yet the permeability of the larger is about 45 per cent greater than 
 that of the smaller. I have satisfied myself that this is due to no error 
 in experiment, but illustrates what extremely small changes will affect 
 the permeability of any metal. 
 
 We have now completed the discussion of the results as far as they 
 refer to the magnetic permeability, leaving the discussion of the tem- 
 porary and permanent or residual magnetism to the future, although 
 these latter, when discussed, will throw great light upon the nature 
 of the coercive force in steel and other metals. The whole subject 
 seems to be a most fruitful one, and I can hardly understand why it has 
 
MAGNETIC PERMEABILITY OF NICKEL AND COBALT 71 
 
 been so much neglected. It may have been that a simple method of 
 experiment was not known; but if so, I believe that my method will be 
 found both accurate and simple, though it may be modified to suit the 
 circumstances. Professor Maxwell has suggested to me that it would 
 be better to use rods of great length than rings, because that in a ring 
 we can never determine its actual magnetization, but must always con- 
 tent ourselves with measuring the change on reversing or breaking the 
 current. This is an important remark, because it has been found by 
 MM. Marianini and Jamin, and was noticed independently by myself 
 in some unpublished experiments of 1870, that a bar of steel which has 
 lain for some time magnetized in one direction will afterwards be more 
 easily magnetized in that direction than in the other. This fact could 
 not have been discovered from a ring; and indeed if a ring got a one- 
 sided magnetism in any way we might never know it, and yet it might 
 affect our results, as indeed we have already seen in the case of the 
 magnetic curve. But at the same time I think that greater errors 
 would result from using long bars. I have tried one of iron 3 feet 
 long and inch diameter; and the effect of the length was still appar- 
 ent, although the ratio of length to diameter was 144. To get exact 
 results it would probably have to be several times this for the given 
 specimen of iron, and would of course have to be greater for a piece 
 of iron having greater permeability. This rod must be turned and 
 must be homogeneous throughout conditions which it would be very 
 difficult to fulfil, and which would be impossible in the case of nickel 
 and cobalt. We might indeed use ellipsoids of very elongated form; 
 and this would probably be the best of all, as the mathematical theory 
 of this case is complete, and it is one of the few where the magnetization 
 is uniform, and which consequently will still hold, although the permea- 
 bility may vary with the amount of magnetization. This form will, of 
 course, satisfy Professor Maxwell's objection. 
 
 The method of the ring introduces a small error which has never 
 yet been considered, and which will affect Dr. Stoletow's results as well 
 as mine. The number of lines of induction passing across the circular 
 section of a ring-magnet we have seen to be 
 
 /+ J ~Jp y* 
 
 Jn a, x 
 
 in which a is the mean radius of the ring, E the radius of the section, 
 n' the number of coils in the helix, and i the intensity of the current. 
 Xow in integrating this before, I assumed that ft was a constant 
 throughout the section of the ring: now we have found that 11 is a 
 
72 HENET A. EOWLAND 
 
 function of the magnetization, and hence a function of the magnetizing- 
 force; but the latter varies in different parts of the section, and hence 
 n must vary. But the correction will be small, because the average 
 value will be nearly the same as if it were a constant. We may estimate 
 the correction in the following manner. Let // and be the values of 
 those quantities at any point in the section of the ring, // and ' the 
 values at the centre of the section, and fjt t and , the observed values. 
 Then, by Taylor's theorem, 
 
 But = 2n ' 1 and ft' = , and so we have 
 a x a 
 
 \ 4 a* 2// dJQ r \ a 2 
 
 Jp' 2 d z >j. I R* , q K 
 
 But in my Tables I have already calculated 
 
 Q 1 
 
 A*J = 
 
 a 
 
 &c. . 
 
 t / i T53 \ J 
 
 ,lfV (l + i ^ + fto.) 
 
 and as ft l is very nearly equal to fjf, and $, to ^)', we have approximately 
 6, din. I IP 3 If . 
 
 -- 
 
 . 
 
 2 4 a 4 
 
 which will give the value of // corresponding to Q' and >'. Hence the 
 correct values of the quantities will be //, ', and S3' = ^V. 
 
 The quantities -^- and ^/- can be obtained either by measuring a 
 
 "/ **/ 
 
 plot of the curve, or from the empirical equation 
 
 = sn 
 
 when we know the values of the constants. In this case 
 
 dp _ , ft, 
 *$/ " 
 ^V/ 
 d? 
 in which 
 
MAGNETIC PERMEABILITY OF NICKEL AND COBALT 73 
 
 In all these the upper signs are to be taken for all values of >, less than 
 
 , and the lower signs for greater values. 
 t> 
 
 On applying these formulas to the observations, I have found that the 
 corrections will in no way influence my conclusions, being always very 
 small; but at the same time the calculation shows that it would be well 
 
 R 
 
 to diminish the ratio as much as possible. In all my rings this ratio 
 a 
 
 did not depart very much from - ; but I would advise future experi- 
 
 o'o 
 
 menters to take it at least as small as ^: the amount of correction 
 
 R 
 
 will be very nearly proportional to the square of . 
 
 ct 
 
 Summary. 
 
 The following laws have been established entirely by my own experi- 
 ments, though in that part of (2) which refers to iron I have been 
 anticipated in the publication by Dr. Stoletow (Phil. Mag. Jan. 1873). 
 When any measurements are given, they are on the metre, gramme, 
 second system. 
 
 (1) Iron, nickel, and cobalt, in their magnetic properties at ordinary 
 temperatures, differ from each other only in the quantity of those 
 properties and not in the quality. 
 
 (2) As the magnetizing-force is increased from upwards, the resist- 
 ance of iron, nickel, and cobalt to magnetization decreases until a 
 minimum is reached, and after that increases indefinitely. This mini- 
 mum is reached when the metal has attained a magnetization of from 
 24 to -38 of the maximum of magnetization of the given metal. 
 
 (3) The curve showing the relation between the magnetization and 
 the magnetic permeability, or Neumann's coefficient, is of such a form 
 that a diameter can be drawn bisecting chords parallel to the axis of 33, 
 and is of very nearly the form given by the equation 
 
 where B, &, and D are constants, jut is the ratio of the magnetization to 
 the magnetizing-force in an infinitely long bar, and 33 is the amount 
 of magnetization. 
 
 (4) If a metal is permanently magnetized, its resistance to change of 
 magnetism is greater for low magnetizing-powers than when it is in the 
 normal state, but is the same for high magnetizing-powers. This 
 
74 HENRY A. EOWLAND 
 
 applies to the permanent state finally attained after several reversals of 
 magnetizing-f orce ; but if we strongly magnetize a bar in one direction 
 and then afterwards apply a weak magnetizing-force in the opposite 
 direction, the change of magnetization will be very great. 
 
 (5) The resistances of nickel and cobalt to magnetization vary with 
 the temperature; but whether it is increased or not in nickel depends 
 upon the amount of magnetization : for a moderate amount of magneti- 
 zation it decreases with rise of temperature very rapidly; but if the 
 magnetization is high the resistance is increased. In cobalt it appar- 
 ently always decreased, whatever the magnetization. The resistance 
 of iron to magnetization is not much affected by the temperature. 
 
 (6) The resistance of any specimen of metal to magnetization de- 
 pends on the kind of metal, on the quality of the metal, on the amount 
 of permanent magnetization, on the temperature, and on the total 
 amount of magnetization, and, in at least iron and nickel, decreases 
 very much on careful annealing. The maximum of magnetization 
 depends on the kind of metal and on the temperature. 
 
 (7) Iron, nickel, and cobalt all probably have a maximum of magneti- 
 zation, though its existence can never be entirely established by experi- 
 ment, and must always be a matter of inference; but if one exists, the 
 values must be nearly as follows at ordinary temperatures. Iron when 
 33 = 175,000 or when 3 = 13,900; nickel when 33 =63,000 or when 
 3 = 4940; cobalt when 33 = 100,000( ?) or when 3 = 8000 (?). 
 
 (8) The maximum of magnetization of iron and nickel decreases with 
 rise of temperature, at least between 10 C. and 220 C., the first very 
 slowly and the second very rapidly. At 220 C. the maximum for iron 
 is when 33 = 172,000 and 3 = 13,600, and for nickel when 33 = 49,000 
 and 3 = 3800. 
 
 The laws which govern temporary and residual magnetism, except so 
 far as they have been hitherto given, I leave for the future, when I 
 shall have time for further experiment on the subject to develop some 
 points which are not yet quite clear. 
 
 Troy, New York, U. S. A., April, 1874. 
 
ON A NEW DIAMAGNETIC ATTACHMENT TO THE LANTERN, 
 WITH A NOTE ON THE THEOEY OF THE OSCILLATIONS 
 OF INDUCTIVELY MAGNETIZED BODIES 
 
 [American Journal of Science [8], IX, 357-361, 1875] 
 
 1. DESCRIPTION OF APPARATUS 
 
 Some time ago, in thinking of the theory of diamagnetism, I came 
 to the conclusion that apparatus of large size was by no means neces- 
 sary in diamagnetic experiments, and on testing my conjectures experi- 
 mentally, I was much pleased to find that they were true. So that for 
 more than a year I have been in the habit of illustrating this subject 
 to my classes by means of a small apparatus weighing only about a 
 pound or two, which I place in my lantern and magnify to a large size 
 on the screen. 
 
 The effects obtained in this way are very fine and are not surpassed 
 by those with the largest magnets; and we are by no means confined, 
 to strongly diamagnetic substances, but, with proper care, can use any- 
 thing, even the most feeble. The apparatus which I used consisted of 
 a horseshoe electro-magnet, made of an iron bar half an inch in diam- 
 eter and about ten inches long, bent into the proper form, and sur- 
 rounded with four or five layers of No. 16 wire. But the following 
 apparatus will, without doubt, be found much more convenient. It can 
 be made of any size, though the dimensions given will probably be 
 found convenient. 
 
 d d 
 
 r j 3 <d 
 
 
 =3 
 
 a 
 
 a. 
 e 
 
 
 
 i 
 
 
 FIGURE 1. 
 
 The apparatus is represented in Fig. 1. To a straight bar of iron h, 
 7 in. long, in. thick, and f in. wide, are attached two pieces e e of 
 the same kind of iron by two set screws g g, which move in slots in the 
 
76 HENRY A. EOWLAND 
 
 piece h. Into these pieces are screwed two tubes c made of iron and 
 having an internal diameter of about T 7 T in. and a thickness not to 
 exceed ^ in. Through these tubes the iron rods a I slide and are 
 held at any point by the screws d. One end b of this rod is rounded 
 off for diamagnetic experiments and the other enlarged and flattened 
 at the end for magnecrystallic experiments. On the tube c a helix of 
 N~o. 16 or No. 18 wire is wound so as to make up a thickness of -4 or -5 
 of an inch and having a length of 2 in. The object of the screws g is 
 principally to allow the rods a & to be reversed quickly and to adjust the 
 position of the helices. When the apparatus is to be used for only one 
 kind of work it can be much simplified by doing away with many of the 
 moving parts. 
 
 This instrument can be used either with the ordinary magic lantern, 
 or better, with one having, a vertical attachment. In the latter case 
 the plane of the instrument is horizontal and the substances are sus- 
 pended from a wire made quite small, so as not to cut off too much 
 light. 
 
 The suspending thread in the case of bismuth can be quite large 
 but for other bodies a single fibre of silk is best; these in the shape of 
 bars half an inch long can be each attached to a fibre having a little 
 wire hook at its upper end and hung in a cabinet until required. 
 
 The theory of feebly magnetic or diamagnetic bodies oscillating in 
 a magnetic field is very simple and yet the results are of the greatest 
 interest, especially the effect of the size of the apparatus, which is 
 here given for the first time. 
 
 2. THEORY 
 
 Let a very small particle of a body whose coefficient of magnetization 
 AC is very small, and either positive or negative, be placed in a magnetic 
 field of intensity R; it will then have an induced magnetic moment of 
 <vR, where v is the volume of the element. The force acting on this 
 particle to cause it to go in any given direction will be equal to the 
 product of the magnetic moment into the rate of variation of R in that 
 
 direction, 1 and hence is K vR ~r in the direction of x. The total force 
 
 ax 
 
 acting on the body in the direction of x is therefore 
 
 1 Thomson, Reprint of Papers, art. 679, Prob. vii. 
 
NEW DlAMAGNETIC ATTACHMENT TO THE LANTERN 77 
 
 and the other components of the force are 
 
 and 
 
 - 
 
 Let, now, the axis of z be vertical, the axis of x in the line of the 
 magnetic poles of the magnet, and y at right angles to both. Then 
 the moment of the forces acting on the body to turn it about the axis 
 
 of z is 
 
 where the integration extends throughout the volume of the body. 
 
 If the body is suspended so as to turn freely about the axis of z it 
 will vibrate about the position for which M is a minimum or else will 
 remain at rest at that point. The number of single oscillations made 
 when the angular elongation & is very small, is 
 
 1 / M 
 
 ' T. V tfj' 
 
 in which M and $ must be measured simultaneously, and I is the 
 moment of inertia of the body. 
 
 I r r r 
 
 A/ I l/f 
 \ J J J 
 
 i Jw d(i^)\, ^ ^ 
 
 y , 3 -, \dxdydz. 
 \ J dx dy j 
 
 Xow let us suppose that the whole apparatus changes size, the relation 
 between the parts remaining constant, so that the apparatus becomes 
 m times as great as before. Then x, y, dx, dy, and dz will increase ra 
 
 times and /, m 5 times. To determine the changes in ^ ^ and -X * 
 
 aye? ^y 
 
 we make use of the theorem of Sir Win. Thomson, that " similar bars 
 of different dimensions, similarly rolled, with lengths of wire propor- 
 tional to the squares of their linear dimensions, and carrying equal 
 currents, cause equal forces at points similarly situated with reference 
 to them." But as the above only applies to equal currents, I have 
 generalized it in the following: In any two magnetic systems whatever, 
 similar in all their parts and composed of any number of permanent or 
 electro-magnets, wires carrying currents, or bodies under magnetic induc- 
 tion, the magnetic force at similar points of each will be the same when the 
 following conditions are complied with: 1st, the magnetic materials at 
 similar prints in the two systems must be exactly the same in quality and 
 
78 HENRY A. KOWLAND 
 
 temper; 2d, the permanent magnets must be magnetized to the same degree 
 at similar points of the systems; 3d, the coils of the electro-magnets and 
 other wires or bundles of wires carrying the current must have similar 
 external dimensions in the two systems and must have the product of the 
 current by the number of wires passing through similar sections of the two 
 systems proportional to the linear dimensions of the systems. 
 
 This will apply to the case we are considering when the product of 
 the current by the number of the turns of wire varies in direct propor- 
 tion to the size of the apparatus. Hence in this case \ and !-i f 
 
 dx ay 
 
 will vary inversely as m. Hence we see that n will be inversely pro- 
 portional to the size of the apparatus; and although we have only 
 proved this for the case when * is small, it is easy to see that it is 
 perfectly general. The advantage of small diamagnetic apparatus is 
 thus apparent, for the smaller we make it the more vibrations the bar 
 will make in a given time and the more promptly will the results be 
 shown. 
 
 It might be thought that by hanging a very small bar in the field oi' 
 a large magnet, we might obtain just as many vibrations as by the use 
 of a small apparatus; but this is not so, for Sir Wm. Thomson has 
 shown 2 that the number of oscillations of a feebly magnetic or diamag- 
 netic body of elongated form in a magnetic field is nearly independent 
 of the length when that is short. So that the only way of increasing 
 the number of vibrations is to decrease the size of the whole apparatus, 
 or to increase the power of the magnets; the latter has a limit and 
 hence we become dependent on the former. 
 
 The theory of the effect of the size of the body is very simple, and we 
 may proceed as follows. Let the body be in the form of a small bar 
 whose sectional area, a, is very small compared with its length, and let 
 f be the angle of the axis of the bar with the line joining the poles, and 
 r the radius vector from the origin. Developing R 2 as a function of 
 x and y by Taylor's theorem, and noting that as R is symmetrical with 
 reference to the planes XZ and YZ, only the even powers of x and y 
 can enter into the development, we have, calling R the value of R 
 at the origin, 
 
 2 \ dy? dy 
 
 r#(/2n 
 
 2.3.4V dtf dtfdf dy* 
 
 2 Reprint of Papers, art. 670. Remarques sur les oscillations d'aiguilles non crys- 
 tallisees. 
 
NEW DlAMAGNETIC ATTACHMENT TO THE LANTERN 79 
 
 When the vibrating body is very small the first two terms will suffice: 
 hence we have 
 
 M= i a 
 
 in which I is the length of the bar. If d is the density of the body 
 (weight of a unit of volume), I = ^ and n becomes 
 
 in which, however, it is to be noted that ^ .7 is essentially negative 
 
 and so the sign of the term containing it will be positive in the actual 
 development. 
 
 This equation is independent of the dimensions of the body, and 
 hence we conclude that when the body is small and very long as com- 
 pared with its other dimensions, the number of vibrations which it will 
 make in a given field is dependent merely on its coefficient of magneti- 
 zation and on its density; a result first given by Sir Wm. Thomson, in 
 the paper referred to. I have given it once more and put it in its 
 present form merely to call attention to the facility with which can 
 be obtained from it when we have measured R in different parts of the 
 field by known methods. This could be done by means of a rotating 
 coil as used by Verdet, or by my magnetic proof plane which I will 
 soon describe, combined with my method of using the earth inductor. 
 This will give the best method that I know of for obtaining K for 
 diamagnetic or weak paramagnetic substances. 
 
 Troy, January 15, 1875. 
 
8 
 NOTES ON MAGNETIC DISTKIBUTION 
 
 [Proceedings of the American Academy of Arts and Sciences, XI, 191, 19^, 187(i. Pre- 
 sented June 9, 1 875] 
 
 In two papers which have recently appeared on this subject, by Mr. 
 Sears (Amer. Jour, of Science, July, 1874), and Mr. Jacques (Proc. 
 Amer. Acad. of Sciences, 1875, p. 445), a method is used for determining 
 magnetic distribution, founded on induced currents, in which results 
 contrary to those published by M. Jamin have been found. It does not 
 seem to have been noticed that the method then used does not give 
 what we ordinarily mean by magnetic distribution. In mathematical 
 language, they have measured the surface integral of magnetic induc- 
 tion across the section of the bar instead of along a given length of its 
 surface. 1 M. Jamin's method gives a result depending on the so-called 
 surface density of the magnetism, which is nearly proportional to the 
 surface integral of the magnetic induction along a given length of the 
 bar. Hence the discrepancy between the different results. Had the 
 experiments of Mr. Sears and Mr. Jacques been made by sliding the 
 helix inch by inch along the bars, their results would have confirmed 
 those of M. Jamin. Four or five years ago, I made a large number of 
 experiments in this way, which I am now rewriting for publication, and 
 where the whole matter will be made clear. At present, I will give the 
 following method of converting one into the other. Let Q be the sur- 
 face integral of magnetic induction across the section of the rod, and 
 
 let Qe be that along one inch of the rod: then Qe <x ^.x beinar the 
 
 (IX 
 
 distance along the rod. Hence, M. Jamin's results depend on the rate 
 of variation of the magnetization of the rod, while those of Mr. Sears 
 and Mr. Jacques depend on the magnetization. In conclusion, let me 
 heartily agree with Mr. Jacques's remarks about M. Jamin's conclusions 
 from his experiments. Such experiments as those give no data what- 
 ever for a physical theory of magnetism, and can all be deduced from 
 the ordinary mathematical theory, which is independent of physical 
 
 1 Maxwell's Electricity and Magnetism, art. 402. 
 
NOTES ON MAGNETIC DISTRIBUTION 81 
 
 hypothesis, combined with what is known with regard to the magnetiz- 
 ing function of iron. This will be shown in the paper I am rewriting. 
 It seems to me that M. Jamin's method is very defective; and I know 
 of no method of experimenting, which is theoretically without objection 
 except that of induced currents, and this I have used in all my experi- 
 ments on magnetic distribution for the last four or five years, and have 
 developed into a system capable of giving results in absolute measure. 
 Mr. Jacques is to be congratulated on pointing out these errors in 
 M. Jamin's conclusions. 
 
 Troy, June 7, 1875. 
 
9 
 
 NOTE ON KOHLKAUSCJFS DETERMINATION OF THE ABSO- 
 LUTE VALUE OF THE SIEMENS MERCURY UNIT OF 
 ELECTRICAL RESISTANCE 
 
 [Philosophical Magazine [4], L, 161-163, 1875] 
 
 In looking over Kohlrausch's paper 1 upon the determination of a 
 resistance in absolute measure, with a view to undertaking something 
 of the kind myself, and also, if possible, to discover the reason of the 
 difference from the results of the Committee of the British Association, 
 I think I have come across an error of sufficient magnitude and in the 
 proper direction to account for the 2 per cent difference. Kohlrausch's 
 experiments were made with such great care and by so experienced a 
 person that it is only after due thought and careful consideration that 
 I take it upon me to offer a few critical remarks. 
 
 We observe, then, first of all, that the principal peculiarity of his 
 method consists in doing away with all measurements of the coils of 
 the galvanometer, and in its place making accurate determinations of 
 the logarithmic decrement both with the circuit closed and open, to- 
 gether with various absolute determinations rendered necessary by this 
 change. In this way the logarithmic decrement is raised from being a 
 small correction to a most important factor in the equation. Hence 
 it is that we should carefully scrutinize the theory and see whether it 
 be correct enough for this purpose ; for only an approximation is needed 
 for the first method. 
 
 The resistances to a bar magnet swinging within a coil may be divided 
 into two principal parts first, that due to the resistance of air and 
 viscosity of suspending fibre, and, second, that due to the induced cur- 
 rent in the coils. The first resistance is usually taken as proportional 
 to the velocity, and thus assumes the viscosity of the air to be the most 
 important element. This is proba,bly true in most cases where the 
 motion is slow. This factor is quite small compared with the second 
 when the magnet is large and heavy and the coils wound close to it, as 
 
 ^oggendorff's Annalen, Erganzungsband vi, p. 1; translated in Phil. Mag., S. 4, 
 vol. xlvii, pp. 294, 342. 
 
NOTE ox KOHLRAUSCH'S DETERMINATION 83 
 
 in Kohlrausch's instrument. Kohlrausch's principal error lies in the 
 omission of the coefficient of self-induction from his equations. 
 
 For the sake of clearness, and because the subject is quite often 
 misapprehended, I shall commence at the beginning and deduce nearly 
 all equations. 
 
 Let us proceed at first in the method of Helmholtz, using the nota- 
 tion of Maxwell's ' Electricity.' 
 
 Let a current of strength / be passing in a circuit whose resistance 
 is 7?, and coefficient of self-induction L. Also let a magnet be near the 
 circuit whose potential energy with respect to the circuit is IV. Let A 
 be the electromotive force of the battery in the circuit. 
 
 The work done by the battery in the time dt is equal to the sum of 
 the work done in heating the wire, in moving the magnet, and in 
 increasing the mutual potential of the circuit on itself. 2 Hence we have 
 
 AUt = PRdt + l~dt + -L j 
 dt 2 
 
 and if A is equal to zero, we find 
 
 /=_.7r + L*L\ 
 
 If we apply this to the case of a magnet swinging within a coil the 
 angle of the magnet from a fixed position being x, we have since -j- 
 
 &3s 
 
 is the moment of the force acting on the magnet with unit current and 
 may be denoted by q, 
 
 dx , r 
 
 where my R is Kohlrausch's w. 
 
 This expression differs from that used by Kohlrausch in the addition 
 of the last term, which is the correction due to self-induction. The 
 last term vanishes whenever the magnet moves with such velocity as 
 to keep the induced current constant ; but in the swinging of a galvano- 
 meter-needle it has a value. 
 
 To form the equation of motion of the needle, we can proceed the 
 rest of the way as Maxwell has done (Electricity, art. 762). Assuming 
 that all frictional resistances to the needle are proportional to the 
 velocity of the needle, we have 
 
 B< S + c w + l)x = r ' ....... ^ 
 
 where B, C, and D are constants. 
 
 2 See remarks in Maxwell's ' Electricity,' art. 544, near bottom of page. 
 
84 HENRY A. ROWLAND 
 
 Eliminating / between this equation and (1), we find 
 
 At first sight this equation will appear to be the same as that of Max- 
 well; but on further examination we see that it is more general in the 
 value of q. 
 
 Equation (3) is the correct equation to use in this case, and reduces 
 to that of Kohlrausch when L = 0. 
 
 To see how this error will affect Kohlrausch's results, we must re- 
 member that he uses this equation to find the constant of his galvano- 
 meter, on which his whole experiment depends; and the error is so 
 interwoven with all his results .that an entire recomputation is neces- 
 sary, provided the data for calculating the coefficient of self-induction 
 of the galvanometer coils and earth inductor can be obtained. 
 
 The equation 
 
 t* tl 
 
 * 2 + / 2 - 2 + /S 
 
 does not hold when self-induction is considered ; and so his fundamental 
 equation (1) is not correct, containing a twofold error. 
 
 The linear differential equation (3) is easily solved; but as the results 
 are complicated, it is hardly worth while at present, until a recalcula- 
 tion can be made. I prefer to solve it on the supposition that L is 
 small, and thus merely obtain a correction to Kohlrausch's equation 
 connecting t and t , after which equation (15) or (17) (Maxwell's ' Elec- 
 tricity/ art. 762) can be used when made more general by substituting 
 q for Om. 
 
 As far as I have had time to go at present, the correction seems to 
 be in the direction of making Kohlrausch's determination more nearly 
 coincide with that of the Committee on Electrical Standards of the 
 British Association. Other engagements occupy my attention at pres- 
 ent ; but I hope to see these corrections made to an otherwise excellent 
 determination of this most important unit. 
 
 London, August 4, 1875. 
 
10 
 
 PKELIMINAEY NOTE ON A MAGNETIC PEOOF PLANE 
 
 [American Journal of Science [3], X, 14-17, 1875] 
 
 About four years ago I made a large number of experiments on the 
 distribution of magnetism on iron and steel bars by means of a coil of 
 wire sliding along the bar; the induced current in the coil as measured 
 by a galvanometer was a measure of the number of lines of force cut by 
 the coil and can be found in absolute measure by my method of using 
 the earth inductor. These researches have never yet been published 
 owing to circumstances beyond my control, but are known to quite a 
 number of persons in this country, and will soon be published. The 
 method there used is the only correct one that I know of for experi- 
 menting on magnetic distribution, and my purpose in this note is to 
 extend it to bodies of all shapes, so that experiments on magnetic dis- 
 tribution may become as simple and easy to perform as those on elec- 
 trical distribution. And so well has my magnetic proof plane accom- 
 plished this that I can illustrate the subject to my classes with the 
 greatest ease. 
 
 The apparatus required is merely a small coil of wire i to ^ inch in 
 diameter, containing from 10 to 50 turns, and a Thomson galvanometer. 
 When we require to reduce to absolute measure, another coil about a 
 foot in diameter and containing 20 or 30 turns is required. Having 
 attached the small coil (or, as I call it, the magnetic proof plane) to 
 the galvanometer, we have merely to lay it on the required spot, and 
 when everything is ready, to pull it away suddenly and carry it to a 
 distance, and the momentary deflection of the galvanometer needle will 
 be proportional to that component of the lines of force at that point 
 which is perpendicular to the plane of the coil. And if we apply it to 
 the surface of a permanent magnet the so-called surface density of the 
 magnetism at that point will be nearly proportional to the deflection. 
 In the case of an electro-magnet the surface density will be nearly pro- 
 portional to the deflection minus the deflection which would be pro- 
 duced by the helix alone, though the last is generally small and may be 
 neglected. I use the words nearly proportional in the above statement 
 because thev are only exactly true in the cases where the lines of force 
 
8G HENKY A. KOWLAND 
 
 proceed from the surface in a perpendicular direction; otherwise the 
 deflections must be multiplied by the secant of the angle made by the 
 lines of force with the surface of the magnet. In the case of an electro- 
 magnet made of very soft iron, theory shows that the lines pass out 
 nearly perpendicular to the surface and so no correction is needed. 
 
 We can also, by a coil of this kind, determine the intensity of the 
 magnetic field at any point and thus be able to make a complete map 
 of it. Having done this, we have all the data necessary to substitute 
 in the formula which I have given in this Journal, 1 and by a simple 
 experiment can thus determine the coefficient of magnetization of any 
 diamagnetic or weak paramagnetic body probably in a more accurate 
 manner than any Weber used. Only the largest-sized magnets could of 
 course be used for this purpose with any accuracy, and indeed they are 
 always to be preferred in obtaining the distribution by this method. 
 
 Having obtained the distribution for any given magnet, the distribu- 
 tion for any similar magnet of the same material but of different size 
 becomes known by a well-known law of Sir William Thomson. 
 
 As, in the present state of our knowledge, magnetic measurements 
 are of small value unless made on the absolute scale, we require to 
 reduce our results to this system. There are several methods of doing 
 this, but the simplest is that which I have used in my experiments on 
 magnetic permeability, and consists in including an earth inductor in 
 the circuit. A coil laid on a perfectly level surface is sufficient for 
 this : when this is turned over, the induced current will be equal to C = 
 
 %n ~VA 
 
 where n is the number of turns in the coil, A its mean area, V 
 -Ti- 
 the vertical component of the earth's magnetism, and R the resistance 
 of the circuit. When the small coil is pulled suddenly away the current 
 
 will be C" = *-&?, and so we have Q = 2V^, in which when a 
 li an 6 
 
 Thomson galvanometer is used C' and C can be replaced by the cor- 
 responding deflections: hence = 2V~-, in which a and n' are the 
 
 an D 
 
 area and number of turns in the small coil and Q is that component of 
 the magnetic field we are measuring in the direction of the axis of the 
 small coil. 
 
 As an illustration of this method I will give a few experiments made 
 with the magnets of a Euhmkorff diamagnetic apparatus, which was 
 altogether about 2 ft. long and had its magnets 2 in. in diameter, with 
 
 'On a new diamagnetic attachment to the lantern, &c., this Journal, May, 1875. 
 
PRELIMINARY NOTE ON A MAGNETIC PROOF PLANE 8? 
 
 a hole in. in diameter through them for experiments on the rotation 
 of the plane of polarization of light, but which in these experiments 
 were closed by the solid poles which were screwed on. The first experi- 
 ments were with two discs of iron, 4*6 in. in diameter and If in. thick, 
 screwed on to the poles. In the first place the poles were turned away 
 from one another, the current being sent through only one magnet, 
 and the values of the magnetic field obtained at different points close to 
 the surface of the disc. These may be numbered as follows : No. 1, at 
 centre of face of disc; No. 2, on face of disc half an inch from the edge; 
 No. 3, on centre of edge of disc. The measures are on the metre, gram, 
 second system. 
 
 1st. Strength of current, 4-4 farads per second. 
 
 1. 2220. 2. 3550. 3. 4440. 
 
 2nd. Strength of current 8-3 farads per second. 
 
 1. 3600. 2. 5300. 3. 7500. 
 
 Next the poles were turned toward each other and the current sent 
 through both magnets, so as to make the poles of the same name. 
 Current 4 '6 farads per second. 
 
 1st. Distance of poles, 3 in. 
 
 1. 1300. 3. 3800. 
 
 2nd. Distance of poles, 1^ in. 
 
 1. 600. 3. 4000. 
 
 Here we see an approach to one of Faraday's places of no magnetic 
 action. 
 
 After this the current in one of the magnets was reversed so as to 
 make the poles opposite. Current the same. 
 
 1st. Distance of poles, 3 in. 
 
 1. 5800. 2. 8200. 3. 6700. 
 
 2nd. Distance of poles, 1 in. 
 
 1. 9800. 2. 7500. 3. 5800. 
 
 It is curious to note how the distribution changes with the distance of 
 the discs; thus, on one disc free from the other, the edge of the disc 
 has the greatest magnetic surface density, but when the two discs form 
 opposite poles and are 3 in. apart, position 2 gives the greatest effect, 
 while, when they are 1 in. apart, the field is greatest at the centre. 
 This entirely agrees with theory. 
 
 The conical poles for diamagnetic experiments were then screwed on. 
 These were portions of cones with an angle at vertex of about 60, with 
 the vertex considerably rounded off. They were one inch apart and 
 the poles were opposite. Current 4-4 farads per second. 
 
88 HENRY A. KOWLAND 
 
 At centre of field between the poles 12500 
 
 On the axis near one pole 32100 
 
 On cone one inch from vertex 11000 
 
 On cylindrical portion of magnet 2f inches from the 
 
 vertex of the cone 5800 
 
 These poles were now replaced by frustums of cones with flat ends, 
 the original diameter of the iron, 2 inches, being reduced at the end to 
 If inches, and they were placed \ inch apart. The field in this case 
 between them was 61000, or nearly up to the maximum of magnetiza- 
 tion of nickel at common temperatures, and above that at high tem- 
 peratures. 
 
 Troy, April 1, 1875. 
 
11 
 
 STUDIES ON MAGNETIC DISTK1BUTION 
 
 [Philosophical Magazine [4], L, 257-277, 348-367, 1875] 
 [American Journal of Science [3], X, 325-335, 451-459, 1875; XI, 17-29, 103-108, 1876] 
 
 PART I. LINEAR DISTRIBUTION 
 
 CONTENTS 
 
 I. Preliminary remarks. 
 II. Mathematical theory. 
 
 III. Experimental methods for measuring linear distribution. 
 
 IV. Iron rods magnetized by induction. 
 
 V. Straight electro-magnets and permanent steel magnets. 
 VI. Miscellaneous applications. 
 
 I. 
 
 In a paper of mine published about two years ago, I alluded to some 
 investigations which I had made in 1870 and 1871 on the distribution 
 of magnetism. It is with diffidence that I approach this subject, being 
 aware of the great mathematical difficulties with which it is surrounded. 
 But as the facts are still in advance of what is known on the subject, 
 and as I see that other investigators * are following hard upon my foot- 
 steps, I thought it would be well to publish them, particularly as it is 
 no fault of mine that they did not appear some years ago. 2 The mathe- 
 matical theory which I give, although not particularly elegant, will at 
 least be found to present the matter in a new and more simple light, 
 and may be considered simply as a development of Faraday's idea of 
 the analogy between a magnet and a voltaic battery immersed in water. 
 I shall throughout speak of the conduction of, and resistance to, lines 
 of magnetic force, and shall otherwise treat them as similar to lines of 
 conducted electricity or heat, it now being well established from the 
 researches of Professor Maxwell and others that this method gives 
 exactly the same results as the other method of considering the action 
 to take place at a distance. 
 
 In arranging this paper I have thought best to give the theory of 
 
 1 Particularly M. Jamin. 
 
 2 All the experiments referred to in this paper were made in the winter of 1870-71. 
 
90 HENRY A. BOWLAND 
 
 the distribution first, and then afterwards to see how the results agree 
 with experiment; in this way we can find out the defects of the theory, 
 and what changes should be made in it to adapt it to experiment. 
 
 At present I am acquainted with two formulae giving the distribu- 
 tion of magnetism on bar magnets: the first was given by Biot, in his 
 Traite de Physique Experimentale et Mathematique, vol. iii, p. 77, and 
 was obtained by him from the analogy of the magnet to a dry electric 
 pile, or to a crystal of tourmaline electrified by heat. He compared 
 his formula with Coulomb's observations, and showed it to represent 
 the distribution with considerable accuracy. Green, in his ' Essay/ 
 has obtained a formula which gives the same distribution; but he ob- 
 tains it by a series of mathematical approximations whi^h it is almost 
 impossible to interpret physically. M. Jamin has recently used a 
 formula of the same form; but I have as yet been unable to find how 
 he obtained it. My own formulae are also quite similar to these, but 
 have the advantage of being obtained in a more simple manner than 
 Green's ; and, what is of more consequence, all the limitations are made 
 at once, after which the solution is exact; so that although they are 
 only approximate, yet we know just where they should differ from 
 experiment. 
 
 II. 
 
 If we take an iron bar and magnetize one end of it either by a magnet 
 or helix, we cause lines of magnetic induction s to enter that end of the 
 bar, and, after passing down it to a certain distance, to pass out into 
 the air and so round to the bar again to complete their circuit. At 
 every part of their circuit they encounter some resistance, and always 
 tend to pass in that direction where it is the least: throughout their 
 whole course they obey a law similar to Ohm's law; and the number 
 of lines passing in any direction between two points is equal to the 
 difference of magnetic potential of those points divided by the resist- 
 ance to the lines. 
 
 The complete solution of the problem before us being impossible, let 
 us limit it by two hypotheses. First, let us assume that the permea- 
 bility of the bar is a constant quantity; and secondly, that the resist- 
 ance to the lines of induction is composed of two parts, the first being 
 that of the bar, and the second that of escaping from the bar into the 
 
 3 For difference between lines of magnetic force and lines of magnetic induction 
 see Maxwell's 'Treatise on Electricity and Magnetism,' arts. 400, 592, and 604. 
 
STUDIES ON MAGNETIC DISTRIBUTION 91 
 
 medium - and that the latter is the same at every part of the bar. The 
 first of these assumptions is the one usually made in the mathematical 
 theory of magnetic induction; but, as has been shown by the experi- 
 ments of Miiller, and more recently by those of Dr. Stoletow and my- 
 self, this is not true; and we shall see this when we come to compare 
 the formula with experiment. The second assumption is more exact 
 than the first for all portions of the bar except the ends. 
 
 Let us first take the case of a rod of iron with a short helix placed on 
 any portion of it, through which a current of electricity is sent. The 
 lines of magnetic induction stream down the bar on either side: at 
 every point of the bar two paths are open to them, either to pass further 
 down the rod, or to pass out into the air. We can then apply the 
 ordinary equations for a derived circuit in electricity to this case. 
 Let n be the magnetic permeability of the iron, 
 
 R be the resistance of unit of length of the rod, 
 
 R' be the resistance of medium along unit of length of rod, 
 
 /> be the resistance at a given point to passing down the rod, 
 
 s be the resistance at the end of the rod, 
 
 Q' 4 be the number of lines of induction passing along the rod 
 
 at a given point, 
 $'. 5 be the number of lines of induction passing from the rod 
 
 into the medium along a small length of the rod JL, 
 L be the distance from the end of the rod to a given point, 
 
 R ' 
 
 A _ V RR' + s 
 
 , dL 
 
 + dp= ,57 
 
 To find ft, the ordinary equation for the resistance of a derived cir- 
 cuit gives 
 
 whence 
 
 4 These are the surf ace-integrals of magnetic induction (see Maxwell's ' Electricity,' 
 
 art. 402) the first across the section of the bar, and the second along a length AZ, 
 
 of the surface of the bar. 
 
 5 It is to be noted that Q', when A is constant, is nearly proportional to the so- 
 called surface-density of magnetism at the given point. 
 
92 HENRY A. EOWLAND 
 
 and 
 
 To find Q', we have 
 
 whence 
 
 and 
 
 fV^AT HAT 
 
 ^ _-"). . . (3) 
 
 When L is very large, or s =*/RR' , we have 
 
 Q' = Cf L > and C: 
 in which L / is reckoned from an origin at any point of the rod. 
 
 These equations give the distribution on the part outside the helix; 
 and we have now to consider the part covered by the helix. Let us 
 
 A: c: E 
 
 FIG. 1. 
 
 limit ourselves to the case where the helix is long and thin, so that the 
 field in its interior is nearly uniform. 
 
 As we pass along the helix, the change of magnetic potential due to 
 the helix is equal to the product of the intensity of the field multiplied 
 by the distance passed over ; so that in passing over an elementary dis- 
 tance dy the difference of potential will be &dy. The number of lines 
 of force which this difference of potential causes in the rod will be equal 
 to Qdy divided by the sum of the resistances of the rod in both direc- 
 tions from the given point. These lines of force stream down the rod 
 on either side of the point, creating everywhere a magnetic potential 
 which can be calculated by equation (2), and which is represented by 
 the curves in Fig. 1. In that figure A B is the rod, C D the helix, and 
 
 cPQ' 
 This could have been obtained directly from the equation ,? 9 =Q / r y , and Q/ e from 
 
 Cl-Li' 
 
 dQ' 
 the equation Q f e = -V A L. 
 
STUDIES ON MAGNETIC DISTEIBUTION 93 
 
 E the element of length dy. Now, if we take all the elements of the 
 rod in the same way and consider the effect at H F, the total magnetic 
 potential at this point will, by hypothesis No. 1, be equal to the sum 
 of the potentials due to all the elements dy. 
 
 Let 4Q' be the number of lines of force produced in the bar at the 
 point E due to the elementary difference of potential at 
 that point, Qdy, 
 AQ" be the number o* lines of force arriving at the point F due 
 
 to the same element, 
 
 Q" be the number of lines passing from bar along length JL, 
 /> be the sum of the resistances of the bar in both directions 
 
 from E, 
 
 /> z be resistance at F in direction of D, 
 y be the distance D E, 
 x be the distance D F, 
 6 be the distance C D, 
 s" and s' be the resistance of the bar, &c., respectively at C in 
 
 the direction of A, and at D in direction of B, 
 be the magnetizing-force of helix in its interior. 
 Let 
 
 At y jt^t -r * AH *v jm, T * 
 
 ** ~ * ^ 9 " ' j---,^ ^>^ 7i 9 
 
 f>* = 
 
 ft 
 
 4- e 
 
 _ 
 
 ~ 2R'r A'A"-1 
 
 This gives the positive part of Q"- To find the negative part, 
 change x into & a;, A' into A", and A" into A', and then change the 
 sign of the whole. 
 
 When the helix is symmetrically placed on the bar, we have s' = s", 
 A'=A"; whence, adding the positive and negative parts together, we 
 have 
 
94 HENRY A. ROWLAND 
 
 " = J -/ y * ~ A ' ( e r (-*> rx> ) (5^) 
 
 ZVTU? A'? b 1 v 
 
 which gives the number of lines of induction passing out from the rod 
 along the length AL when the helix is symmetrically placed on the rod. 
 To get the number of lines of induction passing along the rod at a 
 given point, we have 
 
 f\Z (L 1 A I 
 
 where 
 
 c rt 1 
 
 When the bar extends a distance L' out of both ends of the helix, so 
 that 
 
 if = */RW and A' = 
 
 we have 
 
 It may be well, before proceeding, to define what is meant by mag- 
 netic resistance, and the units in which it is measured. If ft is the 
 magnetic permeability of the rod, we can get an idea of the meaning 
 of magnetic resistance in the following manner. Suppose we have a 
 rod infinitely long placed in a magnetic field of intensity parallel to 
 the lines of force. Let Q' be the number of lines of inductive force 
 passing through the rod, or the surface-integral of the magnetic induc- 
 tion across its section; also let a be the area of the rod. Then by 
 
 definition n = -sL. If L is the length of the rod, the difference of 
 
 flEty 
 
 potential at the ends will be LS& ; hence 
 
 0' - L and fl - - L - L 
 
 ^ X ' ~ IT ~^' 
 
 and R in the formula? becomes 
 
 R _ R, _ . 1 
 
 -ft -jL . 
 
 L* a/j. 
 
 It is almost impossible to estimate R' theoretically, seeing that it 
 will vary with the circumstances. We can get some idea of its nature, 
 however, by considering that the principal part of it is due to the 
 cylindric envelope of medium immediately surrounding the rod. The 
 resistance of such an envelope per unit of length of rod is 
 
STUDIES ox MAGNETIC DISTRIBUTION 95 
 
 where D is the diameter of the envelope, d of the rod, and /JL } the permea- 
 bility of the medium. But we are not able to estimate D. If, however, 
 we have two magnetic systems similar in all their parts, it is evident 
 that beyond a certain point similarly situated in each system we may 
 
 neglect the resistance of the medium, and -r will be the same for the 
 
 two systems. Hence R' is approximately constant for rods of all diam- 
 eters in the same medium, and r takes the form 
 
 r = ^ 
 
 It is evident that the reasoning would apply to rods of any section as 
 well as circular. 
 
 In Green's splendid essay (Eeprint, p. Ill, or Maxwell's ' Treatise 
 on Electricity and Magnetism,' art. 439) we find a formula similar to 
 equation (5), but obtained in an entirely different manner, and applying 
 only to rods not extending beyond the helix. In the ' Keprint,' ft 
 corresponds to my r; and its value, using my notation, is obtained from 
 the equation 
 
 231863 2 hyp. log p + 2p = _ 4 , , .... (8) 
 
 rd 
 where p = -=-. 
 
 rd 
 If we make p a constant in this formula, we must have p == -^ = 
 
 constant; hence 
 
 which is the same result for this case as from equation (7). 
 
 When fj. in the two formula is made to vary, the results are not 
 exactly the same; but still they give approximately the same results for 
 the cases we shall consider; and since the formula is at the best only 
 approximate, we shall not spend time in discussing the merits of the 
 two. 
 
 III. 
 
 Among the various methods of measuring linear magnetic distribu- 
 tion, we find few up to the present time that are satisfactory. Coulomb 
 used the method of counting the number of vibrations made by a 
 magnetic needle when near various points of the magnet. Thus, in 
 
96 HENRY A. KOWLAND 
 
 the curve of distribution most often reproduced from his work, he used 
 a magnetized steel bar 27 French inches long and 2 lines in diameter 
 placed vertically; opposite to it, and at a distance of 8 lines, he hung 
 a magnetic needle 3 lines in diameter and 6 lines long, tempered very 
 hard; and the number of oscillations made by it was determined. The 
 square of this number is proportional to the magnetic field at that point, 
 supposing the magnetism of the needle to be unchanged; and this, 
 corrected for the magnetism of the earth, gives the magnetic field due 
 to the magnet alone. This for points near the magnet and distant from 
 the ends is nearly proportional to the so-called magnetic surface-density 
 opposite the point. At the end Coulomb doubled the quantity thus 
 found, seeing that the bar extended only on one side of the needle. 
 
 It will be seen that this method is only approximate, and almost 
 incapable of giving results in absolute measure. The effect on the 
 needle depends not only on that part of the bar opposite the needle, 
 but on portions to either side, and gives, as it were, the average value 
 for some distance; in the next place, the correction at the end, by 
 multiplying by 2, seems to be inadequate, and gives too small a result 
 compared with other parts. For at points distant from the end the 
 average surface-density at any point will be nearly equal to the average 
 for a short distance on both sides, while at the end it will be greater 
 than the average of a short distance measured back from the end. To 
 these errors must be added those due to the mutual induction of the 
 two magnets. 
 
 The next method we come to is that which has been recently used 
 by M. Jamin, and consists in measuring the attraction of a piece of 
 soft iron applied at different points of the magnet. In this case it 
 does not seem to have been considered that the attraction depends not 
 only on the magnetic density at the given point, but also on that around 
 it, and that a piece of soft iron applied to a magnet changes the distri- 
 bution immediately at all points, but especially at that where the iron is 
 applied. The change is of course less when the magnet is of very hard 
 steel and the piece of soft iron small. Where, however, we wish to 
 get the distribution on soft iron, it becomes a quite serious difficulty. 
 Another source of error arises from the fact that the coefficient of 
 magnetization of soft iron is a function of the magnetization: this 
 source of error is greatest when the contact-piece is long and thin, and 
 is a minimum when it is short and thick and not in contact with the 
 magnet. Hence this method will give the best results when the con- 
 tact-piece is small and in the shape of a sphere and not in contact with 
 
STUDIES ON MAGNETIC DISTRIBUTION 97 
 
 the magnet, and when the method is applied to steel magnets. But 
 after taking all these precautions, the question next arises as to how 
 to obtain the magnetic surface-density from the experiments. Theory 
 indicates, and M. Jamin has assumed, that the attractive force is nearly 
 proportional to the square of the surface-density. But experiment 
 does not seem to confirm this, except where there is some distance 
 between the two bodies, at least in the case of a sphere and a plane 
 surface, as in Tyndall's experiments (Phil. Mag., April, 1851). It is 
 not necessary at present to consider the cause of this apparent dis- 
 crepancy between theory ar>d experiment; suffice it to say that the 
 explanation of the phenomenon is without doubt to be sought for in 
 the variable character of the magnetizing-function of iron. All I wish 
 to show is that the attraction of iron to a magnet, especially when the 
 two are in contact, is a very complicated phenomenon, whose laws in 
 general are unknown, and hence is entirely unsuitable for experiments 
 on magnetic distribution. 
 
 A third method is that used in determining the correction for the 
 distribution on the magnets in finding the intensity of the earth's 
 magnetism. Usually the distribution is not explicitly found in this 
 case; but it is easy to see how it might be. Thus, one way would be as 
 follows: Take the origin of coordinates at the centre of the magnet. 
 Develop the distribution in an ascending series of powers of x with 
 unknown constant coefficients. Calculate the magnetic force due to 
 this distribution for any points along the axis, or else on a line perpen- 
 dicular to the magnet at its centre. Determine the force at a series of 
 points extending through as great a range and as near the magnet as 
 possible. These experiments give a series of equations from which the 
 coefficients in the expansion can be determined. Other and better 
 methods of expansion might be found, except for short magnets, where 
 the method suggested is very good. 
 
 The similarity of this method to that used by Gauss in determining 
 the distribution on the earth is apparent. 
 
 A fourth method is similar to the above, except that the lines of 
 force around the magnet are measured and calculated instead of the 
 force. 
 
 The last two methods are very exact, but are also very laborious, and 
 therefore only adapted to special investigations. Thus, by the change 
 in direction of the lines of force around the magnet, we have a delicate 
 means of showing the change in distribution, as, for instance, when the 
 current around an electro-magnet varies. 
 
98 HENEY A. EOWLAND 
 
 The fifth method is that used lately in some experiments of Mr. 
 Sears (American Journal of Science, July, 1874), but only adapted to 
 temporary magnetization. At a given point on the bar a small coil of 
 wire is placed, and the current induced in it measured by the swing of 
 the galvanometer-needle when the bar is demagnetized. It does not 
 seem to have been noticed that what we ordinarily consider the mag- 
 netic distribution is not directly measured in this way; and indeed, to 
 get correct results, the magnetization should have been reversed, seeing 
 that a large portion of the magnetization will not disappear, on taking 
 away the magnetizing-force, where the bar is long. The quantity which 
 is directly measured is the surface-integral of the temporary magnetic 
 induction across the section of the bar, while the magnetic surface- 
 density is proportional to the surface-integral of magnetic induction 
 along a given portion of the Itar. In other words, the quantity measured 
 
 is Q instead of -^L. We can, however, derive one from the other very 
 easily. 
 
 The sixth and last method is that which I used first in 1870, and by 
 which most of my experiments have been performed. This consists in 
 sliding a small coil of wire, which just fits the bar and is also very 
 narrow, along the bar inch by inch, and noting the induced current 
 over each inch by the deflection of a galvanometer-needle. This meas- 
 ures Q f , except for some corrections which I now wish to note. In the 
 first case, to give exact results, the lines of force should pass out per- 
 pendicular to the bar, or the coil must be very small. But even when 
 the last condition is fulfilled errors will be introduced at certain por- 
 tions of the bar. The error is vanishingly small in most cases, except 
 near the ends; and even there it is not large, except in special cases; 
 for at this part the lines of force pass forward toward the end of the 
 bar, and so the observation next to the end may be too small, while 
 that at the end is too large. The correction can be made by finding 
 where the lines of force through the centre of the section of the coil 
 in its two positions meet the bar. The error from this source is not 
 large, and may be avoided to a great extent. 
 
 One very great advantage in the method of induced currents is the 
 facility with which the results can be reduced to absolute measure by 
 including an earth-inductor in the circuit as I have before described 
 (Phil. Mag., August, 1873). There is also no reaction (except a tem- 
 porary one) between the magnet and current; so that the distribution 
 remains unchanged. Hence it seems to me that this method is the 
 only one capable of giving exact results directly. 
 
STUDIES ON MAGNETIC DISTRIBUTION 99 
 
 The coils of wire which I used consisted of from twenty to one 
 hundred turns of fine wire wound on thin paper tubes which just fitted 
 the bar and extended considerably beyond the coils. The coils were 
 mostly from -1 to -25 of an inch wide and from -1 to -2 inch thick. A 
 measure being laid by the side of the given bar under experiment, the 
 coil was moved from one division of the rule to the next very quickly, 
 and the deflection produced on an ordinary astatic galvanometer noted. 
 After experience this could be done with great accuracy. It might be 
 better in some cases to have the coil slide over a limited distance on 
 the tube, though for the use to which I intend to put the results the 
 other is best. 
 
 Up to 35 Q f is nearly proportional to the deflection; and when any 
 larger value is put down in the Tables, it is the sum of two or more 
 deflections. I have not the data in most cases to reduce my results 
 to absolute measure, but took pains to ensure that certain series of ex- 
 periments should be comparable among themselves. 
 
 Having measured Q e at all points of a rod, we may find Q by adding 
 up the values of Q f from the end of the rod. 
 
 The magnetizing force to which the bar was subjected was in all 
 cases a helix placed at some part of the bar. The iron bars were of 
 course demagnetized thoroughly before use by placing them in the 
 proper position with reference to the magnetic meridian and striking 
 them. 
 
 In the Tables L is the distance in inches from the zero-point, Q f is 
 the deflection of the galvanometer when the helix is passed between the 
 points indicated in the first column. Thus, in Table II, 34-7 is the 
 deflection on the galvanometer when the helix was moved from the 
 tenth to the eleventh inch from the zero-point; and so we may con- 
 sider it as the value of Q f at 10 inches; so that the values of Q ( refer 
 to the half inches, but Q to the even inches. 
 
 In all the calculations the constants in the formulae were taken to 
 represent Q most nearly, and then the corresponding formulae for Q e 
 taken with the same constants. 
 
 For ease in calculating by ordinary logarithmic Tables, we may put 
 
 -rL 1 /ymSrt 
 
 IV. 
 
 Table I is from a bar 17 inches long with a magnetizing helix 1 
 inch long at one end, the zero-point being at the other. Table II is 
 from a bar 9 feet long with a helix 4$ inches long quite near one end, 
 the zero-point being at 1 inch from the helix toward the long end. 
 
100 
 
 HENRY A. EOWLAND 
 
 Table III is from a bar 2 feet long with a helix 4r| inches long near 
 one end, so that its centre was 19f inches from the end on which the 
 experiments were made, the zero-point being at the end. 
 
 In adapting the formula to apply to the case of Table I, we may 
 assume that at the end of the bar s =o> and (7 = 0, which is equivalent 
 to assuming that the number of lines of induction which pass out at 
 the end of the rod are too small to be appreciated. 
 
 TABLE I. 
 
 BAR -18 INCH DIAMETER. AT END OF BAR. 
 
 L. 
 
 < 
 
 Q'. 
 Calcu- 
 
 Error of 
 
 at 
 
 Q'. 
 Calcu- 
 
 Error of 
 
 
 served. 
 
 lated. 
 
 Q,. 
 
 served. 
 
 lated. 
 
 
 
 
 
 
 
 
 
 
 
 
 
 3 
 
 
 .... 
 
 
 2-7 
 
 3-5 
 
 + -8 
 
 5 
 6 
 7 
 8 
 9 
 10 
 11 
 12 
 13 
 14 
 
 2-0 
 2-5 
 3-2 
 3-7 
 4-3 
 5-3 
 6-5 
 7-7 
 9-5 
 
 2-0 
 2-4 
 2-8 
 3-5 
 4-3 
 5-2 
 6-5 
 8-0 
 9-9 
 
 
 -1 
 -4 
 -2 
 
 -1 
 
 + -3 
 + -4 
 
 5-9 
 
 7-9 
 10-4 
 13-6 
 17-3 
 21-6 
 26-9 
 33-4 
 41-1 
 50-6 
 
 6-6 
 8-6 
 11-0 
 13-8 
 17-3 
 21-6 
 26-8 
 33-3 
 41-3 
 51-2 
 
 + -7 
 + -7 
 + -6 
 + -2 
 
 
 -1 
 -1 
 + -2 
 + -6 
 
 n^iCi,=,54 (e +e -, 
 
 In Table II observations were not made over the whole length of 
 the rod, and the zero-point was not at the end of the bar. It is evident, 
 however, that by giving a proper value to s we may suppose the bar to 
 end at any point. As the rod is very long, expressions of the form 
 
 Q'C" = 0'^ L C" and Q' t = rC'e-* L 
 will apply. 
 
 In Table II the observations were near the end of the rod, and were 
 repeated several times. Neglecting the end of the rod, we have s=oo . 
 
 In these Tables we see quite a good agreement between theory and 
 observation; but on more careful examination we observe a certain law 
 in the distribution of errors. Thus in Table I the errors of Q' are all 
 positive between and 8 inches; and this has always been found to be 
 the case at this part of the bar in all my experiments. 
 
 The explanation of this is very simple. In obtaining the formulae,, 
 we assumed that the magnetic permeability of the bar fj. was a constant 
 
STUDIES ON MAGNETIC DISTRIBUTION 
 
 101 
 
 TABLE II. 
 BAR -39 INCH DIAMETER. AT 1 INCH FROM HELIX. 
 
 L. 
 
 served. 
 
 Calcu- 
 lated. 
 
 Error of 
 Q^- 
 
 Q'-C". 
 Ob- 
 served. 
 
 Q'-C". 
 Calcu- 
 lated. 
 
 Error of 
 Q'- 
 
 
 1 
 2 
 3 
 4 
 5 
 6 
 7 
 8 
 9 
 10 
 11 
 12 
 13 
 14 
 15 
 16 
 17 
 18 
 19 
 21 
 23 
 25 
 27 
 29 
 31 
 
 
 
 
 825-2 
 753-5 
 688-3 
 628-8 
 575-3 
 524-1 
 477-4 
 434-2 
 394-2 
 357-0 
 322-3 
 290-6 
 261-1 
 235-4 
 209-9 
 187-9 
 166-4 
 146-4 
 127-3 
 94-8 
 67-3 
 44-3 
 25-8 
 11-3 
 
 
 902-5 
 825-9 
 755-1 
 689-8 
 629-5 
 574-3 
 523-1 
 476-0 
 432-5 
 392-5 
 355-6 
 321-5 
 290-1 
 261-2 
 234-5 
 210-0 
 187-3 
 166-4 
 147-1 
 129-4 
 97-8 
 71-1 
 48-6 
 29-0 
 12-6 
 1-2 
 
 + -7 
 + 1-6 
 + 1-5 
 + -7 
 1-0 
 1-0 
 1-4 
 1-7 
 1-7 
 1-4 
 -8 
 -5 
 + -1 
 -9 
 + -1 
 -6 
 
 + -7 
 + 2-1 
 + 3-0 
 + 3-8 
 + 4-3 
 + 3-2 
 + 1-3 
 1-2 
 
 71-7 
 65-2 
 59-5 
 53-5 
 51-2 
 46-7 
 43-2 
 40-0 
 37-2 
 34-7 
 31-7 
 29-5 
 25-7 
 25-5 
 22-0 
 21-5 
 20-0 
 19-1 
 32-5 
 27-5 
 23-0 
 18-5 
 14-5 
 11-3 
 
 70-8 
 65-3 
 60-2 
 55-5 
 51-2 
 47-2 
 43-5 
 40-1 
 37-0 
 34-1 
 31-4 
 28-9 
 26-6 
 24-6 
 22-7 
 20-9 
 19-3 
 17-8 
 31-5 
 26-7 
 22-8 
 19-4 
 16-5 
 14-0 
 
 -9 
 + -1 
 + -7 
 + 2-0 
 
 + -5 
 + -3 
 + -1 
 -2 
 -6 
 -3 
 -6 
 + -9 
 -9 
 + -7 
 -6 
 .7 
 
 1-3 
 1-0 
 
 -8 
 -2 
 + -9 
 + 2-0 
 
 + 2-7 
 
 Qf _C' // =983r-o8i35z;_80-5=983-(10)--o<tfA_80-5. 
 
 quantity; but it has been shown by Dr. Stoletow and myself, independ- 
 ently of each other, that JJL increases as the magnetism of the bar in- 
 creases when the latter is not great. Hence between and 8 inches 
 the resistance of the bar, R, is greater than at succeeding points, and 
 hence a less number of lines of induction pass down the bar from 8 
 towards than would be given by the formula, which has been adapted 
 to the average value of E at from 9 to 14 inches. In Table II this 
 same fact shows itself towards the end of the Table, and would prob- 
 ably be more prominent had the Table been carried further. However, 
 in this Table all things have combined to satisfy the formula with great 
 accuracy. 
 
 In Table III we come across a fact of an entirely different nature 
 from the above. Fig. 2 is the plot of this Table, and gives the values 
 of Q' ( at different parts of the rod. 
 
102 
 
 HENRY A. EOWLAND 
 
 TABLE III. 
 BAB -39 INCH DIAMETER. AT END OF BAR. 
 
 L. 
 
 served. 
 
 Qe. 
 
 Calcu- 
 lated. 
 
 Error of 
 
 served. 
 
 Q'- 
 Calcu- 
 lated. 
 
 Error of 
 Q'- 
 
 o 
 
 
 
 
 0- 
 
 o 
 
 
 
 1 
 2 
 3 
 
 19-7 
 16-3 
 16-0 
 
 15-2 
 15-3 
 15-5 
 
 4-5 
 1-0 
 -5 
 
 19-7 
 36-0 
 52-0 
 
 15-2 
 30-5 
 46-0 
 
 4-5 
 5-5 
 6-0 
 
 4 
 5 
 6 
 
 15-8 
 16-5 
 17-0 
 
 15-9 
 16-3 
 16-9 
 
 + -1 
 -2 
 -1 
 
 67-8 
 84-3 
 101-3 
 
 61-8 
 78-1 
 95-0 
 
 6-0 
 6-2 
 6-3 
 
 7 
 8 
 9 
 10 
 11 
 12 
 13 
 14 
 15 
 16 
 
 17-6 
 18-4 
 19-2 
 20-3 
 21-8 
 22-8 
 84-8 
 26-8 
 28-8 
 31-8 
 
 17-6 
 18-4 
 19-4 
 20-5 
 21-7 
 23-1 
 24-7 
 26-5 
 28-4 
 30-5 
 
 
 
 + -2 
 + -2 
 -1 
 + -3 
 -1 
 -3 
 -4 
 1-3 
 
 118-9 
 137-3 
 156.5 
 176-8 
 198-6 
 221-4 
 246-2 
 273-0 
 301-8 
 333-6 
 
 112-6 
 130-9 
 150-3 
 170-7 
 192-2 
 215-3 
 239-9 
 266-4 
 294-6 
 325-1 
 
 6-3 
 6-4 
 6-2 
 6-1 
 6-4 
 6-1 
 6-3 
 6-6 
 7-2 
 8-5 
 
 Q' t =7-6(10 os7t-)-io-'OS7L) ; Q'=89(10 37i 10- 37t ). 
 
 The horizontal line in the figure represents values of L, and the verti- 
 cal ordinates are values of Q' g . The full line gives the observed dis- 
 tribution, and the dotted line that according to the formula. 
 
 15 10 5 O 
 
 FIG. 2. Distribution at end of bar. 
 
 The formula gives the distribution very nearly for all points except 
 those near the end. The formula indicates that Q' f decreases contin- 
 ually toward the end; but by experiment we see that it increases near 
 this point. On first seeing this, I thought that it was due to some 
 residual magnetism in the bar; but after repeating the experiment 
 several times with proper care, I soon found that this was always the 
 case. I give the following explanation of it : In the f ormulse we have 
 assumed R', the resistance of the medium, to be a constant; now this 
 resistance includes that of the lines of force as they pass from the rod 
 through the medium and thus back to the other end of the rod ; and of 
 
STUDIES ON MAGNETIC DISTRIBUTION 103 
 
 this whole quantity the part which affects the relative distribution at 
 any part of the rod most is that of the medium immediately surrounding 
 that part; and so the parts near the end have the advantage over those 
 further back, inasmuch as the lines can pass forward as well as outward 
 into the medium. The same thing takes place in the case of the dis- 
 tribution of electricity, where the "density" is inversely proportional 
 to the resistance which the lines of inductive force experience from 
 the medium; and here we find that the "density" is greatest on the 
 projections of the body, showing that the resistance to the lines of in- 
 duction is less in such situations, and by analogy showing that this 
 must also be the case for lines of magnetic force. But this effect is 
 not very great in cylinders until quite near the end; for Coulomb, in a 
 long electrified cylinder, has found the density at one diameter back 
 from the end only 1-25 times that at the centre; and so there is prob- 
 ably a long distance in the centre where the density is sensibly constant. 
 Hence we may suppose that our second hypothesis, that R' is a con- 
 stant, will be approximately correct for all parts of a bar except the 
 ends, though of course this will vary to some extent with the distribu- 
 tion of the lines in the medium; at least the change in E' will be 
 gradual except near the end, and so may be partially allowed for by 
 giving a mean value to r. 
 
 Hence we see that could the formula be so changed as to include 
 both the variation of R and of R', it would probably agree with the 
 three Tables given. 
 
 To study the effect of variation in the permeability more carefully, 
 we can proceed in another manner, and use the formulae only to get 
 the value of r at different parts of the rods. 
 
 No matter how r may vary, equations (2) and (3) will apply to a very 
 small distance Z along the rod; and as the orgin of coordinates may be 
 at any point on the rod, if Q r and Q' f are taken at one point and Q and 
 Q t at another point whose distance from the first is Z, we shall have the 
 four equations 
 
 Calling " =H and ? = G, we shall find, on eliminating C and A 
 and developing r ' and ?~ rt , 
 
104 
 
 HENRY A. EOWLAND 
 
 ? m 1***-i), 
 
 f \ (jf + ti / 
 
 or, to a greater degree of approximation, 
 
 r" 
 
 + 1-6 
 
 (9ft) 
 
 Before applying these formulae to any series of observations, the 
 latter should be freed from most of the irregularities due to accidental 
 causes. For this purpose the following Tables have been plotted and a 
 regular curve drawn to represent as nearly as possible the observations; 
 in other cases a column of differences was formed and plotted. In 
 either case the ordinates of the curves were accepted as the true quan- 
 tities. But, for fear that some might accuse me of tampering with my 
 observations, I have in all cases added these as they were obtained. 
 
 TABLE IV. 
 BAR -19 INCH DIAMETER. AT CENTRE OF BAR. 
 
 L. 
 
 Qe- 
 
 Observed. 
 
 Qi. 
 
 Corrected. 
 
 Q'. 
 Corrected. 
 
 r " IT 
 
 1 K' 
 r 2 ~ K 
 
 1 
 
 2 
 3 
 4 
 5 
 
 24-0 
 17-0 
 13-7 
 11. 6 
 
 10-2 
 
 24-0 
 17-0 
 13-7 
 11-65 
 10-15 
 
 151-7 
 127-7 
 110-7 
 97.0 
 85-4 
 
 041 
 0256 
 0192 
 0168 
 
 24.4 
 39-1 
 52-1 
 59-5 
 
 
 9-0 
 
 9-0 
 
 
 0150 
 
 66-7 
 
 7 
 8 
 
 8-0 
 7-1 
 
 8.0 
 7-15 
 
 66-2 
 
 58-2 
 
 0142 
 0150 
 
 70-4 
 66-7 
 
 9 
 10 
 11 
 12 
 13 
 14 
 15 
 28^ 
 
 6-4 
 5-7 
 4-9 
 4-4 
 3-6 
 3-3 
 22-4 
 
 6-35 
 5-65 
 5-0 
 4-4 
 3.9 
 3-4 
 22-4 
 
 51-1 
 44-7 
 39-1 
 34-1 
 29-7 
 25-8 
 22-4 
 
 0159 
 0160 
 0167 
 0180 
 0184 
 0184 
 
 62-9 
 52-5 
 59-9 
 55-6 
 54-3 
 54-3 
 
 The correction is necessary, because small irregularities in the obser- 
 vations will produce immense changes in r 2 . 
 
 Table IV contains some of the best observations I have obtained. 
 It is from a bar 57 inches long with a helix 1| inch long in the centre 
 to magnetize it. Each quantity is the mean of six observations, these 
 being made on both ends of the bar and with the current in opposite 
 directions. 
 
 In this Table a source of error was guarded against which I have not 
 
STUDIES ON MAGNETIC DISTRIBUTION 105 
 
 seen mentioned elsewhere. When a bar of iron is magnetized at any 
 part and the distribution over the rest quickly measured, on being then 
 allowed to stand some time and the distribution again taken, it will have 
 changed somewhat, the magnetism having, as it were, crept down the 
 bar further. Hence in this Table time was allowed for the bar to reach 
 its permanent state. 
 
 1 R r 
 On looking over column 6, which contains the values of -^ -^ = R'a/i 
 
 (equation 7), we observe that as Q' decreases, the value of R'ap. first 
 increases and then decreases. Now it is not probable that R' undergoes 
 any sudden change of this sort; and so it is probably due to change in 
 the permeability of the rod. Hence by this method we arrive at the 
 same results as by a more direct and exact method. 7 But by this means 
 we are able to prove in the most unequivocal manner that magnetic 
 permeability is a function of the magnetization of the iron and not of the 
 magnetizing force. Hence it is that I have preferred, in my papers on 
 Magnetic Permeability, to consider it in this way in the formulae and 
 also in the plots, while Dr. Stoletow (in his paper, Phil. Mag., January, 
 1873) plots the magnetizing-function as a function of the magnetizing 
 force. 
 
 When we plot the results in this Table with reference to Q' and R'a^, 
 the effect of the variation of R' is apparent; and we see, on comparing 
 the curve with those given in my paper above referred to, that R' in- 
 creases as L increases, at least between L = 2 and L = 8, which is as 
 we should suppose from the arrangement of the apparatus. For this 
 Table I happen to have data for determining Q in absolute measure; 
 and these show that the maximum value of n should be about where 
 the Table shows it to be. 
 
 This method of finding the variation of p is analogous to that of 
 finding conductivity for heat by raising the temperature of one end 
 of a bar and noting the distribution of heat over the bar; indeed the 
 curves of distribution are nearly the same in the two cases. 
 
 If it were thought worth while, it would be very easy to obtain a 
 curve of magnetic distribution for a rod and then enclose the whole 
 rod in a helix and determine its curve of permeability. This would 
 give data for determining R' in absolute measure at every point of the 
 rod. 
 
 To complete the argument that the variation of r z is in great measure 
 due to that of //, I have caused the magnetizing force on a bar to vary. 
 
 7 Phil. Mag., August, 1873. 
 
106 
 
 HENRY A. EOWLAND 
 
 Tables V, VI, and VII are from a bar 9 feet long and -25 inch in 
 diameter. At the centre a single layer of fine wire was wound for a 
 distance of 1 foot; and the current for magnetizing the bar was sent 
 through this. The zero-point was at the centre of this helix and at the 
 centre of the bar; so that the observations on the first 6 inches include 
 the part of the bar covered by the helix. 
 
 The values of Q' f are the sum of four observations on each end of 
 the bar and with the current reversed. The three Tables are compar- 
 able with each other, the same arbitrary unit being used for all. 
 
 TABLE V. 
 MAGNETIZING CURRENT -176. 
 
 L. 
 
 fe 
 
 served. 
 
 Qe- 
 
 Cor- 
 rected. 
 
 Cor- 
 rected. 
 
 ** 
 
 1 R' 
 
 F' = R~- 
 
 Qe". 
 
 Calcu- 
 lated. 
 
 
 
 2-7 
 
 
 
 
 
 2-40 
 
 1 
 
 6-9 
 
 
 
 
 
 7-32 
 
 2 
 
 12-7 
 
 
 
 
 
 12-54 
 
 3 
 
 18-2 
 
 
 
 
 
 18-31 
 
 4 
 
 24-4 
 
 
 
 
 
 24-87 
 
 5 
 6 
 7 
 8 
 9 
 10 
 11 
 12 
 13 
 14 
 15 . 
 16 
 17 j. 
 18 ' 
 End. 
 
 32-4 
 31-5 
 28-2 
 24-9 
 21-4 
 18-6 
 16-8 
 14 2 
 12-0 
 
 17-7 
 
 11-6 
 22-4 
 
 31-7 
 32-0 
 28-2 
 24-7 
 21-7 
 19-0 
 16-4 
 14-2 
 12-0 
 10-0 
 8-2 
 6-6 
 5-1 
 22-4 
 
 220-5 
 188-5 
 160-3 
 135-6 
 113-9 
 94-9 
 78-5 
 64-3 
 52-3 
 42-3 
 34-1 
 27-5 
 22-4 
 
 0190 
 0212 
 0218 
 0236 
 0252 
 0278 
 0311 
 0367 
 0404 
 0440 
 0445 
 0570 
 
 52-4 
 
 47-2 
 45-9 
 42-4 
 39-7 
 36-0 
 32-2 
 27-2 
 24-8 
 22-7 
 22-5 
 17-5 
 
 32-38 
 
 
 A ^ 
 
 II 
 
 OS 
 00 
 
 f 
 
 t-L 
 
 o 
 
 3 
 
 r 
 
 o 
 
 o 
 
 H 
 
 Here we see an excellent confirmation of the results deduced from 
 Table IV. In Table V, where the magnetizing force is very small, and 
 where, consequently, no part of the iron has yet reached its minimum 
 
 1 R' 
 resistance, the value of t ~ ^ R'ap. decreases continually as the value 
 
 of Q' decreases, as it should do. In Table VI, with a higher magnetiz- 
 ing power, which was sufficient to bring a portion of the bar to about 
 
 the minimum resistance, we see that -5 remains nearly stationary for a 
 
 short distance from the helix and then decreases in value. In Table 
 VII, where the bar is highly magnetized and the portion near the zero- 
 
STUDIES ON MAGNETIC DISTRIBUTION 
 
 107 
 
 TABLE VI. 
 MAGNETIZING CURRENT -31. 
 
 L. 
 
 Si 
 
 served. 
 
 CoV- 
 rected. 
 
 Cor- 
 rected. 
 
 t-2. 
 
 r* 
 
 9''- 
 Calcu- 
 lated. 
 
 
 
 16-3 
 
 
 
 
 
 17-3 
 
 2 
 
 22-0 
 
 
 
 
 
 22-3 
 
 3 
 
 32-4 
 
 
 
 
 
 32-28 
 
 4 
 
 43-8 
 
 
 
 
 
 43-34 
 
 5 
 6 
 
 7 
 8 
 9 I 
 
 11 i 
 
 8 
 gj 
 
 16 ( 
 17 f 
 
 1ft I 
 
 55-9 
 55-2 
 46-8 
 
 81-3 
 61-8 
 46-4 
 35-4 
 22-0 
 
 55-1 
 48-1 
 42-3 
 37-4 
 33 
 29-0 
 25-3 
 21-9 
 18-7 
 15-6 
 12-7 
 9-8 
 
 391-9 
 336-8 
 288-7 
 246-4 
 209 
 176-0 
 147-0 
 121-7 
 99-8 
 81-1 
 65-5 
 52-8 
 
 0204 
 0201 
 0202 
 0220 
 0243 
 0262 
 0300 
 0352 
 0405 
 0479 
 
 49-0 
 49-7 
 49-5 
 45-5 
 41-2 
 38-2 
 33-3 
 28-4 
 24-7 
 20-9 
 
 55-90 
 
 #3 
 
 V 
 
 p 
 
 I 
 
 r 
 
 o 
 
 End. 
 
 43-0 
 
 
 
 
 
 _ 
 
 TABLE VII. 
 MAGNETIZING CURRENT 1-12. 
 
 L. 
 
 served. 
 
 & 
 
 Cor- 
 rected. 
 
 Cor- 
 rected. 
 
 r 2 . 
 
 1 
 r* 
 
 Qi'. 
 Calcu- 
 lated. 
 
 
 
 
 
 762-4 
 
 
 
 
 1 
 
 3-5 
 
 
 758 9 
 
 .... 
 
 .... 
 
 2-58 
 
 2 
 
 9-4 
 
 .... 
 
 749-5 
 
 .... 
 
 .... 
 
 8-29 
 
 3 
 
 15-4 
 
 
 734- 1 
 
 .... 
 
 
 15-78 
 
 4 
 5 
 
 6 
 7 
 8 
 9 
 10 
 11 
 12 
 13 
 14 
 15 
 16 
 17 
 18 ^ 
 19} 
 20 * 
 
 27-5 
 44-3 
 66-6 
 71-2 
 59-5 
 51-0 
 45-2 
 40-3 
 36-3 
 33-3 
 30-6 
 28-1 
 25-6 
 23-4 
 20-0 
 
 34-0 
 
 71-2 
 59-7 
 51-2 
 45-2 
 40-3 
 36-8 
 33-5 
 30-5 
 28-0 
 25-4 
 22-7 
 20-3 
 18-1 
 16-0 
 
 706-6 
 662-3 
 595-7 
 524-5 
 464'- 8 
 413-6 
 368-4 
 328-1 
 291-3 
 257-8 
 227-3 
 199-3 
 173-9 
 151-2 
 130-2 
 112-8 
 96-8 
 
 0239 
 0200 
 0162 
 0141 
 0120 
 0107 
 0110 
 0116 
 0118 
 0140 
 0147 
 0161 
 0180 
 
 41-8 
 50-0 
 61-7 
 70-9 
 83-3 
 93-5 
 90-9 
 86-2 
 84-7 
 71-4 
 68-0 
 62-1 
 55-6 
 
 26-70 
 43-36 
 69-37 
 
 if 
 
 
 
 it 
 I 
 
 r 
 
 o 
 
 J 
 
 End. 
 
 
 
 
 
 
 
108 HENEY A. ROWLAND 
 
 points approaches the maximum of magnetization, a increases in value 
 
 as we pass down the bar; and having reached its maximum at L= 11 
 nearly, it decreases. These Tables, then, show in the most striking 
 manner the effect of the variation of the magnetic permeability of iron 
 upon the distribution of magnetism. 
 
 It is evident that these Tables also give the data for obtaining the 
 relative values of R' at different parts of the bar; but the results thus 
 obtained are conflicting, and will need further experiment to obtain 
 accurate results. Where such a small magnetizing force is used as in 
 Table V it is almost impossible to attain accuracy ; and allowance should 
 be made for this in deducing results from it. The greatest liability to 
 error is of course where the magnetization is small; for any small re- 
 sidual magnetism which the bar may contain will be more apparent 
 here although great care was taken to remove all residual magnetism 
 before use. Besides this there are many other disturbances from which 
 the higher magnetizing powers are free. 
 
 If we accept Green's formula as correct, these observations give us data 
 for determining the magnetizing-f unction of iron in a unique manner, for 
 nearly all other methods depend on absolute measurements of some 
 kind. Thus the least value of r z in Table IV for a rod -19 inch diam- 
 eter is -0142, which gives p= -01132, which in Green's formula (equa- 
 tion 8) gives //=3388 for the greatest permeability of this iron; and 
 this is as nearly right as we can judge for this kind of iron. It is to be 
 noted that Green's formula has been found for the portion of the bar 
 covered by the helix; but, as seen from my formulse, it will approxi- 
 mately apply to all portions, though it would be better to find a new 
 formula for each case. 
 
 We shall, toward the last, resume this subject again; and so will leave 
 it for the present. 
 
 The results which I have now given, and indeed all the results of this 
 paper, have been deduced not only from the observations which I pub- 
 lish, but from very many others; so that my Tables may be considered 
 to represent the average of a very extended series of researches, though 
 they are not really so. 
 
 V. 
 
 Let us now consider the case of that portion of the bar which is 
 covered by the helix. First of all, when the helix is symmetrically 
 placed on the rod, equations (5) and (6) will apply. As Q" is the 
 
STUDIES ox MAGNETIC DISTRIBUTION 
 
 109 
 
 quantity which is usually taken to represent the distribution of mag- 
 netism, being nearly proportional to the "surface-density" of mag- 
 netism, I shall principally discuss it. 
 
 In the first place, then, this equation (5) shows that the distribution 
 of magnetism in a very elongated electromagnet, and indeed in a steel 
 magnet, does not change when pieces of soft iron bars of the same 
 diameter as the magnet are placed against the poles, provided that equal 
 pieces are applied to both ends; otherwise there is a change. This result 
 would be modified by taking into account the variation of the permea- 
 bility, &c. 
 
 Let us first consider the case where the rod projects out of the end 
 of the helix, as in Tables V, VI, and VII. By giving proper values to 
 the constants, we obtain the results given in the last column of the 
 
 TABLE VIII. 
 
 
 Strength of magnetizing current. 
 
 
 108. 
 
 194. 
 
 378. 
 
 600. 
 
 
 
 1 
 
 2 
 
 !2-7 
 2-4 
 
 3-2 
 
 2-7 
 
 7 
 9 
 9 
 
 6 
 6 
 
 8 
 
 
 3-3 
 
 3-9 
 
 1-7 
 
 8 
 
 
 4-0 
 
 6-0 
 
 4-0 
 
 3-2 
 
 6 
 
 5-7 
 
 8-7 
 
 9-3 
 
 14-7 
 
 Tables. The agreement with observation is in most cases very perfect. 
 We also see the same variation of r that we before noticed in the rest of 
 the curves, and we see that it is in just the direction theory would 
 indicate from the change of p. 
 
 In these Tables we come to a very important subject, and one to 
 which I called attention some years back namely, the change in the 
 distribution when the magnetizing force varies, and which is due to change 
 of permeability. The following Tables and figures show this extremely 
 well, and are from very long rods with a helix a foot long at their 
 centre, as in the last three Tables. The bar in both these Tables was 
 19 inch in diameter and 5 feet long. The zero-point was at the centre 
 of the bar and of the helix. The Tables give values of Q' e for the 
 magnetizing forces which appear at the head of each column, and which 
 are the tangents of the angles of deflection of the needles of a tangent- 
 galvanometer. Table VIII only gives the part covered by the helix. 
 Both Tables are from the mean of both ends of the bar. 
 
110 
 
 HENRY A. EOWLAND 
 
 These experiments show in the most positive manner the effect we 
 are considering; and we are impressed by them with the great compli- 
 cation introduced into magnetic distribution by the variable character 
 of magnetic permeability. 
 
 In Fig. 3 I have represented the distribution on half the bar, as given 
 in Table IX, the other half being of course similar. Here the greatest 
 
 TABLE IX. 
 
 X. 
 
 C. 
 
 257. 
 
 B. 
 363. 
 
 A. 
 1-303. 
 
 I) 
 
 2-5 
 
 3-1 
 
 1-1 
 1-3 
 
 ii 
 
 7-2 
 
 4-1 
 5-9 
 
 2-1 
 4-0 
 
 
 6-1 
 
 8-2 
 
 9-6 
 
 
 7-7 
 
 10-9 
 
 18-6 
 
 6 
 
 7-9 
 
 11-5 
 
 21-3 
 
 7 
 
 6-5 
 
 9-0 
 
 16-8 
 
 10 
 12 
 15 
 18 
 30 
 
 10-0 
 6-2 
 5-0 
 2-0 
 2-0 
 
 15-0 
 10-9 
 9-8 
 4-7 
 3-6 
 
 27-4 
 20-9 
 21-5 
 14-8 
 16-5 
 
 5 10 15 20 
 
 FIG. 3. Plot of Table IX, showing surface-density for different values of the 
 
 magnetizing force. 
 
 change is observed in the part covered by the helix, though there is 
 also a great change in the other part. These Tables show that, as 
 the magnetization of the bars increases, at least beyond a certain point, 
 the curves on the part covered by the helix increase in steepness; and 
 the figure even shows that near the middle of the helix an increase of 
 magnetizing force may cause the surface-density to decrease; and Table 
 VIII shows this even better. Should we calculate Q", however, we 
 should always find it to increase with the magnetizing force in all cases. 
 These effects can be shown also in the case where the bar does not 
 
STUDIES ON MAGNETIC DISTRIBUTION 
 
 111 
 
 extend beyond the helix, but not nearly so well as in this case, seeing 
 that here Q" can obtain a greater value. 
 
 Assuming that /u is variable, the formula indicates the same change 
 that we observe; for as Q" increases from zero upwards, ft will first 
 increase and then decrease ; so that as we increase the magnetizing force 
 from zero upwards, the curve should first decrease in steepness and 
 then increase indefinitely in steepness. In these Tables the decrease 
 of steepness is not very apparent, because the magnetization is always 
 too great; and indeed on this account it is difficult to show it; but in 
 Tables V, VI, and VII this action is shown to some extent by the 
 
 TABLE x. 
 
 x and L. 
 
 A. 
 245. 
 
 B. 
 360. 
 
 C. 
 
 600. 
 
 D. 
 1-09. 
 
 
 
 + 17-6 
 
 + 29-4 
 
 + 52-0 
 
 + 108-7 
 
 
 + 9-6 
 
 + 16-8 
 
 + 31-5 
 
 + 60-1 
 
 
 + 7-4 
 
 + 13-1 
 
 + 24-3 
 
 + 45-8 
 
 3 
 
 + 5-4 
 
 + 9-8 
 
 + 19-1 
 
 + 34-1 
 
 
 + 3-4 
 
 + 7-2 
 
 + 14-7 
 
 + 22-8 
 
 5 
 
 + 2-0 
 
 + 4-6 
 
 + 9-9 
 
 + 16-0 
 
 6 
 
 -f 0-6 
 
 + 2-4 
 
 + 5-4 
 
 + 9-6 
 
 7 
 
 0-8 
 
 + 0-3 
 
 + 1-2 
 
 + 0-6 
 
 
 1-8 
 
 1-6 
 
 2-1 
 
 0-3 
 
 9 
 1 f\ 
 
 30 
 
 3-6 
 
 6-6 
 
 8-8 
 
 10 
 
 5-0 
 
 6-3 
 
 8-6 
 
 15-6 
 
 11 
 
 7-4 
 
 10-0 
 
 16-4 
 
 27-1 
 
 12 
 
 8-4 
 
 10-0 
 
 16-9 
 
 26-5 
 
 13 
 
 6-0 
 
 7-9 
 
 14-5 
 
 22-6 
 
 14 
 
 5-2 
 
 -7-0 
 
 12-5 
 
 21-0 
 
 15 
 
 ~i a 
 
 
 5-3 
 
 11-9 
 
 19-0 
 
 16 
 
 
 9-4 
 
 19-1 
 
 31-2 
 
 18 
 
 OA 
 
 
 5-3 
 
 15-2 
 
 
 20 
 
 
 6-5 
 
 19-3 
 
 
 24 
 
 Ort 
 
 
 5-6 
 
 6-0 
 
 
 OO 
 
 
 _ 0-7 
 
 1-2 
 
 
 48 
 
 
 
 
 
 values of r in the formulae. The change of distribution with the helix 
 arranged in this way at the centre of the bar is greater than in almost 
 every other case, because the magnetism of the bar, Q", can change 
 greatly throughout the whole length of the helix, and thus the value 
 of r be changed, and so the distribution become different. 
 
 The next case of distribution which I shall consider is that of a very 
 long rod having a helix wound closely round it for some distance at 
 one end. 
 
 Table X is from a bar 9 feet long with a helix wound for one foot 
 along one end. The bar was -25 inch in diameter. All except the first 
 
112 
 
 HENRY A. KOWLAND 
 
 column is the sum of two results with the current in^ opposite direc- 
 tions, and after letting the bar stand for some time, as indeed was done 
 in nearly every case. The first column contains twice the quantities 
 observed, so as to compare with the others. The zero-point was at the 
 end of the bar covered by the helix. 
 
 The value of Q"^ between and 1 includes the lines of force passing 
 out at the end of the bar, and is therefore too large. 
 
 In Fig. 4 we have a plot of the results found for this bar. The 
 curves are such as we should expect from our theory, except for the 
 variations introduced by the causes which we have hitherto considered. 
 Thus the sharp rise in the curve when near the end of the bar has 
 already been explained in connection with Table III. A small portion 
 
 FIG. 4. Plot of Table X. 
 
 of it, however, is due to those lines of induction which pass out through 
 the end section of the bar; and in future experiments these should be 
 estimated and allowed for.* 
 
 To estimate the shape of the curve theoretically in this case, let us 
 take equation (4) once more, and in it make s'=oo and s" = \/TZR', 
 which will make it apply to this case. We shall then have A' = 1, 
 and A" =o>, whence for the positive part of Q' f ' we have 
 
 2R'r l 
 and for the negative part 
 
 (1 + e* 
 
 _ -rxN . 
 
 8 When considering surface-density, we should also allow for the direct action of 
 the helix, though this is always found too small to be worth taking into account 
 except in very accurate experiments. 
 
STUDIES ox MAGNETIC DISTRIBUTION 
 therefore the real value is 
 
 Q,, _ &AL f ( Z _ b} , b _ o\ , f -rx\ . 
 
 U< ~ 2R'r C 
 And if x is reckoned from the end of the rod, we have 
 
 113 
 
 (10) 
 
 When x = 0, this becomes 
 
 and when x = b, it becomes 
 
 the ratio of which is 
 
 and this is the ratio of the values of Q" at the ends of the helix. 
 When & is 12 inches, as in this case, we get the following values of this 
 ratio : 
 
 r 
 
 05. 
 
 1. 
 
 15. 
 
 20. 
 
 30. 
 
 00. 
 
 -*(-*-!) = 
 2 
 
 2256 
 4-43 
 
 3494 
 2-86 
 
 4173 
 2-40 
 
 4546 
 2-20 
 
 4863 
 2-06 
 
 500 
 2-00 
 
 e-'-* 1 
 
 To compare this with our experiments, let us plot Table X once more, 
 rejecting, however, the end observations and completing the curve by 
 the eye, thus getting rid of the error introduced at this point. We then 
 find for this ratio, according to the different curves, 
 
 B. C. D. 
 
 2-1 2-3 3-2 
 
 It is seen that these are all above the limit 2, as they should be 
 though it is possible that it may fall below in some cases, owing to the 
 variation of the permeability. As the magnetization increases, the 
 values of the above ratio show that r decreases, as we should expect it 
 to do from the variation of /*. 
 
 To find the neutral point in this case, we must have in formula (10) 
 
114 
 
 HENRY A. EOWLAND 
 
 where x is the distance of the neutral point from the end. Making 
 b = 12, we have from this : 
 
 r= 
 x= 
 
 05. 
 
 10. 
 
 15. 
 
 20. 
 
 30. 
 
 00 . 
 
 10-1 
 
 8-96 
 
 8-31 
 
 7-89 
 
 7-39 
 
 6-00 
 
 By experiment we find that the neutral point is, in all the cases we 
 have given in Table X, between 7-5 and 8-1 inches, which are quite 
 near the points indicated by theory for the proper values of r, though 
 we might expect curve D to pass through the point x = 9, except for 
 the disturbing causes we have all along considered. 
 
 Our formulae, then, express the general facts of the distribution in 
 this case with considerable accuracy. 
 
 These experiments and calculations show the change in distribution 
 in an electromagnet when we place a piece of iron against one pole only. 
 In an ordinary straight electromagnet the neutral point is at the 
 centre. When a paramagnetic substance is placed against or near one 
 end, the neutral point moves toward it; but if the substance is diamag- 
 netic it moves from it. 
 
 The same thing will happen, though in a less degree, in the case of a 
 steel magnet; so that its neutral point depends on external conditions 
 as well as on internal. 
 
 We now come to practically the most interesting case of distribution, 
 namely that of a straight bar magnetized longitudinally either by a 
 helix around it, or by placing it in a magnetic field parallel to the lines 
 of force; we shall also see that this is the case of a steel magnet mag- 
 netized permanently. This case is the one considered by Biot (Traite 
 de PJiys., tome iii, p. 77) and Green (Mathematical Papers of the late 
 George Green, p. Ill, or Maxwell's ' Treatise/ art. 439), though they 
 apply their formula? more particularly to the case of steel magnets. 
 Biot obtained his formula from the analogy of the magnet to a Zamboni 
 pile or a tourmaline electrified by heat. Green obtained his for the 
 case of a very long rod placed in a magnetic field parallel to the lines 
 of force, and, in obtaining it, used a series of mathematical approxima- 
 tions whose physical meaning it is almost impossible to follow. Prof. 
 Maxwell has criticised his method in the following terms (' Treatise/ 
 art. 439) : " Though some of the steps of this investigation are not 
 rigorous, it is probable that the result represents roughly the actual 
 magnetization in this most important case." From the theory which 
 
STUDIES ON MAGNETIC DISTKIBUTION 115 
 
 I have given in the first part of this paper we can deduce the physical 
 meaning of Green's approximations; and these are included in the 
 hypotheses there given, seeing that, when my formula is applied to the 
 special case considered by Green, it agrees with it where the permea- 
 bility of the material is great. My formula, however, is far more gen- 
 eral than Green's. 
 
 It is to Green that we owe the important remark that the distribu- 
 tion in a steel magnet may be nearly represented by the same formula 
 that applies to electromagnets. 
 
 As Green uses what is known as the surface-density of magnetization, 
 let us first see how this quantity compares with those I have used. 
 
 Suppose that a long thin steel wire is so magnetized in the direction 
 of its length that when broken up the pieces will have the same mag- 
 netic moment. While the rod is together, if we calculate its effect on 
 exterior bodies, we shall see that the ends are the only portions which 
 seem to act. Hence we may mathematically consider the whole action 
 of the rod to be due to the distribution of an imaginary magnetic fluid 
 over the ends of the rod. As any case of magnetism can be represented 
 by a proper combination of these rods, we see that all cases of this sort 
 can be calculated on the supposition of there being two magnetic fluids 
 distributed over the surfaces of the bodies, a unit quantity of which 
 will repel another unit of like nature at a unit's distance with a unit of 
 force. The surface-density at any point will then be the quantity of 
 this fluid on a unit surface at the given point; and the linear density 
 along a rod will be the quantity along a unit of length, supposing the 
 density the same as at the given point. 
 
 Where we use induced currents to measure magnetism we measure 
 the number of lines of force, or rather induction, cut by the wire, and 
 the natural unit used is the number of lines of a unit field which will 
 pass through a unit surface placed perpendicular to the lines of force., 
 The unit pole produces a unit field at a unit's distance; hence the num- 
 ber of lines of force coming from the unit pole is 4 x, and the linear 
 density is 
 
 ' = & ....... < H > 
 
 and the surface-density 
 
 These really apply only to steel magnets ; but as in the case of electro- 
 magnets the action of the helix is very small compared with that of the 
 
116 HENKY A. ROWLAND 
 
 iron, especially when it is very long and the iron soft, 9 we can apply 
 these to the cases we consider. 
 
 Transforming Green's formula into my notation, it gives 
 
 (13) 
 
 in which < is Neumann's coefficient of magnetization by induction, and 
 is equal to 
 
 This equation then gives 
 
 c f 
 
 r(/;.-i) ~- , .... (U) 
 
 Equation (5) can be approximately adapted to this case by making 
 s' oo , which is equivalent to neglecting those lines of force which 
 pass out of the end section of the bar. This gives A' = 1 : hence 
 
 2 / 1 
 Now we have found (equation 7) that r -=- J nearly; and 
 
 this in Green's formula (equation 14) gives 
 
 which is identical with my own when JJL is large, as it always is in the 
 case of iron, nickel, or cobalt at ordinary temperatures. 
 
 When x is measured from the centre of the bar, my equation becomes 
 
 (17) 
 
 The constant part of Biot's formula is not the same as this; but for any 
 given case it will give the same distribution. 
 
 Both Biot and Green have compared their formulae with Coulomb's 
 experiments, and found them to represent the distribution quite well. 
 Hence it will not be necessary to consider the case of steel magnets very 
 extensively, though I will give a few results for these further on. 
 
 9 I take this occasion to correct an error in Jenkin's 'Textbook of Electricity,' 
 where it is stated that by the introduction of the iron bar into the helix, the num- 
 ber of lines of force is increased 32 times. The number should have been from a 
 quite small number for a short thick bar and hard iron to nearly 6000 for a long 
 thin bar and softest iron. 
 
STUDIES ON MAGNETIC DISTRIBUTION 
 
 117 
 
 At present let us take the case of electromagnets. 
 
 For observing the effect of the permeability, I took two wires 12-8 
 inches long and -19 inch in diameter, one being of ordinary iron and 
 the other of Stubs' steel of the same temper as when purchased. These 
 were wound uniformly from end to end with one layer of quite fine 
 wire, making 600 turns in that distance. 
 
 In finding / from Q" f) the latter was divided by 4~JL, except at the 
 end, where the end-section was included with JL in the proper manner. 
 x was measured from the end of the bar in inches. 
 
 The observations in Table XI are the mean of four observations 
 made on both ends of the bar and with the current in both directions. 
 
 TABLE XI. 
 IKON ELECTROMAGNET. 
 
 x = distance 
 from end. 
 
 I 
 
 Q- 4irA. 
 
 Observed. . Observed. 
 
 4irA. 
 
 Computed. 
 
 Error. 
 
 
 
 22-5 41-1 
 
 33-9 
 
 7-2 
 
 } 
 
 12-6 25-1 
 
 26-9 
 
 ' +1-8 
 
 1 
 
 19-3 19-3 
 
 18-9 
 
 0-4 
 
 
 12-0 12-0 
 
 11-7 
 
 -3 
 
 
 6-6 6-6 
 
 7-1 
 
 + -5 
 
 4 
 
 3-9 3-9 
 
 4-0 
 
 + -1 
 
 5 
 
 6 
 
 2-9 2-9 
 
 1.7 
 
 1-2 
 
 4jr2. = 42 
 
 The agreement with the formula in this Table is quite good; but we 
 still observe the excess of observation over the formula at the end, as 
 we have done all along. Here, for the first time, we see the error 
 introduced by the method of experiment which I have before referred 
 to (p. 98) in the apparently small value of 4;rA at x= -75. 
 
 On trying the steel bar, I came across a curious fact, which, how- 
 ever. I have since found has been noticed by others. It is, that when 
 an iron or steel bar has been magnetized for a long time in one direction 
 and is then demagnetized, it is easier to magnetize it again in the same 
 direction than in the opposite direction. The rod which I used in this 
 experiment had been used as a permanent magnet for about a month, 
 but was demagnetized before use. From this rod five cases of distribu- 
 tion were observed: first, when the bar was used as an electromagnet 
 with the magnetization in the same direction as the original mag- 
 
118 
 
 HENKY A. EOWLAND 
 
 netism; second, ditto with magnetization contrary to original mag- 
 netism; third, when used as a permanent magnet with magnetism the 
 same as the original magnetism; fourth, ditto with magnetism oppo- 
 site; and fifth, same as third, but curve taken after several days. The 
 permanent magnetism was given by the current. 
 
 The observations in Tables XI and XII can be compared together, 
 the quantities being expressed in the same unknown arbitrary unit. 
 It is to be noted that the bars in Tables XI and XII were subjected to 
 the same magnetizing force. 
 
 TABLE XII. 
 
 STUBS' STEEL. 
 
 
 Electromagnet. 
 
 Permanent Magnet. 
 
 X. 
 
 Magnetism 
 same as 
 original. 
 
 Magnetism 
 opp site to 
 original. 
 
 Magnetism 
 same as 
 original. 
 
 Magnetism 
 opposite to 
 original. 
 
 Same as third, 
 after three or 
 four days. 
 
 
 Qe- 
 
 4irA. 
 
 Qe- 
 
 47TA. 
 
 Qe- 
 
 4irA. 
 
 Qe- 
 
 4rrA. 
 
 Qe- 
 
 4irA. 
 
 
 i 
 
 23-3 
 11-5 
 
 42-5 
 23-0 
 
 15-9 
 
 7-7 
 
 29-0 
 15-4 
 
 I 14-4 
 
 13-7 
 
 4-8 
 
 4-6 
 
 12-8 
 
 12-2 
 
 H 
 
 8-2 
 6-1 
 
 16-4 
 12-2 
 
 5-9 
 4-3 
 
 11-8 
 8-6 
 
 I 8-2 
 
 8-2 
 
 4-0 
 
 4-0 
 
 7-3 
 
 7-3 
 
 
 7-4 
 
 7-4 
 
 5-5 
 
 5-5 
 
 5-3 
 
 5-3 
 
 2-9 
 
 2-9 
 
 4-8 
 
 4-8 
 
 3 
 
 8-6 
 
 3-6 
 
 2-7 
 
 2-5 
 
 3-0 
 
 3-0 
 
 1-6 
 
 1-6 
 
 2-9 
 
 2-9 
 
 4 
 6 
 
 1-7 
 
 8 
 
 1-0 
 
 5 
 
 2-2 
 
 1-1 
 
 9 
 
 4 
 
 2-0 
 
 1-0 
 
 First of all, from these Tables and figures (p. 119) we notice the 
 change in distribution due to the quality of the substance; thus in Fig. 5 
 we see that the curves for steel are much more steep than that of iron, 
 and would thus give greater values to r in the formula a result to be 
 expected. We also observe in both figures the great change in distri- 
 bution due to the direction of magnetization. In the case of the elec- 
 tromagnet this amounts to little more than a change in scale; but in 
 the permanent magnet there is a real change of form in the curve. It 
 seems probable that this change of form would be done away with by 
 using a sufficient magnetizing power or magnetizing by application of 
 permanent magnets; for it is probable that the fall in the curve E is 
 due to the magnetizing force having been sufficient to change the 
 polarity completely at the centre, but only partially at the ends. 
 
 On comparing the distribution on electromagnets with that on perma- 
 nent magnets, we perceive that the curve is steeper toward the end in 
 
STUDIES ON MAGNETIC DISTRIBUTION 
 
 119 
 
 electromagnets than in permanent magnets. At first I thought it 
 might be due to the direct action of the helix, but on trial found that 
 the latter was almost inappreciable. I do not at present know the 
 explanation of it. 
 
 As before mentioned, Coulomb has made many experiments on the 
 distribution of magnetism on permanent magnets; and so I shall only 
 consider this subject briefly. I have already given one or two results 
 in Table XII. 
 
 654321 
 
 FIG. 5. Results from electromagnets. 
 
 A. Iron, from Table XI. 
 
 B. Steel, from Table XII, magnetized same as originally. 
 
 C. Steel, from Table XII, magnetized opposite to its original magnetism. 
 
 6 S 4 3 2 1 O 
 
 FIG. 6. Results from steel permanent magnets. 
 
 D. Magnetized in its original direction, Table XII. 
 
 E. Magnetized opposite to its original direction, Table XII. 
 Scale four times that of Fig. 5. 
 
 The following Tables were taken from two exactly similar Stubs' 
 steel rods not hardened, one of which was subsequently used in the 
 experiments of Table XII. They were 12-8 inches long and -19 inch 
 in diameter. 
 
 The coincidence of these observations with the formula is very re- 
 
120 
 
 HENRY A. ROWLAND 
 
 markable; but still we see a little tendency in the end observation to 
 rise above the value given by the formula. 
 In equation (7), and also from Green's formula, we have seen that 
 
 * T 
 
 for a given quality and temper of steel p = r - is a constant. From 
 
 to 
 
 Coulomb's experiments on a steel bar -176 inch in diameter (whose 
 quality and temper is unknown, though it was probably hardened) Green 
 has calculated the value of this constant, and obtained -05482, which 
 was found from the French inch as the unit of length, but which is 
 constant for all systems. From Tables XIII and XIV we find the value 
 
 TABLE XIII. 
 
 X. 
 
 Q<- 
 
 Observed. 
 
 47TA. 
 
 Observed. 
 
 47TA. 
 
 Computed. 
 
 Error. 
 
 
 1-28 
 2-56 
 3-84 
 5-12 
 6-40 
 
 46-6 
 23-8 
 12-6 
 7-2 
 2-3 
 
 34-9 
 18-6 
 9-8 
 5-6 
 
 1-8 
 
 34-26 
 18-60 
 9-88 
 4-77 
 1-41 
 
 -6 
 
 
 + -1 
 8 
 4 
 
 47 r ;i=-117<10' 203(& - a:) -10' 203!t ). 
 
 TABLE XIV. 
 
 X. 
 
 Qe- 
 
 Observed. 
 
 Observed. 
 
 4irA. 
 
 Computed. 
 
 Error. 
 
 
 
 1 .98 
 
 42-6 
 
 31-9 
 
 30-74 
 
 1-2 
 
 2-56 
 
 21-4 
 
 16-7 
 
 16-72 
 
 
 
 3- 84 
 
 10-9 
 
 8-5 
 
 8-86 
 
 + -4 
 
 5-12 
 
 5-4 
 
 4-2 
 
 4-28 
 
 + -1 
 
 6-40 
 
 1-7 
 
 1-33 
 
 1-27 
 
 -1 
 
 47rA=-105(10' 203(6 - z) -10' !i031 ). 
 
 of r to be -4674, whence ^= -04440 for steel not hardened. As the 
 
 steel becomes harder this quantity increases, and can probably reach 
 about twice this for very hard steel. 
 
 To show the effect of hardening. I broke the bar used in Table XIV 
 at the centre, thus producing two bars 6-4 inches long. One of these 
 halves was hardened till it could scarcely be scratched by a file ; but the 
 other half was left unaltered. The following Table gives the distribu- 
 tion, using the same unit as that of Tables XIII and XIV. The bars 
 were so short that the results can hardly be relied on ; but they will at 
 least suffice to show the change. 
 
STUDIES ON MAGNETIC DISTKIBUTION 
 
 121 
 
 In Fig. 7 I have attempted to give the curve of distribution from 
 Table XV, and have made the curves coincide with observation as nearly 
 as possible, making a small allowance, however, for the errors intro- 
 duced by the shortness of the bar. It is seen that the effect of harden- 
 ing in a bar of these dimensions is to increase the quantity of magnetism, 
 but especially that near the end. Had the bar been very long, no increase 
 
 TABLE XV. 
 
 X. 
 
 Soft Steel, A. 
 
 Hard Steel, B. 
 
 Or 
 
 4.A. 
 
 Qe- 
 
 47TA. 
 
 
 64 
 
 1-28 
 1-92 
 3-20 
 
 20-4 
 9-8 
 6-0 
 
 3-8 
 
 29-1 
 15-3 
 9-4 
 3-0 
 
 47-7 
 13-9 
 7-0 
 2-6 
 
 68-1 
 21-7 
 11-0 
 2-0 
 
 -Results from permanent magnets. 
 
 A. Soft steel. 
 
 B. Hard steel. 
 
 in the total quantity of magnetism would have taken place; but the distri- 
 bution would have been changed. From this we deduce the important 
 fact that hardening is most useful for short magnets. And it would seem 
 that almost the only use in hardening magnets at all is to concentrate the 
 magnetism and to reduce the weight. Indeed I have made magnets from 
 iron wire whose magnetization at the central section was just as intense 
 as in a steel wire of the same size; but to all appearance it was less 
 
122 HENRY A. KOWLAND 
 
 strongly magnetized than the steel, because the magnetism was more 
 diffused; and as the magnetism was not distributed so nearly at the end 
 as in the steel, its magnetic moment and time of vibration were less. 
 
 It is for these reasons that many makers of surveyors' compasses find 
 it unnecessary to harden the needles, seeing these are long and thin. 
 
 We might deduce all these facts from the formulae on the assumption 
 that r is greater the harder the iron or steel. 
 
 Having now considered briefly the distribution on electromagnets 
 and steel magnets, and found that the formulae represent it in a general 
 way, we may now use them for solving a few questions that we desire 
 to solve, though only in an approximate manner. 
 
 VI. 
 
 M. Jamin, in his recent experiments on magnetic distribution, has 
 obtained some very interesting results, although I have shown his 
 method to be very defective. In his experiments on iron bars mag- 
 netized at one end, he finds the formula s rl to apply to long ones as I 
 have done. Now it might be argued that as the two methods apparently 
 give the same result, they must be equally correct. But let us assume 
 that the attraction of his piece of soft iron F varied as some unknown 
 power n of the surface-density d. Then we find 
 
 F=Ce nrL , 
 
 which shows that the attractive force or any power of that force can 
 be represented by a logarithmic curve, though not by the same one. 
 Hence the error introduced by M. Jamin's method is insidious and not 
 easily detected, though it is none the less hurtful and misleading, but 
 rather the more so. 
 
 However, his results with respect to what he calls the normal mag- 
 net 10 are to some extent independent of these errors ; and we may now 
 consider .them. 
 
 Thus, in explaining the effect of placing hardened steel plates on 
 one another, he says, " Quand on superpose deux lames aimante'es 
 pareilles, les courbes qui represontent les valeurs de F [the attractive 
 force on the piece of soft iron] s'e!6vent, parce que le magnetisme quitte 
 les faces que 1'on met en contact pour se refugier sur les parties ex- 
 te"rieures. En meme temps, les deux courbes se rapprochent 1'une dc 
 1'autre et du milieu de 1'aimant. Get effet augmente avec une troisieme 
 
 10 <On the Theory of the Normal Magnets,' Comptes Rendus, March 31, 1873; 
 translated in Phil. Mag., June, 1873. 
 
STUDIES ON MAGNETIC DISTRIBUTION 123 
 
 lame et avec une quatrieme. Finalement les deux courbes se joignent 
 au milieu." 
 
 In applying the formula to this case of a compound magnet, we have 
 only to remark that when the bars lie closely together they are theoret- 
 ically the same as a solid magnet of the same section, but are practically 
 found to be stronger, because thin bars can be tempered more uniformly 
 hard than thick ones. The addition of the bars to each other is similar, 
 then, to an increase in the area of the rod, and should produce nearly 
 the same effect on a rod of rectangular section as the increase of 
 
 3 
 
 diameter in a rod of circular section. Now the quantity p = ~* is 
 
 m 
 
 nearly constant in these rods for the same quality of steel, whence r 
 decreases as d increases; and this in equation (17) shows that as the 
 diameter is increased, the length being constant, the curves become 
 less and less steep, until they finally become straight lines. This is 
 exactly the meaning of M. Jamin's remark. 
 
 Where the ratio of the diameter to the length is small, the curves of 
 distribution are apparently separated from each other and are given by 
 the equation 
 
 which is not dependent on the length of the rod This is exactly the 
 result found by Coulomb (Biot's Physique, vol. iii, pp. 74, 75). M. 
 Jamin has also remarked this. He states that as he increases the num- 
 ber of plates the curves approach each other and finally unite; this he 
 calls the " normal magnet ; " and he supposes it to be the magnet of 
 greatest power in proportion to its weight. "From this moment," 
 says he, "the combination is at its maximum." The normal magnet, 
 as thus defined, is very indefinite, as M. Jamin himself admits. 
 
 By our equations we can find the condition for a maximum, and can 
 give the greatest values to the following, supposing the weight of the 
 bar to be a fixed quantity in the first three. 
 
 1st. The magnetic moment. 
 
 2nd. The attractive force at the end. 
 
 3rd. The total number of lines of magnetic force passing from the 
 bar. 
 
 4th. The magnetic moment, the length being constant and diameter 
 variable. 
 
 Either of these may be regarded as a measure of the power of the 
 bar, according to the view we take. The magnetic moment of a bar is 
 easily found to be 
 
124 HENRY A. ROWLAND 
 
 M 4rr 2 fl' 1 2~rl4-c-rt h ( 19 ) 
 
 and if ? is the weight of a unit of volume of the steel and W is the 
 weight of the magnet, we have finally 
 
 M- -* 
 
 This only attains a maximum when - oo , or the rod is infinitely 
 
 long compared with its diameter. 
 
 The second case is rather indefinite, seeing it will depend upon 
 whether the body attracted is large or small. When it is small, we 
 require to make the surface-density a maximum, the weight being con- 
 stant. We find 
 
 which attains a maximum as before when -, oo When the attracted 
 
 CL 
 
 body is large, the attraction will depend more nearly upon the linear 
 density, 
 
 
 which is a maximum when - 7 - . 
 
 a p 
 
 For the third case we have the value of Q" at the centre of the bar 
 from equation (6), 
 
 The condition for a maximum gives in this case 
 
 5 _ 1-65 
 d~~ p 
 
 For the last case, in which the magnetic moment for a given length 
 is to be made a maximum, we find 
 
 b_-l 
 d~ p' 
 
 This last result is useful in preparing magnets for determining the 
 
STUDIES ON MAGNETIC DISTRIBUTION 125 
 
 intensity of the earth's magnetism, and shows that the magnets should 
 be made short, thick, and hard for the best effect. 11 
 
 But for all ordinary purposes the results for the second and third 
 cases seem most important, and lead to nearly the same result; taking 
 the mean we find for the maximum magnet 
 
 fCtA\ 
 
 (24) 
 
 We see from all our results that the ratio of the length of a magnet 
 to its diameter in all cases is inversely as the constant p. This con- 
 stant increases with the hardness of the steel; and hence the harder the 
 steel the shorter we can make our magnets. It would seem from this 
 that the temper of a steel magnet should not be drawn at all, but the 
 hardest steel used, or at least that in which p was greatest. The only 
 disadvantage in using very hard steel seems to be the difficulty in 
 imparting the magnetism at first; and this may have led to the practice 
 of drawing the temper; but now, when we have such powerful electro- 
 magnets, it seems as if magnets might be made shorter, thicker, and 
 harder than is the custom. With the relative dimensions of magnets 
 now used, however, hardening might be of little value. 
 
 We can also see from all these facts, that if we make a compound 
 magnet of hardened steel plates there will be an advantage in filing 
 more of them together, thus making a thicker magnet than when they 
 are softer. We also observe that as we pile them up the distribution 
 changes in just the way indicated by M. Jamin, the curve becoming 
 less and less steep. 
 
 Substituting in the formula the value of p which we have found for 
 Stub's steel not hardened, but still so hard as to rapidly dull a file, we 
 find the best ratio of length to diameter to be 33-8 and for the same 
 steel hardened, about 17, though this last is only a rough approxima- 
 tion. This gives what M. Jamin has called the normal magnet. The 
 ratio should be less for a U-magnet than for a straight one. 
 
 For all magnets of the same kind of steel in which the ratio of 
 length to diameter is constant the relative distribution is the same; 
 and this is not only true for our approximate formula, but would be 
 found so for the exact one. 
 
 Thus for the " normal magnet " the distribution becomes 
 
 11 Weber recommends square bars eight times as long as they are broad, and tem- 
 pered very hard. (Taylor's Scientific Memoirs, vol. ii, p. 86.) 
 
126 
 
 HENEY A. ROWLAND 
 
 where C is a constant, and x is measured from the centre. The distri- 
 bution will then be as follows : 
 
 X _ 
 
 0. 
 
 1. 
 
 2. 
 
 3. 
 
 4. 
 
 5. 
 
 A 
 
 
 
 609 
 
 1-27 
 
 2-05 
 
 3-02 
 
 4-26 
 
 This distribution is not the same as that given by M. Jamin; but as 
 his method is so defective, and his " normal magnet " so indefinite, the 
 agreement is sufficiently near. 
 
 The surface-density at any point of a magnet is 
 
 d = 
 
 (25) 
 
 which, for the same kind of steel, is dependent only on ? and -3- 
 Hence in two similar magnets the surface-density is the same at similar 
 
 .1 .2 .A .4 .5 
 
 FIG. 8. Distribution on "normal magnet." 
 
 points, the linear density is proportional to the linear dimensions, the 
 surface integral of magnetic induction over half the magnet or across 
 the section is proportional to the surface dimensions of the magnets, 
 and the magnetic moments to the volumes of the magnets. The forces 
 at similar points with regard to the two magnets will then be the same. 
 All these remarks apply to soft iron under induction, provided the 
 inducing force is the same and hence include Sir William Thomson's 
 well-known law with regard to similar electromagnets; and they are 
 accurately true notwithstanding the approximate nature of the formula 
 from which they have here been deduced. 
 
 Our theory gives us the means of determining what effect the boring 
 of a hole through the centre of a magnet would have. In this case R' 
 
STUDIES ON MAGNETIC DISTRIBUTION 127 
 
 is not much affected, but R is increased. Where the magnet is used 
 merely to affect a compass-needle, we should then see that the hole 
 through the centre has little effect where the magnet is short and thick ; 
 but where it is long, the attraction on the compass-needle is much dimin- 
 ished. Where the magnet is of the U-form, and is to be used for 
 sustaining weights, the practice is detrimental, and the sustaining-power 
 is diminished in the same proportion as the sectional area of the magnet. 
 The only case that I know of where the hole through the centre is an 
 advantage, is that of the deflecting magnets for determining the inten- 
 sity of the earth's magnetism, which may be thus made lighter without 
 much diminishing their magnetic moment. 
 
 In conclusion, let me express my regret at the imperfection of the 
 theory given in this paper; for although the equations are more general 
 than any yet given, yet still they rest upon two quite incorrect hypoth- 
 eses; and so, although we have found these formula? of great use in 
 pursuing our studies on magnetic distribution, yet much remains to be 
 done. A nearer approximation to the true distribution could readily 
 be obtained; but the result would, without doubt, be very complicated, 
 and would not repay us for the trouble. 
 
 In this paper, as well as in all others which I have published on the 
 subject of magnetism, my object has not only been to bring forth new 
 'results, but also to illustrate Faraday's method of lines of magnetic 
 force, and to show how readily calculations can be made on this system. 
 For this reason many points have been developed at greater length than 
 would otherwise be desirable. 
 
12 
 
 ON THE MAGNETIC EFFECT OF ELECTEIC CONVECTION * 
 
 [American Journal of Science 13], XV, 30-38, 1878] 
 
 The experiments described in this paper were made with a view of 
 determining whether or not an electrified body in motion produces 
 magnetic effects. There seems to be no theoretical ground upon which 
 we can settle the question, seeing that the magnetic action of a con- 
 ducted electric current may be ascribed to some mutual action between 
 the conductor and the current. Hence an experiment is of value. Pro- 
 fessor Maxwell, in his ' Treatise on Electricity/ Art. 770, has computed 
 the magnetic action of a moving electrified surface, but that the action 
 exists has not yet been proved experimentally or theoretically. 
 
 The apparatus employed consisted of a vulcanite disc 21-1 centi- 
 metres in diameter and -5 centimetre thick which could be made to 
 revolve around a vertical axis with a velocity of 61- turns per second. 
 On either side of the disc at a distance of -6 cm. were fixed glass plates 
 having a diameter of 38-9 cm. and a hole in the centre of 7-8 cm. The 
 vulcanite disc was gilded on both sides and the glass plates had an 
 annular ring of gilt on one side, the outside and inside diameters being 
 24-0 cm. and 8-9 cm. respectively. The gilt sides could be turned 
 toward or from the revolving disc but were usually turned toward it so 
 that the problem might be calculated more readily and there should 
 be no uncertainty as to the electrification. The outside plates were 
 usually connected with the earth; and the inside disc with an electric 
 battery, by means of a point which approached within one-third of a 
 millimetre of the edge and turned toward it. As the edge was broad, 
 the point would not discharge unless there was a difference of potential 
 between it and the edge. Between the electric battery and the disc, 
 
 1 The experiments described were made in the laboratory of the Berlin University 
 through the kindness of Professor Helmholtz, to whose advice they are greatly in- 
 debted for their completeness. The idea of the experiment first occurred to me in 
 1868 and was recorded in a note book of that date. 
 
Ox THE MAGNETIC EFFECT OF ELECTRIC CONVECTION 129 
 
 a commutator was placed, so that the potential of the latter could be 
 made plus or minus at will. All parts of the apparatus were of non- 
 magnetic material. 
 
 Over the surface of the disc was suspended, from a bracket in the 
 wall, an extremely delicate astatic needle, protected from electric 
 action and currents of air by a brass tube. The two needles were 1-5 
 cm. long and their centres 17-98 cm. distant from each other. The 
 readings were by a telescope and scale. The opening in the tube for 
 observing the mirror was protected from electrical action by a metallic 
 cone, the mirror being at its vertex. So perfectly was this accom- 
 plished that no effect of electrical action was apparent either on charg- 
 ing the battery or reversing the electrification of the disc. The needles 
 were so far apart that any action of the disc would be many fold greater 
 on the lower needle than the upper. The direction of the needles was 
 that of the motion of the disc directly below them, that is, perpendicular 
 to the radius drawn from the axis to the needle. As the support of 
 the needle was the wall of the laboratory and the revolving disc was on a 
 table beneath it, the needle was reasonably free from vibration. 
 
 In the first experiments with this apparatus no effect was observed 
 other than a constant deflection which was reversed with the direction 
 of the motion. This was finally traced to the magnetism of rotation 
 of the axis and was afterward greatly reduced by turning down the 
 axis to -9 cm. diameter. On now rendering the needle more sensitive 
 and taking several other precautions a distinct effect was observed of 
 several millimetres on reversing the electrification and it was separated 
 from the effect of magnetism of rotation by keeping the motion con- 
 stant and reversing the electrification. As the effect of the magnetism 
 of rotation was several times that of the moving electricity, and the 
 needle was so extremely sensitive, numerical results were extremely 
 hard to be obtained, and it is only after weeks of trial that reasonably 
 accurate results have been obtained. But the qualitative effect, after 
 once being obtained, never failed. In hundreds of observations extend- 
 ing over many weeks, the needle always answered to a change of electri- 
 fication of the disc. Also on raising the potential above zero the action 
 was the reverse of that when it was lowered below. The swing of the 
 needle on reversing the electrification was about 10- or 15- millimetres 
 and therefore the point of equilibrium was altered 5 or 7| millimetres. 
 This quantity varied with the electrification, the velocity of motion, 
 the sensitiveness of the needle, etc. 
 9 
 
130 HENRY A. EOWLAND 
 
 The direction of the action may be thus defined. Calling the motion 
 of the disc -\- when it moved like the hands of a watch laid on the 
 table with its face up, we have the following, the needles being over 
 one side of the disc with the north pole pointing in the direction of 
 positive motion. The motion being -f> on electrifying the disc -)- the 
 north pole moved toward the axis, and on changing the electrification, 
 the north pole moved away from the axis. With motion and -(- 
 electrification, the north pole moved away from the axis, and with 
 electrification, it moved toward the axis. The direction is therefore 
 that in which we should expect it to be. 
 
 To prevent any suspicion of currents in the gilded surfaces, the 
 latter, in many experiments, were divided into small portions by radial 
 scratches, so that no tangential currents could take place without suffi- 
 cient difference of potential to produce sparks. But to be perfectly 
 certain, the gilded disc was replaced by a plane thin glass plate which 
 could be electrified by points on one side, a gilder induction plate at 
 zero potential being on the other. With this arrangement, effects in 
 the same direction as before were obtained, but smaller in quantity, 
 seeing that only one side of the plate could be electrified. 
 
 The inductor plates were now removed, leaving the disc perfectly 
 free, and the latter was once more gilded with a continuous gold sur- 
 face, having only an opening around the axis of 3-5 cm. The gilding of 
 the disc was connected with the axis and so was at a potential of zero. 
 On one side of the plate, two small inductors formed of pieces of tin- 
 foil on glass plates, were supported, having the disc between them. On 
 electrifying these, the disc at the points opposite them was electrified 
 by induction but there could be no electrification except at points near 
 the inductors. On now revolving the disc, if the inductors were very 
 small, the electricity would remain nearly at rest and the plate 
 would as it were revolve through it. Hence in this case we should 
 have conduction without motion of electricity, while in the first experi- 
 ment we had motion without conduction. I have used the term 
 " nearly at rest " in the above, for the following reasons. As the disc 
 revolves the electricity is being constantly conducted in the plate so as 
 to retain its position. Now the function which expresses the potential 
 producing these currents and its differential coefficients must be con- 
 tinuous throughout the disc, and so these currents must pervade the 
 whole disc. 
 
Ox THE MAGNETIC EFFECT OF ELECTRIC CONVECTION 131 
 
 To calculate these currents we have two ways. Either we can con- 
 sider the electricity at rest and the motion of the disc through it to 
 produce an electromotive force in the direction of motion and propor- 
 tional to the velocity of motion, to the electrification, and to the surface 
 resistance; or, as Professor Helmholtz has suggested, we can consider 
 the electricity to move with the disc and as it comes to the edge of the 
 inductor to he set free to return by conduction currents to the other 
 edge of the inductor so as to supply the loss there. The problem is 
 capable of solution in the case of a disc without a hole in the centre but 
 the results are too complicated to be of much use. Hence scratches 
 were made on the disc in concentric circles about -6 cm. apart by which 
 the radial component of the currents was destroyed and the problem 
 became easily calculable. 
 
 For, let the inductor cover -th part of the circumference of any 
 
 n 
 
 one of the conducting circles; then, if C is a constant, the current in 
 
 the circle outside the inductor will be +-, and inside the area of the 
 
 1 n 
 
 inductor C^ n ~ l \ On the latter is superposed the convection cur- 
 
 fi 
 
 rent equal to -\-C. Hence the motion of electricity throughout the 
 
 whole circle is - what it would have been had the inductor covered the 
 n 
 
 whole circle. 
 
 In one experiment n was about 8. By comparison with the other 
 experiments we know that had electric conduction alone produced effect 
 we should have observed at the telescope 5- mm. Had electric con- 
 vection alone produced magnetic effect we should have had -j- 5- 7 mm. 
 And if they both had effect it would have been -f- -7 mm., which is prac- 
 tically zero in the presence of so many disturbing causes. No effect 
 was discovered, or at least no certain effect, though every care was used. 
 Hence we may conclude with reasonable certainty that electricity pro- 
 duces nearly if not quite the same magnetic effect in the case of con- 
 vection as of conduction, provided the same quantity of electricity 
 passes a given point in the convection stream as in the conduction 
 stream. 
 
 The currents in the disc were actually detected by using inductors 
 covering half the plate and placing the needle over the uncovered por- 
 tion; but the effect was too small to be measured accurately. To prove 
 
132 HENRY A. KOWLAXD 
 
 this more thoroughly numerical results were attempted, and, after 
 weeks of labor, obtained. I give below the last results which, from 
 the precautions taken and the increase of experience, have the greatest 
 weight. 
 
 The magnetizing force of the disc was obtained from the deflection 
 of the astatic needle as follows. Turning the two needles with poles 
 in the same direction and observing the number n of vibrations, and 
 then turning them opposite and finding the number n' of vibrations in 
 that position, we shall find, when the lower needle is the strongest, 
 
 Y -p, w 2 n" 1 n' 2 A w n . 
 
 JL JL 5; jz = *. 72 77 ** I .... (1) 
 
 w 2 + n ' i? + n D 
 
 where X' and X are the forces on the upper and lower needle re- 
 spectively, A the deflection, D the distance of the scale and H the 
 horizontal component of the earth's magnetism. As X' and n' are very 
 small the first term is nearly X X'. The torsion of the silk fibre was 
 too small to affect the result, or at least was almost eliminated by the 
 method of experiment. 
 
 The electricity was in the first experiment distributed nearly uni- 
 formly over the disc with the exception of the opening in the centre 
 and the excess of distribution on the edge. The surface density on 
 either side was 
 
 V y 
 
 a* - 
 
 V - -V being the difference of potential between the disc and the 
 outside plates, /? the thickness of the disc and B the whole distance 
 apart of the outside plates. The excess on the edge was (Maxwell's 
 Electricity, Art. 196, Eq. 18), 
 
 *=*<?- ^ *** "*> ' < 3 > 
 
 where C is the radius of the disc. 
 
 We may calculate the magnetic effect on the supposition that, as in 
 the conducted current, the magnetizing force due to any element of 
 surface is proportional to the quantity of electricity passing that 
 element in a unit of time. The magnetic effect due to the uniform 
 distribution has the greatest effect. With an error of only a small 
 
Ox THE MAGNETIC EFFECT OF ELECTEIC CONVECTION 133 
 
 fraction of a per cent, we may consider the two sides of the disc to 
 coincide in the centre. Taking the origin of coordinates at the point 
 of the disc under the needle and the centre of the disc on the axis of X. 
 we find for both sides of the disc, the radial component of the force 
 parallel to the disc, 
 
 r c ~ f 
 J_ (C+b) J. 
 
 x)dxdy 
 
 (a 1 + a? + 
 
 f> - (b 
 
 where a is the distance of the needle from the disc and & that from 
 the axis; N is the number of revolutions of the disc per second and 
 v = 28,800,000,000 centimetres per second according to Maxwell's de- 
 termination. The above integral can be obtained exactly by elliptic 
 integrals, but as it introduces a great variety of complete and incom- 
 plete elliptic integrals of all three orders, we shall do best by expanding 
 as follows: 
 
 V 4-JW 7, faNff f . . A a >. -r.v 
 
 X= - P - (A! + A* + A 3 + &c.), ... (4) 
 
 A, = 2jfarc tan -=^ + arc tan ^-^ - a log, 4 , 
 \ a a ] JV 
 
 2sb + a2) loge 
 
 (5s 3 
 
 &c., &c., 
 where 
 
 -, , . 
 
 /it) 
 
 From this must be subtracted the effect of the opening in the centre, 
 for which the same formula will apply. 
 
 The magnetic action of the excess at the edge may be calculated on 
 the supposition that that excess is concentrated in a circle of a little 
 smaller diameter, C", than the disc; therefore, 
 
134 HEXEY A. EOWLAXD 
 
 where fc = ^-i^jL^, and F(Jc) and E(k) are complete elliptic 
 V c? + ( C? + 0) 
 
 integrals of the second and first orders respectively. 
 
 The determination of the potential was by means of the spark which 
 Thomson has experimented on in absolute measure. For sparks of 
 length I between two surfaces nearly plane, we have on the centimetre, 
 gram, second system, from Thomson's experiments, 
 
 V- V = 117-5 (1 + . 0135), 
 
 and for two balls of finite radius, we find, by considering the distribu- 
 tion on the two sheets of an hyperboloid of revolution, 
 
 V-V' = 117-5 (I + -0135) 
 
 where r is the ratio of the length of spark to diameter of balls and had 
 in these experiments a value of about 8. In this case 
 
 V V = 109-6 (I + -0135) . (6) 
 
 A battery of nine large jars, each 48- cm. high, contained the store 
 of electricity supplied to the disc, and the difference of potential was 
 determined before and after the experiment by charging a small jar and 
 testing its length of spark. Two determinations were made before and 
 two after each experiment, and the mean taken as representing the 
 potential during the experiment. 
 
 The velocity of the disc was kept constant by observing a governor. 
 The number of revolutions was the same, nearly, as determined by the 
 sizes of the pulleys or the sound of a Seebeck siren attached to the 
 axis of the disc; the secret of this agreement was that the driving cords 
 were well supplied with rosin. The number of revolutions was 61- per 
 second. 
 
 In such a delicate experiment, the disturbing causes, such as the 
 changes of the earth's magnetism, the changing temperature of the 
 room, &c., were so numerous that only on few days could numerical 
 results be obtained, and even then the accuracy could not be great. 
 The centimetre, gram, second system, was used. 
 
 First Series, a = 2-05, & = 9-08, w=-697, Z> = 110-, H -182 
 nearly, 5 = 1-68, /?=-50, (7 = 10-55, N 61-, v = 28,800,000,000-, 
 7Z ' =-0533, C" = 10. 
 
ON THE MAGNETIC EFFECT OF ELECTRIC CONVECTION 135 
 
 Direction of Electrifica- 
 motion. tion of disc. 
 
 Scale reading 
 in mm. 
 
 Deflection on 
 reversing 
 electriflcat'n 
 in mm. 
 
 Length of 
 spark. 
 
 - 
 
 
 
 99- 
 107-5 
 101-5 
 
 7-25 
 
 295 
 
 
 
 7 
 
 68-5 
 76-5 
 68-0 
 
 8-25 
 
 290 
 
 - 
 
 
 
 97- 
 91-5 
 100- 
 
 7-00 
 
 282 
 
 
 
 1 
 
 59- 
 65-5 
 58-5 
 
 6-75 
 
 265 
 
 - 
 
 i 
 
 92-5 
 85- 
 91-0 
 
 6-75 
 
 290 
 
 ' 
 
 
 
 52-5 
 57-5 
 51-5 
 
 5-50 
 
 285 
 
 + 
 
 
 
 82-0 
 76-0 
 81-7 
 
 5-85 
 
 285 
 
 
 
 1 
 
 36-5 
 43-0 
 36-5 
 
 6-50 
 
 275 
 
 - 
 
 
 
 68-0 
 61-0 
 68-0 
 
 7-00 
 
 290 
 
 
 
 
 
 27-5 
 33-5 
 26-5 
 
 6-50 
 
 288 
 
 Mean values. 
 
 6-735 
 
 2845 
 
 Hence 
 
 From equation (1), 
 
 X- -99X' =, 
 
 305700' 
 Bv calculation from the electrification we find 
 
 = 00000327. 
 
136 
 
 HENEY A. ROWLAND 
 1 
 
 X--992T 1 = ; 
 
 = 00000337. 
 
 296800- 
 
 The effect on the upper needle, X', was about Jg- of that on the 
 lower X. 
 
 Second Series. Everything the same as before except the following. 
 & = 7-65, n'=-Q525. 
 
 Direction of 
 motion. 
 
 Electrifica- 
 tion of disc. 
 
 Scale reading 
 in mm. 
 
 Deflection on 
 reversing 
 electriflcat'n 
 in mm. 
 
 Length of 
 spark. 
 
 
 + 
 
 172-5 
 
 
 
 + 
 
 
 
 165-5 
 
 7-0 
 
 300 
 
 
 + 
 
 172-5 
 
 
 
 
 + 
 
 120-0 
 
 
 
 
 
 + 
 
 127-5 
 121-5 
 
 7-5 
 
 295 
 
 
 
 
 129-0 
 
 
 
 
 
 
 163-5 
 
 
 
 + 
 
 + 
 
 170-5 
 163-0 
 
 7-25 
 
 297 
 
 
 + 
 
 170-5 
 
 
 
 
 + 
 
 118-0 
 
 
 
 
 
 + 
 
 127-0 
 120-0 
 
 8-25 
 
 270 
 
 
 
 
 127-5 
 
 
 
 Mean values. 
 
 7-50 
 
 2955 
 
 Hence for this case we have from equation (1), 
 
 1 
 
 315000- 
 
 And from the electrification, 
 
 T -QQ JT' 
 
 - 
 
 =00000317. 
 
 = -00000349 . 
 
 Third Series. Everything the same as in the first series, except 
 = 8-1, n' = -0521, D = 114. 
 
ON THE MAGNETIC EFFECT OF ELECTRIC CONVECTION 
 
 137 
 
 Direction of 
 motion. 
 
 Electrifica- 
 tion of disc. 
 
 Scale reading 
 in mm. 
 
 Deflection on 
 reversing 
 electrificat'n 
 in mm. 
 
 Length of 
 spark. 
 
 
 + 
 
 151-0 
 
 
 
 
 
 
 
 158-5 
 
 7.50 
 
 287 
 
 
 + 
 
 151-0 
 
 
 
 
 + 
 
 192-0 
 
 
 
 + 
 
 
 
 185-5 
 
 7-25 
 
 292. 
 
 
 + 
 
 193-5 
 
 
 
 
 
 
 157-5 
 
 
 
 
 
 + 
 
 148-5 
 157-5 
 
 8-25 
 
 295 
 
 
 + 
 
 150-0 
 
 
 
 
 
 
 185-0 
 
 
 
 + 
 
 + 
 
 192-5 
 185-5 
 
 7-75 
 
 302 
 
 
 + 
 
 193-5 
 
 
 
 
 
 
 151-0 
 
 
 
 
 
 -1- 
 
 143-5 
 
 7-25 
 
 287 
 
 
 
 
 150-5 
 
 
 
 Mean values. 
 
 7-60 
 
 2926 
 
 J = -380, 
 For this case from equation (1) 
 
 1 
 
 295000 
 
 and from the electrification 
 
 = -2926. 
 
 = -00000339 , 
 
 = -00000355 . 
 
 281500- 
 
 The error amounts to 3, 10 and 4 per cent respectively in the three 
 series. Had we taken Weber's value of v the agreement would have 
 been still nearer. Considering the difficulty of the experiment and 
 the many sources of error, we may consider the agreement very satis- 
 factory. The force measured is, we observe, about ^inr of the hori- 
 zontal force of the earth's magnetism. 
 
 The difference of readings with -f- and - - motion is due to the 
 magnetism of rotation of the brass axis. This action is eliminated 
 from the result. 
 
 It will be observed that this method gives a determination of v, the 
 ratio of the electromagnetic to the electrostatic system of units, and if 
 carried out on a large scale with perfect instruments might give good 
 results. The value v = 300,000,000- metres per second satisfies the 
 first and last series of the experiments the best. 
 
 Berlin, February 15, 1876. 
 
13 
 
 NOTE ON THE MAGNETIC EFFECT OF ELECTRIC 
 CONVECTION 
 
 [Philosophical Magazine [5], VII, 442, 443, 18791 
 
 JOHNS HOPKINS UNIVERSITY, BALTIMORE, April 8, 1878. 
 To the Editors of the Philosophical Magazine and Journal. 
 
 GENTLEMEN: Some three years since, while in Berlin, I made some 
 experiments on the magnetic effect of electric convection, which have 
 since been published in the ' American Journal of Science ' for Jan- 
 uary, 1878. But previous to that, in 1876, Professor Helmholtz had 
 presented to the Berlin Academy an abstract of my paper, which has 
 been widely translated into many languages. But, although Helm- 
 holtz distinctly says, " Ich bemerke dabei, das derselbe den Plan f iir 
 seine (Rowland's) Versuche schon gefasst und vollstandig iiberlegt 
 hatte, als er in Berlin ankam, ohne vorausgehende Einwirkung von 
 meiner Seite," yet nevertheless I now find that the experiment is being 
 constantly referred to as Helmholtz's experiment and that if I get 
 any credit for it whatever, it is merely in the way of carrying out 
 Helmholtz's ideas, instead of all the credit for ideas, design of appar- 
 atus, the carrying out of the experiment, the calculation of results, and 
 everything which gives the experiment its value. 
 
 Unfortunately for me, Helmholtz had already experimented on the 
 subject with negative results; and I found, in travelling through Ger- 
 many that others had done the same. The idea occurred in nearly 
 the same form to me eleven years ago; but as I recognized that the 
 experiment would be an extremely delicate one, I did not attempt it 
 until I could have every facility, which Helmholtz kindly gave me. 
 
 Helmholtz kindly suggested a more simple form of commutator than 
 I was about to use, and also that I should extend my experiments so 
 as to include an uncoated glass disk as well as my gilded vulcanite 
 ones; but all else I claim as my own, the method of experiment in all 
 its details, the laboratory work, the method of calculation indeed every- 
 thing connected with the experiment in any way, as completely as if it had 
 been carried out in my own laboratory 4000 miles from the Berlin labor- 
 atory. Yours truly, H. A. ROWLAND. 
 
14 
 
 XOTE OX THE THEORY OF ELECTRIC ABSORPTION 
 
 [American Journal of Mathematics, J, 53-58, 1878] 
 
 In experimenting with Leyden jars, telegraph cables and condensers 
 of other forms in which there is a solid dielectric, we observe that after 
 complete discharge a portion of the charge reappears and forms what 
 is known as the residual charge. This has generally been explained 
 by supposing that a portion of the charge was conducted below the 
 surface of the dielectric, and that this was afterwards conducted back 
 again to its former position. But from the ordinary mathematical 
 theory of the subject, no such consequence can be deduced, and we 
 must conclude that this explanation is false. Maxwell, in his ' Trea- 
 tise on Electricity and Magnetism,' vol. 2, chap X, has shown that a 
 substance composed of layers of different substances can have this 
 property. But the theory of the whole subject does not yet seem to 
 have been given. 
 
 Indeed, the general theory would involve us in very complicated 
 mathematics, and our equations would have to apply to non-homo- 
 geneous, crystalline bodies in which Ohm's law was departed from and 
 the specific inductive capacity was not constant; we should, moreover, 
 have to take account of thermo-electric currents, electrolysis, and 
 electro-magnetic induction. Hence in this paper I do not propose to 
 do more than to slightly extend the subject beyond its present state 
 and to give the general method of still further extending it. 
 
 Let us at first, then, take the case of an isotropic body in general, in 
 which thermo-electric currents and electrolysis do not exist, and on 
 and in which the changes of currents are so slow that we can omit 
 electro-magnetic induction. The equations then become 1 
 
 , 
 
 in which y is the specific inductive capacity of the substance, If the 
 
 'Maxwell's Treatise, Art. 325. 
 
140 HENET A. BOWLAND 
 
 electric conductivity, V the potential, p the volume density of the elec- 
 tricity, and t the time. 
 
 The subtraction of one equation from the other gives 
 
 To introduce the condition that there shall be no electric absorption, 
 we must observe that when that phenomenon exists, a charge of elecr 
 tricity appears at a point where there was no charge before; in other 
 words, the relative distribution has been changed. Hence, if the rela- 
 tive distribution remains the same, no electric absorption can take 
 place. Our condition is, then, 
 
 where c is independent of t, and // and p' are the densities at the points 
 x, y, z, and x', y' z'. This gives 
 
 
 where c is a function of t only and not of x, y, z, and p is the value of p 
 at the time t = 0. As we have 
 
 1 dV dm dV d /,-. k\ . dV d /, k\ . dV d /, k 
 
 where m = - and n is a line in the direction of the current at the given 
 
 I 
 point, equation (1) becomes 
 
 _1_ d V dm 1 dp 4rr p _ ft 
 m dn dn ~lc ^IT ~ ~^~ ' 
 From equation (2) 
 
 P = f 
 
 and hence 
 
 _!_ dV dm 
 m dn dn 
 
 If we denote the strength of current at the point by 8, we have 
 
NOTE ox THE THEORY OF ELECTRIC ABSORPTION 141 
 
 8- -k dV 
 k Wi' 
 
 and 
 
 1 dm _. j^ /*. 
 cm - 4:rw 8 dn IS 
 
 JL 
 
 this equation (3) gives the value of - =m at all points of the body 
 
 and at all times so that the phenomenon of electric absorption shall not 
 take place. As this equation makes m a function of x, y, z, S and t, 
 the relation in general is entirely too complicated to ever apply to 
 physical phenomena, without some limitation. Firstly then, as c is only 
 an arbitrary function of t, we shall assume that it is constant ; 
 
 .. . 
 
 cm 47:w 2 dn 6' 
 
 The most important case is where m is a constant. Then 
 
 dm _ ~ 
 ~dn ~ 
 and 
 
 c = 4:xm, S=S a s-, p = p.e-. 
 
 In this case, therefore, we see that both the electrification and the 
 currents die away at the rate c. The case where Ohm's law is true and 
 the specific inductive capacity is constant is included in this case, seeing 
 that when Jc and % are both constants their ratio, m, is constant. But 
 it also includes the cases where k and # are both the same functions of 
 V, S, or x, y, z, seeing that their ratio, m, would be constant in this 
 case also. 
 
 When m is not constant, the chances are very small against its satis- 
 fying equation (4). 
 
 Hence, we may in general conclude, that electric absorption will almost 
 certainly take place unless the ratio of conductivity to the specific inductive 
 capacity is constant throughout the body. 
 
 This ratio, m, may become a variable in several manners, as follows : 
 
 1st manner. The body may not be homogeneous. This includes the 
 case, which Maxwell has given, where the dielectric was composed of 
 layers of different substances. 
 
 2d manner. The body may not obey Ohm's law; in this case k would 
 be variable. 
 
 3d manner. The specific inductive capacity, , may vary with the 
 electric force. 
 
142 HEXRY A. KOWLAND 
 
 It is to be noted that the cases of electric absorption which we 
 observe are mostly those of condensers formed of two planes, or of one 
 cylinder inside another, as in a telegraph cable. Our theory shows 
 that different explanations can be given of these two cases. 
 
 The case of parallel plates does not admit of being explained, except 
 on the supposition that m varies in the first manner above given, or in 
 this manner in combination with the others, for we can only conceive 
 of the conductivity and the specific inductive capacity as being func- 
 tions of the ordinate or of the electric force. As the latter is constant 
 for all points between the plates, m would still be constant although it 
 were a function of the electric force, and thus electric absorption would 
 not take place. 
 
 We may then conclude that in the case of parallel plates, omitting 
 explanations based on electrolysis or thermo-electric currents, the only 
 explanation that we can give at present is that which depends on the 
 non-homogeneity of the body, and is the case which Maxwell has given 
 in the form of two different materials. Our equations show that the 
 form of layers is not necessary, but that any departure from homo- 
 geneity is sufficient. It is to be noted that the homogeneity, which we 
 speak of, is electrical homogeneity, and that a mass of crystals with 
 their axes in different directions would evidently not be electrically 
 homogeneous and would thus possess the property in question. In the 
 case of glass it is very possible that this may be the case and it would 
 certainly be so for ice or any other crystalline substance which had 
 been melted and cooled. 
 
 In the case of hard india rubber, the black color is due to the particles 
 of carbon, and as other materials are incorporated into it during the 
 process of manufacture, it is certainly not electrically homogeneous. 
 
 As to the ordinary explanation that the electricity penetrates a little 
 below the surface and then reappears again to form the residual charge, 
 we see that it is in general entirely false. We could, indeed, form a 
 condenser in which the surface of the dielectric would be a better con- 
 ductor than the interior and which would act thus. But in general, 
 the theory shows that the action takes place throughout the mass of 
 the dielectric, where that is of a fine grained structure and apparently 
 homogeneous, as in the case of glass, and consists of a polarization of 
 every part of the dielectric. 
 
 To consider more fully the case of a condenser made of parallel 
 plates, let us resume our original equations. Without much loss of 
 generality we can assume a laminated structure of the substance in 
 
NOTE ON THE THEORY OF ELECTRIC ABSORPTION 143 
 
 the direction of the plane YZ, so that m and V will be only functions 
 of the ordinate x. Our equations then become 
 
 d 
 
 A ~- 
 
 dx dx j dt 
 
 Eliminating p we find 
 
 if A _ 
 
 4- dt dx \dx dx dx 
 Now let us make p = x -=- and as t and x are independent, we find 
 
 CvtC 
 
 on integration, 
 
 (P Pj + 4 " (P m jOoWo) = 0, 
 
 where p is the value of p for some initial value of x, say at the surface 
 of the condenser, and is an arbitrary function of t, seeing that we may 
 vary the charge at the surface of the body in any arbitrary manner. 
 This equation establishes p as a function of m and t only, and as we have 
 
 1 dp 
 ~~ - 
 
 p will also be a function of these only. 
 
 Let us now suppose that at the time t = 0, the condenser is charged, 
 having had no charge before, and let us also suppose that the different 
 strata of the dielectric are infinitely thin and are placed in the same 
 order and are of the same thickness at every 'part of the substance, so 
 that a finite portion of the substance will have the same properties at 
 every part. 
 
 In this case m will be a periodic function of x, returning to the same 
 value again and again. As p is a function of this and of t only, at a 
 given time t, it must return again and again to the same value as we 
 pass through the substance, indicating a uniform polarized structure 
 throughout the body. 
 
 This conclusion would have been the same had we not assumed a 
 laminated structure of the dielectric. In all other cases, except that 
 of two planes, electric absorption can take place, as we have before 
 remarked, even in perfectly homogeneous bodies, provided that Ohm's 
 law is departed from or that the electric induction is not proportional 
 to the electric force, as well as in non-homogeneous bodies. But where 
 the body is thus homogeneous, electric absorption is not due to a uni- 
 
144 HENRY A. KOWLAND 
 
 form polarization, but to distinct regions of positive and negative 
 electrification. 
 
 In the whole of the investigation thus far we have sought for the 
 means of explaining the phenomenon solely by means of the known 
 laws of electric induction and conduction. But many of the phenomena 
 of electric absorption indicate electrolytic action, and it is possible that 
 in many cases this is the cause of the phenomenon. The only object 
 of this note is to partially generalize Maxwell's explanation, leaving 
 the electrolytic and other theories for the future. 
 
15 
 
 RESEARCH ON THE ABSOLUTE UNIT OF ELECTEICAL 
 
 RESISTANCE * 
 
 [American Journal of Science [3], XV, 281-291, 325-336, 430-439, 1878] 
 
 PEELIMINAEY REMABKS 
 
 Since the classical determination of the absolute unit of electrical 
 resistance by the Committee on Electrical Standards of the British 
 Association, two re-determinations have been made, one in Germany and 
 the other in Denmark, which each differ two per cent from the British 
 Association determination, the one on one side and the other on the 
 other side, making a total difference of four per cent between the two. 
 Such a great difference in experiments which are capable of consider- 
 able exactness, seems so strange that I decided to make a new deter- 
 mination by a method different from any yet used, and which seemed 
 capable of the greatest exactness; and to guard against all error, it was 
 decided to determine all the important factors in at least two different 
 ways, and to eliminate most of the corrections by the method of experi- 
 ment, rather than by calculation. The method of experiment depended 
 upon the induction of a current on a closed circuit, and in this respect, 
 resembled that of Kirchhoff, but it differed from his inasmuch as, in 
 my experiment, the indiiction current was produced by reversing the 
 main current, and in Kirchhoff's by removing the circuits to a distance 
 from each other. And it seems to me that this method is capable of 
 greater exactness than any other, and it certainly possessed the greatest 
 simplicity in theory and facility in experiment. 
 
 In the carrying out of the experiment I have partly availed myself 
 of my own instruments and have partly drawn on the collection of the 
 University, which possesses many unique and accurate instruments for 
 electric and magnetic measurements. To insure uniformity and accur- 
 acy, the coils of all these instruments have been wound with my own 
 hands and the measurements reduced to a standard rule which was 
 
 1 1 am greatly indebted to Mr. Jacques, Fellow of the University, who is an excel- 
 lent observer, for his assistance during the experiment, particularly in reading the 
 tangent galvanometer. 
 10 
 
146 HENRY A. KOWLAND 
 
 again compared with the standard at Washington. Unlike many Ger- 
 man instruments, quite fine wire has always been used and the number 
 of coils multiplied, for in this way the constants of the coils can be 
 more exactly determined, there is less relative action from the wire 
 connecting the coils, and above all we know exactly where the current 
 passes. 
 
 The experiment was performed in the back room of a small house 
 near the University, which was reasonably free from magnetic and other 
 physical disturbances. As the magnetic disturbance was eliminated 
 in the experiment, it was not necessary to select a region entirely free 
 from such disturbance. The small probable error proves that sufficient 
 precaution was taken in this respect. 
 
 The result of the experiment that the British Association unit is too 
 great by about -88 per cent, agrees well with Joule's experiment on the 
 heat generated in a wire by a current, and makes the mechanical equiv- 
 alent as thus obtained very nearly that which he found from friction: 
 it is intermediate between the result of Lorenz and the British Asso- 
 ciation Committee; and it agrees almost exactly with the British Asso- 
 ciation Committee's experiments, if we accept the correction which I 
 have applied below. 
 
 The difference of nearly three per cent which remains between my 
 result and that of Kohlrausch is difficult to explain, but it is thought 
 that something has been done in this direction in the criticism of his 
 method and results which are entered into below. My value, when 
 introduced into Thomson's and Maxwell's values of the ratio of the 
 electromagnetic to the electrostatic units of electricity, caused a yet 
 further deviation from its value as given in Maxwell's electromagnetic 
 theory of light: but experiments on this ratio have not yet attained 
 the highest accuracy. 
 
 HISTORY 
 
 The first determination of the resistance of a wire in absolute meas- 
 ure was made by Kirchhoff 2 in 1849 in answer to a question propounded 
 by Neumann, in whose theory of electrodynamic induction a constant 
 appeared whose numerical value was unknown until that time. His 
 method, like that of this paper, depended on induction from currents: 
 only one galvanometer was used and the primary current was measured 
 by allowing only a small proportion of it to pass through the galvano- 
 
 2 Bestimmung der Constanten von welcher die Intensitat inducirter elektrischer 
 Strome abhangt. Fogg. Ann., Bd. 76, S. 412. 
 
Ox THE ABSOLUTE UNIT OF ELECTRICAL RESISTANCE 147 
 
 meter by means of a shunt, while all the induced current passed through 
 it. But, owing to the heating of the wires, the shunt ratio cannot be 
 relied upon as constant, and hence the defect of the method. At pres- 
 ent this experiment has only historical value, seeing that no exact 
 record was kept of it in a standard resistance. However, we know that 
 the wire was of copper and the temperature R. and that the result 
 obtained gave the resistance of the wire $ smaller than Weber found 
 for the same wire at 20 R. in 1851. 
 
 In 1851, "Weber published 8 experiments by two methods, first by 
 means of an earth inductor, and second by observing the damping of a 
 swinging needle. Three experiments gave for the resistance of the 
 
 circuit 1903 -10 8 , 1898 -10 8 , and 1900 -10 s , , but it is to be noted 
 
 sec. 
 
 that a correction of five-eighths per cent was made on account of the 
 time, two seconds, which it took to turn the earth-inductor, and that 
 no account was taken of the temperature, although the material was 
 
 copper. He finds for the value of the Jacobi unit, 598 -10 7 ^. Three 
 
 OCC'B 
 
 years after that, in 1853, Weber made another determination of the 
 specific resistance of copper. 4 But these determinations were more to 
 develope the method than for exact measurement, and it was not until 
 1862 5 that Weber made an exact determination which he expected to 
 be standard. In this last determination he used a method compounded 
 of his first two methods by which the constant of the galvanometer was 
 eliminated, and the same method has since been used by Kohlrausch 
 in his experiments of 1870. The results of these experiments were 
 embodied in a determination of the value of the Siemens unit and of 
 a standard which was sent by Sir Wm. Thomson. As the old Siemens 
 units seem to vary among themselves one or two per cent, and as the 
 result from Thomson's coil differs more than one per cent from that 
 which would be obtained with any known value of the Siemens unit, 
 we cannot be said to know the exact result of these experiments at the 
 present time. Beside which, it was not until the experiments of Dr. 
 Matthiessen on the electric permanence of metals and alloys, that a 
 suitable material could be selected for the standard resistance. 
 
 The matter was in this state when a committee was appointed by the 
 
 3 Elektrodynamische Maasbestimmungen ; or Pogg. Ann., Bd. 82, S. 337. 
 4 Abh. d. Kon. Ges. d. Wissenchaften zu Gottingen, Bd. 5. 
 
 5 Zur Galvanometrie, Gottingen, 1862. Also Abb. d. K. Ges. d. Wis. zu Gottingen, 
 Bd. 10. 
 
148 HENRY A. BOWLAXD 
 
 British Association in 1861, who, by their experiments which have ex- 
 tended through eight years, have done so much for the absolute system 
 of electrical measurements. But the actual determination of the unit 
 was made in 1863-4. The method used was that of the revolving coil 
 of Sir William Thomson, the principal advantage of which was its sim- 
 plicity and the fact that the local variation of the earth's magnetism 
 was entirely eliminated and only entered into the calculation as a small 
 correction. The principle of the method is of extreme beauty, seeing 
 that the same earth's magnetism which causes the needle at the centre 
 of the coil to point in the magnetic meridian also causes the current in 
 the revolving coil which deflects the needle from that meridian. When- 
 ever a conducting body moves in a magnetic field, currents are gener- 
 ated in it in such direction that the total resultant action is such that 
 the lines of force are apparently dragged after the body as though they 
 met with resistance in passing through it : and so we may regard Thom- 
 son's method as a means of measuring the amount of this dragging 
 action. 
 
 But, however beautiful and apparently simple the method may appear 
 in theory, yet when we come to the details we find many reasons for 
 not expecting the finest results from it. Nearly all these reasons have 
 been stated by Kohlrausch, and I can do barely more in this direction 
 than review his objections, point out the direction in which each would 
 affect the result, and perhaps in some cases estimate the amount. 
 
 In the first place, as the needle also induced currents in the coil 
 which tended in turn to deflect the needle, the needle must have a very 
 small magnetic moment in order that this term may be small enough 
 to be treated as a correction. For this reason the magnetic needle 
 was a small steel sphere 8 mm. diameter, and not magnetized to satur- 
 ation. It is evident that in a quiescent magnetic field such a magnet 
 would give the direction of the lines of force as accurately as the large 
 magnets of Gauss and Weber, weighing many pounds. But the mag- 
 netic force due to the revolving coil is intermittent and the needle must 
 show as it were the average force, together with the action due to 
 induced magnetization. Whether the magnet shows the average force 
 acting on it or not, depends upon the constancy of the magnetic axis, 
 and there seems to be no reason to suppose that this would change in 
 the slightest, though it would have been better to have made the form 
 of the magnet such that it would have been impossible. The induced 
 magnetism of the sphere would not affect the result, were it not for the 
 time taken in magnetization: on this account the needle is dragged 
 
Ox THE ABSOLUTE UNIT OF ELECTRICAL EESISTAXCE 149 
 
 with the coil, and hence makes the deflection greater than it should be, 
 and the absolute value of the Ohm too small by a very small quantity. 
 The currents induced in the suspended parts also act in the same 
 direction. Neither of these can be estimated, but they are evidently 
 very minute. 
 
 The mere fact that this small magnet was attached to a comparatively 
 large mirror which was exposed to air currents could hardly have 
 affected the results, seeing that the disturbances would have been all 
 eliminated except those due to air currents from the revolving coil, and 
 which we are assured did not exist from the fact that no deflection took 
 place when the coil was revolved with the circuit broken. In revolving 
 the coil in opposite directions very different results were obtained, and 
 the explanation of this has caused considerable discussion. As this is 
 of fundamental importance I shall consider it in detail. 
 
 The magnet was suspended by a single fibre seven feet long, and the 
 deflection was diminished by its torsion -00132. No mention is made 
 of the method used for untwisting the fibre, and we see that it would 
 require only 2-11 turns to deflect the needle 1 from the meridian. 
 To estimate the approximate effect of this, we may omit from Maxwell's 
 equation * all the other minor corrections and we have 
 
 GKw cos <f _ GKw ]_ 
 
 : *tan?>(l + /)/7~ $t "\nearly, 
 
 1 ; 
 
 sin 
 
 where we have substituted <p /3 for <p in Maxwell's equation in the 
 term involving t. In this equation <p is measured from the magnetic 
 meridian; but let us take (p as the angle from the point of equilibrium. 
 Then tp' = <p' + a and (p" = <p" , where <p' and (f ' are for negativa 
 
 OJ 
 
 rotation and (p" and <p" for positive rotation and = arc sin 
 
 Let 
 
 Then CR = 
 
 CR" = 
 
 _ 
 
 tan 4'" (1 + ' 
 R,= l(R' + R"}. 
 
 Where R' and R" are the apparent values of the resistance as calculated 
 from the negative and positive rotations, and R, is the mean of the 
 
 Reports on Electrical Standards,' p. 103. 
 
150 HENRY A. KOWLAXD 
 
 two as taken from the table published by the British Association Com- 
 mittee. If R is the true resistance, 
 
 1 1 
 
 We shall then find approximately 
 
 n _ 1 + tan v' ; ' tan a _ I tan <l'" tan a 
 
 ~ /., sin a V- tan a 
 -ft 1 
 
 tan f/ \ sin ^"/\ tan 
 
 When a is small compared with </'" or 0', and when these are also small, 
 we have 
 
 R = R, (1 + a 2 (a 2 - | 0) + &c.). 
 
 So that by taking the mean of positive and negative rotations, the 
 effect of torsion is almost entirely eliminated. Now a is the angle by 
 which the needle is deflected from the magnetic meridian by the torsion 
 
 1 / /?' \ 
 and its value is ( 1 -^ ) nearly, when a is small, and this, in one 
 
 Kr \ ** I 
 
 or two of their experiments, exceeds unity or a exceeds 28. 6, which 
 
 Tf 
 
 is absurd. Taking even one of the ordinary cases where -> = 102 
 
 and (p is about ^V we have a= 12 - nearly, which is a value so large 
 that it would surely have been noticed. Hence we may conclude 
 that no reasonable amount of torsion in the silk fibre could have 
 produced the difference in the results from positive and negative 
 rotation, as has been stated by Mr. Fleming Jenkin in his ' Keport on 
 the New Unit of Electrical Eesistance/ r 
 
 The greatest value which we can possibly assign to a which might 
 have remained unnoticed is y 1 ^, which would not have affected the 
 the experiment to any appreciable extent. 
 
 Another source of error which may produce the difference we are 
 discussing is connected with the heavy metal frame of the apparatus, 
 in which currents can be induced by the revolving coil. The coil 
 passes so near the frame-work that the currents in it must be quite 
 strong and produce considerable magnetic effect. Kohlrausch has 
 pointed out the existence of these currents, but has failed to consider 
 the theory of them. Now, from the fact that after any number of 
 revolutions the number of lines of force passing through any part 
 of the apparatus is the same as before, we immediately deduce the 
 
 1 ' Reports on Electrical Standards,' London, 1873, p. 191. 
 
ON THE ABSOLUTE UNIT OF ELECTEICAL EESISTAXCE 151 
 
 fact that, if Ohm's law be correct, the algebraical sum of the currents 
 at every point in the frame is zero, and hence the average magnetic 
 action on the needle zero. But although these currents can have 
 no direct action, they can still act by modifying the current in the 
 coil; for while the coil is nearing one of the supports the current 
 in the coil is less than the normal amount, and while it is leaving 
 it is greater; and although the total current in the coil is the normal 
 amount, yet it acts on the needle at a different angle. By changing 
 the direction of rotation, the effect is nearly but not quite eliminated. 
 The amount of the effect is evidently dependent upon the velocity 
 of rotation and increases with it in some unknown proportion, and 
 the residual effect is evidently in the direction of making the action 
 on the needle too small and thus of increasing R. If these currents 
 are the cause of the different values of R obtained with positive and 
 negative rotation, we should find that if we picked out those experi- 
 ments in which this difference was the greatest, they should give 
 a larger value of R than the others. Taking the mean of all the 
 results " in which this difference is greater than one per cent, we find 
 
 for the Ohm 1.0033 earth ^ uadt , and when it is less than one per 
 
 sec. 
 
 cent, -9966 r - SC*r which is in accordance with the theory, the 
 sec. 
 
 average velocities being ^ and *^ nearly. But the individual 
 observations have too great a probable error for an exact comparison. 
 
 But whatever the cause of the effect we are considering, the follow- 
 ing method of correction must apply. The experiments show that R 
 is a function of the velocity of rotation, and hence, by Taylor's theorem, 
 the true resistance R must be 
 
 R = R (1 -f- Aw + Bw 2 + &c.), 
 
 and when R is the mean of results with positive and negative rotations, 
 R = R (1 -f Bw 2 + DW* + &c.). 
 
 Supposing that all the terms can be omitted except the first two, and 
 using the above results for large and small velocities, we find .R 
 
 _ . 9926 earth quad. But if we - ect the two resu i ts i n wn i c h the 
 sec. 
 
 8 In the table published by the Committee the different columns do not agree, and 
 I have thought it probable that the last two numbers in the next to the last column 
 should read 1-0032 and 1-0065 instead of 1-0040 and -9981, and in my discussion I 
 have considered them to read thus. 
 
152 HENEY A. EOWLAND 
 
 difference of positive and negative rotations is over seven per cent, 
 we find 
 
 sec. 
 
 The rejection of all the higher powers of w renders the correction 
 uncertain, but it at least shows that the Ohm is somewhat smaller 
 than it was meant to be, which agrees with my experiments. 
 
 It is to be regretted that the details of these experiments have 
 never been published, and so an exact estimate of their value can 
 never be made. Indeed we have no data for determining the value 
 of the Ohm from the experiments of 1863. All we know is that, in 
 the final result, the 1864 experiments had five times the weight of 
 those of 1863, and that the two results differed -16 per cent, but 
 which was the larger is not stated. Now the table of results pub- 
 lished in the report of the 1864 experiments contains many errors, 
 some of which we can find out by comparison of the columns. The 
 following corrections seem probable in the eleven experiments : No. 4, 
 second column, read 4-6375 for 4-6275. No. 10, fourth and fifth 
 columns, read 1-0032 and + 0-32 in place of 1-0040 and +0-40. No. 
 11, fourth and fifth columns, read 1-0065 and + 0-65 in place of 0-9981 
 and 0-19. Whether we make these corrections or not the mean 
 value is entirely incompatible with the statement with respect to the 
 1863 experiments. With the corrections the mean value of the 1864 
 
 experiments is 1 Ohm = 1-00071 earth ^ uad \ and without them, using 
 
 sec. 
 
 the fourth column, it is 1-00014. With the corrections the difference 
 between fast and slow rotation is 6 per cent. 
 
 In the year 1870 Professor F. Kohlrausch made a new determination 
 of Siemen's unit in absolute measure, the method being one formed 
 out of a combination of Weber's two methods of the earth inductor and 
 of damping, by which the constant of the galvanometer was eliminated, 
 and is the same as Weber used in his experiments of 1862. His formula 
 for the resistance of the circuit, omitting small corrections, is 
 
 approximately, 
 
 where 8 is the surface of the earth inductor, T is the horizontal inten- 
 sity of the earth's magnetism, K the moment of inertia of the magnet, 
 t the time of vibration of the magnet, ^ the logarithmic decrement, 
 and A and B are the arcs in the method of recoil. 
 
ON THE ABSOLUTE UNIT OF ELECTRICAL EESISTANCE 153 
 
 One of the principal criticisms I have to offer with respect to this 
 method is the great numher of quantities difficult to observe, which 
 enter the equation as squares, cubes, or even fourth powers. Thus S 2 
 depends upon the fourth power of the radius of the earth inductor. 
 Now this earth inductor was wound years before by W. Weber, and the 
 mean radius determined from the length of wire and controlled by 
 measuring the circumference of the layers. Now the wire was nearly 
 3-2 mm. diameter with its coating, and the outer and inner radii were 
 115- mm. and 142 mm. Hence the diameter of the wire occupied two 
 per cent of the radius of the coil, making it uncertain to what point 
 the radius should be measured. As the coil is wound, each winding 
 sinks into the space between the two wires beneath, except at one spot 
 where it must pass over the tops of the lower wires. The wire must 
 also be wound in a helix. All these facts tend to diminish 8 and make 
 its value as deduced from the length of the wire too large; and any 
 kinks or irregularities in the wire tend in the same direction. And 
 these errors must be large in an earth-inductor of such dimensions, 
 where the wire is so large and many layers are piled on each other. 
 If we admit an error of one-half a millimetre in the radius as deter- 
 mined in this way, it would diminish the value of S 2 1-4 per cent, and 
 make Kohlrausch's result only -6 per cent greater than the result of 
 the British Association Committee. 
 
 Three other quantities, T, X and K, are very hard to determine with 
 accuracy, and yet T enters as a square. It is to be noted that this 
 earth-inductor is the same as that used by Weber in his experiment of 
 1862, and which also gave a larger value to the Ohm than those of the 
 British Association Committee. Indeed, the results with this inductor 
 and by this method form the only cases where the absolute resistance of the 
 Ohm has been found greater than that from the experiments of the British 
 Association Committee, 
 
 There seems to be a small one-sided error in A and B which Kohl- 
 rausch does not mention, but which Weber, in his old experiments of 
 1851, considered worthy of a -6 per cent correction, and which would 
 
 diminish by 1-2 per cent. This is the error due to loss of 
 
 time in turning the earth-inductor. As Kohlrausch's needle had a 
 longer time of vibration than Weber's, the correction will be much 
 smaller. In Weber's estimate the damping was not taken into account, 
 and indeed it is impossible to do so with exactness. To get some idea 
 of the value of the correction, however, we can assume that the current 
 
154 HENRY A. KOWLAND 
 
 from the earth-inductor is uniform through a time t'", and the com- 
 plete solution then depends on the elimination of nine quantities from 
 ten complicated equations, and which can only be accomplished approx- 
 imately. If f is the true value of the angular velocity, as given to the 
 needle by the earth-inductor, and f is the velocity as deduced from the 
 ordinary equation for the method of recoil, I find 
 
 where A is the logarithmic decrement, the base of the natural system 
 of logarithms, T the time of vibration of the needle, and t the time 
 during which the uniform current from the earth-inductor flows. In 
 the actual case, the current from the earth-inductor is nearly propor- 
 tional to sin t, and hence it will be more exact to substitute 
 
 / / \2 /iir / / 
 
 4 (--) I taiiitdt = l( 
 V * / / v * 
 
 in the place of t 2 . The formula then becomes 
 
 This modification is more exact when ), is small than when it is large, 
 but it is sufficiently exact in all cases to give some idea of the magni- 
 tude of the error to be feared from this source. Kohlrausch does not 
 state how long it took him to turn his earth-inductor, but as T = 34 
 
 seconds, we shall assume -^ J^ and as / = \ nearly, we have 
 
 -?- = 1-0008, 
 
 r 
 
 which would diminish the value of the resistance by -16 per cent. 
 
 As the time we have allowed for turning the earth-inductor is prob- 
 ably greater than it actually was, the actual correction will be less than 
 this. 
 
 The correction for the extra current induced in the inductor and 
 galvanometer, as given by Maxwell's equation, 9 has been shown by 
 Stoletow to be too small to affect the result appreciably. 
 
 We may sum up our criticism of this experiment in a few words. 
 The method is defective because, although absolute resistance has the 
 
 dimensions of - , yet in this method the fourth power of space and 
 9 ' Electricity and Magnetism,' art. 762. 
 
ON THE ABSOLUTE UNIT OF ELECTEICAL RESISTANCE 155 
 
 the square of time enter, besides other quantities which are difficult to 
 determine. The instruments are defective, because the earth-inductor 
 was of such poor proportion and made of such large wire that its 
 average radius was difficult to determine, and was undoubtedly over- 
 estimated. 
 
 It seems probable that a paper scale, which expands and contracts 
 with the weather was used. And lastly, the results with this inductor 
 and by this method have twice given greater results than anybody else 
 has ever found, and greater than the known values of the mechanical 
 equivalent of heat would indicate. 
 
 The latest experiments on resistance have been made by Lorenz of 
 Copenhagen, 10 by a new method of his own, or rather by an application 
 of an experiment of Faraday's. It consists in measuring the difference 
 of potential between the centre and edge of a disc in rapid rotation 
 in a field of known magnetic intensity. 
 
 A lengthy criticism of this experiment is not needed, seeing that it 
 was made more to illustrate the method than to give a new value to 
 the Ohm. The quantity primarily determined by the experiment was 
 the absolute resistance of mercury, and the Ohm will have various 
 values according to the different values which we assume for the resist- 
 ance of mercury in Ohms. 
 
 One of the principal defects of the experiment is the large ratio 
 between the radius of the revolving disc and the coil in which it 
 revolved. 
 
 In conclusion I give the following table of results, reduced as nearly 
 
 as possible to the absolute value of the Ohm in earth q uad \" 
 
 sec. 
 
 iPogg. Ann., Bd. cxlix, (1873), p. 251. 
 
 11 Since this was written, a new determination has been made by H. F. Weber, of 
 Zurich, in which the different results agree with great accuracy. The result has 
 been expressed in Siemen's units, and the comparison seems to have been made 
 simply with a set of resistance coils and not with standards. The modern Siemen's 
 units seem to be reasonably exact, but from the table published by the British 
 Association Committee in 1864, it seems that at that time there was uncertainty as 
 
 to its value. He obtains 1 8. U. = -9550 ---', which is greater or less than 
 
 sec. 
 
 the British Association determination, according as we take the different ratios of 
 the Siemen's to the British Association unit, ranging from -14 per cent above to 1-92 
 per cent below. In any case the result agrees reasonably well with my own. The 
 apparatus used does not seem to have been of the best, and the exact details are not 
 given. But wooden coils to wind the wire on seem to have been used, which should 
 immediately condemn the experiment where a pair of coils is used, seeing that in 
 that case the constant, both of magnetic effect and of induction, depend on the dis- 
 tance of the coils. It is unfortunate that sufficient details are not given for me to 
 enter into a criticism of the experiment. 
 
156 
 
 HENRY A. EOWLAND 
 
 Date. 
 
 Observer. 
 
 Value of Ohm. 
 
 Remarks. 
 
 1849 
 
 Kirchhoff 
 
 88 to -90 
 
 Approximately. 
 
 1851 
 
 Weber 
 
 95 to -97 
 
 
 1862 
 
 Weber 
 
 ( 1-088 
 
 From Thomson's unit. 
 
 1863-4 
 1870 
 
 B. A. Committee. 
 Kohlrausch 
 
 { 1-075 
 1-0000 
 * -993 
 1-0196 
 
 From Weber's value of Siemen's unit. 
 Mean of all results. 
 Corrected to a zero velocity of coil. 
 
 1873 
 
 Lorenz 
 
 -970 
 
 Taking ratio of quicksilver unit to Ohm = 
 962. 
 
 1876 
 
 Rowland 
 
 \ -980 
 9912 
 
 Taking ratio of quicksilver unit to Ohm= 
 953. 
 From a preliminary comparison with the B. 
 
 
 
 
 A. unit. 
 
 THEORY OF THE METHOD 
 
 When a current is induced in a circuit by magnetic action of any kind, 
 Faraday has shown that the induced current is proportional to the 
 number of lines of force cut by the circuit and inversely as the resist- 
 ance of the circuit. If we have two circuits near each other, the first 
 of which carries a current, and the second is then removed to an infinite 
 distance, there will be a current in it proportional to the number of 
 lines of force cut. Let now a unit current be sent through the second 
 circuit and one of strength E through the first; then, on removing 
 the second circuit, work will be performed which we easily see is also 
 proportional to the number of lines of force cut. Hence, if EM is 
 the work done, Q is the induced current, and R is the resistance of the 
 second circuit, 
 
 -, 
 
 where C is a constant whose value is unity on the absolute system. 
 
 When the current in the first circuit is broken, the lines of force 
 contract on themselves, and the induced current is the same as if the 
 second circuit had been removed to an infinite distance. If the current 
 is reversed the induced current is twice as great; hence in this case 
 
 = ^ or = 
 
 K V 
 
 Hence, to measure the absolute resistance of a circuit on this method, 
 we must calculate M and measure the ratio of Q to E. M is known 
 as the mutual potential of the two circuits with unit currents, and 
 mathematical methods are known for its calculation. 
 
 The simplest and best form in which the wire can be wound for the 
 
Ox THE ABSOLUTE UXIT OF ELECTKICAL KESISTAXCE 157 
 
 calculation of M is in parallel circular coils of equal size and of as 
 small sectional area as possible. For measuring E a tangent galvano- 
 meter is needed, and we shall then have 
 
 E= ^ tanfl. 
 
 6r 
 
 where H is the horizontal intensity of the earth's magnetism at the 
 place of the tangent galvanometer, and G the constant of the galvano- 
 meter. 
 
 For measuring Q we must use the ballistic method, and we have 
 
 . 
 
 which for very small values of ), becomes 
 
 ^ G' - s ' ' 
 
 H' ~W Tain*? I + *A - * A 2 ' 
 
 where H' is the horizontal component of the earth's magnetism at the 
 place of the small galvanometer, G' its constant, T the time of vibra- 
 tion of the needle, and X the logarithmic decrement. 
 
 The ratio of H' to H can be determined by allowing a needle to 
 vibrate in the two positions. But this introduces error, and by the 
 following method we can eliminate both this and the distance of the 
 mirror from the scale by which we find 0' and the error of tangent 
 galvanometer due to length of needle. The method merely consists 
 in placing a circle around the small galvanometer and then taking 
 simultaneous readings with the current passing through it and the 
 tangent galvanometer, before and after each experiment. Let and a' 
 be the deflections of the tangent galvanometer and the other galvano- 
 meter respectively, and let G" be the constant of the circle at the point 
 where the needle hangs, then 
 
 TT JJ I 
 
 -^ tan a = -^j- tan a', 
 
 and we have finally 
 
 TT G tan a' tan 6 \ 
 
 R=M- 
 
 T G 71 ' ta.na sin*0' l+JA U' 
 
 which does not contain H or H', and the distance of the mirror from 
 the scale does not enter except as a correction in the ratio pf sin # 
 and tan a'; and, as a and can be made nearly equal, the correction 
 
158 HENEY A. EOWLAND 
 
 of the tangent galvanometer for the length of needle is almost elimi- 
 nated. When the method of recoil is used, we must substitute - ~TA 
 
 for the term involving /, and sin $A f -f- sin %B' in the place of sin ^ 6' 
 A' and B' being the greater and smaller arcs in that method. This is 
 on the supposition that X is small. 
 
 The ratio of G" to G must be so large, say 12,000, that it is difficult 
 to determine it by direct experiment, but it is found readily by measure- 
 ment or indirect comparison. 
 
 It is seen that in this equation the quantities only enter as the first 
 powers, and that the only constants to be determined which enter the 
 equation are M, G and G", which all vary in simple proportion to the 
 linear measurement. It is to be noted also that the only quantities 
 which require to be reduced to standard measure are M and T, and 
 that the others may all be made on any arbitrary scale. No correction 
 is needed for temperature except to M. Indeed, I believe that this 
 method exceeds all others in simplicity and probable accuracy and its 
 freedom from constant errors, seeing that every quantity was varied 
 except G" and G, whose ratio was determined within probably one in 
 three thousand by two methods. 
 
 Having obtained the resistance of the circuit by this method, we 
 have next to measure it in ohms. For this purpose the resistance of 
 the circuit was always adjusted until it was equal to a certain German 
 silver standard, which was afterward carefully compared with the ohm. 
 This standard was about thirty-five ohms. 
 
 By this method, the following data are needed. 
 
 1. Eatio of constants of galvanometer and circle. 
 
 2. Eatio of the tangents of the two deflections of tangent galvano- 
 meter. 
 
 3. Eatio of the deflection to the swing of the other galvanometer. 
 
 4. Mutual potential of induction coils on each other. 
 
 5. Time of vibration of the needle. 
 
 6. Eesistance of standard in ohms. 
 For correction we need the following : 
 
 1. The logarithmic decrement. 
 
 2. Distance of mirror from scale. 
 
 3. Coefficient of torsion of suspending fibre. 
 
 4. Eate of chronometer. 
 
 5. Correction to reduce to standard metre. 
 
Ox THE ABSOLUTE UNIT OF ELECTRICAL KESISTANCE 159 
 
 6. Variation of the resistance of German silver with the temperature. 
 
 7. Temperature of standard resistance. 
 
 8. Arc of swing when the time of vibration is determined. 
 
 9. Length of needle in tangent and other galvanometer (nearly com- 
 pensated by the method). 
 
 10. The variation of resistance of circuit during the experiment. 
 The following errors are compensated by the method of experiment. 
 
 1. The local and daily variation of the earth's magnetism. 
 
 2. The variation of the magnetism of the needle. 
 
 3. The magnetic and inductive action of the parts of the apparatus 
 on each other. 
 
 4. The correction for length of needle in the tangent galvanometer 
 (nearly). 
 
 5. The axial displacement of the wires in the coils for induction. 
 
 6. The error due to not having the coils of the galvanometer and the 
 circle parallel to the needle. 
 
 7. Scale error (partly). 
 
 8. The zero error of galvanometers. 
 
 CALCULATION OF CONSTANTS 
 
 Circle. For obtaining the ratio of G to G", it is best to calculate 
 them separately and then take their ratio, though it might be found 
 by Maxwell's method ('Electricity,' article 753). But as the ratio is 
 great, the heating of the resistances would produce error in this latter 
 method. 
 
 For the simple circle, 
 
 where A is its radius and B the distance of the plane of the circle to 
 the needle on its axis. 
 
 Galvanometer for Induction Current. For the more sensitive galvano- 
 meter, we must first assume some form which will produce a nearly 
 uniform field in its interior, without impairing its sensitiveness. If we 
 make the galvanometer of two circular coils of rectangular section 
 whose depth is to its width as 108 to 100, and whose centres of sections 
 are at a radius apart from each other, we shall have Maxwell's modifi- 
 cation of Helmholtz's arrangement. The constant can then be found 
 by calculation or comparison with another coil. 
 
160 HEXKY A. EOWLAXD 
 
 Maxwell's formulae are only adapted to coils of small section. Hence 
 we must investigate a new formula. 13 
 
 Let N be the total number of windings in the galvanometer. 
 Let R and r be the outer and inner radii of the coils. 
 Let X and x be the distances of the planes of the edges of the coils 
 
 from the centre. 
 
 Let a be the angle subtended by the radius of any winding at the centre. 
 Let & be the length of the radius vector drawn from the centre to the 
 
 point where we measure the force. 
 Let 6 be the angle between this line and the axis. 
 Let c be the distance from the centre to any winding. 
 Let w be the potential of the coil at the given point. 
 
 Then (Maxwell's 'Electricity,' Art. 695), for one winding. 
 
 W = 2n ] 1 COS a + sin 2 a ( Q[ (a) $1 (#) 
 ( \c 
 
 and for two coils symmetrically placed on each side of the origin, 
 
 W = 4:r \ COS a sin 2 a ( * f ) O 2 ' (a) Q 2 (0) 
 
 I \ * \ c 1 
 
 where Q 2 (0), Q^(0), &c., denote zonal spherical harmonics, and Q 2 '()> 
 Q'i(a) &c., denote the differential coefficients of spherical harmonics 
 with respect to cos a. 
 
 As the needle never makes a large angle with the plane of the coils, 
 it will be sufficient to compute only the axial component of the force, 
 which we shall call F. Let us make the first computation without 
 substitution of the limits of integration, and then afterward substitute 
 these: 
 
 F = 
 
 * f C^-dxdr, 
 
 r)(X x)J J dx 
 
 and we can write 
 
 %*N 
 
 &c. 
 
 12 A formula involving the first two terms of my series, but applying only to the 
 special case of a needle in the centre of a single circle of rectangular section, is 
 given by Weber in his 'Elektrodynamische Maasbestimmungen inbesondere Wider- 
 standsmessungen,' S. 872. 
 
ON THE ABSOLUTE UNIT OF ELECTRICAL RESISTANCE 161 
 where H^ x log. (r + / y? + r 2 ) , 
 
 o _ 1.3.5. . 2t- 
 
 '2 1 (2* -1)2 
 
 ' 2t - 3 (it - l)(2i - 3) 2.4 
 
 D = C 2 *' 8 _ i(t'-l)..(* 6) 
 
 '2i 5 (2i-i)(2t 3)(2i - 5) 2.4.6' 
 
 E t = &c., &c. 
 
 Substituting the limits for x, r and a, we find 
 + V ^ 2 
 
 o = i / 1 f ^ ___ ^_ 1 / If r 3 \\ 
 
 \ X \(ff + X z )l (r 2 + JT')i "^ ^ + a?)l (r 2 + z*)*J J ' 
 
 
 The needle consisted of two parallel lamina? of steel of length, Z, and 
 a distance, W, from each other. As the correction for length is small, 
 we may assume that the magnetism of each lamina is concentrated in 
 two points at a distance n / from each other, where n is a quantity to 
 he determined. 
 Hence 
 
 W 
 
 where cos & /71 .., _,, seeing that the needle hangs parallel to 
 
 * 
 
 the coils. In short thick magnets, the polar distance is about Z and 
 the value of n will be about f . For all other magnets it will be between 
 this and unity. In the present case n = f nearly. 
 
 As all the terms after the first are very minute, this approximation 
 is sufficient, and will at least give us an idea of the amount of this 
 
 source of error. 
 11 
 
162 HENRY A. KOWLAND 
 
 INDUCTION COILS 
 
 The induction coils were in the shape of two parallel coils of nearly 
 equal size and of nearly square section. 
 
 Let A and a he the mean radii of the coils. Let & he the mean 
 distance apart of the coils. 
 
 Let 
 
 C 
 
 Supposing the coils concentrated at their centre of section we know that 
 
 where F(c) and E(c) are elliptic integrals. 
 
 If and y are the depth and width of each coil, the total value of 
 M will he, when A = a nearly, 
 
 and we find 
 
 nc 
 
 (1 
 O -2 _ 12^ A 
 
 ^2 
 
 COEBECTIONS 
 
 Calling /? and <5 the scale deflections corresponding to tan a' and sin 
 , we may write our equation for the value of the resistance 
 
 8 1--35 
 
 where R' is the resistance of the circuit at a given temperature 17-0 C., 
 and E = 2^M-^ Ff (l + a -f & + etc.), in which ^, 5, etc. and a, 6, etc. 
 
 are the variable and constant corrections respectively. 
 a. Correction for damping. 
 
ON THE ABSOLUTE UNIT OF ELECTRICAL KESISTANCE 163 
 
 I. Torsion of fibre. 
 
 The needle of the tangent galvanometer was sustained on a point 
 and so required no correction. The correction for the torsion in the 
 other galvanometer is the same for /? and d and hence only affects T. 
 Therefore, if t is the coefficient of torsion, 
 
 b= - It. 
 
 c. Rate of chronometer. 
 
 Let p be the number of seconds gained in a day above the normal 
 time 
 
 P 
 ~ 86400* 
 
 d. Reduction to normal metre. The portion of this reduction which 
 depends on temperature must be treated under the variable corrections. 
 Let m be the excess of the metre used above the normal metre, ex- 
 pressed in metres; then 
 
 d = + m. 
 
 e. Correction of T for the arc of vibration. This arc was always the 
 same, starting at c^ and being reduced by damping to about c n , 
 
 where c^ and c a are the total arcs of oscillation. 
 
 /. Correction for length of needles. For the tangent galvanometer, 
 the correction is variable. For the circle it is 
 
 /= + 
 
 where I is half the distance between the poles of the needle and A the 
 radius of circle. For the other galvanometer it is included in the 
 formula for G. 
 
 A. Reduction to normal metre. As the dimension of R is a velocity 
 and the induction coils were wound on brass, the correction is 
 
 where f is the coefficient of expansion of brass or copper, t' the actual 
 and t" the normal temperature. 
 
 B. Correction of standard resistance for temperature. Let a be the 
 variation of the resistance for 1 C., ?" be the actual and T the normal 
 temperature 17- C. ; then 
 
164 HENRY A. BOWL AND 
 
 C. Correction for length of needle in tangent galvanometer, 
 
 C = + J^ sin (a + ')f -|r-Y(a' ~ a ) ' 
 \-A-l 
 
 where V is half the distance between the poles of the needle and A' is 
 the radius of the coil. 
 
 D. The resistance of the circuit was constantly adjusted to the 
 standard, but during the time of the experiment the change of temper- 
 ature of the room altered the resistance slightly; this change was 
 measured and the correction will be plus or minus one-half this. The 
 resistance was adjusted several times during each experiment. The 
 correction is Z). 
 
 Some of the errors which are compensated by the experiment need 
 no remark and I need speak only of the following. 
 
 No. 3. By the introduction of commutators at various points all 
 mutual disturbance of instruments could be compensated. 
 
 No. 5. In winding wire in a groove, it may be one side or the other 
 of the centre. By winding the coils on the centre of cylinders which 
 set end to end, on reversing them and taking the mean result, this 
 error is avoided. 
 
 No. 6. The circle was always adjusted parallel to the coils of the 
 galvanometer. Should they not be parallel to the needle, G and 0" 
 will be altered in exactly the same ratios and will thus not affect the 
 result. The same may be said of the deflection of the magnet from 
 the magnetic meridian due to torsion. 
 
 No. 7. /? and 3 both ranged over the same portion of the scale and 
 so scale error is partly compensated. 
 
 No. 8. The zero-point of all galvanometers was eliminated by equal 
 deflections on opposite sides of the zero-point. 
 
 INSTRUMENTS 
 
 Wire and coils. The wire used in all instruments was quite small 
 silk-covered copper wire, and was always wound in accurately turned ls 
 brass grooves in which a single layer of wire just fitted. The separate 
 layers always had the same number of windings, and the wire was 
 wound so carefully that the coils preserved their proper shape through- 
 
 13 To obtain an accurate coil an accurate groove is necessary, seeing that otherwise 
 the wire will be heaped up in certain places. The circle of the tangent galvanometer, 
 which was made to order in Germany, had to be returned in this country before use, 
 and much time was lost before finding out the source of the difficulty. 
 
ON THE ABSOLUTE UNIT OF ELECTRICAL EESISTANCE 165 
 
 out. No paper was used between the layers. As the wire was small, 
 very little distortion was produced at the point where one layer had 
 to rise over the tops of the wires below. Corrections were made for 
 the thickness of the steel tape used to measure the circumference of 
 each layer; also for the sinking of each layer into the spaces between 
 the wires below, seeing that the tape measures the circumference of 
 the tops of the wires. The steel tape was then compared with the 
 standard. 
 
 The advantages of small wire over large are many; we know exactly 
 where the current passes; it adapts itself readily to the groove without 
 kinks; it fills up the grooves more uniformly; the connecting wires 
 have less proportional magnetic effect; and lastly, we can get the 
 dimensions more exactly. The size of wire adopted was about No. 22 
 for most of the instruments. 
 
 The mean radius having been computed, the exterior and interior 
 radii are found by addition and substraction of half the depth of the 
 coil. The sides of the coil were taken as those of the brass groove. 
 
 All coils were wound by myself personally to insure uniformity and 
 exactness. 
 
 Tangent galvanometer. This was entirely of brass or bronze, and 
 had a circle about 50 cm. diameter. The needle was 2-7 cm. long and 
 its position was read on a circle 20- cm. diameter, graduated to 15'. 
 The graduated circle was raised so that the aluminium pointer was on 
 a level with it, thus avoiding parallax. The needle and pointer only 
 weighed a gram or two, and rested on a point at the centre which was 
 so nicely made that it would make several oscillations within 1 and 
 would come to rest within 1' or 2' of the same point every time. I 
 much prefer a point with a light needle carefully made to any suspended 
 needle for the tangent galvanometer, especially as a raised circle can 
 then alone be used. The needle was suspended at a distance from any 
 brass which might have been magnetic. There were a series of coils 
 ascending nearly as the numbers 1, 3, 9, 27, 81, 243, whose constants 
 were all known, but only one was used in this experiment. The proba- 
 ble error of a single reading was about 1'. 
 
 Galvanometer for induction current. This was a galvanometer on a 
 new plan, especially adapted for the absolute measurement of weak 
 currents. It was entirely of brass, except the wooden base, and was 
 large and heavy, weighing twenty or twenty-five pounds. It could be 
 used with a mirror and scale or as a sine galvanometer. It will be 
 
166 HENKY A. EOWLAND 
 
 necessary to describe here only those portions which affect the accuracy 
 of the present experiment. 
 
 The coils were of the form described above in the theoretical portion, 
 and were wound on a brass cylinder about 8-2 cm. long and 11-6 cm. 
 diameter in two deep grooves about 3- cm. deep and 2-5 cm. wide. The 
 opening in the centre for the needle was about 5-5 cm. diameter and 
 the cylinder was split by a saw-cut so as to diminish the damping 
 effect. This coil was mounted on a brass column rising from a gradu- 
 ated circle by which the azimuth of the coil could be determined by 
 two verniers reading to 30". Through the opening in the coil beneath 
 the needle passed a brass bar 95 cm. long and 2 cm. broad, carrying a 
 small telescope at one end. In the present experiment, this bar was 
 merely used in the comparison of the constant of the instrument with 
 that of another instrument. For this purpose the instrument is used 
 as a sine galvanometer by which a great range can be secured, and it 
 could be compared with a coil having a constant twenty-three times 
 less and which was used with telescope and scale. 
 
 The coils contained about five pounds of No. 22 silk-covered copper 
 wire in 1790- turns. 
 
 Two needles were used in this galvanometer, each constructed so that 
 its magnetic axis should be invariable; this was accomplished by affixing 
 two thin laminae of glass-hard steel, to the two sides of a square piece 
 of wood, with their planes vertical. This made a sort of compound 
 magnet very strong for its length, and with a constant magnetic axis. 
 The first needle had a nearly rectangular mirror 2-4 by 1-8 cm. on 
 the sides and -22 cm. thick. The other needle had a circular mirror 
 2-05 cm. diameter and about 1 mm. thick. The needle of the first was 
 1-27 cm. and of the second 1-20 cm. long, and the pieces of wood were 
 about -45 cm. and -6 cm. square respectively. The moment of inertia 
 of both was much increased by two small brass weights attached to 
 wires in extension of the magnetic axis, thus extending the needles to 
 a length of 4-9 cm. and 4-2 cm. respectively. The total weights were 
 5-1 and 5-6 grams and the times of vibration about 7-8 and 11-5 
 seconds. They were suspended by three single fibres of silk about 43 
 cm. long. 
 
 In front of the needle was a piece of plane-parallel glass. This and 
 the mirrors were made by Steinheil of Munich, and were most perfect 
 in every way. 
 
 In the winding of the coils every care was taken, seeing that a small 
 error in so small a coil would produce great relative error. And for 
 
Ox THE ABSOLUTE UNIT OF ELECTRICAL RESISTANCE 167 
 
 this reason the constant was also found by comparison with another 
 coil. The following were the dimensions: 
 
 Mean radius 4-3212 cm. 
 R - 5-6212 r = 3-0212 
 
 X= 3-475565 x= -935565 
 
 R r = 2-6000 X x = 2-54000 
 
 ^=1790- 
 whence 
 
 F= 1832-25 1-70&'& (0) - 4-50i 4 & (0) + -90 6 () 6 (0) - &c. 
 Taking the mean dimensions of the two needles, we have 
 
 1 = 1-23, w = -52, w = |, cos 6' = -748. 
 Q t (0') = + 339 , Q t (6'} = - -354 , Q 6 (a') = - -275 . 
 .-. G = 1832-25 -083 + -071 - -002 + &c. = 1832-24. 
 
 The coil with which this galvanometer was compared was the large 
 coil of an electro-dynamometer similar to that described in Maxwell's 
 'Electricity/ Art. 725, but smaller. The coil was on Helmholtz's 
 principle with a diameter of 27-5 cm., and was very accurately wound 
 on the brass cylinder. There was a total of 240 windings in the coil. 
 The constant of this coil was 78-371 by calculation. 
 
 To eliminate the difference of intensity of the earth's magnetism, an 
 observation was first made and then the positions of the instruments 
 were changed so that each occupied exactly the position of the other: 
 the square root of the product of the two results was the true result 
 free from error. 
 
 The coils of the galvanometer could be separated so that an outer 
 and inner pair could be used together. By comparing these parts 
 separately and adding the constants together we find G. Hence two 
 comparisons are possible, one with the coils together and the other with 
 them separate. The results were for the ratio of the constants 
 
 23-3931 and 23-4008, 
 which give 
 
 G = 1833-37 and 1833-98. 
 The mean result is 
 
 1833-67 -09, 
 
 and this includes seven determinations with two reversals of instru- 
 ments. This result is one part in thirteen hundred greater than found 
 by direct calculation, which is to be accounted for by the small size of 
 the galvanometer coils and the consequent difficulty of their accurate 
 measurement. As comparison with the electro-dynamometer has such 
 
168 HENET A. KOWLAND 
 
 a small probable error, and as it is a much larger coil, it seems best to 
 give this number twice the weight of that found by calculation : we thus 
 obtain 
 
 (7 = 1833-19 
 as the final result. 
 
 It does not seem probable that this can be in error more than one 
 part in two or three thousand. 
 
 Telescope, scale, &c. The telescope, mirrors and plane-parallel glass 
 were all from Steinheil in Munich, and left nothing to be desired in 
 this direction, the image of the scale being so perfect that fine scratches 
 on it could be distinguished. The telescope had an aperture of 4 cm. 
 and a magnifying power of 20 was used. The scale was of silvered 
 brass, one metre long and graduated to millimetres. 
 
 Induction coils. A coil was wound in a groove in the centre of each 
 of three accurately turned brass cylinders of different lengths. Two 
 of them only were used at a time, by placing them end to end, the ends 
 being ground so that they laid on each other nicely. The two coils 
 could be placed in four positions with respect to each other, in each of 
 which they were very exactly the same distance apart. This distance 
 for each of the four positions, was determined at three parts of the 
 circumference by means of a cathetometer, with microscopic objective, 
 reading to ^ mm. The mean of all twelve determinations was the 
 mean distance. In using the coils they were always used in all four 
 positions. The probable error of each set of twelve readings was 
 -001 mm. The data are as follows, naming the coils, A, B and C : 
 
 Mean radius of A = 13-710, of B = 13-690, of C = 13-720. 
 
 Mean distance apart of A and 5 = 6-534, of A and (7 = 9-574, of 
 B and (7=11-471. 
 
 N= 154 for each coil, == -90, y = -84. 
 For A and B we have 
 
 M= 3774860- + T V (74250- 66510-) = 3775500- 
 The remaining terms of the series are practically zero, as was found 
 by dividing one of the coils into parts and calculating the parts sepa- 
 rately and adding them. 
 
 For A and C 
 
 M = 2561410- -f T V (34000- 27230-) = 2561974- 
 For B and (7 
 
 M = 2050600- + T V (27500- 19800-) = 2051320- 
 The calculation of the elliptic integrals was made by aid of the tables 
 of the Jacobi function, q, given in Bertrand's ' Traite de Calcul Inte- 
 
ON THE ABSOLUTE UNIT OF ELECTRICAL RESISTANCE 169 
 
 grale ' as well as by the expansions in terms of the modulus after trans- 
 forming them hy the Landen substitution. 
 
 The Circle. The circle whose constant we have called G" and which 
 was around the galvanometer whose constant was G, was a large wooden 
 one containing a single coil of No. 22 wire. 14 To prevent warping, it 
 was laid up out of small pieces of wood with the grain in the direction 
 of the circumference, and was carefully turned with a minute groove 
 near one edge in which the wire could just lie. It was about 5- cm. 
 broad, 1-8 thick and 82-7 cm. diameter. As the room had no fire in 
 it, the circle remained perfect throughout the experiment. The wire 
 was straightened by stretching and measured before placing on the 
 circle, which last was done with great care to prevent stretching; after 
 the experiment it was measured and found exact to T ' T mm. 
 
 The circle was adjusted parallel and concentric with the coils of the 
 galvanometer, but at a distance of 1-1 cm. to one side, in order to allow 
 the glass tube with the suspending fibre to pass. The length of wire 
 was 259-58 cm. which gives a mean radius of 41-31344 cm. These data 
 give G" = -151925. Preliminary results were also obtained by use of 
 another circle. 
 
 Chronometer. To obtain the time of vibration, a marine chronometer 
 giving mean solar time was used. The rate was only half a second 
 per day. 
 
 Wheatstone bridge. To compare the resistance of the circuit with the 
 arbitrary German silver standard, a bridge on Jenkin's plan, made by 
 Elliott of London, was used. A Thomson galvanometer with a single 
 battery cell gave the means of accurately adjusting the resistance, one 
 division of the scale representing one part in fifty thousand. 
 
 4 Thermometers. Accurate thermometers graduated to half degrees 
 were used for finding the temperature of the standard. 
 
 The arbitrary standard. This was made of about seventy feet of 
 German silver wire, mounted in the same way as the British Association 
 Standard. Immediately after use, two copies, one in German silver and 
 the other in platinum-silver alloy, were made. It had a resistance of 
 about 35 ohms. The temperature was taken as 17 C. 
 
 To obtain the accurate resistance of this standard in ohms, I had two 
 standards of 10 ohms and one of 1, 100, and 1,000 ohms. The 1-ohm, 
 and one of the 10-ohm standards, were made by Elliott of London, and 
 
 u ln another part of my paper I have criticised the use of wooden circles for coil, 
 but it is unobjectionable in the case of a single wire, especially when the needle i& 
 suspended near its centre. 
 
170 HENRY A. EOWLAND 
 
 the others by Messrs. Warden, Muirhead and Clark of the same place. 
 But on careful comparison I found that Warden, Muirhead and Clark's 
 10-ohm standard was 1-00171 times that of Messrs. Elliott Bros. On 
 stating these facts to the two firms I met no response from the first 
 firm, but the second kindly undertook to make me a standard which 
 should be true by the standards in charge of Professor Maxwell at 
 Cambridge." At present I give the result of the comparison with 
 these standards, as well as some others, and also with a set of resistance 
 coils by Messrs. Elliott Bros. 
 
 Commutators. No commutators except those having mercury con- 
 nections were used, and those in the circuit whose resistance was deter- 
 mined were so constructed as to offer no appreciable resistance. The 
 commutator by which the main current was reversed, could be operated 
 in a fraction of a second, so as to cause no delay in the reversal. 
 
 Connecting wires. These were of No. 22 or No. 16 wire and were all 
 carefully twisted together. The insulation was tested and found to be 
 excellent. 
 
 Inductor for damping. This has already been described in my first 
 paper on ' Magnetic Permeability,' and merely consisted of a small 
 horse-shoe magnet with a sliding coil, which was introduced into the 
 secondary circuit. By moving it back and forth, the induced current 
 could be used to stop the vibrations of the needle and make it stationary 
 at the zero point. This is necessary in the method where the first throw 
 of the galvanometer needle constitutes the observation, but in the 
 method of recoil it is not necessary to use it very often. I prefer the 
 method of the first throw as a general rule, but I have used both 
 methods. 
 
 This method of damping will be found much more efficient than that 
 of the damping magnet as taught by Weber, and after practice a single 
 movement will often bring the needle exactly to rest at the zero point. 
 
 Arrangement of apparatus. Two rooms on the ground floor of a 
 small building near the University were set aside for the experiment, 
 making a space 8 m. long by 3-7 m. wide. The plan of the arrange- 
 ment is seen at Fig. 1. The current from the battery, in the Univer- 
 sity, entered at A, the battery being eighteen one-gallon cells of a 
 chromate battery, arranged two abreast and eight for tension. The 
 
 18 As this is nearly a year since, and as I cannot tell when the standard will arrive, 
 I now publish the results as so far obtained, hoping to make a more exact comparison 
 in future. 
 
ON THE ABSOLUTE UXIT OF ELECTRICAL EESISTANCE 
 
 171 
 
 resistance of the circuit was about 20 ohms, and of the whole battery 
 about ^ ohm, thus insuring a reasonably constant current. 
 
 At B some resistance could be inserted by withdrawing plugs so as 
 to vary the current. 
 
 At C is the tangent galvanometer with commutator on a brick pier. 
 The nearness of the commutator produces no error, seeing that we only 
 wish to determine the ratio of two currents. The effect of currents in 
 the commutator was, however, vanishingly small in any case. 
 
 At D is the principal commutator which reversed the current in the 
 induction coils, L, or in the circle, F, when it was in the circuit. 
 
 FIG. 1. 
 
 The secondary circuit included the induction coil, L, the damping 
 inductor, M, and the galvanometer 0. 
 
 At H was the Jenkin's bridge, with standard at P, in a beaker of 
 water, and a Thomson galvanometer at J K. The secondary circuit 
 could be joined to the bridge by raising a U-shaped piece of wire out of 
 the mercury cups. 
 
 The telescope and scale, E, were on a heavy wooden table, and the 
 two galvanometers on brick piers with marble tops. 
 
 A row of gas-burners at Q illuminated the silvered scale in the most 
 perfect manner. 
 
 Adjustments and tests. The circle, F, must be parallel to coils of 
 galvanometer, G. The circle and coils of galvanometer were first 
 adjusted with their planes vertical and then adjusted in azimuth by 
 
172 HENKY A. EOWLAND 
 
 measurement from the end of the bar, R, to the sides of the circle, F. 
 The adjustment was always within 30', which would only cause an error 
 of one part in 25000. 
 
 The needle must hang in the magnetic meridian by a fibre without 
 torsion, and the coils must be parallel to it. These adjustments were 
 carefully made, but, as has been shown, the error from this source is 
 compensated. 
 
 The needle must hang in the centre of the galvanometer coils and 
 on the axis of the circle. The error from this source is vanishingly 
 small. 
 
 The scale must be perpendicular to the line joining the zero point 
 and the galvanometer needle, it must be level and not too much below 
 the galvanometer needle. All errors from this source are partially or 
 entirely compensated by the method of experiment. 
 
 The induction coils, L, must be horizontal, and at the same level as 
 the two galvanometers, so as not to produce any magnetic action on 
 them. The error from this source is exactly compensated by this 
 method of experiment, but could never amount to more than 1 part in 
 2000. 
 
 The tangent galvanometer should have the plane of its coils in the 
 magnetic meridian, but all errors are compensated. 
 
 The connecting wires must be so twisted together and arranged as 
 to produce no magnetic action, but tests were made in all cases where 
 the error was not compensated, and found to be practically zero. The 
 insulation of all coils, wires and commutators was carefully tested. 
 
 Method of experiment. As has been stated before, the method gener- 
 ally used was that of the first throw of the needle, though the method 
 of recoil was also used. For the successful use of the first method a 
 quickly vibrating needle and the damping inductor are indispensable, 
 seeing that with a slow moving needle we can never be certain of its 
 being at rest. By this method it is not necessary to have the needle 
 at rest at the zero point, but, if it vibrates in an arc of only a millimetre 
 or two, we have only to wait till it comes to rest at its point of greatest 
 elongation on either side of the zero point and then reverse the commu- 
 tator. The error by this method is in the direction of making the 
 throw greater in proportion of the cosine of the phase to unity. The 
 smallest throw used was 100 mm. Hence, if the needle vibrated 
 through a total arc of 2 mm., the error would be 1 in 17,000. In reality 
 the needle was always brought to rest much more nearly than this. 
 
 The method of recoil was used once with the needle vibrating in 7-8 
 
ON THE ABSOLUTE UNIT OF ELECTRICAL EESISTANCE 173 
 
 seconds, but the time of vibration was too short and another needle was 
 constructed vibrating in 11-5 seconds, which was a sufficiently long 
 period to be used successfully after practice. 
 
 There seems to be no error introduced by the time taken to reverse 
 the commutator in the method of recoil, seeing that the breaking of 
 the current stops the needle and the making starts it in the opposite 
 direction. As the time was only a fraction of a second the error is 
 minute in any case. 
 
 While the current is broken in the reversal, the battery may re- 
 cuperate a little and there is also some action from the extra current, 
 but there seems to be no doubt that long before the four or six seconds 
 which the needle takes to reach its greatest elongation everything has 
 again settled to its normal condition and the current resumes its 
 original strength. Hence the error from these sources may be con- 
 sidered as vanishingly small. 
 
 Some experiments were made by simply breaking the current and 
 they gave the same result as by reversal. 
 
 The following is the order of observations corresponding to each 
 experiment. 
 
 1st. The time of vibration of needle was observed. 
 
 2d. The current was passed around the circle, F, so as to observe 
 y3 and a. Simultaneous readings were taken at the two galvanometers. 
 The commutator at the tangent galvanometer was then reversed and 
 readings again taken. After that the commutator to the circle was 
 reversed and the operation repeated. This gave four readings for the 
 circle and eight for the tangent galvanometer, as both ends of the 
 needle were read. In some cases these were increased to six and twelve 
 respectively. This operation was repeated three times with currents 
 of different strengths, constituting three observations each of a and /?. 
 To eliminate any action due to the induction coils, they were sometimes 
 connected in one way and sometimes in the opposite way. 
 
 3d. The resistance of the circuit was adjusted equal to the arbitrary 
 standard. 
 
 4th. The circle, F, was thrown out of the circuit and the observations 
 of 6 and d begun. Two throws, d, one on either side of zero were 
 observed and one reading of d taken. The commutators at s and C 
 were then reversed, and the operation repeated. This whole operation 
 was then repeated with currents of three different strengths. The 
 position of the two induction coils was now reversed and observations 
 again made with the three currents. The resistance was now com- 
 
174 HENRY A. ROWLAND 
 
 pared with the standard, the difference noted, and the resistance again 
 adjusted. The observations were completed by turning the induction 
 coils into the two other positions which they could occupy with respect 
 to each other, followed by another comparison of resistance with 
 standard. 
 
 5th. Observations of a and ft were again made as before. 
 
 6th. The time of vibration was again determined. 
 
 The observations as here explained furnished data for three compu- 
 tations of the resistance of the circuit, one with each of the three cur- 
 rents. In each of these three computations, a was the mean of 16 
 readings, ft of 8 or sometimes 12, 6 of 16 and 3 of 16. In using the 
 method of recoil nearly the same order was observed. 
 
 The time of vibration was determined by allowing the needle to 
 vibrate for about ten seconds and making ten observations of transits 
 before and after that period. During the experiment, I usually ob- 
 served at the telescope and Mr. Jacques at the tangent galvanometer. 
 
 The methods of obtaining the corrections require no explanation. 
 
 RESULTS 
 The constant corrections are as follows for the first needle. 
 
 a=-J^+ T ^A= - -00711. 
 
 J = - H = -00020 , 
 
 c = -000006 , 
 
 d = + -000074 at 20' C . 
 
 / = + -00003 , 
 
 a + b + c + d + e +/ '00718. 
 For method of recoil it becomes -00016. 
 Hence for A and B, log JT= 11-4536030 
 Hence for A and 0, log # = 11-2852033 
 Hence for B and C, log #=11-1886619 
 For method of recoil using A and B, log K = 11-4566.630. 
 For second needle and method of recoil, 
 
 a = } f V = - -000050 , 
 
 V * / 
 &=}$= - -00025, 
 
 c = -000006 , 
 d = + -000074 , 
 
ON THE ABSOLUTE UNIT or ELECTRICAL EESIRTANCB 175 
 
 e*Tt<t-ooe><MiT-io w 
 
 t-OOOOOOOOOCOO CO CO7O5OOOOOCOO5SNOO 
 
 COCOCO CO COCOCOCOCOCOCOCOCOCOCOCO 
 
 -^ (Mooascoioaot-co 
 
 Ti'COCO-^COCO^COCOCOCOWCOeOCOCOCOCO'l'COCOCOCOCO 
 
 l-t-ICOOO'*<?O5Ol'- l OaICOCO*-i 
 
176 HENRY A. ROWLAND 
 
 e = + -00003 , 
 / = + '00003 , 
 a + 'b + c + d + e +f= '00017. 
 
 For A and B, log "=11-4566587 
 For A and C, log "=11-2882590 
 For B and C, log " = 11-1917176 
 
 The distance of the mirror from the scale varied between 192-3 and 
 193-5 cm. 
 
 Should we reject the quantity 34-831 in the third experiment so as 
 to make the mean result of that experiment 34-744 instead of 34-773, 
 we should obtain as a mean result of the whole 
 
 34-7156 -0053, 
 
 which has a less probable error than when the above observation is re- 
 tained. The number of plus and minus errors are also more nearly 
 equal and the greatest difference from the mean 1 part in 1100. 
 However the two results do not differ more than 1 part in 10,000. 
 We shall take 
 
 R = 34-719 -007 earth - at 17' C . 
 second. 
 
 as the final result. 
 
 DISCUSSION 
 
 On glancing over the table we see that the number of negative errors 
 greatly exceed the number of positive, but, if we take only the four 
 errors which are greater than 1 part in 5,000, we shall find two of them 
 negative and two positive. 
 
 Combining the results with the different coils we have 
 
 A and B .................... 34-696 -005 
 
 A and C .................... 34-744 -Oil 
 
 B and C .................... 34-716 -007 
 
 Had we no other results to go by, we might suppose that the value of 
 M might not have been found as exactly for these coils as we have 
 supposed them to be. But if we include the preliminary results re- 
 jected on account of the imperfect circle used, we shall find 
 A and B .................... 34-704 -006 
 
 A and C .................... 34-718 -017 
 
 B and C .................... 34-758 -016 
 
 which has the greatest error in an entirely different place. 
 
 From the first series the probable error of each determination of M 
 is 1 in about 2,000. But as this includes the experimental errors which 
 
177 
 
 are about equal to TfrW, the real probable error of M must be about 
 1 part in 2,500. The number of observations is however too small for 
 an exact estimate of the probable errors. 
 
 Taking the results with currents of different strengths, we find 
 For strongest current .................... 34-716 
 
 For medium current ...................... 34-715 
 
 For weakest current ...................... 34-727 
 
 which are almost perfectly accordant. Taking the results from the 
 method of recoil and the ordinary method, we find 
 
 For ordinary method .............. 34-726 -010 
 
 For method of recoil .............. 34-705 -006 
 
 If the probable error is subtracted from the first and added to the 
 second they will very nearly equal each other. Hence the difference is 
 probably accidental. Indeed, by the combination of the results it does 
 not seem possible to find any constant source of error, and therefore 
 the errors should be eliminated by the combination of the results. 
 In the final result 
 
 = 34-7192 -0070 
 
 the probable error, -0070, includes all errors except the ratio of G 
 to G". We may estimate the probable error of G at ^jVff and of G" 
 
 Hence the final probable error of R, including all variables, is 
 or -04 per cent, 
 
 or # = 34-7 19 '015. 
 
 The probable error of the British Association determination was -08 
 per cent, not including the probable error of the constants; and of Kohl- 
 rausch's determination db -33 per cent, including constant errors. 
 
 COMPARISON WITH THE OHM 
 
 The difficulty in obtaining proper standards for comparison has been 
 explained above and I shall have to wait until the arrival of the new 
 standard before making the exact comparison. At present I give the 
 following results, which seem to warrant the rejection of Messrs. Elliott 
 Bros'. 10-ohm standard and to make that of Messrs. Warden, Muirhead 
 and Clark correct. I shall designate the coils by the letter of the firm 
 and by the number of ohms. Experiment gave the following results: 
 
 W (10) = 1-00171 X E (10), experiment of June 8, 1877. 
 
 W (10) = 1-00166 X E (10), experiment of Feb. 23, 1878. 
 
 W (1,000): W (100):: W (10): -999876 E (I), experiment of Febru- 
 ary 23, 1878. 
 12 
 
178 HENRY A. EOWLAND 
 
 Now the greatest source of error in making coils is in passing from 
 the unit to the higher numbers. As the reproduction of single units 
 is a very simple process the single ohm is without much doubt correct, 
 and as the above proportion is correct within one part in 8,000 of what 
 it should be, it seems to point to the great exactness of the standards 
 then used, seeing that the exactness of the proportion could hardly have 
 been accidental. It is also to be noted that Messrs. Warden, Muirhead 
 & Clark's 10-ohm standard agreed more exactly with a set of coils by 
 Messrs. Elliott Bros, than their own unit E (10). 
 
 The resistance of my coil as derived from the different standards is 
 as follows : 
 
 From Elliott Bros, resistance coils 34-979 ohms. 
 
 From Elliott Bros. 10-ohm standard 35-083 ohms. 
 
 From W., M. & C.'s 10-ohm standard 35-024 ohms. 
 
 From W., M. & C.'s 100-ohm standard 35-035 ohms. 
 
 These give for my determination the values of the ohm as follows : 
 
 From Elliott Bros, resistance coils . . .-99257 earth q ^*' 
 
 sec. 
 
 From Elliott Bros. 10-ohm standard -98963 " 
 
 From W., M. & C.'s 10-ohm standard -99129 
 
 From W., M. & C/s 100-ohm standard -99098 
 
 For the reasons given above I accept the mean of the last two results 
 as the value of the ohm. 
 
 To preserve my standard I have made two extra copies of it, the one 
 in German silver and the other in platinum silver alloy. The com- 
 parisons are given below. No. 1 is in German silver and the other in 
 platinum silver alloy. The temperature is 17- C. 
 
 No. 1 1-00034 June, 1877. 
 
 No. 1 1-00029 Feb., 1878. 
 
 No. II -99630 June, 1877. 
 
 No. II -99932 Feb., 1878. 
 
 These are the values of the copies in terms of the original standard 
 
 whose resistance is 34-719 earth quad \ 
 
 sec. 
 
 From these results it would seem that the German silver of which 
 the standard and No. I were composed was perfectly constant in resist- 
 ance. The wire has been in my possession for several years and seems 
 to have reached its constant state. 
 
 The final result of the experiment is 
 
 1 ohm = -9911 earth 
 
 sec. 
 
17 
 
 ON PEOFESSOES AYETON AND PEEEY'S NEW THEOEY OF 
 THE EAETH'S MAGNETISM, WITH A NOTE ON A NEW 
 THEOEY OF THE AUEOEA l 
 
 [Philosophical Magazine, [5], VIII, 102-106, 1879. Proceedings of the Physical Society, 
 
 III, 93-98, 1879] 
 
 Some years ago, while in Berlin, I proved by direct experiment that 
 electric convection produced magnetic action; and I then suggested to 
 Professor Helmholtz that a theory of the earth's magnetism might be 
 based upon the experiment. But upon calculating the potential of 
 the earth required to produce the effect, I found that it was entirely 
 too great to exist without producing violent perturbations in the planet- 
 ary movements, and other violent actions. 
 
 I have lately read Professors Ayrton and Perry's publication of the 
 same theory; and as they seem to have arrived at a result for the 
 potential much less than I did, I have thought it worth while to publish 
 my reasons for the rejection of the theory. 
 
 The first objection to the theory that struck me was, that not only 
 the relative motion but also the absolute motion through space of the 
 earth around the sun might also produce action. And to this end I 
 instituted an experiment as soon as I came home from Berlin. 
 
 I made a condenser of two parallel plates with a magnetic needle 
 enclosed in a minute metal box between them; for I reasoned that, when 
 the plates were charged and were moved forward by the motion of the 
 earth around the sun, they would then act in opposite directions on 
 the enclosed needle, and so cause a deflection when the electrification 
 of the condenser was reversed. On trying the experiment in the most 
 careful manner, there was not the slightest trace of action after all 
 sources of error had been eliminated. 
 
 But the experiment did not satisfy me, as I saw there was some 
 electricity on the metal case surrounding the needle. And so I attacked 
 the problem analytically, and arrived at the curious result that if an 
 electrified system moves forward without rotation through space, the 
 
 1 Read before the Physical Society, June 29th. 
 
180 HENRY A. KOWLAND 
 
 magnetic force at any point is dependent on the electrical force at that 
 same point or, in other words, that all the equipotential surfaces have 
 the same magnetic action. Hence, when we shield a needle from elec- 
 trostatic action, we also shield it from magnetic action. 
 
 This theorem only applies to irrotational motion, and assumes that 
 the elementary law for the magnetic action of electric convection is the 
 same as the most simple elementary law for closed circuits. Hence we 
 see that, provided the earth were uniformly electrified on the exterior 
 of the atmosphere, there would be no magnetic action on the earth's 
 surface due to mere motion of translation through space. 
 
 In calculating the magnetic action due to the rotation, I have taken 
 the most favorable case, and so have assumed the earth to be a sphere 
 of magnetic material of great permeability, ft. It does not seem prob- 
 able that it would make much difference whether the inside sphere 
 rotated or was stationary; or at least the magnetic action would be 
 greatest in the latter case; and hence by considering it stationary we 
 should get the superior limit to the amount of magnetism. 
 
 Let a be the radius of the sphere moving with angular velocity w, 
 and let a be its surface-density in electrostatic measure, and n the ratio 
 of the electromagnetic to the electrostatic unit of electricity. Then the 
 current-function will be 
 
 <p we? I sin Odd = wa? cos . 
 
 n J n 
 
 Hence (Maxwell's ' Treatise/ 672) the magnetic potential inside the 
 sphere is 
 
 8:: ff 
 u = 
 
 and outside the sphere 
 
 = -TT - war cos , 
 o n 
 
 ^ n r 2 
 
 The magnetic force in the interior of the sphere is thus 
 
 F=i* wa. 
 
 n 
 
 or the field is uniform. If the electric potential of the sphere on the 
 electrostatic system is V, we may write 
 
 ^T 
 which is independent of the dimensions of the sphere. 
 
 
AYRTOX AND PEEEY'S THEOEY OF THE EAETH'S MAGNETISM 181 
 
 In this uniform field in the interior of the sphere, let a smaller 
 sphere of radius a! be situated; the potential of its induced magnetiza- 
 tion will he 
 
 ^ 1 ./' C08<? 
 
 Hence the expression for the potential for the space between the two 
 spheres will be 
 
 and outside the electrified sphere it will be 
 
 i *ww r\ I Q 
 
 w \ fi + 2/ r 2 
 
 Let us now take the most favorable case for the production of mag- 
 netism that we can conceive, making a! = a and fj. = ; we then have 
 
 -, 
 
 n r 2 
 
 which is the potential of an elementary magnet of magnetic moment 
 
 ^Va\ 
 n 
 
 But Gauss * has estimated the magnetic moment of the earth to be 
 
 3-3092a 3 . 
 on the millimetre rag. second system. Hence we have 
 
 V= 3-3092 
 w 
 
 for the potential in electrostatic units on the mm. mg. second system. 
 In electromagnetic units it is thus 
 
 V, = 3-3092 ; 
 w 
 
 and hence in volts it is this quantity divided by 10 11 . 
 
 As the earth makes one revolution in 23 56' 4", or in 86164 seconds, 
 we have 
 
 2* 
 
 "86164' 
 and 
 
 n = 299,000,000,000 * millims. per second. 
 
 8 Taylor's Sclent. Mem., vol. ii, p. 225. 
 
 3 From a preliminary calculation of a new determination made with the greatest 
 care, and having a probable error of 1 in 1300. 
 
182 HENRY A. KOWLAND 
 
 Hence the earth must be electrified to a potential of about 
 
 41 X 10 15 volts * 
 
 in order, under the most favorable circumstances, to account for the 
 earth's magnetism. This would be sufficient to produce a spark in 
 atmospheric air of ordinary density of about 
 
 6,000,000 miles! 
 
 Professors Ayrton and Perry have only found the potential 10 8 volts, 
 or 400,000,000 times less than I find it. 
 
 It was this large quantity which caused me to reject the theory; for 
 I saw what an immense effect it would have in planetary perturbations ; 
 and I even imagined to myself the atmosphere flying away, and the 
 lighter bodies on the earth carried away into space by the repulsion. 
 And, doubtless, had not Professors Ayrton and Perry made some mis- 
 take in their calculation by which the force was diminished 16 x 10 16 
 times, they would have feared like results. 
 
 For according to Thomson's formula, the force would be equal to a 
 pressure outwards of 
 
 r- V * 
 ~ 8*a* ' 
 
 which amounts to no less than 
 
 1,800,000 grms. 
 
 per square centimetre! or 10,000 kil. per square inch! Such an electro- 
 static force as this would undoubtedly tear the earth to pieces, and dis- 
 tribute its fragments to the uttermost parts of the universe. If the 
 moon were electrified to a like potential, the force of repulsion would 
 be greater than the gravitation attraction to the earth, and it would 
 fly off through space. 
 
 For these reasons I rejected the theory, and now believe that the 
 magnetism of the earth still remains, as before, one of the great mys- 
 teries of the universe, toward the solution of which we have not yet 
 made the most distant approach. 
 
 4 That this is not too great may be estimated from my Berlin experiment, where a 
 disk moving 5,000,000 times as fast as the earth with a potential of 10,000 volts, 
 produced a magnetic force of T] ^ ffTr of the earth's magnetism, 
 
 5,000,000 x 10,000 x 50,000=2,500,000,000,000,000, 
 
 which is of the same order of magnitude as the quantity calculated, namely 61 x 
 10 15 . It can be seen that this reasoning is correct, because the formulae show that 
 two spheres of unequal size, rotating with equal angular velocity and charged to the 
 same potential, produce the same magnetic force at similar points in the two systems. 
 
AYRTOX AND PERRY'S THEORY OF THE EARTH'S MAGNETISM 183 
 
 In connection with the theory of the earth's magnetism, I had also 
 framed a theory of the Aurora which may still hold. It is that the 
 earth is electrified, and naturally that the electricity resides for the 
 most part on the exterior of the atmosphere and that the air-currents 
 thus carry the electricity toward the poles, where the air descending 
 leaves it and that the condensation so produced is finally relieved 
 by discharge. 
 
 The total effect would thus be to cause a difference of potential be- 
 tween the earth and the upper regions of the air both at the poles and 
 the equator. At the poles the discharge of the aurora takes place in 
 the dry atmosphere. At the equator the electrostatic attraction of the 
 earth for the upper atmospheric layers causes the atmosphere to be in 
 unstable equilibrium. At some spot of least resistance the upper atmos- 
 phere rushes toward the earth, moisture is condensed, and a conductor 
 thus formed on which electricity can collect; and so the whole forms a 
 conducting system by which the electric potential of the upper air and 
 the earth become more nearly equal. This is the phenomenon known 
 as the thunderstorm. 
 
 Hence, were the earth electrified, the electricity would be carried to 
 the higher latitudes by convection, would there discharge to the earth 
 as an aurora, and passing back to the equator would get to the upper 
 regions as a lightning discharge, once more to go on its unending cycle. 
 I leave the details of this theory to the future. 
 
 Baltimore, May 30, 1879. 
 
 Appendix. Since writing the above, Professors Ayrton and Perry's 
 paper has appeared in full ; and I am thus able to point out their error 
 more exactly. Their formula at the foot of page 40G is almost the 
 same as mine; but on page 407, in the fourth equation, the exponent of 
 n should be -f- instead of \, which increases their result by about 
 600,000,000, and makes it practically the same as my own. 
 
 Rotterdam, July 13. 
 
18 
 
 ON THE DIAMAGNETIC CONSTANTS OF BISMUTH AND 
 CALC-SPAK IN ABSOLUTE MEASUKE 
 
 [American Journal of Science [3], XVIII, 360-371, 1879] 
 
 PART I. BY H. A. ROWLAND 
 
 Since my experiments on the magnetic constants of iron, nickel and 
 cobalt, I have sought the means of determining those of some diamag- 
 netic substances, and to that end have described a method in this 
 Journal for May, 1875 (vol. ix, page 357). As Mr. Jacques, Fellow of 
 the University, was willing to take up the experimental portion, I have 
 here worked up the subject more in detail and brought the formulae 
 into practical shape. No experiments have been made on this subject 
 so far, but some rough comparisons with iron have been made by 
 Becquerel, Plucker and Weber. But as iron varies so greatly, and as 
 the methods of experiment are inexact, we cannot be said to know 
 much about the subject. As, however, the relative results of these 
 experiments and those of Faraday can be accepted as reasonably exact 
 for diamagnetic substances and weak paramagnetic ones, it is only 
 necessary to make a determination of one substance such as bismuth, 
 and then the rest can be readily found. But as bismuth is very crys- 
 talline it is necessary to make our formulae general, unless we use bis- 
 muth in a powder, which would introduce error. 
 
 The general method of experiment has been indicated in the paper 
 before referred to, but I may here state that it consists in counting 
 the number of vibrations made by a bar hung in the usual manner 
 between the poles of an electromagnet. The distribution of the mag- 
 netic force in the field being known, we can then calculate the force 
 acting on the body, and the comparison of thi? with the time of vibra- 
 tion gives us the means of determining the constant sought. But I 
 will leave the more exact description to be given by Mr. Jacques in the 
 experimental part. 
 
DlAMAGNETIC CONSTANTS OF BlSMUTH AND CALC-SPAR 185 
 
 EXPLORATION OF FIELD 
 
 The first operation to be performed is to find a formula to express 
 the force of the field at any point, and an experimental means of deter- 
 mining it in absolute measure. The magnet used was one on the 
 method of Euhmkorff, and hence the field was nearly symmetrical 
 around the axis of the two branches, and also with respect to a plane 
 perpendicular to the axis at a point midway between its poles. Should 
 any want of symmetry exist by accident, it will be nearly neutralized 
 in its effect on the final result, seeing that the diamagnetic bar hangs 
 symmetrically. 
 
 The proper expansion of the magnetic potential for this case is 
 therefore a series of zonal spherical harmonics, including only the un- 
 even powers. Hence, if V is the potential, 
 
 V=A l Q t r + A HI Q til i+A w QS + etc., . . . . (1) 
 
 where r is the distance from the centre of symmetry, Q t , Q tit , etc., 
 are the spherical harmonics with respect to the angle between r and 
 the axis, and A t , A ltl , A v , etc., are constants to be found by experi- 
 ment. The only method known of measuring a strong magnetic field 
 with accuracy is by means of induced currents, and in this case I have 
 used a modification of the method of the proof plane as I have described 
 it in this Journal, III, vol. x, p. 14. In the method there described the 
 coil was to be drawn rapidly away from the given point: in the present 
 case the coil was moved along the axis, thus measuring the difference 
 of the field at several points; on then placing it at the centre and 
 drawing it away, the field was measured at that point. The field at 
 the other points "along this axis could then be found by adding the 
 measured difference to this quantity. This method is far more accu- 
 rate than the direct measurement at the different points. 
 
 When a wire is moved in a magnetic field the current induced in it 
 is equal to the change of its potential energy, supposing it to transmit 
 a unit current, divided by the resistance of the circuit. The potential 
 energy of a wire in a magnetic field is (Maxwell's Elec., Art. 410), 
 
 P=I(n- + m:V- + nV 
 
 J \ dx dy dz 
 
 which is simply the surface integral of V over any surface whose edge 
 is in the wire. 
 
 In the present case, take the axis of x in the direction of the axis of 
 the poles and the surface, S, parallel to the plane YZ, and let p be the 
 
186 HENRY A. EOWLAND 
 
 distance in this plane from the centre of the coil we are calculating. 
 Then 
 
 dV ' , ( n 
 - 1 
 
 for a single circle. 
 From(l) 
 
 and /^a--l; r' = - , 
 
 where // = cos (9 , 
 
 p _ 
 
 - 
 
 For a circle of rectangular section we must obtain the mean value of 
 this quantity throughout the section of the coil. 
 
 1 fxo + lr, /po+H 
 
 M=- r I I Pdxdp, 
 
 r lZ t/x lr, t/Po-H 
 
 where X Q and [) are the values of x and f> at the centre of section and 
 27 and c are the width and depth of the groove in which the coil is 
 wound. We can calculate this quantity best by the formula of Maxwell 
 (Electricity, Art. 700), 
 
 Thus we finally find 
 
 M= ^A t {l + T V + } A tll rl Q' tll + i (5, - 3) 
 
 etc. 
 
 It is by aid of this equation that we find the coefficients A t , A lu , 
 etc. in the expansion of the magnetic potential, V. For, let the coil 
 be moved in the field from a position where M has the value M' to 
 where it has the value M " : then if the coil be joined to a galvanometer 
 the current induced will be equal to 
 
 M' - M" 
 R 
 
 where R is the resistance of the circuit. If an earth inductor is in- 
 cluded in the circuit whose integral area is E, when it is reversed the 
 
 2 J-fW 
 current is ^- where H is the component of the earth's magnetism 
 
DlAMAGNETIC CONSTANTS OF BlSMUTH AND CALC-SPAR 187 
 
 perpendicular to the plane of the inductor. The current as measured 
 by the galvanometer in the first case will be C sin \ S (1 -j- /) and in 
 the second C sin D (1 + /), where C is the constant of the galvano- 
 meter and ^ is the logarithmic decrement. 
 Hence 
 
 T[f' _ Tif" 
 
 * 
 
 sm 
 
 In this way we can obtain a series of equations containing A t , A llt , 
 etc., and can thus find these by elimination. 
 
 This completes the exploration, and we have as a result a formula 
 giving the magnetic potential of the field in absolute measure through- 
 out a certain small region in which we can experiment. 
 
 The next process is to consider the action of this field upon any body 
 which we may hang in it. 
 
 CRYSTALLINE BODY IN MAGNETIC FIELD 
 
 Let the body have such feeble magnetic action that the magnetic 
 field is not very much influenced by its presence. In all crystalline 
 substances we know there exist in general three axes at right angles 
 to each other, along which the magnetic induction is in the direction of 
 the magnetic force. Let k 1} Jc 2 and k a be the coefficients of magnetiza- 
 tion in the directions of these axes and let a set of coordinate axes be 
 drawn parallel to these crystalline axes, the coordinates referred to 
 which are designated by x', y' and z', and the magnetic components of 
 the force parallel to which are X', Y' and Z'. 
 
 The energy of the crystalline body will then be 
 
 E = - \fff (k,Z' 2 + Jc, Y n + fc s Z") dx'dy'dz' 
 
 In most cases it is more convenient to refer the equation to axes in 
 some other direction through the crystal. Let these axes be X, Y, Z. 
 Then 
 
 Y , dV dV dV dV 
 X =d^ = ^ a + ^ a + dz a 
 Y' = etc. 
 
188 HENEY A. EOWLAND 
 
 Hence 
 
 Z' - Xa+Ya' 
 
 where a, /?, f ; a!, /3', -f ; and a", /5", /' are the direction cosines of the 
 new axes with reference to the old. 
 We then find 
 
 E= - \fff{ X* (jfcy + JkJP + V) + Y* ( V 2 + V + V 2 ) + Z\k 
 
 + 2YZ 
 
 The most simple and in many respects the most interesting cases 
 are when the crystal has only one optic or magnetic axis. In this 
 
 CclSG $2 ' ' ~ wy 
 
 Hence 
 
 where , a! and a!' are the direction cosines of the magnetic axis with 
 respect to the coordinate axes. 
 
 The first case to consider is that of a mass of crystal in a uniform 
 magnetic field. The magnetic forces which enter the equation are 
 those due to the magnetic action of the body as well as to the field in 
 which the body is placed. In the case of very weak magnetic or 
 diamagnetic bodies the forces are almost entirely those of the field alone. 
 Hence in the case under consideration we may put F = and Z = 0. 
 
 Hence 
 
 and if v is the volume of the body 
 
 As this expression is the same at all points of the field there is no 
 force acting to translate the body from one part of the field to another. 
 The moment of the force tending to increase <p, where <p cos -1 , is 
 
 j pi 
 
 -.- = v X" 1 (k^Tc^ sin <p cos <p . 
 
 By observing the moment of the force which acts on a crystal placed 
 in a uniform magnetic field we can thus find the value of k i k 2 or 
 the difference of the magnetic constant along the axis and at right 
 angles to it. The differences of the constants can also be found in the 
 case of crystals with three axes by a similar process. 
 
 The next case which I shall consider is that of a bar hanging in a 
 
DlAMAGNETIC CONSTANTS OF BlSMUTH AND CALC-SPAR 189 
 
 magnetic field. Let the field be symmetrical around an horizontal axis, 
 and also with reference to a plane perpendicular to that axis at the 
 centre. If the bar is very long with reference to its section and a 
 plane can be passed through it and the axis we must have Z = 0, and 
 the equation becomes 
 
 Let the axis of X coincide with the long axis of the bar, as this will 
 in the end lead to the most simple result, seeing that we have to inte- 
 grate along the length of the bar. 
 
 Let r be the length along the bar from the centre to any point, and 
 let 6 be the angle made by the bar with the axis of symmetry : then 
 
 1 dV 
 
 j>- v _ 
 
 ~~dr ~ 
 
 also let the section of the bar be 
 
 a = dy dz 
 
 and let the axis of the bar pass through the origin from which we have 
 developed the potential in terms of spherical harmonics. We can then 
 write as before 
 
 where Q t , Q ltl , etc., are zonal spherical harmonics with reference to 
 the angle 6, 
 
 from which we have the following: 
 
 X* = A'Q* + SA*,^ + 25^-#f + QA^Q.Q^ 
 
 ^Q&i* + MA ltt A,Q M QS + etc., 
 
 * + ZA.A^Q'ff^ 
 '&i* + ZA^A^&r* + etc.} sin-*, 
 
 The moment of the force tending to increase 6 is 
 
 dE 
 ~W 
 
 whence we may write, 
 
 *i * + *,) + B ((^ - kj '* + h) C (Tc, - 2 ) ' \, 
 
190 HENEY A. EOWLAND 
 
 where d + l V2 7 . a d 
 
 X*ar = sin - 
 
 Y*dr = sin - I Y 2 dr, 
 diJL J_, 
 
 tJ /*+' fi /+' 
 
 C = - ~ I ZXYdr = sin 6 " I ZXYdr, 
 dv J -i a/jLj_, 
 
 where I is half the length of the bar and cosd. 
 
 = U*m0\ A]Q t Q' t + | A* ,#&]* + ^ A'Q.QP + A t A tll ( 
 
 + Q,Q'J P + A t A v (Q'& + Q& ) ^ + V- A UI J T (<?# 
 = U S in0\ A] (QW sin 2 - Q? cos 0) + A] tl ($&' sin 2 9 
 
 - Q'L cos o) -jj- + ^ v (g; $;' sin 2 - c: cos o) .. + ^^ 
 
 + sn tf - ,,, cos ^ - + A,A, ((QW + Q'W sin' o 
 
 -2QW cos^) + A tll A,((Q' tll <?,' + Q'^Q'^ sitf o 
 
 C=+U\A* ((Qff + QV sin 2 e - Q& cos 9) + 3A' tl ((Q 
 
 '^ sin 2 e - Q HI Qf HI cos *)-.+ 5 J 2 ((^ v ^,' - #; 2 ) sin 2 
 
 - cos 
 
 2 
 
 cos 
 
 sn e - 5, V + t J cos o) -. 
 + *Q'<& + 3 sin 2 - 
 
 Where 
 
 Q, =cos0, 
 
 Q M = J (5 cos 3 e 3 cos 0) , 
 
 Q, = i (63 cos 5 70 cos 3 + 15 cos 0) , 
 
 ^; =Y (21 cos 4 0-14 cos 2 + 1), 
 
 <?'/ -o, 
 
 cos 3 7cos0), 
 
 fj. = COS 0. 
 
DlAMAGNETIC CONSTANTS OF BlSMUTH AND CALC-SPAR 191 
 
 
 
 A = 1 sin 0\ ( A] + 1 1 A*,? + -LV/ A * 1 * ZA. A F + Y- AA # 
 - ^ 6 )/' + (- 
 
 = 4 sn - J - 
 
 - m* A ni AJ?) t jf + (if s AIJI _ 
 + -i |s. J /y ^j 6 ) // + (i-W- 5 - ^' ^ 8 - - 
 (7 = -^- 
 
 Or we can write 
 
 A = 41 sin { L>J. + L',u 3 + L" + etc. }, 
 B = U sin e \ MIL + M'ff + etc. \, 
 C = M{N+iy t n + JV'V + etc. }, 
 
 where the values of L, M, etc., are apparent. 
 To sum up we may then write as before 
 
 = - J a\A [(^ - *,) 2 + &,] + 5[(^ - *,) ' 2 + * s ] - C' (&, - *,) '} 
 
 where A, B and (7 are the quantities we have found, a is the cosine of 
 the angle made by the axis of the crystal with the axis of the bar, and a' 
 is the cosine of the angle made by the same axis with a horizontal line 
 at right angles to the bar. 
 The equation 
 
 # = 
 
 gives equilibrium at some angle depending on a and a', and if either of 
 these is zero the angle can be either = or -J-, one of which will be 
 stable and the other unstable according as the body is para- or dia- 
 magnetic. 
 
 For a diamagnetic crystal like bismuth with the axis at right angles 
 to the bar we can put 
 
 n = cos = sin (/> and a = , 
 and we can write 
 
192 HENEY A. EOWLAND 
 
 = J a\4lk (Lfji + L>jf* + etc.) 
 
 &,) a' 2 + k,][M;j. + M'/S + etc.]} 
 or for very small values of // we can write in terms of </> 
 - 2al<>> \lc,L + ((&! - &,) ' 2 + & 2 ) M\. 
 
 If I is the moment of inertia of the bar and t is the time of a single 
 vibration, we may write 
 
 =/-#. 
 
 If we hang up the bar so that a' we have 
 
 and if we hang it up so that a' = %TT we have again 
 
 2a" 
 whence 
 
 7T 2 / 1 
 
 where 
 
 x - ^ - u t A n F + (II ^: /y + v- ^ A) ^- -v/ *,** + -VV/ 
 
 For a cleavage bar of calc spar we must use the general equation. 
 For equilibrium we have 
 
 h {Aa* + Ba' 3 - Caa'\ + k, { A (1 a 2 ) + B (1 - a' 2 ) + Caa' \ = 0, 
 
 which gives us the ratio of Jc 1 to Tc 2 . For this experiment it is best to 
 hang up the bar so that the axis is in the horizontal plane and we 
 should then have 
 
 a 2 = I a' 2 . 
 
 For obtaining another relation it is best to suspend the bar with ' = 
 and we then have the position of stable equilibrium at the point 6 \K 
 which gives 
 
 T?I 
 
 t* 
 
 whence 
 
DlAMAGNETIC CONSTANTS OF BlSMUTH AND CALC-SPAR 193 
 
 these various equations give the complete solution of the problem of 
 finding the various coefficients of magnetization. 
 
 PART II. BY W. W. JACQUES 
 
 In the foregoing part of this paper there have been deduced mathe- 
 matical expressions for the constants He and ~k' both for bismuth and 
 for calc-spar crystals. In these expressions it is necessary to substitute 
 certain quantities obtained by a series of experiments, and it is the 
 purpose of the remaining portion of the paper to describe briefly the 
 way in which these quantities were obtained. 
 
 These experiments are naturally divided into two parts. First, the 
 exploration of the small magnetic field between the two poles of the 
 electromagnet, and second, the determination of the time of swing and 
 certain other constants relating to little bars of the substances experi- 
 mented upon when suspended in this field. 
 
 In order to insure the constancy of the magnetic field, a galvano- 
 meter and variable resistance were inserted in the circuit through 
 which the magnetizing current circulated. This space between the 
 poles of the electromagnet in which the experiments were performed 
 was a little larger than a hen's egg. 
 
 The method of exploring this field was as follows : In the line join- 
 ing the centre of the two poles was placed a little brass rod, along 
 which a very small coil of fine wire was made to slide. To this rod 
 were fixed two little set-screws to regulate the distance through which 
 the coil could be moved. Starting now always from the centre, the 
 coil was moved successively through distances a, & and c, and the cor- 
 responding deflections of a delicate mirror galvanometer contained in 
 the circuit were noted. To each of these deflections was added the 
 deflection due to quickly pulling the coil away from the centre to a 
 distance such that the magnetic potential was negligibly small. Of 
 course, experiments were made on both sides of the centre of the field 
 in order to eliminate any want of symmetry, and the distances through 
 which the coil moved were all carefully measured with a dividing engine. 
 
 In order to reduce the deflections of the galvanometer to absolute 
 13 
 
194 HENRY A. EOWLAND 
 
 measure, an earth inductor was included in the circuit with the little 
 coil and galvanometer and the deflections produced by this were com- 
 pared with those produced by moving the little coil. These deflections 
 were taken between every two observations with the little coil. 
 
 The deflections due to moving the little coil, those due to the earth 
 inductor and that due to pulling the coil away from the centre are 
 given in the following table: 
 
 Distance a. Distance 6. Distance c. 
 
 Coil 4-407 cm. 9-655 cm. 6-363 cm. 
 
 Earth inductor 33-138 cm. 33-137 cm. 33-162 cm. 
 
 Drawing coil away from centre 57-416 cm. 
 
 In order to determine the proper quantities for substitution in the 
 expression for the magnetic potential of the field, it was necessary to 
 measure, besides, the deflections due to the little coil when moved 
 through various distances and those due to the earth inductor. 
 
 The mean radius of the small coil = -3912 cm. 
 
 Number of turns = 83 
 
 Width if coil = -182.4 cm. 
 
 Depth of coil = -1212 cm. 
 
 Integral area of earth inductor = 20716-2 cm. 
 
 Horizontal intensity of earth's magnetism. . . . = -1984cgs. 
 
 The quotient of the mean radius of the coil by the distance moved 
 gave tan d. 
 
 The linear measurements were made with a dividing engine. 
 
 The horizontal intensity of the earth's magnetism was determined 
 by measuring the time of swing of a bar magnet and its effect upon a 
 smaller galvanometer needle. The proper substitution of these quan- 
 tities in the formula given gave the expression in absolute measure 
 for the magnetic potential at any part of the field. 
 
 The remaining part of the experiment and the part that was attended 
 with greatest difficulty, was to prepare little bars of the substances and 
 to determine the times of vibration of these when suspended, first with 
 the axis vertical and then with it horizontal in the magnetic field. 
 Besides this, the dimensions and the moment of inertia of each bar had 
 to be determined, and, in the case of the calc-spar, the angle the bar 
 made with the equatorial line of the poles when in its position of equi- 
 librium, had to be measured. 
 
 Bismuth and calc-spar were the two crystals experimented upon; 
 quite a number of other substances were tried but failed to give good 
 
DlAMAGNETIC CONSTANTS OF BlSMUTH AND CALC-&PAR 195 
 
 results because of the iron contained in them as an impurity. The 
 bars were each about 15 mm. long and about 2 mm. in cross section. 
 The force to be measured being only about -00000001 of that exerted in 
 the case of iron it was necessary to carry out the experiments with the 
 very greatest care. 
 
 In order to obtain bars free from iron, very fine crystals of chemically 
 pure substances were selected and the bars cleaved from them. They 
 were then polished with their various sides parallel to the cleavage 
 planes by rubbing on clean plates of steatite with oil. In order to 
 remove any particles of iron that might have collected upon them 
 during these processes, they were carefully washed with boiling hydro- 
 chloric acid and with distilled water and then wrapped in clean papers, 
 and never touched except after washing the hands with hydrochloric 
 acid and distilled water. 
 
 In order to reduce to a minimum the causes that might interfere 
 with the accurate determination of the times of vibration of these bars 
 the poles of the magnet were encased by a box of glass. From the top 
 of this a tube four feet long extended up toward the ceiling, and inside 
 this was hung a single fibre of silk so small as to be barely visible to 
 the naked eye. The bars were placed in little slings of coarser silk 
 fibre and suspended by this. Outside the glass case was a microscope 
 placed horizontally and having a focus of about six inches. This was 
 directed toward the suspended bar, and when the latter was at rest the 
 cross hairs of the microscope fell upon a little scratch in one end of the 
 bar. Near by was a telegraph sounder arranged to tick seconds. The 
 bar was set swinging through a small arc by making and breaking the 
 current, and the interval between two successive transits of the little 
 scratch on the bar by the cross hairs of the microscope was measured 
 in seconds and tenths of a second by the ear. By keeping count through 
 a large number of successive transits the time of a single swing could 
 be determined with very great accuracy. The bar was caused to swing 
 only through a few degrees of arc and such small correction for ampli- 
 tude as was found necessary was applied. The time of swing was deter- 
 mined first with the axis vertical and then with it horizontal. But 
 besides the time of swing of each bar it was necessary to measure : the 
 length ; area of section; moment of inertia in each position ; and for the 
 calc-spar bar the angle it made with the equatorial plane of the magnet 
 when in its position of equilibrium. This was not necessary in the 
 case of bismuth, because its position of equilibrium lay in the equatorial 
 plane. 
 
196 
 
 HENRY A. ROWLAND 
 
 BISMUTH. 
 
 Time of 
 swing. 
 
 Axis, vertical 7'18 sec. 
 
 Axis, horizontal 5'76 sec. 
 
 Moment of 
 
 Half 
 
 Area of 
 
 inertia. 
 
 length. 
 
 section. 
 
 10976 cgs. 
 10943 cgs. 
 
 7709 cm. 
 
 03778 cm, 
 
 CALC-SPAR. 
 
 Half 
 length. 
 
 Area of 
 section. 
 
 8015cm. -0300cm. 50 30' 
 
 Time of Moment of 
 swing. inertia. 
 
 Axis, vertical 46'35sec. '0303cgs. 
 
 Axis, horizontal 43-39 sec. '0300 cgs. 
 
 The linear measurements were made with a dividing engine, the 
 moments of inertia were calculated from the dimensions of the bars. 
 The angle at which the calc-spar stood was measured by projecting the 
 linear axis on a scale placed at a distance. 
 
 The above quantities being all determined and properly substitutedj 
 the solution of the equations gave for 
 
 Bismuth , . .Tc, = 
 
 Calc-spar 
 
 000 000 012 554 
 000000014324 
 000 000 037 930 
 000000040330 
 
19 
 PRELIMINARY NOTES ON ME. HALL'S RECENT DISCOVERY * 
 
 [Philosophical Magazine [5], IX, 432-434, 1880 ; Proceedings of the Physical Society, IV, 
 10-13, 1880; American Journal of Mathematics, II, 354-356, 1879] 
 
 The recent discovery by Mr. Hall 3 of a new action of magnetism on 
 electric currents opens a wide field for the mathematician, seeing that 
 we must now regard most of the equations which we have hitherto used 
 in electromagnetism as only approximate, and as applying only to some 
 ideal substance which may or may not exist in nature, but which cer- 
 tainly does not include the ordinary metals. But as the effect is very 
 small, probably it will always be treated as a correction to the ordinary 
 equations. 
 
 The facts of the case seem to be as follows, as nearly as they have 
 yet been determined: Whenever a substance transmitting an electric 
 current is placed in a magnetic field, besides the ordinary electromotive 
 force in the medium, we now have another acting at right angles to the 
 current and to the magnetic lines of force. Whether there may not be 
 also an electromotive force in the direction of the current has not yet 
 been determined with accuracy; but it has been proved, within the limits 
 of accuracy of the experiment, that no electromotive force exists in the 
 direction of the lines of magnetic force. This electromotive force in a 
 given medium is proportional to the strength of the current and to 
 the magnetic intensity, and is reversed when either the primary current 
 or the magnetism is reversed. It has also been lately found that the 
 direction is different in iron from what it is in gold or silver. 
 
 To analyze the phenomenon in gold, let us suppose that the line A B 
 represents the original current at the point A, and that B C is the new 
 effect. The magnetic pole is supposed to be either above or below the 
 paper, as the case may be. The line A C will represent the final 
 resultant electromotive force at the point A. The circle with arrow 
 represents the direction in which the current is rotated by the mag- 
 netism. 
 
 1 From the American Journal of Mathematics. Communicated by the Physical 
 Society. 
 
 * Phil. Mag. [5], vol. ix, p. 225. 
 
198 
 
 HENKY A. ROWLAND 
 
 It is seen that all these effects are such as would happen were the 
 electric current to be rotated in a fixed direction with respect to the 
 lines of magnetic force, and to an amount depending only on the mag- 
 netic force and not on the current. This fact seems to point imme- 
 diately to that other very important case of rotation, namely the rota- 
 tion of the plane of polarization of light. For, by Maxwell's theory, 
 light is an electrical phenomenon, and consists of waves of electrical 
 displacement, the currents of displacement being at right angles to the 
 direction of propagation of the light. If the action we are now con- 
 sidering takes place in dielectrics, which point Mr. Hall is now investi- 
 gating, the rotation of the plane of polarization of light is explained. 
 
 I give the following very imperfect theory at this stage of the paper, 
 hoping to finally give a more perfect one either in this paper or a 
 later one. 
 
 North Pole above. 
 
 North Pole below. 
 
 Let $ be the intensity of the magnetic field, and let E be the original 
 electromotive force at any point, and let c be a constant for the given 
 medium. Then the new electromotive force E' will be 
 
 and the final electromotive force will be rotated through an angle which 
 will be very nearly equal to c>. As the wave progresses through the 
 medium, each time it (the electromotive force) is reversed it will be 
 rotated through this angle; so that the total rotation will be this quan- 
 tity multiplied by the number of waves. If ^ is the wave-length in air, 
 and i is the index of refraction, and c is the length of medium, then 
 
 the number of waves will be and the total rotation 
 
 The direction of rotation is the same in diamagnetic and ferromag- 
 netic bodies as we find by experiment, being different in the two; for it 
 
PRELIMINARY NOTES ON MR. HALL'S RECENT DISCOVERY 199 
 
 
 
 is well known that the rotation of the plane of polarization is opposite 
 in the two media, and Mr. Hall now finds his effect to be opposite in 
 the two media. This result I anticipated from this theory of the 
 magnetic rotation of light. 
 
 But the formula makes the rotation inversely proportional to the 
 wave-length, whereas we find it more nearly as the square or cube. 
 This I consider to be a defect due to the imperfect theory ; and it would 
 possibly disappear from the complete dynamical theory. But the for- 
 mula at least makes the rotation increase as the wave-length decreases, 
 which is according to experiment. Should an exact formula be finally 
 obtained, it seems to me that it would constitute a very important link 
 in the proof of Maxwell's theory of light, and, together with a very 
 exact measure of the ratio of the electromagnetic to the electrostatic 
 units of electricity which we made here last year, will raise the theory 
 almost to a demonstrated fact. The determination of the ratio will 
 be published shortly; but I may say here that the final result will not 
 vary much, when all the corrections have been applied, from 299,700,000 
 metres per second; and this is almost exactly the velocity of light. We 
 cannot but lament that the great author of this modern theory of light 
 is not now here to work up this new confirmation of his theory, and 
 that it is left for so much weaker hands. 
 
 But before we can say definitely that this action explains the rota- 
 tion of the plane of polarization of light, the action must be extended 
 to dielectrics, and it must be proved that the lines of electrostatic 
 action are rotated around the lines of force as well as the electric cur- 
 rents. Mr. Hall is about to try an experiment of this nature. 
 
 I am now writing the full mathematical theory of the new action, and 
 hope to there consider the full consequences of the new discovery. 
 
 Addition. I have now worked out the complete theory of the rota- 
 tion of the plane of polarization of light, on the assumption that the 
 displacement currents are rotated as well as the conducted currents. 
 The result is very satisfactory, and makes the rotation proportional to 
 
 ~ , which agrees very perfectly with observation. The amount of rota- 
 tion calculated for gold is also very nearly what is found in some of 
 the substances which rotate the light the least. Hence it seems to me 
 that we have very strong ground for supposing the two phenomena to 
 be the same. 
 
22 
 ON THE EFFICIENCY OF EDISON'S ELECTRIC LIGHT 
 
 BY H. A. ROWLAND AND GEORGE F. BARKER 
 \American Journal of Science, [31, XIX, 337-339, 1880] 
 
 The great interest which is now being felt throughout the civilized 
 world in the success of the various attempts to light houses by elec- 
 tricity, together with the contradictory statements made with respect 
 to Mr. Edison's method, have induced us to attempt a brief examina- 
 tion of the efficiency of his light. We deemed this the more important 
 because most of the information on the subject has not been given to 
 the public in a trustworthy form. We have endeavored to make a 
 brief but conclusive test of the efficiency of the light, that is, the 
 amount of light which could be obtained from one horse power of work 
 given out by the steam engine. For if the light be economical, the 
 minor points, such as making the carbon strips last, can undoubtedly 
 be put into practical shape. 
 
 Three methods of testing the efficiency presented themselves to us. 
 The first was by means of measuring the horse power required to drive 
 the machine, together with the number of lights which it would give. 
 But the dynamometer was not in very wood working order, and it was 
 difficult to determine the number of lights and their photometric 
 power, as they were scattered throughout a long distance, and so this 
 method was abandoned. Another method was by measuring the resist- 
 ance of, and amount of, current passing through a single lamp. But 
 the instruments available for this purpose were very rough, and so 
 this method was abandoned for the third one. This method consisted 
 in putting the lamp under water and observing the total amount of heat 
 generated in the water per minute. For this purpose, a calorimeter, 
 holding about 1^ kil. of water, was made out of very thin copper: the 
 lamp was held firmly in the centre, so that a stirrer could work around 
 it. The temperature was noted on a delicate Baudin thermometer 
 graduated to 0-1 C. 
 
 As the experiment was only meant to give a rough idea of the 
 efficiency within two or three per cent, no correction was made for 
 
ON THE EFFICIENCY OF EDISON'S ELECTRIC LIGHT 
 
 201 
 
 radiation, but the error was avoided as much as possible by having the 
 mean temperature of the calorimeter as near that of the air as possible, 
 and the rise of temperature small. The error would then be much less 
 than one per cent. A small portion of the light escaped through the 
 apertures in the cover, but the amount of energy must have been very 
 minute. 
 
 In order to obtain the amount of light and eliminate all changes of 
 the engine and machine, two lamps of nearly equal power were gener- 
 ally used, one being in the calorimeter while the other was being 
 measured. They were then reversed and the mean of the results taken. 
 The apparatus for measuring the light was one of the ordinary Bunsen 
 instruments used for determining gas-lights, with a single candle at 
 ten inches distance. The candles used were the ordinary standards, 
 burning 120 grains per hour. They were weighed before and after 
 each experiment, but as the amount burned did not vary more than 
 one per cent from 120 grains per hour, no correction was made. 
 
 As the strips of carbonized paper were flat, very much more light 
 was given out in a direction perpendicular to the surface than in the 
 plane of the edge. Two observations were taken of the photometric 
 power, one in a direction perpendicular to the paper, and the other 
 in the direction of the edge, and we are required to obtain the average 
 light from these. If L is the photometric power perpendicular to the 
 paper, and I that of the edge, then the average, I, will evidently be 
 very nearly 
 
 Xo 
 
 COS a sin a d a + I I Sin 2 a d a, 
 
 / 
 
 I 
 
 Ft 
 
 A = J L + p. 
 
 In the paper lamps we found l = 
 The lamps used were as follows: 
 
 nearly; hence x =|L nearly 
 
 No. 
 
 Kind of Carbon. 
 
 Size of Carbon. 
 
 Approximate 
 resistance when cold. 
 
 580 
 
 Paper. 
 
 Large. 
 
 147 ohms. 
 
 201 
 
 n 
 
 it 
 
 147 
 
 850 
 
 it 
 
 Small. 
 
 170 " 
 
 809 
 
 it 
 
 *i 
 
 154 " 
 
 817 
 
 Fibre. 
 
 Large. 
 
 87 
 
 The capacity of the calorimeter was obtained by adding to the capac- 
 ity of the water, the copper of the calorimeter and the glass of the 
 
202 
 
 HENRY A. ROWLAND 
 
 lamp and thermometer. The calorimeter and cover weighed 0-103 
 kil. and the lamps about 0-035 kil. 
 
 First experiment, No. 201 in calorimeter and No. 580 in photometer; 
 capacity of calorimeter = 1-153 + -009 + -007 = 1-169 kil. The 
 temperature rose from 18 -28 C. to 23 -11 C. in five minutes, or l-75 
 F. in one minute. Taking the mechanical equivalent as 775-, which is 
 about right for the degrees of this thermometer, this corresponds to 
 an expenditure of 3486 foot pounds per minute. The photometric 
 power of No. 580 was 17-5 candles maximum, or 13-1 mean, /. 
 
 When the lamps were reversed, the result was 3540 foot pounds for 
 No. 580, and a power of 13-5 or 10-1 candles mean. The mean of 
 these two gives, therefore, a power of 3513 foot pounds per minute for 
 11-6 candles, or 109-0 candles to the horse power. 
 
 To test the change of efficiency when the temperature varied, we 
 tried another experiment with the same pair of lamps, and also used 
 some others where the radiating area was smaller, and, consequently, 
 the temperature had to be higher to give out an equal light. 
 
 We combine the results in the following table, having calculated the 
 number of candles per indicated horse power by taking 70 per cent of 
 the calculated value, thus allowing about 30 per cent for the friction 
 of the engine, and the loss of energy in the magneto-electric machine, 
 heating of wires, etc. As Mr. Edison's machine is undoubtedly one of 
 the most efficient now made, it is believed that this estimate will be 
 found practically correct. The experiment on No. 817 was made by 
 observing the photometric power before and after the calorimeter 
 experiment, as two equal lamps could not be found. As the fibre was 
 round, it gave a nearly equal light in all directions as was found by 
 experiment. 
 
 Lamps used 
 in 
 
 Photometric Power. 
 
 -! 06 
 . c 
 
 i on 
 
 cS <u 
 
 ~:i 
 
 Con 
 
 ST 
 
 "3 53*0 
 
 - - 
 
 |:||^ 
 
 CM I i 
 
 
 
 * 
 
 a 
 5 
 
 
 
 "a It? 
 
 S m 'S 
 
 S ^*^ 
 
 
 
 
 
 
 
 Measured 
 
 
 *$ 
 
 ~a 
 
 P<w 
 
 3^-* i-i 
 
 3-2 oo -3 
 2 o o 
 
 3-2-0^. 
 
 Calori- 
 meter. 
 
 Photo- 
 meter. 
 
 perpen- 
 dicular to 
 paper, L. 
 
 Average, 
 
 A. 
 
 11 
 
 03 c 
 
 g 
 
 CO 3, " 
 
 | 
 03 
 
 fl ^S 
 
 goo'S'S 
 
 gflj 5S =" 
 
 too ao 
 
 iaIS 
 
 be-a ft 
 
 
 
 
 
 O 
 
 P3 
 
 3 
 
 fl 
 
 
 S 
 
 201 
 
 580 
 
 580 
 201 
 
 17-5 
 13-5 
 
 13-1 
 10-1 
 
 2-57 
 
 2.82 
 
 l-75 
 l-62 
 
 3486 
 3540- 
 
 i 109-0 
 
 6-8 
 
 4-8 
 
 580 
 201 
 
 201 
 580 
 
 38-5 
 44-6 
 
 28-9 
 33-5 
 
 2.74 
 2 76 
 
 2 -44 
 2 -29 
 
 5181- 
 
 4898- 
 
 1 204 3 
 
 12-8 
 
 8-9 
 
 850 
 809 
 
 809 
 850 
 
 19-0 
 12-2 
 
 14-3 
 9-2 
 
 2.81 
 2.79 
 
 l-54 
 
 2483- 
 3330- 
 
 i 133-4 
 
 8-3 
 
 5-8 
 
 817 
 
 
 17-2 
 
 2.73 
 
 l-28 
 
 2708- 
 
 209-6 
 
 13-1 
 
 9-2 
 
Ox THE EFFICIENCY OF EDISON'S ELECTRIC LIGHT 203 
 
 The increased efficiency, with rise of temperature, is clearly shown 
 by the table, and there is no reason, provided the carbons can be made 
 to stand, why the number of candles per horse power might not be 
 greatly increased, seeing that the amount which can be obtained from 
 the arc is from 1000 to 1500 candles per horse power. Provided the 
 lamp can be made either cheap enough or durable enough, there is no 
 reasonable doubt of the practical success of the light, but this point 
 will evidently require much further experiment before the light can be 
 pronounced practicable. 
 
 In conclusion, we must thank Mr. Edison for placing his entire 
 establishment at our disposal in order that we might form a just and 
 unbiased estimate of the economy of his light. 
 
27 
 ELECTEIC ABSORPTION OF CRYSTALS 
 
 BY H. A. ROWLAND AND E. L. NICHOLS ' 
 
 [Philosophical Magazine [5], XI, 414-419, 1881; Proceedings of the Physical Society, IV, 
 
 215-221, 1881] 
 
 The theory of electric absorption does not seem to have as yet 
 attracted the general attention which its importance demands; and 
 from the writings of many physicists we should gather the impression 
 that the subject is not thoroughly understood. Nevertheless the sub- 
 ject has been reduced to mathematics; and a more or less complete 
 theory of it has been in existence for many years. Clausius seems to 
 have been the first to give what is now considered the best theory. 
 His memoir, ' On the Mechanical Equivalent of an Electric Discharge/ 
 &c., was read at the Berlin Academy in 1852. 2 In an addition to this 
 memoir in 1866 he shows that a dielectric medium having in. its mass 
 particles imperfectly conducting would have the property of electric 
 absorption. Maxwell, in his ' Electricity,' art. 325, gives this theory 
 in a somewhat different form, and shows that a body composed of layers 
 of different substances would possess the property in question. One 
 of us, in a note in the ' American Journal of Mathematics/ No. 1, 
 1878, put the matter in a somewhat different form, and investigated 
 the conditions for there being no electric absorption. 
 
 All these theories agree in showing that there should be no electric 
 absorption in a perfectly homogeneous medium. A mass of glass can 
 hardly be regarded as homogeneous, seeing that when we keep it 
 melted for a long time a portion separates out in crystals. Glass 
 can thus be roughly regarded as a mass of crystals with their axes in 
 different directions in a medium of a different nature. It should 
 thus have electric absorption. Among all solid bodies, we can select 
 
 1 Communicated by the Physical Society, having been read May 14th, 1881. 
 
 2 1 have obtained my knowledge of this memoir from the French translation, en- 
 titled Tkeorie Mecanique de la Chaleur, par R. Clausius, translated into French by F. 
 Folie: Paris, 1869. The 'Addition' does not appear in the memoir published in 
 Pogg. Ann., vol. Ixxxvi, p. 337, but was added in 1866 to the collection of memoirs. 
 
ELECTRIC ABSORPTION OF CRYSTALS 205 
 
 none which we can regard as perfectly homogeneous along any given 
 line through them, except crystals. The theory would then indicate 
 that crystals should have no electric absorption; and it is the object of 
 this paper to test this point. The theory of both Clausius and Max- 
 well refers only to the case of a condenser made of two parallel planes. 
 In the ' Note ' referred to, one of us has shown that in other forms 
 of condenser there can be electric absorption even in the case of homo- 
 geneous bodies. Hence the problem was to test the electric absorp- 
 tion of a crystal, in the case of an infinite plate of crystal with parallel 
 sides. The considerations with regard to the infinite plate were 
 avoided by using the guard-ring principle of Thomson. 
 
 The crystals which could be obtained in large and perfect plates 
 were quartz and calcite. These were of a rather irregular form, about 
 35 millim. across and 3 millim. thick, and perfectly ground to plane 
 parallel faces. There were two quartz plates cut from the same crystal 
 perpendicular to the axis, and two cleavage-plates of Iceland spar. 
 There were also several specimens of glass ground to the same thickness ; 
 the plates were all perfectly transparent, with polished faces. Exam- 
 ined by polarized light, the quartz plates seemed perfectly homo- 
 geneous at all points except near the edge of one of them. This one 
 showed traces of amethystine structure at that point; and a portion 
 of one edge had a piece of quartz of opposite rotation set in; but the 
 portion which was used in the experiment was apparently perfectly 
 regular in structure. The fact that there are two species of quartz, 
 right- and left-handed, with only a slight change in their crystalline 
 structure, and that, as in amethyst, they often occur together, makes 
 it not improbable that most pieces of right-handed quartz contain 
 some molecules of left-handed quartz, and vice versa. In this case 
 quartz might possess the property of electric absorption to some 
 degree. But Iceland spar should evidently more nearly satisfy the 
 conditions. It is unfortunate that the two pieces of quartz were not 
 cut from different crystals. 
 
 This reasoning was confirmed by the experiments, which showed 
 that the quartz had about one-ninth the absorption of glass; but that 
 the Iceland spar had none whatever, and is thus the first solid so far 
 found having no electric absorption. Some crystals of mica, &c., were 
 tried; but calc spar is the only one which we can say, a priori, is per- 
 
 s [There is a gap in the printed article. On examination of the various plates if 
 the Physical Laboratory of the Johns Hopkins University, some have been found on 
 about 2 mm. thickness, which are probably those used in this research.] 
 
206 HENKY A. EOWLAND 
 
 fectly homogeneous. Thus mica and selenite are so very lamellar in 
 their character, that few specimens ever appear in which the lamina 
 are not more or less separated from one another; and thus they should 
 have electric absorption. 
 
 II 
 
 In the ordinary method of experimenting with the various forms of 
 Leyden jar, there are, besides the residual discharge due to electric 
 absorption in the substance of the insulator, two other sources of a 
 return charge. The surface of the glass being more or less conduct- 
 ing, an electric charge creeps over the surface from the edges of the 
 tinfoil. In discharging the jar in the usual way by a connecting wire, 
 this surface remains charged, and the electricity is gradually con- 
 ducted back to the coatings, and thus recharges them. If, further- 
 more, the coatings be fastened to the glass with shellac or other cement, 
 the return charge may be partly due to it; for we have between the 
 coatings not merely glass, but layers of glass, cement, &c., which the 
 theory shows to give a residual discharge. Besides the coatings are 
 not planes; and hence, as one of us has shown, there may be a return 
 charge, even if the glass gave none between infinite planes. If the 
 plates were merely laid on the glass without cementing, the same 
 result would follow, since the insulator would then consist of air and 
 glass in layers. 
 
 In the present research these were sources of error to be avoided, 
 since the residual discharge due to the insulating plates themselves 
 were to be compared. The condenser-plates were copper disks. These 
 were amalgamated, so that there was a layer of mercury between them 
 and the dielectric, which excluded the air and conducted the electricity 
 directly to the surface of the dielectric : thus the condition of a single 
 substance between the plates was fulfilled. The errors due to the 
 creeping of the charge over the surface of the dielectric and that due 
 to the plates not being infinite were avoided, the first entirely and the 
 second partially, by the use of the guard-ring principle of Sir Win. 
 Thomson. 
 
 Plate IV represents this apparatus. The plate of crystal, c, was 
 placed between two amalgamated plates of copper, a and &, over the 
 upper one of which the guard-ring, d, was carefully fitted; this ring, 
 when down, served to charge and discharge the surface around the 
 plate, a; and so the errors above referred to from the creeping of the 
 charge along the plate, and from the plate not being infinite, were 
 avoided. 
 
PLATE IV. 
 
208 HENEY A. KOWLAND 
 
 The charging battery consisted of six large Leyden jars of nearly a 
 square foot of coated surface each, charged to a small potential. 
 Although accurate instruments were at hand for measuring the poten- 
 tial in absolute measure, it was considered sufficient to use a Harris 
 unit-jar for giving a definite charge; for very accurate measurements 
 were not desired, and the Harris unit-jar was entirely sufficient for the 
 purpose. The return charge was measured by a Thomson quadrant- 
 electrometer of the original well-known form. 
 
 The apparatus shown in Plate IV performs all the necessary opera- 
 tions by a half turn of the handle e. By two half turns of the handle, 
 one forward and the other back, the crystal condenser could be succes- 
 sively charged from the Leyden battery, discharged, the guard-ring 
 raised, the upper plate, a, again insulated, and the connection made 
 with the quadrant-electrometer. 
 
 The copper ring, d, was suspended by three silk threads from the 
 brass disk, /, which in turn could be raised and lowered by the crank, g. 
 A small wire connected the ring with the rod on which was the ball, h. 
 This rod was insulated by the glass tube i, and could revolve about an 
 axis at fc. By the up-and-down motion of the rod the ball came into 
 contact with the ball (Z) connected with the earth, or the ball (ra) con- 
 nected with the battery. When the cranks were in the position shown 
 in the figure, the heavy ball n caused the ball h to rise and press 
 against I; but when / descended, the piece o pressed on the rod and 
 caused h to fall on m. 
 
 Another rod, q, also more than balanced by a ball, r, was insulated by 
 a glass tube, s, and connected with the quadrant-electrometer by a 
 very fine wire. It could also turn around a pivot at t; so that when 
 the ring u rested upon it, it fell on the upper condenser-plate a, and 
 connected with the electrometer; when the weight u was raised by the 
 crank v, the rod rested against f, and so connected the electrometer to 
 the earth, to which the other quadrants were already connected. 
 
 At the beginning of an experiment, the insulating plate to be tested 
 having been placed between the condenser-plates a and &, the handle 
 was brought into such a position that the ring, d, rested on the plate 
 around a. The lengths of the threads between d and f were such that o 
 for this position of the handle did not touch w, and so li remained in 
 connection with the earth; and so d was also connected with the earth, 
 and thus also with &. On now turning the handle further, the ball li 
 descended to the ball m, and thus charged the condenser for any time 
 desired. On now reversing the motion, the following operations took 
 place : 
 
ELECTRIC ABSORPTION OF CRYSTALS 
 
 209 
 
 First, the ball h rose and discharged the condenser. 
 
 Second, the guard-ring d ascended. 
 
 Third, the rod q, which had been previously in contact with p, thus 
 bringing the quadrant-electrometer to zero, now moved down and rested 
 on the upper condenser-plate a. Thus any return charge quickly showed 
 itself on the electrometer. The amount of deflection of the instru- 
 ment depends upon the character of the dielectric, its thickness, the 
 charge of the battery, the time of contact with the battery, and upon 
 the length of time of discharging. 
 
 Ill 
 
 In comparing the glass with the crystal plates, the electrometer was 
 rendered as little sensitive as the ordinary arrangement of the instru- 
 ment without the inductor-plate would allow. The electric absorption 
 of the glass plates for a charge in the battery of two or three sparks 
 from the Harris unit-jar then sufficed, after 20 or 30 seconds contact 
 with the battery and 5 seconds discharging time, to give a deflection of 
 about 200 scale-divisions, which were millimetres. The quartz and 
 calcite plates were then alternately substituted for the glass, the same 
 charge and the same intervals of contact being used, and the resulting 
 deflections noted two plates of each substance of the same thickness 
 being used. 
 
 The results of the measurements are given in the following Tables, 
 the effect of the glass being called 100. 
 
 TABLE I. 
 
 April 12, 1880. 
 
 Charge of battery, 2 sparks. 
 
 Contact, 30 seconds. 
 
 Glass (1st plate) 100-0 
 
 Quartz (1st plate) 17-1 
 
 " (2nd plate). 20-0 
 
 Calcite (1st plate) 0.0 
 
 " (2nd plate) 0-0 
 
 (b) 
 
 April 13, 1880. 
 
 Charge of battery, 3 sparks. 
 
 Contact, 20 seconds. 
 
 Glass (1st plate) 100-0 
 
 Quartz (1st plate) 19-3 
 
 Calcite (1st plate) 0-0 
 
 14 
 
 April 14, 1880. 
 Charge, 3 sparks. 
 Contact, 10 seconds. 
 Plates carefully dried by being in desic- 
 cator over night. 
 
 Glass (1st plate) 100-0 
 
 Quartz (1st plate) 10-7 
 
 Calcite (1st plate) 0-0 
 
 (d) 
 
 April 22, 1880. 
 
 Charge, 2 sparks. 
 
 Contact, 30 seconds. 
 
 Plate in desiccator since April 14. 
 
 Glass (2nd plate) 100-0 
 
 " (1st plate) 96-3 
 
 Quartz (1st plate) 13-4 
 
 " (2nd plate) 12-1 
 
 Calcite (1st plate) 0-0 
 
 " (2nd plate) 0-0 
 
210 
 
 HENKY A. ROWLAND 
 
 TABLE II. 
 
 MAT 1. RELATIVE EFFECTS FOR DIFFERENT INTENSITIES OF CHARGE AND 
 TIME OF CONTACT 
 
 Charge of 
 Battery. 
 
 Material. 
 
 Deflections, in millimetres. 
 
 Contact, 
 5 seconds. 
 
 Contact, 
 10 seconds. 
 
 Contact, 
 30 seconds. 
 
 One spark. . . J 
 
 Glass (1st) 
 Quartz (1st)... 
 Calcite (1st)... 
 
 133-0 
 13-0 
 0-0 
 
 189-3 
 22-7 
 0-0 
 
 225-0 
 34-3 
 0-0 
 
 Two sparks. . J 
 
 Glass (1st) 
 Quartz (1st)... 
 Calcite (1st). . . 
 
 Off the scale 
 24-0 
 0-0 
 
 Off the scale 
 35-0 
 0-0 
 
 Off the scale 
 50-0 
 0-0 
 
 These Tables seem to prove beyond question that calcite in clear 
 crystal has no electric absorption. Quartz seems to have about ^ that of 
 glass; but we have remarked that quartz is not a good substance to test 
 the theory upon. 
 
 Some experiments were made with cleavage-plates of selenite, which 
 are always more or less imperfect, as the laminae are very apt to sepa- 
 rate. These gave, however, effects about -J or ^ those of glass. 
 
 In order to test still further the absence of electric absorption in 
 calcite, the electrometer was rendered very sensitive, and the calcite 
 plates were tested with gradually increasing charges, from that which 
 in glass gave 200 millim. after 1 second contact, up to the maximum 
 charge (ten sparks of the unit-jar) which the condensers were capable 
 of carrying. In these trials, the calcite still showed no effect, even 
 with 30 seconds contact. During these experiments glass was fre- 
 quently substituted for the calcite, to leave no question but that the 
 apparatus was in working order. 
 
 It is to be noted that the relative effects of the quartz and the glass 
 were different for dried plates and plates exposed to the atmosphere. 
 This was possibly due to the glass being a better insulator, and thus 
 retaining its charge better when dry than in its ordinary condition. 
 
 IV 
 
 Thus we have found, for the first time, a solid which has no electric 
 absorption; and it is a body which, above all others, the theory of 
 Clausius and Maxwell would indicate. The small amount of the effect 
 
ELECTRIC ABSORPTION OF CRYSTALS 211 
 
 in quartz and selenite also confirms the theory, provided that we can 
 show that in the given piece of quartz some molecules of right-handed 
 quartz were mixed with the left; for we know that the theoretical con- 
 ditions for the absence of electric absorption are rarely satisfied by 
 laminated substances like selenite or mica. If the theory is con- 
 firmed, the apparatus here described should give the only test we yet 
 have of the perfect homogeneity of insulating bodies; for any optical 
 test cannot penetrate, as this does, to the very structure of the 
 molecule. 
 
28 
 
 [Presented to the Congress of Electricians, Paris, September 17, 1881, and here 
 translated from their Proceedings] 
 
 [Johns Hopkins University Circulars, No. 19, pp. 4, 5, 1882] 
 
 Among the subjects to be discussed by this Congress is that of atmos- 
 pheric electricity, and I should like, at this point, to urge the import- 
 ance of a series of general and accurate experiments performed simul- 
 taneously on a portion of the earth's surface as extended as possible. 
 Here and there on the globe, it is true, an observer has occasionally 
 performed a series of experiments, extending even over several years: 
 but the different observers have not worked in accordance with any pre- 
 concerted plan, it has not been possible to compare their instruments, 
 and even where absolute measurements have been obtained, the exact 
 meaning of the quantity measured has not been perceived. Let us 
 take, for instance, Sir William Thomson's water dropping apparatus, 
 which is used at the Kew Observatory. This apparatus is composed 
 of one tube rising a few feet above the building and of another tube 
 near the ground, so that it is in the angle made by the house and the 
 ground. This apparatus indicates a daily variation in the electricity 
 of the atmosphere, but the result is evidently influenced by the condi- 
 tions of the experiment. Another observer who should fit up an appar- 
 atus in another country might obtain entirely different conditions, so 
 that it would be impossible to compare the results. Hence the neces- 
 sity of having a system. 
 
 The principal aim of scientific investigation is to be able to under- 
 stand more completely the laws of nature, and we generally succeed in 
 doing this by bringing together observation and theory. In science 
 proper, observations and experiments are valuable only in so far as they 
 rest on a theory either in the present or in the 'future. We can as yet 
 present only a plausible theory of atmospheric electricity, but the real 
 way of arriving at the truth in this case is to let ourselves be guided in 
 our future experiments by those which have hitherto been made on 
 this subject. 
 
ON ATMOSPHERIC ELECTEICITY 213 
 
 The principal facts which have been discovered can be stated in a few 
 words. In clear weather, the potential increases as we go higher, at 
 least for certain parts of Europe, and there is a diurnal and annual 
 variation of this quantity which the presence of fogs causes also to vary. 
 The first observers were inclined to attribute the electricity of the 
 atmosphere to the evaporation of water, and an old experiment which 
 consisted in dropping a ball of red-hot platinum into water placed on a 
 gold leaf electrometer, was supposed to confirm this view. Even re- 
 cently a distinguished physicist held this opinion in the case of electric 
 storms. Now when a ball of platinum is thus dropped into water, the 
 excessive commotion thus produced will certainly give rise to electricity; 
 but to assert that this electricity is due to evaporation may very well 
 be an error. It is true that occasionally a red-hot meteorite may fall 
 into the sea, reproducing thus the laboratory experiment; but most of 
 the water is evaporated quietly. Eecently one of my students used 
 under my direction a Thomson quadrant electrometer in order to inves- 
 tigate this question, and although he evaporated large quantities of 
 different liquids, he did not find any trace of electrization. I hope to 
 prove thus conclusively that the electricity of the atmosphere cannot 
 be the result of evaporation. 
 
 Sir William Thomson thinks that the experiments which have been 
 made hitherto indicate that the earth is charged negatively. This con- 
 clusion would certainly explain all the experiments hitherto performed 
 in Europe ; but the only method of reaching certainty on this point is to 
 execute a series of experiments on the whole surface of the globe, and 
 it is this method that I propose to-day. This series of experiments 
 would furnish data for determining not only the fact of terrestrial 
 magnetism, but also by the aid of Gauss's theorem the amount of the 
 charge on the solid portion of the earth; however, this amount cannot 
 be determined for the upper atmosphere. What we want to know is 
 the law according to which the electric potential varies as we ascend 
 on the whole surface of the globe and at the same instant of time, so 
 that it may be possible to obtain the surface integral of the rate of 
 variation of the potential over the whole globe. If the earth were ever 
 to receive an increase of charge coming either from the exterior or from 
 the upper atmosphere, this increase would be known. When, in the 
 London Physical Society, I criticized the theory of Profs. Ayrton and 
 Perry on terrestrial magnetism, I gave at the end of my paper a brief 
 outline of a recent theory on auroras and storms, which was built on 
 the hypothesis of the electrization of the earth. After mature reflec- 
 
214 HENKY A. ROWLAND 
 
 tion I still wish to present to you this theory, which deserves to be 
 thought of in mapping out a system of international experiments on 
 atmospheric electricity. 
 
 Suppose Sir William Thomson's explanation is correct and that the 
 earth is charged with electricity, let us examine what would then 
 happen. If the earth were not exposed to disturbing causes, a portion 
 of the electricity of the globe would discharge itself into the atmosphere 
 and would distribute itself nearly as uniformly as the resistance of the 
 air would allow. The exterior atmosphere thus charged would set itself 
 in motion, and we should have winds produced by the electric repul- 
 sions, and this would last until the electricity had been distributed in a 
 uniform manner on the earth and in the exterior strata of the atmos- 
 phere ; when all would be still once more. An observer stationed on the 
 earth would have no idea of the charge of the exterior atmosphere; but 
 he would discover the charge of the earth by means of the ordinary 
 instruments used in experiments on the electricity of the atmosphere, 
 such as Becquerel's arrows and Thomson's water dropping apparatus. 
 There would be another result which however could not be measured by 
 observers situated on the earth, namely, the extension of the atmos- 
 phere beyond the limits determined by calculation. The rarefied air 
 being electrified would repel itself, and possibly there would be then in 
 the exterior atmosphere a region in which the pressure would vary s T ery 
 slightly for a great difference of elevation. We have learned from 
 auroras and meteors that the atmosphere extends to a much greater 
 distance than that indicated by Newton's logarithmic formula, but I 
 think that what I have said is the first rational explanation of this fact. 
 
 Observe now what would happen if the earth of which we speak were 
 subject to the disturbing causes which exist on our globe; the most 
 important of these disturbing factors are the winds and the general 
 atmospheric circulation. This circulation constantly carries the atmo- 
 sphere from the equator to the two poles, but with very little uni- 
 formity. However, near the poles there must be many points at which 
 the air comes down towards the earth and thus shapes its course towards 
 the equator. Now a body which is a bad conductor, like air, when it is 
 charged tends to carry its charge along with it wherever it goes, and 
 thus the air carries its charge until the moment when it descends 
 towards the earth; then it will leave it behind in the exterior atmo- 
 sphere, in accordance with the tendency of electricity to remain at the 
 surface of charged bodies. The charge will therefore accumulate in the 
 exterior atmosphere, until there is a great tension; the atmosphere 
 
ON ATMOSPHERIC ELECTRICITY 215 
 
 will then discharge itself either towards the earth or through the rare- 
 fied air in the shape of an aurora. At these points the rarefied air 
 probably heaps itself up to a greater height than elsewhere, which 
 would explain the great height at which auroras are sometimes observed. 
 
 The equilibrium which existed previously at the equator would also 
 be destroyed by the absence, at this point, of the primitive charge in 
 the exterior atmosphere, and the earth would have a tendency to dis- 
 charge itself towards the exterior atmosphere. Owing to the difference 
 in the conditions at this point, this tendency will be apt to show itself 
 by the storms which arise oftenest in the equatorial region. Thus the 
 electricity of the earth would tend to circulate in the same way as the 
 air from the equator to the poles and conversely. 
 
 But I do not intend to insist upon this theory here; I wish simply 
 through it to bring out the importance of establishing on the whole 
 surface of the globe a system of general observations on atmospheric 
 electricity. Even if the theory is false, it is only by observation that 
 the truth can be attained. In my opinion, it is almost unworthy of the 
 advanced state of our sciences to-day, that it should be at present impos- 
 sible for us to indicate accurately the origin of the energy which mani- 
 fests itself in auroras and storms. For I have pointed out above that 
 it is necessary to give up explaining these phenomena by the hypothesis 
 of the production of electricity by evaporation. 
 
 I propose therefore that from this section of the Congress a com- 
 mittee be formed to examine what is to be done in order to establish 
 on the whole earth, and especially in the polar regions, a systematic 
 series of observations on atmospheric electricity. 
 
 EDITORIAL NOTE. International Commission of Electricians 
 
 [Professor Rowland sailed from New York, October 14, to attend an 
 international commission of electricians, then about to assemble in 
 Paris. Professor John Trowbridge of Cambridge sailed about the same 
 date. These two gentlemen were selected to represent the United 
 States government by the Department of State Congress having made 
 provision for the appointment of two civilian commissioners. 
 
 This official commission is the outgrowth of the congress of electri- 
 cians which was held a year ago in Paris. That body requested the 
 French government to invite other nations to unite in constituting 
 three international commissions for the study of certain specified 
 problems, namely: 
 
 I. A re-determination of the value of the ohm. 
 
216 HENRY A. ROWLAND 
 
 II. (a) atmospheric electricity. 
 
 (&) protection against damage from telegraphic and telephonic 
 wires (pa ratonn erres) . 
 
 (c) terrestrial currents on telegraphic lines. 
 
 (d) the establishment of an international telemeteorographic 
 
 line. 
 
 III. Determination of a standard of light. 
 
 The study of atmospheric electricity was proposed to the congress by 
 Mr. Rowland. After hearing his paper on this subject, the section to 
 which he belonged adopted on his motion the following resolution which 
 was subsequently approved by the entire congress. 
 
 Resolved that an international commission be charged with determin- 
 ing the precise methods of observation for atmospheric electricity, in 
 order to generalize this study on the surface of the globe. 
 
 As Mr. Eowland did not retain his manuscript, the foregoing trans- 
 lation of the paper as it is printed in the Comptes Rendus of the con- 
 gress has been made b} r Mr. P. B. Marcou and is printed here with the 
 author's consent.] 
 
34 
 THE DETEEMINATION OF THE OHM 
 
 EXTKAIT P'UNE LETTKE DE M. HENKY A. ROWLAND 
 
 [Conference Internationale pour la Determination des Unites Electriques. Proces-Ver- 
 baux, Deuxieme Session, p. 37, Paris, 1884] 
 
 Les experiences relatives a la determination de 1'ohm ont ete pre- 
 parees a Baltimore au moyen d'une partie du credit de 12,500 dollars 
 alloue dans ce but, 1'annee derniere, par le Congres des Etats-Unis. 
 
 Apres une etude preliminaire, les appareils destines a ces exper- 
 iences ont ete mis en construction en juin 1883. Les autorites de 
 1'Universite Johns Hopkins ont bien voulu mettre a ma disposition 
 une construction qui est situee en dehors de la ville, a 1'endroit appele 
 Clifton, et qui a ete transformed en laboratoire. 
 
 La source d'electricite qui servira aux experiences est une pile 
 secondaire du systeme Plante, chargee par une machine dynamo-elec- 
 trique actionnee par une machine a vapeur d'environ 5 chevaux de force. 
 
 Trois methodes au moins seront employees pour la determination 
 de 1'ohm. La premiere repose sur 1'induction mutuelle de deux circuits ; 
 j'ai deja fait usage de cette methode en 1878, mais dans les nouvelles 
 experiences les dimensions des appareils seront considerablement aug- 
 mentees; les bobines auront un metre de diametre. 
 
 La deuxieme methode est basee sur 1'echauffement d'un conducteur 
 par le courant electrique, le meme fil etant echauffe successivement par 
 le courant et par des moyens mecaniques. Les appareils employes 
 seront ceux qui m'ont servi, en 1879, pour determiner 1'equivalent 
 mecanique de la chaleur. Afin d'eviter les pertes, le calorimetre sera 
 rempli d'un liquide non conducteur au lieu d'eau. Pour mesurer 
 1'energie electrique, on a construit un electrodynamometre ayant des 
 bobines d'un metre de diametre. 
 
 La troisieme methode est celle de Lorenz. Pour determiner la 
 vitesse du disque, il sera f-ait usage d'un diapason mu par un mecanisme 
 d'horlogerie, construit par Kb'nig, de Paris. 
 
 La comparison de 1'unite de FAssociation Britannique avec 1'unite 
 mercurielle est pies d'etre terminee; en dehors de cela, aucun resultat 
 
218 HENRY A. EOWLAND 
 
 n'a ete obtenu jusqu'a present, mais je crois pourvoir donner mes re- 
 sultats definitifs en novembre. 
 
 Comme ces experiences seront faites avec les precautions les plus 
 grandes et dans des conditions tres favorables, grace a la generosite du 
 Congres, il est a esperer qu'aucune decision concernant la valeur defi- 
 nitive de 1'ohm ne sera prise avant cette epoque; de cette maniere, les 
 Etats-Unis et d'autres pays pourront accepter 1'etalon arrete. 
 
 HENEY A. KOWLAND. 
 
35 
 
 THE THEOKY OF THE DYNAMO 
 
 [Report of the Electrical Conference at Philadelphia in November, 1884, pp. 72-83, 90, 91, 
 104-107, Washington, 18S6 ; Electrical Review (N. Y.), November 1, 8, 15, 22, 1884] 
 
 I will now proceed with the discussion of ' The Theory of the 
 Dynamo-Electric Machine.' I only claim in the skeleton of the theory 
 which I have here prepared to give a few points which may be of inter- 
 est and possibly of value to those who are constructing these machines. 
 
 The principal losses of the machine I put down under the following 
 heads: (1) Mechanical friction; (2) Foucault currents in the armature; 
 (3) energy of the current used in sustaining the magnet; (4) self-induc- 
 tion of the coils; (o) heating of the armature. 
 
 Of course the efficiency of the machine would be equal to the whole 
 work of the machine minus the different losses divided by the work, 
 namely : , 
 
 JJT w LL efc. 
 
 / 
 
 w 
 
 Thus, when the losses are known, the efficiency of the machine is 
 known. 
 
 The mechanical friction I shall not discuss. 
 
 With respect to Foucault currents in the armature, by dividing up 
 the armature in the proper way, we can get rid of most of these. It is 
 very often effected in the Siemens armature by dividing up the arma- 
 ture into discs. 
 
 I have purposely omitted the loss due to change of magnetism in the 
 armature as the armature revolves. 1 drew attention to this fact sev- 
 eral years ago. It has been recently experimented upon and found 
 that, although there is some heating effect, it is very small indeed. 
 
 With respect to the energy used in sustaining the magnet, if the 
 magnet were of steel there would, of course, be no loss. The only 
 reason for not using a steel magnet is that the field is comparatively 
 weak. The field of a steel magnet is, I suppose, less than one-third of 
 the field due to a good electro-magnet; the two could not be made 
 equal by any possible means. Therefore, in most dynamo machines, 
 the magnet is produced by the current. 
 
220 HENRY A. KOWLAKD 
 
 It is a question what the form of the magnet and the position of 
 these coils should be in order to get the greatest field with the least 
 xpenditure of energy. I have one or two propositions to make on this 
 subject which I think are of some interest. 
 
 The first proposition I have to make is that a round magnet is better 
 than one of elongated cross-section. If the coils are long, and they 
 are usually long enough for the purpose, although the theory assumes 
 an infinite length, the magnetic force at any time acting on a round 
 iron core is exactly the same as on an elongated core. But the area 
 of a circular section is much greater than that of an elongated section 
 of the same circumference, and therefore the same amount of wire 
 which would be used to go around the elongated magnet, would, if 
 extended on a circular section of the same circumference, surround 
 much more iron. 
 
 The principal object of making an elongated magnet is that it may 
 include the whole length of the armature. Most makers who adopt 
 this form think it better to elongate the cross-section than to have a 
 long pole piece. But we have seen that the round form is more efficient 
 in general than the elongated form, and the only question is whether it 
 will be more efficient in this particular case. I shall proceed in this 
 theory upon the known fact that we can consider lines of force as if 
 they were conducted by the iron and the air outside. The conductivity 
 of the iron for the lines of force is very great, much greater than that 
 of air. I experimented on it many years ago, and my idea is that it 
 Varies (according to the degree of magnetization) from several hundred 
 up to 5,000 times that of air. The conductivity for iron is very great, 
 especially for wrought iron; for cast iron it is probably less. Therefore 
 the lines of force will be conducted down through the iron from any 
 point over a circular cross-section very nearly as easily as they are from 
 an elongated cross-section, and the saving in the wire will be con- 
 siderable. 
 
 I have another proposition to make with respect to the magnet, and 
 that is that one circuit of the lines of force is better than a number. 
 There is a loss from having a number of electro-magnets, even if they 
 are round. For this reason, that the same magnetic force is acting in 
 each of these coils provided there is the same number of wires per unit 
 of length; and the same wire will go more times around the same iron 
 concentrated in one magnet than when subdivided into several, and 
 will, therefore, act upon it with more magnetizing force. 
 
 That proposition not only applies to this form of magnet (Fig. 1), 
 
THE THEORY OF THE DYNAMO 
 
 but it also applies to the form where we have the armature revolving 
 between two magnets like this (Fig. 2), because we can turn this lower 
 magnet over and bring the two together. The circuits of the lines of 
 force are around in this direction and in this (arrows, Fig. 2). So that 
 there are two circuits of the lines of force instead of one. The energy 
 expended for a given amount of work will be less with this form (Fig. 1) 
 than with this (Fig. 2). That is of very great value to makers of 
 machines. 
 
 The theorem applies to a number of those old machines where there 
 
 FIG. i. 
 
 Fio. 2. 
 
 was a very large number of little magnets revolving around other little 
 magnets. More work is used in sustaining the magnets in that form 
 of machine than in the more modern form where we have only a few 
 circuits. 
 
 I had a number of drawings made of magnets in the Electrical Exhi- 
 bition, and I find very great difference in this respect; more difference 
 where Siemens armatures are used than in any other kind. In dis- 
 cussing these drawings I do not give any names, nor say whether one 
 machine as a whole is better or worse than another. 
 
 First, I will discuss the general forms of the magnet, and then I wish 
 to say something in respect to the form of the pole pieces that inclose 
 
222 
 
 HENRY A. KOWLAND 
 
 the armature. Of course this form belongs both to the Gramme ring 
 and the Siemens armature. Most modern machines are of this nature, 
 either Gramme or Siemens, and we may consider them both one if 
 we wish. 
 
 We will now proceed with respect to the field in this form of magnet 
 (Fig. 3). The lines of force proceed down the magnet, and are sup- 
 posed to go across here (a &), where wires wound around the revolving 
 armature cut them, and so produce a current. It is evident that any 
 lines which escape across this open space (arrows) are lost. If there 
 
 FIG. a. 
 
 FIG. 4. 
 
 was any leakage of the wire around the magnet, the current, instead of 
 going around the magnet, would go off somewhere else, and we should 
 consider the machine defective because there was a loss of the current. 
 Sq if any of these lines of force, instead of going directly across there 
 (a &), go across the open space (arrows), as they naturally would do, all 
 those lines of force are lost, and we would have to add so much more 
 current in order to make up for this outside loss. I have an illustra- 
 tion of such losses of lines of force from a drawing, which I will give 
 you (Fig. 4). 
 
 This machine has two magnets one above and one below. The lines 
 
THE THEORY OF THE DYNAMO 
 
 223 
 
 of force pass up through here (abed) and then out and around through 
 here (e e), &c., to complete the circuit. As I saw the machine in the 
 exhibition these outside pieces (ee) were closer to the poles of the 
 magnets than I have drawn them. If they are put too near, some lines 
 of force, instead of passing across the field of force, where the wires 
 revolve, as they ought to do, pass off at these openings, the circuits 
 going around in this way (arrows f f). In this case there is a loss due 
 to leakage of the lines of force, and we shall therefore have to expend 
 
 FIG. 5. 
 
 FIG. 6. 
 
 more energy in keeping up the magnet. There is energy expended in 
 keeping up the field outside as well as in keeping up the field through 
 the armature. It is important that this point should be considered. 
 These questions, ' How many lines of force go across this opening and 
 are effective in producing the current, and how many escape off without 
 passing through the opening and are lost?' are just as important as 
 the question of the leakage of the current in the wire. There are 
 defects in many of these machines in that respect. In this form of 
 machine (Fig. 1), where there is a simple circuit, this magnet has to be 
 
224: HENKY A. KOWLAND 
 
 attached somewhere. Very often the magnet is turned vertically, poles 
 downward, and attached to a cast-iron bench. I have no doubt that 
 some lines of force are lost (not much perhaps) in passing across from 
 the magnet to this iron bench. The makers of the machine, I suppose, 
 considered this to some extent, but what is needed is measurement on 
 that point. 
 
 Here is another form of magnet (Fig. 5). That machine would be 
 defective. It has two magnets and two magnetic circuits in the place 
 of one, and many of the lines of force probably make little private cir- 
 cuits of their own around in that way (arrows). Those lines of force 
 are of course lost, and it is more or less defective in that respect. It 
 would be better to diminish the number of magnetic circuits to one. 
 
 (I am only giving a general idea of the principle of these machines, 
 and I do not refer to any in particular.) 
 
 It is also important that these lines of magnetic induction shall find 
 easy passage around in order to produce the most intense field. Thus 
 the opening between the armature and pole pieces must be made as 
 small as possible, in order that the lines of force may find easy passage 
 across it. Everybody recognizes that. Suppose we had a machine made 
 in the following manner (Fig. 6), in which there is a magnet with 
 a Gramme ring here (a), and pole piece here (&), a ring here (c), and 
 pole piece here (d), but no pole pieces opposite these. How are the 
 lines of force to pass around ? I do not know that it would be easy to 
 see how. They evidently go around here (arrows) and get to the other 
 side the best way they can. There is no easy passage around for the 
 lines of force in this case. 
 
 A MEMBER. May they not to some extent follow the shaft ? 
 
 Professor EOWLAND. It is evident that if the shaft is made large 
 enough some go along the shaft in that way (arrows), but there is no 
 easy way for them to get around. 
 
 I have here a formula for the amount of work which one has to 
 expend upon a magnet in order to produce a certain effect. I will take 
 the case which I have considered most efficient, where there is one 
 magnetic circuit. It is an original idea of Faraday that these lines of 
 force are conducted. We suppose the lines of force to pass through 
 the iron and across the opening in this way (arrows, Fig. 1), and they 
 are caused to do that by what may be called the magneto-motive force 
 of the helix. 
 
 I will just obtain an expression for the number of lines of force B. 
 This is not the quantity which Maxwell considers, but it includes the 
 
THE THEORY OF THE DYNAMO 225 
 
 whole number of lines of force which pass through the magnet. We 
 may write B, proportional to N, the number of turns of the wire around 
 the magnet, and C, the current; and inversely proportional to the re- 
 sistance to these lines of force in going around the circuit. The resist- 
 ance to the lines of force is proportional to L, the length of the iron of 
 the system, divided by S, the cross-section of the magnet, supposing it 
 to be uniform, into //, the magnetic permeability of the iron (or the 
 conductivity of the iron for the lines of force). This quantity ft varies 
 with the current, and can readily be obtained. Some years ago I gave 
 a formula for it. It can be expressed simply as dependent upon the 
 magnetization of the iron and a constant depending upon the iron 
 alone. We have something more to add: 
 
 Let I be twice the width of the opening between armature and pole 
 piece, and A the area across which the lines of force flow; then we 
 
 have to add -i and another quantity, which we can call p, which depends 
 
 ^L 
 
 upon the resistance of these lines of force which escape in all direc- 
 tions and represents the loss due to that escapement. Thus we have 
 the final value for the number of lines of force (or rather induction) 
 in the magnet 
 
 NC 
 
 T> 
 
 ti A + p 
 
 This gives us an equation which may be solved with respect to fi. 
 The curve for the magnetic permeability is of this nature (Fig. 7). It 
 will be of a more or less flat form, according to the value of I and p. 
 Therefore, in increasing the magnetic force upon the magnet, it becomes 
 easier and easier to magnetize it until a certain point is reached, and 
 after that it becomes harder and harder. In practice the core should 
 have sufficient cross-section to produce a very strong magnetic field, 
 but not so great as to require too much wire to wind it. The two must 
 be balanced, which can only be done by calculation or, better, by experi- 
 ments on the machine. By examining the force of the magnet at each 
 point, and in that way getting an idea of how these lines of force go, 
 we can see whether the cross-section of the core is large enough to 
 produce all the lines of force necessary for our purpose or not. Of 
 course, in order to have sufficient magneto-motive force to send lines of 
 force across the opening in sufficient quantity, we must have sufficient 
 wire. As the thickness of the coil is increased, we have to use more 
 wire in proportion for a certain diameter of core, which is a disadvan- 
 15 
 
226 
 
 HEXRY A. BOWL AND 
 
 tage, since each coil acts very nearly the same as every other in produc- 
 ing force. But if the core is very short indeed, wire must be piled on 
 it to a very great extent in order to get sufficient magneto-motive force, 
 and as iron is cheaper than copper it might he better to lengthen out 
 the core. I do not know where the lengthening should end, but I 
 should suppose when the requisite wire on the magnet makes a moder- 
 ately thin layer. Of course, as we lengthen out the magnet, the resist- 
 ance of the circuit to magnetization becomes greater; but that is a very 
 small quantity. I do not suppose the increase is very much for a 
 considerable lengthening of the magnet. As I said before, the magnetic 
 conductivity of iron is many times greater than that of air, and we can 
 lengthen out the cores without producing much loss on account of that 
 lengthening. 
 
 Some persons have suggested that there might be a slight gain from 
 
 FIG. 7. 
 
 the fact that iron, after it has been magnetized a great number of times 
 in the same direction, rather likes to be magnetized in the same direc- 
 tion afterwards. If the core is made of any material similar to steel, 
 such as wrought iron or anj'thing of that sort, it might be possible to 
 have some gain from the coercive power of the magnet. There would 
 be loss from that cause at first; but from the continual use of the 
 machine I think it very likely the iron might get a set in the direction 
 of the force. If the core were of steel, for instance, it might be that 
 one could send a strong current through at first and magnetize the steel, 
 and then be able to diminish the current considerably and still keep up 
 a very large magneto-motive force. I do not know how practical that 
 would be, but it seems to me that one could produce a very strong field 
 in that way. In the commencement of the operation of the machine, 
 we would have to send a powerful current to magnetize the steel, and 
 then, without stopping the current, to diminish it. Then the set of 
 
THE THEORY OF THE DYNAMO 
 
 227 
 
 the steel would be in the same direction with the current and produce 
 the field with less expenditure of energy than if it were simply iron. 
 
 There is no difference between a shunt and a series machine. The 
 magnetizing force on the magnet I have set down as proportional to the 
 number of turns multiplied by the current; that is, proportional to the 
 cross-section of the coils multiplied by the current per unit of cross- 
 section, so that the magnetizing action can be the same either from a 
 strong current or a weak current. Therefore, if the exterior dimen- 
 sions of the coils are the same in both cases, the same energy is ex- 
 pended in each in order to produce the same force, so that there is no 
 
 FIG. 8. 
 
 difference between a shunt machine and a series machine as far as the 
 economy of the magnet is concerned. 
 
 I do not wish to take up too much of your time, and will go on to 
 the heating of the armature. Of course the amount of energy expended 
 in the heating of the armature will be dependent on the resistance of 
 the armature. It is well known that the efficiency of the circuit will 
 merely depend upon the relation between the resistance of the arma- 
 ture and the exterior circuit. 
 
 There is one other point in regard to losses ; ' dead wire,' I think, is 
 the technical term for it; I mean that portion of the wire which does 
 not cut the lines of force. In the Gramme pattern the armature is 
 
228 
 
 HEXKY A. EOWLAXD 
 
 inside of the rings. In the Siemens pattern the coils are around the 
 ends of the armature. In a section of the Gramme ring (Fig. 8), the 
 outside portion of the wire (a) is active, since the lines of force follow 
 the core and the outside of the ring around; but the lines of force do 
 not go through the core of the ring, so that the inside portion (6) is 
 dead, so that we can say nearly half the wire is dead wire. In the 
 Siemens armature one cannot see immediately how much dead wire 
 there will be, because it depends upon the length of the armature. The 
 wire is wound around in that way (Fig. 9), and this portion (a a) is 
 active, and this portion (6 &) is dead. If the armature is very thick we 
 would have more dead wire than when it is simply long. I cannot say 
 which has the more dead wire, but I dare say the Gramme has more 
 
 I 1 I I 
 
 J 4_l 
 
 i 1 i 1 i 
 
 FIG. 9. 
 
 than the Siemens. Furthermore, either in the Gramme ring or the 
 Siemens armature (Fig. 10) we have the lines of force running across 
 here (arrows) ; that portion is active ; but these portions (a a) in between 
 the poles are dead, and when the armature revolves we have the lines 
 of force turning around, and I think that would add more dead wire. 
 I believe an attempt has been made to throw out these coils. 
 
 There is no necessity to go further. As I have said, the efficiency of 
 the circuit depends upon the ratio of the resistance of the armature to 
 the resistance of the wires, and therefore, as far as this point is con- 
 cerned, any machine can be made as efficient as one pleases by putting 
 in greater and greater external resistance. But as the magnet remains 
 the same, we would find a point where the efficiency as a whole would 
 not increase for an increase of external resistance, but would actually 
 diminish. There are other things to be taken account of, such as losses 
 
THE THEORY OF THE DYNAMO 
 
 229 
 
 due to the self induction of the coils which produce sparks in them. 
 I have requested Professor Fitzgerald to take up that point, and will 
 leave it for him to consider. 
 
 There is another point with regard to the dynamo which can be 
 treated in this simple manner with no use of the calculus. This is 
 very simple reasoning if you only know the principles. I shall con- 
 sider two machines similar in all respects, except that one is larger than 
 the other, or rather consider one machine, and see what the effect will 
 be when that machine gradually changes in size. 
 
 The point from which we start shall be that the magnetic field is con- 
 stant in the two machines. For, owing to the fact that there is a limit 
 in the magnetization of a magnet, we cannot have a field with more 
 
 FIG. 10. 
 
 than certain strength produced by iron, and I will suppose that the 
 strength is reasonably near that maximum for iron. It cannot be up 
 to the maximum strength, of course, but somewhere near it. I made 
 some experiments many years ago upon an ordinary magnet, the results 
 of which were published in Silliman's Journal, by means of what I call 
 the magnetic proof plane. (Am. J. Sci., vol. 10, 1875, p. 14.) It 
 applies beautifully to dynamo machines, and I obtained everything with 
 it that I have referred to here. If I remember right, I found in that 
 magnet about one-third of the field that an iron magnet could pos- 
 sibly have. 
 
 It is theoretically possible to get a force equal to the magnetizability 
 of the iron, but practically, I suppose that instance is about the case 
 of the ordinary dynamo machine. We start, then, with the supposition 
 that the field of force in the two machines, one of which is larger than 
 
230 HEXEY A. KOWLAKD 
 
 the other, is constant. That is to say, the magnetizing force at any 
 point of one machine is equal to that at a similar point in the other 
 machine. In making a drawing of the machines., it would not matter 
 about the scale of dimensions; the force at a certain point is a certain 
 amount whatever the scale. 
 
 Next consider what must be the current through the wire in the two 
 machines. There are the same numbers of turns of wire around the 
 magnet, and everything is the same except the dimensions. Consider 
 the current passing around the coil of a tangent galvanometer. If the 
 galvanometer grow, in order to produce the same effect at the centre 
 (and not only at the centre but at every point), the current must in- 
 crease in direct proportion to the radius of the coil. When the coil is 
 twice as large the current must be twice as large, in order to produce 
 the same force at every point. Thus, if there is no difference in the 
 material of the two machines, we have their currents in direct propor- 
 tion to their linear dimensions. Make a machine twice as large and 
 the current in the coils must be twice as great to produce the same 
 magneto-motive force. Of course the wire has increased in size; if 
 the machine has increased to twice its original size the cross-section 
 of the wire has increased four times. In other words, from that cause 
 the current per unit of area will vary inversely as the square of I, the 
 linear dimensions; and since we have found the current to vary directly 
 as I, in order to retain the same force in the field, by a combination of 
 the two results, it varies inversely, as I. Therefore, so far as the 
 magnets are concerned, the heating effect, which depends upon the 
 current per unit of cross-section, will decrease with the size, while the 
 surface will increase in proportion to the square of the size. There 
 will, therefore, be less danger of heating in a large magnet than in a 
 small magnet, but this is only with respect to the magnet. 
 
 The resistance of any part of the machine varies, of course, directly 
 as the length of the wire, and inversely as the cross-section. The cross- 
 section varies as Z 2 , so that resistance varies inversely as I. Therefore 
 the larger the machine the less the resistance ; one machine being twice 
 as large as the other, the resistance will be half as great. This applies 
 not only to the work of the magnets, but to the work of the armature. 
 
 I will now consider the electro-motive force. The electro-motive 
 force is proportional to the product of the current and the resistance, 
 or we may write E = RC. We have the current proportional to I, and 
 the resistance inversely proportional to I; therefore the electro-motive 
 force is constant. As we are running the machine, it turns out that 
 
THE THEORY OF THE DYXAMO 231 
 
 the electro-motive force does not vary with the size, but we shall pres- 
 ently see how this is modified so as to get greater electro-motive force 
 for the larger machine. 
 
 The work done is C 2 R in any part of the machine, or in the whole 
 machine, just as you please. This varies directly as I. Therefore the 
 one machine which is twice as large as the other requires twice as much 
 power to run it, and twice as much electrical energy comes out of it. 
 But it is to be remembered that the weight of the machine varies as I s , 
 and we only get work proportional to I out of it. 
 
 So far as results go, we have constructed two machines which differ 
 only in size. The efficiency of these two machines is a constant quan- 
 tity. That will be rather startling to some, who think a large machine 
 is more efficient than a small one. As far as we have gone in any two 
 machines, one of which is simply larger than the other, the efficiency is 
 the same. 
 
 But if we calculate the angular velocity of the armature to keep the 
 proper current we shall find that it varies inversely as the square of the 
 linear dimensions. In other words, in one machine twice as large 
 as another the velocity of the armature must be only one-fourth as 
 great in order to produce the proper current in the wires. This takes 
 account, I think, of every irregularity in the machine. The two 
 machines are exactly the same in every respect. I have not added the 
 loss for the self-induction of the coil. I have an idea that this also 
 should be taken into account, but Mr. Fitzgerald will consider that 
 point. 
 
 ISfow the question comes up, can we increase the velocity of the arma- 
 ture above that point? Is it practically necessary that we should run 
 one machine at one-fourth of the angular velocity if it is twice as large ? 
 It is a practical question; but I should certainly think the velocity was 
 not in that proportion. I should think it would be more nearly in- 
 versely as the size and not inversely as the square of the size. If so, 
 then by so arranging the wire of the armature as to increase the pro- 
 portion of external resistance we can have the same current per unit 
 of section when running the armature faster and the same electro- 
 motive force. If we do that, this whole theory applies; but we shall 
 have increased the external resistance of the machine in comparison 
 with the resistance of the armature, and when we do that we increase 
 the efficiency of the machine. 
 
 I think it is from this cause that we find large machines more efficient 
 than smaller ones; but it is also evident that there is a limit to this, 
 
232 HENRY A. KOWLAND 
 
 which can only be obtained, I suppose, from practically making the 
 machines and seeing how much faster they may be run without flying 
 to pieces. As far as this theory goes, the increase comes not from the 
 size of the machine, but from the fact that we can get a greater electro- 
 motive force with the same angular velocity, and so can reduce the 
 internal resistance in proportion. In very large machines we can make 
 the wire with one turn, not several turns simply bars on the machines. 
 We thus decrease the resistance of the machine, and at the same time, 
 if we run it above this proportion which I have pointed out, we obtain 
 the proper electro-motive force. In other words, the proper electro- 
 motive force is more easily obtained from the large than the small 
 machine, because it is not practically necessary to decrease the velocity 
 so as to keep it inversely as the square of the size. 
 
 [Discussion by Professor Elihu Thomson and others.] 
 
 With respect to Mr. Thomson's remarks, I am very glad to see the 
 matter taken up in this spirit and to have my principles intelligently 
 criticised. However, there was one remark which I wish to state imme- 
 diately as an error, of course, with regard to the steel. Steel can be 
 magnetized to exactly the same degree as soft iron. There is no differ- 
 ence between soft iron and steel in that respect, except that we require 
 an immensely greater force to magnetize steel to the same extent as 
 iron. There are some old papers of mine, which were published in the 
 ' Philosophical Magazine/ I believe, in 1873, relating to experiments 
 where I took iron and steel and several other metals, and showed that 
 the maximum magnetization was the same in all cases. 
 
 But with respect to a number of statements with regard to flat mag- 
 nets and round magnets I am very glad to see my remarks criticised in 
 the manner that they were, because it shows the need of exactly what 
 I stated; and that is experiments upon this subject. The question is 
 one of quantity. My reasoning gave results in one direction, and Mr. 
 Thomson gave reasons for making the magnet in another way, and it is 
 a quantitative question of course as to which is the best; and for that 
 reason I want very much to see experiments made in the manner which 
 I have described by means of this ' magnetic proof plane/ so as to find 
 out what the escape of the lines of magnetic force in all cases is. 
 
 I think we can decide on one point that was brought up without any 
 trouble, and that is with respect to the dynamo made with extended 
 pole piece (Fig. 2), where it was assumed that the lines of force had a 
 
THE THEORY or THE DYNAMO 233 
 
 tendency to go in a particular direction, that it was a sort of gun shoot- 
 ing the lines of force through the armature. That is not true, because 
 they do not have any tendency to go that way at all, and we would only 
 add that much to the area of the end of the magnet. Very few lines of 
 force will go out there, and by putting this additional magnet on we 
 add to the area of the magnet. The lines of force will go out at the 
 sides probably in greater numbers than they would at the end, so that 
 I do not think that particular objection holds in that particular case. 
 It is a question of quantity; the thing should be measured and found 
 out. I see very plainly in my own mind that more lines of force would 
 go out the side by adding this iron here (Fig. 2) than would go out at 
 the end of it by leaving it vacant, as in Fig. 1. But it is a matter of 
 mere opinion. Another reason for having fewer magnets is that the 
 surface is greater in the case of the larger number than of the smaller 
 number for the lines of force to escape from. 
 
 There was another point brought up here with respect to the machine 
 which was made in this way (Fig. 4). It was stated that there was 
 some gain from the magnetic action of this coil on the iron outside. 
 There is undoubtedly a gain: the question is how much, and whether 
 more lines do not escape than would make up for that. With no 
 experiments to go on, it is a case of judgment. My own judgment 
 would be that there would be very little gain ; but, as I said before, the 
 thing should be measured, and then we could find out about that point. 
 
 [Discussion by Professors Sylvanus Thompson and Anthony and 
 others.] 
 
 I am very glad that that point of hollow magnets has been brought 
 up, as I think that the question of hollow magnets, hollow lightning 
 rods, and a great many similar things, causes more difficulty, especially 
 to practical men, than almost anything else. It can be explained in 
 a very few words. Take a hollow bar having the magnetizing coil 
 around it acting to send lines of force along it. They have got to go 
 out to make their complete circuit. They could only end at a certain 
 point if we had free magnetism, that is, a separate magnetic fluid. 
 I speak not from a physical sense but from a mathematical point of 
 view. The principal resistance to the propagation of these lines of 
 force is in the air and not in the magnet. If we take away a large 
 portion of the interior of that magnet we will have the surface the 
 same as it was before, and consequently the external resistances are the 
 
234 HENRY A. EOWLAND 
 
 
 
 same. In such a case as that we leave the magnet about as strong as 
 it was before. But that would not be the case if we compress magnet- 
 ism until we get it up to the point of magnetization of the centre. In 
 that case we should need the whole mass, and it is almost impossible 
 to magnetize to any extent without the centre coming in. It depends 
 on the length of the bar. If we bring the bar around, making a com- 
 plete magnetic circuit of the thing, so that the lines of force do not 
 have to pass out into the air at all when we put a wire around it so as 
 to wind it like a ring at every point, in that case the whole cross-section 
 becomes equally magnetized, if it is not bent too much. If it is a large 
 ring of small cross-section, it is perfectly magnetized across from side 
 to side. We know that perfectly well; it is a result of the law of con- 
 servation of energy. The case of dynamos is like that. We require 
 the whole cross-section to transmit these lines around. The resistance 
 to the magnetization comes partly from this opening and partly from 
 the iron. We have no gain in making these cylinders hollow; indeed 
 we rather increase the outside surface to let lines of force flow into the 
 air. In the case of a dynamo machine, the solid form is not only 
 desirable, but by far the most efficient. 
 
 I have thought of that matter a great deal, and experimented upon 
 it. Indeed this closed circuit is the very idea from which the permea- 
 bility of the iron is determined. All the calculations upon that sub- 
 ject are based upon that law. I think there can be no doubt that in 
 the dynamo the solid form is the proper form, and that the whole cross- 
 section is effective. The whole cross-section of a round piece is just as 
 effective as the whole cross-section of a flat piece. The flat piece ex- 
 poses more surface to the air, and there is more surface for the force 
 to escape from. That is another reason for not making the magnets 
 flat. The round form is that in which there is the least surface, and 
 therefore the least liability of the lines of force to escape. You can 
 conduct the lines of force by a round piece to any point you desire much 
 better than by a flat piece. 
 
 [Discussion by Professor Sylvanus Thompson.] 
 
 I do not know that the theory bears upon the solidity of the core. 
 Of course, the more iron in there the better is the efficiency of the 
 machine. I suppose there would be no objection to dividing that 
 cylinder up into a number, so that the Foucault currents could not 
 exist, if the exterior form was round; but I do have an objection to 
 
THE THEORY OF THE DYNAMO 235 
 
 making it any other shape. Indeed, currents could be more thoroughly 
 eliminated by dividing up the cross-section than by making it of a 
 very elongated form. 
 
 [Discussion by Professor Elihu Thomson.] 
 
 I do not like to rise so often, but I think there is some misapprehen- 
 sion. I have not said anything about large masses of iron. There are 
 the same masses of iron in my method as in any other. The only 
 question is as to making them round or elongated. Of course by 
 dividing this core up it becomes similar to a core of the Euhmkorff 
 coil, and the currents change very rapidly. From Professor Sylvanus 
 Thompson's remarks, I thought that that was desirable. One cannot 
 say that the current is transferred from the core to the wires outside. 
 The same current might take place, and, if the resistances are the 
 same, would take place in the wires outside in both cases. By lengthen- 
 ing the time of action one decreases the electro-motive force or de- 
 creases the external current. If the time is ten minutes one would 
 have one electro-motive force for the external current: if it is five 
 minutes, the electro-motive force would be somewhere near twice as 
 great as before, the whole quantity of electricity passing being the same 
 in both cases. 
 
36 
 
 [Report of the Electrical Conference at Philadelphia in November, 1884, pp. 172-17-t; 
 
 Washington, 1886] 
 
 As this is an important question, especially in some of the Western 
 States, I will say a few words. 
 
 In order to protect buildings from lightning we must have a space 
 into which the lightning cannot come, and have the house situated in 
 that space. What sort of a space do we know in electrical science into 
 which electricity cannot enter from the outside ? It is a closed space 
 I mean a space inclosed by a very good conducting body. All the light- 
 ning in the world might play around a hollow copper globe and it would 
 not affect in the slightest degree anything inside the globe; but the 
 the walls of the vessel need not be solid metal. Of course, if solid, it 
 is all the better ; but if it is made of a net-work of very good conducting 
 material it would protect the inside from lightning strokes. A spark 
 striking on one side of such wire cage would find it easier to go around 
 through the wire of the cage to the other side than it would to go 
 through the centre. This is Maxwell's idea, with reference to protec- 
 tion of houses from lightning, viz., to enclose the house in a rough cage 
 of conducting material. Suppose, for instance, this box is the house, 
 and suppose we start from the roof and run a rod diagonally to each 
 corner and thence down to the earth. We thus make a rough cage. 
 Of course there are openings on the sides; and if we wished to make a 
 better protection we could put rods down the sides wherever we wished. 
 Now, there is ground underneath the house, and the lightning might, 
 by jumping across the centre, find a good conductor through the middle 
 of the house and go down to the earth in that way. How do we prevent 
 that? By running the lightning-rods clear across underneath the 
 house. Then the lightning would find it easier to go around the house 
 than to jump across, even if there were a good conductor through the 
 middle. A house inclosed in a cage of that sort would be perfectly 
 protected, even if it were a powder magazine, or anything of that sort. 
 Of course, in the case of petroleum storage reservoirs, where fumes are 
 given off, there would be danger then, as the stroke might ignite the 
 
ON LIGHTNING PROTECTION 237 
 
 fumes of the petroleum. That would not be the case of a powder 
 magazine. The protection in that case could be made perfect. 
 
 It is not necessary to have lightning-rods insulated. Indeed the 
 question is, can we insulate a lightning-rod ? We may insulate it for a 
 small potential, but lightning coming from a mile or two to strike a 
 house is not going to pay any attention to such an insulator; we may 
 just as well nail the lightning-rod directly to the house as far as that 
 goes. 
 
 The idea of having the lightning-rods inclose the bottom as well as 
 the sides of the house is very important, because we do not know, and 
 we have no right to assume, that the earth is a good conductor. We 
 are perfectly certain if the earth forms a good conductor that then the 
 lightning could go down at the sides into the earth. By inclosing the 
 house in a case both below and above we obviate all that difficulty, and 
 it makes no difference whether the earth is a good conductor or not. 
 
 I am glad of this public opportunity to say something with regard to 
 a peculiar form of lightning-rod; it is in reference to a form of a rod 
 shaped like the letter U. I think the idea is that the lightning strikes 
 on one side, and that it goes down and has inertia and flies up again. 
 The company which advocated this idea had the impudence to bring a 
 lawsuit against a scientific man who said it was a humbug. A company 
 of course can make a great deal of trouble to one man; but when there 
 is such a gross humbug as that around, one would like to undergo the 
 danger of a lawsuit. There is nothing scientific about it; it will endan- 
 ger life in any house in which it is placed. 
 
 Mr. SCOTT. I would like to ask whether a building constructed of 
 iron would not be completely protected from lightning ? 
 
 Professor EOWLAND. Yes, if it has a floor of iron too. If a gas-pipe 
 came up into the centre the lightning might find it easier to go across 
 to the pipe than to go around. But if we made a floor of iron the 
 lightning would find it easier to go around than across to the pipe. It 
 must be an entirely inclosed house. 
 
 Mr. SCOTT. Then would not a petroleum tank entirely constructed 
 of iron with an iron bottom be the safest inclosure possible for petro- 
 leum? 
 
 Professor ROWLAND. The peculiarity of that is that the fumes of 
 petroleum are all the time coming out from the cracks. The whole out- 
 side is probably covered with petroleum. I suppose also the ground is 
 saturated with petroleum. The petroleum as far as the inside goes 
 would be perfectly safe. 
 
238 HENKY A. ROWLAND 
 
 Lieutenant FISKE. I would like to ask how far lightning obeys the 
 ordinary law of currents, whether it takes the path of least resistance 
 or not. Do high potentials always do that? In general across a nar- 
 row space the resistance is greater than going around by the iron, and 
 the question is, to what extent does the lightning obey the law of 
 circuits ? 
 
 Professor ROWLAND. I would like to say one word more with respect 
 to petroleum. In the case of the tank you have a mixture of the petro- 
 leum vapor and air which probably would explode. Unless the tank was 
 a very good conductor there might be also a little spark in the interior, 
 not enough to hurt a man in there; but the smallest spark inside the 
 tank would cause an explosion. I am not certain whether the iron of 
 the tank is a good enough conductor to prevent every trace of spark in 
 the interior. Indeed, suppose we had a tank with a cover upon it. 
 That is supposed to be a closed vessel, yet the lightning would have to 
 pass from top to bottom between the cover and the tank, and perhaps 
 a little spark would take place in the interior; and possibly in going 
 from one of the plates of the iron tank to the other it may find some 
 resistance and jump over some small plate in the interior of the tank. 
 It would be a most difficult thing to protect. 
 
 With regard to that other question, lightning in the air, of course, 
 does not obey Ohm's law; it is entirely a discontinuous anomaly. It is 
 like the breaking of a metal. A piece of metal is supposed to break at 
 a certain strain; but it does not always break then; it pulls out in 
 strings or something of that sort. One cannot measure the distance 
 and say the lightning is going to jump across that distance. 
 
37 
 THE VALUE OF THE OHM 
 
 [La Lumieve filectrique, XXVI, pp. 188, 189, 477, 1887] 
 
 La Yaleur de PTJnite de Besistance de 1'Association Britannique. 
 
 A la derniere reunion de 1' Association britannique, le professeur 
 H. A. Eowland a donne la valeur definitive de 1'unite de resistance 
 electrique de 1'Association, telle qu'elle a ete determined par la com- 
 mission americaine. La valeur donnee en 1876 etait : unite B. A. = 
 0-9878 ohm. 
 
 Dans la derniere determination, on s'est servi des methodes de Kirch- 
 hoff et de celle de Lorenz. 
 
 La premiere a donne une valeur de 0-98646 40 et la seconde 0-9864 
 18; son erreur probable est done de moins de la moitie de celle de la 
 premiere methode. 
 
 Le professeur Eowland a egalement determine la resistance d'une 
 colonne de mercure de 1 mm. 2 de section et de 100 centimetres de lon- 
 gueur, et a trouve 0-95349 unites B. A. 
 
 Valeur de 1'Etalon B. A. de 1'Ohm, d'apres les Mesures de la Com- 
 mission, Americaine, par Eowland. 
 
 Les observations ont ete terminees en 1884 deja, mais les calculs 
 viennent d'etre termines et seront publics prochainement. En 1786: 
 
 Eowland a trouve 1 unite B. A. = 0-9878 ohm. 
 
 Kimball a trouve 1 unite B. J.. = 0-9870 ohm. 
 
 Maintenant Eowland trouve par la methode de Kirchhoff et a 1'aide 
 de 73 observations 
 
 1 unite B. A. = (0-98627 40) ohms 
 
 et Kimball par la methode de Lorenz et au moyen de 43 observations 
 1 unite B. A. = (0-98642 18) ohms. 
 
 En combinant les deux resultats, on trouve que 1'unite mercurielle est 
 egale a 0-95349 unites B. A., c'est-a-dire que 1'ohm de mercure cor- 
 respond a une colonne de mercure de 106-32 cm. 
 
 Eappelons ici les valeurs obtenues par diiferents physiciens et qui se 
 rapprochent le plus du resultat ci-dessus : 
 
240 HENEY A. KOWLAND 
 
 Lord Eayleigh 106-25 cm. 
 
 Glazebrook 106-29 cm. 
 
 Wiedemann 106-19 cm. 
 
 Mascart 106-37 cm. 
 
 Weber . ,.106-16 cm. 
 
38 
 ON A SIMPLE AND CONVENIENT FOEM OF WATER BATTERY 
 
 [American Journal of Science [3], XXXI21, 147, 1887 ; Philosophical Magazine [5], 
 XXIII, 303, 1887 ; Johns Hopkins University Circulars, No. 57, p. 80, 1887] 
 
 For some time I have had in use in my laboratory a most simple, 
 convenient and cheap form of water battery whose design has been in 
 one of my note-books for at least fifteen years. It has proved so useful 
 that I give below a description for the use of other physicists. 
 
 Strips of zinc and copper, each two inches wide, are soldered to- 
 gether along their edges so as to make a combined strip of a little less 
 than four inches wide, allowing for the overlapping. It is then cut 
 by shears into pieces about one-fourth of an inch wide, each composed 
 of half zinc and half copper. 
 
 A plate of glass, very thick and a foot or less square, is heated and 
 coated with shellac about an eighth of an inch thick. The strips of 
 copper and zinc are bent into the shape of the letter IT, with the 
 branches about one-fourth of an inch apart, and are heated and stuck 
 to the shellac in rows, the soldered portion being fixed in the shellac, 
 and the two branches standing up in the air, so that the zinc of one 
 piece comes within one-sixteenth of an inch of the copper of the next 
 one. A row of ten inches long will thus contain about thirty elements. 
 The rows can be about one-eighth of an inch apart and therefore in a 
 space ten inches square nearly 800 elements can be placed. The plate 
 is then warmed carefully so as not to crack and a mixture of beeswax 
 and resin, which melts more easily than shellac, is then poured on the 
 plate to a depth of half an inch to hold the elements in place. A frame 
 of wood is made around the back of the plate with a ring screwed to 
 the centre so that the whole can be hung up with the zinc and copper 
 elements below. 
 
 When required for use, lower so as to dip the tips of the elements 
 into a pan of water and hang up again. The space between the ele- 
 ments being -fa inch, will hold a drop of water which will not evaporate 
 for possibly an hour. Thus the battery is in operation in a minute and 
 is perfectly insulated by the glass and cement. 
 
 This is the form I have used, but the strips might better be soldered 
 face to face along one edge, cut up and then opened. 
 16 
 
40 
 
 ON AN EXPLANATION OF THE ACTION OF A MAGNET ON 
 CHEMICAL ACTION 1 
 
 BY HENRY A. ROWLAND AND Louis BELL 
 
 [American Journal of Science [3], XXXVI, 39-47, 1888; Philosophical Magazine [5]. 
 
 XXVI, 105-114, 1888] 
 
 In the year 1881 Prof. Eemsen discovered that magnetism had a 
 very remarkable action on the deposition of copper from one of its solu- 
 tions on an iron plate, and he published an account in the American 
 Chemical Journal for the year 1881. There were two distinct phe- 
 nomena then described, the deposit of the copper in lines approximat- 
 ing to the equipotential lines of the magnet, and the protection of the 
 iron from chemical action in lines around the edge of the poles. It 
 seemed probable that the first effect was due to currents in the liquid 
 produced by the action of the magnet on the electric currents set up 
 in the liquid by the deposited copper in contact with the iron plate. 
 The theory of the second kind of action was given by one of us, the 
 action being ascribed to the actual attraction of the magnet for the 
 iron and not to the magnetic state of the latter. It is well known 
 since the time of Faraday that a particle of magnetic material in a 
 magnetic field tends to pass from the weaker to the stronger portions 
 of the field, and this is expressed mathematically by stating that the 
 force acting on the particle in any direction is proportional to the rate 
 of variation of the square of the magnetic force in that direction. 
 This rate of variation is greatest near the edges and points of a mag- 
 netic pole, and more work will be required to tear away a particle of 
 iron or steel from such an edge or point than from a hollow. This 
 follows whether the tearing away is done mechanically or chemically. 
 Hence the points and edges of a magnetic pole, either of a permanent 
 or induced magnet, are protected from chemical action. 
 
 One of Prof. Remsen's experiments illustrates this most beautifully. 
 He places pieces of iron wire in a strong magnetic field, with their 
 axes along the lines of force. On attacking them with dilute nitric 
 acid they are eaten away until they assume an hour-glass form, and are 
 
 1 Read at the Manchester meeting of the British Association, September, 1887. 
 
ACTION OF A MAGNET ox CHEMICAL ACTION 243 
 
 furthermore pitted on the ends in a remarkable manner. On Prof. 
 Remsen's signifying that he had abandoned the field for the present, 
 we set to work to illustrate the matter in another manner by means 
 of the electric currents produced from the change in the electrochemical 
 nature of the points and hollows of the iron. 
 
 The first experiments were conducted as follows: Two bits of iron 
 or steel wire about 1 mm. in diameter and 10 mm. long were imbedded 
 side by side in insulating material, and each was attached to an insulated 
 wire. One of them was filed to a sharp point, which was exposed by 
 cutting away a little of the insulation, while the other was laid bare on 
 a portion of the side. The connecting wires were laid to a reflecting 
 galvanometer, and the whole arrangement was placed in a small beaker 
 held closely between the poles of a large electromagnet, the iron wires 
 being in the direction of the lines of force. When there was acid or 
 any other substance acting upon iron in the beaker, there was always a 
 deflection of the galvanometer due to the slightly different action on 
 the two poles. When the magnet was excited the phenomena were 
 various. When dilute nitric acid was placed in the beaker and the 
 magnet excited, there was always a strong throw of the needle at the 
 moment of making circuit, in the same direction as if the sharp pointed 
 pole had been replaced by copper and the other by zinc. This throw 
 did not usually result in a permanent deflection, but the needle slowly 
 returned toward its starting point and nearly always passed it and 
 produced a reversed deflection. This latter effect was disregarded for 
 the time being, and attention was directed to the laws that governed 
 the apparent ' protective throw,' since the reversal was so long delayed 
 as to be quite evidently due to after effects and not to the immediate 
 action of the magnet. 
 
 With nitric acid this throw was always present in greater or less 
 degree, and sometimes remained for some minutes as a temporary 
 deflection, the time varying from this down to a few seconds. The 
 throw was independent of direction of current through the magnet, and 
 apparently varied in amount with the strength of acid and with the 
 amount of deflection due to the original difference between the poles. 
 This latter fact simply means that the effect produced by the magnet 
 is more noticeable as the action on the iron becomes freer. 
 
 When a pair of little plates exposed in the middle were substituted 
 for the wires, or when the exposed point of the latter was filed to a 
 flat surface, the protective throw disappeared, though it is to be noted 
 that the deflection often gradually reversed in direction when the cur- 
 
244 HENRY A. EOWLAND 
 
 rent was sent through the magnet; i. e., only the latter part of the 
 previous phenomenon appeared under these circumstances. 
 
 When the poles, instead of being placed in the field along the lines 
 of force, were held firmly perpendicular to them, the protective throw 
 disappeared completely, though as before there was a slight reverse 
 after-effect. 
 
 Some of Professor Eemsen's experiments on the corrosion of a wire 
 in strong nitric acid were repeated with the same results as he obtained, 
 viz.: the wire was eaten away to the general dumb-bell form, though 
 the protected ends instead of being club-shaped were perceptibly hol- 
 lowed. When the wire thus exposed was filed to a sharp point the 
 extreme point was very perfectly protected, while there was a slight 
 tendency to hollow the sides of the cone, and the remainder of the 
 wire was as in the previous experiments. In both cases the bars were 
 steel and showed near the ends curious corrugations, the metal being 
 left here and there in sharp ridges and points. In one case the cylinder 
 was eaten away on sides and ends so that a ridge of almost knife-like 
 sharpness was left projecting from the periphery of the ends. 
 
 These were the principal phenomena observed with nitric acid. 
 Since this acid is the only one which attacks iron freely in the cold, in 
 Prof. Eemsen's experiment, this was the one to which experiments were 
 in the main confined. With the present method, however, it was pos- 
 sible to trace the effect of the magnet whenever there was the slightest 
 action on the iron, and consequently a large number of substances, some 
 of which hardly produce any action, could be used with not a little facility. 
 
 In thus extending the experiments some difficulties had to be 
 encountered. In many cases the action on the iron was so irregular 
 that it was only after numerous experiments under widely varying 
 conditions that the effect of the magnet could be definitely determined. 
 Frequently the direction of the original action would be reversed in the 
 course of a series of experiments without any apparent cause, but in 
 such case the direction of the effect due to the magnet remained always 
 unchanged, uniformly showing protection of the point so long as the 
 wires remained parallel to the lines of force. When, however, the 
 original action and the magnetic effect coincided in direction, the repe- 
 tition of the latter showed a decided tendency to increase the former. 
 
 When using solutions of various salts more or less freely precipitated 
 by the iron, it frequently happened that the normal protective throw 
 was nearly or quite absent, but showed itself when the magnet circuit 
 was broken as a violent throw in the reverse direction, showing that the 
 combination had been acting like a miniature storage batterv which 
 
ACTION OF A MAGNET ON CHEMICAL ACTION 
 
 245 
 
 promptly discharged itself when the charging was discontinued by 
 breaking the current through the magnet. The gradual reversal of 
 the current some little time after exciting the magnet was noted fre- 
 quently in these cases, as before. Owing to this peculiarity and their 
 generally very irregular action, the various salts were disagreeable sub- 
 stances to experiment with, though as a rule they gave positive results. 
 
 Unless the poles were kept clean experimenting became difficult from 
 the accumulation of decomposition products about them and oxidation 
 of their surfaces. A few experiments showed how easily the original 
 deflection could be modified, nearly annulled or even reversed in direc- 
 tion by slight differences in the condition of the poles. These difficul- 
 ties of the method are, however, more than counterbalanced by its 
 rapidity and delicacy when proper precautions are taken. 
 
 Xearly thirty substances were tested in the manner previously de- 
 scribed; but comparatively few of them gave very decided effects with 
 the magnet, though, as later experiments have shown, the protective 
 action is a general one. The substances first tried were as follows. 
 The table shows the various acids and salts tried, and their effects as 
 shown by the original apparatus: 
 
 Substances. 
 
 Effect due to 
 Magnet. 
 
 Notes. 
 
 Nitric acid 
 
 Sulphuric " 
 
 Hydrochloric acid. 
 
 Acetic 
 
 Formic 
 
 Oxalic 
 
 Tartaric 
 
 Chromic 
 
 Perchloric 
 
 Chloric 
 
 Bromic 
 
 Phosphoric 
 
 Permanganic 
 
 Chlorine water 
 
 Bromine (l 
 
 Iodine " 
 
 Copper sulphate 
 
 " nitrate 
 
 " acetate 
 
 " chloride 
 
 " tartrate 
 
 Mercuric bromide 
 
 " chloride 
 
 Mercurous nitrate 
 
 Ferric chloride 
 
 Silver nitrate 
 
 Platinum tetrachloride. 
 
 Strong. 
 
 Little or none. 
 n 
 
 None. 
 
 Some effect. 
 K 
 
 None. 
 
 Slight effect. 
 Decided " 
 
 Some. 
 
 Slight. 
 Some. 
 
 Decided. 
 Some. 
 
 Always powerful protective throw. 
 Does not act very readily on the iron. 
 
 Sometimes quite distinct throw, irregular. 
 Much less marked than with chromic. 
 
 Hardly any effect on iron. 
 More than with perchloric. 
 
 Mainly showing as throw, on breaking. 
 
 Throw, on breaking. 
 
 Very slight solution, weak. 
 
 Mainly as throw on breaking, [breaking. 
 
 Both protective throw, and sometimes on 
 
 Action very irregular. 
 
246 HEXKY A. EOWLAND 
 
 Several things are worthy of note in this 'list. In the first place 
 those solutions of metallic salts which are precipitated by iron all show 
 distinct signs of protective action when the current is passed through 
 the magnet. Of the various acids this is not generally true ; only those 
 show the magnetic effect, which act on iron without the evolution of 
 hydrogen, and are powerful oxidizing agents. In general, substances 
 which acted without the evolution of hydrogen gave an effect with the 
 magnet. 
 
 From these experiments it was quite evident that the protective 
 action, whatever its cause, was more general than at first appeared and 
 steps were next taken to extend it to the other magnetic metals. Small 
 bars were made of nickel and cobalt and tried in the same manner as 
 before. These metals are acted on but very slightly by most acids, and 
 the range of substances which could be used was therefore very small, 
 but all the substances which gave the magnetic effects with iron poles 
 gave a precisely similar, though much smaller effect, whenever they 
 were capable of acting at all on the nickel and cobalt. This was notably 
 the case with nitric acid, bromine water, chlorine water, and platinum 
 tetrachloride, which were the substances acting readily on the metals in 
 question. Even with these powerful agents, however, the magnetic 
 action was very much less than with iron, and experimentation on 
 metals even more weakly magnetic was evidently hopeless. 
 
 As a preliminary step toward ascertaining the cause* of the magnetic 
 action and its non-appearance where the active substance evolved hydro- 
 gen, it now became necessary to discover and if possible eliminate the 
 cause of the reversal of the current which regularly followed the protec- 
 tive throw. Experiments soon showed that it could not be ascribed to 
 accumulation of decomposition products around the electrodes, and 
 polarization, while it could readily neutralize the original deflection, 
 could not reverse its direction. Whatever the cause, it was one which 
 did not act with any great regularity, and it was soon found that stirring 
 the liquid while the magnet was on, uniformly produced the effect ob- 
 served. Since one pole was simply exposed over a small portion of its 
 side while the other had a sharp projecting point, it was the latter which 
 was most freely attacked when there were currents in the liquid, whether 
 these were stirred up artificially or were produced by the change in gal- 
 vanic action due to the presence of the magnet. AVhen the poles were 
 placed in fine sand saturated with acid this reversing action was much 
 diminished, and in fact anything which tended to hinder free circulation 
 of the liquid produced the same effect. Several materials were tried and 
 
.Acxiox OF A MAGNET ox CHEMICAL ACTION 247 
 
 of these the most successful was an acidulated gelatine which was 
 allowed to harden around the poles. In this case the protective throw 
 was not nearly as large as in the free acid, since the electrodes tended 
 to become polarized while the gelatine was hardening, and only weakly 
 acid gelatine would harden at all; but the reversing action completely 
 disappeared, so that, when the magnet was put on, a permanent deflec- 
 tion was produced instead of a transitory throw. 
 
 This point being cleared up attention was next turned to the negative 
 results obtained with acids which attack iron with evolution of hydro- 
 gen. The galvanometer was made much more sensitive and removed 
 from any possible disturbing action due to the magnet; and with these 
 precautions the original experiments were repeated, it seeming probable 
 that even if the magnetic effect were virtually annulled by the hydrogen 
 evolved, some residual effect might be observed. 
 
 This residual effect was soon detected, first with hydrobromic acid, 
 and then with hydrochloric, hydriodic, sulphuric and others. The 
 strongest observed effect was with hydriodic acid, but as this may pos- 
 sibly have contained traces of free iodine it may be regarded as some- 
 what doubtful. The effect in all these cases was very small, and though 
 now and then suspected in the previous work, could not have been 
 definitely determined, much less measured. 
 
 Some rough measurements were made on the electromotive forces 
 involved in this class of phenomena by getting the throw of the galvano- 
 meter for various small known values of the E. M. F. The values found 
 varied greatly, ranging from less than 0-0001 volt in case of the acids 
 evolving hydrogen, up to 0-02 or 0-03 volts with nitric acid and certain 
 salts. These were the changes produced by the magnet, while the 
 initial electromotive forces normally existing between the poles would 
 be, roughly speaking, from 0-0001 to nearly 0-05 volts, never disappear- 
 ing and rarely reaching the latter figure. 
 
 From these experiments it therefore appears that the protective 
 action of the magnetic field is general, extending to all substances which 
 act chemically on the magnetic metals. While this is so, the strongest 
 effect is obtained with those substances which act without the evolution 
 of hydrogen. But the series is really quite continuous, perchloric acid 
 for instance producing but little more effect than hydrobromic, while 
 this in turn differs less from perchloric than from an acid like acetic. 
 It seems probable that the action of the hydrogen evolved is partially 
 to shield the pole at which it is evolved, and lessen the difference be- 
 tween the poles produced by the magnet. It probably acts merely 
 
248 HENRY A. BOWLAND 
 
 mechanically, for it is to be noted that those acids which evolve a gas 
 other than hydrogen (perchloric acid, for instance), which is not ab- 
 sorbed by the water, tend to produce little magnetic effect compared 
 with those which act without the evolution of any gas. 
 
 As to the actual cause of the protective action exercised by the mag- 
 netic field, all these experiments go to show that it is quite independent 
 of the substance acting, with the exception above noted, and is probably 
 due to the attractive action of the magnet on the magnetic metals 
 forming the poles subjected to chemical action, as we have before 
 explained. 
 
 In the first place, whenever iron is acted upon chemically in a mag- 
 netic field those portions of it about which the magnetic force varies 
 most rapidly are very noticeably protected, and this protection as nearly 
 as can be judged varies very nearly with the above quantity. Wherever 
 there is a point there is almost complete protection, and wherever there 
 is a flat surface, no matter in how strong a field, it is attacked freely. 
 Whenever in the course of the action there is a point formed, the above 
 condition is satisfied and protection at once appears. Thus, in the 
 steel bars experimented on, whenever the acid reached a spot slightly 
 harder than the surrounding portions it produced a little elevation from 
 which the lines of force diverged, and still further shielding it produced 
 a ridge or point, sharp as if cut with a minute chisel. Mckel and 
 cobalt tend to act like iron, though they are attacked with such diffi- 
 culty that the phenomena are much less strongly marked. With the 
 non-magnetic metals they are completely absent. Now, turning to the 
 experiments with the wires connected with a galvanometer, the same 
 facts appear in a slightly different form. 
 
 When the poles were placed perpendicular to the lines of force instead 
 of parallel to them, the magnet produced no effect whatever, showing, 
 first, that the effect previously observed depended not merely on the 
 existence of magnetic force but on its relation to the poles, and, sec- 
 ondly, that when the poles were so placed as to produce little deflection 
 of the lines of force the protective effect disappeared. 
 
 When the pointed pole was blunted the effect practically disappeared, 
 the poles remaining parallel to the lines of force, and when plates were 
 substituted for the wires no effect was produced in any position, show- 
 ing that the phenomena were not due to the directions of magnetization 
 but to the nature of the field at the exposed points. In short, whatever 
 the shape or arrangement of the exposed surfaces, if at any point or 
 points the rate of variation of the square of the magnetic force is 
 
ACTION OF A MAGNET ox CHEMICAL ACTION 249 
 
 greater than elsewhere, such points will be protected, while if the force 
 is sensibly constant over the surfaces exposed there will be no protection 
 at any point. With all the forms of experimentation tried this law 
 held without exception. It therefore appears that the particles of 
 magnetic material on which the chemical action could take place are 
 governed by the general law of magnetic attraction and are held in 
 place against chemical energy precisely as they would be held against 
 purely mechanical force. To sum up: 
 
 When the magnetic metals are exposed to chemical action in a 
 magnetic field such action is decreased or arrested at any points where 
 the rate of variation of the square of the magnetic force tends toward 
 a maximum. 
 
 It is quite clear that the above law expresses the facts thus far 
 obtained, and while in any given case the action of the magnet is often 
 complicated by subsidiary effects due to currents or by-products, the 
 mechanical laws of motion of particles in a magnetic field hold here as 
 elsewhere and cause the chemical action to be confined to those points 
 where the magnetic force is comparatively uniform. 
 
 The effect of currents set up in the liquid during the action of the 
 magnet cannot be disregarded especially in such experiments as those 
 of Xichols (this Journal, xxxi, 272, 1886) where the material acted on 
 was powdered iron and the disturbances produced by the magnet would 
 be particularly potent. The recent experiments of Colardeau (Journal 
 de Physique, March, 1887) while perhaps neglecting the question of 
 direct protection of the poles, have furnished additional proof of the 
 purely mechanical action of the magnet by reproducing some of the 
 characteristic phenomena where chemical action was eliminated and 
 the only forces acting were the ordinary magnetic attractions. 
 
 An attempt was made to reverse the magnetic action, i. e. to deposit 
 iron in a magnetic field and increase its deposition where there was a 
 sharp pole immediately behind the plate on which the iron was being 
 deposited. This attempt failed. The action was very irregular and the 
 results not decisive. The question of stirring effect was also examined. 
 Usually stirring the liquid about one pole increased the action on that 
 pole, but sometimes produced little effect or even decreased it. This 
 however is in entire agreement with the irregular action sometimes 
 observed in the case of the after-effect in the original experiments. 
 
 An excellent method of experiment is to imbed an iron point in wax 
 leaving the minute point exposed: imbed a flat plate also in wax and 
 expose a point in its centre. Place the point opposite to the plate, but 
 
250 HENRY A. EOWLAND 
 
 not too near and place in the liquid between the poles of a magnet and 
 attach to the galvanometer as before. 
 
 There is a wide field for experiment in the direction indicated above, 
 for it is certainly very curious that the effect varies so much. If hydro- 
 gen were as magnetic as iron, of course acids which liberated it would 
 have no action. But it is useless to theorize blindly without further 
 experiment; and we are drawn off by other fields of research. 
 
 In this Journal for 1886, (1. c.) Professor E. L. Nichols has investi- 
 gated the action of acids on iron in a magnetic field. He remarks that 
 the dissolving of iron in a magnetic field is the same as removing it to 
 an infinite distance and hence the amount of heat generated by the 
 reaction should differ when this takes place within or without the 
 magnetic field. Had he calculated this amount of heat due to the 
 work of withdrawing it from the field, he would probably have found 
 his method of experiment entirely too rough to show the difference, for 
 it must be very small. He has not given the data, however, for us to 
 make the calculation. The results of the experiments were inconclu- 
 sive as to whether there was greater or less heat generated in the field 
 than without. 
 
 In the same Journal for December, 1887, he describes experiments 
 on the action of the magnet on the passive state of iron in the magnetic 
 field. In a note to this paper and in another paper in this Journal for 
 April, 1888, he describes an experiment similar to the one in this paper 
 but without our theory with regard to the action of points. Indeed 
 he states that the ends of his bars acted like zinc, while the middle was 
 like platinum, a conclusion directly opposite to ours. The reason of this 
 difference has been shown in this paper to be probably due to the cur- 
 rents set up in the liquid by the reaction of the magnet and the electric 
 currents in the liquid. 
 
 In conclusion we may remark that our results differ from Professor 
 Nichols in this: First, we have given the exact mathematical theory 
 of the action and have confirmed it by our experiments, having studied 
 and avoided many sources of error, while Professor Nichols gives no 
 theory and does not notice the action of points. Secondly, our experi- 
 ments give a protective action to the points and ends of bars, while 
 Professor Nichols thinks the reverse holds and that these are more 
 easily dissolved than unmagnetized iron. 
 
43 
 
 ON THE ELECTROMAGNETIC EFFECT OF CONVECTION- 
 CURRENTS 
 
 BY HENRY A. ROWLAND AND CABY T. HUTCHINSOX 
 [Philosophical Magazine [5], XXVII, 445-460, 1889] 
 
 The first to mention the probable existence of an effect of this kind 
 was Faraday/ who says : " If a ball be electrified positively in the 
 middle of a room and then be moved in any direction, effects will be 
 produced as if a current in the same direction had existed." He was 
 led to this conclusion by reasoning from the lines of force. 
 
 Maxwell, writing presumably in 1872 or 1873, outlines an experi- 
 ment, similar to the one now used, for the proof of this effect. 
 
 The possibility of the magnetic action of convection-currents occurred 
 to Professor Rowland in 1868, and is recorded in a note-book of that 
 date. 
 
 In his first experiments, made in Berlin in 1876, Prof. Rowland used 
 a horizontal hard rubber disk, coated on both sides with gold, and 
 revolving between two glass condenser-plates. Each coating of the 
 disk formed a condenser with the side of the glass nearer it; the two 
 sides of the disk were charged to the same potential. The needle was 
 placed perpendicular to a radius, above the upper condenser-plate, and 
 nearly over the edge of the disk. The diameter of the hard rubber 
 disk was 21 cm., and the speed 61 per second. 
 
 The needle system was entirely protected from direct electrostatic 
 effect. On reversing the electrification, deflexions of from 5 to 7-5 
 mm. were obtained, after all precautions had been taken to guard 
 against possible errors. Measurements were made, and the deflexions 
 as calculated and observed agreed quite well; but it was not possible to 
 make the measurements with as great accuracy as was desired, and 
 hence the present experiment. 
 
 Helmholtz, 2 in 1875 and later, carried out some experiments bearing 
 
 i Experimental Researches, vol. i, art. 1644. *Wiss. Abh. i, p. 778. 
 
252 HEXRY A. EOWLAXD 
 
 on this subject. According to the " potential theory " of electrody- 
 namics which he wished to test, unclosed circuits existed. The end of 
 one of these open circuits would exert an action on a close magnetic or 
 electric circuit. So the following experiment was made by M. Schiller, 3 
 under his direction. 
 
 A closed steel ring was uniformly magnetized, the magnetic axis coin- 
 ciding with the mean circle of the ring. This was hung by a long fibre 
 and placed in a closed metal case. A point attached to a Holtz machin.j 
 was fixed near the box, and a brush-discharge was kept up from this 
 point. If the point acted as a current-end, a deflexion would be ex 
 pected, on the potential theory. No deflexion was observed, although 
 the calculated deflexion was 23 scale-divisions. The inference is tha', 
 either the potential theory is untrue, or else that there is no unclosed 
 circuit in this case, i. e. that the convection-currents completing the 
 circuit have an electromagnetic effect. 
 
 Schiller's further work, not bearing directly upon convection-cur- 
 rents, leads him to the conclusion that all circuits are closed, and that 
 displacement-currents have an electromagnetic effect. 
 
 Dr. Lecher is reported to have repeated Professor Eowland's experi- 
 ment, with negative results. His paper has not been found. 
 
 Rontgen* has discovered a similar action; he rotates a dielectric disk 
 between the enlarged plates of a horizontal condenser and gets a de- 
 flexion of his needle. He apparently guards against the possibility of 
 this being due to a charge on his disk. A calculation of the force he 
 measures shows it to be almost one-eighth of that in the Berlin experi- 
 ment. His apparatus is not symmetrically arranged, the disk being 
 much closer to the upper condenser-plate; the distances from the upper 
 and lower plates are 0-14 and 0-25 cm. respectively. He uses a 
 difference of potential corresponding to a spark-length of 0-3 cm. 
 in air between balls of 2 cm. diameter, i. e. about 33 electrostatic 
 units, equal to the sparking potential between plane surfaces : t 0-26 
 cm. The disk is an imperfect conductor, and altogether it does not 
 seem clear, in spite of the precautions taken, that this is not diu- to 
 convection-currents. 
 
 In the Berlin apparatus, as stated above, the needle is near the edge 
 of the disk; the magnetic effect produced is assumed to be proportional 
 to the surface-density multiplied by the linear velocity; hence the force 
 will be much greater at the edge of the disk than near the centre : but 
 
 3 Pogg. Ann. clix, p. 456. * Sitzb. d. Berl. Akad., Jan. 19, 1888. 
 
PLATE V 
 
ELECTROMAGNETIC AFFECT OF COXVECTIOX-CURREXTS 253 
 
 the iield will be more irregular, and so make accurate measurements 
 more difficult. 
 
 In the present apparatus a uniform field is secured by using two 
 vertical disks rotating about horizontal axes in the same line; the needle 
 sy.-tcin is placed between the disks, opposite their centres. The disk? 
 are in the meridian; they are gilded on the faces turned towards the 
 needle. Between the disks are placed two glass condenser-plates gilded 
 on the surfaces near the disk; and between these glasses is the needle. 
 The whole apparatus is symmetrical about the lower needle of the 
 astatic system. 
 
 Each disk is surrounded by a gilded hard rubber guard-plate in order 
 to keep the density of the charge uniform at the edges. The guard- 
 plates are provided with adjusting-screws to enable them to be put 
 accurately in the plane of the disks; and the glass plates in turn have 
 adjusting-screws for securing parallelism with the guard-plates. The 
 glass was carefully chosen as being nearly plane. Disks, glass plates, 
 and guard-plates all have radial scratches, to prevent conduction-cur- 
 rents from circulating around the coatings. 
 
 In the periphery of the disk are set eight brass studs which pene- 
 trate radially for about 5 centim., then turning off at a right angle run 
 parallel to the axis until they come out on the surface of the disks. 
 They there make contact with the gold foil. Metal brushes set in the 
 guard-plate bear on these studs, and in this way the disks are electrified. 
 
 The figure (PI. V, Fig. 1) gives a vertical projection of the entire 
 disk-apparatus : D D are the disks ; G G G G the guard-rings ; Y Y Y Y 
 the condenser-plates ; R R R R hard rubber rings fitting on the should- 
 ers A A; X X X X bearing-boxes for the axle; P P P P supporting- 
 standards ; E E metal bases sliding in the bed B B, and held in any 
 position by screws Z ; F F the bases carrying the glass plates, sliding in 
 the same way as the others. S S S 8 are the adjusting-screws for the 
 guard-plates, and 1 1 for the glass plates. L L L L are collars for catch- 
 ing the oil from the bearings; C C, C' C' are speed-counters, C C gear 
 with the axle, and C' C' with C C in the manner shown; each has 200 
 teeth, and speed-reading is taken every 40,000 revolutions. 
 
 The needle system is enclosed in the brass tube T, ending in the 
 larger cylindrical box in which are the mirror and upper needle. This 
 is closed in by the conical mouth-piece Q, across the opening of which 
 is ] daced a wire grating. The mirror is shown at M, the upper needle 
 at y and the lower at N. The system is hung by a fibre-suspension 
 about 30 <?m. in length, protected by a glass tube. The needle- 
 
25-1 HENEY A. EOWLAND 
 
 system is made by fitting two small square blocks of wood on an alumi- 
 nium wire; on two sides of each of the wooden blocks are cemented 
 small scraps of highly magnetized watch-spring. The needle thus made 
 is about 1 X 1 X 10 mm. 
 
 The mirror is fixed just below the upper needle, and is read by a 
 telescope 200 cm. distant. The plane of the mirror is at an angle 
 of 45 with the plane of the disks for convenience. The whole is sup- 
 ported by the board 00 attached to a wall -bracket. 
 
 Two controlling magnets (W W) with their poles turned in opposite 
 directions are used. By means of the up and down motion of either 
 magnet, any change in the sensitiveness can be attained; and by the 
 motion in azimuth, the zero point is controlled. The advantage of its 
 use lies in the extremely delicate means it affords of changing the 
 sensitiveness, much more delicate than with a single magnet. 
 
 The bed-plate B is screwed to one end of a table, at the other end of 
 which a countershaft is placed (Fig. 2). This is run by an electric 
 motor in the next room, the belt running through the open doorway. 
 The motor is 14 metres from the needle. 
 
 Although the disks and countershaft were carefully balanced when 
 first set up, and the table braced and weighted by a heavy stone slab, 
 yet at the speed used, 125 per second, the shaking of the entire appar- 
 atus was considerable; the needle was so unsteady that it could not be 
 read. This was seen to be due to vibrations of the telescope itself and 
 not to the needle. To prevent it, each leg of the table on which the 
 telescope rested was set in a box about 30 cm. deep filled with saw- 
 dust, and a heavy stone slab was placed on top of this table. This 
 entirely did away with the trouble; the swing of the needle was as 
 regular when the apparatus was revolving as when it was at rest. 
 
 The two hard rubber rings (RR) mentioned above have grooves cut 
 in their peripheries ; in these grooves wires are wound. These serve as 
 a galvanometer for determining the needle-constant. When not in use 
 they are held in the position shown in the figure, but when it is desired 
 to determine the needle-constant they are slipped on the shoulders 
 (AAAA) and pushed up in contact with the back of the disks. Each 
 has two turns: this arrangement will be referred to as the disk- 
 galvanometer. 
 
 If a known current is sent through the disk-galvanometer, and the 
 geometrical constant be known, the part of the constant depending on 
 the field and needle is determined. 
 
 The current is measured by a sine-galvanometer, placed in another 
 
ELECTRON AGXETIC EFFECT OF COXYECTIOX-CURREXTS .*'>"> 
 
 part of the room. To determine H at the sine-galvanometer a metre 
 brass circle is put around the sine-galvanometer, and the needle of the 
 latter used as the needle of the tangent-galvanometer thus made. 
 I- ing this tangent-glavanometer in connection with a Weber electro- 
 dynamometer, H at the sine-galvanometer is measured. 
 
 The charging was by a Holtz machine connected to a battery of six 
 gallon Leyden jars. These latter are in circuit with a reversing-key, 
 an electrostatic gauge, and the disks. 
 
 The potential was measured by a large absolute electrometer; all 
 previous observers have used spark-length between balls, with Thom- 
 son's formula. Greater accuracy is claimed for this work, largely on 
 this account. 
 
 In this instrument the movable plate is at one end of a balance-arm, 
 from the other end of which hangs, on knife-edges, a balance-pan. 
 This movable plate is surrounded by a guard-ring. 
 
 The lower plate is fixed by an insulating rod to a metal stem, which 
 slides up and down in guides. The distances are read off on a scale on 
 the metal stem. The zero reading is got by inserting a piece of plane 
 parallel glass whose thickness has been measured. The lower plate and 
 <riiard-ring have a diameter of 35 cm., and the movable disk a diameter 
 of 10 cm. 
 
 The routine of the observations was as follows: A determination 
 of H and the needle-constant (/?) was first made. The electrostatic 
 gauge was then set at a certain point, and readings of difference of 
 potential were taken. The disks were now started, electrified, and a 
 series of three elongations of the needle taken; the electrification re- 
 versed and three more elongations taken, &c. 
 
 About every five minutes speed-readings had to be noted, and at each 
 reversal it was necessary to replenish the charge in order to keep the 
 gauge-arm just at the mark. In this way a ' series ' of readings con- 
 sisting of about 25 reversals was made. After the series, electrometer 
 readings were again taken; the conditions were then changed in some 
 way. and another series begun. 
 
 The circumstances to be changed are : distance of disks from needle ; 
 distance of glass plates from needle; electrification; and direction of 
 rotation. 
 
 The calculation of the deflexion is based on the assumption that the 
 magnetic effect of a rotating charge is proportional to the quantity of 
 electricity passing any point per second, just as with a conduction- 
 current. Below are the formulae used. 
 
256 HEXEY A. ROWLAND 
 
 In the equations the letters have the following meanings. All quan- 
 tities are given in terms of C. G. S. units. 
 
 X= Distance from centre of disk to lower needle. 
 r = Distance from centre of disk to upper needle. 
 c = Radius of disk. 
 I = Distance between needles. 
 a = Radius of windings of disk-galvanometer. 
 i = Distance, centre of disk-galvanometer to lower needle. 
 p = Distance, centre of disk-galvanometer to upper needle. 
 N = Number of revolutions per second. 
 
 a = Surface-density of electrification in electrostatic measure. 
 V= Ratio of the units. 
 
 a = Angle of torsion of the electro-dynamometer. 
 <f> = Angle of deflexion of sine-galvanometer. 
 8 = Angle of deflexion of tangent-galvanometer. 
 J = Change of zero-point on electrifying the disks = half the charge 
 
 on reversing. 
 
 * = Scale-reading for disk-galvanometer. 
 w = Weight on pan of electrometer. 
 D = Distance of glass plates and disks. 
 ^ = Electrometer reading, 
 z = Condenser distance. 
 
 Force, in the direction of the axis, due to a circular current of radius 
 c, at a distance x on the axis 
 
 Strength of convection-current 
 
 NT 
 
 .'. total force due to the disk of radius c 
 
 _ 4 ^ _ _- 
 
 ~ ~V 
 
 and for the two disks acting in the same direction, total force 
 
 T_Q_2 Na A 
 V A ' 
 
 This gives the force on the lower needle. 
 
ELECTROMAGNETIC EFFECT OF CONVECTION-CURRENTS 257 
 
 Correction for the upper needle : 
 
 Potential at any point due to a circular current, 
 
 V'= Cldw, 
 equals the solid angle subtended at the point by the circle 
 
 Substituting the value of /, we have as the potential of the disk 
 
 '* * 
 
 a. 4.. .81 1M 
 
 /_v 1.3...(2i-l) p /c\"l 
 
 ( ; a.4...2Ha*+2) W J 
 
 But 
 
 and 
 
 8 p _' 
 
 & ft 
 
 .'. The force 
 
 f _atc". 
 \ ~^^ 
 
 and for the two, 
 
 where the sign of the entire expression has been changed, since the 
 poles of the upper and lower needles are opposite. 
 Or 
 
 X_Q_ * Z? 
 i or. ^. 
 
 17 
 
258 HENRY A. KOWLAND 
 
 Needle constant. 
 
 The disk-galvanometer windings have in the same way, for the lower 
 needle, the force due to current I in one turn 
 
 For the four turns, 
 
 X'=8-/<7. 
 
 Upper needle. The force is got in the same way as for the disk, omit- 
 ting the integration, i. e. we must multiply the general term of B by 
 
 _ an d replace 2* by /. This gives 
 
 CL V 
 
 yfil.3...(a-l)2Y\ M p 1. 
 
 " 2.4 ... at 7 W ^ / ' 
 
 a replacing c, and p, r. 
 For the total force, 
 
 ,_8^/r p /av_ 3p /Y n 
 
 l - - r 1 \~ \ J- f ^4 I ~ I T. 
 
 p L w \^/ J 
 
 or 
 
 Forces acting on the needle system: 
 
 Let M = moment of lower needle, 
 Let M' = moment of upper needle, 
 then 
 
 Couple on lower needle due to field = H M sin 6, 
 
 Couple on upper needle due to field = H'M' sintf. 
 
 Total couple = (EM H'M') sin 6. 
 
 Due to disk-galvanometer: 
 
 Couple on lower needle = MX' cos 6, 
 Couple on upper needle = M' X^' cos#. 
 
 Total couple = { MX' + M'XJ }cos 6, 
 
 = S7iI\MC + M'D \cos0. 
 .: for equilibrium, 
 
 S-I\MO + M'D\ cos 6 = \HM- H'M'} sin fl, 
 or 
 
 __ (HM- H'M'} tan e 
 
ELECTROMAGNETIC EFFECT OF CONVECTION-CURRENTS 259 
 
 n ]u-t 
 
 But =, = 0-03 nearly, and -^ is approximately unity. . 
 
 . I== (HM-H'_M^^ 
 
 8nM(C + Z>) 
 or 
 
 -f '- =. - 1 1 3 (say) . 
 
 M tan o 
 
 Similarly, for the revolving disks, 
 
 = /? tan J. 
 
 8 , ^ ^ 
 
 ^_ O'<- T^~ ' - < 
 
 F /?. J 
 
 For the sine-galvanometer: 
 
 TT 
 
 I = sin <p. 
 
 /. 7=10-* 5-46 ZTsin f, 
 and 
 
 /5 = 10-*. 5-46 
 
 tan P 
 
 For measurement of H : 
 Electrodynamometer, 
 
 ls =0- z jr V sin a. 
 
 ^ = constant of windings = 10~ 3 . 6'454. 
 K- moment of inertia = 10 2 . 8-266. 
 T= time of one swing =2-441. 
 .-. i = 10~ 2 . 7-59 Vsin . 
 
 Tangent galvanometer: 
 
 i = |C tan d = ^ tan 8 . 
 2-w 
 
 n = no. turns = 10. 
 b = radius turns = 49-98. 
 .-. t = 0-795 JJ tan d, 
 
 and, substituting the value of t, 
 
 JI=10-'. 9-55 ***. 
 tan d 
 
260 HENRY A. KOWLAND 
 
 Surface density (a): 
 
 a is obtained from electrometer-readings. 
 
 V 
 
 V *-f i/ 
 
 A 
 
 A = corrected area of movable plate 
 f=*r{5im 
 
 .: V = 10 X 1'756 D iJ~uT, 
 
 and ff = 1-397 - VaT. 
 
 e ' 
 
 As soon as the attempt was made to electrify the apparatus, diffi- 
 culties of insulation were met with. The charged system was quite 
 extensive, and the opportunity for leakage was abundant; in addition, 
 the winter here has been very damp. Most of the trouble of this kind 
 has been due to the glass in the apparatus; in no case where glass was 
 used as an insulator has it proved satisfactory, not even when the air 
 was dry. First, the stand with glass legs, on which the Ley den- jar 
 battery was placed, was found to furnish an excellent earth-connection. 
 
 Paraffin blocks interposed stopped this. The reversing-key had 
 three glass rods in it, all of which were found to leak ; six different spec- 
 imens of glass, some bought particularly for this as insulating glass, 
 were all found to allow great leakage. Shellacing had no effect. Hard 
 rubber was finally substituted for glass ; and after that the key insulated 
 very well, even in damp weather. 
 
 On charging the glass plates, the disks being earthed, it seemed 
 almost as if there was a direct earth-connection, so rapid was the fall of 
 the charge. This was not regarded at the time, as the plates were 
 always kept earthed ; but later, when it became necessary to charge the 
 plates, the insulation had to be made good. 
 
 Investigation showed that this was caused by leakage directly through 
 the substance of the glass to the brass back-pieces (H H). Hard rubber 
 pieces were substituted, and the trouble was entirely removed. 
 
 There was at first a deflexion in reversing the electrification while 
 the disks were at rest. This was of course due to direct electrostatic 
 effect; but it was not for some time clear where the point of weakness 
 in the electrostatic screen lay. It was found to be the faulty contact 
 between the tinfoil covering of the glass tube and the brass collar; the 
 brass had been lacquered. After this was corrected there was never 
 
ELECTROMAGNETIC EFFECT OF COXVECTION-CUKRENTS 261 
 
 again any deflexion on reversing the charge, although the precaution 
 was taken of testing it every day or so. 
 
 The currents induced in the axle by the rotation caused no incon- 
 venience; if the disks are rotated in the same direction their effect is 
 added, while the effect of the axles is in opposite directions. Even 
 when the disks were rotated oppositely, the deflexion due to the axles 
 was only 3 or 4 cm., and remained perfectly constant. 
 
 On running the disks, unelectrified, without the glass plates between 
 them and the needle, a deflexion of 4 or 5 cm. was noticed. This was 
 perfectly steady deflexion, and could easily be shown to be due to the 
 presence of the plate, as it ceased when the plates were replaced. 
 
 This was very troublesome for a time, especially as the presence of a 
 brass plate in place of the glass was found to diminish the deflexion, 
 but did not bring the needle back to zero as the glasses did. On look- 
 ing at the figure (Plate Y, Fig. 1) it will be seen that there is a brass 
 plug (/) closing the bottom of the tube in which the needle is placed. 
 The rapid rotation of the disks caused a very appreciable exhaustion 
 at the centre, and consequently a steady stream of air was sucked down 
 the tube through the open mouthpiece, and out through the imperfect 
 connection of the plug. Air-currents were not at first suspected, as the 
 deflexion was so very steady. The brass plate used was smaller than 
 the glass, and hence did not completely shield the tube. 
 
 After the brass back-pieces (H H) had been taken out, and a hard 
 rubber substituted, it was found that with one direction of rotation the 
 needle was extremely unsteady; it would run up the scale for several 
 centimetres, stop suddenly, &c. evidently a forced vibration. This 
 was traced to air-currents also. Now, the air blew into the open mouth 
 of the cone. The apparatus had been run for some months with this 
 open, and not the slightest irregularity had been seen. But the hard 
 rubber pieces were very much larger than the brass ones which were 
 removed ; they filled up the lower space to a greater extent, and deflected 
 the air upwards more than before, causing the unsteadiness. With the 
 opposite rotation the air was thrown down instead of up, and conse- 
 quently did not affect the needle. 
 
 The first systematic observations were made in January, 1889, with 
 the disks charged and plates earthed. The deflexion on reversing was 
 got without difficulty, and it was in the direction to be expected; that 
 is, with positive electrification, the effect was equivalent to a current in 
 the direction of motion of the disk. A number of series were taken in 
 the next two months; they agreed among themselves well enough, but 
 
262 HENEY A. EOWLAND 
 
 did not follow the law assumed. The deviation can best be explained 
 in this way: The equations above show that for a fixed position of 
 
 N~ D N 
 
 the disks J oc a-, a-x. If then, N and /9 being constant, the con- 
 p e p 
 
 denser plates are moved up to the disk, step by step, thus varying e, 
 and D be changed at the same time so as to keep D/e <xa, a constant, 
 the deflexions should be constant. 
 
 Such was not found to be the case; the deflexions were directly 
 proportioned to e instead of being constant : that is, with greater differ- 
 ence of potential, the deflexions were greater, although the surface 
 density remained constant. Finally this was found to be due to a 
 charge on the back surface of the gold coating. The end of the axle 
 comes nearly up to the surface of the disk and taken with all the brass 
 work must form a condenser of a certain capacity with the inner face 
 of the gold foil. 
 
 This made a change necessary in the method of working; the disks 
 had to be earthed and the glasses charged. This was done; but now 
 the deflexions were found always to be greater with positive rotation 
 (Zenith, North, Nadir, South) then with negative. 
 
 It was considered possible that the brushes might have something 
 to do with this, so they were taken off. Earth connection with the disk 
 was made by drilling through to the surface of the disk in the line of 
 the axle and setting in a screw, which came flush with the surface and 
 also made contact with the axle; this, however, made no difference, the 
 deflexions for negative rotation were always smaller. 
 
 Table I gives the results of a number of observations. All were 
 taken with the plates charged and the disks earthed by means of the 
 axle. 
 
 The meaning of the letters has been given; l//9is directly propor- 
 tional to the needle sensitiveness. 
 
 The sudden variations in the values of 1//9 are due to changes pur- 
 posely made in the needle. 
 
 The last column gives the values of V. This work is not intended 
 as a determination of V, but the calculation is made merely to show to 
 what degree of approximation the effect follows the assumed law. 
 
 The deflexions are about the same as those obtained in the Berlin 
 experiments 5 to 8 mm. on reversing. The force measured then 
 was 1/50000 H; now it is 1/125000 H. The sensitiveness of the needle 
 in the two cases was almost the same. In the former experiment a 
 force of 3 X 10~ 7 deflected the needle 1' of arc; the corresponding num- 
 
ELECTROMAGNETIC EFFECT OF CONVECTION-CURRENTS 
 
 263 
 
 ber now is 2-7 X 10~ 7 r slightly more sensitive. The scale distances 
 were 110 and 200 cm. respectively. So this experiment gives about 
 
 
 TABLE I. 
 
 No. 
 
 Rotation. 
 
 X. 
 
 e. 
 
 N. 
 
 <r. 
 
 1//3. 
 
 2A. 
 
 V. 
 
 
 
 
 
 
 
 
 mm. 
 
 
 1 
 
 + 
 
 2-54 
 
 1-24 
 
 122 
 
 1-16 
 
 1-50. 10 5 
 
 5-3 
 
 2-42.101 
 
 2 
 
 + 
 
 2-57 
 
 11 
 
 125 
 
 1-30 
 
 3-11 
 
 9-0 
 
 3-38 
 
 8 
 
 + 
 
 
 II 
 
 129 
 
 1-23 
 
 2-15 
 
 6-94 
 
 3-00 
 
 4 
 
 _ 
 
 
 11 
 
 129 
 
 1-23 
 
 ii 
 
 5-58 
 
 3-68 
 
 5 
 
 + 
 
 
 1-21 
 
 127 
 
 1-21 
 
 2-25 
 
 5-6 
 
 3-74 
 
 6 
 
 
 
 
 a 
 
 133 
 
 1-21 
 
 u 
 
 5-7 
 
 3-74 
 
 7 
 
 + 
 
 
 Cl 
 
 130 
 
 1-47 
 
 " 
 
 8-4 
 
 3-10 
 
 8 
 
 _ 
 
 
 II 
 
 133 
 
 1-47 
 
 u 
 
 7-3 
 
 3-64 
 
 9 
 
 + 
 
 
 1-24 
 
 121 
 
 1-32 
 
 2-22 
 
 9-4 
 
 2-26 
 
 10 
 
 _ 
 
 
 11 
 
 130 
 
 1-32 
 
 ii 
 
 7-2 
 
 3-16 
 
 11 
 
 + 
 
 
 11 
 
 125 
 
 1-26 
 
 2-17 
 
 7-6 
 
 2-70 
 
 12 
 
 _ 
 
 
 11 
 
 126 
 
 1-26 
 
 < 
 
 5-7 
 
 3-64 
 
 13 
 
 + 
 
 2-85 
 
 1-50 
 
 125 
 
 1-19 
 
 2-23 
 
 6-5 
 
 2-82 
 
 14 
 
 
 
 
 ii 
 
 129 
 
 1-19 
 
 ii 
 
 5-0 
 
 3-78 
 
 15 
 
 
 
 
 u 
 
 125 
 
 1-11 
 
 2-19 
 
 5-85 
 
 2-82 
 
 16 
 
 + 
 
 
 1-43 
 
 127 
 
 1-08 
 
 2-35 
 
 7-3 
 
 2-46 
 
 17 
 
 
 
 
 u 
 
 128 
 
 1-08 
 
 ti 
 
 5-4 
 
 3-32 
 
 18 
 
 
 
 
 it 
 
 129 
 
 1-08 
 
 u 
 
 5-3 
 
 3-42 
 
 19 
 
 + 
 
 3-22 
 
 1-80 
 
 123 
 
 1-13 
 
 2-44 
 
 5-1 
 
 3-30 
 
 20 
 
 
 
 ii 
 
 u 
 
 124 
 
 1-13 
 
 11 
 
 4-9 
 
 3-48 
 
 
 
 
 
 
 
 
 
 3- 19 x ]0i 
 
 TABLE II. 
 
 #13. 
 
 #14- 
 
 mm. 
 
 
 6-7 
 
 5-1 
 
 5-1 
 
 4-9 
 
 6-6 
 
 3-9 
 
 7-6 
 
 5-3 
 
 8-0 
 
 5-0 
 
 5-8 
 
 5-2 
 
 6-3 
 
 4-9 
 
 8-0 
 
 5-0 
 
 8 
 
 5-0 
 
 4-3 
 
 4-4 
 
 5-9 
 
 6-6 
 
 6-0 
 
 5-0 
 
 6-5 
 
 5-0 
 
 the same scale-deflexion at twice the distance with a force ^ as great. 
 The agreement between the two is seen to be quite good. 
 
 The observations, except Nos. 1, 2, 15, and 18 given above, were taken 
 
264 HENRY A. EOWLAND 
 
 in pairs first one direction of rotation and the other immediately after- 
 wards, everything except the rotation being kept constant. 
 
 The table shows that, in every case except one, the deflexion for 
 negative rotation is appreciably smaller than the corresponding positive. 
 
 The difference is too great to be due to accidental errors in the read- 
 ings, as the following table, giving the successive deflexions in the case 
 of #13 and #14 will show. 
 
 There is but one deflexion in #13 as small as the mean of #14, and 
 but one in #14 as large as the mean of #13. 
 
 This is a fair example of the way the deflexions run. As a further 
 illustration of this take#17 and#18; these two are identical in arrange- 
 ment, but the direction of rotation is in one case got by crossing the 
 belts from the countershaft to the disks and leaving the main bolt 
 straight; in the other the main belt is crossed while the auxiliary belts 
 are straight. The deflexions are the same. This, too, shows that the 
 difference cannot be due to any effect of the countershaft. The cause 
 of this has not yet been explained. The work is to be continued with 
 this and also with new apparatus, made like the Berlin apparatus, but 
 with the disk much larger, 30 cm. in diameter; at least double the 
 speed then obtained will be used. This ought to give deflexions on 
 reversal of 1-5 to 1-7 cm. 
 
 The values of V do not agree so well as might be looked for; but. 
 when, in addition to the numerous difficulties already mentioned, the 
 smallness of the deflexion is considered, and the possibility of the needle 
 being affected by currents or magnets in other portions of the labora- 
 tory, so far away as not to be guarded against, and which might well be 
 changed between the time of taking the observation and the determin- 
 ation of the needle-constant, and, finally, that a distubing cause of some 
 kind is still undoubtedly present, the agreement is seen to be as good 
 as could justly be expected. 
 
 Physical Laboratory, Johns Hopkins University, 
 April 22, 1889. 
 
 NOTE, added April 29 
 
 There seems to be a misunderstanding in certain quarters as to the 
 nature of the deflexion obtained in Prof. Eowland's first experiment. 
 The paper reads : " The swing of the needle on reversing the electri- 
 fication was about 10 to 15 mm., and therefore the point of equilibrium 
 was altered 5 to 7-5 mm/' This has been construed to mean that the 
 
ELECTROMAGNETIC EFFECT OF CONVECTION-CURRENTS 265 
 
 deflexion was merely a throw, and that no continuous deflexion was 
 obtained. This is entirely erroneous; there was always a continuous 
 deflexion. The throw was read merely because the needle was always 
 more or less unsteady, and better results could be got by seizing a 
 favorable moment when the needle was quiet and reading the throw, 
 than by attempting to take the successive elongations, or waiting for 
 the needle to come to rest. In the experiment described above the 
 needle was very steady and no such trouble was experienced. On elec- 
 trifying, the needle would take up a certain position and would remain 
 there as long as the charge was kept up ; on reversal, it would move off 
 to a new and perfectly definite position about 6 to 7 mm. away, and 
 remain there, &c. H. A. E. 
 
 C. T. H. 
 
44 
 
 ON THE RATIO OF THE ELECTROMAGNETIC TO THE 
 ELECTROSTATIC UNIT OF ELECTRICITY 
 
 Br flcxKr A. ROWLAXD, with the *UUnc<r of E. H. BALL mud L. B. FLETCMEK 
 
 (PkitMipktrml MmpuiHe [5J, XXVIII. 304-315, 1889; 4wrfe SOWTM/ / &* [S], 
 
 JTJTJT K///, 299-998, IMf] 
 
 The determination described below was made in the laboratory of 
 the Johns Hopkins University about ten years ago, and was laid aside 
 for further experiment before publication. The time never arrived to 
 complete it, and I now seize the opportunity of the publication of a 
 determination of the ratio by Mr. ROM in which the same standard 
 condenser was used, to publish it. Mr. Rosa has used the method of 
 getting the ratio in terms of a resistance. Ten years ago the absolute 
 resistance of a wire was a very uncertain quantity and, therefore, I 
 adopted the method of measuring a quantity of electricity electro- 
 statically and then, by passing it through a galvanometer, measuring it 
 electromagnet ically. 
 
 The method consisted, then, in charging a standard condenser, whose 
 geometrical form was accurately known, to a given potential as meas- 
 ured by a very accurate absolute electrometer, and then passing it 
 through a galvanometer whose constant was accurately known, and 
 measuring the swing of the needle. 
 
 DESCBIPTIOX OF IXSTBCTCEXTS 
 
 Ekctrt/rnetT. This was a very fine instrument made partly according 
 to my design by Edelmann, of Munich, As first made, it had many 
 faults which were, however, corrected here. It is on Thomson's guard 
 ring principle with the movable plate attached to the arm of a balance 
 and capable of accurate adjustment. The disc is 10-18 cm. diameter 
 in an opening of 10-38 cm. and the guard plates about 33-0 cm. diam- 
 eter. All the surfaces are nickel plated and ground and polished to 
 optical surfaces and capable of accurate adjustment so that the dis- 
 tance between the plates can be very accurately determined. The 
 balance is sensitive to a mg. or less and the exact position of the beam 
 
RATIO Of ffx-JUxmrntaftLomtem^f. 10 TEr.m !'<iHi!if '^TH* TTSTHT Bfl 
 
 :- :\ : I'.-':.:: .::._- ' - : : ' - :-.r in i ' -.-: -: " -, . --- :;; -/.: - 
 
 ^ :. iesiedi throttgh- 
 
 ovt iis attire nnge bjr Tailing; the detracts and weights to give the 
 
 constant puifnlial of a standard gaiage r and fband to give relative icad- 
 
 :r_- ' "::;: 1 in ^ - '.^i.-:. I' - :---;-: --: ->.: :-;^- : :. ;-;- ;- ->.-: 
 
 ..._. ,' i -. | .,. i .. ,_ : ..-.-..^ -'--.; --.J.--.-7 I"' -> -;. -.- .-_; _- -.; . -. : ,. ,- [ogfid 
 
 .'-. - ".- r ;.":-? ::". " . " " "r i~ -iriil " " : ; ~". "" !oin.bine<3 weigiit^ tnd 
 dEctvartalK fontty it ins fbvnd Dest to limit its swing' to a -fa nna. OB. 
 cadk aide of its normal posrtiwm. The mean of two meadin^R of the 
 
 :;--,i- :-. - r -.: r.: ".:- -'-. - >..i:r ;omp up md the >ther lown. ---.- ;-.-: 
 one r 
 
 The ad justm - :~ ~ - :' the plates parallel to each 0>ther ami o^f the 
 nwiainle vlate in the Diane of the <nard rin<r could be made to almost 
 
 IT JT ^ Ij 
 
 i.~ -7'r7. "- ~~ potential "i khe ~~~. 
 
 where 4 is the drnfanrr of the plates, w the absolute force on the 
 
 _. . -;-_: -\i-.-_ j.- i J_ -; . :^ -.;-.-; -. - \ According " iTaiw ?I1 
 
 where ^ aia^ ^ are the iradn. of the disc anxi the openrng^ foe it 
 = Rl // _-.. .':.-. \i.i- :orred Ha^ Aaal 1 
 nenee we kave^ finaEhr r 
 
 F= 
 
 
 Stmmioni canaVvwr. This Terr aenate instrument was made from 
 
 irsj-- '-- )[? ".---,- -'- . r -, y..~ 5Tork, L~ : :onsisted ' J >ne 
 
 knfflorw baiL vezy acennateljr ttnmeii and nickel pW**^ in which two bolls 
 
 .-: : ---.-... ,.'-;-._-"--,- , - : /.-..- '-;;;.- -:'_ i be - ?rv 
 
 IT - 
 
 ;i . ,. r . .:._..: . .-. ., :'-"-.'- -.- -.-. - ,-^-.\ - wus made 
 
 ITT two wires aftMrat -J^T ^^ dBanwteTy one of which was protruded 
 
 -- . _-:- - -.., '-., .-. - - .'-,.: - .-- ,-. -- , --- . .-;-.-. - 
 
 r .--:: - mm Bam niftaVav- -. : -':- -.-: :~- tntrodiBBBJ ri 
 aaiitan nlni in iffiit Iftn iHimliii^i Tins eonld be efiected five times 
 
 ^- - - . . - - : 7~- , ; . - -. ---.".;.'- -. - -.-,--.-.-. -. .;-.-,,;-; -^--. 
 
 ini d py ^aiing in water, and the ckilioafadie capacities fiwmd to be 
 50-00 and 29-556 e-g. SL mniteiw 
 
 :- .- V.~ 7 -i - : >;-:. 
 
268 HENRY A. KOWLAND 
 
 Galvanometer for Electrical Discharges. This was very carefully m- 
 sulated by paper and then put in hot wax in a vacuum to extract the 
 moisture and fill the spaces with wax. It had two coils, each of about 
 70 layers of 80 turns each of No. 36 silk covered copper wire. They 
 were half again as large as the ordinary coils of a Thomson galvano- 
 meter. The two coils were fixed on the two sides of a piece of vulcanite 
 and the needle was surrounded on all sides by a metal box to protect 
 it from the electrostatic action of the coils. A metal cone was attached 
 to view the mirror through. The insulation was perfect with the 
 quickest discharge. 
 
 The constant was determined by comparison with the galvanometer 
 described in this Journal, vol. xv, p. 334. The constant then given has 
 recently been slightly altered. The values of its constant are 
 
 By measurement of its coils 1832-24 
 
 By comparison with coils of electrodynamometer. . . . 1833-67 
 By comparison with single circle 1832-56 
 
 Giving these all equal weights, we have 
 
 1832-82 
 
 instead of 1833-19 as used before. 
 
 The ratio of the new galvanometer constant to this old one was 
 found by two comparisons to be 
 
 10-4167 
 10-4115 
 
 Mean, 10-4141 
 Hence we have 
 
 G = 19087. 
 
 Electrodynamometer. This was almost an exact copy of the instru- 
 ment described in Maxwell's treatise on electricity except on a smaller 
 scale. It was made very accurately of brass and was able to give very 
 good results when carefully used. The strength of current is given 
 by the formula 
 
 - 
 
 T ysin a 
 
 where K is the moment of inertia of the suspended coil, t its time of 
 vibration, a the reading of the head, and C a constant depending on 
 the number of coils and their form. 
 
RATIO OF ELECTROMAGNETIC TO ELECTROSTATIC UNIT 269 
 
 LARGE COILS. 
 
 Total number of windings 240 
 
 Depth of groove -84 cm. 
 
 Width of groove -76 cm. 
 
 Mean radius of coils 13-741 cm. 
 
 Mean distance apart of coils 13-786 cm. 
 
 SUSPENDED COILS. 
 
 Total numher of windings 126 
 
 Depth of groove -41 cm. 
 
 Width of groove -38 cm. 
 
 Mean radius 2-760 cm. 
 
 Mean distance apart 2-707 cm. 
 
 These data give, by Maxwell's formulae, 
 
 (7 = 0-006457. 
 
 In order to be sure of this constant, I constructed a large tangent 
 galvanometer with a circle 80 cm. diameter and the earth's magnetism 
 was determined many times by passing the current from the electro- 
 dynamometer through this instrument and also by means of the ordi- 
 nary method with magnets. In this way the following values were 
 found. 
 
 Magnetic Electrical 
 
 method. method. 
 
 December 16, 1879 -19921 -19934 
 
 January 3, 1879 -19940 -19942 
 
 February 25, 1879 -19887 -19948 
 
 February 28, 1879 -19903 -19910 
 
 March 1, 1879 -19912 -19928 
 
 Mean -19912 -19933 
 
 which differ only about 1 in 1000 from each other. Hence we have 
 for C: 
 
 From calculation from coils -006457 
 
 From tangent galvanometer -006451 
 
 Mean -006454 c. g. s. units. 
 
 The suspension was bifilar and no correction was found necessary for 
 the torsion of the wire at the small angles used. 
 
270 HENRY A. EOWLAND 
 
 The method adopted for determining the moment of inertia of the 
 suspended coil was that of passing a tube through its centre and placing 
 weights at different distances along it. In this way was found 
 
 K = 82Q-Q c. g. s. units. 
 
 The use of the electrodynamometer in the experiment was to determine 
 the horizontal intensity of the earth's magnetism at any instant in the 
 position of the ballistic galvanometer. This method was necessary on 
 account of the rapid changes of this quantity in an ordinary building 1 
 and also because a damping magnet, reducing the earth's field to about 
 J its normal value, was used. For this purpose the ballistic galvano- 
 meter was set up inside the large circle of 80 cm. diameter with one 
 turn of wire and simultaneous readings of the electrodynamometer and 
 needle of ballistic galvanometer were made. 
 
 THEORY OF EXPERIMENT. 
 We have for the potential 
 
 v 8*? , , , /-[", , -00021 
 
 - * d ^w -- ed V w\ 1 H g 
 
 For the magnetic intensity acting on the needle 
 
 TT__ 2xnp"-c V 1C sin a 
 *(p 2 + J 2 )itan? 
 For the condenser charge 
 
 Whence 
 
 _ eGC (p^ + b^Z Nt i*l wd tan? P.. >* 
 
 '"*V TV sin a 2 sin 0[_ ~ 2 
 
 but 
 
 and 2 sin $0 = I * |~1 i f * Y ~| nearly. 
 
 ML \ us J " 
 
 So that finally 
 
 = eGC _.__ - __ 
 
 A=0; -0011; -0030; -0056; -0090 for 1, 2, 3, 4, 5 discharges as inves- 
 tigated below. 
 
 1 This experiment was completed before the new physical laboratory was finished. 
 
EATIO or ELECTROMAGNETIC TO ELECTROSTATIC UNIT 271 
 
 -0002 
 
 .Frrrz -0013 for first ball of condenser and -0008 for other, as investi- 
 
 gated below. 
 
 I = correction for torsion of fibre = as it is eliminated. 
 e = constant of electrometer = 17-221. 
 Q = constant of ballistic galvanometer = 19087. 
 p = radius of large circle = 42-105 cm. 
 w = number of coils on circle = 1. 
 c = constant of electrodynamometer = -006454. 
 K =. moment of inertia of coil of electrodynamometer = 826 -6. 
 b = distance of plane of large circle from needle 1-27. 
 C = capacity of condenser = 50-069 or 29-556. 
 D = distance of mirror from scale = 170-18 cm. 
 w = weight in pan of balance. 
 t = time of vibration of suspended coil. 
 7*= time of vibration of needle of ballistic galvanometer. 
 ,3 = deflection of needle on scale when constant current is passed. 
 a = reading of head of electrodynamometer when constant current 
 
 is passed. 
 
 o = swing caused by discharge of condenser. 
 A = distance of plates of electrometer. 
 IV = number of discharges from condenser. 
 X = logarithmic decrement of needle. 
 A = correction due to discharges not taking place in an instant. 
 
 The principal correction, requiring investigation is A. Let the posi- 
 tion and velocity of the needle be represented by 
 
 x = v sin U and v = f b cos bt, where b = / 1. 
 
 At equal periods of time t t , 2/ r 3t t , etc., let new impulses be given to 
 the needle so that the velocity is increased by v at each of these times. 
 The equations which will represent the position and velocity of the 
 needle at any time are, then, 
 
272 HENRY A. EOWLAND 
 
 between and t t x =. a sin bt v = a b cos bt 
 
 " t t and 2t t x = a' sin b(t + t'} v = a'b cos b(t + /') 
 " 2^ and 3*, x = a" sin b(t + I") v = a"b cos b(t + t") 
 
 At the times 0, t t , 2t,, etc., we must have 
 
 x = v = a b 
 
 a sin W, = a' sin *(*, + *') v + a b cos W, = a'b cos (/, + t ) 
 
 a' sin &(2f, + t'} = a" sin b(2t, + t") v.a'b cos b(2t, + t") 
 
 etc. = a"b cos *(3f, + J") 
 
 etc. 
 
 Whence we have the following series of equations to determine a', a", 
 etc., and t', t", etc. 
 
 a fi b* = 2 i 2 + v* + 2r a b cos U t \ sin b(t t + t'} = |? sinW, 
 
 " 2 * 2 = a' 2 5 2 4- Vo 2 + 2y a'i cos b(2t, - t') ; sin b(2t t + t") = ^sin i(2/, + /') 
 
 S^ + i!"); sin 4(3^ + /'")= sin J(3/ 4 + r') 
 etc. etc. 
 
 "When t, is small compared with the time of vibration of the magnet, 
 we have very nearly t' \t t \ t" = i fl t'" = f t fl etc. 
 
 a" = 2a \l + cos bt t ) = 4<(1 - t (W,) 2 ) 
 
 fl'" -9a 2 (l-f(^) 2 ) 
 
 a'"* = 16a \l-$(bt t y) 
 
 a iv2 = 25a 2 (l 2 (&,)*) 
 
 T2 = 
 Whence 
 
 a' = 2a (l - 4 (&,)') 
 
 a" =3-/ (l -*(,)') 
 
 a'" =K(1-|(*O*). 
 
 a iT =5fl (l- (d/,)) 
 
 Now a , a', a", a'" and a" are the values of 3 with 1, 2, 3, 4 and 5 
 discharges and a , 2a , 3a , 4a and 5a are the values provided the 
 discharges were simultaneous. 
 
 This correction is quite uncertain as the time, ,, is uncertain. 
 
 In assuming that the impulses were equal we have not taken account 
 of the angle at which the needle stands at the second and subsequent 
 discharges, nor the magnetism induced in the needle under the same 
 circumstances. One would diminish and the other would increase the 
 
EATIO OF ELECTROMAGNETIC TO ELECTROSTATIC UNIT 273 
 
 effect. I satisfied myself by suitable experiments that the error from 
 this cause might be neglected. 
 
 The method of experiment was as follows: The store of electricity 
 was contained in a large battery of Leyden jars. This was attached 
 to the electrometer. The reading of the potential was taken, the 
 handle of the discharger was turned and the momentary swing observed 
 and the potential again measured. The mean of the potentials ob- 
 served, with a slight correction, was taken as the potential during the 
 time of discharge. This correction came from the fact that the first 
 reading was taken before the connection with the condenser was made. 
 The first reading is thus too high by the ratio of the capacities of the 
 condenser and battery and the mean reading by half as much. Hence 
 we must multiply d by 1 F where F= -0013 for first ball of con- 
 denser and -0008 for other. This will be the same for 1 or 5 dis- 
 charges. From 10 to 20 observations of this sort constituted a set, and 
 
 the mean value of -, which was calculated for each observation sepa- 
 rately, was taken as the result of the series. 
 
 Before and after each series the times of vibration, t and T, and the 
 readings, /9 and a, were taken. The logarithmic decrement was ob- 
 served almost daily. 
 
 EE STILTS 
 
 The table on the following page gives the results of all the observa- 
 tions. 
 
 These results can be separated according to the number of discharges 
 as follows: 
 
 1. 
 
 300-59 
 300-17 
 296-72 
 297-84 
 298-90 
 298-57 
 299-05 
 300-80 
 296-56 
 
 2. 
 
 3. 
 
 4. 
 
 5. 
 
 298-37 
 
 295-73 
 
 296-43 
 
 296-50 
 
 298-61 
 
 296-40 
 
 297-24 
 
 296-37 
 
 297-43 
 
 298-75 
 
 301-82 
 
 297-38 
 
 297.78 
 
 298-66 
 
 295-02 
 
 296-87 
 
 300-19 
 
 296-75 
 
 295-22 
 
 296-31 
 
 298-80 298-48 297-26 29715 296-69 
 18 
 
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EATIO OF ELECTROMAGNETIC TO ELECTROSTATIC UNIT 275 
 
 In taking the mean, I have ignored the difference in the weights due 
 to the number of observations, as other errors are so much greater than 
 those due to estimating the swing of the needle incorrectly. 
 
 It will be seen that the series with one discharge is somewhat greater 
 than with a larger number. This may arise from the uncertainty of 
 the correction for the greater number of discharges, and I think it is 
 best to weight them inversely as this number. As the first series has, 
 also, nearly twice the number of any other, I have weighted them as 
 follows : 
 
 Wt. vxlO- 8 
 
 8 298-80 
 
 4 298-48 
 
 3 297-26 
 
 2 297-15 
 
 1 296-69 
 
 Mean 298-15 
 
 Or v = 29815000000 cm. per second. 
 
 It is impossible to estimate the weight of this determination. It is 
 slightly smaller than the velocity of light, but still so near to it that 
 the difference may well be due to errors of experiment. Indeed the 
 difference amounts to a little more than half of one per cent. It is seen 
 that there is a systematic falling off in the value of the ratio. This is 
 the reason of my delaying the publication for ten years. 
 
 Had the correction, A, for the number of discharges been omitted, 
 this difference would have vanished; but the correction seems perfectly 
 certain, and I see no cause for omitting it. Indeed I have failed to find 
 any sufficient cause for this peculiarity which may, after all, be acci- 
 dental. 
 
 As one of the most accurate determinations by the direct method and 
 made with very elaborate apparatus, I think, however, it may possess 
 some interest for the scientific world. 
 
47 
 NOTES ON THE THEORY OF THE TRANSFORMER 
 
 [Johns Hopkins University Circulars, No. 99, pp. 104, 105, 1892; Philosophical 
 Magazine |51, XXXIV, 54-57, 1892 ; Electrical World, XX, 20, 1892] 
 
 As ordinarily treated the coefficient of self and mutual induction of 
 transformers is assumed to be a constant and many false conclusions 
 are thus drawn from it. 
 
 I propose to treat the theory in general, taking account of the hyster- 
 esis as well as the variation in the magnetic permeability of the iron. 1 
 
 The quantity p as used by Maxwell is the number of lines of magnetic 
 induction enclosed by the given conductor. This will be equal to the 
 number of turns of the wire into the electric current multiplied by the 
 magnetic permeability and a constant. But the magnetic permeability 
 is not a constant but a function of the magnetizing force, and hence we 
 must write 
 
 p Bny + C(nyY + D(ny} b + etc. 
 
 Where B, C, etc., are constants, n is the number of turns and y the 
 strength of current. 
 
 In this series only the odd powers of y can enter in order to express 
 the fact that reversal of the current produces a negative magnetization 
 equal in amount to the direct magnetization produced by a direct cur- 
 rent. This is only approximately true, however, and we shall presently 
 correct it by the introduction of hysteresis. It is, however, very nearly 
 true for a succession of electric waves. 
 
 To introduce hysteresis, first suppose the current to be alternating so 
 that y = c sin (bt -f- e) where t is the time and e the phase. The intro- 
 duction of a term A cos (U -\- e) into the value of the number of lines 
 of induction will then represent the effect very well. But the current 
 is not in general a simple sine curve and so we must write 
 
 y = a x sin (bt + e^ + a 2 sin (2bt + e 2 ) + a s sin (3bt + e 3 ) + . 
 
 1 The problem is treated by the method of magnetic circuit first applied by me to 
 iron bars in my paper on 'Magnetic Distribution' (Pliil. Mag., 1875), and afterwards 
 to the magnetic circuit of dynamos at the Electrical Conference at Philadelphia in 
 1884. I also used the same method in my paper on magnetic permeability in 1873. 
 
NOTES ON THE THEORY OF THE TRANSFORMER 277 
 
 In this case it is much more difficult to express the hysteresis empir- 
 ically. In most cases the first term in the value of y is the largest. A 
 term of the same nature as before will, in this case, suffice to express 
 the hysteresis approximated. We can then write for the total flux of 
 magnetic induction 
 
 p = A cos (U + ei) + Buy + Cn 3 y* + Dtfy 5 + etc. 
 
 Problem 1. To find the electromotive force necessary to make the 
 electric current a sine curve in a transformer without secondary. Let 
 the resistance be E, and make y = c sin (bt). Then Maxwell's equation 
 becomes 
 
 *= 
 
 Substituting the value of y we have 
 
 E= (RcAbn} sin (bt} + Bncb cos (bt} + 3 Cn 3 sin 2 (bt) cos bt + etc. 
 But 
 
 Sin *bt cos bt = \ (cos bt cos 3 U} 
 Sin *bt cos U = jig. (cos 5 bt 3 cos 3 U + 2 cos bt) 
 Si n 6 ^ cos bt = etc. 
 
 Hence the electromotive force that must be given to the circuit must 
 contain not only the given frequency of the current but also frequencies 
 of 3, 5, 7, etc., times as many. In other words, the odd harmonics. 
 
 Problem 2. Transformer without secondary, the electromotive force 
 being a sine curve. 
 
 E sin U = Ry + n . 
 ct t 
 
 First it is to be noted that when we place in this equation the general 
 value of y and make the coefficients of like functions of bt zero, all the 
 even harmonics will strike out. 
 
 Hence the value of the electric current will be 
 
 y = a 1 sin(W + i) + 3 sin (3 bt + e 3 )+a 6 sin (5bt + e t )+. 
 Substituting this value in the value for p, the equation is theoretically 
 sufficient to determine a v a z , etc., and e lf e 3) etc. The equations are 
 cubic or of higher order and the solution can only be approximate and I 
 have not thought it worth while to go further with the calculation. 
 However, it is easy to draw the following conclusion: 
 
 1. A simple harmonic current through an iron transformer will pro- 
 duce a secondary electromotive force and current, or both, which con- 
 tain not only the fundamental period but the higher odd harmonics. 
 
278 HENRY A. HOWL AND 
 
 2. This effect is not due to hysteresis but to the variation in the mag- 
 netic permeability. 
 
 3. The harmonics increase with the increase in magnetization of the 
 iron and nearly vanish as the magnetization decreases, although it is 
 doubtful if they ever quite vanish. Hence, an increase of resistance 
 will decrease the harmonics. 
 
 4. In the method of introducing the hysteresis into the equations, it 
 enters as an addition to the resistance in the term Ra { -f- Anb, where 
 R is the resistance, a^ the maximum current, A the coefficient of hyster- 
 esis, which is dependent upon the amount of magnetization of the iron, 
 
 n the number of turns of wire, and b= is 2- divided by the time of 
 
 a complete period. 
 
 The introduction of the hysteresis into the ordinary equations, there- 
 fore, presents little or no difficulty. 
 
 Many observers have noted that the current curve in a transformer 
 was not a sine curve and Prof. Ayrton has shown the presence of the 
 odd harmonics but gives no explanation. Mr. Fleming has attributed 
 them to hysteresis, but I believe the present paper gives the first true 
 explanation. 
 
 Problem 3. To find the work of hysteresis. Let the .resistance, R, 
 be zero. The work done will then be the integral of the current times 
 the electromotive force, or 
 
 (1 P fit 
 dt a 
 
 the integral to be taken for one period of the current. 
 
 27T 
 
 f*** I d*u dii 1 
 
 w= I- bA sin (bt + e,} y + Bny / + (7n s 3 y 2 - 7 f- + \dt 
 
 I II \ ' if a J fjf -J fit 
 
 / V |_ Ui J 
 
 w = A ~a\. 
 o 
 
 All the other terms are zero. 
 
 In a unit of time the energy absorbed is 
 
 Steinmetz has found by experiment that this varies as the 1-6 power 
 of the magnetic induction. Of course the present theory gives nothing 
 of this but only suggests a way of introducing the hysteresis into cal- 
 culations of this nature. For this purpose replace A by A 1 ^- 6 and the 
 
NOTES ON THE THEOBY OF THE TRANSFORMER 279 
 
 work of hysteresis becomes -=- a which is thus the formula of Stein- 
 
 </ 
 
 metz. 
 
 In the case where a secondary exists the number of turns of wire 
 being n 1 and the current y 1 , we have simply to replace ny in the above 
 formula by ny -}- n^y 1 and change the phase of the hysteresis term so 
 as to be 90 from the combined magnetizing force, ny -f- n^y 1 . The 
 equations of the currents will then be, by Maxwell's formula, 
 
 E=Ry + n 
 
 which suffice to determine both y and y 1 . The result is too complicated 
 to be attractive. The equations show, however, that the odd harmonics 
 must appear in either the electromotive forces or the primary or second- 
 ary currents, if not in all of them at once. The exact distribution is 
 only a case of complicated calculation. 
 
 It is to be specially noted that all formulae by which self induction is 
 balanced by a condenser will not be correct when applied to an iron 
 transformer but only to an air transformer. They will, however, apply 
 approximately to iron transformers in which the magnetization is small 
 and thus probably will apply better to transformers with an open 
 magnetic circuit than with a closed one. 
 
 Also an iron transformer should not be compared with an air trans- 
 former or two iron transformers with different magnetizations with 
 each other. 
 
 In conclusion I may add that the mathematical difficulties might be 
 overcome by another mode of attack but other work draws me in 
 another direction and I leave the matter to be worked up further by 
 others. 
 
48 
 
 NOTES ON THE EFFECT OF HARMONICS ON THE TRANS- 
 MISSION OF POWER BY ALTERNATING CURRENTS 
 
 [Electrical World, XX, 368, 1892; La Lumiere Electrique, XL VII, 42-44, 1893] 
 
 In a recent number of The Johns Hopkins University Circular and 
 the Phil. Mag. for July, 1892, x I have shown that an iron transformer 
 introduces harmonics of the periods 3, 5, 7, etc./ times the fundamental 
 period into the currents and electromotive forces both primary and 
 secondary of a transformer and that these increased in value as the 
 iron was more and more magnetized. 
 
 It is my present object to call attention to the effect of these har- 
 monics on the transmission of power and its measurement. For light- 
 ing purposes they are evidently of very little significance, as currents 
 of all periods are equally efficient in producing heat. There is a loss, 
 however, in the fact that they cause more loss of heat in the wires and 
 the iron of the transformers. But for the transmission of power the 
 case is very different. Here the motors are designed to run at speeds 
 dependent on the period; if there is more than one period the adjust- 
 ment fails, and there is a loss. The harmonics are thus useless in the 
 transmission of power by synchronous motors, and are of very little use 
 in motors with revolving fields. In these cases the harmonics travel 
 around the circuits, heating the wires and the iron without producing 
 valuable work. They then represent an almost complete loss in the 
 transmission of power, and as they may contain 10, 20 or even 30 or 40 
 per cent of the current, according to the magnetization of the trans- 
 former, they are probably responsible for some loss of efficiency in many 
 cases, as will be shown further on. 
 
 Indeed, I believe they are the explanation of many seeming mysteries 
 in the working of alternating current motors. 
 
 Special arrangements of condensers and coils can be made to pick 
 out these harmonics so that they become more important than the 
 
 1 See also the Electrical World of July 9, 1892. 
 
 2 The periods 2, 4, 6, etc., can evidently be introduced by magnetizing the iron of 
 the transformer in one direction by a constant current, or having it originally with 
 an asymmetrical magnetic set. 
 
EFFECT OF HARMONICS ON THE TRANSMISSION OF POWER 281 
 
 original period. This may occur accidentally and cause many curious 
 results in the working of motors. 
 
 It is, then, of the first importance in the transmission of power that 
 the curves shall be pure sine curves, and dynamos, 3 transformers and 
 motors must be designed in the future with reference to this point. 
 It would seem, also, that most calculations on the efficiency of power 
 transmission by alternating currents must be at fault unless they 
 include the action of the harmonics. 
 
 As to the amount of loss from this cause it is difficult to decide in 
 general. With synchronous motors the harmonics simply flow around 
 the wires without producing useful current of any kind. But this may 
 not cause great loss if the resistance is small. Indeed, considerable 
 distortion may represent small loss of power in certain cases and great 
 loss in others, according to the difference of phase of the current and 
 electromotive force in the harmonics. 
 
 In the case of motors with rotary fields the harmonics produce fields 
 revolving with velocities 3, 5, 7, etc., times the primary field. Now it 
 is essential for the efficiency of these motors that the armature shall 
 revolve nearly as fast as the field, and hence the efficiency for the 
 harmonics must be very small indeed, and this must decrease the effi- 
 ciency of the apparatus as a whole. 
 
 As to the heating of the wires by the harmonics, it is easy to see that 
 the total heating due to all the currents of different periods will simply 
 be the sum of the heatings due to each of the currents separately. 
 
 The effect of harmonics on the hysteresis is much more complicated 
 and can hardly be calculated without further experiment. However, 
 the following hypotheses may give some idea of the action. Let the 
 primary electromotive force be considered unity, and let a 3 , a 5 , etc., be 
 the electromotive forces of the harmonics. If these acted separately 
 on the hysteresis the total would be : 
 
 Again, if they all combined so that the maximum electromotive force 
 is equal to the sum of them all, the hysteresis will be nearly: 
 
 3 Dynamos and motors introduce the odd harmonics on account of the variations 
 of the self-induction of the machine, which becomes very apparent when a strong 
 current is flowing. The armature reactions may also introduce the harmonics. 
 
282 HENRY A. EOWLAND 
 
 However, it is hardly probable that this last condition would be often 
 satisfied, in which case this formula would give too great a value. 
 When the harmonics are small this last formula can be written nearly 
 
 As an example, suppose a 3 =-3 and a 5 -2 and a 7 = 1, these two 
 formula give an increase of 10 and 24 per cent in the loss due to 
 hysteresis. 
 
 The current heating is only 
 
 l + a\ + a\ + etc. 4 
 Or, in the example, 
 
 1 + -09 + -04 + -01 == 1-14. 
 
 It would seem, then, that the losses due to hysteresis and current 
 heating may be much increased by the harmonics. 
 
 I believe the statement has been made that the form of the curve 
 does not influence the hysteresis. This is evidently incorrect, unless 
 we take the top of the curve to reckon from, in which case the statement 
 agrees with the second hypothesis given above if the harmonics are of 
 the proper phase. 
 
 To estimate the influence on the efficiency of a plant, assume the 
 efficiency of the dynamo and synchronous motor with primary currents 
 as each equal to 90 per cent, and of the two transformers equal to 93 
 per cent, and assume that all the currents have the same harmonics as 
 given above. The total efficiency will be 70 per cent. If the harmonics 
 are now added, the 30 per cent loss will become about 35 per cent, the 
 efficiency will be decreased to 65 per cent nearly, a loss of 5 per cent. 
 There is too much assumption about this calculation to warrant full 
 belief, and the figures are given more as a challenge to further investi- 
 gation than as facts. That there is a decrease of efficiency is certain, 
 but the amount must be determined by further experiment and mathe- 
 matical investigation. But, however small the loss, provided it occurs 
 in the transformers or the dynamos and motors, it may be of great 
 consequence on account of its heating effect, because the output of 
 these is limited by the amount of the heat generated. 
 
 The practical conclusion seems to be that transformers and the arma- 
 tures of dynamos to be used in the transmission of power must be 
 designed for low magnetizations. By experiment with transformers, 
 
 4 This formula assumes that the resistance is the same for the harmonics, whereas 
 it is greater on account of the ' skin ' effect. 
 
EFFECT OF HARMONICS ox THE TRANSMISSION OF POWER 283 
 
 made by Dr. Duncan in this laboratory, immense distortion of the 
 curves has been found when the induction exceeds 12,000 lines per 
 square centimetre, while the curves are comparatively smooth with only 
 5000; hence I scarcely think it advisable to use more than 5000 for 
 transformers, even though low frequency were used. As to dynamos 
 and motors the limit will depend on the variety of machine used and 
 will not influence the better class very much. 
 
 The fixing of the limit of magnetization of transformers at 5000 
 causes the output with given current to vary inversely as the frequency. 
 As the hysteresis with slow frequency will be less, we may increase the 
 current somewhat to make up for it. As to the exact law, it depends 
 on the relative dimensions of wire and iron. Practically we might 
 estimate for an ordinary transformer that the output varied inversely 
 as the eight-tenth power of the frequency. 
 
 The law that the output varies inversely as the four-tenth power of 
 the frequency assumes that the magnetization increases with decrease 
 of frequency and thus distorts the curves as shown above. 
 
 The immense increase of the size and cost of transformers when dis- 
 tortion of the curve is avoided precludes the use of very low frequencies 
 even were it otherwise desirable. 
 
 It is to be noted that the action of the iron in producing harmonics 
 is directly on the electromotive force, and the amount of current flow- 
 ing will depend on the resistance and the self-induction of the circuit. 
 The resistance, owing to so-called ' skin ' effect, will be greater for the 
 harmonics than for the fundamental period. Self-induction depending 
 on the air will always diminish the harmonics, while if it is due to iron 
 it may either increase or decrease them according to their phase. 
 
 The measurement of the energy supplied by an alternating current is 
 also much complicated by the presence of harmonics. 
 
 Let the current be 
 
 C = A^ sin (bt + <i) + A s sin (3 U -f ?> 3 ) + A & sin (5 bt + ? s ) + 
 and electromotive force 
 
 E = B, sin bt + B 3 sin (3 bt + v'- 8 ) + B, sin ( 5 bt + *.',) + 
 The energy transmitted is, then, per unit of time 
 
 C'CE dt= r'cEd (bt) 
 
 If n is the number of complete periods in the primary term, then b = 
 2;rn and the energy transmitted per second becomes 
 
 \\.A 1 B 1 cos <p + A 3 B, cos O 3 - 8 ) + A, B, cos (cr 5 - <?' 5 ) + etc.] 
 
284 HENRY A. EOWLAND 
 
 An ordinary wattmeter in the form of an electrodynamometer with 
 non-inductive coils would give the correct value of this quantity, but 
 any attempt to multiply the mean electromotive force by the current 
 and the cosine of the phase would lead to an incorrect result unless this 
 was done for each harmonic separately. 
 
 It is to be noted that the introduction of condensers to balance self- 
 induction will only work for one period at a time. 
 
 Indeed very many of the results hitherto obtained by observers and 
 theorists will require modification in the presence of these harmonics. 
 
 It would seem from the above that the transmission of a current for 
 electric lighting is quite a different thing from the transmission of a 
 suitable current for motors. It will be remembered that the transmis- 
 sion in the Frankfort-Lauffen experiment was one of a lighting current 
 alone and that some mystery seems to hang over the motor tests. Can 
 the presence of these harmonics have anything to do with this ? 
 
53 
 
 [The Engineering Magazine, VIII, 589-596, January, 1895] 
 
 It is not uncommon for electricians to be asked whether modern 
 science has yet determined the nature of electricity, and we often find 
 difficulty in answering the question. When the latter comes from a 
 person of small knowledge which we know to be of a vague and general 
 nature, we naturally answer it in an equally vague and general manner; 
 but when it comes from a student of science anxious and able to bear 
 the truth, we can now answer with certainty that electricity no longer 
 exists. Electrical phenomena, electrostatic actions, electromagnetic 
 action, electrical waves, these still exist and require explanation; but 
 electricity, which, according to the old theory, is a viscous fluid throw- 
 ing out little amoeba-like arms that stick to neighboring light sub- 
 stances and, contracting, draw them to the electrified body, electricity 
 as a self-repellent fluid or as two kinds of fluid, positive and negative, 
 attracting each other and repelling themselves, this electricity no 
 longer exists. For the name electricity, as used up to the present time, 
 signifies at once that a substance is meant, and there is nothing more 
 certain to-day than that electricity is not a fluid. 
 
 This makes the task of one who attempts to explain modern elec- 
 trical theory a very difficult one, for the idea of electricity as a fluid 
 pervades the whole language of electrical science, and even the defini- 
 tions of electrical units as adopted by all scientists suggest a fluid theory. 
 No wonder, then, that some practical men have given up in despair 
 and finally concluded that the easiest way to understand a telegraph 
 line is to consider that the earth is a vast reservoir of electrical fluid, 
 which is pumped up to the line wire by the battery and finally descends 
 to its proper level at the distant end. Is not this the proper conclusion 
 to draw from that unfortunate term ' electric current ' ? Kemember- 
 ing this fact, that we cannot yet free ourselves from these old theories, 
 and exactly suit our words to our meaning, we shall now try to under- 
 stand the modern progress in electrical theory. 
 
 This whole progress is based upon something in the human mind 
 which warns us against the possibility of attraction at a distance 
 
286 HENRY A. ROWLAND 
 
 through vacant space: Newton felt this impossibility in the case of 
 gravitation, but it is to Faraday that we must look principally for the 
 idea that electrical and magnetic actions must be carried on by means 
 of a medium filling all space and usually called the ether. The develop- 
 ment of this idea leads to the modern theory of electrical phenomena. 
 
 Take an ordinary steel magnet and, like Faraday, cover it with a 
 sheet of paper, and upon this sprinkle iron filings. Mapped before us 
 we see Faraday's lines of magnetic force extending from pole to pole. 
 We can calculate the form of these lines on the supposition that a 
 magnetic fluid is either distributed over the poles of the magnet or 
 on its molecules, assuming that attraction takes place through space 
 without an intervening medium. But at this idea the mind of Faraday 
 revolted, and he conceived that these lines, drawn for us by the iron 
 filings, actually exist in the ether surrounding the magnet; he even 
 conceived of them as having a tension along their length and a repul- 
 sion for one another perpendicular to their length. 
 
 Two magnets, then, near each other, become connected by these lines, 
 which, like little elastic bands always pulling along their length, strive 
 to bring the magnets together. These so-called lines of force (now 
 called tubes of force) were, by his theory, conducted better by iron and 
 worse by bismuth than by the ether of space, and so gave the explana- 
 tion of magnetic attraction and diamagnetic repulsion. 
 
 The same theory of lines of force was also applied by Faraday to 
 electrified bodies, and thus all electrostatic attractions were explained. 
 By this idea of lines of force it will be seen that Faraday did away 
 with all action at a distance and with all magnetic and electrical fluids, 
 and substituted, instead, a system in which the ether surrounding the 
 magnet or the electrified body became the all-important factor and the 
 magnet or electrified body became simply the place where the lines of 
 force ended: where a line of magnetic force ended, there was a portion 
 of imaginary magnetic fluid: where a line of electric force ended, there 
 was a portion of imaginary electric fluid. As the quantities of so- 
 called plus and minus electricity in any system are equal, we can 
 thus imagine every charged electrical system to be composed of a 
 group of tubes of electrical force (more strictly electric induction) 
 which unite the plus and minus electrified bodies, each unit tube having 
 one unit of plus electricity on one end and one unit of minus electricity 
 on the other. The tension along the tube explains the reason why 
 such an arrangement acts as if there were real plus and minus elec- 
 trical fluids on the ends of the tube, attracting one another at a dis- 
 
MODERN THEORIES AS TO ELECTRICITY 287 
 
 tance. Consider a plus electrified sphere far away from other bodies. 
 The lines of force radiate from it in all directions, and, heing symmetri- 
 cal around the sphere, they pull it equally in all directions. Now 
 bring near it a minus electrified body, and the lines of force turn toward 
 it and become concentrated on the side of the sphere toward such a 
 body. Hence the lines pull more strongly in the direction of the 
 negative body, and the sphere tends to approach it. 
 
 In the case of a conducting body the lines of force always pass out- 
 wards perpendicularly to the surface, and hence, if we know the distri- 
 bution of the lines over the surface, or the so-called surface density of 
 the electricity, we can always tell in which direction the body tends to 
 move. It is not necessary to know whether there are any attracting 
 bodies near the conductor, but only the distribution of the lines. These 
 lines then do away with all necessity for considering action at a dis- 
 tance, for we only have to imagine a kind of ether in which lines of 
 force with given properties can exist, and we have the explanation of 
 electric attraction. 
 
 But the question now arises as to how the lines of electric force can 
 be produced in the ether, or, in other words, how bodies can be charged. 
 
 In the first place we know that equal quantities of plus and minus 
 electricity are always produced. As an illustration, suppose it is re- 
 quired to charge two balls with electricity. Pass a conducting wire 
 between them with a galvanic battery in its circuit. The galvanic 
 battery generates the lines of force ; these crowd together around it and 
 push each other sideways until their ends are pushed down the wire 
 and many of them are pushed out upon the balls. 
 
 When the tension backwards along the lines of force just balances 
 the forward push of the electromotive force of the battery, equilibrium 
 is established. If the wire is a good conductor, there may be electrical 
 oscillations before the lines come to rest in a given position, and this I 
 shall consider below. 
 
 The motion of the ends of the lines of force over and in the wire 
 constitutes what is called an electric current in the wire which is 
 accompanied by magnetic action around it and also by waves of electro- 
 magnetic disturbance which pass outward into space. 
 
 If, after equilibrium is established, we remove the wire, we have 
 simply two charged spheres connected by lines of electrostatic force 
 and thereby attracted to each other. If we replace the battery by a 
 dynamo or by an electric machine the effect is the same. 
 
 But there is another way by which bodies are often charged and 
 
288 HENEY A. EOWLAND 
 
 that is by friction. In this case we can suppose the glass to take hold 
 of one end of the lines of force and the rubber the other end and it is 
 then only necessary to pull the bodies asunder to fill the space with 
 lines. The friction is merely needed to bring the two bodies into inti- 
 mate contact and remove them gently from each other. 
 
 The following considerations may guide us in understanding the 
 details of the process. It is well known from Faraday's researches 
 that a given quantity of electricity has a fixed relation to the chemical 
 equivalents of substances. Thus it requires 10,000 absolute electro- 
 magnetic units of electricity to deposit 114 grams of silver, 68 grams of 
 copper, 34 grams of zinc, etc. 
 
 Hence we can consider, for instance, in chloride of silver that the 
 atoms of silver are joined to the atoms of chlorine by lines of electro- 
 static force which hold them to each other. If, by rubbing the chloride 
 of silver, we could remove the chlorine on the rubber while leaving 
 the silver, we could stretch them asunder and so fill space with the lines 
 of electrostatic force. According to this theory, then, each atom has 
 a number of lines of force attached to it, and it is only by stretching 
 the atoms apart that we can fill an appreciable space with them and so 
 cause electrostatic action at a distance. 
 
 We come to the conclusion, then, that all electrification is originally 
 produced by separating the atoms of bodies from one another, which 
 can be done by breaking contact, by friction, or by direct chemical 
 action of one substance on another, or in some other manner not so 
 common. The lines of electrostatic force in a case of electricity at 
 rest must always begin and end on matter, and they can never have 
 their ends in space free from matter. The ends can be carried along 
 with the matter, constituting electric convection, or they can slide 
 through a metallic conductor or an electrolyte or rarefied gas, making 
 what we call an electric current; but, as they cannot end in a vacuum, 
 they cannot pass through it. Thus we conclude that a vacuum is a 
 perfect non-conductor of electricity. 
 
 The exact process by which the ends of the lines of force pass 
 through and along a conductor can at present be only dimly imagined, 
 and no existing theory can be considered as entirely satisfactory. In 
 the case of an electrolyte, however, we can form a fairly perfect picture 
 of what takes place as the decomposition goes on. Thus, in the case of 
 zinc and copper in hydrochloric acid, we can imagine the zinc plate 
 attracting the chlorine of the acid, thus stretching out the natural line 
 of electric force connecting the chlorine atom and the first hydrogen 
 
MODERN THEORIES AS TO ELECTRICITY 289 
 
 atom; we can imagine the atoms of chlorine and hydrogen in the body 
 of the liquid recombining with each other and their lines of force unit- 
 ing until they form a complete line long enough to stretch from the 
 zinc to the copper plate; and all without once making a line of force 
 without its end upon matter. We can further imagine the ends of this 
 line sliding along the copper and zinc plates to the conducting wires 
 and down their length, thus making an electric current and carrying 
 the energy of chemical action to a great distance. 
 
 If the ends of the lines should slide along the wire without any 
 resistance, the wire would be a perfect conductor: but all substances 
 present some resistance, and in this case heat is generated. This we 
 always find where an electric current passes along a wire: as to the 
 exact nature of this resistance or the nature of metallic conduction in 
 general we know little, but I believe we are approaching the time when 
 we can at least imagine what happens in this most interesting case. 
 
 Besides the heating due to the electric current, steadily flowing, we 
 must now account for the magnetic lines of force surrounding the cur- 
 rent and the magnetic induction of one current on the other. 
 
 If the current is produced by the ends of the tubes of electrostatic 
 force moving along the wire, then we may imagine that the movement 
 of the lines of electrostatic force in space produces the lines of mag- 
 netic force in a direction at right angles to the motion and to the 
 direction of the lines of electrostatic force. At the same time we must 
 be careful not to assume too readily that one is the cause and the other 
 the effect : for we well know that a moving line of magnetic force (more 
 properly induction) produces, as Faraday and Maxwell have shown, an 
 electric force perpendicular to the magnetic line and to the direction of 
 motion. Neither line can move without being accompanied by the 
 other, and we can, for the moment, imagine either one as the cause of 
 the other. However, for steady currents, it is simpler to take the mov- 
 ing lines of electrostatic force as the cause and the magnetic lines as 
 the effect. 
 
 We have now to consider what happens when we have to deal with 
 variable currents rather than steady ones. 
 
 In this case we know from the calculations of the great Maxwell 
 and the demonstrations of Hertz that waves of electromagnetic disturb- 
 ance are given out. To produce these waves, however, very violent 
 disturbances are necessary. A fan waved gently in the air scarcely 
 produces the mildest sort of waves, while a bee, with comparatively 
 small wings moved quickly and vigorously, emits a loud sound. 
 19 
 
 %\ 
 
290 HENKY A. KOWLAND 
 
 So, with electricity, we must have a very violent electrical vibration 
 before waves carrying much energy are given out. 
 
 Such a vibration we find when a spark passes from one conductor 
 to another. The electrical system may be small in size, but the im- 
 mensely rapid vibrations of millions of times per second, like the quick 
 vibration of a bee's wing, sends out a volume of waves that a slowly 
 moving current is not capable of producing. The velocity of these 
 waves is now known to be very nearly 300,000 kilometers per second. 
 This is exactly the velocity of waves of light, or other radiation in 
 general, and there is no doubt at present in the minds of physicists 
 that these waves of radiation are electromagnetic waves. 
 
 By this great discovery, which almost equals in importance that of 
 gravitation, Maxwell has connected the theories of electricity and of 
 light, and no theory of one can be complete without the other. Indeed 
 they must both rest upon the properties of the same medium which 
 fills all space the ether. 
 
 Not only must this ether account for all ordinary electrical and mag- 
 netic actions, and for light and other radiation, but it must also account 
 for the earth's magnetism and for gravitation. 
 
 To account for the earth's magnetism, we must suppose the ether 
 to have such properties that the rotation of ordinary matter in it pro- 
 duces magnetism. To account for gravitation it must have such prop- 
 erties that two masses of matter in it tend to move toward each other 
 with the known law of force, and without any loss of time in the action 
 of the force. We know that moving electrical or magnetic bodies re- 
 quire a time represented by the velocity of light before they can attract 
 each other in the line joining them. But, for gravitation, no time is 
 allowable for the propagation of the attraction. 
 
 But the problem is not so hopeless as it at fiist appears. Have we 
 not in two hundred and fifty years ascended from the idea of a viscous 
 fluid surrounding the electrified body and protruding arms outward to 
 draw in the light surrounding bodies to the grand idea of a universal 
 medium which shall account for electricity, magnetism, light, and 
 gravitation ? 
 
 The theory of electricity and magnetism reduces itself, then, to the 
 theory of the ether and its connection with ordinary matter, which we 
 imagine to be always immersed in it. The ether is the medium by 
 which alone one portion of matter can act upon another portion at a 
 distance through apparently vacant space. 
 
 Let us then attempt to see in greater detail what the ether must 
 exDlain in order that we may, if possible, imagine its nature. 
 
MODERN THEORIES AS TO ELECTRICITY 291 
 
 1st. It must be able to explain electrostatic attraction. These 
 electrostatic forces are mostly rather feeble as we ordinarily see them. 
 Air breaks down and a spark passes when the tension on the ether 
 amounts to about j^-g- pound to the square inch. It is the air, how- 
 ever, that causes the break-down. Take the air entirely away, and we 
 then know no limit to this force. In a suitable liquid it may amount 
 to 500 times that in air or 5 pounds to 1 square inch, and become a 
 very strong force indeed. In* a perfect vacuum the limit is unknown, 
 but it cannot be less than in a liquid, and may thus possibly amount 
 to hundreds, if not thousands, of pounds to the square inch. 
 
 2d. It must explain magnetic action. These actions are apparently 
 stronger than electrostatic actions, but in reality they are not neces- 
 sarily so. A tension on the ether of only a few hundred pounds on 
 the square inch will account for all magnetic attraction that we know of, 
 although we are able to fix no limit to the force the ether will sustain. 
 No signs have ever been discovered of the ether breaking down. 
 
 Again, we must be able to account for the magnetic rotation of 
 polarized light as it passes through the magnetic field; and it can only 
 be accounted for by assuming a rotation around the lines of mag- 
 netic force. This action, however, takes place only while the lines 
 of magnetic force pass through matter, and it has never been observed 
 in the ether itself. The velocity of rotation, however, is immense, the 
 plane of polarization rotating in some cases 300,000,000 times per 
 second. 
 
 The ether must also account for the earth's magnetism. If we 
 assume that magnetic lines of force are simply vortex filaments in the 
 ether, we have only to suppose that the ether is carried around by the 
 rotation of the earth, and we have the explanation needed. The mag- 
 netism of the earth would then be simply a whirlpool in the ether. 
 
 3d. The ether must be able to transmit to a distance an immense 
 amount of energy either by means of electromagnetic waves as in light 
 or by the similar action which takes place in the ether surrounding a 
 wire carrying an electric current. 
 
 The amount of energy which can be transmitted by the ether in 
 this manner is enormous, far exceeding that which can be carried by 
 anything composed of ordinary matter. Thus take the case of sun- 
 light: on the earth's surface illuminated by strong sunlight a horse- 
 power of energy falls on every 7 square feet. At the surface of the 
 sun the etherial waves carry energy outward at the rate of nearly 8000 
 horse-power per square foot! 
 
292 HENRY A. EOWLAND 
 
 Again, an electric wire as large as a knitting needle, surrounded 
 with a tube half an inch in diameter in which a perfect vacuum has 
 been made to prevent the escape of electricity, may convey to a dis- 
 tance a thousand horse-power, indeed even ten thousand or more horse- 
 power, there being apparently no limit to the amount the ether can 
 carry. 
 
 Compare this with the steam-engine, where only a few hundred 
 horse-power require an enormous and clumsy steam pipe. Or, again, 
 the amount carried by a steel shaft, which, at ordinary rate of speed, 
 would require to be about a foot in diameter to transmit 10,000 horse- 
 power. 
 
 When we compare the energy transmitted through a square foot of 
 ether in waves, as in the case of the sun, with the amount that can be 
 conveyed by means of sound waves in air or even sound waves in steel, 
 the comparison becomes simply ridiculous, the ether being so im- 
 mensely superior. As quick as light, the ether sends its wave energy 
 to the distance of a million miles while the sluggard air carries it one. 
 Thus, with equal strain on each, the ether carries away a million times 
 the energy that the air could do. 
 
 4th. The ether must account for gravitation. For this purpose we 
 are allowed no time whatever to transmit the attraction. As soon as 
 the position of two bodies is altered, just so soon must the line of action 
 from one to the other be in the straight line between them. 
 
 If this were not so, the motion of the planets around the sun would 
 be greatly altered. Toward the invention of such an ether, capable 
 of carrying on all these actions at once, the minds of many scientific 
 men are bent. Now and then we are able to give the ether such proper- 
 ties as to explain one or two of the phenomena, but we always come 
 into conflict with other phenomena that equally demand explanation. 
 
 There is one trouble about the ether which is rather difficult to 
 explain, and that is the fact that it does not seem to concentrate itself 
 about the heavenly bodies. As far as we are able to test the point, 
 light passes in a straight line through space even when near one of 
 the larger planets, unless the latter possesses an atmosphere. This 
 could hardly happen unless the ether was entirely incompressible or 
 else possessed no weight. 
 
 If the ether is the cause of gravitation, however, it is placed out- 
 side the category of ordinary matter, and it may thus have no weight 
 although still having inertia, a thing impossible for ordinary matter 
 where the weight is always exactly proportional to inertia. 
 
MODEEN THEOKIES AS TO ELECTBICITY 293 
 
 Ether, then, is not matter, but something on which many of the 
 properties of matter depend. 
 
 It is curious to note that Newton conceived of a theory of gravita- 
 tion based on the ether, which he supposed to be more rare around 
 ordinary matter than in free space. But the above considerations 
 would cause the rejection of such a theory. We have absolutely no 
 adequate theory of gravitation as produced by ether. 
 
 To explain magnetism, physicists usually look to some rotation in 
 the ether. The magnetic rotation of the plane of polarization of light 
 together with the fact of the mere rotation of ordinary matter, as 
 exemplified by the earth's magnetism, both point to rotation in the 
 ether as the cause of magnetism. A smoke ring gives, to some extent, 
 the modern idea of a magnetic line of force. It is a vortex filament 
 in the ether. 
 
 Electrostatic action is more difficult to explain, and we have hardly 
 got further than the vague idea that it is due to some sort of elastic 
 yielding in the ether. 
 
 Light and radiation in general are explained when we understand 
 clearly magnetic and electrostatic actions as the two are linked together 
 with certainty by MaxwelFs theory. 
 
 Where is the genius who will give us an ether that will reconcile 
 all these phenomena with one another and show that they all come 
 from the properties of one simple fluid filling all space, the life-blood 
 of the universe the ether? 
 
60 
 
 [American Journal of Science [4], IV, 429-448, 1897 ; Philosophical Magazine [5], XL V, 
 
 66-85, 1898] 
 
 The electrical quantities pertaining to an electric current which it 
 is usually necessary to measure, outside of current, electromotive force, 
 watts, etc., are resistances, self and mutual inductances and capacities. 
 I propose to treat of the measurement of alternating currents, electro- 
 motive force and watts in a separate paper. Eesistances are ordinarily 
 best dealt with by continuous currents, except liquid resistances. I 
 propose to treat in this paper, however, mainly of inductances, self and 
 mutual, and of capacities together with their ratios and values in abso- 
 lute measure as obtained by alternating currents. I also give a few 
 methods of resistance measurement more accurate than usually given 
 by means of telephones or electrodynamometers as usually used and 
 specially suitable for resistances of electrolytic liquids. 
 
 I have introduced many new and some old methods, depending upon 
 making the whole current through a given branch circuit equal to zero. 
 These always require two adjustments and they must often be made 
 simultaneously. However, some of them admit of the adjustments 
 being made independently of each other, and these, of course, are the 
 most convenient. But all these zero methods do not admit of any 
 great accuracy unless very heavy currents are passed through the 
 resistances. The reason of this is that an electrodynamometer cannot 
 be made nearly as sensitive for small currents as a magnetic galvano- 
 meter. The deflection of an electrodynamometer is as the square of 
 the current. To make it doubly sensitive requires double the number 
 of turns in both the coils. Hence we quickly reach a limit of sensitive- 
 ness. It is easy to measure an alternating current of -0001 ampere and 
 difficult for -00001 ampere. A telephone is more sensitive and an 
 instrument made by suspending a piece of soft iron at an angle of 45, 
 as invented by Lord Eayleigh, is also probably more sensitive. 
 
 For this reason I have introduced here many new methods, depend- 
 ing upon adjusting two currents to a phase-difference of 90 which I 
 believe to be a new principle. This I do by passing one current through 
 
ELECTEICAL MEASUREMENT BY ALTERNATING CURRENTS 295 
 
 the fixed and the other through the suspended coil of an electrodynamo- 
 meter. By this means a heavy current can be passed through the fixed 
 coils and a minute current through the movable coil, thus multiplying 
 the sensitiveness possibly 1000 times over the zero current method. 
 
 I have also found that many of the methods become very simple if 
 we use mutual inductances made of wires twisted together and wound 
 into coils. In this way the self inductances of the coils are all practi- 
 cally equal and the mutual inductances of pairs of coils also equal. 
 Hence we have only to measure the minute difference of these two to 
 reduce the constants of the coil to one constant, and yet by proper 
 connections we can vary the inductances in many ratios. Three wires 
 is a good number to use. However, the electrostatic induction between 
 the wires must be carefully allowed for or corrected if much greater 
 accuracy than y^ is desired. 
 
 By these various methods the measurement of capacities and induc- 
 tances has been made as easy as the measurement of resistances, while 
 the accuracy has been vastly improved and many sources of error 
 suggested. 
 
 Relative results are more accurate than absolute as the period of an 
 alternating current is difficult to determine, and its wave form may 
 depart from a true sine curve. 
 
 Let self inductances, mutual inductances, capacities and resistances 
 be designated by L or I, M or ra, C or c, E or r with the same suffixes 
 when they apply to the same circuit, the mutual inductance having two 
 suffixes. Let & be 2 TT times the number of complete periods per second, 
 
 or & = 2-n. The quantities &L, bM or ^ are of the dimensions of 
 
 resistance and thus -^., &*LC or b*MC have no dimensions. I'LM, -^ 
 
 M 
 
 or -fy have dimensions of the square of resistances. 
 
 Where we have a mutual inductance M 12 , we have also the two self 
 inductances of the coils L t and L 2 . When these coils are joined in the 
 two possible manners, the self inductance of the whole is 
 
 L, + Z 2 + ZM U or L! + L, - 2M n . 
 
 In case of a twisted wire coil the last is very small. Likewise 
 L 1 L 2 3/ 2 12 will be very small for a twisted wire coil, as is found by 
 multiplying the first two equations together. 
 
 If there are more coils we can write similar equations. For three 
 coils we have 
 
296 HENRY A. KOWLAND 
 
 12 + 2M 1 
 
 2. 
 3. 
 
 Connecting them in pairs, we have the self inductances 
 
 L 1 + L 2 2M 12 L 1 + L 3 2M 13 
 
 There are many advantages in twisting the wires of the standard 
 inductance together, but it certainly increases the electrostatic action 
 between the coils. This latter source of error must be constantly in 
 mind, however, and, for great accuracy, calculated and corrected for. 
 But by proper choice of method we may sometimes eliminate it. 
 
 For the most accurate standards, I do not recommend the use of 
 twisted wire coils, at least without great caution. But for many pur- 
 poses it certainly is a great convenience, especially where only an 
 accuracy of one per cent is desired. In some calculations I have made, 
 I have obtained corrections of from one to one-tenth per cent from 
 this cause. 
 
 For twisted wires the above results reduce to 3L -f- 61f, 3L 2M . 
 Similar equations can be obtained for a larger number of wires. For 
 twisted wire coils, n wires joined abreast, the self induction is 
 
 -=1 , which is practically equal to L or M. The resistance 
 
 is E/n. 
 
 When we have n = p -\- m wires twisted and wound in a coil and we 
 connect them p direct and m reverse, the resistance and self induction 
 will be 
 
 nR*+FR[AC+CnAB] , If [n (A + B) 0~\ + VABC 
 (nR)*+(bC? 2 
 
 where R is the resistance of one coil and 
 
 A = L + (n 
 B=L - M 
 
 This gives self inductances and resistances equal or less than L and R. 
 The correction for electrostatic induction remains to be put in. For 
 the general case, the equation is very complicated for coils abreast, 
 with mutual inductances. 
 
 The number of mutual inductances to be obtained is M for two 
 wires, 0, M, 2M for three wires, 0, M, 2M, 3M for four wires, etc. From 
 
297 
 
 these results we see that we are always able to reduce mutual to self 
 inductance. Measuring the self inductance of a coil connected in 
 different ways, we can always determine the mutual inductances in 
 terms of the self inductances. 
 
 Thus we need not search for methods of directly comparing mutual 
 inductances with each other, although I have given two of these, but 
 we can content ourselves with measuring self inductances and capaci- 
 ties. Fortunately most of the methods are specially adapted to the 
 latter, the ratio of self inductance to capacity being capable of great 
 exactness by many methods. 
 
 In the use of condensers I have met with great difficulty from the 
 presence of electric absorption. I have found that this can be repre- 
 sented by a resistance placed in the circuit of the condenser, which 
 resistance is a function of current period. 
 
 I have developed MaxwelPs theory of electric absorption in this 
 manner. Correcting his equations for a small error, I have developed 
 the resistance and capacity of a condenser as follows: 
 
 Let a condenser be made of strata of thicknesses a x a 2 , etc., and 
 specific induction capacities fc x Jc 2) etc., and resistances p^ p 2 , etc. Then 
 we have 
 
 where 
 
 etc. 
 
 etc. 
 
 Mr. Penniman has experimented in the Johns Hopkins University 
 laboratory with condensers by method 25 and found some interesting 
 results. With a mica standard condenser of microfarad he was not 
 
298 HENEY A. KOWLAND 
 
 able to detect any electric absorption, although I have no doubt one 
 of the more accurate methods will show it. 
 
 With a condenser, probably of waxed paper, he found 
 
 Number of complete Capacity in Apparent resistance 
 
 periods per second. microfarads. in ohms. 
 
 14-0 4-64 139-6 
 
 32-0 4-96 34-1 
 
 53-3 4-96 20-5 
 
 131-1 4-94 5-2 
 
 The first value of the capacity seems to be in error, possibly one of 
 calculation. However, the result seems to show a nearly constant 
 capacity but a resistance increasing rapidly with decrease of period, as 
 Maxwell's formula show. The constant value of the capacity remains 
 to be explained. 
 
 Mr. Penniman will continue the investigation with other condensers, 
 liquid and solid, as well as plates in electrolytic liquids. 
 
 The results in the other measurements have been fairly satisfactory, 
 but many of the better methods have only been recently discovered and 
 are thus untried. But we must acknowledge at once that work of the 
 nature here described is most liable to error. Every alternating cur- 
 rent has, not only its fundamental period, but also its harmonics, so 
 that very accurate absolute values are almost impossible to be obtained 
 without great care. To eliminate them, I propose to use an arrange- 
 ment of two parallel circuits, one containing a condenser and the other 
 a self-inductance, each with very little resistance. The long period 
 waves will pass through the second side and the short ones through the 
 condenser side. By shunting off some of the current from the second 
 side, it will be more free from harmonics than the first one. 
 
 However, in a multipolar dynamo, especially one containing iron, 
 there is danger of long period waves also, which this method might 
 intensify. A second arrangement, using the condenser side, might 
 eliminate them. However, many dynamos without iron and without 
 too many poles and properly wound produce a very good curve without 
 harmonics, especially if the resistance in the circuit is replaced by a 
 self inductance having no iron. These remarks apply only to absolute 
 determinations. Eatios of inductance, self and mutual, and capacity 
 are independent of the period, and thus it can always be eliminated. 
 Measurements of resistances also are independent. 
 
 But there are other errors which one who has worked with continuous 
 
ELECTRICAL MEASUREMENT BY ALTERNATING CURRENTS 299 
 
 currents may fall into. Nearly all alternating currents generate elec- 
 tromagnetic waves which are so strong that currents exist in every 
 closed circuit with any opening between conductors in the vicinity. 
 
 We eliminate this source of error by twisting wires together and other 
 expedients. But in avoiding one error, we plunge into another. For, 
 by twisting wires we introduce electrostatic capacity between them, 
 which may vitiate our results. Thus, in methods 23 or 24 for com- 
 paring mutual inductances, if there is electrostatic capacity between 
 the wires, a current will flow through the electrodynamometer in the 
 testing circuit and destroy the balance. 
 
 Various expedients suggest themselves to eliminate this trouble, as, 
 for instance, the variation of the resistance A in the above, but I shall 
 reserve them for a future paper. I may say, however, that it is some- 
 times possible, as in method 12 for instance, to choose a method in 
 which the error does not exist. 
 
 However, with the best of methods, much rests with the experimenter, 
 as errors from electromagnetic and electrostatic induction are added 
 to errors from defective insulation when we use alternating currents. 
 
 These errors are generally less than one per cent, however, and intel- 
 ligent and careful work reduces them to less than this. 
 
 The following methods generally refer by number to the plate on 
 which the resistances, etc., are generally marked. One large circle 
 with a small one inside represent an electrodynamometer. Of course 
 the circuit of the small coil can be interchanged with the large one. 
 Generally we make the smaller current go through the hanging coil. 
 
 By the methods 1 to 14, we adjust the electrodynamometer to zero 
 by making the phase difference in the two coils 90. For greatest 
 sensitiveness, the currents through the two coils must be the greatest 
 possible, heating being the limit. This current should be first calcu- 
 lated from the impedance of the circuit, as there is danger of making 
 it too great. 
 
 In the second series of methods, 15-26, the branch circuit in which 
 the current is to be is indicated by 0. 
 
 Resistances in the separate circuits are represented by R, R', R t , etc., 
 and r, r', r t , etc. Corresponding self inductances and capacities in the 
 same circuits are L, L', L t , etc., and I, I', I,, etc., or C, C', C ',, etc., and 
 c, c', c t , etc. b = 27tn where n is the number of complete current waves 
 per second. 
 
 The currents must be as heavy as possible, ^ ampere or more, and it 
 is well to make those that require a current of more than j-^ ampere of 
 
300 HENKY A. EOWLANB 
 
 larger wire freely suspended in oil. A larger current can, however, be 
 passed through an ordinary resistance box for a second or two without 
 danger. A few fixed coarse resistances of large wire in air or oil with 
 ordinary resistance boxes for fine adjustment, are generally all that 
 are required. Special boxes avoiding electrostatic induction are, how- 
 ever, the best, but are not now generally obtainable. 
 
 In some methods, such as 8, 9, 10, etc., we can eliminate undesirable 
 terms containing the current period by using a key which suddenly 
 changes the connections before the period has time to change much. 
 
 In using twisted wire mutual inductances, methods 7 and 12 are 
 about or entirely free from error due to electrostatic action between 
 the wires. In all the methods this error is less when the resistance of 
 the coils is least and in 23 and 24 when A is least. In method 8 the 
 error is very small when the coil resistances and R are small and r great. 
 In this method with 1 henry and 1 microfarad the error need not 
 exceed 1 in 1000. Probably the same remarks apply to 9, 10, 11, also. 
 By suitable adjustment of resistances in the other method, the error 
 may be reduced to a minimum. It can, of course, be calculated and 
 corrected for. 
 
 An electrodynamometer can be made to detect -OOC1 ampere without 
 making the self inductance of the suspended coil more than -0007 
 henrys or that of the stationary coils more than -0006 henrys, the 
 latter coil readily sustaining a current of -^ amperes without much 
 heating. 
 
 An error may creep in by methods 1-14 if the current through the 
 suspension is too great, thus heating it and possibly twisting it. This 
 should be tested by short circuiting the suspended coil or varying the 
 current. For the zero method it is eliminated by always adjusting 
 until there is no motion on reversing the current through one coil. 
 
 Inductances containing iron introduce harmonics and vary with cur- 
 rent strength. Thus they have no fixed value. 
 
 Closed circuits or masses of metal near a self inductance, dimmish 
 it, and increase the apparent resistance which effects vary with the 
 period. Short circuits in coils are thus detected. 
 
 Electrolytic cells act as capacities which, as well as the apparent 
 resistance, vary with the current period. They also introduce har- 
 monics. The same may be said of an electric arc. 
 
 An incandescent lamp or hot wire introduces harmonics into the 
 circuit. 
 
 Hysteresis in an iron inductance acts as an apparent resistance in 
 
ELECTKICAL MEASUREMENT BY ALTERNATING CURRENTS 301 
 
 the wire almost independent of the current period, and does not, of 
 itself, introduce harmonics. The harmonics are due to the variation 
 of the magnetic permeability with the amount of magnetization. 
 
 Electric absorption in a condenser acts as a resistance varying with 
 the square of the period, the capacity also varying, as I have shown 
 above. 
 
 In general any circuit containing resistances, inductances and capaci- 
 ties combined acts as a resistance and inductance or capacity, both of 
 which vary with the current period, the square of the current period 
 alone entering. For symmetry the square of the current period can 
 alone enter in all these cases and those above. 
 
 Hence only inductances containing no iron or not near any closed 
 metallic circuits have a fixed value. The same may be said of con- 
 densers, as they must be free from electric absorption or electrolytic 
 action to have constants independent of the period. There is no ap- 
 parent hysteresis in condensers and the constants do not apparently 
 vary with the electrostatic force. 
 
 The following numbers indicate both the number of the method and 
 the figures in the plate, p. 302. 
 
 Method 1. 
 
 L' _ [r (R. + R' 
 ~c 
 
 Method 2. 
 
 -R.R"} \_R, (r+R"} + R u (r + fl,)] 
 
 Method 3. 
 In (1) make R' = R" = R, t = Q or in (2) make R" = R t = 0, R,, = <x> , 
 
 ^ = rR 
 
 c 
 
 In case the circuit r contains some self inductance, I, we can correct 
 for it by the equation 
 
302 
 
 HENRY A. EOWLAND 
 
 17. 
 
 In methods 1 to 14 inclusive the concentric circles are the coils of the electro- 
 dynamometer. Either one is the fixed coil and the other the hanging coil. Oblong 
 figures are inductances and when near each other, are mutual inductances. A pair 
 of cross lines is a condenser. 
 
ELECTRICAL MEASUREMENT BY ALTERNATING CURRENTS 303 
 
 Method 4- 
 
 + fl,,)] [# ( 
 R' R" 
 
 Method 5. 
 
 L, = [jy (r + R it ) + R"(R' 
 
 A _ [fl, (^" 
 
 c ' (R r + R") (R" + R 
 
 Method 6. 
 
 c O 
 
 We can correct for self inductions, U, L" in the circuits R', R" by 
 using the exact equation 
 
 R'R"(r+R")(R+R')=--0 
 or approximately 
 
 = (R+B) (R'^--^- 
 
 -. 
 + etc. 
 
 Method 7. 
 R,R 3 M 13 M l2 + b*\_L 3 M l2 -MrM [^J/ M - Jf.JfJ = 
 
 For a coil containing three twisted wires, M 12 = M 1S = M 23 and the 
 self inductions of the coils are also equal to each other and nearly equal 
 to the mutual inductions. Put an extra self induction L 3 in R 3 and a 
 
 capacity C 2 in R 2 . Replace L 3 by L -f- L 3 and L 2 by L and we 
 
 6 2 
 
 can write 
 
 As L M is very small and can be readily known, the formula will 
 give ^r When L M = we have 
 
 Method 8. 
 
 V M(M+ 1) = rR 2b* M* =~rR+(rR)' 
 
 or V M(M L) = (rR)' 2b 2 LM rR (rR)' 
 
304 HENRY A. EOWLAKD 
 
 Placing a capacity in the circuit R, we have also 
 b'M (M+ L) - %= rR 
 
 In case the coil is wound with two or more twisted wires, M L is 
 small and known. For two wires, M L is negative. For three 
 wires, two in series against the third, M can be made nearly equal to 
 2L. Hence M, L and C can be determined absolutely, or C in terms 
 of M or vice versa. 
 
 To correct for the self induction, I, or r we have the exact equations 
 
 If the condenser is put in r, we have 
 
 T M 
 
 or - = rR + VM(L-M} 
 
 Method 9. 
 MM-*, = R, 
 
 or - VL'M + *=R I 
 
 Making R" = co and r + R' = r we have 
 - VL'M+ M or VUM- ^ t 
 
 C Lr 
 
 Taking two observations we can eliminate WL'M and we have 
 
 Knowing L'M we can find C'. Throwing out C' (i. e., making it 
 oo ) we can find WL'M in absolute measure : then put in C' and find its 
 value as above. 
 
 To correct for self induction in R /f we have for case R" = oo , the 
 exact equation 
 
ELECTRICAL MEASUREMENT BY ALTERNATING CURRENTS 305 
 
 The correction, therefore, nearly vanishes for two twisted wires in a 
 coil where U M = and C is taken out. 
 
 Method 10. 
 
 c c 
 
 \_R,R" - R lt R'-\ \rlR' + R" + R,+ fl,,] + ( + R) (R" + ) \ 
 
 This can be used in the same manner as 9 to which it readily reduces. 
 But it is more general and always gives zero deflection when adjusted, 
 however M is connected. To throw out (7 make it oo . 
 
 Method 11. 
 L M_ 
 
 c 
 L + M 
 
 - M} (L- M} 
 
 c 
 
 For the upper equation the last term may be made small and the 
 method may be useful for determining L M when c is known. 
 Me'thod 8, however, is better for this. 
 
 Method 12. 
 
 L' = R+R' 
 I ~ r 
 
 Should the circuits R and r also have small self inductances, L and I, 
 we can use the exact equation 
 
 rR 
 
 When L' and Z are approximately known, we can write the following, 
 using the approximate value on the right side of the equation 
 L'_ R+R'T, Lr L r , VLl , 
 
 I ' r 
 Taking out L' and putting a condenser, (7, in R we have 
 
 For a condenser, R can be small or zero. 
 20 
 
306 HENRY A,. BOWLAND 
 
 Method 13. 
 
 (A} \bL"- 1 ,,T - [R tl R'-R,R"'\ I 
 [_ bC"_\ 
 
 This determines capacities or self inductions in absolute value. As 
 described above, mutual induction can also be determined by convert- 
 ing it into self induction. 
 
 Method 
 
 Of course, in any of these equations, methods 13 or 14, L" is elimi- 
 nated by making L" = or the condenser, C, is omitted by making 
 C = oo. 
 
 Method 15. 
 
 / 
 
 R'R- 
 
 R'"R 
 
 or ^- or - 5 2 Z 6 V/ R '" R '" R ~ R ' R " (^ 
 " ' ~ '" '"-" 
 
 
 
 C, L 
 
 When ^ //; = oo we have 
 
 A -fl'^y, (R" + R"') R"R l R" t _ ft, r> ^" r 7->"/ r> E>' E> T 
 
 ^r/ - ^>/// ~ Ka> u ~f>rrt I 2i && **u\ 
 
 b 2 L c" R^RtR'R,! 
 
 ' R"R'" 
 
 If we adjust by continuous current, we shall have R'"R I R'R tt = Q. 
 For a condenser we can made R" = provided there is no electric 
 absorption. In this case l} 2 L t C" is indeterminate and we can adjust 
 
 to findw,. However, two simultaneous adjustments are required. 
 
 But I have shown that the presence of electric absorption in a con- 
 denser causes the same effect as a resistance in its circuit, the resist- 
 ance, however, varying* with the period of the current. Hence R" must 
 
ELECTRICAL MEASUREMENT BY ALTERNATING CURRENTS 307 
 
 include this resistance. However, the value of R" will not affect the 
 first adjustment much and so the method is easy to work. If it is 
 sensitive enough it will be useful in measuring the electric absorption 
 of condensers in terms of resistance. 
 It has the advantage of being practically independent of the current 
 
 period for ^ as it should be. 
 
 
 For comparison of capacities the same simplification does not occur. 
 Indeed the method is of very little value in this case, being sur- 
 passed by 16. 
 
 Method 16. 
 (A) [R,R"-R l ,R'-\[W+r' + r"] + W[R l r"-r f RJ = 
 
 t _ 
 
 L, r C" ~ R,, + R tl ( W+ r'r + ") 
 
 The first equation is satisfied by adjusting the Wheatstone bridge so 
 as to make 
 
 (R I R'R II R)=Q R/'-R l /=Q R l (R ll + r")-R ll (K + r')=Q 
 That is 
 
 R, -R' -^ 
 
 R tl ~ ~R" ~ r" 
 
 We can then adjust W with alternating currents. This is a very 
 good method and easy of application but requires many resistances of 
 known ratio. Many of these, however, may be equal without disad- 
 vantage. A well known case is given by making r' and r" = 0. 
 
 (B) By placing self inductions or condensers in R, and r" instead 
 of the above we have the following 
 
 or VL ,-" or L > - << 
 
 L '' r '-" 
 
 Wr 
 
 + 1 or - or + VL 1"= 
 FUP c" 
 
 ") (Rfi'-RuR)* W(R/'-R ll r f ) 
 W+R" 
 
 Making R" = we have 
 
 c" r " L , 
 
 or - VLp" or -' = 
 
 In case we adjust the bridge to R,W R'R /I = and a condenser 
 
308 HENRY A. EOWLAJSTD 
 
 is in r" so that we can make r" = 0, the value of l 2 L t c" will be inde- 
 terminate and we can find J f by the adjustment of W alone. 
 
 i C 
 
 This is an excellent method, apparently, as only one adjustment is 
 required. 
 However, see the remarks on method 15. This present method 
 
 r" = for is Anderson's with, however, alternating currents instead 
 
 C 
 
 of direct as in his. 
 
 The other two values are imaginary in this case. Indeed the whole 
 
 method, B, is only of special value for , as two adjustments are needed 
 
 c 
 
 for the others. 
 
 Method 17. 
 (A) TF=oo. 72=00 
 
 VML'= R t R" - R tl R 
 L' 
 
 By this method the self induction of the mutual induction coil is 
 eliminated. But it is difficult to apply, as two resistances must be 
 adjusted and the adjustment will only hold while the current period 
 remains constant. The same remarks apply to B and C following. 
 
 (B) R=>. 
 
 ,+ R" + #] + (R + JB,) (R" 
 
 M~ RW 
 
 x> 
 
 L' _ R (R + R, + R" + #) + (K + #,) (R" 
 M~ RR tl 
 
 Method 18. 
 R t R" - R'R tl = 
 
 L ' - i L R " a. R' + R" 
 W'~ *"%, ~W^~ 
 
 L' and M' belong to the same coil. By adjusting the Wheatstone 
 bridge first, W can then be afterwards adjusted. 
 
ELECTRICAL MEASUREMENT BY ALTERNATING CURRENTS 309 
 To find the ratio for any other coil independent of the induction coil, 
 
 TJ 
 
 we can first find ^ as above. Then add L to the same circuit and we 
 M 
 
 L 4- L' 
 can find ^, Whence we can get L. This seems a convenient 
 
 jj 
 
 method if it is sensitive enough, as the value of -jj, should be accurately 
 
 jd 
 
 known for the inductance standard. 
 
 Method 19. 
 'l-M*} = S- [RR t -R"Rl 
 
 L' _R' + RL'l-M*l ,,\_K + R. R'R^-R'R.jl , , 
 
 ~ ~ ~~~ ~~ * 
 
 M~ r r* \M 
 
 This is useful in obtaining the constants of an induction standard. 
 For twisted wires L'l M 2 should be nearly 0, depending, as it does, 
 
 on the magnetic leakage between the coils, -^.is often known suffi- 
 
 ciently nearly for substitution in the right hand member. It can, 
 however, be found by reversing the inductance standard. 
 
 Method 20. 
 R'R tl - R'R, = 
 W R L 
 
 L' any value. 
 
 In case of a standard inductance, M and L are known, especially 
 when the wires are twisted. 
 
 The method can then be used for determining any other inductance, 
 L', and is very convenient for the purpose. 
 
 R n and R t + R tl are first calculated from the inductance standard. 
 The Wheatstone bridge is then adjusted and W varied until a balance 
 is obtained. This balance is independent of the current period, as also 
 in the next two methods. 
 
 Method 21. 
 R'R tl - R"R, = 
 
 I _R' + R, L' _(K + Rp. L' _R + R ll ^M 
 M -- ^^ ; Tt~ rR, T = ~^T~ 
 
 This is Niven's method adapted to alternating currents. See re- 
 marks to method 20. 
 
310 HEXEY A. EOWLAXD 
 
 Methods 20 and 21 are specially useful when one wishes to set up an 
 apparatus for measuring self induction, as the resistances R', R", 
 R t , R lt can be adjusted once for all in case of a given induction standard 
 and only W or r need be varied afterwards. 
 
 Method 22. 
 L '1 = KA. M =R R"- ^ = R" (i 
 
 This is Carey Foster's method adapted to alternating currents and 
 changed by making R" finite instead of zero. 
 
 The ratio of R' -f- R, to R t is computed from the known value of 
 the induction standard. R" is then adjusted and C" obtained. In 
 general the adjustment can be obtained by changing R t and R". The 
 adjustment is independent of the current period. 
 
 Method 23. 
 
 "rJvA^r+s+n, 
 
 m 
 If we make R = we have 
 
 tfmL' = rR t 
 
 M^r+R' + R, 
 
 m ~ r 
 
 This method requires two simultaneous adjustments. M must also 
 be greater than m. As M and L' belong to the same coil, we can con- 
 sider this method as one for determining m in terms of the M and L' of 
 some standard coil. 
 
 The resistance, A, can be varied to test for, or even correct, the error 
 due to electrostatic action between the wires of the induction standard. 
 
 Method 2.L 
 
 M t M'r" M'~r,( 
 This is a good method for comparing standards. We first determine 
 
 -^ for each coil by one of the previous methods. Then we can calcu- 
 late ^ and adjust the other resistances to balance. 
 
 It is independent of the period of the current and suitable for stand- 
 
ELECTRICAL MEASUREMENT BY ALTERNATING CURRENTS 311 
 
 ards of equal as well as of different values, as the mutual inductances 
 can have any ratio to each other. 
 
 For twisted wire coils r t = r' very nearly. See method 23 for the 
 use of the resistance, A. 
 
 Method 25. 
 
 In Fig. 6 remove the shunt R' and self induction L. 
 
 This method then depends upon the measurement of the angular 
 deflection when a self induction or a capacity is put in the circuit of 
 the small coil of the electrodynamometer and comparing this with the 
 deflection, when the circuit only contains resistance. 
 
 The resistance of the circuit, r, is supposed to be so great compared 
 with R that the current in the main circuit remains practically un- 
 altered during the change. 
 
 There is also an error due to the mutual induction of the electro- 
 dynamometer coils which vanishes when r is great. 
 
 'Z i r+R" 
 L-j-- -grr-J 
 
 These formulas assume that the deflection is proportional to 6. This 
 assumption can be obviated by adjusting 6 = 6' when we have 
 
 1 
 
 W R" 
 
 These can be further simplified by making R " R". 
 The method thus becomes very easy to apply and capable of con- 
 siderable accuracy. As the absolute determination depends on the 
 current period, however, no great accuracy can be expected for absolute 
 values except where this period is known and constant, a condition 
 almost impossible to be obtained. The comparison of condensers or of 
 inductances is, however, independent of the period and can be carried 
 out, however variable the period, by means of a key to make the change 
 instantaneously. 
 
 Method 26. 
 
 Similar results can be obtained by putting the condenser or induc- 
 tance in R" instead of r, but the current through the electrodynamo- 
 meter suspension is usually too great in this case unless r is enormous. 
 We have in this case for equal deflections, 
 
 1 //r 7?" _ v 7?"\ 
 
 ^ or PL'" = R" (R"+r) p r >'' 
 where r, and R" are the resistances without condenser or self induction. 
 
312 HENKY A. EOWLAND 
 
 This is a very good method in many respects. 
 
 For using 25 and 26, a key to make instantaneous change of connec- 
 tions is almost necessary. 
 
 To measure resistance by alternating currents, a Wheatstone bridge 
 is often used with a telephone. 
 
 I propose to increase the sensitiveness of the method by using my 
 method of passing a strong current through the fixed coils of an 
 electrodynamometer while the weaker testing current goes through the 
 suspended system. 
 
 Using non-inductive resistances, methods 10, 13 A, B, C, and 14 all 
 reduce to proper ones. 10 or 14 is specially good and I have no doubt 
 will be of great value for liquid resistances. The liquid resistances 
 must, however, be properly designed to avoid polarization errors. The 
 increase of accuracy over using the electrodynamometer in the usual 
 manner is of the order of magnitude of 1000 times. 
 
 Since writing the above I have tried some of the methods, especially 
 6 and 12, with much satisfaction. By the method 12, results to 1 in 
 1000 can be obtained. Eeplacing U by an equal coil, the ratio of the 
 two, all other errors being eliminated, can be obtained to 1 in 10,000, 
 or even more accurately. 
 
 The main error to be guarded against in method 12, or any other 
 where large inductances or resistances are included, arises from twist- 
 ing the wires leading to these. The electrostatic action of the leads, 
 or the twisted wire coils of an ordinary resistance box, may cause errors 
 of several per cent. Using short small wire leads far apart, the error 
 becomes very small. 
 
 Method 6 is also very accurate, but the electric absorption of the 
 condensers makes much accuracy impossible unless a series of experi- 
 ments is made to determine the apparent resistance due to this cause. 
 
 In method 12 I have not yet detected any error due to twisting the 
 wires of coils I. However, the electrostatic action of twisted wire coils 
 is immense and the warning against their use which I have given above 
 has been well substantiated by experiment. Only in case of low resist- 
 ances and low inductances or in cases like that just mentioned is it to 
 be tolerated for a moment. Connecting two twisted wires in a coil in 
 series with a resistance between them, I have almost neutralized the 
 self induction, which was one henry for each coil or four henrys for 
 them in series;! 
 
 Altogether the results of experiment justify me in claiming that 
 
ELECTRICAL MEASUREMENT BY ALTERNATING CURRENTS 313 
 
 these methods will take a prominent place in electrical measurement, 
 especially where fluid resistances, inductances and capacities are to be 
 measured. They also seem to me to settle the question as to standard 
 inductances or capacities, as inductances have a real constant which can 
 now be compared to 1 in 10,000, at least. 
 
 The new method of measuring liquid resistances with alternating 
 currents allows a tube of quite pure water a meter long and 6 Tnm. 
 diameter having a resistance of 10,000,000 ohms to be determined to 1 
 in 1000 or even 1 in 10,000. The current passing through the water 
 is very small, being at least 500 times less than that required when the 
 bridge is used in the ordinary way. Hence polarization scarcely enters 
 at all. 
 
 It is to be noted that all the methods 15 to 24 can be modified by 
 passing the main current through one coil of the electrodynamometer 
 and the branch current through the other. The deflection will then be 
 zero for a more complicated relation than the ones given. If, however, 
 one adjustment is known and made, the method gives the other equa- 
 tion. 
 
 Thus method 18 requires R t E" R'R II = Q. Hence, when this is 
 satisfied we must have the other condition alone to be satisfied. Also in 
 method 22, when we know the ratio of the self and mutual inductances 
 in the coil, the resistances can be adjusted to satisfy one equation while 
 the experiment will give the other and hence the capacity in terms of 
 the inductances. 
 
 Again, pass a current whose phase can be varied through one coil of 
 the electrodynamometer, and the circuit to be tested through the other. 
 Vary the adjustments of resistances until the deflection is zero, how- 
 ever the phase of current through the first coil may be varied. 
 
 The best methods to apply the first modification to are 15 A, 16 A 
 and B, 18, 20, 21, 22 and 24. In these, either a Wheatstone bridge can 
 be adjusted or the ratio of the self and mutual inductances in a given 
 coil can be assumed as known and the resistances adjusted thereby. 
 
 The value of this addition is in the increased accuracy and sensitive- 
 ness of the method, an increase of more than one hundred fold being 
 assured. 
 
 As a standard I recommend two or three coils laid together with their 
 inductances determined and not a condenser, even an air condenser. 
 
62 
 ELECTEICAL MEASUREMENTS 
 
 BT HENRY A. ROWLAND AND THOMAS DOBBIN PENNIMAN 
 [American Journal of Science [4], VIII, 35-57, 1899] 
 
 In a previous article * mention was made of some work then being 
 carried on at the Johns Hopkins University to test the methods for 
 the measurement and comparison of self -inductance, mutual inductance, 
 and capacity there described. 
 
 In the present paper, there will be given an account of the experi- 
 ments performed with some of the methods described in the previous 
 article, together with a method for the direct measurement of the 
 effect of electric absorption in terms of resistance. 
 
 The methods that were tried were 25, 26, 9, 3, 12 and 6. 
 
 Description of the Electrodynamometer, Dynamos, Coils, Condensers, 
 Resistances and Connections used in the Experiments 
 
 Electrodynamometer. The electrodynamometer was one constructed 
 at the University, having a sensitiveness, with the coils in series, of 1 
 scale division deflected for -0007 ampere. 
 
 The hanging coil was made up of 240 turns of No. 34 copper wire B 
 and S gauge. The coil was suspended by a bronze wire connected with 
 one terminal of the coil. The other terminal of the coil was a loop of 
 wire hanging from the bottom of the coil and attached to the side of 
 the case; both the suspension and the loop were brought out to binding 
 posts. The resistance of the coil with suspension was 21-7 ohms. 
 
 The fixed coils were made up of 300 turns each of No. 30 B and S 
 gauge copper wire. The coils were wound on cup-shaped metal forms 
 and soaked in a preparation of wax. The form was then removed and 
 the coils placed a radius apart as in the arrangement of Helmholtz. 
 
 Dynamos. There were two dynamos used, a Westinghouse alter- 
 nator, and a small alternating dynamo constructed at the University. 
 
 Journal, iv, p. 429, December, 1897; Philosophical Magazine, January, 1898. 
 
ELECTRICAL MEASUREMENTS 315 
 
 The Westinghouse dynamo was one having 10 poles so that each revo- 
 lution of the armature produced 5 complete periods. The period of 
 this dynamo was determined by taking the time of 1000 revolutions of 
 the armature. This was accomplished by having the armature make 
 an electric connection with a bell every 200 revolutions and taking the 
 time of 5 of these. The taking of the speed during every experiment 
 gave more regular results, as the speed was constantly changing, the 
 dynamo being run by the engine in the University power-house when it 
 was subject to great change of load. This dynamo had a period of 
 about 132 complete periods per second. 
 
 For the production of a current of less period than that of the West- 
 inghouse, the small alternator constructed at the University was used. 
 This dynamo was run by a small continuous Sprague motor. The arma- 
 ture of the small alternator consisted of 8 coils, which coils were fas- 
 tened flat on a German silver plate, the plate revolving between 8 field 
 pieces producing 4 poles. The object of having the coils of the arma- 
 ture on a metal plate was to secure a nearly constant speed. The metal 
 plate produced a load that varied as the velocity and due to induced 
 currents in the plate. The varying load, depending on the velocity of 
 the moving plate, produced a nearly constant speed, which rendered 
 unnecessary the constant taking of the speed. When this dynamo was 
 used, the speed was only determined two or three times during a series 
 of readings or experiments. The average of these determinations was 
 taken as the speed during the whole series of experiments under con- 
 sideration. 
 
 Coils. The coils whose inductances were determined were all made 
 in the same way, being wound on a metal form and soaked in a prepa- 
 ration of wax. When the wax was hard the metal form was removed. 
 This enabled the coils to be placed close together, as their sides were 
 flat and smooth. The coils all had the same internal and external 
 diameter, but their width varied, that being determined by the number 
 of turns that were desired. 
 
 Coils. P v External diameter 35-46 cm., internal diameter 23-8 
 cm., was made up of about 1200 turns of No. 16 B and 8 gauge single 
 covered cotton copper wire, roughly wound; the turns were not smooth; 
 self-inductance as finally determined -566 henry. 
 
 P 2 ., Same dimensions. Turns were put on evenly. The number 
 of turns was 1300 of No. 16 B and 8 single covered cotton copper wire. 
 Self-inductance -724 henry. 
 
 A. Same internal and external diameters as P, but the width was 
 
316 HENKY A. EOWLAND 
 
 4-3 cm. Number of turns 3700 No. 20 B and 8 gauge single covered 
 cotton copper wire. Self -inductance as determined 5-30 henrys. 
 
 BI B 2 . This coil was made by winding two wires in parallel and all 
 four of the terminals brought out to binding posts. Thus the coils 
 could be used as two single coils, when the coils will be denoted by the 
 symbols B^ and B 2 as the case may be, or as a single coil, the coils 5 1 
 and B 2 being joined up in series or in parallel. The dimensions of the 
 coils BI B 2 were the same as A. Each of the coils B^ and B 2 were 
 made up of 1600 turns of No. 22 B and 8 single covered cotton copper 
 wire. The self-inductance of these coils taken separately when com- 
 pared with P, which was determined absolutely, was nearly 1 henry. 
 On this account B was taken as being 1 henry, and the other coils were 
 compared with it as a standard. 
 
 C. Same dimensions as P 2 . Number of turns 1747 of No. 22 B and 
 8 single covered cotton copper wire. Self-inductance as determined 
 1-30 henrys. 
 
 Condensers. 2 and 3. Two paraffined paper condensers that had a 
 capacity of 2 and 3 microfarads respectively. 
 
 Jd Troy. A -Jd microfarad standard mica condenser built by the 
 Troy Electric Co. 
 
 Jd Elliott. A -Jd microfarad standard mica condenser built by Elliott 
 Bros. 
 
 Resistances. The resistances used in the experiments were of two 
 kinds, those wound with double wire so as to have no self-inductance, 
 as the ordinary resistance box, and those wound on frames or cards 
 which had some small self-inductance, but almost no electrostatic 
 capacity. The resistances which had self-inductance are called open 
 resistances to distinguish them from resistance boxes, and were of 
 different kinds and dimensions. 
 
 Sources of Error and Experimental Difficulties 
 
 In all work with alternating currents there are two great sources of 
 error that have to be guarded against. These are the errors that may 
 arise from the inductance of one part of the apparatus on another, as, 
 for example, the direct induction of a coil in the circuit on the coils 
 of -the electrodynamometer, and the effect of the electrostatic capacity 
 of the leads and connections. In connecting the coils great care had 
 to be taken to avoid the effect of electrostatic action of the leads and 
 connections. For if there was a current of very considerable magni- 
 
ELECTEICAL MEASUREMENTS 317 
 
 tude, the difference of potential between the terminals of the coil 
 might be great. If the connections under these circumstances were 
 made with double wire, as is customary, a great error was introduced 
 due to the electrostatic capacity of the leads. The error was sometimes 
 as much as 7 per cent (see method 24). This error could be shown to 
 be due to the electrostatic action of the leads by shifting a resistance in 
 circuit with the coil in question from one end of the double wire to 
 the other . The effect of this was to still further increase the difference 
 of potential between the leads, and this increased the error. Experi- 
 ments of this character showed the necessity of using open leads and 
 open resistances having little or no capacity in all cases in which the 
 coils experimented on and the resistance boxes used in their determina- 
 tion have a current of any considerable magnitude passing through 
 them. In several of the following methods constancy of current was 
 necessary. This was accomplished by various means that will be de- 
 scribed in their actual application. 
 
 METHODS 
 
 The methods that were tried were 25, 26, 9, 3, 12 and 6 described in 
 this Journal, December, 1897. 2 
 
 Method 25. Method of equal deflections. Absolute method for the 
 determination of self-inductance or capacity in terms of electromagnetic 
 units. 
 
 In this method the hanging coil is shunted off the fixed coils circuit, 
 and this with a non-inductive resistance in circuit with the hanging 
 coils is made the same as that of a certain inductive resistance in cir- 
 cuit with the hanging coil. The connections are made as in the Figs. 
 1, 2, where C e ibt , C r 1 e*' M +*i), C^^+W are currents. R, R', r, resist- 
 ances. They represent the entire resistance of their respective branches. 
 L represents self-inductance of the coil by which it is placed. The 
 outer circle in Fig. 1 represents the fixed coils and the small circle the 
 hanging coil of the electrodynamometer. In Fig. 2 the terminals of 
 the fixed and hanging coils are represented by F and H. D is a revers- 
 ing commutator. K is a key to send the current first through the 
 inductive and then through the non-inductive resistance. & = Z-xn, 
 n = complete alternations per sec. This is the general notation adopted 
 throughout the article. 
 
 2 Phil. Mag., January, 1898. 
 
318 
 
 HENEY A. ROWLAND 
 
 The quantity to be found is C C^ cos^, which is proportional to 
 the deflection of the hanging coil in the two positions of K. 
 In one position 
 
 FIG. 2. 
 
 Therefore 
 
 In the other position of K 
 Therefore 
 
ELECTRICAL MEASUREMENTS 319 
 
 0=0, as is an angle whose tangent is , and (7 = nearly. In the 
 case of equal deflection D = D' and therefore 
 VD=(R'-R) (R+r} 
 
 If capacity had been used in the place of self-inductance the formula 
 would be 
 
 If self-inductance and capacity were used in series 
 
 The application of this formula to the measurement of self-induc- 
 tance gave results that agreed to within the accuracy with which the 
 period of the alternations could be determined. That is, the results 
 agreed to within about 1 per cent. In the determination of L the 
 resistance in circuit R was varied from the least possible resistance as 
 determined by the coils up to 1000 ohms and more, and the self- 
 inductance was determined under these various conditions. These 
 results agreed among themselves, and were apparently independent of 
 the resistance in circuit with it. In the application of this method to 
 the determination of capacity, however, great trouble was encountered, 
 as the capacity apparently varied both with the resistance in circuit 
 with it and with the period. This variation was regular for each period, 
 the value derived depending on the resistance in circuit. This irregu- 
 larity of derived value of the capacity led to the investigation and 
 development of Maxwell's formula on the effect of absorption, a neces- 
 sary characteristic of heterogeneous substances. 
 
 When the formula was deduced, as may be seen in the article already 
 referred to, the absorption comes in as an added resistance, the resist- 
 ance being constant for a given period. By an inspection of the results 
 this was found to be the case. The finding of the resistance due to 
 absorption in this method is one of approximation, but the values 
 deduced compare very favorably with those determined by direct meas- 
 urement, as will be seen later when various results are collected. In 
 the actual experiments the condensers used were two paraffined paper 
 condensers of about 2 and 3 microfarads. The currents used had 
 different periods, as seen in the table following, where n = 133, 53-3, 
 31 -9 and 14. 
 
 The process was to place in the condenser circuit a resistance R, and 
 
320 HENEY A. EOWLAND 
 
 then to move the key K back and forth until R' was found that gave 
 the same deflection. D, Fig. 2, was now reversed and the process 
 repeated. This was repeated with different values of R and n and the 
 apparent capacity. This gave great variation of apparent capacity with 
 different values of R, which should not be the case, and, therefore, 
 gave a means of finding the resistance due to absorption or absorption 
 resistance, as we will designate, by approximation. As the effect of 
 absorption is a resistance it is possible to find what resistance, if added 
 to R, will make all the values of the capacity as determined for the 
 different values of R the same. Therefore it should be the same for 
 any two values of R. Calling the two values of R in the two cases 
 R % and J? 2 respectively and the two corresponding values of R', R^', and 
 R%, and let A be the added resistance due to absorption, the capacity 
 should be the same in the two cases, or 
 
 + r) - (#- 
 
 A _ - 
 
 From this A is found for the period used. By doing this for a 
 number of different values of R, the true value of A is approximated. 
 A was thus found for the condensers 2 and 3 microfarads with different 
 values of n. The calculations were again performed adding to the 
 different values of R a constant resistance A. The capacity that was 
 found when A is added to R is called the corrected capacity. In the 
 table below are collected the corrected values of the capacities together 
 with n and the resistance A. 
 
 Capacity 4-94 4-96 4-96 4-64 microfarads. 
 
 n 131-1 53-3 31-98 14- complete alternations. 
 
 A '5-19 20-5 34-09 139-62 absorption resistance in ohms. 
 
 The last value of the capacity seems 'to be an error, possibly one of 
 calculation. However, the results seem to show a nearly constant 
 capacity, but a resistance increasing rapidly with decrease of period, as 
 Maxwell's formula shows. The constant value of the capacity remains 
 to be explained. 
 
 But in the above, determinations of absorption resistance are by 
 approximation. Professor Eowland has, therefore, devised a method 
 by which it can be measured directly. This method, with the results 
 that have been derived by it, will now be given. 
 
ELECTEICAL MEASUBEMENTS 
 
 321 
 
 Method for the Direct Measurement of Absorption Resistance 
 In a Wheatstone bridge (Fig. 3) let the resistance of the different 
 
 arms be denoted by R,, R', R tl , R" and r. Let J^have in circuit a 
 
 self-inductance L t and let r have in circuit with it a self-inductance. 
 Let C, ibt be the current through R, and C ** + *) be the current 
 
 through r when a periodic electromotive force is applied to a and d in 
 
 the figure. 
 
 Let C' be the current through R t , and C" be the current through r 
 
 when there is a constant difference of potential between a and d. The 
 
 ratio of the current in this case is 
 
 c' 
 
 R"R-R'R 
 
 R (R" 
 
 _ 
 r(R' + R"} 
 
 i 
 
 i 
 
 FIG. 3. 
 
 
 R, \ 
 R' b / n 
 
 SA 
 
 ,_ Kn a 
 
 a 
 
 v 
 
 J r c 
 
 
 
 
 / 
 R" 
 
 
 FIG. 4. 
 
 When a periodic electromotive force is applied to a and d, the ratio 
 of the currents in this case is 
 
 __ 
 
 C 1 ~ R (R >r +RJ + r (R~+~R') + ibl (R + R") 
 
 Separating the real and imaginary parts 
 o ,_ (R"R 
 
 If now the fixed coils of the electrodynamometer are placed in the 
 R, arm of the bridge, and the hanging coil is placed in cross connection 
 of the bridge, as in Fig. 4, the different resistances may be adjusted 
 21 
 
322 
 
 HENRY A. KOWLAXD 
 
 until there is no deflection, in which case <f> = 90 or cos<= 0, therefore 
 
 (R"R t - RRJ [#' (R" + RJ + r (R' + R"}-] + VILfl' (R' + R"} = , 
 
 R" (R + R") 
 
 .'. R'R. = R'R.. - VIL. 
 
 I J? f ( J?" i J? \ i /. / V i ZP"\ ' 
 K \t T -tv.) -\- T (^JV + JK ) 
 
 If in connection with L' a capacity C is added, the formula becomes, 
 substituting for L /t L t j~- . 
 
 (R'R' + .R") 
 
 c J R' (R" + ) - r (R + R"} ' 
 In most cases since I and L, are generally the self-inductances of the 
 
 instruments the term & 2 1 L t can be neglected in comparison with - 
 
 C 
 
 and the equation becomes 
 
 Tftt T> T>t -p , I R" (R 1 + R ) 
 
 * - * + ~ 
 
 FIG. 5. 
 
 In this equation R, includes both the ohmic and the absorption resist- 
 ance. The value of R, is determined in terms of known quantities, 
 that is the resistance and 2 and C. It was not necessary that I and C 
 should be exactly known as the last term in the equation above plays 
 the part of a correction term, and is in all cases below small and in 
 some cases negligible. The capacities that were used in the experi- 
 ments were the 2 and 3 microfarads, the ^ microfarad Elliott condenser, 
 and the microfarad Troy condenser. 
 
 Experiments. The process of experimenting was to apply a periodic 
 electromotive force to a and d, and to adjust the different resistances 
 until there was no deflection of the coil in the same way as in the 
 ordinary measurement of resistance on a Wheatstone bridge. The 
 different resistances R', R", R n and r being known, the apparent value 
 of the resistance R, was found, and knowing the ohmic resistance of 
 the R, circuit, the absorption resistance appears as the difference. 
 
ELECTBICAL MEASUBEMENTS 
 
 323 
 
 Some interest lies not alone in that the method is applicable, but that 
 it confirmed the supposition that absorption resistance acts as an ordi- 
 nary ohmic resistance in series in the circuit. This was confirmed by 
 the fact that when condensers were in series and in parallel, their 
 absorption resistances acted under these conditions like ohmic resist- 
 ances, being increased in the one case and decreased in the other, and 
 in the right ratio. This agreement was not exact, as the absorption 
 resistance was extremely sensitive both to change of period and change 
 of temperature. The great sensitiveness to change of temperature was 
 shown either by letting the current go through the condensers for a 
 little time, or placing the condensers before a hot air flue; in either 
 case after cooling, the absorption resistance returned to its original 
 value. The cooling was very slow, as there was very little radiation 
 from the condensers inclosed in wooden boxes. 
 
 The results are now given for the condensers 2 and 3 microfarads. 
 In the calculation of the results the last term of the equation, that is 
 
 7 ry> f nr , 
 
 , , ^- - - 
 
 
 condensers 2 and 3 microfarads were used. 
 
 has been left out, as it was very small when 
 
 
 CONDENSERS 2 AND 3 MICROFARADS IN 
 
 PARALLEL. 
 
 
 =134, Z=-0007 .-. 
 
 last 
 
 term negligible. 
 
 R" 
 
 R y/ r R' 
 
 
 R/ 
 
 Resis. of 
 R' circuit 
 in ohms. 
 
 Resistance 
 due to 
 absorption. 
 
 422- 
 
 6 488-6 5457-3 347 
 
 9 
 
 39-29 
 
 33 
 
 77 
 
 5-30 
 
 1488- 
 
 6 488-2 
 
 123 
 
 4 
 
 40-50 
 
 
 
 
 6-73 
 
 984- 
 
 1 
 
 
 82 
 
 1 
 
 40-72 
 
 33 
 
 81 
 
 6-91 
 
 2671- 
 
 6 
 
 
 22 
 
 5 
 
 41-116 
 
 | 
 
 
 7-30 
 
 423- 
 
 
 
 
 357 
 
 3 
 
 41-237 
 
 
 
 
 7-42 
 
 5474- 
 
 3 
 
 
 464 
 
 5 
 
 41-42 
 
 
 i 
 
 7-61 
 
 6734- 
 
 
 
 374 
 
 9 
 
 41-67 
 
 
 
 
 7-86 
 
 1 ohm in R"=f 
 
 scale divisi 
 
 n. 
 
 
 
 
 i 
 
 
 7486- 
 
 
 
 638 
 
 6 
 
 41-64 
 
 
 i 
 
 7-83 
 
 9466- 
 
 
 
 81 
 
 15 
 
 41-85 
 
 
 i 
 
 8-04 
 
 Condensers 2 and 3 placed before the register and heated for 1 hour : 
 
 7489-7 488-27 713-8 46-534 34-33 12-20 
 
 After standing 1 hours in air at temperature of 12 -2 C. condenser 
 has been open so that resistances have been cooled: 
 
 1240-5 487-8 109- 42-86 34- 8-86 
 
 After standing some little time: 
 
 7482-5 487-8 " 651-6 42-47 34- 8-49 
 
 The above table shows conclusively the heating of the condenser by 
 the current, and the dependence of the absorption upon the temper- 
 ature. 
 
K" 
 
 R// 
 
 R, 
 
 r 
 
 R, 
 
 348-5 
 
 488-6 
 
 396-3 
 
 11020-7 
 
 55-61 
 
 7488- 
 
 it 
 
 849-2 
 
 u 
 
 55-41 
 
 (i 
 
 (i 
 
 844-1 
 
 4026- 
 
 55-07 
 
 3485- 
 
 u 
 
 396-1 
 
 u 
 
 55-58 
 
 324 HENRY A. ROWLAND 
 
 CONDENSERS 2 AND 3 IN PARALLEL. N=57-6. 
 
 R, in 
 ohms. A. 
 
 33-77 21-84 
 
 " 21-64 
 
 21-30 
 
 21-81 
 
 Average, 21-63 
 N=56-6 per second. 
 3485- 200-24 976-7 4026- 56-00 22-23 
 
 Comparing these values with those found in the use of method 25 
 the agreement is at once apparent. 
 
 N= _ 134- 131- _ 57-6 _ 56-6 _ 53- 
 
 Method 25 _ 5-19 20-5 
 
 Direct measure- 5-30 cold 21-63 22-23 
 
 ment. 7-00 warm 
 
 It should be remembered, in comparing the results, that the values 
 obtained by method 25 would naturally be smaller than those found by 
 direct measurement, as in method 25 the current going through the 
 condensers was extremely small; there was therefore practically no 
 heating. 
 
 The experiments that confirm the mathematical theory that the 
 absorption resistance could be treated as ordinary ohmic resistance were 
 performed with the two condensers, ^ Troy and ^ Elliott microfarad 
 condensers. These are next given. 
 
 In these results it was necessary to take into account, in the calcula- 
 tion of the apparent value of R,, the last term of the equation, that is 
 
 L R" (R' + R"} 
 
 c R' 
 
 $ Troy and ^ Elliott in series, 1 o'clock. 
 
 Apparent Ohmic resist- Absorption 
 value ance resistance 
 
 R" R/, R' r ofR, of R, A. 
 
 4751-8 499-9 404-8 4754- 43-141 34-143 8-998 
 
 ^ Troy, 2 o'clock. 
 
 4750- 497 75 352-4 37-288 34-144 3-144 
 
 i Elliott, 2.45 o'clock. 
 
 4749-3 497-67 390-3 " 41-260 " 7-116 
 
 Troy and ^ Elliott in parallel, 4 o'clock. 
 
 4749-3 497-6 350-23 " 36-94 34-15 2-79 
 
 Troy and Elliott in series. 
 
 4748-5 497-55 418-15 " 44-612 34-12 10-492 
 
ELECTRICAL MEASUREMENTS 325 
 
 Calculating what the absorption resistance should be for Troy and 
 ^ Elliott in series, from the absorption resistances of the two con- 
 densers when determined separately, it is equal to 10-26 ohms, which is 
 greater than the first and less than the last value above, showing that 
 the condensers were heating during the experiments. Calculating the 
 absorption resistance of Troy and -J Elliott in parallel in the same 
 way, it is equal to 2-209 ohms, which is less than the value afterwards 
 obtained by experiment for the same reason. 
 
 The method was shown not to be based on any false supposition, by 
 substituting in place of the condenser a coil of known self-inductance. 
 When this was done the value of R^ as calculated from the other resist- 
 ances and the self-inductances should be the same as the actual ohmic 
 resistance of the circuit. 
 
 This was tried with two coils P 2 and A and the agreement was re- 
 markably close, as seen in the next table. 
 
 Coil P used in place of condenser in the E t circuit: 
 
 Deduced value Actual value 
 
 R" R,, R' r ofR, of R, 
 
 474-9 487-8 758-2 5457- 77-86 77-8 
 
 Coil A in place of condenser in the R, circuit: 
 
 474-9 487-8 218-3 " 224-12 223-9 
 
 In these experiments great care was taken that the measurements 
 of the resistances were performed immediately after the adjustment. 
 In this way the actual resistances at the time of the experiment were 
 obtained, and so the effect of the heating by the current was some- 
 what eliminated. 
 
 Methods 26, 9 and 3 give good results, but the methods that gave 
 the most satisfaction were methods 12 and 6, method 12 being for the 
 comparison of two self-inductances and method 6 for the comparison 
 of a self-inductance with a capacity. These give some remarkable 
 results, the theory and deductions of the methods being as follows : 
 
 Method 12. Zero Method for the Comparison of two 8 elf -Inductances 
 
 Let the connections be made as in the figure where the hanging coil 
 and the fixed coils are in two distinct circuits. 
 
 Let C<f iu etc. be the currents, A' and A" reversing commutators, 
 R", R and r the resistance of the different circuits, L" and L the self- 
 inductances, If the mutual inductance of the coils B\ and B 2 by which 
 it is placed. When a periodic electromotive force a m is applied to 
 A, B the quantity to be found is C^ C 8 cos ($ 3 0J where <p, fa 
 is the difference of phase. 
 
326 HENRY A. KOWLAND 
 
 The current in the R" circuit is then 
 
 C ci (bt + < J^/ 
 ^ r - T>H 
 
 + ibL" 
 
 The current in the E circuit is 
 
 = (7 e t. 
 
 Substituting the value of C" e fbt in equation (1) and simplifying, it 
 becomes 
 
 "r ibL"r 
 
 FIG. 6. 
 
 Therefore the deflection is proportional to 
 cos ($, 0,) = (7|~ 
 
 and the condition for zero deflection is 
 
 - VLMR'r + VL"Mr(R+r) = 0, 
 L _R+r 
 
 The condition therefore of zero deflection is independent of M . But 
 M is one of the factors of the electromotive force in the R" circuit, and 
 on it therefore depends the sensitiveness, as it determines the current 
 through the R" circuit. In the first figures of this method the fixed 
 coils are in the R" circuit, and the hanging coil in the R circuit, but 
 this is not necessary, as the fixed and hanging coils can be reversed. 
 The choice of which of the above arrangements should be used depends 
 
ELECTEICAL MEASUREMENTS 
 
 327 
 
 on the impedances of the two circuits, as other things being equal the 
 smaller current should go through the hanging coil. 
 
 Experiments. The coils used in the experiments were coils P lf P 2 , 
 C, B 1} B 2 , and A, which coils are described on page 315. From the 
 dimensions of P 2 and its self-inductance as found by method 25, B t was 
 designed to have a self-inductance of one henry. This will be shown 
 to be nearly the case. For ease of comparison B 1 has been taken in 
 the calculations of the results as being equal to one henry, and the 
 other coils were compared with this coil as a standard. 
 
 In these experiments the connections were made as in the figure 7, 
 the coil BI that was taken as the standard being placed in circuit with 
 the fixed coils of the electrodynamometer as L" and the resistance of 
 this circuit was unaltered during the experiments in any particular 
 series. The coils whose self-inductances were to be determined were 
 placed in the hanging coil circuit and the resistance R was changed 
 until there was no deflection. The resistance of the two circuits, R" 
 and R -{- r were then measured by a Wheatstone bridge. 
 
 The resistance r was in all cases small in order that (7 ibt should be 
 large, and therefore by induction <7 1 *< M +*> the current through the 
 fixed coils was made large and the instrument sensitive. The method 
 
328 HENRY A. KOWLAND 
 
 being very accurate, as will be seen later, great care had to be used to 
 eliminate all sources of error, as for example, electrostatic action. In 
 the first trial of the method small differences were noticed in the ratio 
 of two self-inductances, depending both on the resistances used, and 
 also on the connections of the coils, whether the leads were double, 
 single, long or short. The same variation was noticed when several 
 coils were joined in series and compared with another coil, and when 
 these coils were compared separately and their sum taken. 
 
 This irregularity led to an investigation of the effects of various 
 resistances and connections in one of the circuits, the other circuit 
 being unaltered. A little farther on, the variation in the deduced value 
 of the self -inductance of one of the coils, when different resistances and 
 leads were used, will be given, which variation was caused by the 
 electrostatic action of the connections, etc. (Page 316.) 
 
 The necessity of eliminating electrostatic action made obligatory the 
 use of open resistances which had small self-inductances. These re- 
 sistances were of three kinds resistances in the form of spirals, resist- 
 ances wound on thin strips of micanite or paper, and those wound on 
 open frames; see page 316. 
 
 The self-inductance of the first and second classes of resistances was 
 very small, as in one case there were only a few turns, and in the other 
 the cross-section was very small. 
 
 The third class were those wound on frames whose self-inductances 
 were calculated. There were several resistances of 2000 ohms each, 
 whose self -inductances were -0000436 henry, which would hardly affect 
 the phase of the current or the impedance of the circuit. 
 
 These coils were subdivided into resistances of various amounts. 
 Another frame resistance used was of 7463 ohms divided into parts of 
 about 250 ohms each. The self-inductance of the entire 7463 ohms 
 was -000105 henry. 
 
 As the open resistances were not divided into small amounts it was 
 necessary to use resistance boxes for adjustment; as few ohms as possi- 
 ble were used in each case. 
 
 From the fact that the coils of the electrodynamometer had self- 
 inductance a correction was introduced in order that the ratio of the 
 resistances should give the ratio of the self-inductances of the coils 
 direct. 
 
 The value of this correction in ohms was calculated as follows: 
 
ELECTRICAL MEASUREMENTS 329 
 
 Calculation of Correction Due to Fixed and Hanging Coils 
 
 Self-inductance of fixed coils =f= *0164 henry 
 " " " hanging coil h = -0007 " 
 
 Correction due to fixed coils. From an inspection of the tables it 
 is seen that 
 
 L R+r L R + r 
 
 01 
 
 B,+f~ R" 1.0164 ~~~90T' 
 
 rhere L is the self -inductance of some coil and R -\- r is the corre- 
 sponding resistance. B, is taken as equal to 1 henry 
 
 L 
 
 R + r~ 902 ' 
 But the comparison of L with B^ = 1 is wanted, therefore both numer- 
 
 ator and denominator of ~ ~ are divided by 1-0164 or 
 
 yo 
 
 . L \=B 
 
 R+r 887-45 ' 
 . L_ R + r 
 
 B ~ 887-45 ' 
 
 That is, the self-inductance of -0164 henry of the fixed coils produced a 
 correction of 887-45 902 = 14-55 ohms, which must be applied to 
 the R" circuit if the self-inductance of that circuit is to be considered 
 as 1 henry. 
 
 Correction due to hanging coil. The self-inductance = -0164 henry 
 of the fixed coils gives a correction of * 14-55 ohms, therefore the self- 
 inductance -0007 henry of the hanging coil gives a correction of -62 
 ohms to the R -\- r circuit. Applying these corrections, the results 
 obtained for the several coils under various conditions are given below. 
 The results are given in the following order. 
 
 First. The values are calculated using double leads in the circuits 
 but open resistances as far as possible. 
 
 Second. The variation of the apparent value of the self-inductance 
 of one of the coils with different positions of the coil, resistances, and 
 different kinds of leads. 
 
 Third. Short leads separated about 6 inches and crossed, used with 
 all the coils except B^. 
 
 Fourth. Open leads aad open resistances in the determinations. In 
 the table R" was open resistance plus the resistance of coil B^ and 
 fixed coils of instrument. R + r was made up of the small coil and 
 open resistance plus the amount in the Queen ordinary resistance box. 
 
330 
 
 HENRY A. KOWLAXD 
 
 After all the inductive effect of the leads was removed and the ordi- 
 nary resistance box used as little as possible, there was a different value 
 obtained for the ratio of the self -inductances dependent on the position 
 of the reversing commutator A'. With all the coils used the greater 
 value occurred with the same position of A'. This was due to the 
 electrostatic action between the coils B^ and B 2 , for if the terminals of 
 the coil B 2 and the commutator A' were reversed at the same time, 
 there was no change in the value of the ratio of the inductances. This 
 showed that it was dependent on the coil itself and not on the leads 
 and it could therefore not be eliminated. 
 
 It is to be noticed that the values obtained for the lower number 
 of alternations are always greater than those found with the higher 
 number of alternations. This was caused by the electrostatic action of 
 the turns of the coil on each other. In the case of the coil P 2 this effect 
 would be caused by supposing a capacity of -0007 microfarads shunted 
 across the terminals. 
 
 The results are now given comparing the different coils with B^ as 
 a standard and equal to 1 henry. 
 
 DOUBLE LEADS OF BELL WIRE AND OPEN RESISTANCE 
 r = 106 ohms, n = 45 complete periods per second. 
 
 ". Correc. 
 
 Coils. 
 
 + C 
 
 901-6 
 
 -14-55 
 
 901-7 
 
 
 
 Cor- Aver- 
 
 Com. 
 
 
 Queen. 
 
 R+r. rec. age. 
 
 A'. 
 
 Ratio. 
 
 887-05 292 
 
 2300 
 
 2 -62 2304-9 
 
 1 
 
 2-5983 
 
 
 310 
 
 2311 
 
 
 
 
 2 
 
 
 
 19 
 
 1158 
 
 3 
 
 1159-0 
 
 1 
 
 1-3099 
 
 
 22 
 
 1161 
 
 2 
 
 
 2 
 
 
 
 103 
 
 1659 
 
 
 1661-2 
 
 1 
 
 1-8727 
 
 
 109 
 
 1664 
 
 8 
 
 
 2 
 
 
 
 92 
 
 1800 
 
 2 
 
 1802-6 
 
 1 
 
 2-0288 
 
 
 99 
 
 1806 
 
 5 
 
 
 2 
 
 
 887-15 149 
 
 4776 
 
 5 
 
 4786-5 
 
 1 
 
 5-3956 
 
 196 
 
 4818 
 
 
 
 
 2 
 
 
 Current increased about 2 times. 
 
 A + C 901 
 
 902 
 
 P, 
 
 
 141 
 
 4787 
 
 
 
 4781 
 
 3 
 
 1 
 
 5-3898 
 
 
 184 
 
 4807 
 
 
 
 
 2 
 
 
 887 
 
 05 211 
 
 5936 
 
 
 5958 
 
 3 
 
 1 
 
 6-7170 
 
 
 264 
 
 5982 
 
 
 
 
 2 
 
 
 
 51 
 
 6575 
 
 5 
 
 6602 
 
 5 
 
 1 
 
 7-4430 
 
 
 104 
 
 6631 
 
 
 
 
 
 2 
 
 
 887 
 
 45 158 
 
 4778 
 
 9 
 
 4795 
 
 25 
 
 1 
 
 5-4036 
 
 
 192 
 
 4813 
 
 
 
 
 2 
 
 
 
 183 
 
 1146 
 
 5 
 
 1146 
 
 7 
 
 1 
 
 1-9922 
 
 
 186 
 
 1148 
 
 5 
 
 
 
 2 
 
 
 
 7 
 
 643 
 
 15 
 
 642 
 
 67 
 
 1 
 
 7242 
 
 
 8 
 
 643 
 
 6 
 
 
 
 2 
 
 
 
 91 
 
 502 
 
 5 
 
 502 
 
 16 
 
 1 
 
 5658 
 
 
 
 503 
 
 1 
 
 
 
 2 
 
 
ELECTRICAL MEASUREMENTS 
 
 331 
 
 DOUBLE LEADS. n=about 133 complete alternations per sec. 
 
 Coils. R" Correc. Queen. R+r. 
 
 P, 901-9 14-55 887-85 90 + s 500-4 
 
 u < 500-23 
 
 P., " 3 639-35 
 
 u " 4 639-6 
 
 A 901-87 887-32 ? 4742-2 
 
 " 133 4760-0 
 
 C 901-9 887-35 44 1151-4 
 
 44 1151-4 
 
 Cor- Aver- 
 
 Coi 
 
 rec. age. 
 
 A' 
 
 f-62 499-69 
 
 1 
 
 
 
 2 
 
 
 638-85 
 
 1 
 
 
 
 2 
 
 
 4750-48 
 
 1 
 
 
 
 2 
 
 
 1150-94 
 
 1 
 
 
 
 8 
 
 Ratio. 
 5631 
 
 7198 
 
 5-3537 
 
 1-2970 
 
 In the above determinations the coils were arranged in the way as 
 indicated in the figure having leads of double bell wire. 
 
 A SERIES OF DETERMINATIONS OF A UNDER VARIOUS CONDITIONS. 
 Open resistance R on table (original position). 
 
 Cor- 
 
 Coils. R" Correc. Queen. R+r. rec. 
 
 A 902-0 14-55 887-45 149 + s 4776-5 -62 
 " " " " 196 + s 4818- " 
 
 " 901-95 " 887-4 ? 4783-5 " 
 
 " " " " 190 + s 4808-5 " 
 
 Open resistance E moved up to coil A (b^). 
 
 Aver- Com. 
 age. A'. Ratio. 
 
 4786-58 1 5-3936 
 
 2 
 4795-38 1 5-403 
 
 2 
 
 u " ? 4518- " 4517-38 2 5-0905 
 
 Open resistance E moved to the other side of A (& 2 ). 
 
 144 + s 4518- " 4518-88 1 5-0922 
 <( u u u ci 4521- " 2 
 
 Coil A placed in P x position and open resistance E restored to its 
 position, and 159' of double wire added to the circuit. 
 
 Cor- Aver- Com. 
 
 Coils. R". Correc. Queen. R+r. rec. age. A'. Ratio. 
 
 A 901-95 14-55 887-4 547- + 4129 -62 
 
 547 " 1 
 
 4676 
 
 583 + 4129 
 583 
 
 4712 
 
 4693-38 2 5-2888 
 
 Coil A at end of double wire 69' + 159' = 228' long. 
 
 607 + 4129 
 607 
 
 4736 
 
 634 + 4129 
 634 
 
 4763 
 
 New leads placed in B circuit, the wires were about 6" from each 
 other. 
 
332 
 
 HENRY A. EOWLAND 
 
 Coils. R". Correc. Queen. R+7-, 
 
 A 902-6 14-55 888-05 569+4129 
 
 " " 569 
 
 4698 
 
 594 + 4129 
 594 
 
 Open resistance placed next Coil A. 
 
 4723 
 
 663 + 4129 
 663 
 
 4292 
 
 Cor- Com. 
 
 rec. Average. A'. Ratio. 
 
 4709-88 1 5-3088 
 2 
 
 4791-3 1 5-3956 
 4292- 2 
 
 7 
 0-6 
 
 In the following all connections were made with open leads, and open 
 resistances were used. 
 
 Pe- 
 
 Cor- Aver- Com. 
 
 riod. 
 
 Coils. 
 
 R" 
 
 Correc. 
 
 
 Queen. 
 
 R+r. 
 
 rec. age. 
 
 A'. 
 
 Ratio. 
 
 40 
 
 P, 
 
 902- 
 
 -14-55 887- 
 
 46 
 
 90 + s 
 
 503 
 
 07 
 
 -62 502 
 
 71 
 
 1 
 
 5664 
 
 'i 
 
 it 
 
 it 
 
 u u 
 
 
 90+s 
 
 503 
 
 6 
 
 M 
 
 
 2 
 
 
 133 
 
 it 
 
 it 
 
 u it 
 
 
 88 + s 
 
 522 
 
 53 
 
 ti 
 
 
 1 
 
 
 n 
 
 11 
 
 ti 
 
 it u 
 
 
 88 + 8 
 
 502 
 
 15 
 
 501 
 
 72 
 
 2 
 
 5653 
 
 40 
 
 P Q 
 
 902 55 
 
 888 
 
 
 17 + s 
 
 644 
 
 3 
 
 u 
 
 
 1 
 
 
 M 
 
 u 
 
 it 
 
 u u 
 
 
 18 + s 
 
 644 
 
 76 
 
 " 643 
 
 91 
 
 
 
 7251 
 
 133 
 
 it 
 
 it 
 
 11 u 
 
 
 17+s 
 
 643 
 
 05 
 
 M 
 
 
 1 
 
 
 u 
 
 it 
 
 ii 
 
 u 11 
 
 
 17 + s 
 
 643 
 
 1 
 
 " 642 
 
 45 
 
 2 
 
 7234 
 
 40 
 
 C 
 
 902-4 
 
 " 887- 
 
 So 
 
 28 + s 
 
 1159 
 
 6 
 
 ti 
 
 
 1 
 
 
 it 
 
 u 
 
 " 
 
 it ti 
 
 
 28 + s 
 
 1159 
 
 1 
 
 1158- 
 
 73 
 
 2 
 
 1-3050 
 
 133 
 
 ti 
 
 it 
 
 it u 
 
 
 24 + 8 
 
 1157 
 
 
 
 ii 
 
 
 1 
 
 
 ii 
 
 tt 
 
 M 
 
 it it 
 
 
 26 + s 
 
 1158 
 
 8 
 
 " 1157 
 
 28 
 
 2 
 
 1-3034 
 
 40 
 
 C + PI 
 
 902- 
 
 ' 887 
 
 45 
 
 105 + s 
 
 1658 
 
 8 
 
 it 
 
 
 1 
 
 
 ii 
 
 it 
 
 it 
 
 I 11 
 
 
 110 + s 
 
 1664 
 
 1 
 
 1660 
 
 77 
 
 2 
 
 1-8713 
 
 133 
 
 it 
 
 u 
 
 1 If 
 
 
 101+8 
 
 1656 
 
 7 
 
 ti 
 
 
 1 
 
 
 M 
 
 it 
 
 f- 
 
 t II 
 
 
 106 + s 
 
 1660 
 
 3 
 
 " 1657 
 
 96 
 
 2 
 
 1 8683 
 
 40 
 
 C + P a 
 
 902-5 
 
 ' 887- 
 
 95 
 
 10 + 8 
 
 1803 
 
 
 
 u 
 
 
 1 
 
 
 'i 
 
 tf 
 
 it 
 
 u u 
 
 
 12+8 
 
 1805 
 
 
 
 " 1803 
 
 3 
 
 2 
 
 2-0261 
 
 133 
 
 II 
 
 it 
 
 ti i< 
 
 
 8+8 
 
 1800 
 
 5 
 
 n 
 
 
 1 
 
 
 ii 
 
 II 
 
 11 
 
 It 11 
 
 
 8 + 8 
 
 1800 
 
 2 
 
 " 1799 
 
 65 
 
 2 
 
 2-0221 
 
 40 
 
 PI + PS 
 
 902-4 
 
 " 887- 
 
 85 
 
 60 + s 
 
 2306 
 
 3 
 
 2307 
 
 98 
 
 1 
 
 2-5995 
 
 
 + c 
 
 
 
 
 
 
 
 
 
 
 
 u 
 
 11 
 
 u 
 
 u u 
 
 
 I 
 
 2310 
 
 9 
 
 u 
 
 
 2 
 
 
 133 
 
 11 
 
 ii 
 
 11 11 
 
 
 56 + s 
 
 2304 
 
 1 
 
 2304 
 
 13 
 
 1 
 
 2-5951 
 
 ii 
 
 II 
 
 it 
 
 tt u 
 
 
 57 + s 
 
 2305 
 
 4 
 
 tt 
 
 
 2 
 
 
 40 
 
 A 
 
 902-43 
 
 " 887- 
 
 88 
 
 85 + s 
 
 4703 
 
 
 ti 
 
 
 1 
 
 
 n 
 
 it 
 
 u 
 
 II 11 
 
 
 106 + s 
 
 4724 
 
 2 
 
 " 4712 
 
 98 
 
 2 
 
 5-3080 
 
 133 
 
 it 
 
 902-4 
 
 " 887- 
 
 85 
 
 82 + 8 
 
 4704 
 
 2 
 
 it 
 
 
 1 
 
 
 u 
 
 ti 
 
 it 
 
 11 It 
 
 
 85 + s 
 
 4707 
 
 
 
 ii 4704 
 
 98 
 
 2 
 
 5-2991 
 
 40 
 
 A + C 
 
 902-35 
 
 887- 
 
 8 
 
 1146+s 
 
 9149 
 
 5 
 
 " 
 
 
 1 
 
 
 
 2M 
 
 
 
 
 
 
 
 
 
 
 
 it 
 
 11 
 
 u 
 
 u u 
 
 
 1227 + 8 
 
 9233 
 
 5 
 
 " 9190 
 
 88 
 
 2 
 
 10-3515 
 
 133 
 
 u 
 
 902-4 
 
 887- 
 
 85 
 
 1170 + s 
 
 9171 
 
 7 
 
 it 
 
 
 1 
 
 
 11 
 
 ti 
 
 11 
 
 u u 
 
 
 1194 + s 
 
 9191 
 
 7 
 
 9181 
 
 08 
 
 2 
 
 10-3395 
 
 40 
 
 A + C 
 
 902 35 
 
 " 887- 
 
 8 
 
 111+s 
 
 2550 
 
 9 
 
 ii 
 
 
 1 
 
 
 
 + 2M 
 
 
 
 
 
 
 
 
 
 
 
 n 
 
 u 
 
 u 
 
 it it 
 
 
 146 + 8 
 
 2556 
 
 4 
 
 2553 
 
 03 
 
 2 
 
 2-8716 
 
 133 
 
 u 
 
 u 
 
 u u 
 
 
 38+s 
 
 2548 
 
 7 
 
 u 
 
 
 1 
 
 
 11 
 
 u 
 
 u 
 
 u it 
 
 
 38 + s 
 
 2548 
 
 7 
 
 " 2548 
 
 08 
 
 2 
 
 2-8701 
 
 40 
 
 A + C 
 
 902 6 
 
 888-05 
 
 123 
 
 5852 
 
 
 ii 
 
 
 1 
 
 
 u 
 
 11 
 
 u 
 
 ii if 
 
 
 169 
 
 5898 
 
 
 " 5880 
 
 13 
 
 2 
 
 6-6225 
 
 133 
 
 it 
 
 u 
 
 u u 
 
 
 134 
 
 5863 
 
 5 
 
 u 
 
 
 1 
 
 
 u 
 
 it 
 
 ii 
 
 u u 
 
 
 140 
 
 5869 
 
 
 
 " 5865 
 
 63 
 
 2 
 
 6-6054 
 
ELECTRICAL MEASUREMENTS 333 
 
 The above results show to what accuracy self-inductances of different 
 values can be compared to each other, or to one of the self-inductances 
 taken as a standard. The reason that the agreement between the 
 different determinations is not greater than it is, even though the elec- 
 trodynamometer was sensitive to a change of 1 part in 10000 in R -\- r, 
 is that there was always some little heating of the resistances, and 
 although they were measured in each determination on a Wheatstone 
 bridge, still it was impossible to determine the exact resistance at the 
 time that the experiment was made. This slight effect of the heating 
 of the resistance would not enter in the comparison of two nearly equal 
 self-inductances, that is the comparison of a coil with a standard. The 
 accuracy of this comparison can be made to depend on the accuracy 
 with which R -j- r can be determined for zero deflection, and this can 
 be done to about 1 part in 10000. To do this, first the standard coil 
 and the coil to be compared are substituted in turn in place of L in 
 figure; they are thus compared separately to a third coil. But as the 
 standard and the coil to be compared are nearly equal in self-inductance, 
 the difference or self-inductance can be determined by the amount 
 necessary to change R -\- r, and this change will be nearly independent 
 of the slight heating of the resistances. To make a coil of the same 
 self -inductance as the standard, the standard is placed in the R -\- r 
 circuit and the value of R -\- r is found that produces no deflection. 
 The coil to be compared is then substituted in place of the standard 
 keeping R -)- r fixed, and the self-inductance of this coil is changed 
 until there is no deflection, as in the case of the standard. The 
 accuracy with which this can be done depends on the accuracy with 
 which R -f- r can be set or 1 part in 10000. The method therefore 
 gives a means of comparing and constructing coils to agree in self- 
 inductance to within 1 part in 10000 with a standard. 
 
 Method 6. Zero Method for the Comparison of 8 elf -Inductance with 
 
 Capacity 
 
 This method resembles method 12 and the connections are made as 
 in the figures when both the hanging coil and fixed coils of the electro- 
 dynamometer are shunted off the main circuit. 
 
 Let the currents be denoted by C>>*, C^+M, (7 2 e*(W+W, O.eW+fc), 
 and (7 4 itbt+<M . The resistance by R", /, R and r. The capacity by C. 
 The self -inductance by L. A' and A" are reversing commutators and 
 F the terminals of the fixed coils and H the terminals of the hanging 
 coil of the electrodynamometer. 
 
334 
 
 HENEY A. EOWLAND 
 
 If now a periodic electromotive force is applied to the terminals A 
 and B the equations connecting the different currents are as below, 
 from which equations the quantity C^C Z cos (fa < 3 ) is to be found, 
 which is proportional to the deflection. From the figure 
 
 "+ -i-V 
 ibc / 
 
 FIG. 8. 
 
 In the same way it is found that 
 0* = i 
 
 FIG. 9. 
 
 Therefore the real part is 
 
 & cos (t, - 0.) = 01 
 
 ibc 
 
 / rr' 
 
 c 
 
 D, 
 
ELECTRICAL MEASUREMENTS 
 
 335 
 
 where D is the deflection. When D is equal to zero 
 
 \-r'} A = o 
 
 or 
 
 In the experiments by this method the microfarad Elliott condenser 
 was used, and it was compared with the different coils P 1} P z , A, and C. 
 The connections were made with open leads and open resistances were 
 used as far as possible, but it was necessary to use resistance boxes for 
 the last adjustments. The connections having been made as in figure, 
 the process of experimenting was to keep r and / constant and to 
 adjust R" and R until there was no deflection of the hanging coil. The 
 resistance of the circuits R" -\- r' and R -\- r were then measured on a 
 Wheatstone bridge. The commutator A' was reversed and the process 
 was repeated. The condenser had absorption (see p. 323) which caused 
 the resistance R" -f- r' to be increased by 7-11 ohms. When the capac- 
 ity is calculated, taking into account the absorption, it is called the 
 corrected capacity, as in the other tables of the paper. 
 
 COLLECTED RESULTS. 
 
 n=133. 
 
 Results found by taking sum 
 
 and diff . of separate 
 
 measurements. 
 
 5648 (C + Y l )C=P l 
 
 5730 (C + PI + P a ) (C + P a )=P, 
 
 7187 (C + P a ) C=P 2 
 
 7269 (C + P. + P,) (C + P,) = P, 
 
 3029 (C + P,) P, = C 
 
 2990 (C + P S ) P 4 =C 
 
 3065 (C + P, + P a ) P, P 2 =C 
 
 3022 (A + C) C=A 
 
 2917 (C + P, + P 2 ) C=P, + P a 
 
 2888 P, + P a 
 
 8677 C + P, 
 
 8718 (C + Pj + P.,) P a =C + P 1 
 
 0298 (C + P, + P a ) P,=C + P a 
 
 5920 P! + P a + C 
 
 6025 A + C=A + C 
 
 In method 12 corrections due to the hanging coil and fixed coils were 
 calculated so that the ratio of the resistances would give the ratio of the 
 self-inductances direct. In this method (6) since the capacity was in 
 circuit with the hanging coil, the self-inductance was so small that it 
 was neglected. The self-inductance of the coils P, etc., which were 
 joined in circuit with the fixed coils, were increased by the self-induc- 
 tance of the fixed coils, that is by -0164 henry. 
 
 Coils. 
 
 n=40. 
 Results found 
 by direct 
 measurement, 
 
 Results found Results found 
 by taking by direct 
 sum diff., etc., meas. of coils 
 of separate and combination 
 meas. of coils. 
 
 PI 
 
 11 
 
 5664 
 
 5663 
 5734 
 
 5653 
 
 
 P 2 
 
 7251 
 
 7211 
 
 7282 
 
 7233 
 
 9 1 
 
 C 
 
 1-3050 
 
 1-3049 
 
 1-3034 
 
 
 ii 
 
 
 1-3010 
 
 
 
 ii 
 
 
 1-3070 
 
 
 
 A 
 
 5-3080 
 
 5-3175 
 
 5-2991 
 
 5-: 
 
 P +P 
 
 
 1-2945 
 
 
 1- 
 
 ii 
 
 
 1-2915 
 
 
 1- 
 
 C + P, 
 ii 
 
 1-8713 
 
 1-8714 
 1-8744 
 
 1-8683 
 
 1- 
 1- 
 
 C + P a 
 
 + PI + PJ 
 
 2-0261 
 2-5995 
 
 2-0331 
 2-5965 
 
 2-0221 
 2-5951 
 
 2- 
 2- 
 
 A + C 
 
 6-6225 
 
 6-6130 
 
 6-6054 
 
 6- 
 
336 
 
 HENEY A. ROWLAND 
 
 The table below gives the various results. 
 
 N. Coil. 
 
 Queen in Position 
 current with of 
 R"+r. H"+r. R+r. Product. A'. L. 
 
 C. 
 
 40 P 
 
 (1 U 
 
 2008- 
 2005- 
 
 205- 
 200- 
 
 1095-7 2198522- 1 
 
 2 
 
 7251 
 0164 
 
 3373 
 
 7415 
 
 33 " 
 
 <i U 
 
 2024-5 
 2025-5 
 
 221- 
 222- 
 
 " 2218792- 1 
 " 2 
 
 7223 
 0164 
 
 3330 
 
 Cor. 
 C. 
 
 3323 
 
 40 A 12741-5 
 
 133 
 
 40 
 
 133 
 
 40 
 
 12720- 
 " 12716- 
 
 3430-8 
 3425-8 
 
 3448-8 
 3447-0 
 
 1578-5 
 1578-4 
 
 30- 
 30- 
 
 236- 
 220- 
 
 98- 
 93- 
 
 1241-85 15922394- 
 
 15775610- 
 
 1140-8 
 
 106 + s 1140-8 
 105 + s 
 
 57 +s 1088-9 
 
 58 + s '< 
 
 3911004- 
 
 3933354- 
 
 1718719-7 
 
 7397 
 
 5-3080 
 0164 
 
 5-3244 
 
 5-2991 
 0164 
 
 5-3155 
 
 1 3050 
 0164 
 
 1-3214 
 
 1-3034 
 0164 
 
 1-3198 
 
 5653 
 0164 
 
 5817 
 
 3344 
 
 3368 
 
 3379 
 
 3355 
 
 3384 
 
 3363 
 
 3346 
 
 This method can be used with great accuracy for the comparison of 
 the capacity of a condenser with a standard condenser. In the com- 
 parison, first one condenser and then the other would be placed in the 
 R -f- r circuit. If the two condensers are of nearly the same capacity, 
 the degree of accuracy of the comparison depends upon the accuracy 
 with which R" -f- r' can be set. The degree of accuracy of setting 
 R" -f- r' varies with the value of the self -inductance with which the 
 condensers are compared. In the experiments just given, using the 
 different coils, the degree of accuracy with which two ^ microfarad con- 
 densers could have been compared would vary from 1 part in 2000 to 
 one part in 14000. The two condensers are supposed to be without 
 absorption, as its presence would cause trouble unless the absorption 
 resistances were known. 
 
ELECTFJCAL MEASUREMENTS 337 
 
 Resume. Summing up the results deduced in this paper, it is seen 
 that the methods for the absolute determination of self-inductance 
 and capacity do not give as concordant results as could be wished. The 
 irregularity of results was caused, in the most part, both in the deter- 
 mination of self -inductance and capacity by the variation of the periods 
 of the currents used in the experiments. As the period enters directly 
 into the determination of self-inductance and capacity, all variations 
 of the period will appear in the results. The determination of capacity 
 is complicated by the presence of electric absorption (p. 323 et seq.). 
 The effect of electric absorption is shown to be that of an added resist- 
 ance in series with the condenser, called absorption resistance. A 
 direct method is given by which absorption resistance can be measured 
 (p. 319), and experiments are given which show that when condensers 
 possessing absorption are in series or in parallel, their absorption re- 
 sistances act under these conditions as ohmic resistances in series with 
 the separate condensers (p. 323). Absorption resistance is also found 
 to be extremely sensitive to temperature. 
 
 The methods for the comparison of two self-inductances or a self- 
 inductance and a capacity are independent of the period, and when the 
 self-inductances are of different magnitudes the comparison can be 
 made with an accuracy of 1 part in 10000. These methods, therefore, 
 give a means of comparison of a self-inductance with a standard self- 
 inductance, or a capacity with a standard capacity to an accuracy of 1 
 part in 10000, or they allow the establishment of standards. 
 
 22 
 
63 
 
 EESISTANCB TO ETHEEEAL MOTION 
 
 Br H. A. ROWLAND, N. E. GILBERT AND P. C. MCJUNCKIN 
 [Johns Hopkins University Circiilars, No. 146, p. 60, 1900] 
 
 An attempt has been made to determine within what limits it is 
 possible to say that there is no frictional or viscous resistance in the 
 ether of space. Modern theories of magnetism are based on some kind 
 of rotary or vortical motion in the ether and if a piece of iron is mag- 
 netized we imagine that the molecules, or something about them, rotate 
 also. The existence of permanent magnets shows that any retardation 
 due to any kind of resistance must be very slight. 
 
 In the case of an electro-magnet, any energy used in overcoming such 
 resistance, if it exists, must be derived from the exciting current and 
 the disappearance of such energy will produce an apparent resistance 
 added to that of the wire. An attempt was therefore made to deter- 
 mine whether a wire carrying a current had the same electrical resist- 
 ance when producing a magnetic field that it had when not producing it. 
 
 The experiment consisted in winding two coils of wire together on 
 an iron core and determining whether the resistance was the same in 
 two cases : 
 
 (1). When the current was so passed through the coils that both 
 produced a field in the same direction. 
 
 (2). When the current was so passed that the fields produced counter- 
 balanced each other. 
 
 The great difficulty in the experiment lay in the necessity of measur- 
 ing the resistance of a coil in which a comparatively large current was 
 flowing. In order to overcome the effect of changes in resistance due 
 to changes in temperature, two coils were wound, as nearly as possible 
 identical, and these double coils were used for the four arms of a 
 Wheatstone's bridge so that the temperature would rise in all four arms 
 equally. Each coil consisted of about 2500 turns of doubled No. 30 
 copper wire, the whole enclosed in an iron case, boiled in wax for five 
 hours and cooled in a vacuum. The insulation resistance was then 
 about eleven megohms. Iron cores were used and it was found that 
 the cases effectually protected the coils against sudden changes in tern- 
 
339 
 
 perature due to air currents as well as serving for yokes to the magnets. 
 A current of one-tenth ampere was used which insured a high state 
 of magnetization in the iron when two coils were in series, giving 5000 
 turns. 
 
 The coils were connected in the bridge in such a way that the two 
 coils in one case formed the opposite arms of the bridge. By means 
 of a reversing switch the current in one of these coils could be reversed. 
 This changed the field which might affect two opposite arms of the 
 bridge and thus doubled the deflection. Another switch might have 
 been inserted in the other pair of arms and thus doubled the deflection 
 again but errors due to the switches would also have been doubled and 
 no advantage gained. The switch was carefully constructed with large 
 copper rods dipping into copper mercury cups but, at best, the inac- 
 curacies of the switch limited the accuracy of the experiment. 
 
 The fine adjustments were made by resistance boxes shunted round 
 one of the coils. About 15,000 ohms in this shunt balanced the bridge. 
 A change of one ohm in the shunt gave a deflection of two millimeters 
 and indicated a change in the resistance of the arm of yinnnnr ohm. The 
 whole resistance being over 100 ohms this would give a determination 
 of one part in 2,000,000 or, since the deflection is doubled, one part in 
 4,000,000 for each arm. The result of 30 readings each way was that 
 the shunt resistance was about 3-4 ohms less with magnetic field than 
 without. The shunt was so placed that this gives a less resistance by 
 one part in 1,200,000 when producing a magnetic field. 
 
 The above result is in the wrong direction. The difficulty may lie in 
 the fact that the galvanometer, though used at night, was unsteady at 
 best, or it may be due to leakage. The resistance of the coils was 100 
 ohms while the insulation resistance was 11,000,000 ohms. If the leak- 
 age is symmetrical along the doubled wire it will not affect the galvano- 
 meter upon reversing the current in one coil. This assumption may 
 not be justified. 
 
PART III 
 
 HEAT 
 
16 
 
 ON THE MECHANICAL EQUIVALENT OF HEAT, WITH SUB- 
 SIDIAEY RESEAKCHES ON THE VARIATION OF THE 
 MERCURIAL FROM THE AIR THERMOMETER, AND ON 
 THE VARIATION OF THE SPECIFIC HEAT OF WATER l 
 
 [Proceedings of the American Academy of Arts and Sciences, XV, 75-200, 1880] 
 
 INVESTIGATIONS ON LIGHT AND HEAT, made and published wholly or in part with 
 appropriation from the RUMFOBD FUND 
 
 Presented June llth, 1879 
 
 CONTENTS 
 
 I. Introductory remarks .... 343 
 
 II. Thermometry 345 
 
 (a.) General view of Thermom- 
 etry 345 
 
 (&.) The Mercurial Thermometer 346 
 (c.) Relation of the Mercurial 
 
 and Air Thermometers 352 
 
 1. General and Historical 
 
 Remarks .... 352 
 
 2. Description of Appa- 
 
 ratus 358 
 
 3. Results of Comparison 366 
 (d.) Reduction to the Absolute 
 
 Scale 381 
 
 Appendix to Thermometry . 384 
 
 III. Calorimetry 387 
 
 (a.) Specific Heat of Water . 387 
 (6.) Heat Capacity of the Calo- 
 rimeter 399 
 
 IV. Determination of Equivalent . 404 
 
 V. 
 
 (a.) Historical Remarks . . . 404 
 
 1. General Review of 
 
 Methods 405 
 
 2. Results of Best Deter- 
 
 minations .... 409 
 (&.) Description of Apparatus 422 
 
 1. Preliminary Remarks . 422 
 
 2. General Description . 424 
 
 3. Details 426 
 
 (c) Theory of the Experiment 430 
 
 1. Estimation of Work 
 
 Done 430 
 
 2. Radiation 435 
 
 3. Corrections to Ther- 
 
 mometers, etc. . . 439 
 (d.) Results 441 
 
 1. Constant Data . . . 441 
 
 2. Experimental Data and 
 
 Tables of Results . 441 
 Concluding Remarks and Criti- 
 cism of Results and Methods 465 
 
 I. INTRODUCTOKY REMARKS 
 
 Among the more important constants of nature, the ratio of the 
 heat unit to the unit of mechanical work stands forth prominent, and 
 
 1 This research was originally to have been performed in connection with Professor 
 Pickering, but the plan was frustrated by the great distance between our residences. 
 An appropriation for this experiment was made by the American Academy of Arts 
 and Sciences at Boston, from the fund which was instituted by Count Rumford, and 
 liberal aid was also given by the Trustees of the Johns Hopkins University, who are 
 desirous, as far as they can, to promote original scientific investigations. 
 
344 HENEY A. KOWLAND 
 
 is used almost daily by the physicist. Yet, when we come to consider 
 the history of the subject carefully, we find that the only experimenter 
 who has made the determination with anything like the accuracy 
 demanded by modern science, and by a method capable of giving good 
 results, is Joule, whose determination of thirty years ago, confirmed 
 by some recent results, to-day stands almost, if not quite, alone among 
 accurate results on the subject. 
 
 But Joule experimented on water of one temperature only, and did 
 not reduce his results to the air thermometer; so that we are still left 
 in doubt, even to the extent of one per cent, as to the value of the 
 equivalent on the air thermometer. 
 
 The reduction of the mercurial to the air thermometer, and thence 
 to the absolute scale, has generally been neglected between and 100 
 by most physicists, though it is known that they differ several tenths 
 of a degree at the 45 point. In calorimetric researches this may pro- 
 duce an error of over one, and even approaching two per cent, especially 
 when a Geissler thermometer is used, which is the worst in this respect 
 of any that I have experimented on; and small intervals on the mer- 
 curial thermometers differ among themselves more than one per cent 
 from the difference of the glass used in them. 
 
 Again, as water is necessarily the liquid used in calorimeters, its 
 variation of specific heat with the temperature is a very important 
 factor in the determination of the equivalent. Strange as it may 
 appear, we may be said to know almost nothing about the variation 
 of the specific heat of water with the temperature between and 
 100 C. 
 
 Regnault experimented only above 100 C. The experiments of 
 Hirn, and of Jamin and Amaury, are absurd, from the amount of varia- 
 tion which they give. Pfaundler and Platter confined themselves to 
 points between and 13. Miinchausen seems to have made the best 
 experiments, but they must be rejected because he did not reduce to 
 the air thermometer. 
 
 In the present series of researches, I have sought, first, a method 
 of measuring temperatures on the perfect gas thermometer with an 
 accuracy scarcely hitherto attempted, and to this end have made an 
 extended study of the deviation of ordinary thermometers from the 
 air thermometer; and, secondly, I have sought a method of determin- 
 ing the mechanical equivalent of heat so accurate, and of so extended 
 a range, that the variation of the specific heat of water should follow 
 from the experiments alone. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 345 
 
 As to whether or not these have been accomplished, the following 
 pages will show. The curious result that the specific heat of water 
 on the air thermometer decreases from to about 30 or 35, after 
 which it increases, seems to be an entirely unique fact in nature, seeing 
 that there is apparently no other substance hitherto experimented upon 
 whose specific heat decreases on rise of temperature without change of 
 state. From a thermodynamic point of view, however, it is of the 
 same nature as the decrease of specific heat which takes place after 
 the vaporization of a liquid. 
 
 The close agreement of my result at 15 -7 C. with the old result of 
 Joule, after approximately reducing his to the air thermometer and 
 latitude of Baltimore, and correcting the specific heat of copper, is 
 very satisfactory to us both, as the difference is not greater than 1 in 
 400, and is probably less. 
 
 I hope at some future time to make a comparison with Joule's ther- 
 mometers, when the difference can be accurately stated. 
 
 II. THERMOMETKY 
 (a.) General View 
 
 The science of thermometry, as ordinarily studied, is based upon 
 the changes produced in bodies by heat. Among these we may mention 
 change in volume, pressure, state of aggregation, dissociation, amount 
 and color of light reflected, transmitted, or emitted, hardness, pyro-elec- 
 tric and thermo-electric properties, electric conductivity or specific in- 
 duction capacity, magnetic properties, thermo-dynamic properties, &c.; 
 and on each of these may be based a system of thermometry, each one 
 of which is perfect in itself, but which differs from all the others widely. 
 Indeed, each method may be applied to nearly all the bodies in nature, 
 and hundreds or thousands of thermometric scales may be produced, 
 which may be made to agree at two fixed points, such as the freezing 
 and boiling points of water, but which will in general differ at nearly, 
 if not all, other points. 
 
 But from the way in which the science has advanced, it has come 
 to pass that all methods of thermometry in general use to the present 
 time have been reduced to two or three, based respectively on the 
 apparent expansion of mercury in glass and on the absolute expansion of 
 some gas, and more lately on the second law of thermodynamics. 
 
 Each of these systems is perfectly correct in itself, and we have no 
 right to designate either of them as incorrect. We must decide a priori 
 
346 HEJOIY A. EOWLAND 
 
 on some system, and then express all our results in that system: the 
 accuracy of science demands that there should be no ambiguity on that 
 subject. In deciding among the three systems, we should be guided 
 by the following rules : 
 
 1st. The system should be perfectly definite, so that the same tem- 
 perature should be indicated, whatever the thermometer. 
 
 2d. The system should lead to the most simple laws in nature. 
 
 Sir William Thomson's absolute system of thermometry, coinciding 
 with that based on the expansion of a perfect gas, satisfies these most 
 nearly. The mercurial thermometer is not definite unless the kind of 
 glass is given, and even then it may vary according to the way the bulb 
 is blown. The gas thermometer, unless the kind of gas is given, is not 
 definite. And, further, if the temperature as given by either of these 
 thermometers was introduced into the equations of thermo-dynamics, 
 the simplest of them would immediately become complicated. 
 
 Throughout a small range of temperature, these systems agree more 
 or less completely, and it is the habit even with many eminent physi- 
 cists to regard them as coincident between the freezing and boiling 
 points of water. We shall see, however, that the difference between 
 them is of the highest importance in thermometry, especially where 
 differences of temperature are to be used. 
 
 For these reasons I have reduced all my measures to the absolute 
 system. 
 
 The relation between the absolute system and the system based on 
 the expansion of gases has been determined by Joule and Thomson 
 in their experiments on the flow of gases through porous plugs (Philo- 
 sophical Transactions for 1862, p. 579). Air was one of the most 
 important substances they experimented upon. 
 
 To measure temperature on the absolute scale, we have thus only to 
 determine the temperature on the air thermometer, and then reduce 
 to the absolute scale. But as the air thermometer is very inconvenient 
 to use, it is generally more convenient to use a mercurial thermometer 
 which has been compared with the air thermometer. Also, for small 
 changes of temperature the air thermometer is not sufficiently sensi- 
 tive, and a mercurial thermometer is necessary for interpolation. I shall 
 occupy myself first with a careful study of the mercurial thermometer. 
 
 (6.) The Mercurial Thermometer 
 
 Of the two kinds of mercurial thermometers, the weight thermometer 
 is of little importance to our subject. I shall therefore confine myself 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 347 
 
 principally to that form having a graduated stem. For convenience 
 in use and in calibration, the principal bulb should be elongated, and 
 another small bulb should be blown at the top. This latter is also of 
 the utmost importance to the accuracy of the instrument, and is placed 
 there by nearly all makers of standards. 2 It is used to place some of 
 the mercury in while calibrating, as well as when a high temperature 
 is to be measured; also, the mercury in the larger bulb can be made 
 free from air-bubbles by its means. 
 
 Most standard thermometers are graduated to degrees; but Regnault 
 preferred to have his thermometers graduated to parts of equal capacity 
 whose value was arbitrary, and others have used a single millimeter 
 division. As thermometers change with age, the last two methods are 
 the best; and of the two I prefer the latter where the highest accuracy 
 is desired, seeing that it leaves less to the maker and more to the 
 scientist. The cross-section of the tube changes continuously from 
 point to point, and therefore the distribution of marks on the tube 
 should be continuous, which would involve a change of the dividing 
 engine for each division. But as the maker divides his tube, he only 
 changes the length of his divisions every now and then, so as to average 
 his errors. This gives a sufficiently exact graduation for large ranges 
 of temperature; but for small, great errors may be introduced. Where 
 there is an arbitrary scale of millimeters, I believe it is possible to 
 calibrate the tube so that the errors shall be less than can be seen with 
 the naked eye, and that the table found shall represent very exactly 
 the gradual variation of the tube. 
 
 In the calibration of my thermometers with the millimetric scale, I 
 have used several methods, all of which are based upon some graphical 
 method. The first, which gives all the irregularities of the tube with 
 great exactness, is as follows: 
 
 A portion of the mercury having been put in the upper bulb, so as 
 to leave the tube free, a column about 15 mm. long is separated off. 
 This is moved from point to point of the tube, and its length carefully 
 measured on the dividing engine. It is not generally necessary to 
 move the column its own length every time, but it may be moved 
 20 mm. or 25 mm., a record of the position of its centre being kept. 
 To eliminate any errors of division or of the dividing engine, readings 
 were then taken on the scale, and the lengths reduced to their value 
 in scale divisions. The area of the tube at every point is inversely as 
 
 *Geissler and Casella omit it, which should condemn their thermometers. 
 
348 HENEY A. EOWLAND 
 
 the length of the column. We shall thus have a series of figures nearly 
 equal to each other, if the tube is good. By subtracting the smallest 
 from each of the others, and plotting the results as ordinates, with the 
 thermometer scale as abscissas, and drawing a curve through the points 
 so found, we have means of finding the area at any point. The curve 
 should not be drawn exactly through the points, but rather around 
 them, seeing they are the average areas for some distance each side of 
 the point. With good judgment, the curve can be drawn with great 
 accuracy. I then draw ordinates every 10 mm., and estimate the aver- 
 age area of the tube for that distance, which I set down in a table. 
 As the lengths are uniform, the volume of the tube to any point is 
 found by adding up the areas to that point. 
 
 But it would be unwise to trust such a method for very long tubes, 
 seeing the mercury column is so short, and the columns are not end to 
 end. Hence I use it only as supplementary to one where the column 
 is about 50 mm. long, and is always moved its own length. This estab- 
 lishes the volumes to a series of points about 50 mm. apart, and the 
 other table is only used to interpolate in this one. There seems to be 
 no practical object in using columns longer than this. 
 
 Having finally constructed the arbitrary table of volumes, I then 
 test it by reading with the eye the length of a long mercury column. 
 No certain error was thus found at any point of any of the thermom- 
 eters which I have used in these experiments. 
 
 While measuring the column, great care must be taken to preserve 
 all parts of the tube at a uniform temperature, and only the extreme 
 ends must be touched with the hands', which should be covered with 
 cloth. 
 
 If V is the volume on this arbitrary scale, the temperature on the 
 mercurial thermometer is found from the formula T = C V t , where 
 C and t are constants to be determined. If the thermometer contains 
 the and 100 points, we have simply 
 
 r _ 100 
 T~^T" * 
 
 '100 '0 
 
 Otherwise C is found by comparison with some other thermometer, 
 which must be of the same kind of glass. 
 
 It is to be carefully noted that the temperature on the mercurial 
 thermometer, as I have defined it, is proportional to the apparent ex- 
 pansion of mercury as measured on the stem. By defining it as pro- 
 portional to the true volume of mercury in the stem, we have to intro- 
 duce a correction to ordinary thermometers, as Poggendorff has shown. 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 349 
 
 As I only use the mercurial thermometer to compare with the air 
 thermometer, and as either definition is equally correct, I will not 
 further discuss the matter, but will use the first definition, as being 
 the simplest. 
 
 In the above formula I have implicitly assumed that the apparent 
 expansion is only a function of the temperature; but in solid bodies 
 like glass there seems to be a progressive change in the volume as time 
 advances, and especially after it has been heated. And hence in mer- 
 curial and alcohol thermometers, and probably in general in all ther- 
 mometers which depend more or less on the expansion of solid bodies, 
 we find that the reading of the thermometer depends, not only on its 
 present temperature, but also on that to which it has been subjected 
 within a short time; so that, on heating a thermometer up to a certain 
 temperature, it does not stand at the same point as if it had been cooled 
 from a higher temperature to the given temperature. As these effects 
 are without doubt due to the glass envelope, we might greatly diminish 
 them by using thermometers filled with liquids which expand more 
 than mercury : there are many of these which expand six or eight times 
 as much, and so the irregularity might be diminished in this ratio. But 
 in this case we should find that the correction for that part of the 
 stem which was outside the vessel whose temperature we were deter- 
 mining would be increased in the same proportion; and besides, as all 
 the liquids are quite volatile, or at least wet the glass, there would be 
 an irregularity introduced on that account. A thermometer with liquid 
 in the bulb and mercury in the stem would obviate these inconven- 
 iences ; but even in this case the stem would have to be calibrated before 
 the thermometer was made. By a comparison with the air-thermom- 
 eter, a proper formula could be obtained for finding the temperature. 
 
 But I hardly believe that any thermometer superior to the mercurial 
 can at present be made, that is, any thermometer within the same 
 compass as a mercurial thermometer, and I think that the best result 
 for small ranges of temperature can be obtained with it by studying 
 and avoiding all its sources of error. 
 
 To judge somewhat of the laws of the change of zero within the 
 limits of temperature which I wished to use, I took thermometer No. 
 6163, which had lain in its case during four months at an average 
 temperature of about 20 or 25 C., and observed the zero point, after 
 heating to various temperatures, with the following result. The time 
 of heating was only a few minutes, and the zero point was taken imme- 
 
350 
 
 HENRY A. KOWLAKD 
 
 diately after; some fifteen minutes, however, being necessary for the 
 thermometer to entirely cool. 
 
 TABLE I. SHOWING CHANGE OF ZERO POINT. - 
 
 Temperature 
 of Bulb 
 before finding 
 the Point. 
 
 Change of 
 Point. 
 
 Temperature 
 of Bulb 
 before finding 
 the Point. 
 
 Change of 
 Point. 
 
 22- 5 
 
 
 
 70-0 
 
 115 
 
 30-0 
 
 016 
 
 81-0 
 
 170 
 
 40-5 
 
 033 
 
 90-0 
 
 231 
 
 51-0 
 
 039 
 
 100-0 
 
 313 
 
 60-0 
 
 105 
 
 100-0 
 
 347 
 
 The second 100 reading was taken after boiling for some time. 
 
 It is seen that the zero point is always lower after heating, and that 
 in the limits of the table the lowering of the zero is about proportional 
 to the square of the increase of temperature above 25 C. This law 
 is not true much above 100, and above a certain temperature the 
 phenomenon is reversed, and the zero point is higher after heating; 
 but for the given range it seems quite exact. 
 
 It is not my purpose to make a complete study of this phenomenon 
 with a view to correcting the thermometer, although this has been 
 undertaken by others. But we see from the table that the error can- 
 not exceed certain limits. The range of temperature which I have 
 used in each experiment is from 20 to 30 C., and the temperature 
 rarely rose above 40 C. The change of zero in this range only amounts 
 to 0-03C. 
 
 The exact distribution of the error from this cause throughout the 
 scale has never been determined, and it affects my results so little that 
 I have not considered it worth investigating. It seems probable, how- 
 ever, that the error is distributed throughout the scale. If it were 
 uniformly distributed, the value of each division would be less than 
 before by the ratio of the lowering at zero to the temperature to which 
 the thermometer was heated. 
 
 The maximum errors produced in my thermometers by this cause 
 would thus amount to 1 in 1300 nearly for the 40 thermometer, and 
 to about 1 in 2000 for the others. Eather than allow for this, it is 
 better to allow time for the thermometer to resume its original state. 
 
 Only a few observations were made upon the rapidity with which 
 the zero returned to its original position. After heating to 81, the 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 351 
 
 zero returned from 0-170 to 0-148 in two hours and a half. 
 After heating to 100, the zero returned from 0-347 to 0-110 
 in nine days, and to 0-022 in one month. Eeasoning from this, I 
 should say that in one week thermometers which had not been heated 
 ahove 40 should be ready for use again, the error being then supposed 
 to be less than 1 in 4000, and this would be partially eliminated by 
 comparing with the air thermometer at the same intervals as the ther- 
 mometer is used, or at least heating to 40 one week before comparing 
 with the air thermometer. 
 
 As stated before, when a thermometer is heated to a very high 
 point, its zero point is raised instead of lowered, and it seems probable 
 that at some higher point the direction of change is reversed again; 
 for, after the instrument comes from the maker, the zero point con- 
 stantly rises until it may be 0-6 above the mark on the tube. This 
 gradual change is of no importance in my experiments, as I only use 
 differences of temperature, and also as it was almost inappreciable in 
 my thermometers. 
 
 Another source of error in thermometers is that due to the pressure 
 on the bulb. In determining the freezing point, large errors may be 
 made, amounting to several hundredths of a degree, by the pressure of 
 pieces of ice. In my experiments, the zero point was determined in 
 ice, and then the thermometer was immersed in the water of the com- 
 parator at a depth of about 60 cm. The pressure of this water affected 
 the thermometer to the extent of about 0-01, and a correction was 
 accordingly made. As differences of temperature were only needed, 
 no correction was made for variation in pressure of the air. 
 
 It does not seem to me well to use thermometers with too small a 
 stem, as I have no doubt that they are subject to much greater irregu- 
 larities than those with a coarse bore. For the capillary action always 
 exerts a pressure on the bulb. Hence, when the mercury rises, the 
 pressure is due to a rising meniscus which causes greater pressure than 
 the falling meniscus. Hence, an apparent friction of the mercurial 
 column. Also, the capillary constant of mercury seems to depend on 
 the electric potential of its surface, which may not be constant, and 
 would thus cause an irregularity. 
 
 My own thermometers did not show any apparent action of this kind, 
 but Pfaimdler and Platter mention such an action, though they give 
 another reason for it. 
 
352 HENRY A. EOWLAND 
 
 t * 
 (c.) Relation of the Mercurial and Air Thermometers ,J* 
 
 ' ' & 
 1. GENERAL AND HISTORICAL REMARKS 
 
 * .-* 
 Since the time of Dulong and Petit, many experiments Have been 
 
 made on the difference between the mercurial and the air thermometer, 
 but unfortunately most of them have been at high temperatures. As 
 weight thermometers have been used by some of the best experimenters, 
 I shall commence by proving that the weight thermometer and stem 
 thermometer give the same temperature; at the same time, however, 
 obtaining a convenient formula for the comparison of the air ther- 
 mometer with the mercurial. 
 
 For the expansion of mercury and of glass the following formulae 
 must hold : 
 
 For mercury, V V (I + at +~W + &c.} ; 
 " glass. V = V\ (1 + at + /3f + tic.} ; 
 
 In both the weight and stem thermometers we must have V = V. 
 
 '0 "i ! 7 ! /vTo ! ~p ' V -^ L*~V I X> ~P O6, ). 
 
 1 + at + pt + <XC. 
 
 where V and V are the volumes of the glass and of the mercury 
 reduced to zero, and t is the temperature on the air thermometer. 
 The temperature by the weight thermometer is 
 
 P -1 
 
 P7 
 
 where P , P , &c., are the weights of mercury in the bulb at C., 
 t C., &c. 
 
 Now these weights are directly as the volumes of the mercury at 0. 
 
 /. -p = 1 + At + Bt* + &c., 
 seeing that V is constant. 
 
 ... 7'=100 ra ^ +B/ ' + * <; - 
 
 + &c.' 
 
 In the stem thermometers we have V , the volume of mercury at 0, 
 constant, and the volume of the glass that the mercury fills, reduced 
 to 0, variable. As the volume of the glass T' is the volume reduced 
 to 0, it will be proportional to the volume of bulb plus the volume of 
 the tube as read off on the scale which should be on the tube. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 353 
 
 T = 100 -Af, ;t _ (V',) = 10 ( F 
 ^ + 5f + &c. 
 
 7*= 100 
 
 100 ^4 + (100)' B + &c. 
 which is the same as for the weight thermometer. 
 If the fixed points are and t' instead of and 100, we can write 
 
 &C ' 
 
 At' + Et" + Ct' s + &c. 
 
 T-f 
 
 T= t 1 + (t - t) 
 
 As T and are nearly equal, and as we shall determine the constants 
 experimentally, we may write 
 
 t = T - at (f - t) (b - t} + &c., 
 
 where t is the temperature on the air thermometer, and T that on the 
 mercurial thermometer, and a and & are constants to be determined for 
 each thermometer. 
 
 The formula might be expanded still further, but I think there are 
 few cases which it will not represent as it is. Considering & as equal 
 to 0, a formula is obtained which has been used by others, and from 
 which some very wrong conclusions have been drawn. In some kinds 
 of glass there are three points which coincide with the air thermometer, 
 and it requires at least an equation of the third degree to represent 
 this. 
 
 The three points in which the two thermometers coincide are given 
 by the roots of the equation 
 
 t(t' 
 and are, therefore, 
 
 In the following discussion of the historical results, I shall take 
 and 100 as the fixed points. Hence, i' = 100. To obtain a and &, 
 two observations are needed at some points at a distance from and 
 100. That we may get some idea of the values of the constants in 
 the formula for different kinds of glass, I will discuss some of the 
 experimental results of Eegnault and others with this in view. 
 23 
 
354 
 
 HENRY A. ROWLAND 
 
 Regnault's results are embodied, for the most part, in tables given on 
 p. 239 of the first volume of his Relation des Experiences. The figures 
 given there are obtained from curves drawn to represent the mean of 
 his experiments, and do not contain any theoretical results. The direct 
 application of my formula to his experiments could hardly be made with- 
 out immense labor in finding the most probable value of the constants. 
 
 But the following seem to satisfy the experiments quite well: 
 
 Cristal de Choisy-le-Roi b = 0, 
 
 Verre Ordinaire b = 245, 
 
 Verre Vert b = 270, 
 
 Verre de Suede b = +10 
 
 a = .000 000 32. 
 \ = .000 000 34. 
 a = .000 000 095 
 a .000 000 14. 
 
 From these values I have calculated the following: 
 
 TABLE II. REGNAULT'S RESULTS COMPARED WITH THE FORMULA. 
 
 
 Choisy-le-Roi. 
 
 Verre Ordinaire. 
 
 Verre Vert. 
 
 Verre de Suede. 
 
 ti 
 
 
 
 
 
 1 
 
 
 j 
 
 
 
 
 3 
 
 
 
 
 j 
 
 
 
 a 
 
 
 
 9 
 
 | 
 
 -2 
 
 
 
 d 
 
 * 
 
 g 
 
 SJ 
 
 1 
 
 c 
 
 a 
 o 
 
 S 
 
 
 H 
 
 E 
 
 3 
 
 2 
 
 C 
 
 "3 
 
 0) 
 
 C 
 
 3 
 
 2 
 
 
 3 
 
 
 
 
 
 2 
 o 
 
 i 
 
 fi 
 5 
 
 s 
 i 
 
 o 
 
 iH 
 
 5 
 
 i 
 
 
 
 p 
 I 
 
 o 
 
 S 
 
 | 
 
 O 
 
 1 
 
 S 
 
 100 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 120120-12 
 
 120-09 
 
 + 03 
 
 119-95119-90 
 
 + 05 
 
 120-07 
 
 120-09 
 
 01 
 
 120-04120-04 
 
 
 
 140140-29 
 
 140-25 
 
 + -04 
 
 139-85'139-80 
 
 + 05 
 
 140-21140-22 
 
 01 
 
 140-11140-10 
 
 + 01 
 
 160160-52 
 
 160 49 + 03! 159 74 159 72 
 
 + 02 
 
 160-40160-39 
 
 + 01 
 
 160-20160-21 
 
 01 
 
 180180-80 
 
 180-83 03 
 
 179-63179-68 
 
 05 
 
 180-60180-62 
 
 02 
 
 180-33180-34 
 
 01 
 
 200201-25201-28 
 
 03 
 
 199-70199-69 
 
 + 01 
 
 200-80,200-89 
 
 09 
 
 200-50200-53 
 
 03 
 
 220221-82221-86 
 
 04 
 
 219-80219-78 
 
 + 02 
 
 221-20221-23 
 
 03 
 
 320-75220-78 
 
 03 
 
 240242-55 ! 242-56 
 
 01 
 
 239-90239-96 
 
 06 
 
 241-60 
 
 241-63 
 
 03 
 
 241-16241-08 
 
 + 08 
 
 260263-44263-46 
 
 02 
 
 260-20260-21 
 
 01 
 
 262-15262-09 
 
 + -07 
 
 
 
 
 280284-48284-52 
 
 04 
 
 3280-58280-00 
 
 -02 
 
 282-85 
 
 282 63 
 
 + -22 
 
 
 
 
 300305-72305-76 
 
 04 
 
 301-08301-12 
 
 04 
 
 
 
 
 
 
 320 S97 95 327 20 
 
 05 
 
 321-80321 -80 
 
 00 
 
 
 
 
 
 
 
 340 
 
 349 30 
 
 348-88 
 
 + 42 
 
 434-00 
 
 342-64 
 
 + 36 
 
 
 
 
 
 
 
 
 
 
 
 
 
 The formula, as we see from the table, represents all Eegnault's 
 curves with great accuracy, and if we turn to his experimental results 
 we shall find that the deviation is far within the limits of the experi- 
 mental errors. The greatest deviation happens at 340, and may be 
 accounted for by an error in drawing the curve, as there are few experi- 
 mental results so high as this, and the formula seems to agree with 
 them almost as well as Regnault's own curve. 
 
 3 Corrected from 280-52 in Regnault's table. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 355 
 
 The object of comparing the formula with Regnault's results at 
 temperatures so much higher than I need, is simply to test the formula 
 through as great a range of temperatures, and for as many kinds of 
 glass, as possible. If it agrees reasonably well throughout a great 
 range, it will probably be very accurate for a small range, provided 
 we obtain the constants to represent that small range the best. 
 
 Having obtained a formula to represent any series of experiments, 
 we can hardly expect it to hold for points outside our series, or even 
 for interpolating between experiments too far apart, as, very often, a 
 small change in one of the constants may affect the part we have not 
 experimented on in a very marked manner. Thus in applying the 
 formula to points between and 100 the value of & will affect the 
 result very much. In the case of the glass Choisy-le-Eoi many values 
 of 6 will satisfy the observations besides 6 = 0. For the ordinary 
 glass, however, & is well determined, and the formula is of more value 
 between and 100. 
 
 The following table gives the results of the calculation. 
 
 TABLE III. REGNAULT'S RESULTS COMPARED WITH THE FORMULA. 
 
 Air 
 Thermom- 
 
 Calculated 
 a = -000 000 32 
 b = 0. 
 
 Calculated 
 o = -000 000 34 
 b = 245. 
 
 Observed. 
 
 J 
 
 Calculated 
 a = -000 000 44 
 
 J 
 
 
 Choisy-le-Koi. 
 
 Verre 
 Ordinaire. 
 
 Verre 
 Ordinaire. 
 
 
 Verre 
 Ordinaire. 
 
 
 
 10 
 
 
 
 10-00 
 
 
 10-07 
 
 
 
 
 
 
 10-10 
 
 
 
 20 
 
 19-99 
 
 20-12 
 
 
 
 20-17 
 
 
 30 
 
 29-98 
 
 30-15 
 
 30-12 
 
 + 03 
 
 30-21 
 
 + 09 
 
 40 
 
 39-97 
 
 40-17 
 
 40-23 
 
 06 
 
 40-23 
 
 
 
 50 
 
 49-96 
 
 50-17 
 
 50-23 
 
 06 
 
 50-23 
 
 
 
 60 
 
 59 95 
 
 60-15 
 
 60-24 
 
 09 
 
 60-21 
 
 03 
 
 70 
 
 69-95 
 
 70-12 
 
 70-22 
 
 10 
 
 70-18 
 
 04 
 
 80 
 90 
 
 79-96 
 89-97 
 
 80-09 
 90-05 
 
 80-10 
 
 01 
 
 80-11 
 90-07 
 
 + 01 
 
 100 
 
 100 
 
 100 
 
 100 
 
 
 
 100 
 
 
 
 Kegnault does not seem to have published any experiments on Choisy- 
 le-Roi glass between and 100, but in the table between pp. 226, 227, 
 there are some results for ordinary glass. The separate observations 
 do not seem to have been very good, but by combining the total number 
 of observations I have found the results given above. The numbers in 
 the fourth column are found by taking the mean of Eegnault's results 
 for points as near the given temperature as possible. The agreement 
 
t 
 
 356 HENRY A. EOWLAJSTD 
 
 is only fair, but we must remember that the same specimens of glass 
 were not used in this experiment as in the others, and that for these 
 specimens the agreement is also poor above 100. The values a = 
 .000,000,44 and & = 260 are much better for these specimens, and 
 the seventh column contains the values calculated from these values. 
 These values also satisfy the observations above 100 for the given 
 specimens. 
 
 The table seems to show that between and 100 a thermometer of 
 Choisy-le-Eoi almost exactly agrees with the air thermometer. But 
 this is not at all conclusive. Regnault, however, remarks, 4 that be- 
 tween and 100 thermometers of this glass agree more nearly with 
 the air thermometer than those of ordinary glass, though he states 
 the difference to amount to -1 to -2 of a degree, the mercurial ther- 
 mometer standing below the air thermometer. With the exception of 
 this remark of Eegnault's, no experiments have ever been published 
 in which the direction of the deviation was similar to this. All ex- 
 periments have found the mercurial thermometer to stand above the 
 air thermometer between and 100, and my own experiments agree 
 with this. However, no general rule for all kinds of glass can be 
 laid down. 
 
 Boscha has given an excellent study of Eegnault's results on this 
 subject, though I cannot agree with all his conclusions on this subject. 
 In discussing the difference between and 100 he uses a formula of 
 the form 
 
 T 1= t(lOQ t), 
 ct 
 
 and deduces from it the erroneous conclusion that the difference is 
 greatest at 50 C., instead of between 40 and 50. His results for 
 T t at 50 are 
 
 Choisy-le-Eoi .22 
 
 Verre Ordinaire +.25 
 
 Verre Vert +.14 
 
 Yerre de- Suede +.56 
 
 and these are probably somewhat nearly correct, except the negative 
 value for Choisy-le-Eoi. 
 
 With the exception of Eegnault, very few observers have taken up 
 this subject. Among these, however, we may mention Eecknagel, who 
 
 4 Comptes Rendus, Ixix. 
 
Osr THE MECHANICAL EQUIVALENT or HEAT 
 
 357 
 
 has made the determination for common glass between and 100. 
 I have found approximately the constants for my formula in this case, 
 and have calculated the values in the fourth column of the following 
 table. 
 
 TABLE IV. RECKNAGEL'S RESULTS COMPARED WITH THE FORMULA. 
 
 
 Mercurial Thermometer. 
 
 
 Air 
 Thermometer. 
 
 
 Difference. 
 
 
 
 
 Observed. 
 
 Calculated. 
 
 
 
 
 
 
 
 
 
 
 10 
 
 10-08 
 
 10-08 
 
 
 
 20 
 
 20-14 
 
 20-14 
 
 
 
 30 
 
 30-18 
 
 30-18 
 
 
 
 40 
 
 40-20 
 
 40-20 
 
 
 
 50 
 
 50-20 
 
 50-20 
 
 
 
 60 
 
 60-18 
 
 60-18 
 
 
 
 70 
 
 70-14 
 
 70-15 
 
 + 01 
 
 80 
 
 80-10 
 
 80-11 
 
 + 01 
 
 90 
 
 90-05 
 
 90-06 
 
 + 01 
 
 100 
 
 100-00 
 
 
 
 
 
 J=290, a = .000 000 33, 
 
 It will be seen that the values of the constants are not very different 
 from those which satisfy Eegnault's experiments. 
 
 There seems to be no doubt, from all the experiments we have now 
 discussed, that the point of maximum difference is not at 50, but at 
 some less temperature, as 40 to 45, and this agrees with my own 
 experiments, and a recent statement by Ellis in the Philosophical 
 Magazine. And I think the discussion has proved beyond doubt that 
 the formula is sufficiently accurate to express the difference of the 
 mercurial and air thermometers throughout at least a range of 200, 
 and hence is probably very accurate for the range of only 100 between 
 and 100. 
 
 Hence it is only necessary to find the constants for my thermometers. 
 But before doing this it will be well to see how exact the comparison 
 must be. As the thermometers are to be used in a calorimetric research 
 in which differences of temperature enter, the error of the mercurial 
 compared with the air thermometer will be 
 
 = a \U' 2 (J + 
 
358 HENRY A. ROWLAND 
 
 which for the constants used in Eecknagel's table becomes 
 
 Error = d -- I = .000 000 33 1 29000 780^ + 3f \. 
 clt 
 
 This amounts to nearly one per cent at 0, and thence decreases to 
 45, after which it increases again. As only 0-2 at the 40 point 
 produces this large error at 0, it follows that an error of only 0-02 
 at 40 will produce an error of y^nro at 0. At other points the errors 
 will be less. 
 
 Hence extreme care must be taken in the comparison and the most 
 accurate apparatus must be constructed for the purpose. 
 
 2. DESCRIPTION OF APPARATUS 
 The Air Thermometer 
 
 In designing the apparatus, I have had in view the production of 
 a uniform temperature combined with ease of reading the thermom- 
 eters, which must be totally immersed in the water. The uniformity, 
 however, needed only to apply to the air thermometer and to the bulbs 
 of the mercurial thermometer, as a slight variation in the temperature 
 of the stems is of no consequence. A uniform temperature for the air 
 thermometer is important, because it must take time for a mass of air 
 to heat up to a given temperature within 0-01 or less. 
 
 Fig. 1 gives a section of the apparatus. This consists of a large 
 copper vessel, nickel-plated on the outside, with double walls an inch 
 apart, and made in two parts, so that it could be put together water- 
 tight along the line a &. As seen from the dimensions, it required 
 about 28 kilogrammes of water to fill it. Inside of this was the vessel 
 mdefghkln, which could be separated along the line d Ic. In the 
 upper part of this vessel, a piston, q, worked, and could draw the water 
 from the vessel. The top was closed by a loose piece of metal, o p, 
 which fell down and acted as a valve. The bottom of this inner 
 vessel had a false bottom, c I, above which was a row of large holes ; 
 above these was a perforated diaphragm, s. The bulb of the air ther- 
 mometer was at /, with the bulbs of the mercurial thermometers almost 
 touching it. The air thermometer bulb was very much elongated, being 
 about 18 cm. long and 3 to 5 cm. in diameter. Although the bulbs of 
 the thermometers were in the inner vessel, the stems were in the 
 outer one, and the reading was accomplished through the thick glass 
 window u v. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 359 
 
 The change of the temperature was effected by means of a Bunsen 
 burner under the vessel w. 
 
 The working of the apparatus was as follows: The temperature 
 having been raised to the required point, the piston q was worked to 
 stir up the water; this it did by drawing the water through the holes 
 
 "31 
 
 FIG. 1. 
 
 FIG. 2. 
 
 at c I and the perforated diaphragm s, and thence up through the 
 apparatus to return on the outside. When the whole of the water is 
 at a nearly uniform temperature the stirring is stopped, the valve op 
 falls into place, and the connection of the water in the outer and inner 
 vessels is practically closed as far as currents are concerned, and be- 
 fore the water inside can cool a little the outer water must have cooled 
 considerably. 
 
360 HENKY A. EOWLAND 
 
 So effective was this arrangement that, although some of the ther- 
 mometers read to 0-007 C., yet they would remain perfectly stationary 
 for several minutes, even when at 40 C. At very high temperatures, 
 such as 80 or 90 C., the burner was kept under the vessel w all the 
 time, and supplied the loss of the outer vessel by radiation. The inner 
 vessel would under these circumstances remain at a very constant tem- 
 perature. The water in the outer vessel never differed by more than 
 a small fraction of a degree from that in the inner one. 
 
 To get the and 100 points the upper parts of the vessel above 
 the line a & were removed, and ice placed around the bulb of the air 
 thermometer, and left for several hours, until no further lowering took 
 place. For the 100 point the copper vessel shown in Fig. 3 was used. 
 The portion y of this vessel fitted directly over the bulb of the air 
 thermometer. On boiling water in x, the steam passed through the 
 tube to the air thermometer. It is with considerable difficulty that 
 the 100 point is accurately reached, and, unless care be taken, the 
 bulb will be at a slightly lower temperature. Not only must the bulb be 
 in the steam, but the walls of the cavity must also be at 100. To 
 accomplish this in this case, a large mass of cloth was heaped over the 
 instrument, and then the water in x vigorously boiled for an hour or so. 
 After fifteen minutes there was generally no perceptible increase of 
 temperature, though an hour was allowed so as to make certain. 
 
 The external appearance of the apparatus is seen in Fig. 2. The 
 method of measuring the pressure was in some respects similar to that 
 used in the air thermometer of Jolly, except that the reading was taken 
 by a cathetometer rather than by a scale on a mirror. The capillary 
 stem of the air thermometer leaves the water vessel at a, and passes 
 to the tube &, which is joined to the three-way cock c. The lower part 
 of the cock is joined by a rubber tube to another glass tube at d, which 
 can be raised and lowered to any extent, and has also a fine adjustment. 
 These tubes were about 1-5 cm. diameter on the inside, so that there 
 should be little or no error from capillarity. Both tubes were exactly 
 of the same size, and for a similar reason. 
 
 The three-way cock is used to fill the apparatus with dry air, and 
 also to determine the capacity of the tube above a given mark. In 
 filling the bulb, the air was pumped out about twenty times, and 
 allowed to enter through tubes containing chloride of calcium, sulphuric 
 acid, and caustic soda, so as to absorb the water and the carbonic acid. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 361 
 
 The Cathetometer 
 
 The cathetometer was one made by Meyerstein, and was selected 
 because of the form of slide used. The support was round, and the 
 telescope was attached to a sleeve which exactly fitted the support. 
 The greatest error of cathetometers arises from the upright support 
 not being exactly true, so that the telescope will not remain in level 
 at all heights. It is true that the level should be constantly adjusted, 
 but it is also true that an instrument can be made where such an ad- 
 justment is not necessary. And where time is an element in the 
 accuracy, such an instrument should be used. In the present case it 
 was absolutely necessary to read as quickly as possible, so as not to 
 
 FIG. 3. 
 
 leave time for the column to change. In the first place the round 
 column, when made, was turned in a lathe to nearly its final dimen- 
 sions. The line joining the centres of the sections must then have 
 been. very accurately straight. In the subsequent fitting some slight 
 irregularities must have been introduced, but they could not have been 
 great with good workmanship. 5 The upright column was fixed, and 
 the telescope moved around it by a sleeve on the other sleeve. Where 
 the objects to be measured are not situated at a very wide angle from 
 each other, this is a good arrangement, and has the advantage that any 
 side of the column can be turned toward the object, and so, even if it 
 
 4 The change of level along the portion generally used did not amount to more 
 than -1 of a division, or about -Olmm. at the mercury column, as this is about the 
 smallest quantity which could be observed on the level. 
 
362 HENRY A. ROWLAND 
 
 were crooked, we could yet turn it into such a position as to nearly 
 eliminate error. 
 
 It was used at a distance of about 110 cm. from the object, and no 
 difficulty was found after practice in setting it on the column to j\ mm. 
 at least. The cross hairs made an angle of 45 with the horizontal, as 
 this was found to be the most sensitive arrangement. 
 
 The scale was carefully calibrated, and the relative errors c for the 
 portion used were determined for every centimeter, the portion of the 
 scale between the and 100 points of the air thermometer being 
 assumed correct. There is no object in determining the absolute value 
 of the scale, but it should agree reasonably well with that on the 
 barometer; for let H , H t , and H 1QO be the readings of the barometer, 
 and Ti , h t , and /t 100 the readings of the cathetometer at the temperatures 
 denoted by the subscript. Then approximately 
 
 (.#100 + /? 100 ) (fft> + ^o) ^100 HQ + h lw A 
 
 As the height of the barometer varies only very slightly during an 
 experiment, the value of this expression is very nearly 
 
 "100 "0 
 
 which does not depend on the absolute value of the scale divisions. 
 
 But the best manner of testing a cathetometer is to take readings 
 upon an accurate scale placed near the mercury columns to be meas- 
 ured. I tried this with my instrument, and found that it agreed with 
 the scale to within two or three one-hundredths of a millimeter, which 
 was as near as I could read on such an object. 
 
 In conclusion, every care was taken to eliminate the errors of this 
 instrument, as the possibility of such errors was constantly present in 
 my mind; and it is supposed that the instrumental errors did not 
 amount to more than one or two one-hundredths of a millimeter on the 
 mercury column. The proof of this will be shown in the results 
 obtained. 
 
 The Barometer 
 
 This was of the form designed by Fortin, and was made by James 
 Green of New York. The tube was 2-0 cm. diameter nearly on the 
 outside, and about 1-7 cm. on the inside. The correction for capillarity 
 is therefore almost inappreciable, especially as, when it remains con- 
 
 6 These amounted to less than -016mm. at any part. 
 
Ox THE MECHAXICAL EQUIVALENT OF HEAT 3f>3 
 
 stant, it is exactly eliminated from the equation. The depression for 
 this diameter is about -08 mm., but depends upon the height of the 
 meniscus. The height of the meniscus was generally about 1-3 mm.; 
 but according as it was a rising or falling meniscus, it varied from 
 1-4 to 1-2 mm. These are the practical values of the variation, and 
 would have been greater if the barometer had not been attached to the 
 wall a little loosely, so as to have a slight motion when handled. Also 
 in use the instrument was slightly tapped before reading. The varia- 
 tion of the height of the meniscus from 1-2 to 1-4 mm. would affect 
 the reading only to the extent of -01 to -02 mm. 
 
 The only case where any correction for capillarity is needed is in 
 finding the temperatures of the steam at the 100 point, and will then 
 affect that temperature only to the extent of about 0-005. 
 
 The scale of the instrument was very nearly standard at C., and 
 was on brass. 
 
 At the centre of the brass tube which surrounded the barometer, a 
 thermometer was fixed, the bulb being surrounded by brass, and there- 
 fore indicating the temperature of the brass tube. 
 
 In order that it should also indicate the temperature of the barome- 
 ter, the whole tube and thermometer were wrapped in cloth until a 
 thickness of about 5 or 6 cm. was laid over the tube, a portion being 
 displaced to read the thermometers. This wrapping of the barometer 
 was very important, and only poor results were obtained before its 
 use; and this is seen from the fact that 1 on the thermometer indi- 
 cates a correction of -12 mm. on the barometer, and hence makes a 
 difference of 0-04 on the air thermometer. 
 
 As this is one of the most important sources of error, I have now 
 devised means of almost entirely eliminating it, and making continual 
 reading of the barometer unnecessary. This I intend doing by an 
 artificial atmosphere, consisting of a large vessel of air in ice, and 
 attached to the open tube of the manometer of the air thermometer. 
 
 The Thermometers 
 
 The standard thermometers used in my experiments are given in 
 the following table on the next page. 
 
 The calibration of the first four thermometers has been described. 
 The calibration of the Kew standard was almost perfect, and no cor- 
 rection was thought necessary. The scale divided on the tube was to 
 half-degrees Fahrenheit; but as the 32 and 212 points were not cor- 
 rect, it was in practice used as a thermometer with arbitrary divisions. 
 
364 
 
 HEXKY A. EOWLAND 
 
 
 
 
 
 
 
 
 
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 Chemical Laboratory, 
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 11 11 
 
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ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 365 
 
 The interval between the and 100 points, as Welsh found it, was 
 180 -12, usinff barometer at 30 inches, or 180 -05 as corrected to 
 760 mm. of mercury. 8 At the present time it is 179 -68,* showing a 
 change of 1 part in 486 in twenty-five years. This fact shows that 
 the ordinary method of correcting for change of zero is not correct, and 
 that the coefficient of expansion of glass changes with time. 10 
 
 I have not been able to find any reference to the kind of glass used 
 in this thermometer. But in a report by Mr. Welsh we find a com- 
 
 TABLE VI. COMPARISON BY WELSH, 1852. 
 
 Mean of 
 Kew Standards 
 Nos. 4 and 14. 
 
 Fastr6 231, 
 Regnault. 
 
 J 
 Kew. 
 
 Troughton and 
 Simms 
 (Royal Society). 
 
 A 
 
 Kew. 
 
 3200 
 
 3200 
 
 3200 
 
 38-71 
 
 38-72 +-01 
 
 38-70 
 
 01 
 
 45-04 
 
 45-03 
 
 01 
 
 45-03 
 
 01 
 
 49-96 
 
 49-96 
 
 00 
 
 49-96 
 
 00 
 
 55-34 
 
 55-37 
 
 + 03 
 
 55-34 
 
 00 
 
 60-07 
 
 60-05 
 
 02 
 
 60-06 
 
 01 
 
 65-39 
 
 65-41 
 
 + 02 
 
 65-36 
 
 03 
 
 69-93 
 
 69-95 
 
 + 02 
 
 69-93 
 
 00 
 
 74-69 
 
 74-69 | -00 
 
 74-72 
 
 + 03 
 
 80-05 
 
 80-06 
 
 + 01 
 
 80-14 
 
 + 09 
 
 85-30 
 
 85-33 
 
 + 03 
 
 85-44 
 
 + 14 
 
 90-50 
 
 90-51 
 
 + 01 
 
 90-56 
 
 + 06 
 
 95-26 
 
 95-24 
 
 02 
 
 95-40 
 
 + 14 
 
 101-77 
 
 101-77 
 
 00 
 
 101-94 
 
 + 15 
 
 109-16 
 
 109-15 -01 
 
 109-25 
 
 + 08 
 
 212-00 
 
 212-00 
 
 00 
 
 212-00 
 
 00 
 
 parison, made on March 19, 1852, of some of his thermometers with 
 two other thermometers, one by Fastre, examined and approved by 
 Eegnault, and the other by Troughton and Simms. The thermometer 
 which I used was made a little more than a year after this; and it is 
 
 8 Boiling point, "Welsh, Aug. 17, 1853, 212 -17; barometer 30 in. 
 Freezing point, " " " 32 -05. 
 
 Boiling point, Rowland, June 22, 1878, 212 -46; barometer 760 mm. 
 Freezing point, " " 32-78. 
 
 The freezing point was taken before the boiling point in either case. 
 9 179 -70, as determined again in January, 1879. 
 
 10 The increase shown here is 1 in 80 nearly ! It is evidently connected with the 
 change of zero ; for when glass has been heated to 100, the mean coefficient of ex- 
 pansion between and 100 often changes as much as 1 in 50. Hence it is not 
 strange that it should change 1 in 80 in twenty-five years. I believe this fact has 
 been noticed in the case of standards of length. 
 
366 HENRY A. ROWLAND 
 
 reasonable to suppose that the glass was from the same source as the 
 standards Nos. 4 and 14 there used. We also know that Regnault was 
 consulted as to the methods, and that the apparatus for calibration 
 was obtained under his direction. 
 
 I reproduce the table on preceding page with some alterations, the 
 principal one of which is the correction of the Troughton and Simms 
 thermometers, so as to read correctly at 32 and 212, the calibration 
 being assumed correct, but the divisions arbitrary. 
 
 It is seen that the Kew standards and the Fastre agree perfectly, but 
 that the Troughton and Simms standard stands above the Kew ther- 
 mometers at 100 F. 
 
 The Geissler standard was made by Geissler of Bonn, and its scale 
 was on a piece of milk glass, enclosed in a tube with the stem. The 
 calibration was fair, the greatest error being about 0-015 C., at 50 C.; 
 but no correction for calibration was made, as the instrument was only 
 used as a check for the other thermometers. 
 
 3. EESULTS OF COMPARISON 
 Calculation of Air Thermometw 
 
 This has already been described, and it only remains to discuss the 
 formula and constants, and the accuracy with which the different, 
 quantities must be known. 
 
 The well-known formula for the air thermometer is 
 
 ff-ft+4 
 
 m _J 
 
 * V 
 
 i 
 
 - fl 
 
 V\ 'l + a? "1 + 0* J 
 
 Solving with reference 1 to T, and placing in a more convenient form, 
 we have 
 
 H-h' + *H-., 
 
 T= - - _ nearlv, 
 
 a A' _L_ __*_ 
 v 
 
 where ' 
 
 and r = a = -00364. 
 
 For the first bulb, v 
 
 For the second bulb, v_ 
 
 V 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 367 
 
 To discuss the error of T due to errors in the constants, we must 
 replace by its experimental value, seeing that it was determined 
 with the same apparatus as that by which T was found. As it does 
 not change very much, we may write approximately 
 
 ^=100 
 
 H h 
 
 
 I /H loo H\_b m H lw -bH\ 
 
 ~m- r t\ 
 
 From this formula we can obtain by differentiation the error in 
 each of the quantities, which would make an error of one-tenth of 
 one per cent in T. The values are for T = 40 nearly; = 20; 
 H wo h = 270 mm. ; and h = 750 mm. If x is the variable, 
 
 , dx *rp dx T _ 04 dx 
 
 ~~dT ~oTT 1000 ~ ~dT ' 
 
 TABLE VII. ERRORS PRODUCING AN ERROR IN T OF 1 IN 1000 AT 40 C. 
 
 
 
 
 
 foinn 
 
 ft 
 
 bioo 
 
 bioo-b 
 
 
 H. 
 
 f/ioo or h. 
 
 JL 
 
 a 
 
 a 
 
 a 
 
 a 
 
 
 
 
 ' 
 
 7> 
 
 Jhnn i . OinnrO _ 4 , A 
 
 bioo 
 
 
 
 
 
 a 
 
 a sani. 
 
 a 
 
 
 Absolute 
 
 
 
 
 
 
 
 
 value, 
 
 llmm. 
 
 27 mm. 
 
 005 
 
 00074 
 
 00087 
 
 0047 
 
 00087 
 
 Ax 
 
 
 
 
 
 
 
 
 Relative 
 
 
 
 
 
 
 
 
 value, 
 
 
 
 0-9 
 
 10 
 
 12 
 
 62 
 
 
 Ax 
 
 
 
 
 
 
 
 
 X 
 
 
 
 
 
 
 
 
 From this table it would seem that there should be no difficulty in 
 determining the 40 point on the air thermometer to at least 1 in 2000; 
 and experience has justified this result. The principal difficulty is in 
 the determination of H, seeing that this includes errors in reading the 
 barometer as well as the cathetometer. For this reason, as mentioned 
 before, I have designed another instrument for future use, in which 
 the barometer is nearly dispensed with by use of an artificial atmos- 
 phere of constant pressure. 
 
 The value of -^.does not seem to affect the result to any great extent; 
 
 and if it was omitted altogether, the error would be only about 1 in 
 1000, assuming that the temperature t was the same at the determina- 
 tion of the zero point, the 40 point, and the 100 point. It seldom 
 varied much. 
 
 The coefficient of expansion of the glass influences the result very 
 slightly, especially if we know the difference of the mean coefficients 
 
368 
 
 HENRY A. ROWLAND 
 
 between and 100, and say 10 and -f 10. This difference I at 
 first determined from Regnault's tables, but afterwards made a deter- 
 mination of it, and have applied the correction. 11 
 
 The table given by Regnault is for one specimen of glass only; and 
 I sought to better it by taking the expansion at 100 from the mean 
 of the five specimens given by Regnault on p. 231 of the first volume 
 of his Relation des Experiences, and reducing the numbers on page 237 
 in the same proportion. I thus found the values given in the second 
 column of the following table. 
 
 TABLE VIII. COEFFICIENT OF EXPANSION OF THE GLASS OF THE AIR THER- 
 MOMETER, ACCORDING TO THE AIR THERMOMETER. 
 
 Tempera- 
 ture ac- 
 cording to 
 Air Ther- 
 mometer. 
 
 Values of b 
 used for a first 
 Calculation. 
 
 b from 
 Regnault's 
 Table, 
 Glass No. 5. 
 
 Experimental Results. 
 
 Apparent 
 Coefficient of 
 Expansion of 
 Mercury. 
 
 5, using 
 Regnault's 
 Value for 
 Mercury. 12 
 
 ft, using 
 Recknagel's 
 Value for 
 Mercury. 13 
 
 b, using 
 Wttllner's 
 Value for 
 Mercury. 14 
 
 
 20 
 40 
 60 
 80 
 100 
 
 0000252 
 0000253 
 0000256 
 0000259 
 0000262 
 0000264 
 
 0000263 
 0000264 
 0000267 
 0000270 
 0000273 
 0000276 
 
 
 
 
 
 00015410 
 00015395 
 00015391 
 
 0000254 
 0000258 
 0000261 
 
 .0000264 
 0000266 
 0000267 
 
 0000273 
 0000276 
 0000278 
 
 00015381 
 
 0000277 
 
 .0000277 
 
 0000287 
 
 The second column contains the values which I have used, and one 
 of the last three columns contains my experimental results, the last 
 being probably the best. The errors by the use of the second column 
 compared with the last are as follows: 
 
 TT i inr from using & 100 6 40 = -0000008 instead of -0000011; 
 TD 3 r j r from using & 100 = -0000264 instead of -0000287; 
 
 or, ^Vrr for both together. 
 
 As the error is so small, I have not thought it worth while to entirely 
 recalculate the tables, but have calculated a table of corrections (see 
 opposite page), and have so corrected them. 
 
 11 This was determined by means of a large weight thermometer in which the mer- 
 cury had been carefully boiled. The glass was from the same tube as that of the air 
 thermometer, and they were cut from it within a few inches of each other. 
 
 12 Relations des Experiences, i, 328. 
 13 Fogg. Ann., cxiii, 135. 
 "Experimental Physik, Wiillner, i, 67. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 369 
 
 T= T {1 + 373 (b( w - M - (273+ T}(V - b)\, 
 T= T' {I .000858 + (273+7 v )(& b')\ t 
 
 T= -99975 T approximately between and 40. The last is true 
 within less than -j-gVir f a degree. 
 
 The two bulbs of the air thermometer used were from the same piece 
 of glass tubing, and consequently had nearly, if not quite, the same 
 coefficient of expansion. 
 
 In the reduction of the barometer and other mercurial columns to 
 zero, the coefficient -000162 was used, seeing that all the scales were 
 of brass. 
 
 In the tables the readings of the thermometers are reduced to 
 volumes of the tube from the tables of calibration, and they are cor- 
 rected for the pressure of water, which increased their reading, except 
 at 0, by about 0-01C. 
 
 TABLE IX. TABLE OF CORRECTIONS. 
 
 T 
 
 T 
 
 Correction. 
 
 Calculated 
 Temperature. 
 
 Corrected 
 Temperature. 
 
 
 
 
 
 
 
 
 
 
 
 10 
 
 9-9971 
 
 0029 
 
 20 
 
 19-9946 
 
 0054 
 
 30 
 
 29-9924 
 
 0076 
 
 40 
 
 39-9907 
 
 0093 
 
 50 
 
 49-9894 
 
 0106 
 
 60 
 
 59-9865 
 
 0135 
 
 80 
 
 79-9880 
 
 0120 
 
 100 
 
 100- 
 
 
 
 The order of the readings was as follows in each observation: 1st, 
 barometer; 2d, cathetometer; 3d, thermometers forward and backward; 
 4th, cathetometer; 5th, barometer, &c., repeating the same once or 
 twice at each temperature. In the later observations, two series like 
 the above were taken, and the water stirred between them. 
 
 The following results were obtained at various times for the value of 
 a with the first bulb : 
 
 0036664 
 
 0036670 
 
 0036658 
 
 0036664 
 
 0036676 
 
 Mean a = -00366664 
 
 24 
 
370 
 
 HEXRY A. KOWLAXD 
 
 obtained by using the coefficient- of expansion of glass -0000264: at 
 100, or a -0036698, using the coefficient -0000287. 
 
 The thermometers Nos. 6163, 6165, 6166, were always taken out of 
 the bath when the temperature of 40 was reached, except on Novem- 
 ber 14, when they remained in throughout the whole experiment. 
 
 The thermometer readings are reduced to volumes by the tables of 
 calibration. 
 
 TABLE X. IST SERIES, Nov. 14, 1877. 
 
 Relative 
 Weight. 
 
 Air 
 Thermometer. 
 
 V 
 6163. 
 
 V 
 6166. 
 
 V 
 
 6167. 
 
 Temperature 
 by 6167. 
 
 J 
 
 4 
 
 
 
 115-33 
 
 21-25 
 
 6-147 
 
 
 
 
 
 4 
 
 17 -1425 
 
 422-84 
 
 255-80 
 
 15-685 
 
 17-661 
 
 236 
 
 4 
 
 23 -793 
 
 534-71 
 
 341 05 
 
 19-157 
 
 24 -089 
 
 296 
 
 5 
 
 30 -582 
 
 653-49 
 
 431-71 
 
 22-833 
 
 30 896 
 
 314 
 
 2 
 
 38 -569 
 
 793 1 8 
 
 
 47-175 
 
 3 8 -93 5 
 
 366 
 
 2 
 
 51 -040 
 
 
 
 33-864 
 
 51 -320 
 
 280 
 
 4 
 
 59 -137 
 
 
 
 38-256 
 
 59 -452 
 
 315 
 
 
 
 
 
 
 
 
 The first four series, Tables X to XIII, were made with one bulb 
 to the air thermometer. A new bulb was now made, whose capacity 
 
 was 192-0 c. cm., that of the old being 201-98 c. cm. The value of L. 
 
 for the new bulb was -0058. 
 follows : 
 
 June 8th 
 June 22d 
 June 25th 
 
 ]\Iean 
 
 The values of li' and a were obtained as 
 
 00366790 
 00366977 
 00366779 
 
 0036685 
 
 ft' 
 
 753-876 
 753-805 
 753-837 
 
 753-84 
 
 This value of is calculated with the old coefficient for glass. The 
 new would have given -0036717. 
 
 It now remains to determine from these experiments the most prob- 
 able values of the constants in the formula, comparing the air with 
 the mercurial thermometer. The formula is, as we have found, 
 
 but I have generally used it in the following form: 
 
 t=CV-f mt (100 /) (1 n (100 -f #)) , 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 
 
 371 
 
 N 
 
 CO 
 
 oo 
 
 CO 
 
 CO 
 
 o; 
 
 t- CO 
 
 CD 71 
 
 CD 
 OS 
 
 OS CO 
 I- OS 
 
 CO 
 
 CO rH 
 1C *3* 
 
 3 
 
 
 CO 
 CO 
 
 fij 
 
 
 
 o 
 
 CD 
 
 o 
 l> 
 
 O O 
 
 00 rH 
 
 
 
 O 
 
 
 
 00 rH 
 
 
 
 CO 
 
 O O 
 CO -rfl 
 t- 00 
 
 o 
 >* 
 
 oo 
 
 
 o 
 
 OS 
 OS 
 
 
 OS 
 OO 
 
 1C 
 OS 
 CO 
 
 CO 
 
 OS 1C 
 oo os 
 
 CO 71 
 
 1 
 
 rH CO 
 
 00 05 
 
 OS 
 CO 
 
 O CO 
 CD t- 
 
 1C * 
 
 OS 
 
 o 
 
 CO 
 00 
 
 S : 
 
 CO 
 
 6 -3 
 E 
 
 o 
 t- 
 
 
 
 CO 
 rH 
 
 o 
 I- 
 
 CM 
 
 
 
 OO rH 
 
 o 
 
 o 
 
 
 
 00 rH 
 Tf< 1C 
 
 o 
 
 CO 
 
 
 
 CO T>< 
 
 I- 00 
 
 o 
 
 00 
 
 o 
 
 OS 
 OS 
 
 o 
 
 OS 
 OS 
 
 _o 
 
 CM 
 
 1C r-i 
 
 00 
 t- 
 
 
 
 rH CO 
 O 1C 
 
 CO 
 71 
 
 rH I- 
 
 O rH 
 
 t- 
 
 rH CO 
 
 O TjH 
 
 CO 
 
 
 CO CO 
 77 OS 
 
 I 
 
 '3 
 
 O 
 
 O OO 
 
 CO 
 
 00 
 
 OS rH 
 
 CM * 
 
 rH 
 
 OS CM 
 
 T* 1C 
 
 CO 
 
 CO "*1< 
 t- 00 
 
 00 
 
 
 s 
 
 ^g 
 
 OO 7* 
 7* OO 
 rH SM 
 
 CO 
 00 
 OS 
 
 to 
 
 77 
 
 -J} ~ 
 
 71 CO 
 
 OS 
 1C 
 
 CO 30 
 ^H O 
 1C 71 
 
 CO 
 
 o 
 
 o t- 
 
 CO CO 
 00 t- 
 
 t- 
 
 CO 
 
 o 
 
 
 
 rH 
 
 to 
 
 CO 
 
 rH 
 
 rH 
 
 iH 
 
 rH OO 
 71 CM 
 
 00 
 
 71 * 
 
 CO CO 
 
 
 
 1C rH 
 <fl 1C 
 
 rH 
 1C 
 
 
 CO 
 
 
 CO 
 
 ^g 
 
 8 2 
 
 rH CO 
 
 CO 
 
 00 
 
 CO 
 
 71 
 
 71 
 
 
 
 
 
 
 
 
 
 0* 77 
 
 CO 
 77 
 7? 
 
 OS 
 
 CO 
 
 o 
 
 00 
 
 O 
 -f 
 
 o 
 
 00 
 
 
 
 
 
 
 
 
 * 3D 
 
 
 
 71 
 
 1C * 
 
 00 
 
 
 
 
 
 
 
 
 -H 7> 
 
 
 2 
 
 -,r -r 
 
 -f 
 
 
 . 
 
 . 
 
 
 
 
 |j 
 
 OO 
 
 CO 
 CM 
 
 t- 
 
 OS o 
 
 X 
 CO 
 
 Tt< CO 
 rH 
 
 CD l> 
 
 CO 
 
 o 
 
 O ^JH 
 * CO 
 
 CO 
 
 CO 
 
 CO O 
 
 Tjl O 
 
 CO - 
 
 11 
 
 o' 
 
 o 
 
 CO 
 
 rH 
 
 o 
 CM 
 
 o o 
 
 00 rH 
 
 o 
 
 o 
 
 o o 
 
 OO rH 
 
 * 1C 
 
 o 
 
 CO 
 
 o o 
 CO ^ 
 l> 00 
 
 o 
 
 00 
 
 o 
 
 OS 
 OS 
 
 
 OS O H 
 
 OS O - 
 
 ^ 
 
 ! 
 
 CO 
 
 -* 
 
 00 
 CO 
 
 OS t~ 
 
 CO OS 
 
 i 
 
 rH <M 
 
 o 
 
 iC 
 
 rH 1C 
 
 t- OS 
 
 iC 
 OS 
 
 rH 
 CO 
 
 0> 
 
 o <* 
 
 CO t- 
 
 n 
 
 w 
 
 1C 
 
 .c 
 
 1C 1C 
 
 1C 
 
 CO CD 
 
 CO 
 
 CO CO 
 
 to 
 
 t- 
 
 ^ : ii 
 
 o 
 
 OS 
 
 o 
 
 77 
 
 1C 
 CO 
 
 o ^* 
 
 CO 1C 
 
 CO 
 1C 
 
 30 O 
 
 CO t- 
 
 t- 
 
 00 
 
 3D 77 
 
 OS rH 
 
 77 
 
 rH 
 
 (M 
 
 CO 
 
 *; 
 
 CO 
 
 ki 
 
 < 
 
 
 
 * * 
 
 
 
 
 
 .C 
 
 1C 
 
 1C 
 
 *_ 
 
 OS 
 
 CO 
 00 
 
 OS 
 
 OS t- 
 
 t- t- 
 
 t- 
 
 71 CO 
 
 O CO 
 
 OS 
 
 CO OS 
 
 OS 
 OS 
 
 CO 
 CO 
 
 CO 
 rH 
 
 
 
 CO 
 
 rH 
 
 OS 
 
 CO 
 
 o 
 
 71 CD 
 t- 
 
 IC 
 
 o 
 
 t- iC 
 77 CO 
 
 00 
 
 CO 
 rH 
 
 CO 77 
 OS 77 
 rH 77 
 
 1 
 
 CO 
 77 
 
 CO 
 CO 
 
 
 CO 
 
 o 
 
 1C 
 
 OS 
 
 CO * 
 
 OS 
 CO 
 
 OS CO 
 CO O 
 
 rH 
 CO 
 
 rH O 
 CO CO 
 
 CD 
 CO 
 
 O 
 
 o 
 
 CO 
 00 
 
 ti 
 
 CO 
 CO 
 
 t- 
 
 OS 
 00 
 
 o 
 
 71 
 
 CO 
 
 71 CO 
 71 iC 
 
 00 30 
 
 1C 
 1C 
 00 
 
 CO 1C 
 t- 00 
 
 00 00 
 
 00 
 
 rH 
 OS 
 
 CO 77 
 
 *f t* 
 
 OS OS 
 
 t- 
 
 OS 
 
 o 
 
 77 
 
 -H 
 
 s 
 
 III 
 
 00 -* 
 77 CO 
 
 f- 
 
 t- 
 
 1C t- 
 
 71 rH 
 
 1C 
 
 o 
 
 00 00 
 O l- 
 
 OO 
 CO 
 
 t- CM 
 
 ID fl 
 
 OS 
 1C 
 
 o 
 
 rH 
 
 rH 
 
 iff 
 
 j> co 
 
 7 i 
 
 CO 
 
 rH 
 
 00 
 
 o * 
 
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 CO 
 00 
 
 O rn 
 rH rH 
 
 CO 
 
 rfi 
 
 rH rH 
 
 t- O 
 
 rH . 71 
 
 H 
 
 O 
 77 
 
 CO 
 
 1 i 
 
 |i? 
 
 o 
 o 
 
 2 
 
 CO 
 
 77 SM 
 
 CO 
 
 ^ 1C 
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 CO 
 OS 
 
 CO 71 
 
 r- 
 
 o 
 
 O 
 
 OS 
 
 t- I 
 
 life 
 
 i- 
 
 7* 
 
 I- 
 
 I- 
 
 ?i ^ 
 
 77 
 
 ! 
 
 gl 
 
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 - 1 
 
 O 
 
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 5 B-J5 
 
 
 
 
 
 
 
 
 
 
 
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 it 
 
 77 CO 
 
 
 
 71 
 
 71 rH 
 
 CO 
 
 77 77 
 
 - 
 
 CO CO 
 
 CO 
 
 O 
 
 o 
 
372 
 
 HENKY A. EOWLAND 
 
 
 8^ 
 
 s CD 
 
 
 
 00 
 
 CM 
 
 00 
 
 
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 10 
 
 00 
 
 
 90 
 
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 IO 
 
 
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 o 
 
 
 
 
 
 
 
 
 o 
 
 o 
 
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 BcB 
 
 
 
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 00 
 
 CO 
 
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 00 
 
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 rH 
 
 
 CM 
 
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 8 
 
 o 
 
 
 rH 
 
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 CO 
 
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 IS 
 
 
 
 
 
 
 
 
 
 
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 o 
 
 
 rH 
 
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 00 
 
 
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 rH 
 
 rH 
 
 CM 
 
 
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 CO 
 
 
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 l- 
 
 CO 
 
 o 
 
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 CO 
 
 ^ 
 
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 rWjB 
 
 rH 
 
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 CO 
 
 l- 
 
 t- 
 
 rH 
 
 
 
 
 
 
 
 rH 
 
 c\-> 
 
 w 
 
 * 
 
 
 
 
 ; 
 
 g 
 
 
 
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 OS 
 
 rH 
 
 IO 
 
 t- 
 
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 30 
 
 
 CO 
 CO 
 
 
 HI 
 
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 OS 
 
 CO 
 
 CO 
 
 CO 
 
 * 
 
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 S 
 
 rH 
 
 O rH 
 
 OS 
 
 ^ 
 
 t- 
 
 CM 
 
 OS 
 
 CO 
 
 
 
 
 
 
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 CO 
 
 t- 
 
 t 
 
 CO 
 
 
 
 
 
 
 
 
 
 
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 ^ 
 
 00 
 
 J-^ 
 
 f^ 
 
 co 
 
 00 
 
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 O 
 
 rH 00 
 
 10 
 
 CM 
 
 CO 
 
 o 
 
 IO 
 
 o 
 
 o 
 t- 
 
 oo 
 
 CXI 
 
 
 
 ^t 
 
 SI 
 
 oa 
 
 
 O 
 
 IO IO 
 
 
 
 o 
 
 o 
 00 
 
 rH 
 
 o 
 CO 
 CM 
 
 o 
 
 OS 
 
 o 
 
 00 
 
 CO 
 
 o 
 00 
 CO 
 
 ^ 
 
 p 
 
 
 
 
 
 
 
 
 
 
 fc 
 
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 OS 1-H 
 
 rH 
 
 OS 
 
 IO 
 
 CM 
 
 CO 
 
 CXI 
 
 -4 
 
 rQ 1 CS 
 
 
 rH CXI 
 
 CO 
 
 
 CD 
 
 l- 
 
 OS 
 
 OS 
 
 i-s 
 
 
 
 
 
 
 
 
 
 
 
 N^ 
 
 
 IO IO 
 
 IO 
 
 IO 
 
 IO 
 
 IO 
 
 IO 
 
 IO 
 
 oT 
 
 
 
 
 
 
 
 
 
 
 w 
 
 w 
 
 
 
 
 
 
 
 
 
 
 
 
 H 
 
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 CO 
 
 * + 
 
 o5 
 
 OS O 
 
 OS O 
 
 o 
 
 00 
 rH 
 
 OS 
 
 o 
 
 CO 
 
 CO 
 
 ca 
 
 P 
 
 ^ 
 
 
 
 
 
 
 
 
 
 
 
 
 CO 
 
 CO ->TI 
 
 i 
 
 TtH 
 
 * 
 
 * 
 
 "* 
 
 * 
 
 3 
 
 !> 
 
 
 
 
 
 
 
 
 
 H 
 
 
 
 
 
 
 
 
 
 
 1 
 
 I-H 
 
 ^ 
 
 
 rH T 
 
 
 
 t- 
 
 OS 
 
 II 
 
 OS 
 
 HH 
 
 
 
 
 OS OS 
 
 CO 
 
 ^ 
 
 00 
 
 
 
 CO 
 
 
 M 
 
 ft 
 
 
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 i 
 
 CO 
 
 CD 
 
 -* 
 
 o 
 
 OS 
 
 W 
 
 
 
 rH 
 
 ext 
 
 
 CD 
 
 * 
 
 o 
 
 rH 
 
 OS 
 
 i-5 
 
 
 OS 
 
 
 
 
 
 
 
 
 pa 
 < 
 
 
 IO 
 
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 CO 
 
 oo 
 
 rH 
 OS 
 
 CD 
 CO 
 
 8 
 
 o 
 
 -H 
 
 00 
 
 OS 
 
 H 
 
 3 
 
 CO 
 
 O CXt 
 
 rfl 
 
 CO 
 
 t> 
 
 10 
 
 rH 
 
 OS 
 
 
 
 Ttl 
 
 CO CO 
 
 t- 
 
 OS 
 
 rH 
 
 
 IO 
 
 
 
 
 t- 
 
 t- t- 
 
 t- 
 
 t- 
 
 00 
 
 00 
 
 00 
 
 00 
 
 
 o 
 
 
 
 
 
 
 
 
 
 
 a> g-*^ 
 
 3 
 
 OS CO 
 
 CD 
 
 O5 
 
 t- 
 
 OS 
 
 2> 
 
 o 
 
 
 S!D 
 
 CO 
 
 
 OS 
 
 o 
 
 Tt< 
 
 rH 
 
 CM 
 
 
 
 S o 
 
 J^. 
 
 CXI O 
 
 ^ 
 
 -t! 
 
 UH 
 
 CM 
 
 CO 
 
 t- 
 
 
 |3f 
 
 rH 
 1 
 
 1 1 
 
 rH 
 
 CO 
 
 IO 
 
 CD 
 
 CO 
 
 CO 
 
 
 *H O 
 II 
 
 OJTJ 
 
 CO 
 rH 
 
 OS CO 
 
 o o 
 
 00 
 
 00 
 
 OS 
 CO 
 
 O5 
 00 
 
 CO 
 00 
 
 CO 
 
 
 a 9 
 
 4* 
 
 CO CO 
 
 CM 
 
 CM 
 
 ct 
 
 n 
 
 CM 
 
 CM 
 
 
 25 
 
 CO 
 
 CO CD 
 
 CD 
 
 CO 
 
 CD 
 
 CO 
 
 CO 
 
 CO 
 
 
 11 
 
 
 
 
 
 
 
 
 
 
 g* 
 
 
 
 
 
 
 
 
 
 
 _> jg 
 
 
 
 
 
 
 
 
 
 
 5 '3 
 
 
 
 
 
 
 
 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 373 
 
 1 , 
 
 ; ; 
 
 
 TH 
 
 o 
 
 OS 
 
 CO 
 
 to 
 
 oo 
 
 CNJ 
 
 H 
 
 OS 
 
 o 
 
 00 
 
 00 
 
 
 a SB o 
 
 
 
 o 
 
 00 
 
 
 
 TH 
 
 o 
 
 CO 
 
 TH 
 
 o 
 IO 
 
 
 
 o 
 
 CO 
 
 
 
 OS 
 04 
 
 o 
 
 00 
 CO 
 
 o 
 
 OS 
 OS 
 
 
 j> 
 
 : ; 
 
 
 to 
 
 10 
 
 iH 
 CO 
 
 TH 
 TH 
 
 t- 
 
 IS 
 
 IO 
 CO 
 
 TH 
 
 CO 
 
 >H 
 
 oo 
 
 
 + 
 O 
 
 
 
 
 00 
 
 CO 
 
 TH 
 
 OS 
 
 TH 
 
 IO 
 
 o 
 
 CO 
 
 o 
 
 CO 
 
 OS 
 CO 
 
 Os 
 OS 
 
 a 
 o 
 
 o 
 
 IO 
 
 O CO 
 CO t- 
 
 00 
 
 00 
 CO 
 
 o 
 
 OS 
 
 CO 
 
 1 1 
 
 t- 
 
 OS 
 
 TH 
 
 OS 
 
 F 
 
 to 
 
 04 
 
 
 3* 
 i 
 
 fc-1 
 
 CO TH 
 
 to 04 
 
 I- CO 
 
 TH -H 
 
 1 
 
 10 
 
 t- 
 
 co 
 
 CO 
 
 Os 
 
 CO 
 
 1O 
 
 10 
 
 o 
 
 -# 
 to 
 
 to 
 
 CO 
 
 to 
 
 TH 
 
 OS 
 
 z> 
 
 
 
 o 
 
 "3 
 
 O 
 
 t^5 * 
 
 tO TH 
 
 CO 50 
 I- IO 
 
 to 
 
 5 
 
 CO 
 
 Os 
 
 l- 
 
 
 
 TH 
 
 00 
 
 OS 
 04 
 
 iH 
 00 
 CO 
 
 
 
 
 
 2 
 
 CO ^ 
 
 CO ^ 
 TH rH 
 
 e 
 
 CO 
 O4 
 
 co 
 
 CO 
 
 to 
 
 o 
 to 
 
 TH 
 
 l- 
 
 ? 
 
 
 
 ja 
 
 TH 
 
 04 
 
 04 CO 
 I- OS 
 
 04 
 
 Os 
 O4 
 
 t- 
 
 o 
 
 O4 
 
 to 
 
 00 
 
 co 
 
 TH 
 
 to 
 
 
 
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 "a 1 
 
 ^ TH 
 
 g o* 
 
 t- iH 
 
 O4 
 
 t- 
 
 TH 
 
 o 
 
 Os 
 
 TH 
 
 00 
 
 to 
 
 O4 
 
 to 
 
 10 
 CO 
 
 TH 
 
 04 
 
 00 
 TH 
 
 : 
 
 
 s ^ 
 a 
 
 "*" ? 
 
 in" oo 
 
 4i Q> 
 
 OS IO 
 00 0* 
 
 * oo 
 
 TH 
 
 04 
 IO 
 
 O4 
 
 OS 
 
 CO 
 
 to 
 
 IO 
 
 
 o 
 to 
 
 
 
 IO 
 
 oo 
 
 o 
 
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 IO 
 
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 ft . 
 
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 qj 03 
 
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 o 
 
 t- 
 
 
 
 t- 
 
 
 O4 
 
 TH 
 
 
 00 
 
 TH 
 
 o 
 
 IO 
 
 
 
 OS 
 
 
 
 OS 
 
 o 
 
 CO 
 CO 
 
 
 
 OS O 
 
 OS | 
 
 y> <x> 
 
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 o3 si 
 
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 rQ 
 
 to 04 
 
 IO tO 
 
 TH TH 
 
 OS 
 CO 
 04 
 
 to 
 
 t- 
 
 1O 
 
 CO 
 
 Os 
 
 l> 
 
 OS 
 
 o 
 to 
 
 CO 
 CO 
 
 I- 
 
 10 
 
 CO 
 
 t- 
 
 OS 
 d 
 
 OS 
 
 TH 
 
 CO 
 
 o5 5 
 
 o 
 
 hi - 
 
 
 IO IO 
 
 10 
 
 IO 
 
 IO 
 
 IO 
 
 10 
 
 IO 
 
 10 
 
 10 
 
 t- 
 
 o o 
 
 <H 
 33 TJ 
 > <O 
 
 K " t~ 
 
 33 .(- o 
 
 OS 04 
 
 CO T* 
 
 
 
 OS 
 
 o 
 
 OS 
 
 o 
 
 OS 
 
 to 
 
 TH 
 
 TH 
 
 to 
 
 CO 
 CO 
 
 o 
 
 OS 
 CO 
 
 to 
 
 00 
 CO 
 
 OS 
 TH 
 
 t- t- 
 
 Os O 
 CO O 
 
 .2 
 
 H 3 
 
 ~ ** 
 
 05 ^2 
 
 t> o 
 
 ^ * 
 
 TX ^ 
 
 * 
 
 * 
 
 * 
 
 <* 
 
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 TH 
 
 <* 
 
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 to -4* 
 
 1 
 
 o 2 
 
 oj oj 
 
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 10 
 
 fe 
 
 t- 00 
 
 ^1 CO 
 
 CO 
 
 10 
 
 
 
 t- 
 
 TH 
 
 o 
 l- 
 
 00 
 CO 
 
 t- 
 
 10 
 
 i 
 
 CO 
 
 o 
 
 to OS 
 OS 04 
 
 t- o 
 
 a to 
 
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 1 
 
 o to 
 
 to 
 
 IH 
 
 t- 
 
 o 
 
 CO 
 
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 CO 
 
 to 
 
 t- 
 
 CO 
 
 t> 
 
 o 
 o 
 
 TH 
 
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 6 S 
 
 CO 
 
 o 
 
 IO ;O 
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 CO 
 
 OS 
 
 04 
 
 o 
 
 oo 
 
 10 
 
 00 
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 CO 
 
 to 
 
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 CO 
 
 co 
 
 CO 
 CO 
 
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 00 
 
 TH 
 
 CO 
 
 SS 5 
 
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 II II 
 
 ^. Q 
 
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 t- t- 
 
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 t- 
 
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 t- 
 
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 00 
 
 CO 
 
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 04 
 
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 CO 
 
 10 to 
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 TH 
 
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 TH O 
 TH 
 
 to to 
 
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 CO 
 10 
 
 co 
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 00 
 
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 CO 
 
 00 
 
 TH 
 
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 t" 
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 t- 
 
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 04 
 
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 IO 
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 00 
 
 l- 
 
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 t- t- 
 
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 t- 
 
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 t- 
 
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 t- 
 
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 t- 
 
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 t- z> 
 
 
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 co 
 
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 HENRY A. ROWLAND 
 
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 CM 
 
 to 
 
 O! 
 
 iM 
 
 CM 
 
 CO 
 
 1C 
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 O5 
 
 to 
 
 
 1 : :+ + + + + + + + : 
 
 fe" 
 
 o 
 
 i 
 
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 c 
 
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 CO 
 
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 rH 
 
 o 
 
 
 o 
 
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 o 
 
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 o 
 
 
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 o 
 
 o 
 
 CM 
 
 o 
 
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 cS 
 
 
 
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 S 
 
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 rH 
 
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 CM 
 
 
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 35 
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 CM 
 
 rH 
 
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 rH 
 
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 35 
 
 
 
 
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 35 
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 5 
 
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 35 
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 c 
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 35 
 
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 w 
 
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 35 
 
 30 
 
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 t- 
 
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 o* 
 
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 rH 
 
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 r- 
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 l- 
 
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 t- 
 
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 2 
 
 00 
 
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Ox THE MECHANICAL EQUIVALENT OF HEAT 
 
 375 
 
 J- 
 
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 65 SS 
 
 
 
 
 
 
 
 
 
 
 
 "Si tt 
 
 * 
 
 
 
 
 
 
 
 
 
 
 
376 HENET A. EOWLAND 
 
 And the following relations hold among the constants : 
 
 C = G' (1 + m (60 8400 )) , nearly , 
 a = mn, 
 
 b = ~ 100, 
 n 
 
 T=CVt 9 , 
 i t 
 
 *t l o n' ' 
 
 In these formulae t is the temperature on the air thermometer; V is 
 the volume of the stem of the mercurial thermometer, as determined 
 from the calibration and measured from any arbitrary point; and C", 
 f , m, and n are constants to be determined. 
 
 The best way of finding these is by the method of least squares. 
 C" must be found very exactly; t is only to be eliminated from the 
 equations; m must be found within say ten per cent, and n need only 
 be determined roughly. To find them only within these limits is a 
 very difficult matter. 
 
 Determination of n 
 
 As this constant needs a wide range of temperatures to produce much 
 effect, it can only be determined from thermometer No. 6167, which 
 was of the same glass as 6163, 6165, and 6166. It is unfortunate that 
 it was broken on November 21, and so we only have the experiments 
 of the first and second series. From these I have found w = -003 
 nearly. This makes b = 233, which is not very far from the values 
 found before from experiments above 100 by Eegnault on ordinary 
 glass." 
 
 Determination of C and m 
 
 I shall first discuss the determination of these for thermometers 
 Nos. 6163, 6165, and 6166, as these were the principal ones used. 
 
 As No. 6163 extended from to 40, and the others only from 
 to 30, it was thought best to determine the constants for this one 
 first, and then find those for 6165 and 6166 by comparison. As this 
 comparison is deduced from the same experiments as those from which 
 we determine the constants of 6163, very nearly the same result is 
 
 15 Some experiments with Baudin thermometers at high temperatures have given 
 me about 240, a remarkable agreement, as the point must be uncertain to 10 or 
 more. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 377 
 
 found as if we obtained the constants directly by comparison with the 
 air thermometer. 
 
 The constants of 6163 can be found either by comparison with 6167, 
 or by direct comparison with the air thermometer. I shall first deter- 
 mine the constants for No. 6167. 
 
 The constants C and t for this thermometer were found directly 
 by observation of the and 100 points; and we might assume these, 
 and so seek only for m. In other words, we might seek only to ex- 
 press the difference of the thermometers from the air thermometer 
 by a formula. But this is evidently incorrect, seeing that we thus 
 give an infinite weight to the observations at the and 100 points. 
 The true way is obviously to form an equation for each temperature, 
 giving each its proper weight. Thus from the first series we find for 
 No. 6167, 
 
 Weight. Equations of Condition. 
 
 4 = 6-147 C t , 
 
 4 17 -427 = 15-685 C 1 930m, 
 
 4 23-793 = 19-157 C t 1140m, 
 &c. &c. &c. 
 
 5 100 =60-156 C t , 
 
 which can be solved by the method of least squares. As t is unim- 
 portant, we simply eliminate it from the equations. I have thus 
 found, 
 
 Weight. 
 
 1 Nov. 14 (7 = 1-85171 m= -000217 
 
 2 Nov. 20, 21 (7 = 1-85127 m= -000172 
 
 Mean = 1-85142 m= -000187 
 
 The difference in the values of m is due to the observations not being 
 so good as were afterwards obtained. However, the difference only 
 signifies about 0-03 difference from the mean at the 50 point. After 
 November 20 the errors are seldom half of this, on account of the 
 greater experience gained in observation. 
 
 The ratio of C for 6167 and 6163 is found in the same way. 
 
 Weight. 
 
 1 Nov. 14 -0310091 
 
 2 Nov. 20 -0309846 
 
 Mean -0309928 
 
378 HENRY A. BOWLAND 
 
 Hence for 6163 we have in this way 
 
 C = -057381 C" = -056995 m = -000187. 
 
 By direct comparison of No. 6163 with the air thermometer., we find 
 the following: 
 
 m. 
 
 000239 
 000166 
 000226 
 000155 
 000071 
 .000115 
 
 Date. 
 
 Weight. 
 
 C'. 
 
 Nov. 14 
 
 1 
 
 056920 
 
 Nov. 20 
 
 2 
 
 056985 
 
 Jan. 25 
 
 3 
 
 056986 
 
 Feb. 11 
 
 4 
 
 056997 
 
 June 8 
 
 3 
 
 056961 
 
 June 22 
 
 2 
 
 056959 
 
 Mean -056976 -000004 -000154 -000010 
 
 The values of C" agree with each other with great exactness, and 
 the probable error is only 0-003 C. at the 40 point. 
 
 The great differences in the values of m, when we estimate exactly 
 what they mean in degrees, also show great exactness in the experi- 
 ments. The mean value of m indicates a difference of only 0-05 
 between the mercurial and air thermometer at the 20 point, the 
 and 40 points coinciding. The probable error of m in degrees is only 
 0.003C. 
 
 There is one more method of finding m from these experiments; and 
 that is by comparing the values of C' with No. 6167, the glass of 6167 
 being supposed to be the same as that of 6163. 
 
 We have the formula 
 
 C = C"(l + 34-8??i). 
 
 Hence 
 
 CC' 
 
 m = 
 
 3i-SC' 
 
 We thus obtain the following results: 
 
 Date. 
 
 Weight. 
 
 Value of m 
 
 Nov. 14 
 
 1 
 
 000236 
 
 Nov. 20 
 
 2 
 
 000218 
 
 Jan. 25 
 
 3 
 
 000217 
 
 Feb. 11 
 
 4 
 
 000197 
 
 June 8 
 
 3 
 
 000215 
 
 June 22 
 
 2 
 
 000216 
 
 Mean -000213 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 379 
 
 The results for m are then as follows : 
 
 From direct comparison of Xo. 6167 with the air thermometer -000187 
 From direct comparison of Xo. G163 with the air thermometer -000154 
 From comparison of Xo. 6163 with Xo. 6167 -000213 
 
 The first and last are undoubtedly the most exact numerically, but 
 they apply to Xo. 6167, and are also, especially the first, derived from 
 somewhat higher temperatures than the 20 point, where the correc- 
 tion is the most important. The value of m, as determined in either 
 of these ways, depends upon the determination of a difference of tem- 
 perature amounting to 0-30, and hence should be quite exact. 
 
 The value of m, as obtained from the direct comparison of Xo. 6163 
 with the air thermometer, depends upon the determination of a differ- 
 ence of about 0-05 between the mercurial and the air thermometer. 
 At the same time, the comparison is direct, the temperatures are the 
 same as we wish to use, and the glass is the same. I have combined 
 the results as follows: 
 
 m from Xo. 6167 -000200 
 
 m from Xo. 6163 -000154 
 
 Mean 00018 1 
 
 It now remains to deduce from the tables the ratios of the constants 
 for the different thermometers. 
 
 The proper method of forming the equations of condition are as 
 follows, applying the method to the first series : 
 
 Weight. 
 
 4 21-25 C llt = 115-33 C l i\ 
 
 4 255-80 C llt = 422-84 C, r, 
 
 4 34 1 -05 C llt = 534-71 C t r. 
 
 5 431-71 C llt = 653-49 C t i\ 
 
 where (?, is the constant for Xo. 6166, C, is that for Xo. 6163, and 
 r is a constant to be eliminated. Dividing by C lt the equations can 
 
 be solved for jw. The following table gives the results : 
 "t 
 
 16 See Appendix to Thermometry, where it is finally thought best to reject the 
 value from No. 6167 altogether. 
 
380 
 
 HENEY A. EOWLAND 
 
 TABLE XVI. RATIOS OF CONSTANTS. 
 
 Date. 
 
 Weight. 
 
 6163 
 
 6167 
 
 6166 
 
 6167 
 
 6166 
 6163 
 
 6165 
 6163 
 
 6165 
 6166 
 
 Nov. 14 
 Nov. 20 
 Jan. 25 
 Feb. 11 
 June 8 
 June 22 
 
 1 
 2 
 3 
 4 
 3 
 2 
 
 031009 
 030985 
 
 040658 
 040670 
 
 1-3111 
 1-3128 
 1-3122 
 1-3115 
 1-3108 
 1-3122 
 
 
 
 
 
 
 
 8-0588 
 8-0605 
 8-0588 
 
 6-1449 
 6-1469 
 6-1428 
 
 
 
 
 
 
 
 Mean 
 
 .030993 
 .00005 
 
 .040666 
 000003 
 
 1.31175 
 -0004 
 
 8 . 0594 
 .0002 
 
 6.1451 
 .0004 
 
 From these we have the following, as the final most probable results : 
 
 C n = 8-0601 C lt 
 <7,,, = 1-31175 0,, 
 
 C, = -031003 <7 iv , 
 = -24991 <7 iv , 
 0,,,= -040661 IT , 
 
 of which the last three are only used to calculate the temperatures on 
 the mercurial thermometer, and hence are of little importance in the 
 remainder of this paper. 
 
 The value of C' which we have found for the old value of the coeffi- 
 cient of expansion of glass was 
 
 C' = -056976; 
 
 and hence, corrected to the new coefficient, it is, as I have shown, 
 
 C, =.056962. 
 Hence, G n = '45912 , 
 
 <7 y// = -074720. 
 
 And we have finally the three following equations to reduce the ther- 
 mometers to temperatures on the air thermometer: 
 
 Thermometer No. 5163: 
 T = -056962 V 1' -00018 T (40 T) (1 -003 (T -f 40)). 
 
 Thermometer "No. 6165: 
 T= -45912 V" V -00018 T (T 40) (1 -003 (T + 40)). 
 
 Thermometer No. 6166: 
 T= -074720 V'" V" ' 00018 T (T 40) (1 -003 (T+40)); 
 
 where V, V" ', and V" are the volumes of the tube obtained by cali- 
 bration; t ', t ", and t " f are constants depending on the zero point, and 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 381 
 
 of little importance where a difference of temperature is to be meas- 
 ured; and T is the temperature on the air thermometer. 
 
 On the mercurial thermometer, using the and 100 points as fixed, 
 we have the following by comparison with No. 6167: 
 
 Thermometer No. 6163; = -057400 V t ; 
 Thermometer No. 6165; = -46265 V 1 ; 
 Thermometer No. 6166; = -075281 V 1 . 
 
 The Kew Standard 
 
 The Kew standard must be treated separately from the above, as the 
 glass is not the same. This thermometer has been treated as if its 
 scale was arbitrary. 
 
 In order to have variety, I have merely plotted all the results with 
 this thermometer, including those given in the Appendix, and drawn 
 a curve through them. Owing to the thermometer being only divided 
 to -J F., the readings could not be taken with great accuracy, and so 
 the results are not very accordant; but I have done the best I could, 
 and the result probably represents the correction to at least 0-02 or 
 0-03 at every point. 
 
 (d) Reduction to the Absolute Scale 
 
 The correction to the air thermometer to reduce to the absolute 
 scale has been given by Joule and Thomson, in the Philosophical 
 Transactions for 1854; but as the formula there used is not correct, 
 I have recalculated a table from the new formula used by them in their 
 paper of 1862. 
 
 That equation, which originated with Rankine, can be placed in the form 
 
 where p, v, and /j. are the pressure, volume, and absolute temperature 
 of a given weight of the air; D is its density referred to air at C. 
 and 760 mm. pressure; fa is the absolute temperature of the freezing 
 point; and m is a constant which for air is 0-33 C. 
 For the air thermometer with constant volume 
 
 T = 100 P'~P 
 
 or, since D = 1, 
 
 tt - /,, = T- -00088 T 
 
 from which I have calculated the following table of corrections: 
 
382 
 
 HENRY A". ROWLAND 
 
 TABLE XVII. REDUCTION OF AIR THERMOMETER TO ABSOLUTE SCALE. 
 
 T 
 Air Thermometer. 
 
 M ("0 
 
 Absolute Temperature. 
 
 A 
 
 or Correction to Air 
 Thermometer. 
 
 
 
 
 
 
 
 
 
 10 
 
 9-9972 
 
 0028 
 
 20 
 
 19-9952 
 
 0048 
 
 30 
 
 29-9939 
 
 0061 
 
 40 
 
 39-9933 
 
 0067 
 
 50 
 
 49-9932 
 
 0068 
 
 60 
 
 59-9937 
 
 0063 
 
 70 
 
 69-9946 
 
 0054 
 
 80 
 
 79-9956 
 
 0044 
 
 90 
 
 89-9978 
 
 0022 
 
 100 
 
 100-000 
 
 
 
 200 
 
 200-037 
 
 + -037 
 
 300 
 
 300-092 
 
 + -092 
 
 400 
 
 400-157 
 
 -1- -157 
 
 500 
 
 500-228 
 
 + -228 
 
 It is a curious circumstance, that the point of maximum difference 
 occurs at about the same point as in the comparison of the mercurial 
 and air thermometers. 
 
 From the previous formula, and from this table of corrections, the 
 following tables were constructed. 
 
 TABLE XVIII. THERMOMETER No. 6163. 
 
 Reading In 
 Millimeters on 
 Stem. 
 
 Temperature 
 on Mercurial 
 Thermometer, 
 and 100 fixed. 
 
 Temperature 
 on Mercurial 
 Thermometer 
 and 40 fixed by 
 Air Thermom. 
 
 Temperature 
 on Air Ther- 
 mometer. 
 
 Temperature 
 on Absolute 
 Scale from C. 
 
 Reading In 
 Millimeters on 
 Stem. 
 
 Temperature 
 ou Mercurial 
 Thermometer, 
 0andlOUnxed. 
 
 Temperature 
 on Mercurial 
 Thermom., 
 and 40 fixed by 
 Air Thermom. 
 
 Temperature 
 ou Air Ther- 
 mometer. 
 
 Temperature 
 on Absolute 
 Scale fromOC. 
 
 50 
 
 923 
 
 - 917 
 
 _911 
 
 -911 
 
 240 
 
 20-557 
 
 20-409 
 
 20-350 
 
 20345 
 
 58-1 
 
 
 
 
 
 
 
 
 
 250 
 
 21-670 
 
 21.515 
 
 21-457 
 
 21-452 
 
 60 
 
 + -217 
 
 + -215 
 
 + -214 
 
 + 214 
 
 260 
 
 22-776 
 
 22-616 
 
 22 559 22 554 
 
 70 
 
 1-356 
 
 1-336 
 
 1-328 
 
 1 328 
 
 270 
 
 23-884 
 
 23-713 
 
 23-657 
 
 23.652 
 
 80 
 
 2-494 
 
 2-475 
 
 2-461 
 
 2-460 
 
 280 
 
 24-989 
 
 24-810 
 
 24-755 
 
 24-750 
 
 90 
 
 3-631 
 
 3-604 
 
 3-584 
 
 3-583 
 
 290 
 
 26-093 25-907 
 
 25-854 
 
 25 848 
 
 100 
 
 4-767 
 
 4-733 
 
 4-707 
 
 4-706 
 
 300 
 
 27-200 27-006 
 
 26-956 
 
 26-950 
 
 110 
 
 5-903 
 
 5-860 
 
 5-829 
 
 5-827 
 
 310 
 
 28-311 
 
 28-108 
 
 28-060 
 
 28 056 
 
 120 
 
 7-036 
 
 6-986 
 
 6-950 
 
 6-948 
 
 320 
 
 29-425 
 
 29-214 
 
 29-169 
 
 39-163 
 
 130 
 
 8-170 
 
 8-111 
 
 8-071 
 
 8-069 
 
 330 
 
 30-541 
 
 30-324 
 
 30-282 
 
 30 -276 
 
 140 
 
 9-304 
 
 9-237 
 
 9-193 
 
 9-190 
 
 340 
 
 31-662 
 
 31-436 
 
 31-398 
 
 31-392 
 
 150 
 
 10-436 
 
 10.361 
 
 10-314 
 
 10-311 
 
 350 
 
 32.782 
 
 32-548 
 
 32,- 51 4 
 
 32-508 
 
 160 
 
 11-568 
 
 11-485 
 
 11-435 
 
 11-432 
 
 360 
 
 33-903 
 
 33-660 
 
 33-630 
 
 33-624 
 
 170 
 
 12-700 
 
 12-608 
 
 12-556 
 
 12-553 
 
 370 
 
 35-023 
 
 34-773 
 
 34-748 
 
 34-742 
 
 180 
 
 13-829 
 
 13-730 
 
 13-676 
 
 13-672 
 
 380 
 
 36-143 
 
 35-884 
 
 35-864 
 
 35-857 
 
 190 
 
 14-957 
 
 14-850 
 
 14-794 
 
 14-790 
 
 390 
 
 37-261 
 
 36-994 
 
 36-979 
 
 36-972 
 
 200 
 
 16-081 
 
 15-966 
 
 15-909 
 
 15-905 
 
 400 
 
 38-377 
 
 38-103 
 
 38-094 
 
 38-087 
 
 210 
 
 17-203 
 
 17-080 
 
 17-022 
 
 17-018 
 
 410 
 
 89-493 
 
 39-210 
 
 39-206 
 
 39 199 
 
 220 
 
 18-322 
 
 18-191 
 
 18-132 
 
 18-127 
 
 420 
 
 40-604 
 
 40-314 
 
 40-316 
 
 40-309 
 
 230 
 
 19-440 
 
 19-301 
 
 19-242 
 
 19-237 
 
 
 
 
 
 
TABLE XIX. THERMOMETER No. 6165. 
 
 Reading In 
 Millimeters on 
 
 Htom. 
 
 Temperature 
 on Mercurial, 
 Thermometer, 
 0* and 100 fixed. 
 
 Temperature 
 on Mercurial 
 Thermom., 
 and 40 fixed by 
 Air Thermom. 
 
 O 1 S) m ^ 
 U u . U. * o 
 
 S*2 HI 
 
 tH <Q CO O "> 
 fc- ^ S I* 03 O 
 b 0> .Q *-t 
 
 o, o a<*~ 1 
 
 o a 5 fl< 3 
 H o H 0$ 
 
 Reading In 
 Millimeters on 
 Stem. 
 
 Temperature 
 on Mercurial 
 Thermometer, 
 and 10U fixed. 
 
 Temperature 
 on Mercurial 
 Thermom., 
 and 40 fixed by 
 Air Thermom. 
 
 Temperature 
 on Air Ther- 
 mometer. 
 
 Temperature 
 on Absolute 
 Scale from C. 
 
 30 
 
 464 
 
 460 
 
 o o 
 .457 -457 
 
 230 
 
 17-198 
 
 17-067 
 
 17-009 
 
 17-005 
 
 35 
 
 
 
 
 
 
 
 240 
 
 18-056 
 
 17-920 
 
 17-861 
 
 17-8.57 
 
 40 
 
 + 463 
 
 + -460 
 
 + 457 +-457 
 
 250 
 
 18-917 
 
 18-773 
 
 18-714 
 
 18-709 
 
 50 
 
 1-387 
 
 1-376 
 
 1-368 1-368 
 
 260 
 
 19-771 
 
 19-621 j 19-562 
 
 19-557 
 
 60 
 
 2-307 
 
 2-290 
 
 2-276 2-275 
 
 270 
 
 20-621 
 
 20-465 ! 20-406 
 
 20-401 
 
 70 
 
 3-216 3-192 
 
 3-174 3-173 
 
 280 
 
 21-469 
 
 21-306 1 21-247 
 
 21-242 
 
 80 
 
 4-122 4-092 
 
 4-069 4-068 
 
 290 
 
 22-308 
 
 22-139 22-081 
 
 22-076 
 
 90 
 
 5-022 
 
 4-984 
 
 4-957 4-955 
 
 300 
 
 23-144 
 
 22-969 
 
 22-912 
 
 22-907 
 
 100 
 
 5-916 
 
 5-872 
 
 5 841 5 839 
 
 310 
 
 23-974 
 
 23-792 
 
 23-736 
 
 23-731 
 
 110 
 
 6-804 
 
 6-753 
 
 6-714 6.712 
 
 320 
 
 24 796 
 
 24-607 24.552 
 
 24-547 
 
 120 
 
 7-685 
 
 7-628 
 
 7-590 7-588 
 
 330 
 
 25-618 
 
 25-424 25-370 
 
 25-365 
 
 130 
 
 8-564 
 
 8-500 
 
 8-459 8.456 
 
 340 
 
 26-433 
 
 26-232 26-180 
 
 26-174 
 
 140 
 
 9-439 9.368 
 
 9-324 9-321 
 
 350 
 
 27-245 
 
 27-038 
 
 26-987 
 
 26-981 
 
 150 
 
 10-309 10-232 
 
 10-186 10-183 
 
 360 
 
 28-049 
 
 27-837 27-788 
 
 27-782 
 
 160 
 
 11-174 11-091 
 
 11-042 11-039 
 
 370 
 
 28-856 
 
 28-637 28-590 
 
 28 584 
 
 170 
 
 12-038 11.947 
 
 11-896 11-893 
 
 380 
 
 29-651 
 
 29-426 29-382 
 
 29-376 
 
 180 
 
 12-900 12-802 
 
 12.749 12.746 
 
 390 
 
 30-449 
 
 30-218 30-176 
 
 30-170 
 
 190 
 
 13-760 13-655 
 
 13-601 13-598 
 
 400 
 
 31-249 
 
 31-011 ; 30-971 
 
 30-965 
 
 200 
 
 14-619 14-508 
 
 14-453 14-450 
 
 410 
 
 32-073 
 
 31-829 31-782 
 
 31-786 
 
 210 
 
 15-479 15-362 
 
 15-305 15-302 
 
 420 
 
 32-861 
 
 32-611 
 
 32-577 
 
 32-581 
 
 220 
 
 16-340 
 
 16-215 
 
 16-157 16-153 
 
 
 
 
 
 
 TABLE XX. THERMOMETER No. 6166. 
 
 a 
 
 in iT 1 ? 
 
 -6 
 
 m i 
 
 
 
 a 
 
 --o ffi _ .--d 
 
 
 > _ d 
 
 Reading In 
 Millimeters c 
 Stem. 
 
 Temperatun 
 ou Mercurla 
 Thermomete] 
 0aud 100 flxe 
 
 Temperature 
 on Mercurla 
 Thermometel 
 and 40 flxe 
 
 Temperatun 
 on Air Ther- 
 mometer. 
 
 Temperaturi 
 on Absolute 
 Scale from 
 
 Reading In 
 Millimeters o 
 Stem. 
 
 Temperatur 
 on Mercurla 
 Thermomete 
 and 100 flxe 
 
 Temperatur 
 on Mercurla 
 Thermomete 
 and 40 flxe 
 
 Temperatur 
 on Air Ther 
 mometer. 
 
 Temperatur 
 on Absolute 
 Scale from t> 
 
 20 
 
 036 
 
 036 
 
 034 
 
 034 
 
 230 
 
 16-478 
 
 16-356 
 
 16-298 
 
 16-294 
 
 30 
 
 + 770 
 
 + 764 
 
 + 759 
 
 + 759 
 
 240 
 
 17-259 
 
 17-132 
 
 17-074 
 
 17-070 
 
 40 
 
 1-574 
 
 1-562 
 
 1-553 
 
 1-553 
 
 250 
 
 18-042 
 
 17-908 
 
 17-849 
 
 17-845 
 
 50 
 
 2 368 
 
 2-350 
 
 2-336 
 
 2-335 
 
 260 
 
 18-825 
 
 18-686 
 
 18-627 
 
 18-622 
 
 60 
 
 3-156 
 
 3-133 
 
 3-115 
 
 3-114 
 
 270 
 
 19-609 
 
 19-464 
 
 19-405 
 
 19-400 
 
 70 
 
 3-941 
 
 3-911 
 
 3 889 
 
 3-888 
 
 280 
 
 20-392 
 
 20-241 
 
 20-182 
 
 20-177 
 
 80 
 
 4-726 
 
 4-691 
 
 4-665 
 
 4-664 
 
 290 
 
 21-176 
 
 21-019 
 
 20-960 
 
 20-955 
 
 90 
 
 5 509 
 
 5-468 
 
 5-438 
 
 5-436 
 
 300 
 
 21 735 
 
 21-793 
 
 21-735 
 
 21 730 
 
 100 
 
 6-293 
 
 6-246 
 
 6-212 
 
 6-210 j 
 
 310 
 
 22-511 
 
 22 569 
 
 22-511 
 
 22-506 
 
 110 
 
 7-076 
 
 7-024 
 
 6 -988 
 
 6-986 
 
 320 
 
 23-292 
 
 23-349 
 
 23-292 
 
 23-287 
 
 120 
 
 7-862 
 
 7-804 
 
 7 765 
 
 7-763 
 
 330 
 
 24-075 
 
 24-131 
 
 24 075 
 
 24-070 
 
 130 
 
 8-649 
 
 8-585 
 
 8-544 
 
 8-542 
 
 340 
 
 24-855 
 
 24-910 
 
 24-855 
 
 24-850 
 
 140 
 
 9-437 
 
 9-367 
 
 9 323 
 
 9-321 
 
 350 
 
 25-634 
 
 25-687 
 
 25 634 
 
 25-628 
 
 150 
 
 10-228 
 
 10-151 
 
 10-105 
 
 10-102 
 
 360 
 
 26-415 
 
 26-466 
 
 26-412 
 
 26-406 
 
 160 
 
 11-017 
 
 10-935 
 
 10-887 
 
 10-884 
 
 370 
 
 27-441 
 
 27-245 
 
 27-195 
 
 27-189 
 
 170 
 
 11-805 
 
 11-717 
 
 11-667 
 
 11-664 
 
 380 
 
 28 240 
 
 28-030 
 
 27-982 
 
 27-976 
 
 180 
 
 12-589 
 
 12-496 
 
 12-444 
 
 12-441 
 
 390 
 
 29-030 
 
 28-814 
 
 28-768 
 
 28-762 
 
 190 
 
 13-370 
 
 13-271 
 
 13-217 
 
 13-214 
 
 400 
 
 29-819 
 
 29-597 
 
 29-550 
 
 29-544 
 
 200 
 
 14-148 
 
 14-043 
 
 13-988 
 
 13-984 
 
 410 
 
 30-608 
 
 30-381 
 
 30-339 
 
 30-333 
 
 210 
 
 14-923 
 
 14-812 
 
 14-756 
 
 14-753 
 
 420 
 
 31-396 
 
 31-162 
 
 31-123 
 
 31-117 
 
 220 
 
 15- 699 
 
 15 583 
 
 15-526 
 
 15-522 
 
 430 
 
 32-189 
 
 31-950 
 
 31-914 
 
 31-908 
 
384 
 
 HENRY A. BOWLAND 
 
 In using these tables a correction is of course to be made should the 
 zero point change. 
 
 TABLE XXI. CORRECTION OF KEW STANDARD TO THE ABSOLUTE SCALE. 
 
 Temperature C. 
 
 Correction in 
 degrees C. 
 
 
 
 
 
 10 
 
 03 
 
 20 
 
 05 
 
 30 
 
 06 
 
 40 
 
 07 
 
 50 
 
 07 
 
 60 
 
 06 
 
 70 
 
 04 
 
 80 
 
 02 
 
 90 
 
 01 
 
 100 
 
 
 
 Appendix to Thermometry 
 
 The last of January, 1879, Mr. S. W. Holman, of the Massachusetts 
 Institute of Technology, came to Baltimore to compare some thermom- 
 eters with the air thermometer; and by his kindness I will give here 
 the results of the comparison which we then made together. 
 
 As in this comparison some thermometers made by Fastre in 1851 
 were used, the results are of the greatest interest. 
 
 The tables are calculated with the newest value for the coefficient of 
 expansion of glass. The calibration of all the thermometers, except 
 the two by Casella, has been examined, and found good. The Casella 
 thermometers had no reservoir at the top, and could not thus be readily 
 calibrated after being made. The G-eissler also had none, but I suc- 
 ceeded in separating a column. 
 
 The absence of a reservoir at the top should immediately condemn 
 a standard, for there is no certainty in the work done with it. 
 
 From these tables we would draw the inference that No. 6163 repre- 
 sents the air thermometer with considerable accuracy. At the same 
 time, both tables would give a smaller value of ra than I have used, 
 and not very far from the value found before by direct comparison, 
 namely, -00015. 
 
 The difference from using m= -00018 would be a little over 0-01 C. 
 at the 20 point. 
 
 All the other thermometers stand above the air thermometer, between 
 and 100, by amounts ranging between about 0-05 and 0-35C., 
 
. 
 
 385 
 
 TABLE XXII. SEVENTH SERIES. 
 
 Air 
 
 Ther- 
 mome- 
 ter. 
 
 Original Readings. 
 
 Reduced Readings. 
 
 6163. 
 
 7334 
 Baudln. 
 
 Kew 
 Stand- 
 ard 
 No. 104. 
 
 32374 
 Casella. 
 
 Gelss- 
 ler. 
 
 6163 
 Reduced 
 to Air 
 Ther- 
 mome- 
 ter. 
 
 7334 
 Baudln. 
 
 Kew 
 Stand- 
 ard 
 No. 104. 
 
 32374 
 Casella. 
 
 Gelss- 
 ler. 
 
 6 
 
 is-43 
 6-08 
 12-68 
 20-49 
 24-55 
 29-51 
 39-45 
 39-15 
 51-17 
 61-12 
 70-74 
 80-09 
 80-39 
 89-95 
 89-92 
 100-00 
 
 "58-83 
 63-5 
 113-0 
 171-55 
 242-0 
 278-8 
 323-9 
 413-1 
 410-7 
 
 11 
 
 32-68 
 33-60 
 43-65 
 55-47 
 69-55 
 76-90 
 85-88 
 103-72 
 103-23 
 124-84 
 142-73 
 159-87 
 176-50 
 177-23 
 194-35 
 194-22 
 212-37 
 
 + 20 
 71 
 6-33 
 12-91 
 20-77 
 24-80 
 29-80 
 39-76 
 39-48 
 51-49 
 61-47 
 71-00 
 80-31 
 80-74 
 90-22 
 90-18 
 100-06 
 
 + 69 
 
 13-42 
 21-29 
 25-33 
 30-32 
 40-22 
 39-98 
 51-83 
 61-69 
 71-14 
 80-25 
 80-66 
 90-11 
 90-06 
 99-32 
 
 8 
 
 52 
 6-08 
 12-65 
 20-49 
 24-54 
 29 52 
 39-47 
 39-20 
 
 8 
 
 o 
 
 
 52 
 6-11 
 12-68 
 20-57 
 24-61 
 29-61 
 39-53 
 39-26 
 51-29 
 61-24 
 70-78 
 80-04 
 80-44 
 89-97 
 89-90 
 100-00 
 
 8 
 51 
 6-13 
 12-70 
 20-56 
 24-59 
 29-58 
 39-54 
 39-26 
 51-26 
 61-23 
 70-76 
 80-06 
 80-49 
 89-97 
 89-93 
 100-00 
 
 8 
 
 
 12-73 
 20-63 
 24-66 
 29-66 
 39-62 
 39-34 
 51-32 
 61-29 
 70-83 
 80-02 
 80-43 
 89-93 
 89-89 
 100-00 
 
 
 12-59 
 20-48 
 24-50 
 29-49 
 39-43 
 39-15 
 51-10 
 61-05 
 70-57 
 79-74 
 80-15 
 89-63 
 89-59 
 99-69 
 
 12-82 
 20-74 
 24-81 
 29-83 
 39-80 
 39-56 
 51-49 
 61-41 
 70-92 
 80-10 
 80-51 
 90-03 
 89-98 
 100-00 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 TABLE XXIII. EIGHTH SERIES. 
 
 Air 
 Ther- 
 mome- 
 ter. 
 
 Original Readings. 
 
 Reduced Readings. 
 
 6163. 
 
 378 
 Fastre. 
 
 7316 
 Baudln. 
 
 368 
 Fastr6. 
 
 3235 
 Casella. 
 
 6163 
 Reduced 
 to Air 
 Ther- 
 mome- 
 ter. 
 
 376 
 
 Fastrfi. 
 
 7316 
 Baudln. 
 
 368 
 
 Fastre. 
 
 3236 
 Casella. 
 
 6 
 3.67 
 11-55 
 20-72 
 32-19 
 39-36 
 50-71 
 60-10 
 73-82 
 86-50 
 
 " 58 60 
 90-7 
 161-6 
 243-7 
 347-4 
 411-85 
 
 111-3 
 130-0 
 170-9 
 217-9 
 276-9 
 313-85 
 372-0 
 420-0 
 490-6 
 555-25 
 550-2 
 624-93 
 
 23 
 
 11-40 
 20-59 
 32-09 
 39-26 
 50-57 
 59-92 
 73-59 
 86-16 
 85-21 
 99-70 
 
 87-6 
 106-25 
 147-2 
 194-2 
 253-2 
 290-1 
 248-2 
 396-45 
 466-85 
 531-22 
 525-95 
 600-58 
 
 32-80 
 39-35 
 53-70 
 70-15 
 90-80 
 103-68 
 123-65 
 140-80 
 165-68 
 188-20 
 186-42 
 212-45 
 
 o 
 
 
 3-61 
 11-56 
 20-70 
 32-17 
 39-36 
 
 o 
 
 3-64 
 11-60 
 20-75 
 32-24 
 39-43 
 50-75 
 60-10 
 73-84 
 86-48 
 86-45 
 100-00 
 
 
 
 8 
 
 3-64 
 11-62 
 20-80 
 32-28 
 39-48 
 50-80 
 60-21 
 73-93 
 86-56 
 85-45 
 100-00 
 
 8 
 
 3-65 
 11-63 
 20-79 
 32-29 
 39-45 
 50-57 
 60-12 
 73-97 
 86-56 
 85-51 
 100-00 
 
 11-64 
 20-84 
 32-34 
 39-52 
 50-84 
 60-19 
 73-87 
 86-51 
 85-50 
 100-00 
 
 
 
 
 100-00 
 
 none standing below. Indeed, no table has ever been published show- 
 ing any thermometer standing below the air thermometer between 
 
 17 The original readings in ice were 58-68 and 58-45, to which -15 was added to 
 allow for the pressure of water in the comparator. This, of course, gives the same 
 final result as if -15 were subtracted from each of the other temperatures. No cor- 
 rection was made to the others. 
 
 18 Probably some error of reading. 
 
 25 
 
386 
 
 HENEY A. ROWLAND 
 
 and 100. By inference from experiments above 100 on crystal glass 
 by Regnault, thermometers of this glass should stand below, but it 
 never seems to have been proved by direct experiment. The Fastre 
 thermometers are probably made of this glass, and my Baudin's cer- 
 tainly contain lead; and yet these stand above, though only to a small 
 amount, in the case of the Fastre's. 
 
 The Geissler still seems to retain its pre-eminence as having the 
 greatest error of the lot. 
 
 The Baudin thermometers agree well together, but are evidently 
 made from another lot of glass from the No. 6167 used before. These 
 last two depart less from the air thermometer. The explanation is 
 plain, as Baudin had manufactured more than one thousand ther- 
 mometers between the two, and so had probably used up the first stock 
 of glass. And even glass of the same lot differs, especially as Regnault 
 has shown that the method of working it before the blow-pipe affects 
 it very greatly. 
 
 It is very easy to test whether the calorimeter thermometers are of 
 the same glass as any of the others, by testing whether they agree with 
 No. 6163 throughout the whole range of 40. The difference in the 
 values of m for the two kinds of glass will then be about -003 of the 
 difference between them at 20, the and 40 points agreeing. The 
 only difficulty is in calibrating or reading the 100 thermometers accur- 
 ately enough. 
 
 The Baudin thermometers were very well calibrated, and were 
 graduated to ^ C., and so were best adapted to this kind of work. 
 Hence I have constructed the following tables, making the and 40 
 points agree. 
 
 TABLE XXIV. COMPARISON OF 6163 AND THE BATJDIN STANDARDS. 
 
 6163 
 Mercurial 
 and 40 
 fixed. 
 
 7334.19 
 
 Difference. 
 
 6163 
 Mercurial 
 and 40 
 fixed. 
 
 7316. 19 
 
 Difference. 
 
 
 
 
 
 
 
 
 
 
 
 
 
 12-699 
 
 12-673 
 
 + 026 
 
 11-609 
 
 11-584 
 
 + 025 
 
 20-547 
 
 20-553 
 
 006 
 
 20-762 
 
 20-746 
 
 + 016 
 
 24-604 
 
 24-567 
 
 + 037 
 
 32-203 
 
 32-211 
 
 008 
 
 29-564 
 
 29-550 
 
 + 014 
 
 39-358 
 
 39-358 
 
 
 
 39-337 
 
 39-337 
 
 
 
 
 
 
 19 A correction of 0-01 was made to the zero points of these thermometers on ac- 
 count of the pressure of the water. 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 387 
 
 Taking the average of the two, it would seem that No. 6163 stood 
 about -015 higher than the mean of 7334 and 7316 at the 20 point, 
 or 6163 has a higher value of ra by -000045 than the others. 
 
 These differ about -17 from the air thermometer at 40, which gives 
 the value of m about -000104. Whence m for 6163 is -00015, as we 
 have found before by direct comparison with the air thermometer. 
 
 I am inclined to think that the former value, -00018, is too large, 
 and to take -00015, which is the value found by direct comparison, as 
 the true value. As the change, however, only makes at most a differ- 
 ence of 0-01 at any one point, and as I have already used the previous 
 value in all calculations, I have not thought it worth while to go over 
 all my work again, but will 'refer to the matter again in the final 
 results, and then reduce the final results to this value. 
 
 m. CALOKIMETKY 
 (a) Specific Heat of Water 
 
 The first observers on the specific heat of water, such as De Luc, 
 completed the experiment with a view of testing the thermometer; and 
 it is curious to note that both De Luc and Flaugergues found th tem- 
 perature of the mixture less than the mean of the two equal portions 
 of which it was composed, and hence the specific heat of cold water 
 higher than that of warm. 
 
 The experiments of Flaugergues were apparently the best, and he 
 found as follows : " 
 
 3 parts of water at and 1 part at 80 R. gave 19 -86 K. 
 2 parts of water at and 2 parts at 80 R. gave 39 -81 R. 
 1 part of water at and 3 parts at 80 R. gave 59 -87 R. 
 
 But it is not at all certain that any correction was made for the 
 specific heat of the vessel, or whether the loss by evaporation or radia- 
 tion was guarded against. 
 
 The first experiments of any accuracy on this subject seem to have 
 been made by F. E. Neumann in 1831. 21 He finds that the specific 
 heat of water at the boiling point is 1-0127 times that at about 28 C. 
 (22 R.). 
 
 The next observer seems to have been Regnault, 22 who, in 1840, 
 
 M Gehler, Phys. Worterbuch, i, 641. 
 "Pogg. Ann., xxiii, 40. 
 22 Ibid., li, 72. 
 
388 HENRY A. EOWLAND 
 
 found the mean specific heat between 100 C. and 16 C. to be 1-00709 
 and 1-00890 times that at about 14. 
 
 But the principal experiments on the subject were published by 
 Eegnault in 1850, 23 and these have been accepted to the present time. 
 It is unfortunate that these experiments were all made by mixing water 
 above 100 with water at ordinary temperatures, it being assumed that 
 water at ordinary temperatures changes little, if any. An interpolation 
 formula was then found to represent the results; and it was assumed 
 that the same formula held at ordinary temperature, or even as low 
 as C. It is true that Eegnault experimented on the subject at 
 points around 4 C. by determining the specific heat of lead in water 
 at various temperatures; but the results were not of sufficient accuracy 
 to warrant any conclusions except that the variation was not great. 
 
 Boscha has attempted to correct Eegnault's results so as to reduce 
 them to the air thermometer; but Eegnault, in Comptes Rendus, has 
 not accepted the correction, as the results were already reduced to the 
 air thermometer. 
 
 Him (Comptes Rendus, Ixx, 592, 831) has given the results of some 
 experiments on the specific heat of water at low temperatures, which 
 give the absurd result that the specific heat of water increases about 
 six or seven per cent between zero and 13! The method of experi- 
 ment was to immerse the bulb of a water thermometer in the water 
 of the calorimeter, until the water had contracted just so much, when 
 it was withdrawn. The idea of thus giving equal quantities of heat 
 to the water was excellent, but could not be carried into execution 
 without a great amount of error. Indeed, experiments so full of error 
 only confuse the physicist, and are worse than useless. 
 
 The experiments of Jamin and Amaury, by the heating of water by 
 electricity, were better in principle, and, if carried out with care, would 
 doubtless give good results. But no particular care seems to have 
 been taken to determine the variation of the resistance of the wire 
 with accuracy, and the measurement of the temperature is passed over 
 as if it were a very simple, instead of an immensely difficult matter. 
 Their results are thus to be rejected; and, indeed, Eegnault does not 
 accept them, but believes there is very little change between 5 and 25. 
 
 In PoggendorfFs Annalen for 1870 a paper by Pfaundler and Platter 
 appeared, giving the results of experiments around 4 C., and deducing 
 the remarkable result that water from to 10 C. varied as much as 
 
 "Pogg. Ann., Ixxix, 241; also, Rel. d. Exp., i, 729. 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 389 
 
 twenty per cent in specific heat, and in a very irregular manner, first 
 decreasing, then increasing, and again decreasing. But soon after an- 
 other paper appeared, showing that the results of the previous experi- 
 ments were entirely erroneous. 
 
 The new experiments, which extended up to 13 C., seemed to give 
 an increase of specific heat up to about 6, after which there was appar- 
 ently a decrease. It is to be noted that Geissler's thermometers were 
 used, which I have found to depart more than any other from the air 
 thermometer. 
 
 But as the range of temperature is very small, the reduction to the 
 air thermometer will not affect the results very much, though it will 
 somewhat decrease the apparent change of specific heat. 
 
 In the Journal de Physique for November, 1878, there is a notice of 
 some experiments of M. von Miinchausen on the specific heat of water. 
 The method was that of mixture in an open vessel, where evaporation 
 might interfere very much with the experiment. No reference is made 
 to the thermometer, but it seems not improbable that it was one from 
 Geissler; in which case the error would be very great, as the range was 
 large, and reached even up to 70 C. The error of the Geissler would 
 be in the direction of making the specific heat increase more rapidly 
 than it should. The formula he gives for the specific heat of water at 
 the temperature t is 
 
 1 -f -000302 i. 
 
 Assuming that the thermometer was from Geissler, the formula, re- 
 duced to the air thermometer, would become approximately 
 
 1 -00009 t+ -0000015 t 2 . 
 
 Had the thermometer been similar to that of Kecknagel, it would 
 have been 1 -f -000045 t -f -000001 t 2 . 
 
 It is to be noted that the first formula would actually give a decrease 
 of specific heat at first, and then an increase. 
 
 As all these results vary so very much from each other, we can 
 hardly say that we know anything about the specific heat of water 
 between and 100, though Kegnault's results above that temperature 
 are probably very nearly correct. 
 
 It seems to me probable that my results with the mechanical equiv- 
 alent apparatus give the variation of the specific heat of water with 
 considerable accuracy; indeed, far surpassing any results which we 
 can obtain by the method of mixture. It is a curious result of those 
 experiments, that at low temperatures, or up to about 30 C., the spe- 
 
390 HENKY A. EOWLAXD 
 
 cific heat of water is about constant on the mercurial thermometer made 
 by Baudin, but decreases to a minimum at about 30 when the reduction 
 is made to the air thermometer or the absolute scale, or, indeed, the Kew 
 standard. 
 
 As this curious and interesting result depends upon the accurate 
 comparison of the mercurial with the air thermometer, I have spent 
 the greater part of a year in the study of the comparison, but have not 
 been able to find any error, and am now thoroughly convinced of the 
 truth of this decrease of the specific heat. But to make certain, I have 
 instituted the following independent series of investigations on the 
 specific heat of water, using, however, the same thermometers. 
 
 The apparatus is shown in Fig. 4. A copper vessel, A, about 20 cm. 
 in diameter and 23 cm. high, rests upon a tripod. In its interior is a 
 three-way stopcock, communicating with the small interior vessel B, 
 the vessel A, and the vulcanite spout C. By turning it, the vessel B 
 could be filled with water, and its temperature measured by the ther- 
 mometer D, after which it could be delivered through the spout into 
 the calorimeter. As the vessel B, the stopcock, and most of the spout, 
 were within the vessel A, and thus surrounded by water, and as the 
 vulcanite tube was very thin, the water could be delivered into the 
 calorimeter without appreciable change of temperature. The proof of 
 this will follow later. 
 
 The calorimeter, E, was of very thin copper, nickel-plated very 
 thinly. A hole in the back at F allowed the delivery spout to enter, 
 and two openings on top admitted the thermometers. A wire attached 
 to a stirrer also passed through the top. The calorimeter had a capac- 
 ity of about three litres, and weighed complete about 388-3 grammes. 
 Its calorific capacity was estimated at 35-4 grammes. It rested on 
 three vulcanite pieces, to prevent conduction to the jacket. Around 
 the calorimeter on all sides was a water-jacket, nickel-plated on its 
 interior, to make the radiation perfectly definite. 
 
 The calorific capacity of the thermometers, including the immersed 
 stem and the mercury of the bulb, was estimated as follows : 14 cm. of 
 stem weighed about 3-8 gr., and had a capacity of -8 gr.; 10 gr. of 
 mercury had a capacity of -3 gr.; total, 1-1 gr. 
 
 Often the vessel B was removed, and the water allowed to flow 
 directly into the calorimeter. 
 
 The following is the process followed during one experiment at low 
 temperatures. The vessel A was filled with clean broken ice, the open- 
 ing into the stopcock being covered with fine gauze to prevent any 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 391 
 
 small particles of ice from flowing out. The whole was then covered 
 with cloth, to prevent melting. The vessel was then filled with water, 
 and the two thermometers immersed to get the zero points. The 
 calorimeter being about two-thirds filled with water, and having been 
 weighed, was then put in position, the holes corked up, and one ther- 
 mometer placed in it, the other being in the melting ice. An obser- 
 vation of its temperature was then taken every minute, it being fre- 
 quently stirred. 
 
 FIG. 4. 
 
 When enough observations had been obtained in this way, the cork 
 was taken out of the aperture F and the spout inserted, and the water 
 allowed to run for a given time, or until the calorimeter was full. It 
 was then removed, the cork replaced, and the second thermometer 
 removed from the ice to the calorimeter. Observations were then 
 taken as before, and the vessel again weighed. 
 
 Two thermometers were used in the way specified, so that one might 
 approach the final temperature from above and the other from below. 
 But no regular difference was ever observed, and so some experiments 
 
392 HENRY A. EOWLAND 
 
 were made with both thermometers in the calorimeter during the whole 
 experiment. 
 
 The principal sources of error are as follows : 
 
 1st. Thermometers lag behind their true reading. This was not 
 noticed, and would probably be greater in thermometers with very fine 
 stems like Geissler's. At any rate, it was almost eliminated in the 
 experiment by using two thermometers. 
 
 2d. The water may be changed in temperature in passing through 
 the spout. This was eliminated by allowing the water to run some 
 time before it went into the calorimeter. The spout being very thin, 
 and made of vulcanite, covered on the outside with cloth, it is not 
 thought that there was any appreciable error. It will be discussed 
 more at length below, and an experiment given to prove this. 
 
 3d. The top of the calorimeter not being in contact with the water, 
 its temperature may be uncertain. To eliminate this, the calorimeter 
 was often at the temperature of the air to commence with. Also the 
 water was sometimes violently agitated just before taking the final 
 reading, previous to letting in the cold water. Even if the tempera- 
 ture of this part was taken as that of the air, the error would scarcely 
 ever be of sufficient importance to vitiate the conclusions. 
 
 4th. The specific heat of copper changes with the temperature. 
 Unimportant. 
 
 5th. Some water might remain in the spout whose temperature might 
 be different from the rest. This was guarded against. 
 
 6th. Evaporation. Impossible, as the calorimeter was closed. 
 
 7th. The introduction of cold water may cause dew to be deposited on 
 the calorimeter. The experiments were rejected where this occurred. 
 
 The corrections for the protruding thermometer stem, for radiation, 
 &c., were made as usual, the radiation being estimated by a series of 
 observations before and after the experiment, as is usual in determin- 
 ing the specific heat of solids. 
 
 June 14, 1878. First Experiment 
 Time. Ther. 6163. Ther. 6166. Points. 
 
 41 296-75 6163, 57-9 Air, 21 C. 
 
 42 296-7 6165, 34-8 Jacket about 25 C. 
 
 43 296-7 6166, 20-5* 
 
 44 296-65 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 393 
 
 Time. Ther. 6163. Ther. 6166. 
 
 44i-44f Water running. 
 
 46* 218-7 251-7 
 
 47* 218-8 251-8 
 
 48* 218-9 252-0 
 
 Temperature before 296-6 
 Correction for + -2 
 
 296-8=26-597 
 
 Correction for stem + '019 
 
 Initial temperature of 
 
 calorimeter 26-616 
 
 218-6 + -2 = 218-8 = 17-994 
 Correction for stem -006 
 
 Points. 
 
 Calorimeter before 2043-0 
 
 " after 2853'3 
 
 Water at added 810-3 
 
 Thermometer 1-1 
 
 Total at 8114 
 
 Calorimeter before 2043'0 
 
 Weight of Vessel 388-3 
 
 Water 1654-7 
 
 Capacity of calorimeter 35-4 
 
 " thermometer 1*1 
 
 Total capacity 1691-2 
 
 251-6 - 1 = 251-5 = 17-962- 
 
 Correction for stem -006 
 
 17-956 
 
 17-988 
 Mean temperature of mixture, 17 -972. 
 
 Mean specific heat 18 _ 1691-2 X 8-644 _ 
 Mean specific heat 18 27 ~~ 811-4 X 17'972 
 
 June lit. Second Experiment 
 
 Calorimeter before 2016-3; temperature 361-4 by No. 6163. 
 Calorimeter after 3047-0; temperature 244-5 and 288-7. 
 
 Air, 21 C.; jacket about 27. 
 
 361-4+ -2 = 361-6 = 33-803, or 33-863 when corrected for stem. 
 244-5 -|_ -2 = 244-7 = 20-865; no correction for stem. 
 288-7 1 = 288-6 = 20 -846; no correction for stem. 
 
 Mean, 20 -855. 
 
 Mean specific heat between and 21 _ ^.QQgg 
 Mean specific heat between 21 and 34 
 
 June l-'f. Third Experiment 
 
 Calorimeter before 1961-8; temperature 293-6 by No. 6166. 
 Calorimeter after 3044-6; temperature 243-7 and 213-0. 
 
 Air and jacket, about 18 C. 
 
394 HENET A. EOWLAND 
 
 393-6 -l = 393-5 = 29-036, or 29-077 when corrected for stem. 
 243-7 -1 = 243 -6 = 17 -349; no correction for stem. 
 213-0 + -2 = 213-2 = 17 -374; no correction for stem. 
 
 Mean, 17 -361. 
 
 Mean specific heat between and 17 1-0024 
 
 Mean specific heat between 17 and 29 ~ 
 
 It is to he observed that thermometer No. 6166 in all cases gave 
 temperatures about 0-02 or 0-03 below No. 6163. This difference 
 is undoubtedly in the determination of the zero points, as on June 15 
 the zero points were found to be 20-4 and 58-0. As one has gone up 
 and the other down, the mean of the temperatures needs no correction. 
 
 June 15 
 
 Calorimeter before 2068-2; temperature 364-6 by No. 6166. 
 Calorimeter after 2929-2; temperature 249-7 and 217-7. 
 
 Air and jacket at about 22 C. 
 
 264-6 = 26-766, or 26-782 when corrected for stem. 
 249-7 = H -822, or 17-812 when corrected for stem. 
 217-7+ -l = 217-8=17-884, or 17-874 when corrected for stem. 
 
 Bejected on account of great difference in final temperatures by the 
 two thermometers, which was probably due to some error in reading. 
 
 June 21 
 
 Calorimeter before 2002-7; temperature 330-3 by No. 6163. 
 Calorimeter after 3075-2; temperature 221-9 and 256-6. 
 
 Air and jacket, 21 C. 
 
 330-3 + -1 = 330-4 = 30-321, or 30-359 when corrected for stem. 
 221-9+ -1=222-0 = 18-349, or 18-343 when corrected for stem. 
 256-6+ -0 = 256-6 = 18-358, or 18-352 when corrected for stem. 
 
 Mean, 18 -347. 
 
 Specific heat between and 18 __ 
 Specific heat between 18 and 30 ~~ 
 
 June 21 
 
 Calorimeter before 2073-8; temperature 347-8 by No. 6166. 
 Calorimeter after 2986-8: temperature 234-5 and 206-6. 
 
 Air and jacket, about 21 C. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 395 
 
 347-8+ -0 = 347-8 = 25 -457, or 25-471 when corrected for stem. 
 234-5 + -0 = 234-5 = 16-643, or 16-636 when corrected for stem. 
 206-6 + -1 = 206-7 = 16-651, or 16-644 when corrected for stem. 
 
 Mean, 16 -640. 
 
 Specific heat between and 17 _ .99971 
 Specific heat between 17 and 25 ~~ 
 
 Eejected because dew was formed on the calorimeter. 
 
 A series was now tried with both thermometers in the calorimeter 
 from the beginning. 
 
 June 25 
 
 Calor. before 2220-3; temperat. 325-6 by No. 6166; 309-9 by No. 6165. 
 Calor. after 3031-4; temperat. 233-4 by No. 6166; 224-6 by No. 6165. 
 
 Air, 24 -2 C.; jacket, 23 -5. 
 
 325-6 + -0 = 325-6 = 23-725, or 23-726 when corrected for stem. 
 
 309-9 + -2 = 310-1 = 23-739, or 23-740 when corrected for stem. 
 
 233-4+ -0 = 233-4 = 16-558, or 16-545 when corrected for stem. 
 
 224-6+ -2 = 224-8 = 16-562, or 16-549 when corrected for stem. 
 
 Means, 23 -733 and 16 -547. 
 
 Specific heat between and l' _ 
 Specific heat between 16 and 24 ~ 
 
 June 25 
 
 Calor. before 2278-6; temperat. 340-35 by No. 6166; 324-1 by No. 6165. 
 Calor. after 3130-2; temperat. 242-5 by No. 6166; 232-8 by No. 6165. 
 
 Air, 23 -5 C.; jacket, 22 -5. 
 
 340-35 + -0 = 340-35 = 24 -877, or 24 -881 when corrected for stem. 
 324-1 +-2 = 324-3 = 24 -899, or 24 -903 when corrected for stem. 
 242-5 + -0 = 242-5 =17 -264, or 17 -253 when corrected for stem. 
 232-8 + -2 = 233-0 =17 -261, or 17 -250 when corrected for stem. 
 
 Specific heat between and 17 _ i . 
 Specific heat between 17 and 25 
 
 Calor. before 2316-35; temperat. 386-1 by No. 6166; 368-4 by No. 6165. 
 Calor. after 2966-90; temperat. 295-4 by No. 6166; 281-7 by No. 6165. 
 
 Air, 23-5C.; jacket, 22 -5. 
 
396 HENKY A. KOWLAND 
 
 386-1+ -0 = 386-1 = 28-455, or 2S-465 when corrected for stem. 
 
 268-4+ -2 = 368-6 = 28-472, or 28-482 when corrected for stem. 
 
 295-4+ -0 = 295-4 = 21-374, or 21-368 when corrected for stem. 
 
 281-7 + -2 = 281-9 = 21-400, or 21-394 when corrected for stem. 
 
 Means, 28 -473 and 21 -381. 
 
 Specific heat between and 21 
 "~ 
 
 _ -. 
 
 ~ 
 
 Specific heat between 2r"and~28" " 
 
 Two experiments were made on June 23 with warm water in vessel 
 A, readings being taken of the temperature of the water, as it flowed 
 out, by one thermometer, which was then transferred to the calorimeter 
 as before. 
 
 June 23 
 
 Water in A while running, 314-15 by No. 6163. 
 
 Calor. before 1530-9; temperat. 281-1 by No. 6166. 
 
 Calor. after 2996-3; temperat. 328-4 by No. 6166; 272-7 by No. 6163. 
 
 314-15 + -1 = 314-25 = 28-526, or 28-552 when corrected for stem. 
 281-1 +-0 = 281-1 =20 -262, or 20 -258 when corrected for stem. 
 328-4 +-0 = 328-4 =23 -945, or 23 -950 when corrected for stem. 
 272-7 + -1 = 272-8 =23 -960, or 23 -966 when corrected for stem. 
 
 Specific heat between 20 and 24 _ .QQDQ 
 Specific heat between 24 and 29 ~ 
 
 June 23 
 Water in A while running, 383-9 by No. 6163. 
 
 Calor. before 1624-9; temperat. 286-75 by 6166. 
 
 Calor. after 3048-2; temperat. 392-45 by 6166, and 318-1 by 6163. 
 
 383-9 + -1 = 384-0 =36-303, or 36-357 when corrected for stem. 
 286-75+ -0 = 286- 75 = 20 -702, or 20 -700 when corrected for stem. 
 392-45+ -0 = 392-45 = 28 -954, or 28 -980 when corrected for stem. 
 318-1 +-1 = 318-2 =28 -964, or 28 -992 when corrected for stem. 
 
 Specific heat between 21 and 29 _ . 
 Specific heat between 29 and 36 
 
 To test the apparatus, and also to check the estimated specific heat 
 of the calorimeter, the water was almost entirely poured out of the 
 calorimeter, and warm water placed in the vessel A, which was then 
 allowed to flow into the calorimeter. 
 
ON THE MECHANICAL EQUIVALENT or HEAT 397 
 
 Water in A while running, 309-0 by No. 6163. 
 
 Calor. before 391-3; temperat. 314-5 by 6166. 
 
 Calor. after 3129-0; temperat. 308-3 by 6166, and 378-5 by 6163. 
 
 Air about 21 C. 
 
 Therefore, water lost 0-078, and calorimeter gained 5. Hence the 
 capacity of the calorimeter is 39. 
 
 Another experiment, more carefully made, in which the range was 
 greater, gave 35. 
 
 The close agreement of these with the estimated amount is, of 
 course, only accidental, for they depend upon an estimation of only 
 0-08 and 0-12 respectively. But they at least show that the water is 
 delivered into the calorimeter without much change of temperature. 
 
 A few experiments were made as follows between ordinary tempera- 
 tures and 100, seeing that this has already been determined by Reg- 
 nault. 
 
 Two thermometers were placed in the calorimeter, the temperature 
 of which was about 5 below that of the atmosphere. The vessel B 
 was then filled, and the water let into the calorimeter, by which the 
 temperature was nearly brought to that of the atmosphere; the opera- 
 tion was then immediately repeated, by which the temperature rose 
 about 5 above the atmosphere. The temperature of the boiling water 
 was given by a thermometer whose 100 was taken several times. 
 
 As only the rise of temperature is needed, the zero points of the 
 thermometers in the calorimeter are unnecessary, except to know that 
 they are within 0-02 of correct. 
 
 June 18 
 Temperature of boiling water, 99 -9. 
 
 Calor. before 2684-7; temperat. 259-2 by 6166, and 248-3 by 6165. 
 Calor. after 2993-2; temperat. 381-0 by 6166, and 363-4 by 6165. 
 
 259-3 = 18-568, or 18-555 when corrected for stem. 
 248- 3 = 18 -564, or 18 -551 when corrected for stem. 
 381-0 = 28-054, or 28-065 when corrected for stem. 
 363-4 = 28 -055, or 28 -066 when corrected for stem. 
 
 Specific heat 28 100 _ , . Of)24 
 Specific heat 18 - 28 ~ 
 
 Other experiments gave 1-0015 and 1-0060, the mean of all of which 
 
398 HENEY A. EOWLAXD 
 
 is 1-0033. Regnault's formula gives 1-005; but going directly to his 
 experiments, we get about 1-004, the other quantity being for 110. 
 
 The agreement is very satisfactory, though one would expect my 
 small apparatus to lose more of the heat of the boiling water than 
 Regnault's. Indeed, for high temperatures my apparatus is much 
 inferior to Regnault's, and so I have not attempted any further experi- 
 ments at high temperatures. 
 
 My only object was to confirm by this method the results deduced 
 from the experiments on the mechanical equivalent; and this I have 
 done, for the experiments nearly all show that the specific heat of water 
 decreases to about 30, after which it increases. But the mechanical 
 equivalent experiments give by far the most accurate solution of the 
 problem; and, indeed, give it with an accuracy hitherto unattempted in 
 experiments of this nature. 
 
 But whether water increases or decreases in specific heat from to 
 30 depends upon the determination of the reduction to the air ther- 
 mometer. According to the mercurial thermometers Nos. 6163, 6165 and 
 6166, treating them only as mercurial thermometers, the specific heat of 
 water up to 30 is nearly constant, ~bui by the air thermometer, or ~by the 
 Kew standard or Fastre, it decreases. 
 
 Full and complete tables of comparison are published, and from them 
 any one can satisfy himself of the facts in the case. 
 
 I am myself satisfied that I have obtained a very near approximation 
 to absolute temperatures, and accept them as the standard. And by 
 this standard the specific heat of water undoubtedly decreases from 
 to about 30. 
 
 To show that I have not arrived at this result rashly, I may mention 
 that I fought against a conclusion so much at variance with my precon- 
 ceived notions, but was forced at last to accept it, after studying it for 
 more than a year, and making frequent comparisons of thermometers, 
 and examinations of all other sources of error. 
 
 However remarkable this fact may be, being the first instance of the 
 decrease of the specific heat with rise of temperature, it is no more 
 remarkable than the contraction of water to 4. Indeed, in both cases 
 the water hardly seems to have recovered from freezing. The specific 
 heat of melting ice is infinite. Why is it necessary that the specific 
 heat should instantly fall, and then recover as the temperature rises? 
 Is it not more natural to suppose that it continues to fall even after the 
 ice is melted, and then to rise again as the specific heat approaches infin- 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 399 
 
 ity at the boiling point? And of all the bodies which we should select as 
 probably exhibiting this property, water is certainly the first. 
 
 (&.) Heat Capacity of Calorimeter 
 
 During the construction of the calorimeter, pieces of all the material 
 were saved in order to obtain the specific heat. The calorimeter which 
 Joule used was put together with screws, and with little or no solder. 
 But in my calorimeter it was necessary to use solder, as it was of a much 
 more complicated pattern. The total capacity of the solder used was 
 only about -$fa of the total capacity including the water; and if we 
 should neglect the whole, and call it copper, the error would be only 
 about y-gVfr- Hence it was considered sufficient to weigh the solder 
 before and after use, being careful to weigh the scraps. The error in 
 the weight of solder could not possibly have been as great as ten per 
 cent, which would affect the capacity only 1 part in 12,000. 
 
 To determine the nickel used in plating, the calorimeter was weighed 
 before and after plating; but it weighed less after than before, owing 
 to the polishing of the copper. But I estimated the amount from the 
 thickness of a loose portion of the plating. I thus found the approxi- 
 mate weight of nickel, but as it was so small, I counted it as copper. 
 The following are the constituents of the calorimeter: 
 
 Thick sheet copper 25-1 per cent. 
 
 Thin sheet copper 45-7 " 
 
 Cast brass 17-9 " 
 
 Boiled or drawn brass 5-7 " 
 
 Solder 4-0 
 
 Steel 1-6 " 
 
 100-0 
 Mckel -3 " 
 
 To determine the mean specific heat, the basket of a Regnault's 
 apparatus was filled with the scraps in the above proportion, allowing 
 the basket of brass gauze, which was very light, to count toward the 
 drawn brass. The specific heat was then determined between 20 and 
 100, and between about 10 and 40. Between 20 and 100 the 
 ordinary steam apparatus was used, but between 10 and 40 a special 
 apparatus filled with water was used, the water being around the tube 
 containing the basket, in the same manner as the steam is in the 
 
400 HENRY A. EOWLAND 
 
 original apparatus. In the calorimeter a stirrer was used, so that the 
 basket and water should rapidly attain the same temperature. The water 
 was weighed before and after the experiment, to allow for evaporation. 
 A correction of about 1 part in 1000 was made, on account of the heat 
 lost by the basket in passing from the apparatus to the calorimeter, in 
 the 100 series, but no correction was made in the other series. The 
 thermometers in the calorimeter were Nos. 6163 and 6166 in the dif- 
 ferent experiments. 
 
 The principal difficulty in the determination is in the correction for 
 radiation, and for the heat which still remains in the basket after some 
 time. After the basket has descended into the water, it commences to 
 give out heat to the water; this, in turn, radiates heat; and the tempera- 
 ture we measure is dependent upon both these quantities. 
 
 Let T = temperature of the basket at the time t 
 
 i( IT" _ (I (( 
 
 JW <- 
 
 " " " water t 
 
 Ql __ Q 
 
 (I Q'l __ ( (( (( QO 
 
 6" = T". 
 We may then put approximately 
 
 TT" = (T - T")e-~z, 
 where c is a constant. But 
 
 rpl rpn rpi rp 
 
 0" 0' ' ' Q tf ' 
 
 hence 
 
 To find c we have 
 
 1 0" 0' 
 
 t 3 ff' 
 
 where 6" can be estimated sufficiently accurately to find C" approxi- 
 mately. 
 
 These formulae apply when there is no radiation. When radiation 
 takes place, we may write, therefore, when t is not too small, 
 
 00' = (0" #')(! - e-~T) 
 
 where is a coefficient of radiation, and t is a quantity which must be 
 subtracted from t, as the temperature of the calorimeter does not rise 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 401 
 
 instantaneously. To estimate t , T a being the temperature of the air, 
 we have, according to Newton's law of cooling, 
 
 t 
 
 C(t- Q = _ T C(0 T a } dt nearly, 
 
 ~ a / 
 
 0" 0' 
 t = c tf , _ T nearly, 
 
 ri 
 
 where it is to be noted that -,, _ is nearly a constant for all values of 
 
 " *- a 
 
 0" T a according to Newton's law of cooling. 
 
 The temperature reaches a maximum nearly at the time 
 
 0"o' t 
 
 and if 6 m is the maximum temperature, we have the value of 0" as 
 follows : 
 
 0" = T" = 0^ + C(t m + cL): 
 
 \. m ' v/ 7 
 
 and this is the final temperature provided there was no loss of heat. 
 
 When the final temperature of the water is nearly equal to that of 
 the air, C will be small, but the time i m of reaching the maximum 
 will be great. If a is a constant, we can put C = a (6" T a ), and 
 G(t n + c ) will be a minimum, when 
 
 or a = - 
 
 ac 
 
 That is, the temperature of the air must be lower than the tempera- 
 ture of the water, so that T a = 6" as nearly as possible ; but the for- 
 mula shows that this method makes the corrections greater than if we 
 make T a = d', the reason being that the maximum temperature is not 
 reached until after an infinite time. It will in practice, however, be 
 found best to make the temperature of the water at the beginning 
 about that of the air. It is by far the best and easiest method to 
 make all the corrections graphically, and I have constructed the follow- 
 ing graphical method from the formula?. 
 
 First make a series of measurements of the temperature of the water 
 of the calorimeter, before and after the basket is dipped, together with 
 the times. Then plot them on a piece of paper as in Fig. 5, making 
 the scale sufficiently large to insure accuracy. Five or ten centimeters 
 to a degree are sufficient. 
 
 nab c d is the plot of the temperature of the water of the calori- 
 26 
 
402 
 
 HENRY A. EOWLAND 
 
 meter, the time being indicated by the horizontal line. Continue the 
 line d c until it meets the line I a. Draw a horizontal line through 
 the point I. At any point, &, of the curve, draw a tangent and also a 
 vertical line bg; the distance eg will be nearly the value of the con- 
 stant c in the formula?. Lay off I f equal to c, and draw the line fJiTc 
 through the point h, which indicates the temperature of the atmos- 
 phere or of the vessel surrounding the calorimeter. Draw a vertical 
 line, j Ic, through the point Tc. From the point of maximum, c, draw 
 a line, j c, parallel to d m, and where it meets Ic j will be the required 
 point, and will give the value of 6". Hence, the rise of temperature, 
 corrected for all errors, will be Ic j. 
 
 This method, of course, only applies to cases where the final tem- 
 perature of the calorimeter is greater than that of the air; otherwise 
 there will be no maximum. 
 
 FIG. 5. 
 
 In practice, the line d m is not straight, but becomes more and more 
 nearly parallel to the base line. This is partly due to the constant 
 decrease of the difference of temperature between the calorimeter and 
 the air, but is too great for that to account for it. I have traced it to 
 the thin metal jacket surrounding the calorimeter, and I must condemn, 
 in 'the strongest possible manner, all such arrangements of calorimeters 
 as have such a thin metal jacket around them. The jacket is of an 
 uncertain temperature, between that of the calorimeter and the air. 
 When the calorimeter changes in temperature, the jacket follows it but 
 only after some time; hence, the heat lost in radiation is uncertain. 
 The true method is to have a water jacket of constant temperature, and 
 then the rate of decrease of temperature will be nearly constant for a 
 long time. 
 
 The following results have been obtained by Mr. Jacques, Fellow of 
 the University, though the first was obtained by myself. Corrections 
 were, of course, made for the amount of thermometer stem in the air. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 403 
 
 Temperature. Mean Specific Heat. 
 
 24 to 100 -0915 
 
 26 to 100 -0915 
 
 25 to 100 -0896 
 
 13 to 39 -0895 
 
 14 to 38 -0885 
 
 9 to 41 -0910 
 
 To reduce these to the mean temperature of to 40, I have used 
 the rate of increase found by Bede for copper. They then become, for 
 the mean from to 40, 
 
 0897 
 0897 
 0878 
 0893 
 0883 
 0906 
 
 Mean -0892 -00027 
 
 As the capacity of the calorimeter is about four per cent of that of 
 the total capacity, including the water, this probable error is about -g-oW 
 of the total capacity, and may thus be considered as satisfactory. 
 
 I have also computed the mean specific heat as follows, from other 
 observers : 
 
 Copper between 20 and 100 nearly. 
 
 0949 Dulong. 
 
 0935 Eegnault. 
 
 0952 Eegnault. 
 
 0933 Bede. 
 
 0930 Kopp. 
 
 0940 
 
 This reduced to between and 40 by Bede's formula gives -0922. 
 Hence we have the following for the calorimeter: 2 * 
 
 24 The cast brass was composed of 28 parts of copper, 2 of tin, 1 of zinc, and 1 of 
 lead. The rolled brass was assumed to have the same composition. The solder was 
 assumed to be made of equal parts of tin and lead. 
 
404 HEXRY A. ROWLAND 
 
 Per cent. Specific Heat between and 40 C. 
 
 Copper 91-4 -0922 
 
 Zinc -7 -0896 
 
 Tin 3-6 -0550 
 
 Lead 2-7 -0310 
 
 Steel 1-6 -1110 
 
 Mean -0895 
 
 The close agreement of this number with the experimental result 
 can only be accidental, as the reduction to the air thermometer would 
 decrease it somewhat, and so make it even lower than mine. However, 
 the difference could not at most amount to more than 0-5 per cent, 
 which is very satisfactory. 
 
 The total capacity of the calorimeter is reckoned as follows : 
 
 Weight of calorimeter 3-8712 kilogrammes. 
 
 Weight of screws . . . . -0016 kilogrammes. 
 
 Weight of part of suspending wires. . -0052 kilogrammes. 
 Total weight 3-8780 kilogrammes. 
 
 Capacity = 3-878 X '0892 = -3459 kilogrammes. 
 
 To this must be added the capacity of the thermometer bulb and 
 several inches of the stem, and of a tube used as a safety valve, and we 
 must subtract the capacity of a part of the shaft which was joined to 
 -the shaft turning the paddles. Hence, 
 
 3459 
 -f- -0011 
 4- -0010 
 0010 
 
 Capacity =-3470 
 
 As this is only about four per cent of the total capacity, it is not 
 necessary to consider the variation of this quantity with the tempera- 
 ture through the range from to 40 which I have used. 
 
 IV. DETERMINATION OF EQUIVALENT 
 (o.) Historical Remarks 
 
 The history of the determination of the mechanical equivalent of heat 
 is that of thermodynamics, and as such it is impossible to give it at 
 length here. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 405 
 
 I shall simply refer to the few experiments which a priori seem to 
 possess the greatest value, and which have been made rather for the 
 determination of the quantity than for the illustration of a method, 
 and shall criticise them to the best of my ability, to find, if possible, the 
 cause of the great discrepancies. 
 
 1. GENERAL REVIEW OF METHODS 
 
 Whenever heat and mechanical energy are converted the one into 
 the other, we are able by measuring the amounts of each to obtain the 
 ratio. Every equation of thermodynamics proper is an equation 
 between mechanical energy and heat, and so should be able to give us 
 the mechanical equivalent. Besides this, we are able to measure a 
 certain amount of electrical energy in both mechanical and heat units, 
 and thus to also get the ratio. Chemical energy can be measured in 
 heat units, and can also be made to produce an electric current of known 
 mechanical energy. Indeed, we may sum up as follows the different 
 kinds of energy whose conversion into one another may furnish us with 
 the mechanical equivalent of heat.' And the problem in general would 
 be the ratio by which each kind of energy may be converted into each of 
 the others, or into mechanical or absolute units. 
 
 a. Mechanical energy. 
 
 6. Heat. 
 
 c. Electrical energy. 
 
 d. Magnetic energy. 
 
 e. Gravitation energy. 
 
 f. Radiant energy. 
 
 g. Chemical energy. 
 h. Capillary energy. 
 
 Of these different kinds of energy, only the first five can be measured 
 other than by their conversion into other forms of energy, although Sir 
 William Thomson, by the introduction of such terms as " cubic mile of 
 sunlight," has made some progress in the case of radiation. Hence for 
 these five only can the ratio be known. 
 
 Mechanical energy is measured by the force multiplied by the dis- 
 tance through which the force acts, and also by the mass of a body multi- 
 plied by half the square of its velocity. Heat is usually referred to the 
 quantity required to raise a certain amount of water so many degrees, 
 though hitherto the temperature of the water and the reduction to the 
 air thermometer have been almost neglected. 
 
406 HENRY A. ROWLAND 
 
 The energy of electricity at rest is the quantity multiplied by half the 
 potential ; or of a current, it is the strength of current multiplied by the 
 electro-motive force, and by the time ; or for all attractive forces varying 
 inversely as the square of the distance, Sir William Thomson has given 
 the expression 
 
 TF/**' 
 
 where R is the resultant force at any point in space, and the integral is 
 taken throughout space. 
 
 These last three kinds of energy are already measured in absolute 
 measure and hence their ratios are accurately known. The only ratio, 
 then, that remains is that of heat to one of the others, and this must be 
 determined by experiment alone. 
 
 But although we cannot measure f, g, h in general, yet we can often 
 measure off equal amounts of energy of these kinds. Thus, although we 
 cannot predict what quantities of heat are produced when two atoms of 
 different substances unite, yet, when the same quantities of the same 
 . substances unite to produce the same compound, we are safe in assuming 
 that the same quantity of chemical energy comes into play. 
 
 According to these principles, I have divided the methods into direct 
 and indirect. 
 
 Direct methods are those where & is converted directly or indirectly 
 into a, c, d, or e, or vice versa. 
 
 Indirect methods are those where some kind of energy, as g, is con- 
 verted into &, and also into a, c, d, or e. 
 
 In this classification I have made the arrangement with respect to 
 the kinds of energy which are measured, and not to the intermediate 
 steps. Thus Joule's method with the magneto-electric machine would 
 be classed as mechanical energy into heat, although it is first converted 
 into electrical energy. The table does not pretend to be complete, but 
 gives, as it were, a bird's-eye view of the subject. It could be extended 
 by including more complicated transformations; and, indeed, the sym- 
 metrical form in which it is placed suggests many other transformations. 
 As it stands, however, it includes all methods so far used, besides many 
 more. 
 
 In the table of indirect methods, the kind of energy mentioned first is 
 to be eliminated from the result by measuring it both in terms of heat 
 and one of the other kindsof energy, whose value is known in absolute 
 or mechanical units. 
 
ON THE MECHANICAL EQUIVALENT or HEAT 
 
 407 
 
 It is to be noted that, although it is theoretically possible to measure 
 magnetic energy in absolute units, yet it cannot be done practically with 
 any great accuracy, and is thus useless in the determination of the 
 equivalent. It could be thus left out from the direct methods without 
 harm, as also out of the next to last term in the indirect methods. 
 
 TABLE XXV. SYNOPSIS OF METHODS FOR OBTAINING THE 
 MECHANICAL EQUIVALENT OF HBAT. 
 
 j Mechanical Energy 
 J. Gravltatlon 
 
 4 ft. Heat, Electric Energy . 
 
 y. Heat, Magnetic Energy 
 
 1. Reversible process 
 
 I 2. Irreversible 
 cess 
 
 pro- 
 
 l. Reversible process 
 
 2. Irreversible 
 cess 
 
 pro- 
 
 f a. Expansion or compression ac- 
 cording to adlabatlc curve. 
 6. Expansion or compression ac- 
 cording to Isothermal curve. 
 
 c. Expansion or compression ac- 
 
 cording to any curve with re- 
 generator. 
 
 d. Electro-magnetic engine driven 
 
 by thermo-electric pile In a 
 circuit of no resistance. 
 
 a. Friction, percussion, etc. 
 
 6. Heat from magneto-electric cur- 
 rents, or electric machine. 
 
 a. Thermo-electric currents. 
 
 ft. Pyro-electric phenomena (prob- 
 ably). 
 
 a. Heating of wire by current, or 
 heat produced by discharge 
 of electric battery. 
 
 ( a. Thermo-electric current mag- 
 
 1. Reversible process '. netizlng a magnet in a circuit 
 
 of no resistance. 
 
 2. Irreversible pro- ( a. Heating of magnet when de- 
 
 cess I magnetized. 
 
 a. Radiant Energy, Heat 
 
 (Radiant energy absorbed 
 by blackened eurface.) 
 
 0. Chemical Energy, Heat 
 
 (Combustion, etc.) 
 
 y. Capillary energy, Heat 
 
 (Heat produced when a liq- 
 uid Is absorbed by a po- 
 rous solid.) 
 
 S. Electrical energy, Heat 
 
 (Heat generated in a wire 
 by an electrical current.) 
 
 e. Magnetic Energy, Heat 
 
 (Heat generated on demag- 
 netizing a magnet.) 
 
 Gravitation Energy, Heat 
 (Heat generated by a tail- 
 ing body.) 
 
 Crooke's radiometer. 
 Thermo-electric pile. 
 Thermo-electric pile with electro- 
 magnet In circuit. 
 
 1. Cannon. 
 
 2. Electro-magnet machine run by 
 
 galv. battery. 
 Current from battery. 
 Electro-magnet magnetized by a 
 
 battery current. 
 
 a. Mechanical Energy. 
 
 5. Electrical " 
 
 c. Magnetic " 
 
 d. Gravitation " 
 
 a. Mechanical Energy 
 
 6. Electrical " 
 
 c. Magnetic " ? 
 
 d. Gravitation " 
 
 a. Mechanical Energy. Movement of liquid by capillarity. 
 . _. j Electrical currents from capillary 
 
 " *' { action at surface of mercury. 
 
 c. Magnetic " 
 
 d. Gravitation " Raising of liquid by capillarity. 
 
 agneto-electric or electro-mag- 
 netic machine. Electric at- 
 traction. 
 Electro-magnet. 
 
 a. Mechanical Energy 
 
 6. Magnetic " 
 c. Gravitation " 
 
 j M 
 
 a. Mechanical Energy 
 
 6. Electrical 
 c. Gravitation 
 
 Armature attracted by a perma- 
 nent Magnet. 
 
 Induced current on demagnetizing 
 a magnet. 
 
 a. Mechanical Energy. J Velocity Imparted to a falling 
 6. Electrical " I body. 
 
 c. Magnetic 
 
408 
 
 HENRY A. ROWLAND 
 
 TABLE XXVI. HISTORICAL TABLE OF EXPERIMENTAL RESULTS. 
 
 Method 
 in 
 General. 
 
 Method in Particular. 
 
 Observer. 
 
 Date. 
 
 Result. 
 
 A 
 A 
 
 A 
 A 
 
 /: 
 S 
 
 a 
 a 
 
 a 
 
 ft 
 
 ;-' 
 ft 
 
 1 
 
 2 
 
 9 
 
 '3 
 
 n 
 b 
 
 a 
 
 b 
 
 or 
 c 
 
 a 
 
 b 
 a 
 
 2 
 1 
 
 Compression of air 
 
 Joule" 
 Joule" 
 
 1845 443-8 
 1845 437-8 
 
 Expansion " 
 
 Theory of gases (see below) . 
 
 " vapors (see below) 
 
 
 
 Experiments on steam-engine 
 
 Hirn v " 
 Hirn v " 
 
 Edlund* 1 " 
 
 Rumford ix 
 Joule 1 " 
 Joule lv 
 Joule v 
 Joule vi 
 Joule vl 
 Joule vi 
 Him 1 
 Favre lx 
 Him 1 " 1 
 Him'' 11 
 Hirn T 
 Him* 11 
 Hirn T " 
 Puluj* 1 " 
 Joule 
 
 Joule" 1 
 
 Vioile* 
 
 Quintus 
 Icilius* 1 
 also Weber 
 Lenz, also 
 Weber 
 Joule* 1 " 
 H. F. Weber* 1 ' 
 
 Joule" 1 
 Favre IV 
 
 Weber, 
 Boscha, 
 Favre, and 
 Silbermann 
 
 Joule 
 Boscha* 11 
 
 1857 
 1860-1 
 
 1865 J 
 
 1798 
 1843 
 1845 
 1847 
 1850 
 1850 
 1850 
 1857 
 1858 
 1858 
 1858 
 1860-1 
 1860-1 
 1860-1 
 1876' 
 1878 
 
 1843 
 1870 J 
 
 (.1857 
 
 J1859J 
 
 1867 
 
 1878 
 
 1843 
 
 1858 
 
 Il857 
 J1859 
 
 413-0 
 420-432 
 443-6 
 430-1 
 428-3 
 940ft.lbs. 
 424-6 
 488-3 
 428-9 
 423-9 
 424-7 
 425-2 
 371-6 
 413-2 
 400-450 
 425-0 
 432-0 
 432-0 
 425-0 
 426-6 
 423-9 
 
 460-0 
 435.2 
 434-9 
 435-8 
 437 '4 
 
 399-7 
 
 396-4 
 478-2 
 429-5 
 428-15 
 
 499-0 
 443-0 
 
 432-1 
 419-5 
 
 ti ti 11 
 
 Expansion and contraction of metals. . . 
 Boring of cannon 
 
 Friction of water in tubes 
 
 " ' in calorimeter 
 
 <* " in calorimeter 
 
 " " in calorimeter 
 
 Friction of mercury in calorimeter 
 
 " plates of iron 
 
 metals 
 
 " metals in mercury calor. . . . 
 " metals. . . 
 
 Boring of metals . 
 
 Water in balance afrottement 
 
 Flow of liquids under strong pressure. . 
 Crushing of lead 
 
 
 Water in calorimeter 
 
 Heating by magneto-electric currents. . . 
 
 Heat generated in a disc between the ) 
 poles of a magnet f 
 
 Heat developed in wire of known ab- \ 
 solute resistance ") 
 
 Do. do. do. 
 
 Do. do. do. 
 Do. do. do. 
 
 Diminishing of the heat produced in a 1 
 battery circuit when the current V 
 produces work ) 
 
 Do. do. do. 
 
 Heat due to electrical current, electro- "| 
 chemical equivalent of water = 
 009379, absolute resistance electro- i 
 motive force of Daniell cell, heat [ 
 developed by action of zinc on sul. | 
 of copper J 
 
 Heat developed in Daniell cell 
 
 Electro-motive force of Daniell cell. . . . 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 
 
 409 
 
 2. KESULTS OF BEST DETERMINATIONS ' 
 
 On the basis of this table of methods I have arranged the following 
 table, showing the principal results so far obtained. 
 
 In giving the indirect results, many persons have only measured one 
 of the transformations required; and as it would lengthen out the table 
 very much to give the complete calculation of the equivalent from these 
 selected two by two, I have sometimes given tables of these parts. As 
 the labor of looking up and reducing these is very great, it is very 
 possible that there have been some omissions. 
 
 I have taken the table published by the Physical Society of Berlin, 1 as 
 the basis down to 1857, though many changes have been made even 
 within this limit. 
 
 I shall now take up some of the principal methods, and discuss them 
 somewhat in detail. 
 
 Method from Theory of Gases 
 
 As the different constants used in this method have bf en obtained by 
 many observers, I first shall give their results. 
 
 TABLE XXVII. SPECIFIC HEAT OF GASES. 
 
 
 Limit to 
 Temperature. 
 
 Approximate 
 Temperature 
 of Water. 
 
 Temperature 
 reduced to 
 
 Specific Heat. 
 
 
 Air 
 
 
 , 
 
 Mercurial 
 
 i -2669 I 
 
 Delaroche and 
 
 
 20 to 210 
 
 -iZ { 
 
 Thermometer 
 
 Air 
 Thermometer 
 
 y ( 
 
 i 23751"' 
 
 Berard. 
 Regnault. 
 
 
 20 to 100 
 
 20 j 
 
 Mercurial 
 Thermometer 
 
 j -2389"" 
 
 E.Wiedemann. 
 
 Hydrogen.. . 
 
 
 . .j 
 
 Mercurial 
 
 \3-2936 -( 
 
 Delaroche and 
 
 
 15 to 200 
 
 1 
 
 12-2 | 
 
 Thermometer 
 
 Air 
 Thermometer 
 
 / t 
 1 3 -4090" 1 
 
 Berard. 
 Regnault. 
 
 
 21 to 100 
 
 21 | 
 
 Mercurial 
 Thermometer 
 
 13-410"" 
 
 E.Wiedemann. 
 
 25 Taking mean results on page 101 of Rel. des Exp., torn, ii., 
 
410 HENRY A. KOWLAND 
 
 TABLE XXVIII. COEFFICIENT OF EXPANSION OF AlR UNDER CONSTANT VOLUME 
 
 
 Taking Expansion of Mercury 
 according- to Regnault. 
 
 Taking Expansion of Mercury 
 according to Wiillner's Re- 
 calculation of Regnault's 
 Experiments. 
 
 Regnault 
 
 0036655 
 
 0036687 
 
 Magnus 
 
 0036678 
 
 0036710 
 
 Jolly 
 
 0036695 
 
 0036727 
 
 Rowland 
 
 0036675 
 
 0036707 
 
 
 
 
 Mean 
 
 0036676 
 
 0036708 
 
 
 
 
 TABLE XXIX. RATIO OF SPECIFIC HEATS OF AIR. 
 
 Method. 
 
 Observer. 
 
 Date. 
 
 Ratio 
 of Specific 
 Heats. 
 
 Method of Clement & Desormes, ) 
 globe 20 litres I 
 
 Clement & | 
 Desormes""' J 
 
 1812 
 Published in 
 
 t 1-354 
 
 Never fully published 
 
 Gay-Lussac et Welter 1 ' 1 . 
 
 1819 
 
 1-3748 
 
 Method of C16ment & Desormes. . 
 Using Breguet thermometer 
 
 Delaroche et Berard* 11 . . 
 Favre & Silbermann""'. 
 
 1853 
 
 1-249 
 1-421 
 
 Clement & Desormes, globe 39 ) 
 
 Masson" 
 
 1858 
 
 1-4196 
 
 Clement & Desormes 
 
 Weisbach" 1 . . . . '. 
 
 1859 
 
 1 4025 
 
 C16ment & Desormes, globe 10 ) 
 
 Hirn xxli 
 
 1861 
 
 1-3845 
 
 litres ) 
 
 
 
 
 Passage of gas from one vessel ) 
 
 Cazin" lv 
 
 1862 
 
 1-41 
 
 into another, globes 60 litres j 
 Pressure in globe changed by ) 
 
 
 1863 
 
 
 aspirator, globe 25 litres. . . . ) 
 Heating of gas by electric cur- ) 
 
 Jamin & Richard 1 "" 1 . . . 
 
 1864 
 
 1-41 
 
 Clement & D6sormes 
 
 Tresca et Laboulaye"' 1 . 
 
 1864 
 
 
 Barometer under air-pump re- ) 
 
 Kohlrausch 1 "' 
 
 1869 
 
 1-302 
 
 ceiver of 6 litres ) 
 
 
 
 
 Compression and expansion of ) 
 
 Regnault 
 
 1871 J 
 
 Results lost 
 in the siege 
 
 C16ment&D6sormes with metal- ) 
 
 R6ntgen" v " 
 
 I 
 
 1873 
 
 of Paris. 
 1-4053 
 
 lie manometer, globe 70 litres ) 
 Compression of gas by piston. 
 
 Amagat XXI 
 
 1874 
 
 1-397 
 
 
 
 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 411 
 
 fgsi 
 
 so 
 
 t- 
 
 SO 
 
 ^ 
 
 CO 
 
 H9 
 
 
 
 o 
 
 00 
 
 
 
 "3 Q." ''"'S 
 
 CM 
 
 CM 
 
 CM 
 
 nr> 
 
 o 
 
 CM 
 
 
 
 CM 
 
 ^^ 
 
 
 . 
 
 ^ o + S 
 
 CO 
 
 CO 
 
 CO 
 
 CM 
 
 CO 
 
 CO 
 
 
 
 CO 
 
 CO 
 
 
 
 
 
 8*6=1 
 
 CO 
 
 CO 
 
 CO 
 
 ts 
 
 CO 
 
 CO 
 
 ' 
 
 
 CO 
 
 CO 
 
 
 
 ii-OflJS 
 
 
 ; 
 
 
 
 ; 
 
 
 00 
 
 s 
 
 
 
 t- 
 
 co 
 
 rH 
 t- 
 
 -** 0*^ 
 
 
 
 . 
 
 
 
 
 CM 
 
 CO 
 
 rH 
 CO 
 
 
 
 CM 
 
 O 
 
 ^ M ^ O A 
 
 -*S Q 
 
 
 
 
 
 
 
 
 H 
 
 S 
 
 CO 
 
 
 
 
 CO 
 
 OO 
 
 scaSri 
 
 O o ts-S~" 
 
 s 
 
 O5 
 
 S 
 
 t- 
 
 s 
 
 o 
 
 3 
 S 
 
 s 
 
 so 
 
 CO 
 
 s 
 
 CO 
 35 
 
 
 
 o 
 
 0* 
 
 CM 
 
 rH 
 
 
 
 CO 
 
 CO 
 
 eo 
 
 CO 
 
 CO 
 CO 
 CO 
 
 35 
 M 
 M 
 
 53 
 CO 
 
 04 
 
 CO 
 CO 
 
 rg 
 
 CO 
 
 CM 
 
 CO 
 CO 
 
 CO 
 CO 
 
 CO 
 CO 
 
 CO 
 CO 
 CO 
 
 
 
 * 
 
 
 1 
 
 <* 
 
 ? 
 
 
 
 
 
 s 
 
 s 
 
 
 
 Md 
 
 H - 
 
 
 . 
 
 . 
 
 S 
 
 
 
 
 
 
 
 
 o 
 "3 t 
 
 CO 
 
 >A 
 
 
 <H 
 CM 
 
 VH 
 
 35 
 CO 
 
 
 CO 
 
 CM 
 
 
 1A 
 
 o 
 
 
 
 CM 
 
 
 35 
 
 jj 
 
 
 
 
 
 
 35 
 
 
 CO 
 
 cc 
 
 
 K r^ 
 
 t- 
 
 
 
 CO 
 
 
 
 
 CO 
 
 
 
 CO 
 
 TO 
 
 
 
 o 
 
 
 
 l-H 
 
 i-l 
 
 
 CO 
 
 
 CO 
 
 CO 
 
 
 CO 
 
 CO 
 
 
 
 
 
 
 
 
 
 
 
 fa 
 
 
 
 
 Id 
 
 1! 
 
 d 
 
 
 
 I- 
 
 
 fa 
 
 
 
 O5 
 
 fa 
 
 35 
 
 d 
 
 O5 
 
 d 
 
 d 
 
 d 
 
 
 
 o 
 
 to + 38 
 
 d 
 
 o 
 
 35 
 
 O 
 
 d 
 
 l- 
 
 rH 
 
 d 
 
 
 
 o 
 
 !l 
 
 o 
 
 o 
 
 
 O 
 
 CO 
 
 CO 
 
 O 
 
 o 
 
 o 
 
 35 
 
 
 rH 
 
 
 
 fa 
 o 
 
 oo 
 
 IA 
 O 
 
 O 
 00 
 
 o 
 
 o 
 CM 
 
 
 
 
 
 
 
 
 
 
 1 
 
 
 
 
 Iss 
 
 
 o 
 
 o 
 
 O 
 
 
 
 CO 
 
 "5 
 
 OQ 
 
 "o 
 
 rH 
 
 
 
 35 
 
 " 
 
 
 
 st 
 
 t- 
 
 CO 
 
 00 
 
 OQ 
 
 OQ 
 
 
 
 CO 
 
 rH 
 
 *.%> 
 
 
 
 
 
 
 
 CM 
 
 rH 
 
 
 
 
 
 
 
 
 VI 
 
 
 
 
 
 
 
 a 
 
 
 
 
 
 
 o 
 
 
 
 
 
 
 
 fe 
 
 
 
 
 
 
 
 13 
 
 
 
 
 
 ^3 
 
 a 
 
 o 
 
 
 
 
 i 
 
 France 
 
 Dussel 
 
 -3 
 a 
 i i 
 
 3 
 s 
 
 1 1 
 
 France 
 
 Austri 
 
 Hollan 
 
 Hollan 
 
 OQ 
 o 
 
 PH 
 
 
 OQ 
 
 France 
 
 s 
 
 00 
 CO 
 
 -i 
 
 CM 
 
 rH 
 
 c 
 
 
 
 CM 
 
 ct 
 
 CO 
 
 1A 
 
 4 
 
 CO 
 
 3 
 
 SO 
 
 
 l> 
 
 00 
 
 CO 
 
 CO 
 
 CO 
 
 CO 
 
 H 
 
 CO 
 
 o* 
 
 CO 
 
 00 
 
 CO 
 
 
 
 
 
 
 
 
 
 
 r- 
 
 
 
 ""I 
 
 
 
 
 
 
 
 
 r 
 
 
 
 
 '. 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 S 
 
 ,0 
 
 *> 
 
 
 
 . 
 
 H 
 M 
 
 
 
 M 
 
 
 
 
 a 
 
 L* 
 
 P 
 
 
 
 
 M 
 
 
 
 M 
 
 
 
 
 
 
 
 
 
 
 
 
 h 
 
 a 
 
 _, 
 
 5 
 
 
 a 
 
 a 
 
 a 
 
 o 
 so 
 
 
 M 
 M 
 hi 
 
 '. 
 
 J3 
 2 
 
 
 S 
 
 
 H 
 
 M 
 
 
 o 
 
 
 
 =5 
 
 
 fl? 
 
 
 oS 
 
 
 o 
 
 I 
 
 o 
 
 X 
 
 S? 
 
 I 
 
 
 VI 
 
 
 
 
 a 
 
 oS 
 
 " 
 
 OQ 
 
 O 
 
 fa 
 
 
 
 H 
 
 
 o 
 
 ,0 
 
 fl 
 
 S9 
 
 bo 
 
 a 
 
 = 
 
 3 
 
 "P, 
 
 4 
 
 
 "3 
 
 
 
 09 
 | 
 
 oJ 
 
 
 a 
 o 
 G 
 
 a 
 o 
 
 "o 
 
 
 V 
 
 b 
 
 i 
 
 "3 
 
 z 
 
 b 
 
 eS 
 
 C8 
 
 2 
 
 & 
 
 
 
 PQ 
 
 
 
 
 PQ 
 
 OQ 
 
 * 
 
 
 PH 
 
 OQ 
 
 PQ 
 
 
 
 i 
 
 i i 
 
 - 
 
 ^T 
 
 CO 
 
 -^ - 
 
 
 
 
 
 
 
 -1* 
 
 SO 
 
 t- 
 
 00 
 
 35 
 
 O 
 rH 
 
 w 
 
 - 6 
 
 
 
412 HENRY A. KOWLAND 
 
 References. (Tables XXVI to XXX.) 
 
 j Physical Society of Berlin, Fort, tier Phys., 1858. 
 " Joule, Phil. Mag., ser. 3, TO!, xxvi. See also Mec. Warmeaquivalent, 
 
 Gesammelte Abhandlungen von J. P. Joule, Braunschweig, 1872. 
 111 Joule, Phil. Mag., ser. 3, vol. xxiii. See also 2 above. 
 iv <i u u u xxvi. . " " 
 
 v u u u u u xxvii. " " 
 
 i u u u X xxi. " " 
 
 vii Hirn, Theorie Mec. de la Chaleur, ser. 1, 3 me ed. 
 Tiii Edlund, Pogg. Ann., cxiv. I, 1865. 
 
 ix Favre, Comptes Rend., Feb. 15, 1858; also Phil. Mag., xv. 406. 
 x Violle, Ann. de Chim., ser. 4, xxii. 64. 
 xi Quintus Icilius, Pogg. Ann., ci. 69. 
 xli Boscha, Pogg. Ann., cviii. 162. 
 xiii Joule, Report of the Committee on Electrical Standards of the B. A., London, 
 
 1873, p. 175. 
 
 xiv H. F. Weber, Phil. Mag., ser. 5, v. 30. 
 xv Favre, Comptes Rend., xlvii. 599. 
 XTi Regnault, Rel. des Experiences, torn. ii. 
 xvil E. Wiedemann, Pogg. Ann., clvii. 1. 
 
 xvl11 Clement et Desormes, Journal de Physique, Ixxxix. 333, 1819. 
 xlx Laplace, Mec. Celeste, v. 125. 
 
 xx Masson, Ann. de Chim. et de Phys., ser. 3, torn. liii. 
 xxi Weisbach, Der Civilingenieur, Neue Folge, Bd. v., 1859. 
 xxii Hirn, Theorie Mec. de la Chaleur, i, 111. 
 xxiii Favre et Silbermann, Ann. de Chim., ser. 3, xxxvii. 1851. 
 xxiv Cazin, Ann. de Chim., ser. 3, torn. Ixvi. 
 xxv Dupr6, Ann. de Chim., 3 me ser., Ixvii. 359, 1863. 
 xxvi Kohlrausch, Pogg. Ann., cxxxvi. 618. 
 xsvii Rontgen, Pogg. Ann., cxlviii. 603. 
 xxvlil Jamin et Richard, Comptes Rend., Ixxi. 336. 
 xxix Tresca et Laboulaye, Comptes Rend., Iviii. 358. Ann. du Conserv. des Arts 
 
 et Metiers, vi. 365. 
 
 xxx Amagat, Comptes Rend., Ixxvii. 1325. 
 xxxi Mem. de 1'Acad. des Sci., 1738, p. 128. 
 xxxii Benzenberg, Gilbert's Annalen, xlii. 1. 
 xxxm Goldingham, Phil. Trans., 1823, p. 96. 
 
 xxxiv Ann. de Chim., 1822, xx. 210 also, (Euvres de Arago, Mem. Sci., ii. 1. 
 xxxv Stampfer und Von Myrbach, Pogg. Ann., v. 496. 
 xxxvi Moll and Van Beek, Phil. Trans., 1824, p. 424. See also Shroder van der Kolk, 
 
 Phil. Mag., 1865. 
 xxxvii p arr y an( j Foster, Journal of the Third Voyage, 1824-5, Appendix, p. 86. Phil. 
 
 Trans., 1828, p. 97. 
 
 xxxviii Savart, Ann. de Chim.; ser. 2, Ixxi. 20. Recalculated. 
 XMIX Bravais et Martins, Ann. de Chim., ser. 3, xiii. 5. 
 11 Regnault, Rel. des Exp., iii. 533. 
 
 xli Delaroche et Berard, Ann. de Chim., Ixxxv. 72 and 113. 
 xl " Puluj, Pogg. Ann., clvii. 656. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 413 
 
 Estimating the weight rather arbitrarily, I have combined them as 
 follows : 
 
 No. 
 
 1 
 2 
 3 
 
 4 
 5 
 6 
 7 
 8 
 9 
 10 
 
 Velocity at 0- C. 
 Dry Air. 
 
 Estimated Weight 
 of Observation. 
 
 332-6 
 
 2 
 
 332-7 
 
 2 
 
 330-9 
 
 2 
 
 330-8 
 
 4 
 
 332-5 
 
 3 
 
 332-8 
 
 7 
 
 .332-0 
 
 1 
 
 331-8 
 
 1 
 
 332-4 
 
 4 
 
 330-7 
 
 10 
 
 Mean 331-75 
 
 Or, corrected for the normal carbonic acid in the atmosphere, it be- 
 comes 331-78 metres per second in dry pure air at C. 
 
 From Eegnault's experiments on the velocity in pipes I find by 
 graphical means 331-4 m. in free air, which is very similar to the above. 
 
 Calculation from Properties of Gases 
 
 K= specific heat of gas at constant pressure. 
 lc = specific heat of gas at constant volume. 
 p = pressure in absolute units of a unit of mass. 
 v = volume in absolute units of a unit of mass. 
 H = absolute temperature. 
 J= Joule's equivalent in absolute measure. 
 = K 
 
 General formula for all bodies: 
 
 _ 1 
 
 ~~ l _j^_(dp_\ (dv_\ ' 
 
 V 1 I dv \ 
 
 r = -7-i-r-i 
 
 T _ /* ( dp \ / dv \ f 
 *' 7? \7fc).\dJ ) F^T' 
 
414 HENEY A. ROWLAND 
 
 Also, 
 
 J= ~ ~^(!*L\ ~^L' 
 \ dp ),,, V 
 
 Application to gases; Rankine's formula is, 
 
 (4L) SB A/1 + *,*L *.}, 
 
 \ d/j. h ii \ ;j. v J 
 
 dp- 1 - -, - . 1 + 
 
 If a.v is the coefficient of expansion between and 100, then 
 
 AI, = (1 + -00635m), 
 whence 
 
 where a' p and a, are the true coefficients of expansion at the given 
 temperature; 
 
 + 5m *.*. 
 
 According to Thomson and Joule's experiments m = 0-33 C. for air 
 and about 2-0 for C0 2 . Hence //= 272 -99. 
 
 The equations should be applied to the observations directly at the 
 given temperature, but it will generally be sufficient to use them after 
 reduction to C. Using K = -2375 according to Regnault for air, we 
 have for the latitude of Baltimore, 
 
 From Rontgen's value r = 1-4053 = 430-3. 33 
 
 J 
 
 " Amagat's " 1-397 = 436-6. 
 
 " velocity of sound 331-78m. per sec. = 429'6. 
 
 */ 
 
 33 R6ntgen gives the value 428-1 for the latitude of Paris as calculated by a formula 
 of Shroder v. d. Kolk, and 427-3 from the formula for a perfect gas, and these both 
 agree more nearly with my result than that calculated from my own formula. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 415 
 
 Using Wiedemann's value for K, -2389, these become 
 
 = 427-8 ; -^ = 434-0 ; = 427-1 . 
 999 
 
 As Wiedemann, however, used the mercurial thermometer, and as 
 the reduction to the air thermometer would increase these figures from 
 2 to -8 per cent, it is evident that Eegnault's value for K is the more 
 nearly correct. I take the weights rather arbitrarily as follows : 
 
 Weight. J. 
 
 Eontgen 3 430-3 
 
 Amagat 1 436-6 
 
 Velocity of sound 4 429-6 
 
 Mean 430-7 
 
 And this is of course the value referred to water at 14 C. and in the 
 latitude of Baltimore. My value at this point is 427-7. 
 
 This determination of the mechanical equivalent from the properties 
 of air is at most very imperfect, as a very slight change in either f or 
 the velocity of sound will produce a great change in the mechanical 
 equivalent. 
 
 From Theory of Vapors 
 
 Another important method of calculating the mechanical equivalent 
 of heat is from the equation for a body at its change of state, as for 
 instance in vaporization. Let v be the volume of the vapor, and v' the 
 volume of the liquid, H the heat required to vaporize a unit of mass of 
 the water; also let p be the pressure in absolute units, and // the absolute 
 temperature. Then 
 
 JH 
 
 The quantity H and the relation of p to // have been determined with 
 considerable accuracy by Regnault. To determine J it is only required 
 to measure the volume of saturated steam from a given weight of water; 
 and the principal difficulty of the process lies in this determination, 
 though the other quantities are also difficult of determination. 
 
 This volume can be calculated from the density of the vapor, but this 
 is generally taken in the superheated state. 
 
416 HENRY A. KOWLAND 
 
 The experiments of Fairbairn and Tate 34 are probably the best direct 
 experiments on the density of saturated vapor, but even those do not 
 pretend to a greater accuracy than about 1 in 100. With Eegnault's 
 values of the other quantities, they give about Joule's value for the 
 equivalent, namely 425. Him, Herwig, and others have also made the 
 determination, but the results do not agree very well. Herwig even 
 used a Geissler standard thermometer, which I have shown to depart 
 very much from the air thermometer. 
 
 Indeed, the experiments on this subject are so uncertain, that physi- 
 cists have about concluded to use this method rather for the deter- 
 mination of the volume of saturated vapors than for the mechanical 
 equivalent of heat. 
 
 From the Steam-Engine and Expansion of Metals 
 
 The experiments of Hirn on the steam-engine and of Edlund on the 
 expansion and contraction of metals, are very excellent as illustrating 
 the theory of the subject, but cannot have any weight as accurate deter- 
 minations of the equivalent. 
 
 From Friction Experiments 
 
 Experiments of this nature, that is, irreversible processes for con- 
 verting mechanical energy into heat, give by far the best methods for 
 the determination of the equivalent. 
 
 Rumford's experiment of 1798 is only valuable from an historical 
 point of view. Joule's results since 1843 undoubtedly give the best 
 data we yet have for the determination of the equivalent. The mean of 
 all his friction experiments of 1847 and 1850 which are given in the 
 table is 425-8, though he prefers the smallest number, 423-9, of 1850. 
 This last number is at present accepted throughout the civilized world, 
 though there is at present a tendency to consider the number too small. 
 But this value and his recent result of 1878 have undoubtedly as much 
 weight as all other results put together. 
 
 As sources of error in these determinations I would suggest, first, 
 the use of the mercurial instead of the air thermometer. Joule com- 
 pared his thermometers with one made by Fastre. In the Appendix 
 to Thermometry I give the comparison of two thermometers made by 
 Fastre in 1850, with the air thermometer, as well as of a large number 
 of others. From this it seems that all thermometers as far as measured 
 
 3* Phil. Mag., ser. 4, xxi, 230. 
 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 417 
 
 stand above the air thermometer between and 100, and that the 
 average for the Fastre at 40 is about 0-1 C. Using the formula given 
 in Thermometry this would produce an error of about 3 parts in 1000 
 at 15 C., the temperature Joule used. 
 
 The specific heat of copper which Joule uses, namely, -09515, is 
 undoubtedly too large. Using the value deduced from more recent 
 experiments in calculating the capacity of my calorimeter, -0922, 
 Joule's number would again be increased 13 parts in 10,000, so that 
 we have, 
 
 Joule's value 423-9, water at 15-7 C. 
 
 Eeduction to air thermometer -|-1'3 
 
 Correction for specific heat of copper. . -f- -5 
 Correction to latitude of Baltimore. . . -f- -5 
 
 426-2 
 
 It does not seem improbable that this should be still further in- 
 creased, seeing that the reduction to the air thermometer is the smallest 
 admissible, as most other thermometers which I have measured give 
 greater correction, and some even more than three times as great as 
 the one here used, and would thus bring the value even as high as 429. 
 
 One very serious defect in Joule's experiments is the small range 
 of temperature used, this being only about half a degree Fahrenheit, 
 or about six divisions on his thermometer. It would seem almost im- 
 possible to calibrate a thermometer so accurately that six divisions 
 should be accurate to one per cent, and it would certainly need a very 
 skillful observer to read to that degree of accuracy. Further, the same 
 thermometer " A " was used throughout the whole experiment with 
 water, and so the error of calibration was hardly eliminated, the tem- 
 perature of the water being nearly the same. In the experiment on 
 quicksilver another thermometer was used, and he then finds a higher 
 result, 424-7, which, reduced as above, gives 427-0 at Baltimore. 
 
 The experiments on the friction of iron should be probably rejected 
 on account of the large and uncertain correction for the energy given 
 out in sound. 
 
 The recent experiments of 1878 give a value of 772-55, which re- 
 duced gives at Baltimore 426-2, the same as the other experiment. 
 
 The agreement of these reduced values with my value at the same 
 temperature, namely 427-3, is certainly very 'remarkable, and shows 
 what an accurate experimenter Joule must be to get with his simple 
 27 
 
418 HENRY A. EOWLAND 
 
 apparatus results so near those from my elaborate apparatus, which 
 almost grinds out accurate results without labor except in reduction. 
 Indeed, the quantity is the same as I find at about 20 C. 
 
 The experiments of Him of 1860-61 seem to point to a value of the 
 equivalent higher than that found by Joule, but the details of the 
 experiment do not seem to have been published, and they certainly 
 were not reduced to the air thermometer. 
 
 The method used by Violle in 1870 does not seem capable of accur- 
 acy, seeing that the heat lost by a disc in rapid rotation, and while 
 carried to the calorimeter, must have been uncertain. 
 
 The experiments of Him are of much interest from the methods 
 used, but can hardly have weight as accurate determinations. Some 
 of the methods will be again lef erred to when I come to the description 
 of apparatus. 
 
 Method by Heat Generated by Electric Cwrent 
 
 The old experiments of Quintus Icilius or Lenz do not have any 
 except historical value, seeing that Weber's measure of absolute resist- 
 ance was certainly incorrect and we now have no means of finding its 
 error. 
 
 The theory of the process is as follows. The energy of electricity 
 being the product of the potential by the quantity, the energy ex- 
 pended by forcing the quantity of electricity, Q, along a wire of re- 
 sistance, R, in a second of time, must be Q Z R, and as this must equal 
 the mechanical equivalent of the heat generated, we must have JH 
 Q z Rt, where H is the heat generated and t is the time the current Q 
 flows. 
 
 The principal difficulty about the determination by this method 
 seems to be that of finding R in absolute measure. A table of the 
 values of the ohm as obtained by different observers, was published by 
 me in my paper on the 'Absolute Unit of Electrical Besistance/ in 
 the American Journal of Science, Vol. XV, and I give it here with 
 some changes. 
 
 The ratio of the Siemens unit to the ohm is now generally taken at 
 9536, though previous to 1864 there seems to have been some doubt 
 as to the value of the Siemens unit. 
 
 Since 1863-4, when units of resistance first began to be made with 
 great accuracy, two determinations of the heat generated have been 
 made. The first by Joule with the ohm, and the second by H. F. 
 Weber, of Zurich, with the Siemens unit. 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 
 
 419 
 
 Each determination of resistance with each of these experiments 
 gives one value of the mechanical equivalent. As Lorenz's result was 
 only in illustration of a method, I have not included it among the exact 
 determinations. 
 
 TABLE XXXI. 
 
 Date. 
 
 Observer. 
 
 Value of Ohm. 
 
 Remarks. 
 
 1849 
 
 Kirchhoff 
 
 88 to -90 
 
 Approximately. 
 
 1851 
 
 Weber 
 
 95 to -97 
 
 Approximately. 
 
 1862 
 
 Weber 
 
 j 1-088 
 j 1-075 
 
 From Thomson's unit. 
 From Weber's value of Siemens unit. 
 
 1863-4 
 
 B. A. Committee 
 
 j 1-0000 
 } -993 
 
 Mean of all results. 
 Corrected by Rowland to zero vel- 
 
 
 
 
 ocity of coil. 
 
 1870 
 
 Kohlrausch 
 
 1-0193 
 
 
 1873 
 
 Lorenz 
 
 975 
 
 Approximately. 
 
 1876 
 
 Rowland 
 
 99113s 
 
 From a preliminary comparison with 
 
 
 
 
 the B. A. unit. 
 
 1878 
 
 H. F. Weber 
 
 1-0014 
 
 Using ratio of Siemens unit to ohm, 
 
 
 
 
 9536. 
 
 The result found by Joule was J= 25187 in absolute measure using 
 feet and degrees F., which becomes 429-9 in degrees C. on a mercurial 
 thermometer and in the latitude of Baltimore, compared with water 
 at 18-6C. 
 
 TABLE XXXII. EXPERIMENTS OF JOULE. 
 
 Observer. 
 
 Value of 
 B. A. Unit. 
 
 Mechanical equivalent 
 from Joule's Exp. 
 
 Mechanical equivalent 
 reduced to Air Ther- 
 mometer and cor- 
 rected for 8p. Ht. of 
 Copper. 
 
 B. A. Committee 
 
 1-0000 
 
 429-9 
 
 431-4 
 
 Ditto corrected by Rowland 
 Kohlrausch 
 
 993 
 1-0193 
 
 426-9 
 438-2 
 
 428-4 
 439-7 
 
 Rowland 
 
 9911 
 
 426-1 
 
 427-6 
 
 H. F. Weber 
 
 1-0014 
 
 430-5 
 
 432-0 
 
 
 
 
 
 The experiments of H. F. Weber 36 gave 428-15 in the latitude of 
 Zurich and for 1 C. on the air thermometer and at a temperature of 
 18 C. This reduced to the latitude of Baltimore gives 428-45. 
 
 My own value at this temperature is 426-8, which agrees almost 
 exactly with the fourth value from my own determination of the abso~ 
 lute unit. 37 
 
 K Given -9912 by mistake in the other tables. 
 3Phil. Mag., 1878, 5th ser., v. 135. 
 
 37 The value of the ohm found by reversing the calculation would be -992, almost 
 exactly my value. 
 
420 
 
 HENEY A. ROWLAND 
 
 There can be no doubt that Joule's result is most exact, and hence 
 I have given his results twice the weight of Weber's. Weber used a 
 wire of about 14 ohms' resistance, and a small calorimeter holding only 
 250 grammes of water. This wire was apparently placed in the water 
 without any insulating coating, and yet current enough was sent 
 through it to heat the water 15 during the experiment. No precau- 
 tion seems to have been taken as to the current passing into the water, 
 which Joule accurately investigated. Again, the water does not seem 
 to have been continuously stirred, which Joule found necessary. And 
 further, Newton's law of cooling does not apply to so great a range 
 as 15, though the error from this source was probably small. Further- 
 
 TABLE XXXIII. 
 
 EXPERIMENTS OF H. F. WEBER. 
 
 Mean of Joule and 
 Weber, giving Joule 
 twice the Weight of 
 Weber. 
 
 Observer. 
 
 Value of 
 B. A. Unit. 
 
 Mechanical equivalent 
 of Heat from Weber's 
 Experiments. 
 
 Mean equivalent re- 
 duced to Air Ther- 
 mometer in the Lati- 
 tude of Baltimore. 
 
 B. A. Committee 
 
 1-000 
 993 
 1-0193 
 9911 
 1-0014 
 
 427-9 
 424-9 
 436-2 
 424-1 
 
 428-5 
 
 430-2 
 427-2 
 439-1 
 426-4 
 431-4 
 
 Ditto corrected by Rowland 
 Kohlrausch 
 
 
 H. F. Weber 
 
 
 more, I know of no platinum which has an increase of coefficient of 
 001054 for 1 C., but it is usually given at about -003. 
 
 There can be no doubt that experiments depending on tKe heating 
 of a wire give too small a value of the equivalent, seeing that the 
 temperature of the wire during the heating must always be higher 
 than that of the water surrounding it, and hence more heat will be 
 generated than there should be. Hence the numbers should be slightly 
 increased. Joule used wire of platinum-silver alloy, and Weber plati- 
 num wire, which may account for Weber's finding a smaller value than 
 Joule, and Weber's value would be more in error than Joule's. Undoubt- 
 edly this is a serious source of error, and I am about to repeat an 
 experiment of this kind in which it is entirely avoided. Considering 
 this source of error, these experiments confirm both my value of the 
 ohm and of the mechanical equivalent, and unquestionably show a large 
 error in Kohlrausch's absolute value of the Siemens unit or ohm. 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 421 
 
 The experiments of Joule and Favre, where the heat generated by 
 a current, both when it does mechanical work and when it does not, 
 are very interesting, but can hardly have any weight in an estimation 
 of the true value of the equivalent. 
 
 The method of calculating the equivalent from the chemical action 
 in a battery, or the electro-motive force required to decompose any 
 substance, such as water, is as follows: 
 
 Let E be such electro-motive force and c be the quantity of chemical 
 substance formed in battery or decomposed in voltameter per second. 
 Then total energy of current of energy per second is EQ, where Q is 
 the current, or cQHJ, where H is the heat generated by unit of c, or 
 required to decompose unit of c. Hence, if the process is entirely 
 reversible, we must have in either case 
 
 CHJ = E. 
 
 But the process is not always reversible, seeing that it requires more 
 electro-motive force to decompose water than is given by a gas battery. 
 This is probably due to the formation at first of some unstable com- 
 pound like ozone. The process with a battery seems to be best, and we 
 can thus apply it to the Daniell cell. The following quantities are 
 mostly taken from Kohlrausch. 
 
 The quantity c has been found by various observers, and Kohlrausch M 
 gives the mean value as -009421 for water according to his units (mg., 
 mm., second system). Therefore for hydrogen it is -001047. 
 
 The quantity H can be observed directly by short-circuiting the 
 battery, or can be found from experiments like those of Favre and 
 Silbermann. 
 
 The electro-motive force E can be made to depend either upon the 
 absolute measure of resistance, or can be determined, as Thomson has 
 done, in electro-static units. In electro-magnetic units it is 
 
 Absolute Measure 
 
 Siemens. Ohms. according to my 
 
 Determination. 
 
 After Waltenhof en 11-43 10-90 10-80 XlO 10 
 
 " Kohlrausch 39 11-71 H'17 11-07X10 10 
 
 After Favre, 1 equivalent of zinc developes in the Daniell cell 23993 
 heat units; 
 
 . / E 
 
 38 Fogg. Ann., cxlix, 179. 
 
 39 Given by Kohlrausch, Pogg. Ann., cxlix, 182. 
 
422 HEXRY A. ROWLAND 
 
 On the rag., mm., second system, we have -# = 10-935 X 10 10 , c = 
 001047, H = 23993, g = 9800-5 at Baltimore. 
 
 /. = 444160 mm. = 444-2 metres. 
 9 
 
 Using Kohlrausch's value for absolute resistance, he finds 456-5, 
 which is much more in error than that from my determination. I do 
 not give the calculation from the Grove battery, because the Grove 
 battery is not reversible, and action takes place in it even when no 
 current flows. 
 
 Thomson finds the difference of potential between the poles of a 
 Daniell cell in electro-static measure to be -00374 on the cm., grm., 
 second system. 40 Using the ratio 29,900,000,000 cm. per second, as I 
 have recently found, but not yet published, we have 111,800,000 on 
 the electro-magnetic system or 11-18 X 10 10 on the mm., mg., second 
 system. This gives 
 
 = 474.3 metres. 
 
 g 
 
 General Criticism 
 
 All the results so far obtained, except those of Joule, seem to be of 
 the crudest description; and even when care was apparently taken in 
 the experiment, the method seems to be defective, or the determination 
 is made to rest upon the determination of some other constant whose 
 value is not accurately known. Again, only one or two observers have 
 compared their thermometers with the air thermometer, although I 
 have shown in ' Thermometry ' that an error of more than one per 
 cent may be made by this method. The range of temperature is also 
 small as a general rule and the specific heat of water is assumed con- 
 stant. 
 
 Hence a new determination, avoiding these sources of erfor, seems 
 to be imperatively demanded. 
 
 (6.) Description of Apparatus 
 1. PRELIMINARY EEMARKS 
 
 As we have seen in the historical portion, the only experiments of a 
 high degree of accuracy to the present time are those of Joule. Looked 
 at from a general point of view, the principal defects of his method 
 were the use of the mercurial instead of the air thermometer, and the 
 small rate at which the temperature of his calorimeter rose. 
 
 40 Thomson, Papers on Electrostatics and Magnetism, p. 246. 
 
ON THE MECHANICAL EQUIVALEXT OF HEAT 423 
 
 In devising a new method a great rise of temperature in a short time 
 was considered to be the great point, combined, of course, with an accu- 
 rate measurement of the work done. For a great rise of temperature 
 great work must be done, which necessitates the use of a steam-engine 
 or other motive power. For the measurement of the work done, there 
 is only one principle in use at present, which is, that the work trans- 
 mitted by any shaft in a given time is equal to 2/r times the product of 
 the moment of the force by the number of revolutions of the shaft in 
 that time. 
 
 In mechanics it is common to measure the amount of the force 
 twisting the shaft by breaking it at the given point, and attaching the 
 two ends together by some arrangement of springs whose stretching 
 gives the moment. Morin's dynamometer is an example. Him 41 gives 
 a method which he seems to consider new, but which is immediately 
 recognized as Huyghens's arrangement for winding clocks without stop- 
 ping them. As cords and pulleys are used which may slip on each other, 
 it cannot possess much accuracy. I have devised a method by cog- 
 wheels which is more accurate, but which is better adapted for use in 
 the machine-shop than for scientific experimentation. 
 
 But the most accurate method known to engineers for measuring the 
 work of an engine is that of White's friction brake, and on this I have 
 based my apparatus. Him was the first to use this principle in deter- 
 mining the mechanical equivalent of heat. In his experiment a hori- 
 zontal axis was turned by a steam-engine. On the axis was a pulley 
 with a flat surface, on which rested a piece of bronze which was to be 
 heated by the friction. The moment of the force with which the fric- 
 tion tended to turn the piece of bronze was measured, together with 
 the velocity of revolution. This experiment, which Him calls a balance 
 de frottement, was first constructed by him to test the quality of oils used 
 in the industrial arts. He experimented by passing a current of water 
 through the apparatus and observing the temperature of the water be- 
 fore and after passing through. He thus obtained a rough approxima- 
 tion to Joule's equivalent. 
 
 He afterward constructed an apparatus consisting of two cylinders 
 about 30 cm. in diameter and 100 cm. long, turning one within the 
 other, the annular space between which could be filled with water, or 
 through which a stream of water could be made to flow whose tempera- 
 ture could be measured before and after. The work was measured by 
 the same method as before. 
 
 41 Exposition de la Theorie Mecanique de la Chaleur, 3 m 6d., p. 18. 
 
424 HENRY A. BOWLAND 
 
 But in neither of these methods does Him seem to have recognized 
 the principle of the work transmitted by a shaft being equal to the 
 moment of the force multiplied by the angle of rotation of the shaft. 
 In designing his apparatus, he evidently had in view the reproduction 
 in circular motion of the case of friction between two planes in linear 
 motion. 
 
 Since I designed my apparatus, Puluj 42 has designed an instrument 
 to be worked by hand, and based on the principle used by Him. He 
 places the revolving axis vertical, and the friction part consists of two 
 cones rubbing together. But no new principle is involved in his appa- 
 ratus further than in that used by Him. 
 
 In my apparatus one of the new features has been the introduction 
 of the Joule calorimeter in the place of the friction cylinders of Him 
 or the cones of Puluj. At first sight the currents and whirlpools in 
 such a calorimeter might be supposed to have some effect; but when 
 the motion is steady, it is readily seen that the torsion of the calorimeter 
 is equal to that of the shaft, and hence the principle must apply. 
 
 This change, together with the other new features in the experi- 
 ments and apparatus, has at once made the method one of extreme 
 accuracy, surpassing all others very many fold. 
 
 2. GENEBAL DESCRIPTION 
 
 The apparatus was situated in a small building, entirely separate 
 from the other University buildings, and where it was free from dis- 
 turbances. 
 
 Fig. 6 gives a general view of the apparatus. To a movable axis, ab, 
 a calorimeter similar to Joule's is attached, and the whole is suspended 
 by a torsion wire, c. The shaft of the calorimeter comes out from the 
 bottom, and is attached to a shaft, ef, which receives a uniform motion 
 from the engine by mean's of the bevel wheels g and Ji. To the axis, 
 ab, an accurate turned wheel, M, was attached, and the moment of 
 the force tending to turn the calorimeter was measured by the weights 
 o and p, attached to silk tapes passing around the circumference of the 
 wheel in combination with the torsion of the suspending wire. To this 
 axis was also attached a long arm, having two sliding weights, q and r, 
 by which the moment of inertia could be varied or determined. 
 
 42 Pogg. Ann., clvii, 437. 
 
 "Joule's latest results were published after this was written, and I was not aware 
 that he, had made this improvement until lately. The result of his experiment, how- 
 ever, reached me soon after, and I have referred to it in the paper, but I did not see 
 the complete paper until much later. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 425 
 
 FIG. 6. 
 
426 HENRY A. EOWLAND 
 
 The number of revolutions was determined by a chronograph, which 
 received motion by a screw on the shaft ef, and which made one revo- 
 lution for 102 of the shaft. On this chronograph was recorded the 
 transit of the mercury over the divisions of the thermometer. 
 
 Around the calorimeter a water jacket, tu, made in halves, was 
 placed, so that the radiation could be estimated. A wooden box sur- 
 rounded the whole, to shield the observer from the calorimeter. 
 
 The action of the apparatus is in general as follows: As the inner 
 paddles revolve, the water strikes against the outer paddles, and so 
 tends to turn the calorimeter. When this force is balanced by the 
 weights op, the whole will be in equilibrium, which is rendered stable 
 by the torsion of the wire cd. Should any slight change take place in 
 the velocity, the calorimeter will revolve in one direction or the other 
 until the torsion brings it into equilibrium again. The amount of tor- 
 sion read off on a scale on the edge of Tel gives the correction to be 
 added to or subtracted from the weights op. 
 
 One observer constantly reads the circle Tel, and the other constantly 
 records the transits of the mercury over the divisions of the ther- 
 mometer. 
 
 A series extending over from one half to a whole hour, and record- 
 ing a rise of 15 C. to perhaps 25 C., and in which a record was made 
 for perhaps each tenth of a degree, would thus contain several hundred 
 observations, from any two of which the equivalent of heat could be 
 determined, though they would not all be independent. Such a series 
 would evidently have immense weight; and, in fact, I estimate that, 
 neglecting constant errors, a single series has more weight than all of 
 Joule's experiments of 1849, on water, put together. 44 
 
 The correction for radiation is inversely proportional to the ratio of 
 the rate of work generated to the rate at which the heat is lost; 
 and this for equal ranges of temperature is only 7 V as great in my 
 measures as in Joule's; for Joule's rate of increase was about 0-62 C. 
 per hour, while mine is about 35 C. in the same time, and can be in- 
 creased to over 45 C. per hour. 
 
 3. DETAILS 
 The Calorimeter 
 
 Joule's calorimeter was made in a very simple manner, with few 
 paddles, and without reference to the production of currents to mix 
 
 44 Forty experiments, with an average rise of temperature of 0-56 F., equal to 
 0-31 C., gives a total rise of 12 -4 C., which is only about two-thirds the average of 
 one of my experiments. As my work is measured with equal accuracy, and my 
 radiation with greater, the statement seems to be correct. 
 
N THE MECHANICAL EQUIVALENT OF HEAT 
 
 427 
 
 up the water. Hence the paddles were made without solder, and were 
 screwed together. Indeed, there was no solder about the apparatus. 
 
 But, for my purpose, the number of paddles must be multiplied, so 
 that there shall be no jerk in the motion, and that the resistance may 
 be great; they must be stronger, to resist the force from the engine, 
 and they must be light, so as not to add an uncertain quantity to the 
 calorific capacity. Besides this, the shape must be such as to cause 
 the whole of the water to run in a constant stream past the thermom- 
 eter, and to cause constant exchange between the water at the top and 
 at the bottom. 
 
 FIG. 7. 
 
 FIG. 8. 
 
 Fig. 7 shows a section of the calorimeter, and Fig. 8 a perspective 
 view of the revolving paddles removed from the apparatus, and with the 
 exterior paddles removed from around it; which could not, however, be 
 accomplished physically without destroying them. 
 
 To the axis cb, Fig. 7, which was of steel, and 6 mm. in diameter, a 
 copper cylinder, ad, was attached, by means of four stout wires at e, 
 and four more at f. To this cylinder four rings, g, Ji, i, j, were attached, 
 which supported the paddles. Each one had eight paddles, but each 
 ring was displaced through a small angle with reference to the one 
 below it, so that no one paildle came over another. This was to make 
 the resistance continuous, and not periodical. The lower row of pad- 
 dles were turned backwards, so that they had a tendency to throw the 
 water outwards and make the circulation, as I shall show afterwards. 
 
428 HENRY A. ROWLAND 
 
 Around these movable paddles were the stationary paddles, consist- 
 ing of five rows of ten each. These were attached to the movable 
 paddles by bearings,, at the points c and Jc, of the shaft, and were re- 
 moved with the latter when this was taken from the calorimeter. 
 When the whole was placed in the calorimeter, these outer paddles were 
 attached to it by means of four screws, I and m, so as to be immovable. 
 
 The cover of the calorimeter was attached to a brass ring, which 
 was nicely ground to another brass ring on the calorimeter, and which 
 could be made perfectly tight by means of a little white-lead paini 
 The shaft passed through a stuffing-box at the bottom, which was 
 entirely within the outer surface of the calorimeter, so that the heat 
 generated should all go to the water. The upper end of the shaft 
 rested in a bearing in a piece of brass attached to the cover. In the 
 cover there were two openings, one for the thermometer, and the 
 other for filling the calorimeter with water. 
 
 From the opening for the thermometer, a tube of copper, perforated 
 with large holes, descended nearly to the centre of the calorimeter. 
 The thermometer was in this sieve-like tube at only a short distance 
 from the centre of the calorimeter, with the revolving paddles outside 
 of it, and in the stream of water, which circulated as shown by the 
 arrows. 
 
 This circulation of water took place as follows. The lower paddles 
 threw the water violently outwards, while the upper paddles were pre- 
 vented from doing so by a cylinder surrounding the fixed paddles. 
 The consequence was, that the water flowed up in the space between 
 the outer shell and the fixed paddles, and down through the central 
 tube of the revolving paddles. As there was always a little air at the 
 top to allow for expansion, it would also aid in the same direction. 
 These currents, which were very violent, could be observed through 
 the opening's. 
 
 The calorimeter was attached to a wheel, fixed to the shaft db, by 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 429 
 
 the method shown in Fig. 9. At the edge of the wheel, which was of 
 the exact diameter of the calorimeter, two screws were attached, from 
 which wires descended to a single screw in the edge of the calorimeter. 
 Through the wheel, a screw armed with a vulcanite point pressed upon 
 the calorimeter, and held it firmly. Three of these arrangements, at 
 distances of 120, were used. To centre the calorimeter, a piece of 
 vulcanite at the centre was used. By this method of suspension very 
 little heat could escape, and the amount could he allowed for hy the 
 radiation experiments. 
 
 The Torsion System 
 
 The torsion wire was of such strength that one millimeter on the 
 scale at the edge of the wheel signified 11-8 grammes, or ahout y^ of 
 the weights op generally used. There were stops on the wheel, so 
 that it could not move through more than a small angle. The weights 
 were suspended by very flexible silk tapes, 6 mm. or 8 mm. broad and 
 0-3 mm. thick. They varied from 4-5 k. to 8-5 k. taken together. The 
 shaft, ab, was of uniform size throughout, so that the wire c suspended 
 the whole system, and no weight rested on the bearings. 
 
 The pulleys, m, n, Fig. 6, were very exactly turned and balanced, and 
 the whole suspended system was so free as to vibrate for a considerable 
 time. However, as will be shown hereafter, its freedom is of little 
 consequence. 
 
 The Water Jacket 
 
 Around the calorimeter, a water jacket, t u, was placed, so that the 
 radiation should be perfectly definite. During the preliminary experi- 
 ments a simple tin jacket was used, whose temperature was determined 
 by two thermometers, one above and the other below, inserted in tubes 
 attached to the jacket. 
 
 The Driving Gear 
 
 The cog-wheels, g, h, were made by Messrs. Brown and Sharpe, of 
 Providence, and were so well cut that the motion transmitted to the 
 calorimeter must have been very uniform. 
 
 The Chronograph 
 
 The cylinder of the chronograph was turned by a screw on the shaft 
 ef, and received one revolution for 102 of the paddles; 155 revolutions 
 of the cylinder, or 15,810 of the paddles, could be recorded, though, 
 
430 HENRY A. EOWLAND 
 
 when necessary, the paper could be changed without stopping, and the 
 experiment thus continued without interruption. 
 
 The Frame and Foundation 
 
 The frame was very massive and strong, so as to prevent oscillation; 
 and the whole instrument weighed about 500 pounds as nearly as could 
 be estimated. It was placed on a solid brick pier, with a firm founda- 
 tion in the ground. The trembling was barely perceptible to the hand 
 when running the fastest. 
 
 The Engine 
 
 The driving power was a petroleum engine, which was very efficient 
 in driving the apparatus with uniformity. 
 
 The Balance 
 
 For weighing the calorimeter, a balance capable of showing the 
 presence of less than T \ gramme with 15,000 grammes was used. The 
 weights, however, by Schickert, of Dresden, were accurate among them- 
 selves to at least 5 mg. for the larger weights, and in proportion for 
 the smaller. A more accurate balance would have been useless, as will 
 be seen further on. 
 
 Adjustments 
 
 There are few adjustments, and they were principally made in the 
 construction. 
 
 In the first place, the shafts ab and ef must be in line. Secondly, 
 the wheels rrm must be so adjusted that their planes are vertical, and 
 that the tapes shall pass over them symmetrically, and that their edges 
 shall be in the plane of the wheel Id. 
 
 Deviation from these adjustments only produced small error. 
 
 (c.) Theory of the Experiment 
 1. ESTIMATION OF WORK DONE 
 
 The calorimeter is constantly receiving heat from the friction, and 
 is giving out heat by radiation and conduction. Now, at any given 
 instant of time, the temperature of the whole of the calorimeter is not 
 the same. Owing to the violent stirring, the water is undoubtedly at 
 a very uniform temperature throughout. But the solid parts of the 
 calorimeter cannot be so. The greatest difference of temperature is 
 evidently soon after the commencement of the operation. But after 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 431 
 
 some time the apparatus reaches a stationary state, in which, but for 
 the radiation, the rise of temperature at all points would be the same. 
 This steady state will be theoretically reached only after an infinite 
 time; but as most of the metal is copper, and quite thin, and as the 
 whole capacity of the metal work is only about four per cent of the 
 total capacity, I have thought that one or two minutes was enough to 
 allow, though, if others do not think this time sufficient, they can 
 readily reject the first few observations of each series. When there 
 is radiation, the stationary state will never be reached theoretically, 
 though practically there is little difference from the case where there is 
 no radiation. 
 
 The measurement of the work done can be computed as follows. 
 Let M be the moment of the force tending to turn the calorimeter, and 
 dd the angle moved by the shaft. The work done in the time t will 
 be fMdft. If the moment of the force is constant, the integral is 
 simply Mti; but it is impossible to obtain an engine which runs with 
 perfect steadiness, and although we may be able to calculate the inte- 
 gral, as far as long periods are concerned, by observation of the torsion 
 circle, yet we are not thus able to allow for the irregularity during one 
 revolution of the engine. Hence I have devised the following theory. 
 I have found, by experiments with the instrument, that the moment of 
 the force is very nearly, for high velocities at least, proportional to the 
 square of the velocity. For rapid changes of the velocity, this is not 
 exactly true, but as the paddles are very numerous in the calorimeter, 
 it is probably very nearly true. We have then 
 
 where C is a constant. Hence the work done becomes 
 
 n r (dov, a n r/dff\',. 
 
 W= C I -jj- \dO = C I ( rr \flt- 
 
 J \dt ) J \tltj 
 
 As we allow for irregularities of long period by readings of the tor- 
 sion circle, we can assume in this investigation that the mean velocity 
 is constant, and equal to t? . The form of the variation of the velocity 
 must be assumed, and I shall put, without further discussion, 
 
 dt 
 
 We then find, on integrating from a to 0, 
 
432 HENEY A. KOWLAND 
 
 which is the work on the calorimeter during one revolution of the 
 engine. 
 
 The equation of the motion of the calorimeter, supposing it to be 
 nearly stationary, and neglecting the change of torsion of the suspend- 
 ing wire, is 
 
 m dV WD , nt f- 2* A 2 A 
 
 + Cvl (1 + c cos - - = 0, 
 
 TIT ^ 
 
 g dt* 2 \ a 
 
 where m is the moment of inertia of the calorimeter and its attach- 
 ments, <p is the angular position of the calorimeter, W is the sum of 
 the torsion weights, and D is the diameter of the torsion wheel. Hence, 
 
 = L j J/ \_Cvl (I + 
 
 til (_ 
 
 When WD = 2Cv Q z (I -\- -|c 2 ), the calorimeter will merely oscillate 
 around a given position, and will reach its maximum at the times t = 0, 
 a, a, &c. 
 
 The total amplitude of each oscillation will be very nearly 
 
 ,,,_,,/ _ Cfrfra'c = WDga'c 
 v*m 2x*m ' 
 
 If x is the amplitude of each oscillation, as measured in millimetres, 
 on the edge of the wheel of "diameter D, we have <p <p' =. -?. 
 
 Hence . c = ^, 
 
 where n is the number of revolutions of the engine per second. 
 Having found c in this way, the work will be, during any time, 
 
 w = TT WDN(l + c 2 ) , 
 where N is the total number of revolutions of the paddles. 
 
 A variation of the velocity of ten per cent from the mean, or twenty 
 per cent total, would thus only cause an error of one per cent in the 
 equivalent. 
 
 Hence, although the engine was only single acting, yet it ran easily, 
 had great excess of power, and was very constant as far as long periods 
 were concerned. The engine ran very fast, making from 200 to 250 
 revolutions per minute. The fly-wheel weighed about 220 pounds, and 
 had a radius of 1 feet. At four turns per second, this gives an energy 
 of about 3400 foot-pounds stored in the wheel. The calorimeter re- 
 quired about one-half horse-power to drive it; and, assuming the same 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 433 
 
 for the engine friction, we have about 140 foot-pounds of work re- 
 quired per revolution. Taking the most unfavorable case, where all 
 the power is given to the engine at one point, the velocity changes 
 during the revolution about four per cent, or c would nearly equal .02, 
 causing an error of 1 part in 2500 nearly. By means of the shaking 
 of the calorimeter, I have estimated c as follows, the value of m being 
 changed by changing the weight on the inertia bar, or taking it off 
 altogether. The estimate of the shaking was made by two persons 
 independently. 
 
 m. x observed. c calculated. 
 
 2,200,000 grms. cm. a -6 mm. '016 
 
 3,100,000 " -36 " -013 
 
 11,800,000 " -13 " -017 
 
 Mean, c = '015 
 
 causing a correction of 1 part in 5000. 
 
 Another method of estimating the irregularity of running is to put 
 on or take off weights until the calorimeter rests so firmly against the 
 stops that the vibration ceases. Estimated in this way, I have found 
 a little larger value of c, namely, about -017. 
 
 But as one cannot be too careful about such sources of error, I 
 have experimented on the equivalent with different velocities and with 
 very different ways of running the engine, by which c was greatly 
 changed, and so have satisfied myself that the correction from this 
 source is inappreciable in the present state of the science of heat. 
 
 Hence I shall simply put for the work 
 
 w = xNWD, 
 
 in gravitation measure at Baltimore. To reduce to absolute measure, 
 we must multiply by the force of gravity given by the formula 
 g = 9-78009 + -0508 sm s ? , 
 
 which gives 9-8005 metres per second at Baltimore. If the calorimeter 
 moved without friction, no work would be required to cause it to 
 vibrate back and forth, as I have described; but when it moves with 
 friction, some work is required. When I designed the apparatus, I thus 
 had an idea that it would be best to make it as immovable as possible 
 by adding to its moment of inertia by means of the inertia bar and 
 weights. But on considering the subject further, I see that only the 
 excess of energy represented by c 2 xNWD can be used in this way. For, 
 when the calorimeter is rendered nearly immovable by its great moment 
 28 
 
 ^aas^=5r^=rR^cs=^^^j^s^xs^-Jua^ 
 
434 HENRY A. EOWLAXD 
 
 of inertia, the work done on it is, as we have seen, TtNWD (1 -f- c 2 ); 
 but if it had no inertia, it is evident that the work would be only 
 TiNWD. If, therefore, the calorimeter is made partially stationary, 
 either by its moment of inertia or by friction, the work will be some- 
 where between these two, and the work spent in friction will be only 
 so much taken from the error. Hence in the latter experiments the 
 inertia bar was taken off, and then the calorimeter constantly vibrated 
 through about half a millimeter on the torsion scale. 
 
 Besides this quick vibration, the calorimeter is constantly moving to 
 the extent of a few millimetres back and forth, according to the vary- 
 ing velocity of the engine. As frequent readings were taken, these 
 changes were eliminated. In very rare cases the weights had to be 
 changed during the experiment; but this was very seldom. 
 
 The vibration and irregular motion of the calorimeter back and forth 
 served a very useful purpose, inasmuch as it caused the friction of the 
 torsion apparatus to act first in one direction and then in the other, so 
 that it was finally eliminated. The torsion apparatus moved very 
 freely when the calorimeter was not in position, and would keep 
 vibrating for some minutes by itself, but with the calorimeter there 
 was necessarily some binding. But the vibration made it so free that 
 it would return quickly to its exact position of equilibrium when drawn 
 aside, and would also quickly show any small addition to the weights. 
 This was tried in each experiment. 
 
 To measure the heat generated, we require to know the calorific 
 capacity of the whole calorimeter, and the rise of temperature which 
 would have taken place provided no heat had been lost by radiation. 
 The capacity of the calorimeter alone I have discussed elsewhere, find- 
 ing the total amount equal to -347 k. of water at ordinary tempera- 
 tures. The total capacity of the calorimeter is then A -f- -347, where 
 A is the weight of water. Hence Joule's equivalent in absolute meas- 
 ure is 
 
 T _ 
 
 ~ ( 
 
 where n is the number of revolutions of the chronograph, it making 
 one revolution to 102 of the paddles. 
 
 The corrections needed are as follows : 
 
 1st. Correction for weighing in air. This must be made to W, the 
 cast-iron weights, and to A -f- -347, the water and copper of the calori- 
 meter. If / is the density of the air under the given conditions, the 
 correction is -835 A. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 435 
 
 2d. For the weight of the tape by which the weights are hung. 
 
 rm,- "0006 
 This i 
 
 3d. For the expansion of torsion wheel, D' being the diameter at 
 20 C. This is -000018 (t" 20). Hence, 
 
 ' " 
 
 where t i' is the rise of the temperature corrected for radiation. 
 
 2. RADIATION 
 
 The correction for radiation varies, of course, with the difference of 
 temperature between the calorimeter and jacket; but, owing to the 
 rapid generation of heat, the correction is generally small in proportion. 
 The temperature generated was generally about 0-6 per minute. The 
 loss of temperature per minute by radiation was approximately -00140 
 per minute, where is the difference of the temperature. This is one 
 per cent for 10 -7, and four per cent for 14 -2. Generally, the calori- 
 meter was cooler than the jacket to start with, and so a rise of about 
 20 could be accomplished without a rate of correction at any point 
 of more than four per cent, and an average correction of less than two 
 per cent. An error of ten per cent is thus required in the estimation 
 of the radiation to produce an average error of 1 in 500, or 1 in 250 
 at a single point. The coefficients never differ from the mean more 
 than about two per cent. The observations on the equivalent, being 
 at a great variety of temperatures, check each other as to any error in 
 the radiation. 
 
 The losses of heat which I place under the head of radiation include 
 conduction and convection as well. I divide the losses of heat into the 
 following parts: 1st. Conduction down the shaft; 2d. Conduction by 
 means of the suspending wires or vulcanite points to the wheel above; 
 3d. True radiation; 4th. Convection by the air. To get some idea of 
 the relative amounts lost in this way, we can calculate the loss by 
 conduction from the known coefficients of conduction, and we can get 
 some idea of the relative loss from a polished surface from the experi- 
 ments of Mr. Nichol. In this way I suppose the total coefficient of 
 radiation to be made up approximately as follows: 
 
 Conduction along shaft ............ -00011 
 
 Conduction along suspending wires. . . . -00006 
 
 True radiation .................... -00017 
 
 Convection ........................ -00106 
 
 Total . -00140 
 
436 HENEY A. EOWLAND 
 
 The conduction through the vulcanite only amounts to -0000002. 
 
 From this it would seem that three-fourths of the loss is due to 
 radiation and convection combined. 
 
 The last two losses depend upon the difference of temperature be- 
 tween the calorimeter and the jacket, but the first two upon the differ- 
 ence between the calorimeter and frame of the machine and the wheel 
 respectively. The frame was always of very nearly the same tempera- 
 ture as the water jacket, but the wheel was usually slightly above it. 
 At first its temperature was noted by a thermometer, and the loss to 
 it computed separately; but it was found to be unnecessary, and finally 
 the whole was assumed to be a function of the temperature of the 
 calorimeter and of the jacket only. 
 
 At first sight it might seem that there was a source of error in 
 having a journal so near the bottom of the calorimeter, and joined to 
 it by a shaft. But if we consider it a moment, we shall see that the 
 error is inappreciable; for even if there was friction enough in the 
 journal to heat it as fast as the calorimeter, it would decrease the 
 radiation only seven per cent, or make an average error in the experi- 
 ment of only 1 in 700. But, in fact, the journal was very perfectly 
 made, and there was no strain on it to produce friction; besides which, 
 it was connected to a large mass of cast-iron which was attached to 
 the base. Hence, as a matter of fact, the journal was not appreciably 
 warmer after running than before, although tested by a thermometer. 
 The difference could not have been more than a degree or so at most. 
 
 The warming of the wheel by conduction and of the journal by fric- 
 tion would tend to neutralize each other, as the wheel would be warmer 
 and the journal cooler during the radiation experiment than the fric- 
 tion experiment. 
 
 The usual method of obtaining the coefficient of radiation would be 
 to stop the engine while the calorimeter was hot, and observe the 
 cooling, stirring the water occasionally when the temperature was read. 
 This method I used at first, reading the temperature at intervals of 
 about a half to a whole hour. But on thinking the matter over, it 
 became apparent that the coefficient found in this way would be too 
 small, especially at small differences of temperature; for the layer 
 next to the outside would be cooled lower than the mean temperature, 
 and the heat could only get to the outside by conduction through the 
 water or by convection currents. 
 
 Hence I arranged the engine so as to run the paddles very slowly, 
 so as to stir the water constantly, taking account of the number of 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 437 
 
 the revolutions and the torsion, so as to compute the work. As I had 
 foreseen, the results in this case were higher than by the other method. 
 At low temperatures the error of the first method was fifteen per cent; 
 but at high, it did not amount to more than about three to five per 
 cent, and probably at very high temperatures it would almost vanish. 
 
 I do not consider it necessary to give all the details of the radiation 
 experiments, but will merely remark that, as the calorimeter was nickel- 
 plated, and as seventy-five per cent of the so-called radiation is due 
 to convection by the air, the coefficients of radiation were found to be 
 very constant under similar conditions, even after long intervals of 
 time. 
 
 The experiments were divided into two groups; one when the tem- 
 perature of the jacket was about 5 C., and the other when it averaged 
 about 20 C. 
 
 The results were then plotted, and the mean curve drawn through 
 them, from which the following coefficients were obtained. These 
 coefficients are the loss of temperature per minute, and per degree 
 difference of temperature. 
 
 TABLE XXXV.* COEFFICIENTS OF RADIATION. 
 
 Difference be- 
 tween Jacket and 
 Calorimeter. 
 
 Jacket 5. 
 
 Jacket 20. 
 
 o 
 
 5 
 
 00138 
 
 00134 
 
 
 
 00135 
 
 00130 
 
 + 5 
 
 00137 
 
 00132 
 
 10 
 
 00142 
 
 00138 
 
 15 
 
 00148 
 
 00144 
 
 20 
 
 00154 
 
 00150 
 
 25 
 
 00158 
 
 .00154 
 
 As the quantity of water in the calorimeter sometimes varied slightly, 
 the numbers should be modified to suit, they being true when the total 
 capacity of the calorimeter was 8-75 kil. The total surface of the 
 calorimeter was about 2350 sq. cm., and the unit of time one minute. 
 To compare my results with those of McFarlane and of Nichol given 
 in the Proc. K. S. and Proc. R. S. E., I will reduce my results so that 
 they can be compared with the tables given by Professor Everett in his 
 ' Illustrations of the Ccntimeter-Gramme-Second System of Units/ 
 pp. 50, 51. 
 
 * [There is no table numbered XXXIV.] 
 
438 
 
 HENRY A. ROWLAND 
 
 The reducing factor is -0621, and hence the last results for the jacket 
 at 20 C. become: 
 
 TABLE XXXVI. 
 
 Difference of 
 Temperature. 
 
 Coefficient of Radia- 
 tion on the C. G. S. 
 
 System. 
 
 McFarlane's 
 Value. 
 
 Ratio. 
 
 8 
 
 000081 
 
 000168 
 
 2-07 
 
 5 
 
 000082 
 
 000178 
 
 2-17 
 
 10 
 
 000086 
 
 000186 
 
 2-16 
 
 15 
 
 000089 
 
 000193 
 
 2-17 
 
 20 
 
 000093 
 
 000201 
 
 2-16 
 
 25 
 
 000096 
 
 000207 
 
 2.15 
 
 The variation which I find is almost exactly that given by McFar- 
 lane, as is shown by the constancy of the column of ratios. But my 
 coefficients are less than half those of McFarlane. This may possibly 
 be due to the fact that the walls of McFarlane's enclosure were black- 
 ened, and to his surface being of polished copper and mine of polished 
 nickel: his surface may also have been better adapted by its form to 
 the loss of heat by convection. The results of Nichol are also much 
 lower than those of McFarlane. 
 
 The fact that the coefficients of radiation are less with increased 
 temperature of jacket is just contrary to what Dulong and Petit found 
 for radiation. But as I have shown that convection is the principal 
 factor, I am at a loss to check my result with any other observer. 
 Dulong and Petit make the loss from convection dependent only upon 
 the difference of temperature, and approximately upon the square root 
 of the pressure of the gas. Theoretically it would seem that the loss 
 should be less as the mean temperature rises, seeing that the air be- 
 comes less dense and its viscosity increases. Should we substitute 
 density for pressure in Dulong's law, we should have the loss by con- 
 vection inversely as the square root of the mean absolute temperature, 
 or approximately the absolute temperature of the jacket. This would 
 give a decrease of one per cent in the radiation for about 6, which is 
 not far from what I have found. 
 
 To estimate the accuracy with which the radiation has been obtained 
 is a very difficult matter, for the circumstances in the experiment are 
 not the same as when the radiation was obtained. In the first place, 
 although the water is stirred during the radiation, yet it is not stirred 
 so violently as during the experiment. Further, the wheel above the 
 calorimeter is warmer during radiation than during the experiment. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 439 
 
 Both these sources of error tend to give too small coefficients of radia- 
 tion, and this is confirmed by looking over the final tables. But I have 
 not felt at liberty to make any corrections based on the final results, as 
 that would destroy the independence of the observations. But we are 
 able thus to get the limits of the error produced. 
 
 During the preliminary experiments a water jacket was not used, 
 but only a tin case, whose temperature was noted by a thermometer 
 above and below. The radiation under these circumstances was larger, 
 as the case was not entirely closed at the bottom, and so permitted more 
 circulation of air. 
 
 3. CORRECTIONS TO THERMOMETERS, ETC. 
 
 Among the other corrections to the temperature as read off from 
 the thermometers, the correction for the stem at the temperature of 
 the air is the greatest. The ordinary formula for the correction is 
 000156n( t"). But, in applying this correction, it is difficult to 
 estimate n, the number of degrees of thermometer outside the calo- 
 rimeter and at the temperature of the air, seeing that part of the stem 
 is heated by conduction. The uncertainty vanishes as the thermometer 
 becomes longer and longer, or rather as it is more and more sensitive. 
 But even then some of the uncertainty remains. I have sought to 
 avoid this uncertainty by placing a short tube filled with water about 
 the lower part of the thermometer as it comes out of the calorimeter. 
 The temperature of this was indicated by a thermometer, by aid of 
 which also the heat lost to the water by conduction through the ther- 
 mometer stem could be computed; this, however, was very minute com- 
 pared with the whole heat generated, say 1 in 10,000. 
 
 The water being very nearly at the temperature of the air, the stem 
 above it could be assumed to be at the temperature of the air indicated 
 by a thermometer hung within an inch or two of it. The correction for 
 stem would thus have to be divided into two parts, and calculated 
 separately. Calculated in this way, I suppose the correction is perfectly 
 certain to much less than one hundredth of a degree : the total amount 
 was seldom over one-tenth of a degree. 
 
 Among the uncertain errors to which the measurement of tempera- 
 ture is subjected, I may mention the following: 
 
 1. Pressure on bulb. A pressure of 60 cm. of water produced a 
 change of about 0-01 in the thermometers. When the calorimeter 
 was entirely closed there was soon some pressure generated. Hence 
 the introduction of the safety-tube, a tube of thin glass about 10 cm. 
 
440 HENRY A. EOWLAXD 
 
 long, extending through a cork in the top of the calorimeter. The top 
 of the safety-tube was nearly closed by a cork to prevent evaporation. 
 Had the tube been shorter, water would have been forced out, as well 
 as air. 
 
 2. Conduction along stem from outside to thermometer bulb. To 
 avoid this, not only was the bulb immersed, but also quite a length of 
 stem. As this portion of the stem, as also the bulb, was surrounded 
 by water in violent motion, there could have been no large error from 
 this source. The immersed stem to the top of the bulb was generally 
 about 5 cm. or more, and the stem only about -8 cm. in diameter. 
 
 3. The thermometer is never at the temperature of the water, be- 
 cause the latter is constantly rising; but we do not assume that it is 
 so in the experiment. We only assume that it lags behind the water 
 to the same amount at all parts of the experiment, and this is doubt- 
 less true. 
 
 To see if the amount was appreciable, I suddenly threw the apparatus 
 out of gear, thus stopping it. The temperature was observed to con- 
 tinue rising about 0-02 C. Allowing 0-01 for the rise due to motion 
 after the word "Stop" was given, we have about 0-01C. as the 
 amount the thermometer lagged behind the water. 
 
 4. Evaporation. A possible source of error exists in the cooling of 
 the calorimeter by evaporation of water leaking out from it. 
 
 The water was always weighed before and after the experiment in 
 a balance giving -i. gramme with accuracy. The normal amount of 
 loss from removal of thermometer, wet corks, &c., was about 1 gramme. 
 The calorimeter was perfectly tight, and had no leakage at any point 
 in its normal state. Once or twice the screws of the stuffing-box 
 worked loose, but these experiments were rejected. 
 
 The evaporation of 1 gramme of water requires about 600 heat units, 
 which is sufficient to depress the temperature of the calorimeter about 
 0-07 C. As the only point at which evaporation could take place was 
 through a hole less than 1 mm. diameter in the safety-tube, I think it 
 is reasonable to assume that the error from this source is inappreciable. 
 But to be doubly certain, I observed the time which drops of water of 
 known weight and area, placed on the warm calorimeter, took to dry. 
 From these experiments it was evident that it would require a consid- 
 erable area of wet surface to produce an appreciable effect. This wet 
 surface never existed unless the calorimeter was wet by dew deposited 
 on the cool surface. To guard against this error, the calorimeter was 
 never cooled so low that dew formed; it was carefully rubbed with a 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 441 
 
 towel, and placed in the apparatus half an hour to an hour before the 
 experiment, exposed freely to the air. The surface being polished, the 
 slightest deposit of dew was readily visible. The greatest care was 
 taken to guard against this source of error, and I think the experiment 
 is free from it. 
 
 (d.) Results 
 1. CONSTANT DATA 
 
 Joule's equivalent in gravitation measure is of the dimensions of 
 length only, being the height which water would have to fall to be 
 heated one degree. Or let water flow downward with uniform velocity 
 through a capillary tube impervious to heat; assuming the viscosity 
 constant, the rate of variation of height with temperature will be 
 Joule's equivalent. 
 
 Hence, besides the force of gravity the only thing required in abso- 
 lute measure is some length. The length that enters the equation 
 is the diameter of the torsion wheel. This was determined under a 
 microscope comparator by comparison with a standard metre belong- 
 ing to Professor Eogers of Harvard Observatory, which had been 
 compared at Washington with the Coast Survey standards, as well as 
 by comparison with one of our own metre scales which had also been 
 so compared. The result was -26908 metre at 20 C. 
 
 To this must be added the thickness of the silk tape suspending the 
 weights. This thickness was carefully determined by a micrometer 
 screw while the tape was stretched, the screw having a flat end. The 
 result was -00031 m. 
 
 So that, finally, D' ~ -26939 metre at 20 C. Separating the con- 
 stant from the variable parts, the formula now becomes 
 
 JL = j*6-324^ ^ + .ooooiS 0" - 20) + * 
 
 g = 9-8005 at Baltimore. 
 
 It is unnecessary to have the weights exact to standard, provided they 
 are relatively correct, or to make double weighings, provided the same 
 scale of the balance is always used. For both numerator and denomi- 
 nator of the fraction contain a weight. 
 
 2. EXPEBIMENTAL DATA AND TABLES OF RESULTS 
 
 In exhibiting the results of the experiments, it is much more satisfac- 
 tory to compute at once from the observations the work necessary to 
 raise 1 kil. of the water from the first temperature observed to each sue- 
 
442 HENRY A. EOWLAND 
 
 ceeding temperature. By interpolation in such a table we can then 
 reduce to even degrees. To compare the different results I have then 
 added to each table such a quantity as to bring the result at 20 about 
 equal to 10,000 kilogramme-metres. 
 
 The process for each experiment may be described as follows. The 
 calorimeter was first filled with distilled water a little cooler than the 
 atmosphere, but not so cool as to cause a deposit of dew. It was then 
 placed in the machine and adjusted to its position, though the outer half 
 of the jacket was left off for some time, so that the calorimeter should 
 become perfectly dry; to aid which the calorimeter was polished with a 
 cloth. The thermometer and safety-tube were also inserted at this 
 time. 
 
 After half an hour or so, the chronograph was adjusted, the outer half 
 of the jacket put in place, the wooden screen fixed in position, and all 
 was ready to start. The engine, which had been running quietly for 
 some time, was now attached, and the experiment commenced. First the 
 weights had to be adjusted so as to produce equilibrium as nearly as 
 possible. 
 
 The observers then took their positions. One observer constantly 
 recorded the transit of the mercury over the divisions of thermometer, 
 making other suitable marks, so that the divisions could be afterwards 
 recognized. He also read the thermometers giving the temperatures 
 of the air, the bottom of the calorimeter thermometer, and of the wheel 
 just above the calorimeter; and sometimes another, giving that of the 
 cast-iron frame of the instrument. 
 
 The other observer read the torsion wheel once every revolution of 
 the chronograph cylinder, recording the time by his watch. He also 
 recorded on the chronograph every five minutes by his watch, and like- 
 wise stirred the water in the jacket at intervals, and read its temper- 
 ature. 
 
 The recording of the time was for the purpose of giving the connect- 
 ing link between the readings of the torsion circle and of the ther- 
 mometer. This, however, as the readings were quite constant, had 
 only to be done roughly, say to half a minute of time, though the rec- 
 ords of time on the chronograph were true to about a second. 
 
 The thermometers to read the temperature of the water in the jacket 
 were graduated to 0-2 C., but were generally read to 0-1 C., and had 
 been compared with the standards. There was no object in using more 
 delicate thermometers. 
 
 After the experiment had continued long enough, the engine was 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 443 
 
 stopped and a radiation experiment begun. The last operation was to 
 weigh the calorimeter again, after removing the thermometer and safety 
 tube, and also the weights which had been used. 
 
 The chronograph sheet, having then been removed from the cylin- 
 der, had the time records identified and marked, as well as the ther- 
 mometer records. Each line of the chronograph record was then num- 
 bered arbitrarily, and a table made indicating the stand of the ther- 
 mometer and the number of the revolutions and fractions of a revolu- 
 tion as recorded on the chronograph sheet. The times at which these 
 temperatures were reached was also found by interpolation, and re- 
 corded in another column. 
 
 From the column of times the readings of the torsion circle could be 
 identified, and so all the necessary data would be at hand for calculating 
 the work required to raise the temperature of one kilogramme of the 
 water from the first recorded temperature to any succeeding tempera- 
 ture. 
 
 As these temperatures usually contained fractions, the amount of 
 work necessary to raise one kilogramme of the water to the even degrees 
 could then be found from this table by interpolation. Joule's equiva- 
 lent at any point would then be merely the difference of any two suc- 
 ceeding numbers; or, better, one tenth the difference of two numbers 
 situated 10 apart, or, in general, the difference of the numbers divided 
 by the difference of the temperatures. 
 
 It would be a perfectly simple matter to make the record of the tor- 
 sion circle entirely automatic, and I think I shall modify the apparatus 
 in that manner in the future. 
 
 It would take too much space to give the details of each experiment; 
 but, to show the process of calculation, I will give the experiment of 
 Dec. 17, 1878, as a specimen. The chronograph sheet, of course, I 
 cannot give. The computation is at first in gravitation measure, but 
 afterwards reduced to absolute measure. 
 
 The calorimeter before the experiment weighed 12-2733 kil. 
 The calorimeter after the experiment weighed 12-2716 kil. 
 
 Mean 12-2720 kil. 
 Weight of calorimeter alone 3-8721 kil. 
 
 . . Water alone weighed 8-3999 kil. 
 
 3470 kil. 
 
 Total capacity 8-7469 kil. 
 
444 HENRY A. ROWLAND 
 
 The correction for weighing in air was -835 / -00106. 
 The total term containing the correction is therefore -99878. 
 
 log 86-324 =1-9361316 
 
 log -99878 = 1-9994698 
 
 1-9356014 
 
 log 8-7469 = -9418542 
 
 log const, factor = -9937472 = log 9-85706. 
 
 Hence the work per kilogramme is 9-85706 S~Wn in gravitation 
 measure, the term 2'Wn being used to denote the sum of products 
 similar to Wn as obtained by simultaneous readings of torsion circle 
 and records on chronograph sheet. 
 
 Zero of torsion wheel, 79-3 mm. 
 
 Value of 1 mm. on torsion wheel -0118 kil. 
 
 The following were the records of time on the chronograph sheet : 
 
 Time observed. Revolutions of Chronograph. Time calculated. 
 
 15 8-74 15-2 
 
 20 25-32 20-1 
 
 25 42-10 25-0 
 
 30 59-05 30-0 
 
 35 76-00 35-0 
 
 40 93-03 40-0 
 
 45 109-97 45-0 
 
 50 126-92 50-0 
 
 55 144.14 55-0 
 
 The times were calculated by the formula 
 
 Time = -294 X Revolutions + 12-66, 
 
 which assumes that the engine moves with uniform velocity. As the 
 principal error in using an incorrect interpolation formula comes from 
 the calculation of the radiation, and as this formula is correct within 
 a few seconds for all the higher temperatures, we can use it in the cal- 
 culation of the times. 
 
 The records of the transits of the mercury over the divisions of the 
 thermometer were nearly always made for each division, but it is use- 
 less to calculate for each. I usually select the even centimeters, and 
 take the mean of the records for several divisions on each side. 
 
 While the mercury was rising 1 cm. on No. 6163, there would be 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 445 
 
 about seven revolutions of the chronograph, and consequently seven 
 readings of the torsion circle, each one of which was the average for a 
 little time as estimated by the eye. 
 
 I have obtained more than thirty series of results, but have thus far 
 reduced only fourteen, five of which are preliminary, or were made with 
 the simple jacket instead of the water jacket, the radiation to which 
 was much greater, as there was a hole at the bottom which allowed more 
 circulation of the air. The mean of the preliminary results agrees so 
 closely with the mean of the final results, that I have in the end given 
 them equal weight. 
 
 On March 24th, the same thermometer was used for a second experi- 
 ment directly after the first, seeing that the chronograph failed to work 
 in the first experiment until 8 was reached. The error from this cause 
 was small, as the first experiment only reached to 26 C., and hence 
 there could have been no change of zero, as this is very nearly the tem- 
 perature at which the thermometer was generally kept. 
 
 Having thus calculated the work in conjunction with the tempera- 
 ture, I have next interpolated so as to obtain the work at the even de- 
 grees. The tables so formed I have combined in two ways : first, I have 
 added to the column of work in each table an arbitrary number, such as 
 to make the work at 20 about 10,000, and have then combined them as 
 seen in Table LI, and, secondly, I have subtracted each number from 
 the one 10 farther down the table, and divided the numbers so found 
 by 10, thus obtaining the mechanical equivalent of heat. 
 
 In these tables four thermometers have been used, and yet they were 
 so accurate that little difference can be observed in the experiments 
 which can be traced to an error of the thermometer, although the Kew 
 standard has some local irregularities. The greatest difference between 
 any column of Table LI and the general mean is only 10 kilogramme- 
 metres, or 0-023 degree, and this includes all errors of calibration of 
 thermometers, radiation, &c. This seems to me to be a very remarkable 
 result, and demonstrates the surpassing accuracy of the method. In- 
 deed, the limit of accuracy in thermometry is the only limit which we 
 can at present give to this method of experiment. Hence the large 
 proportional time spent on that subject. 
 
 The accuracy of the radiation is demonstrated, to some extent, by 
 the agreement of the results obtained even with different temperatures 
 of the jacket. But on close observation it seems apparent that the 
 coefficients of radiation should be further increased as there is a ten- 
 dency of the end figures in each series to become too high. This is 
 
446 HENEY A. ROWLAND 
 
 exactly what we should suppo&e, as we have seen that nearly all sources 
 of error tend in the direction of making the radiation too small. For 
 instance, an error came from not stirring the water during the radiation, 
 and there must be a small residual error from not stirring so fast 
 during radiation as during the experiment. Besides this, some parts 
 around the calorimeter were warm during the radiation which were cool 
 during the experiment. And both of these make the correction for 
 radiation too small. However, the error from this source is small, and 
 cannot possibly affect the general conclusions. In each column of 
 Tables LI and LII a dash is placed at the temperature of the jacket, 
 and for fifteen degrees below this point the error in the radiation must 
 produce only an inappreciable error in the equivalent: taking the ob- 
 servations within this limit as the standards, and rejecting the others, 
 we should still arrive at very nearly the same conclusions as if we ac- 
 cepted the whole. 
 
 Most of the experiments are made with a weight of about 7-3 kil., as 
 everything seemed to work best with this weight But for the sake 
 of a test I have run the weight up to 8-6 and down to 4-4 kil., by which 
 the rate of generation of the heat was changed nearly three times. 
 By this the correction for the radiation and the error due to the irregu- 
 larity of the engine are changed, and yet scarcely an appreciable differ- 
 ence in the results can be observed. 
 
 The tables explain themselves very well, but some remarks may be 
 in order. Tables XXXVII to L inclusive are the results of fourteen 
 experiments selected from the total of about thirty, the others not hav- 
 ing been worked up yet, though I propose to do so at nry leisure. 
 
 Table LI gives the collected results. At the top of each column the 
 date of the experiment and number of the thermometer are given, to- 
 gether with the approximate torsion weight and the rate of rise of tem- 
 perature per hour. The dash in each column gives approximately the 
 temperature of the jacket, and hence of the air. There are four col- 
 umns of mean values, but the last, produced from the combination of 
 the table by parts, is the best. 
 
 Table LII gives the mechanical equivalent of heat as deduced from 
 intervals of 10 on Table LI. The selection of intervals of 10 tends 
 to screen the variation of the specific heat of water from view, but a 
 smaller interval gives too many local irregularities. In taking the 
 mean I have given all the observations equal weight, but as the Kew 
 standard was only graduated to -J F. it was impossible to calibrate it 
 so accurately as to avoid irregularities of 0-02C. which would affect 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 
 
 447 
 
 the quantities 1 in 500. Hence, in drawing a curve through the results, 
 as given in the last column, I have almost neglected the Kew, and have 
 otherwise sought to draw a regular curve without points of inflection. 
 The figures in the last column I consider the best. 
 
 Table LIII takes the mean values as found in Tables LI and LII, 
 and exhibits them with respect to the temperatures on the different 
 thermometers, to the different parts of the earth, and also gives the 
 reduction to the absolute scale. I am inclined to favor the absolute 
 scale, using ra= -00015, as given in the Appendix to Thermometry, 
 rather than -00018, as used throughout the paper. 
 
 Table LIV gives what T consider the final result of the experiment. 
 It is based on the result ra= -00015 for the thermometers, and is cor- 
 rected for the irregularity of the engine by adding 1 in 4000. 
 
 The minor irregularities are also corrected so that the results signify 
 a smooth curve, without irregularity or points of contrary flexure. 
 But the curve for the work does not differ more than three kilogramme- 
 metres from the actual experiment at any point, and generally coincides 
 with it to about one kilogramme-metre. These differences signify 
 0-007 C. and 0-002 C., respectively. The mechanical equivalent is 
 for single degrees rather than for ten degrees, as in the other tables. 
 
 TABLE XXXVII. FIRST SERIES. Preliminary. 
 January 16, 1878. Jacket and Air about 14 C. 
 
 h 
 
 
 
 
 
 s* 
 
 jg 
 
 
 j 
 
 2 
 
 
 
 id 
 
 
 Correction. 
 
 
 if 
 
 
 
 ^ 
 
 S 
 
 ~ = 
 IS 
 
 & 
 
 P* 
 
 
 
 It 
 
 t 
 
 5 8 s 
 3 C 
 
 15 
 
 
 
 A 
 
 
 
 l 
 
 ||1 
 
 
 
 -= 
 
 
 S 
 P 
 
 00 
 
 c 
 
 
 8| 
 
 >2 
 
 y 
 
 
 
 S 
 
 *s 
 
 S 
 
 1 
 
 *5 
 
 2 
 
 
 
 
 
 
 
 
 
 
 
 
 
 140 
 
 52-0 
 
 005 
 
 
 
 9-185 
 
 5-485 
 
 7 "iflQ 
 
 
 
 
 
 
 160 
 180 
 203 
 220 
 240 
 
 56-0 
 59-2 
 63-4 
 66-5 
 70-2 
 
 003 
 
 + 006 
 + 011 
 + 020 
 
 017 
 022 
 015 
 001 
 + 027 
 
 11-412 
 13-650 
 16-230 
 18-137 
 20-392 
 
 18-023 
 30-652 
 45-329 
 56-241 
 69-153 
 
 7-478 
 7-442 
 7-394 
 7-364 
 7. 3^4. 
 
 951 
 1906 
 3010 
 3825 
 4786 
 
 io 
 11 
 
 12 
 13 
 14 
 
 348 
 775 
 1202 
 1629 
 2056 
 
 5728 
 6155 
 6582 
 7009 
 7436 
 
 259 
 
 74-0 
 
 + 028 
 
 + 067 
 
 22-538 
 
 81-484 
 
 
 5702 
 
 15 
 
 2484 
 
 7864 
 
 289 
 
 80-0 
 
 + 045 
 
 + 161 
 
 25-943 
 
 101-214 
 
 
 7156 
 
 16 
 
 2912 
 
 8292 
 
 
 
 
 
 
 
 
 
 17 
 
 3340 
 
 8720 
 
 
 
 
 
 
 
 
 
 18 
 
 3767 
 
 9147 
 
 
 
 
 
 
 
 
 
 19 
 
 4193 
 
 9573 
 
 
 
 
 
 
 
 
 
 20 
 
 4619 
 
 9999 
 
 
 
 
 
 
 
 
 
 21 
 
 5048 
 
 10428 
 
 
 
 
 
 
 
 
 
 22 
 
 5472 
 
 10852 
 
 
 
 
 
 
 
 
 
 23 
 
 5899 
 
 11279 
 
 
 
 
 
 
 
 
 
 24 
 
 6326 
 
 11706 
 
 
 
 
 
 
 
 
 
 25 
 
 6753 
 
 12133 
 
 
 
 
 
 
 
 
 
 
 26 
 
 7180 
 
 12560 
 
 
 
 
 
 
 
448 
 
 HENRY A. ROWLAND 
 
 TABLE XXXVIII SECOND SERIES. Preliminary. 
 
 March 7, 1878. Jacket 18.5 to 22. 5. Air about 21 C. 
 
 Thermometer 
 No. 6163. 
 
 
 
 e 
 
 R 
 
 Correction. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 2n. 
 
 Mean Weight 
 W. 
 
 Work per Kilo- 
 gramme = 
 2 10-060 Wn. 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 + 6812 
 
 S 
 
 
 
 i 
 
 f6 
 
 170 
 180 
 190 
 200 
 210 
 220 
 230 
 240 
 250 
 260 
 270 
 280 
 290 
 300 
 310 
 320 
 330 
 340 
 350 
 360 
 370 
 380 
 390 
 
 19-9 
 
 016 
 
 
 
 12-537 
 13-646 
 14-755 
 15-863 
 16-972 
 18-085 
 19-196 
 20-305 
 21-419 
 22 533 
 23-642 
 24-754 
 25-867 
 26-990 
 28-119 
 29-253 
 30-393 
 31 540 
 32-689 
 33-842 
 34-998 
 36-158 
 37-321 
 
 5-03 
 11-12 
 17-22 
 23-36 
 29-55 
 35-70 
 41-90 
 48-09 
 54-30 
 
 7-737 
 7-710 
 7.666 
 7-642 
 7-641 
 7.630 
 7.611- 
 7.600 
 7.596 
 7.582 
 7.552 
 7.547 
 7.576 
 7-611 
 7-604 
 7-611 
 7-617 
 7-602 
 7-592 
 7-576 
 7-550 
 7-550 
 
 
 474 
 947 
 1421 
 1897 
 2369 
 2845 
 3319 
 3794 
 
 4740 
 5213 
 5687 
 6164 
 6643 
 7125 
 7608 
 8097 
 8590 
 9081 
 9576 
 10071 
 10567 
 
 18 
 
 14 
 15 
 16 
 17 
 18 
 19 
 20 
 21 
 22 
 23 
 24 
 25 
 26 
 27 
 28 
 29 
 30 
 31 
 32 
 33 
 34 
 35 
 36 
 37 
 
 198 
 625 
 1052 
 1480 
 1909 
 2333 
 2761 
 3189 
 3615 
 4041 
 4467 
 4892 
 5318 
 5744 
 6168 
 6593 
 7017 
 7441 
 7867 
 8294 
 8722 
 9149 
 9577 
 10004 
 10430 
 
 7010 
 7437 
 7864 
 8292 
 8721 
 9145 
 9573 
 10001 
 10427 
 10853 
 11279 
 11704 
 12130 
 12556 
 12980 
 13405 
 13829 
 14253 
 14679 
 15106 
 15534 
 15961 
 16389 
 16816 
 17242 
 
 
 
 
 
 
 
 26-8 
 
 010 
 
 .036 
 
 
 
 
 
 
 
 33.8 
 
 + .003 
 
 036 
 
 
 
 
 66-69 
 72-92 
 79-16 
 85-42 
 91-67 
 97-98 
 104-28 
 110-67 
 117-12 
 123-54 
 130-04 
 136-56 
 143-08 
 
 
 
 
 40-8 
 
 + 0-20 
 
 001 
 
 
 
 
 
 
 
 47-8 
 
 + 044 
 
 + 073 
 
 51-4 
 
 
 
 
 
 55-0 
 
 + 072 
 
 + 184 
 
 58-7 
 
 + 588 
 
 + 261 
 
 
 
 
 
 
 
 
 
 
 
 
 
 TABLE XXXIX THIRD SERIES. Preliminary. 
 March 12, 1878. Jacket 13-2 to 16-6. Air about 15 C. 
 
 Thermometer 
 No. 6166. 
 
 
 S 
 H 
 
 Correction. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 
 2n. 
 
 4(1 Mean Weight 
 W. 
 
 Work per 
 Kilogramme 
 = 2 9-9690 Wn. 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 + 7599. 
 
 S 
 
 I 
 
 i 
 
 
 
 205 
 210 
 220 
 230 
 
 28-0 
 28-6 
 29-9 
 31-1 
 
 
 
 
 
 + -002 
 
 14-368 
 14-754 
 15-529 
 16-307 
 
 3-156 
 5-334 
 
 9-770 
 14-184 
 
 U-5167 
 
 
 164 
 495 
 
 827 
 
 
 
 
 
 15 
 
 16 
 
 17 
 
 269 
 696 
 1122 
 
 7868 
 8295 
 8721 
 
 + 003 
 
 + 010 
 
 45 In the calculation of this column, more exact data were used than given in the 
 other two columns, seeing that the original calculation was made every 5 mm. of the 
 thermometer. Hence the last figure may not always agree with the rest of the data. 
 
 46 As this table was originally calculated for every 5 mm. on the thermometer, I 
 have given the weights which were used to check the more exact calculation. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 449 
 
 TABLE XXXIX. Continued. 
 
 Thermometer 
 No. 6106. 
 
 i 
 
 EH 
 
 Correction. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 
 2n. 
 
 Mean Weight 
 W. 
 
 Work per 
 Kilogramme 
 = 2 9-690 TFn. 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 + 7599. 
 
 1 
 
 
 
 I 
 
 240 
 
 250 
 260 
 270 
 280 
 290 
 300 
 310 
 320 
 330 
 340 
 350 
 360 
 370 
 380 
 390 
 400 
 410 
 420 
 
 32-4 
 33-6 
 34-9 
 36-2 
 37-4 
 38-7 
 39 9 
 41-2 
 42-5 
 43-7 
 45-0 
 46-3 
 47-6 
 48-9 
 50-1 
 51-4 
 52-7 
 54-0 
 55-3 
 
 
 
 17-090 
 17-875 
 18-662 
 19-452 
 20-242 
 21-029 
 21-825 
 22-619 
 23-418 
 24-220 
 25-023 
 28-825 
 26-628 
 27-438 
 28-253 
 29-069 
 29-884 
 30-703 
 31-519 
 
 18-642 
 23-080 
 27-550 
 32-014 
 36-474 
 40-924 
 45-424 
 49-838 
 54-302 
 58-844 
 63-366 
 67.874 
 72-403 
 76-987 
 81-550 
 86-100 
 90-720 
 95-316 
 99-920 
 
 (.7-5462 
 (.7 -5668 
 (.7-5875 
 V 7- 5763 
 (.7-5872 
 (.7-5801 
 
 1160 
 1495 
 1831 
 2167 
 2504 
 2840 
 3179 
 3514 
 3853 
 4194 
 4536 
 4876 
 5219 
 5565 
 5910 
 6255 
 6604 
 6951 
 7299 
 
 o 
 
 18 
 19 
 20 
 21 
 22 
 23 
 24 
 25 
 26 
 27 
 28 
 29 
 30 
 31 
 
 1548 
 1975 
 2401 
 2828 
 3253 
 3676 
 4101 
 4526 
 4951 
 5378 
 5803 
 6226 
 6653 
 7078 
 
 9147 
 9574 
 10000 
 10427 
 10852 
 11275 
 11700 
 12125 
 12550 
 12977 
 13402 
 13825 
 14252 
 14677 
 
 + 009 
 
 + -021 
 
 + 014 
 
 + 038 
 
 + 019 
 
 + 055 
 
 + 024 
 
 + 089 
 
 + 030 
 
 + 120 
 
 + 038 
 
 + 159 
 
 + 047 
 
 + 202 
 
 + 056 
 
 + 251 
 
 
 
 
 
 
 
 + 066 
 
 + 304 
 
 
 
 
 
 
 
 TABLE XL. FOUBTH SERIES. Preliminary." 
 March 24, 1878. Jacket 5-4 to 8 -2. Air about 6 C. 
 
 Thermometer 
 No. 6163. 
 
 I 
 
 B 
 
 Correction. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 
 In. 
 
 Mean Weight 
 W. 
 
 o.e 
 
 y* 
 
 ft|o 
 
 LJ 03 T 1 
 
 * tHCO 
 SH >s^ 
 
 .2 & 
 *|M 
 
 *l 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 + 4903. 
 
 a 
 
 2 
 
 en 
 
 1 
 
 130 
 140 
 150 
 160 
 170 
 180 
 190 
 200 
 210 
 220 
 230 
 240 
 250 
 260 
 270 
 280 
 290 
 
 27 ; 4 
 29-2 
 31-0 
 32-9 
 34-7 
 36-6 
 38-4 
 40-3 
 42-2 
 44-2 
 46-1 
 
 + 002 
 
 
 
 8-071 
 9-204 
 10-340 
 11-480 
 12-620 
 13-763 
 14-908 
 16-054 
 17-202 
 18-350 
 19-504 
 
 42-364 
 48-898 
 55-438 
 62-066 
 68-669 
 75-330 
 81-973 
 88-597 
 95-264 
 101-941 
 108-588 
 
 7-471 
 7-446 
 7-442 
 7-405 
 7-390 
 7-398 
 7-431 
 7-429 
 7-437 
 7-433 
 
 V 7-4617 
 
 7-509 
 7-502 
 
 
 485 
 968 
 1458 
 1944 
 2433 
 2921 
 3410 
 3902 
 4395 
 4886 
 
 6855 
 7350 
 7844 
 
 O 
 
 8 
 9 
 10 
 11 
 12 
 13 
 14 
 15 
 16 
 17 
 18 
 19 
 20 
 21 
 22 
 23 
 24 
 25 
 26 
 
 -30 
 
 398 
 823 
 1252 
 1680 
 2107 
 2534 
 3960 
 3387 
 3815 
 4245 
 4672 
 5098 
 5524 
 5950 
 6376 
 6802 
 7228 
 7651 
 
 4872 
 5300 
 5725 
 6154 
 6582 
 7009 
 7436 
 8862 
 8289 
 8717 
 9147 
 9574 
 10000 
 10426 
 10852 
 11278 
 11704 
 12130 
 12553 
 
 + 010 
 
 + 019 
 
 + 017 
 
 + 050 
 
 + 025 
 
 + 093 
 
 + 034 
 
 + 150 
 
 + 046 
 
 + -222 
 
 .... 
 
 
 
 
 
 
 
 
 53-6 
 55-7 
 57-7 
 
 + 073 
 
 + 399 
 
 24-124 
 
 25-288 
 26-456 
 
 135-158 
 141-803 
 148-427 
 
 + 084 
 
 + 524 
 
 
 
 
 
 
 47 The first part of the experiments was lost, as the pen of the chronograph did 
 not work. 
 29 
 
450 
 
 HENRY A. EOWLAND 
 
 TABLE XLI. FIFTH SERIES. Preliminary. 
 March 24, 1878. Jacket 5-4 to 8-4. Air about 6C. 
 
 Thermometer 
 No. 6163. 
 
 1 
 
 H 
 
 Correction. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 
 2n. 
 
 Mean Weight 
 W. 
 
 Work per 
 Kilogramme 
 = 29-8816 Wn. 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 + 2250. 
 
 a 
 
 i 
 
 02 
 
 d 
 
 I 
 
 w 
 
 75 
 80 
 90 
 100 
 110 
 120 
 130 
 140 
 150 
 160 
 170 
 180 
 190 
 200 
 210 
 220 
 230 
 240 
 250 
 260 
 270 
 280 
 290 
 300 
 810 
 
 0-9 
 1-7 
 3-4 
 5-1 
 6-8 
 8-5 
 10-2 
 12-0 
 13-7 
 15-5 
 17-2 
 19-0 
 20-8 
 22-6 
 24-3 
 26-1 
 27-9 
 29-6 
 
 003 
 
 
 
 1-891 
 2-451 
 3-569 
 4-690 
 5-810 
 6-936 
 8-060 
 9-190 
 10-323 
 11-459 
 12-600 
 13-742 
 14-882 
 16-025 
 17-170 
 18-316 
 19-467 
 20-615 
 
 3-154 
 6-118 
 12-174 
 18-172 
 24-212 
 30-397 
 36-621 
 42-854 
 49-068 
 55 398 
 61-707 
 68-036 
 74-358 
 80-716 
 87-064 
 93-402 
 99-677 
 105-950 
 
 8-1544 
 8-0900 
 8-0409 
 8-0074 
 7-9170 
 7-8973 
 7-8786 
 7-8512 
 7-8061 
 7-7799 
 7-7622 
 7-7643 
 7-7807 
 7-8419 
 7-8468 
 7-8579 
 7-8802 
 
 (.7-8980 
 
 7-9038 
 7-9091 
 7-8979 
 7-8974 
 
 
 239 
 723 
 1200 
 1677 
 2161 
 2647 
 3132 
 3614 
 4103 
 4588 
 5073 
 5558 
 6047 
 6539 
 7030 
 7518 
 8006 
 
 9482 
 9976 
 10474 
 10974 
 11481 
 
 o 
 
 2 
 3 
 4 
 5 
 6 
 6 
 8 
 9 
 10 
 11 
 12 
 13 
 14 
 15 
 16 
 17 
 18 
 19 
 20 
 21 
 22 
 23 
 24 
 25 
 26 
 27 
 28 
 
 46 
 
 477 
 906 
 1332 
 1759 
 2189 
 2621 
 3050 
 3477 
 3905 
 4333 
 4759 
 5183 
 5608 
 6036 
 6466 
 6895 
 7320 
 7745 
 8170 
 8597 
 9024 
 9451 
 9878 
 10305 
 10733 
 11160 
 
 2296 
 2727 
 3156 
 3582 
 4009 
 4439 
 4871 
 5300 
 5727 
 6155 
 6583 
 7009 
 7433 
 7858 
 8286 
 8716 
 9145 
 9570 
 9995 
 10420 
 10847 
 11274 
 11701 
 11128 
 12555 
 12983 
 13410 
 
 002 
 
 012 
 
 
 
 017 
 
 + 003 
 
 012 
 
 + 007 
 
 + 005 
 
 + 015 
 
 + 032 
 
 + 024 
 + 028 
 
 + 068 
 + 092 
 
 + 039 
 
 + 150 
 
 + 050 
 
 + 270 
 
 
 
 
 
 
 34-9 
 36-7 
 38-5 
 40-2 
 42-1 
 
 + 069 
 
 + 351 
 
 24-072 
 25-231 
 26-395 
 27-565 
 
 28-748 
 
 124-863 
 131-181 
 137-560 
 143-972 
 150-467 
 
 + 087 
 
 + 450 
 
 + 109 
 
 + 583 
 
 
 
 
 
 
 
 
 
 
 
 TABLE XLIL SIXTH SEEIES. 
 May 14, 1878. Jacket 12-1 to 12-4. Air about 13 C. 
 
 Thermometer 
 No. 6165. 
 
 I 
 
 p 
 
 Correction. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 2n. 
 
 Mean Weight W 
 
 Work per 
 Kilogramme 
 = 2 9.9051 Wn. 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 + 5433. 
 
 a 
 s 
 
 02 
 
 i 
 
 140 
 150 
 160 
 170 
 180 
 190 
 200 
 210 
 220 
 
 46-4 
 47-9 
 49-4 
 50-9 
 52-5 
 54-0 
 55-5 
 57-0 
 58-5 
 
 002 
 
 
 
 9-319 
 10-178 
 11-032 
 11-886 
 12-740 
 13-596 
 14-454 
 15-314 
 16-174 
 
 1-93 
 7-07 
 12-19 
 17-37 
 22-52 
 27-70 
 32-88 
 38-07 
 43-29 
 
 I 7- 2291 
 17-1608 
 i 7- 1500 
 I 7-1512 
 
 
 370 
 735 
 1102 
 1467 
 1835 
 2201 
 2568 
 2938 
 
 9 
 10 
 It 
 12 
 13 
 14 
 15 
 16 
 17 
 
 137 
 293 
 721 
 1151 
 1579 
 2007 
 2434 
 2863 
 3290 
 
 5296 
 5726 
 6154 
 
 6584 
 7012 
 7440 
 7867 
 8296 
 8723 
 
 000 
 
 007 
 
 + 002 
 
 008 
 
 + 006 
 
 002 
 
 + 010 
 
 + 011 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 451 
 
 TABLE XLII. Continued. 
 
 Thermometer 
 No. 6165. 
 
 i 
 
 H 
 
 Correction. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 2n. 
 
 Mean Weight W. 
 
 gtl 
 
 S.B~ 
 
 O oos 
 
 ^5" 
 M| 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 + 5433. 
 
 a 
 
 s 
 
 
 
 1 
 
 230 
 240 
 250 
 260 
 270 
 280 
 290 
 300 
 310 
 320 
 330 
 340 
 350 
 360 
 370 
 380 
 390 
 400 
 410 
 420 
 
 60-0 
 61-6 
 
 
 
 17037 
 17-093 
 
 48-50 
 53-70 
 
 jl.7-1446 
 ]. 7-1536 
 J. 7-1230 
 [7-1344 
 \. 7-1302 
 17-1117 
 I 7 -0958 
 1^7-1076 
 '. 7-1088 
 .7-1064 
 
 3306 
 3675 
 
 4778 
 5148 
 5514 
 5878 
 6240 
 6600 
 6962 
 7319 
 7680 
 8035 
 8396 
 8754 
 9115 
 9475 
 9833 
 10192 
 
 o 
 18 
 19 
 20 
 21 
 22 
 23 
 24 
 25 
 26 
 27 
 28 
 29 
 30 
 31 
 32 
 83 
 
 3716 
 4142 
 4567 
 4993 
 5420 
 5846 
 6271 
 6696 
 7121 
 7547 
 7973 
 8400 
 8829 
 9259 
 9678 
 10096 
 
 9149 
 9575 
 10000 
 10426 
 10853 
 11279 
 11704 
 12129 
 12554 
 12980 
 13406 
 13833 
 14262 
 14692 
 15111 
 15529 
 
 + 015 
 
 + 031 
 
 
 
 
 
 
 66-2 
 67-7 
 69-2 
 70-7 
 72-2 
 73-7 
 75-2 
 76-2 
 78-2 
 79-7 
 81-2 
 82-7 
 84-2 
 85-7 
 87-2 
 88-7 
 
 + 024 
 
 + 075 
 
 20-500 
 21-362 
 22-220 
 23-076 
 23-928 
 24-774 
 25-624 
 26-467 
 27-309 
 28-147 
 28-990 
 29-825 
 30-663 
 31 505 
 32-377 
 33-226 
 
 69-27 
 74-50 
 79-69 
 84-84 
 89-97 
 95-05 
 100-19 
 105-27 
 110-39 
 115-44 
 120-57 
 125-66 
 130-78 
 135-90 
 140-98 
 146-08 
 
 + 031 
 
 + 113 
 
 + 039 
 
 + 158 
 
 + 047 
 
 + 212 
 
 + 056 
 
 + 272 
 
 + 065 
 
 + -341 
 
 + 076 
 
 + 417 
 
 + 087 
 
 + 504 
 
 
 
 
 
 
 
 
 
 
 
 
 TABLE XLIII. SEVENTH SERIES. 
 May 15, 1878. Jacket 11. 8 to 12. Air about 12 C. 
 
 Thermometer 
 No. 6163. 
 
 
 
 S 
 
 EH 
 
 Correction. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 2n. 
 
 Mean Weight W. 
 
 Work per 
 Kilogramme 
 = 2 9.9387 Wn. 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 + 5097. 
 
 S 
 
 3 
 
 
 
 d 
 * 
 
 130 
 140 
 150 
 160 
 170 
 180 
 190 
 200 
 210 
 220 
 230 
 240 
 250 
 260 
 270 
 280 
 290 
 
 30.9 
 32.2 
 33.6 
 35.0 
 36.3 
 37.6 
 38.9 
 40.2 
 41.5 
 42.8 
 44.2 
 45.5 
 46.9 
 48.3 
 49.6 
 50.9 
 52.3 
 
 .004 
 
 
 
 8.538 
 9.315 
 10.094 
 10.875 
 11.654 
 12.433 
 13.209 
 13.984 
 14.758 
 15.536 
 16.317 
 17.103 
 17.891 
 18.682 
 19.475 
 20.269 
 21.079 
 
 5.07 
 9.73 
 14.36 
 18.98 
 23.56 
 28.16 
 32.74 
 37.31 
 41.84 
 46.38 
 50.99 
 55.62 
 60.29 
 
 69.63 
 74.34 
 79.01 
 
 t 7. 2850 
 1.7. 3011 
 i 7.3165 
 i 7. 3460 
 17.3094 
 |^7.2846 
 J^7.2822 
 ^7.2610 
 
 
 335 
 668 
 1003 
 1335 
 1670 
 2003 
 2337 
 2667 
 2998 
 3332 
 3667 
 4005 
 
 4681 
 5021 
 5358 
 
 
 
 
 
 9 
 10 
 11 
 12 
 13 
 14 
 15 
 16 
 17 
 18 
 19 
 20 
 21 
 22 
 23 
 24 
 
 199 
 628 
 1056 
 1484 
 1913 
 2344 
 2770 
 3196 
 3623 
 4052 
 4478 
 4906 
 5324 
 5754 
 6179 
 6603 
 
 5296 
 5725 
 6153 
 6581 
 7010 
 7441 
 7867 
 8293 
 8720 
 9149 
 9575 
 10003 
 10421 
 10851 
 11276 
 11700 
 
 .002 
 
 .006 
 
 
 
 .010 
 
 + .003 
 
 .008 
 
 + .006 
 
 .000 
 
 + .010 
 
 + .013 
 
 + .014 
 
 + .032 
 
 + .019 
 
 
 
 + .056 
 
 + .025 
 
 + .090 
 
452 
 
 HENRY A. ROWLAND 
 
 TABLE XLIII. Continued. 
 
 Thermometer 
 No. 6163. 
 
 1 
 
 H 
 
 Correction. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 2. 
 
 Mean Weight W. 
 
 Work per 
 Kilogramme 
 = 2 9.9387 Wn. 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 
 +5097. 
 
 a 
 2 
 
 CD 
 
 c 
 
 03 
 
 M 
 
 300 
 310 
 320 
 330 
 340 
 350 
 360 
 370 
 380 
 390 
 400 
 410 
 420 
 
 53.6 
 55.0 
 56.4 
 57.8 
 59.2 
 60.5 
 61.9 
 63.2 
 64.6 
 66.0 
 67.4 
 68.8 
 70.1 
 
 
 
 21.866 
 22.665 
 23.471 
 24.281 
 25.088 
 25.896 
 26 . 706 
 27.523 
 28.346 
 29.172 
 29.996 
 30.827 
 31.653 
 
 83.71 
 88.42 
 93.14 
 97.88 
 102.61 
 107.36 
 112.14 
 116.88 
 121.62 
 126.34 
 131.12 
 135.90 
 140.66 
 
 ) 7.2504 
 | 7.2893 
 | 7.3047 
 ) 7.3389 
 ) 7.4109 
 
 ) 7.4356 
 ' 7.4581 
 
 5697 
 6037 
 6379 
 6722 
 7065 
 7410 
 7759 
 8104 
 8454 
 8801 
 9155 
 9508 
 9861 
 
 25 
 26 
 27 
 28 
 29 
 30 
 31 
 32 
 
 7028 
 7454 
 7883 
 8307 
 8729 
 9157 
 9582 
 10009 
 
 12125 
 12551 
 12980 
 13404 
 13826 
 14254 
 14679 
 15106 
 
 + .032 
 + .039 
 
 + .127 
 + .172 
 
 + .046 
 
 + .222 
 
 + .055 
 
 + .279 
 
 + .065 
 
 + .345 
 
 
 
 
 
 
 
 + .075 
 + .080 
 
 + .419 
 + .456 
 
 
 
 
 
 
 
 TABLE XLIV EIGHTH SERIES. 
 
 May 23, 1878. Jacket 16.2 to 16.5. Air about 20 C. 
 
 Thermometer 
 No. 6166. 
 
 1 
 H 
 
 Correction. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 2n. 
 
 Mean Weight W. 
 
 Work per 
 Kilogramme 
 = 2 9.9075 Wn. 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 
 + 8409. 
 
 S 
 
 
 GO 
 
 d 
 S 
 
 230 
 240 
 250 
 260 
 270 
 280 
 290 
 300 
 310 
 320 
 330 
 340 
 350 
 360 
 370 
 380 
 390 
 400 
 410 
 420 
 
 23.9 
 
 25.4 
 26.8 
 28.3 
 29.7 
 31.2 
 32.7 
 34.2 
 35.6 
 37.1 
 38.6 
 40.1 
 41.6 
 43.1 
 44.6 
 46.0 
 47.5 
 49.0 
 50.6 
 52.1 
 
 .007 
 
 
 
 16?287 
 17.063 
 
 39.120 
 43.982 
 
 6.9137 
 L 6. 9358 
 
 6.9007 
 6.9125 
 
 6.8878 
 6.8866 
 6.8594 
 6.8358 
 6.8748 
 6.9184 
 6.9444 
 6.9291 
 6.9338 
 6.9385 
 6.9444 
 6.9467 
 6.9314 
 
 
 333 
 
 1338 
 1673 
 2010 
 2346 
 2682 
 3020 
 3363 
 3702 
 4044 
 4385 
 4727 
 5074 
 5418 
 5766 
 6115 
 6464 
 
 o 
 
 17 
 18 
 19 
 20 
 21 
 22 
 23 
 24 
 25 
 26 
 27 
 28 
 29 
 30 
 31 
 
 306 
 735 
 1163 
 1592 
 2019 
 2446 
 2871 
 3298 
 3722 
 4150 
 4574 
 4999 
 5423 
 5851 
 6275 
 
 8715 
 9144 
 9572 
 10001 
 10428 
 10855 
 11280 
 11707 
 12131 
 12559 
 12983 
 13408 
 13832 
 14260 
 14684 
 
 
 
 
 
 
 
 .000 
 
 + .005 
 
 19.405 
 20.190 
 20.978 
 21.765 
 22.554 
 23.350 
 24.151 
 24.952 
 25.751 
 26.552 
 27.361 
 28.175 
 28.989 
 29.800 
 30.624 
 31.445 
 
 58.602 
 63.503 
 68.428 
 73.351 
 78.283 
 83.245 
 88.314 
 93.294 
 98.275 
 103.232 
 108.216 
 113.269 
 118.281 
 123.329 
 128.399 
 133.480 
 
 
 
 + !008 
 
 + .040 
 
 + .017 
 
 + .028 
 
 + .085 
 + .144 
 
 
 
 + .039 
 
 + .217 
 
 + .047 
 
 + .281 
 
Ox THE MECHANICAL EQUIVALENT OF HEAT 
 
 453 
 
 TABLE XLV. NINTH SERIES. 
 May 27, 1878. Jacket 19.6 to 20. Air about 23 C. 
 
 Thermometer 
 No. 6163. 
 
 1 
 
 B 
 
 Correction. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 2w. 
 
 Mean Weight. W. 
 
 Work per 
 Kilogramme 
 = 2 9.9077 Wn. 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 + 8246. 
 
 S 
 5 
 
 
 
 1 
 
 200 
 210 
 220 
 230 
 240 
 250 
 260 
 270 
 280 
 290 
 300 
 310 
 320 
 330 
 340 
 350 
 360 
 370 
 380 
 390 
 400 
 410 
 420 
 
 38.0 
 39.4 
 40.9 
 42.3 
 43.8 
 45.3 
 
 .015 
 
 
 
 15.890 
 17.000 
 18.106 
 19.219 
 .20.329 
 21.442 
 22.552 
 23.659 
 24.771 
 25.885 
 27.006 
 28.133 
 29.264 
 30.404 
 31.552 
 32.702 
 33.853 
 35.011 
 36.170 
 37.331 
 38.497 
 39.664 
 40.833 
 
 6.33 
 11.74 
 17.17 
 22.62 
 28.13 
 33.68 
 
 1 8. 8108 
 
 1 8. 7341 
 8.6030 
 
 ) 8.4800 
 
 ^8.4399 
 
 J 
 
 ^8.4765 
 
 \ 8.4552 
 -I 8.4015 
 1 8.4222 
 I 8.4706 
 8.4316 
 
 
 473 
 946 
 1419 
 1895 
 2368 
 
 3785 
 4263 
 4737 
 5215 
 5697 
 6182 
 6669 
 7159 
 7652 
 8143 
 8638 
 9128 
 9626 
 10126 
 10620 
 
 16 
 17 
 18 
 19 
 20 
 21 
 22 
 23 
 24 
 25 
 26 
 27 
 28 
 29 
 30 
 31 
 32 
 33 
 34 
 35 
 36 
 37 
 38 
 39 
 40 
 41 
 
 47 
 473 
 901 
 1326 
 1754 
 2180 
 2606 
 3031 
 3457 
 3883 
 4312 
 4734 
 5159 
 5584 
 6010 
 6435 
 6860 
 7286 
 7714 
 8138 
 8565 
 8988 
 9414 
 9842 
 10268 
 10691 
 
 8293 
 8719 
 9147 
 9572 
 10000 
 10426 
 10852 
 11277 
 11703 
 12129 
 12558 
 12980 
 13405 
 13830 
 14256 
 14681 
 15106 
 15532 
 15960 
 16384 
 16811 
 17234 
 17660 
 18088 
 18514 
 18937 
 
 Oil 
 
 .010 
 
 -.005 
 
 .011 
 
 + .002 
 
 .004 
 
 
 49.8 
 51.3 
 52.9 
 54.4 
 56.0 
 57.5 
 59.1 
 60.6 
 62.2 
 63.8 
 65.4 
 67.0 
 68.6 
 70.2 
 71.8 
 
 + .009 
 
 + .012 
 
 50.55 
 56.25 
 61.93 
 67.63 
 73.36 
 79.15 
 84.97 
 90.85 
 96.78 
 102.66 
 108.59 
 114.45 
 120.36 
 126.33 
 132.26 
 
 + .019 
 
 + .037 
 
 + .029 
 
 + .072 
 
 + .042 
 
 + .118 
 
 + .056 
 
 + .173 
 
 + .071 
 
 + .242 
 
 + .088 
 
 + .322 
 
 + .105 
 
 + .419 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
454 
 
 HENRY A. KOWLAND 
 
 TABLE XLVL TENTH SERIES. 
 June 3, 1878. Jacket 18. 1 to 18. 4. Air about 20 C. 
 
 Thermometer 
 No. 6166. 
 
 6 
 S 
 
 B 
 
 Correction. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 2n. 
 
 Mean Weight W. 
 
 Work per 
 Kilogramme 
 = 2 9.8878 Wn. 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 + 9076. 
 
 S 
 
 
 as 
 
 1 
 
 250 
 260 
 270 
 280 
 290 
 300 
 310 
 320 
 330 
 340 
 350 
 360 
 370 
 380 
 390 
 400 
 410 
 
 4.1 
 7.0 
 9.9 
 12.8 
 15.7 
 18.7 
 21.6 
 24.5 
 27.5 
 30.5 
 33.6 
 36.6 
 39.6 
 42.7 
 45.8 
 48.9 
 52.0 
 
 -.007 
 !6o3 
 
 
 + .004 
 
 17.838 
 18.617 
 19.401 
 20.188 
 20.978 
 21.763 
 22.551 
 23.354 
 24. 162 
 24.970 
 25.780 
 26.593 
 27.415 
 28.246 
 29.079 
 29.911 
 30.754 
 
 7.82 
 
 23.19 
 30.95 
 38.70 
 46.41 
 54.21 
 62.04 
 69.92 
 77.92 
 85.89 
 93.94 
 102.05 
 110.34 
 118.49 
 126.66 
 134.89 
 
 | 4. 3899 
 1 4. 3919 
 J4.3912 
 1 4. 3907 
 | 4. 3624 
 J4.3542 
 1 4. 3362 
 i 4. 3978 
 
 
 
 667 
 1005 
 1341 
 1676 
 2014 
 2354 
 2696 
 3041 
 3385 
 3731 
 4081 
 4437 
 4786 
 5141 
 5499 
 
 18 
 19 
 20 
 21 
 22 
 23 
 24 
 25 
 26 
 27 
 28 
 29 
 30 
 31 
 
 69 
 496 
 925 
 1350 
 1778 
 2204 
 2627 
 3054 
 3479 
 3904 
 4332 
 4852 
 5179 
 5604 
 
 9145 
 9572 
 10001 
 10426 
 10854 
 11280 
 11703 
 12130 
 12555 
 12980 
 13408 
 13828 
 14255 
 14680 
 
 + .003 
 
 + .020 
 
 + .008 
 
 + 0.037 
 
 + .014 
 
 + .078 
 
 + .020 
 
 + .132 
 
 + .028 
 
 + .198 
 
 + .036 
 
 + .281 
 
 
 
 
 + .044 
 
 + .377 
 
 . . I 
 
 
 TABLE XLVIL ELEVENTH SERIES. 
 June 19, 1878. Jacket 19. 6 to 20. Air about 23 C. 
 
 Thermometer 
 No. 6163. 
 
 6 
 S 
 
 B 
 
 Correction. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 2n. 
 
 Mean Weight W. 
 
 Work per 
 Kilogramme 
 = 2 9.8404 Wn. 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 + 10620. 
 
 S 
 5 
 
 -t-> 
 
 02 
 
 i 
 
 W 
 
 250 
 
 260 
 270 
 280 
 290 
 300 
 310 
 320 
 330 
 340 
 350 
 360 
 370 
 380 
 390 
 400 
 410 
 420 
 
 .... 
 
 .002 
 + .002 
 
 
 + .006 
 
 21?450 
 22.562 
 
 8.933 
 16.087 
 
 6.7572 
 
 I 6. 7678 
 
 
 476 
 
 o 
 
 21 
 22 
 23 
 24 
 25 
 26 
 27 
 28 
 29 
 30 
 31 
 32 
 33 
 34 
 35 
 36 
 37 
 38 
 39 
 40 
 41 
 
 -192 
 235 
 
 662 
 1087 
 1511 
 1939 
 2365 
 2789 
 3214 
 3638 
 4063 
 4488 
 4913 
 5337 
 5760 
 6187 
 6614 
 7040 
 7465 
 7891 
 8317 
 
 10428 
 10855 
 11282 
 11707 
 12131 
 12559 
 12985 
 13409 
 13834 
 14258 
 14683 
 15108 
 15533 
 15957 
 16380 
 16807 
 17234 
 17660 
 18085 
 18511 
 18937 
 
 .... 
 
 + .010 
 
 + .029 
 
 24.789 
 25.907 
 27.032 
 28.168 
 29.307 
 30.456 
 31.612 
 32.774 
 33.939 
 35.110 
 36.280 
 37.456 
 38.637 
 39.821 
 41.010 
 
 30 281 
 37.439 
 44.655 
 51.848 
 59.098 
 66.390 
 73 . 724 
 81.153 
 88.462 
 95.734 
 103.093 
 110-560 
 118.121 
 125.693 
 133.250 
 
 i 6 . 7749 
 i 6. 7896 
 j. 6. 7973 
 i 6. 8188 
 I 6. 9165 
 j. 6. 7876 
 I 6. 7808 
 
 1421 
 1899 
 2379 
 2860 
 3344 
 3832 
 4323 
 4817 
 5311 
 5807 
 6307 
 6808 
 7311 
 7815 
 8321 
 
 
 + .019 
 
 + .063 
 
 .... 
 
 + .031 
 
 + .113 
 
 
 
 + .043 
 
 + .177 
 
 
 + .058 
 
 + .257 
 
 
 + .072 
 
 + .351 
 
 
 + .087 
 
 + .463 
 
 
 + .106 
 
 + .595 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 455 
 
 '0961 + 
 tuBJ 
 jad JIJ 
 
 cooo;<Mioaoocoa 
 
 jcad 3{JO^ i _j_ i-ii-is<(Moijcoco'* < '*icirtioo>i>t-oooooooioio 
 
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 90iS8'6S 
 
 90iS8'6 
 
 eoo-*ooCMOcO'-it-O5inift<?>coo t- wo 
 
 JO 
 
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 OOOOOOOOOOOOO500O5O5O:OiOOO5O OJ O 
 
 t- 00 00 OS O5 O iH i-l 
 
 *(< MI ^fi Tt< M< WlftW 
 
 qdBJJSouoaqo 
 
 JO SUOt?.niOA9}J 
 
 jo oqnx 
 
 MTV 
 
 oo 10 
 10 o 
 -oo 
 
 O O 
 
 o o 
 
 : l' : + : + : 
 
 & r-< 
 
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 O 1 I *H 
 
 co 
 
 -N 
 
 '8919 jo 
 mooq 
 58 aqnx 
 
 00 O! 
 
 m in 
 
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 *t *< 
 
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 '8919 'ON ^q 
 
 J9J8UIIJOIBO JO 
 
 .1.1 n nu.- 
 
 ot-cOi-iyico'* 
 
 6919 ' 
 
456 
 
 HENRY A. EOWLAND 
 
 TABLE XLIX. THIRTEENTH SERIES. 
 Dec. 19, 1878. Jacket 3.2 to 3.5. Air 4. 2 to 5.2 
 
 C. 
 
 Thermometer 
 No. 6163. 
 
 Corrections. 
 
 Corrected 
 Temperature. 
 
 Revolutions of 
 Chronograph 2n. 
 
 Mean Weight W. 
 
 Work per 
 Kilogramme 
 9.8938 X Wn. 
 
 2 9.8938 Wn. 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work + 1964. 
 
 a 
 5 
 
 00 
 
 1 
 
 70 
 80 
 90 
 100 
 110 
 120 
 130 
 140 
 150 
 160 
 170 
 180 
 190 
 200 
 210 
 220 
 230 
 240 
 250 
 260 
 270 
 280 
 
 
 
 
 
 1?248 
 2.378 
 3.500 
 4.626 
 5.751 
 6.881 
 8.013 
 9.148 
 10.284 
 11.424 
 12.569 
 13.713 
 14.859 
 16.005 
 17.154 
 18.300 
 19.452 
 20.604 
 21.760 
 22.912 
 24.065 
 25.221 
 
 1.72 
 7.38 
 13.11 
 18.89 
 24.70 
 30.55 
 36.38 
 42.27 
 48.10 
 53.92 
 59.81 
 65.72 
 71.57 
 77.50 
 83.40 
 89.30 
 95.23 
 101.17 
 
 8.6610 
 8.5571 
 8.4325 
 8.3688 
 8.4155 
 8.4189 
 8.3953 
 8.4366 
 8.4484 
 8.4189 
 8.3988 
 8.4153 
 8.3811 
 8.3835 
 8.3976 
 8.4035 
 
 8.4460 
 
 1 
 
 5*8.4555 
 
 8.4602 
 8.4779 
 
 485.0 
 485.1 
 482.2 
 481.1 
 487.1 
 485.6 
 489.2 
 486.6 
 486.5 
 490.6 
 491.1 
 487.1 
 491.7 
 489.4 
 490.2 
 493.0 
 496.4 
 
 981.3 
 
 494.7 
 494.0 
 
 
 485.0 
 970.1 
 1452.3 
 1933.4 
 2420.5 
 2906.1 
 3395 . 3 
 3881.9 
 4368.4 
 4859.0 
 5350.1 
 5837.2 
 6328.9 
 6818.3 
 7308.5 
 7801.5 
 8297.9 
 
 1 
 2 
 3 
 4 
 5 
 6 
 7 
 8 
 9 
 10 
 11 
 12 
 13 
 14 
 15 
 16 
 17 
 18 
 19 
 20 
 21 
 22 
 23 
 24 
 25 
 
 106 
 + 323 
 754 
 1184 
 1612 
 2041 
 2472 
 2901 
 3331 
 3760 
 4187 
 4615 
 5045 
 5472 
 5898 
 6327 
 6753 
 7180 
 7608 
 8038 
 8465 
 8891 
 9317 
 9746 
 10173 
 
 1858 
 2287 
 2718 
 3148 
 3576 
 4005 
 4436 
 4865 
 5295 
 5724 
 6151 
 6579 
 7009 
 7436 
 7862 
 8291 
 8717 
 9144 
 9572 
 10002 
 10429 
 10855 
 11281 
 11710 
 12137 
 
 
 
 .003 
 
 + .001 
 
 + .003 
 
 + .005 
 
 + .019 
 
 + .009 
 
 + .044 
 
 + .016 
 
 + .080 
 
 + .023 
 
 + .126 
 
 + .033 
 
 + .183 
 
 + .044 
 
 + .251 
 
 + .056 
 
 + .332 
 
 112.90 
 118.81 
 124.70 
 
 9279.2 
 9773.9 
 10267.9 
 
 + .069 
 
 + .424 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 
 
 457 
 
 TABLE L. FOURTEENTH SERIES. 
 December 20, 1878. Jacket 1.5 to 1.9. Air about 3.4 C. 
 
 Temperature 
 by Kew 
 Standard. 
 
 4 
 
 a 
 
 H 
 
 Corrections. 
 
 Corrected Tem- 
 perature Abso- 
 lute Scale. 
 
 Revolution of 
 Chronograph 
 2n. 
 
 Mean Weight 
 W. 
 
 k e 
 
 11^ 
 Sfi 
 
 2 
 
 *s 
 
 Temperature. 
 
 Work per 
 Kilogramme. 
 
 Work per 
 Kilogramme 
 + 2210. 
 
 Reduction 
 to Absolute 
 Scale. 
 
 1 
 
 i 
 
 36.0 
 38.5 
 41.0 
 43.5 
 46.0 
 48.5 
 51.0 
 53.5 
 56.0 
 58.5 
 61.0 
 63.5 
 66.0 
 68.5 
 71.0 
 73.5 
 76.0 
 78.5 
 
 56.0 
 58.4 
 .9 
 3.3 
 5.8 
 8.2 
 10.7 
 13.2 
 15.6 
 18.2 
 20.7 
 23.3 
 25.9 
 28.5 
 31.2 
 33.8 
 36.5 
 39.2 
 
 .00 
 
 
 
 
 
 182 
 3.23 
 4.62 
 6.02 
 7.43 
 8.84 
 10.26 
 11.68 
 13.12 
 14.56 
 16.01 
 17.46 
 18.92 
 20.39 
 21.86 
 23.34 
 24.84 
 26.33 
 
 8.03 
 16.37 
 24.78 
 33.19 
 41.48 
 49.81 
 58.18 
 66.56 
 74.95 
 83.56 
 92.27 
 100.99 
 109.95 
 118.84 
 127.83 
 136.75 
 145.78 
 154.80 
 
 7.3682 
 7.3458 
 7.3705 
 7.4012 
 7.4142 
 7.4177 
 7.4390 
 7.4107 
 7.3493 
 7.3269 
 7.2335 
 7.1603 
 7.2075 
 7.1839 
 7.2122 
 7.2252 
 7.2134 
 
 
 601 
 
 1206 
 1812 
 2412 
 3016 
 3624 
 4234 
 4842 
 5461 
 6085 
 6703 
 7330 
 7957 
 8589 
 9218 
 9857 
 10493 
 
 O 
 
 2 
 3 
 4 
 5 
 6 
 7 
 8 
 9 
 10 
 11 
 12 
 13 
 14 
 15 
 16 
 17 
 18 
 19 
 20 
 21 
 22 
 23 
 24 
 25 
 26 
 
 77 
 503 
 936 
 1370 
 1803 
 2226 
 2656 
 3084 
 3513 
 3942 
 4369 
 4790 
 5220 
 5650 
 6081 
 6507 
 6935 
 7364 
 7791 
 8219 
 8648 
 9074 
 9499 
 9925 
 10352 
 
 2287 
 2713 
 3146 
 3580 
 4013 
 4436 
 4866 
 5294 
 5723 
 6152 
 6579 
 7000 
 7430 
 7860 
 8291 
 8717 
 9145 
 9574 
 10001 
 10429 
 10858 
 11284 
 11709 
 12135 
 12562 
 
 -.01 
 
 .00 
 
 + .01 
 
 -.02 
 
 + .01 
 
 + .04 
 
 -.03 
 
 + .02 
 
 + .09 
 
 -.04 
 
 + .03 
 
 + .16 
 
 -.04 
 
 + .05 
 
 + .25 
 
 -.05 
 
 + .06 
 
 + .38 
 
 -.05 
 
 + .08 
 
 + .52 
 
 -.05 
 
 + .10 
 
 + .69 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
458 
 
 HENRY A. ROWLAND 
 
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 00 O CO IO CO 
 JO O * 00 CM 
 
 co r> t- i- oo 
 
 ^S S unoqj9d 98 
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 CM OS CO CM OS 
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ON THE MECHANICAL EQUIVALENT OF HEAT 459 
 
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460 
 
 HENRY A. ROWLAND 
 
 
 
 
 
 
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ON THE MECHANICAL EQUIVALENT OF HEAT 
 
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 ^ d rH os oo t** co in *n 
 
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 d d d d d d d d d 
 
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 dddddddd 
 
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 dddddddd 
 
 
 
 
 
 
 
 
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 cosoioeoinmininin 
 d d d d d d d d d 
 
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 d d d d 
 
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462 
 
 HEXEY A. EOWLAND 
 
 Mechanical Equivalent of Heat. 10 Series on the 
 
 Mercurial Thermometric 
 Scale, the Glass similar 
 to the 
 
 1*| 
 
 i>iccoi-Haoz>iCTt<i-ioct-5O 
 
 : : :SS^^^S^^S 
 
 uipnBjj 
 
 .(M^-lOOOlCTt<CO-HOCOOt> 
 
 ' ' : SNwSct^N 
 
 pJBpUB^g 
 A192 
 
 . . .cooooeo^esoooas.ccocs.o 
 
 wSwWWNCQWWWWWN 
 
 J9I88I9Q 
 
 .SilCCOOCJ^r-IOOOOO 
 
 ' '. Icococoeocococococococococo 
 
 Absolute Thermomet. Scale. 
 
 Absolute C. 
 G S. System. 
 
 SUISR 
 
 OOOOO>OSO5O5OiCOCOCOCO 
 
 o __L____^LJ^!__L____J!!!!____ 
 
 '81000' = I" 
 
 -r-iooooosososajoscocooo 
 
 
 Kilogr.- Metres 
 at Baltimore. 
 
 
 . . .^c*ot--*(MOOS?O^WOOO 
 
 
 : : :SiwNNNNwwww 
 
 "BS5- 
 
 . . .1-^WOSCO^OJOt-iCCO^OS 
 
 ! '. IOSCSCSOOOOGOOO co t~ z> t- t- o 
 
 Work. 
 
 'WmraMVSd* 
 
 OCO'^'l-t-OSOlO' (OOiCOt-tOlC'tiTH 
 O'*DOOOCN(-#t-CT-<<MM<tOOOO<M'* 
 O'*COCS}t-r-llCOSCOOOCN}OO'*O5COl- 
 OO'IMCOCO'<tl'*Tj(lCicO5Ol~t-D-aOOO 
 
 o 
 
 Per Kilogr. of Water. 
 
 . lllOO'I . 
 
 oscjiCJOt-i-*t-ocoicooi-i:oocS'-i 
 
 CXJl~'-llCOTjHCCCOl-THlCOTtHOO<Mt- 
 <MeMCOCOM<^Tt<iC 1 C5O5Ct~t-t-003O 
 
 >B89?,9 W - n Son 3 
 
 .98000'T s ^ B 
 3 
 
 *CiC5OT^ i ^COCN('--tOSlCCOOt^- 1 ^THOS 
 OSCMlCOO-HTt<l>OCSJ)CCOTHCO!OO5r-l 
 
 Rc>-ino4ieoAci-iioOTfiaO'Mb< 
 
 <N<MCOCO"*<Tj<TtliClC5O5Ol-t-l OOOO 
 
 -9uiniBi!8ofi5i 
 
 CBSSOCSCSOOCOt-iCWOl-iCUJOCO 
 CO-HlCt-OcOSOOSIJiCOOOCOCOOS-H 
 < MI>T-ilCO'tlOO<Mt>i-liCO-*iCOCJt- 
 
 Temperature. 
 
 Approximate, Mercurial Thermom. 
 
 w, 
 
 T^ i ( O5 C^l CO CO CO ^ ^ ^ iC iC *C 1C 5O 5O 
 
 oooooooooooooooo 
 
 C^CO^lC5O?>OOC35Ot lO5CO^iC5Ot- 
 
 f PL JO 
 
 <MiyicO'<*'icictot-t-ooooosoooi i 
 
 OOOOOOOoOOOO'-l'-'i-ii-l 
 
 (MCO^iCCOt^COOJO TJCO^iCcot- 
 
 
 .p PW e a 
 
 Hi iTHCSllMWCViCJCOCOCO^f^T^Tt*^ 
 
 oooooooooooooooo 
 
 weo^wcot-coosorHWco^jcjoh- 
 
 VSSS8 
 
 ?S-^lCt-OSOr-iSXJCO^lCtOOOCOC^H 
 
 
 MI9 a 1P a 
 
 co-*iC5Ocoo5Oi-iffjeo-*icot>aso 
 
 o 
 
 (MCO-*COt-OOOSOT-liNCO-*iCI> 
 
 Absolute Scalel 
 
 QIOOO- = i 
 
 OOOOOOOOOOOOOOr-lrH 
 OO OOOOOOOOOOOOOOO 
 
 WCO^io?ct-OOOSO'H(jjcO'*COl> 
 
 
 '81000' = Smsn 
 
 0<MC0^1CCOI-OOOSO^<MCO^>C501- 
 
 
Ox THE MECHANICAL EQUIVALENT or HEAT 
 
 463 
 
 ICCOCOi-HrHOSOSOOOOt-OCt-OOOOOSOSr-JrHOI 
 lCiClClCiC'^'^''t < '^ 1 '^^* 1T **'^ l '^'^'^ | lClClC 
 01010101010101010101010101010101010101 
 
 COiCiC^TfiCOOIOIOIOICOCO^lCiCCOoOCiO . . . . 
 O1O1O1O1O1O1O1O1O1O1O1O1O1O1O1O1O1O1O1 " ' " " 
 
 COt-COlC-*OlO1r-(OOOOSOOOrHO1O1CO 
 
 CIC1^'C1CIC1C1C1C1C1C'<<1C1C1C1C1C1C1C " * * 
 O1O1O1O1O1CMO1O1CMO1O1O1C 
 
 OSOSOOOOOr-*OlOl^^COt~O5OOlTt'ic . . . 
 
 ooiwco'co'coco'ccco'eoco'eo'eocoeoTi3'*M<T)5 
 
 OJO1O1O1O1O1O1O1O1O1O1O1O1O1OJO1O1O1O1 
 
 WOOSt-COlC'^'COOI-Ht-lrHrHrHi-lOIOIeOCO 
 
 0*OO5t-COM<COOl*-lOeJSCSOSOSOOOO 
 Q000>*i>t~*t t t t t-CO5OCOCOt~^l>t 
 
 t-iC^OlrHOCsooi-cocococococet l-oooo ; ; 
 cc'co'ococo'o'ic'icicicic'ic'ic'icic'ic'icic'ic 
 
 O1O1O1O1O1O1O1O1O1O1O1O1O1O1O1O1O1O1O1 
 
 t^lCrtiOlrHOSOOt COlClC^^^^^iClCiC 
 
 COCO5O5O5OiClCiCiClClClCiClClCiClClc*C . . . 
 OJO1O1O1O1O1O1O1O1O1O1O1O1O1O1O1O1O1O1 . . . 
 
 coe*OGO5ocooioo5ooiascooiGooiot--*oi c 'oo'Coi 
 
 5OOOOrHCOlCt-COOOlCOiCl NB0 OOO1COlCC > -C3SOO1 1 ^ 
 rHlCO*(t10OO1COOlCOSCOt*' |1CO^OOO15OO1COSCO 
 CJSOSOOOr-lr-IOIOIOJCOCO^^lClClCCOCOt-t-l-CO 
 
 t-^OCOO100^tlOO'*OSCOlCO1t-OO'*O5COOCOO1t Ol 
 ^*l-OO11Ct OOllCt-OOJiCt-OSOlTtlt- OOllCt-O 
 
 rHiCO^OOOIt-rHlCOS-^OOOIeOOiCOSCOCOOICOOlC 
 OSOSOOOrHr-l04C1O1COCO^TtlC'CiCCOCOl-t-OOaO 
 
 t-^O5OO1001COOlCOSTt(COCOOOOlCr-ICOO1CO^t*OSC 
 *^.r*iroiCtoO1iCl>OO!lCt~OO1iCt~OO11Ct"*O 
 
 t-r-iiCOS-^OOOlcOr-liCOSCOCOOICOOlCOS 
 
 Oi- j <-HOioioicocoTj<Tj(iciciCcocor-.i-oooo 
 
 COOSSOOt-Oll-OSt-W^OCOi-IOO^ttr-ICOOl 
 .r-.f->COCOOOOO11COOOCOlCOOOCOOOrH 
 
 rHlCCSTjtOOOICOr-llCOSCOaOOICOOlCOS 
 i-HO101O1COCO-*-*lClCiCcoCOl->0000 
 
 COOOCOOOCIOOOOSOSOSOSOSOSOSOOOOOO 
 OOOOOOOOOOOOOOOOOOi-jrHr-JrHrH 
 
 adosorHWco'^'ioeo'^odosOrHoico^iccdt^odoso 
 
 1-1 IO!O1O1O1O1O1O1O1O1O1COCOCOCOCOeOCOCOCOCOTt< 
 
 ooosorHoico^iccot^cdosOrHoieo'-^iccdt^coosc:) 
 
 rHr-iOlO1O1O1OlOJCMO1O1O1SOCOCOeOCOCOCOCOCOCO-* 
 
 jCiClCiCiCiCcOCOCOCOCOCOCOCO5Ob - l > *l > -t !> 
 
 O O O O O C5 O O O O O O O O O O O O CD O O O O __ 
 
 a6os'o^oicoTiiiccdt>odosorHOco''*iccdt-odo5Or-I a 
 OJOioioioioiojesjoiojcocoeocoeocococoeoco-* 1 * o 
 
 eoT*^^^^lftftee>^ttC3SOSOOr^*^rHO1OlO1C > 10 : l 
 
 oioioicoeococococoeoeocococo -^ 
 ooosot ioico^iC5Ot-odosO'-5oieo'Tjiic5oi-ooos~ 
 
 r-l-jcoOIOlOIOIOIOIOlOIOICOCOCOCOCOCOCOCOCOCO 
 
 3 
 
 eoeo-}<icciccocoi-t-coaooooioso5csoso 
 
 O1O1O1O1O1O1O*WO1O1O1O1O1O1O1O1CO1O1O1CO 
 
 oooso'i-Hoieo-HJiccdi-odosOrHoieo-^iceo't-odoso 
 rHr-ioioioioioioioioioioicococoeoeocococoroco'* 
 
 s 
 
 OOOSOr-lOICO^lCCOI^OOOSOrHOleO^lCCOl OOOSOO 
 1-HrHOIOIOIOIOIOlOlOlOIOICOCOCOCOCOCOCO 
 
 00 OS O rH 
 
 CO' 
 
 CO l- 
 
 eo t- 
 
464 
 
 HENEY A. KOWLAND 
 
 TABLE LIV. FINAL MOST PROBABLE RESULTS. 
 
 CD 
 
 Work. 
 
 Mechanical 
 Equivalent. 
 
 2 
 
 Work. 
 
 Mechanical 
 Equivalent. 
 
 O o * 
 
 -P 
 
 a 
 
 i 
 
 ,io$ 
 
 (BOOO 
 
 i . 
 
 a 
 
 i 
 
 ,io5 
 
 pi 
 
 
 22 
 
 32 
 
 <!~ . 
 
 
 S"5 
 
 2-2 
 
 lug 
 
 ^G3 ' 
 
 
 a 
 
 2 
 
 ag 
 
 . S 
 
 -u"S 
 
 S OD 9 
 
 ;3 t> 
 
 a <*> s 
 
 . . S 
 
 8 "8 
 
 sga 
 
 OCQ 
 
 S 2 
 
 a>S->-U 
 
 8*3 
 
 s 25 
 
 302 
 
 s 2 a 
 
 aJu2 
 
 &gs 
 
 11 5 
 
 00 . 
 
 bc+^'-S 
 
 Jv83 
 
 ll 
 
 SS g 
 
 ttf)'* J 4^* 
 
 o p ~~ ( 
 
 |o6 
 
 l"|l 
 
 |||" 
 
 H 
 
 2 K 
 
 q 
 
 S m 
 
 hi 
 
 ID 
 g 
 
 2 = 
 
 
 
 5 w 
 
 i 
 
 
 
 00000. 
 
 
 0000. 
 
 o 
 
 
 00000. 
 
 
 0000. 
 
 2 
 
 2289 
 
 2443 
 
 
 
 22 
 
 10852 
 
 10835 
 
 426.1 
 
 4176 
 
 3 
 
 2720 
 
 2865 
 
 
 
 23 
 
 11278 
 
 11253 
 
 426.0 
 
 4175 
 
 4 
 
 3150 
 
 3286 
 
 
 
 24 
 
 11704 
 
 11670 
 
 425.9 
 
 4174 
 
 5 
 
 3580 
 
 3708 
 
 429.8 
 
 4212 
 
 25 
 
 12130 
 
 12088 
 
 425.8 
 
 4173 
 
 6 
 
 4009 
 
 4129 
 
 429.5 
 
 4209 
 
 26 
 
 12556 
 
 12505 
 
 425.7 
 
 4172 
 
 7 
 
 4439 
 
 4550 
 
 429.3 
 
 4207 
 
 27 
 
 12982 
 
 12922 
 
 425.6 
 
 4171 
 
 8 
 
 4868 
 
 4970 
 
 429.0 
 
 4204 
 
 28 
 
 13407 
 
 13339 
 
 425.6 
 
 4171 
 
 9 
 
 5297 
 
 5390 
 
 428.8 
 
 4202 
 
 29 
 
 13833 
 
 13756 
 
 425.5 
 
 4170 
 
 10 
 
 5726 
 
 5811 
 
 428.5 
 
 4200 
 
 30 
 
 14258 
 
 14173 
 
 425.6 
 
 4171 
 
 11 
 
 6154 
 
 6230 
 
 428.3 
 
 4198 
 
 31 
 
 14684 
 
 14950 
 
 425.6 
 
 4171 
 
 12 
 
 6582 
 
 6650 
 
 428.1 
 
 4196 
 
 32 
 
 15110 
 
 15008 
 
 425.6 
 
 4171 
 
 13 
 
 7010 
 
 7070 
 
 427.9 
 
 4194 
 
 33 
 
 15535 
 
 15425 
 
 425.7 
 
 4172 
 
 14 
 
 7438 
 
 7489 
 
 427.7 
 
 4192 
 
 34 
 
 15961 
 
 15842 
 
 425.7 
 
 4172 
 
 15 
 
 7865 
 
 7908 
 
 427.4 
 
 4189 
 
 35 
 
 16387 
 
 16259 
 
 425.8 
 
 4173 
 
 16 
 
 8293 
 
 8327 
 
 427.2 
 
 4187 
 
 36 
 
 16812 
 
 16676 
 
 425.8 
 
 4173 
 
 17 
 
 8720 
 
 8745 
 
 427.0 
 
 4185 
 
 37 
 
 17238 
 
 17094 
 
 
 
 18 
 
 9147 
 
 9164 
 
 426.8 
 
 4183 
 
 38 
 
 17664 
 
 17511 
 
 
 
 19 
 
 9574 
 
 9582 
 
 426.6 
 
 4181 
 
 39 
 
 18091 
 
 17930 
 
 
 
 20 
 
 10000 
 
 10000 
 
 426.4 
 
 4179 
 
 40 
 
 18517 
 
 18347 
 
 
 
 21 
 
 10426 
 
 10418 
 
 426.2 
 
 4177 
 
 41 
 
 18943 
 
 18765 
 
 
 
 
 
 TABLE LV. QUANTITY TO ADD TO THE EQUIVALENT AT BALTIMORE TO 
 REDUCE TO ANT LATITUDE. 
 
 Latitude. 
 
 Addition in 
 Kilogramme-Metres. 
 
 
 
 
 
 + 0.89 
 
 10 
 
 + 0.82 
 
 20 
 
 + 0.63 
 
 30 
 
 + 0.34 
 
 40 
 
 + 0.08 
 
 50 
 
 0.41 
 
 60 
 
 0.77 
 
 70 
 
 -1.06 
 
 80 
 
 1.26 
 
 90 
 
 -1.33 
 
 Manchester 0.5 ; Paris 0.4 ; Berlin 0.5. 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 465 
 
 V. CONCLUDING REMARKS, AND CRITICISM OF RESULTS AND 
 
 METHODS 
 
 On looking over the last four columns of Table LIII, which gives 
 the results of the experiments as expressed in terms of the different 
 mercurial thermometers, we cannot but be impressed with the unsatis- 
 factory state of the science of thermometry at the present day, when 
 nearly all physicists accept the mercurial thermometer as the standard 
 between and 100. The wide discrepancy in the results of calori- 
 metric experiments requires no further explanation, especially when 
 physicists have taken no precaution with respect to the change of zero 
 after the heating of the thermometer. They show that thermometry 
 is an immensely difficult subject, and that the results of all physicists 
 who have not made a special study of their thermometers, and a com- 
 parison with the air thermometer, must be greatly in error, and should 
 be rejected in many cases. And this is specially the case where Geissler 
 thermometers have been used. 
 
 The comparison of my own thermometers with the air thermometer is 
 undoubtedly by far the best so far made, and I have no improvements to 
 offer beyond those I have already mentioned in the ' Appendix to Ther- 
 mometry/ And I now believe that, with the improvement to the air 
 thermometer of an artificial atmosphere of constant pressure, we could 
 be reasonably certain of obtaining the temperature at any point up to 
 50 C. within 0-01 C. from the mean of two or three observations. 
 I believe that my own thermometers scarcely differ much more than 
 that from the absolute scale at any point up to 40 C., but they represent 
 the mean of eight observations. However, there is an uncertainty of 
 0-01 C. at the 20 point, owing to the uncertainty of the value of m. 
 But taking m= -00015, I hardly think that the point is uncertain to 
 more than that amount for the thermometers Nos. 6163, 6165, and 6166. 
 
 As to the comparison of the other thermometers, it is evidently un- 
 satisfactory, as they do not read accurately enough. However, the fig- 
 ures given in Table LIII are probably very nearly correct. 
 
 The study of the thermometers from the different makers introduces 
 the question whether there are any thermometers which stand below the 
 air thermometer between and 100. As far as I can find, nobody has 
 ever published a table showing such a result, although Bosscha infers that 
 thermometers of " Cristal de Choisy-le-Eoi " should stand below, and 
 his inference has been accepted by Eegnault. But it does not seem 
 to have been proved by direct experiment. My Baudin thermometers 
 seem to contain lead as far as one can tell from the blackening in a gas 
 30 
 
466 HENRY A. ROWLAND 
 
 flame, but they stand very much above the air thermometer at 40. I 
 have since tried some of the Baudin thermometers up to 300, and find 
 that they stand Mow the air thermometer between 100 and 240 ; they 
 coincide at about 240, and stand above between 240 and 300. This 
 is very nearly what Eegnault found for " Verre Ordinaire." It is to be 
 noted that the formula obtained from experiments below 100 makes 
 them coincide at 233, which is remarkably close to the result of actual 
 experiment, especially as it would require a long series of experiments 
 to determine the point within 10. 
 
 The comparison of thermometers also shows that all thermometers 
 in accurate investigations should be used as thermometers with arbi- 
 trary scales, neither the position of the zero point nor the interval be- 
 tween the and 100 points being assumed correct. The text books 
 only give the correction for the zero point, but my observations show 
 that the interval between the and 100 points is also subject to a sec- 
 ular change as well as to the temporary change due to heating. Of 
 all the thermometers used, the Geissler is the worst in this as in other 
 respects, except accuracy of calibration, in which it is equal to most of 
 the others. 
 
 The experiments on the specific heat of water show an undoubted 
 decrease as the temperature rises, a fact which will undoubtedly sur- 
 prise most physicists as much as it surprised me. Indeed, the dis- 
 covery of this fact put back the completion of this paper many months, 
 as I wished to make certain of it. There is now no doubt in my mind, 
 and I put the fact forth as proved. The only way in which an error 
 accounting for this decrease could have been made appears to me to be 
 in the determination of ra in " Thermometry." The determination of 
 m rests upon the determination of a difference of only 0-05 C. between 
 the air thermometer and the mercurial, the and 40 points coincid- 
 ing, and also upon the comparison of the thermometers with others 
 whose value of m was known, as in the Appendix. Although the quan- 
 tity to be measured is small, yet there can be no doubt at least that m 
 is larger than zero; and if so, the specific heat of water certainly has a 
 minimum at about 30. 
 
 One point that might be made against the fact is that the Kew stand- 
 ard, Table L, gives less change than the others. But the calibra- 
 tion of the Kew standard, although excellent, could hardly be trusted to 
 0-02 or 0-03 C., as the graduation was only to F. In drawing the 
 curve for the difference between the Kew standard and the air ther- 
 mometers, I ignored small irregularities and drew a regular curve. On 
 
ON THE MECHANICAL EQUIVALENT OF HEAT 467 
 
 looking over the observations again, I see that, had I taken account of 
 the small irregularities, it would have made the observations agree more 
 nearly with the other thermometers. Hence the objection vanishes. 
 However, I intend working up some observations which I have with the 
 Kew standard at a higher temperature, and shall publish them at a 
 future time. 
 
 There is one other error that might produce an apparent decrease in 
 the specific heat, and that is the slight decrease in the torsion weight 
 from the beginning to the end of most of the experiments, probably due 
 to the slowing of the engine. By this means the torsion circle might 
 lag behind. I made quite an investigation to see if this source of error 
 existed, and came to the conclusion that it produced no perceptible 
 effect. An examination of the different experiments shows this also, 
 for in some of them the weight increases instead of decreasing. See 
 Tables XXXVII to L. 
 
 The error from the formation of dew might also cause an apparent 
 decrease; but I have convinced myself by experiment, and others can 
 convince themselves from the tables, that this error is also inappre- 
 ciable. 
 
 The observations seem to settle the point with regard to the specific 
 heat at the 4 point within reasonable limits. There does not seem 
 to be a change to any great extent at that point, but the specific heat 
 decreases continuously through that point. It would hardly be possible 
 to arrive at this so accurately as I have done by any method of mixture, 
 for Pfaundler and Platter, who examined this point, could not obtain 
 results within one per cent, while mine show the fact within a fraction 
 of one per cent. 
 
 The point of minimum cannot be said to be known, though I have 
 placed it provisionally between 30 and 35 C., but it may vary much 
 from that. 
 
 The method of obtaining the specific heat of the calorimeter seems 
 to be good. The use of solder introduces an uncertainty, but it is too 
 small to affect the result appreciably. The different determinations of 
 the specific heat of the calorimeter do not agree so well as they might, 
 but the error in the equivalent resulting from this error is very small, 
 and, besides, the mean result agrees well with the calculated result. It 
 may be regarded as satisfactory. 
 
 The apparatus for determining the equivalent could scarcely be im- 
 proved much, although perhaps the record of the torsion might be made 
 automatic and continuous. The experiment, however, might be im- 
 
HENRY A. ROWLAND 
 
 proved in two ways; first, by the use of a motive power more regular in 
 its action; and, second, by a more exact determination of the loss due to 
 radiation. The effect of the irregularity of the engine has been calcu- 
 lated as about 1 in 4000, and I suppose that the error due to it cannot 
 be as much as that after applying the correction. The error due to 
 radiation is nearly neutralized, at least between and 30, by using 
 the jacket at different temperatures. There may be an error of a small 
 amount at that point (30) in the direction of making the mechanical 
 equivalent too great, and the specific heat may keep on decreasing to 
 even 40. 
 
 Between the limits of 15 and 25 I feel almost certain that no sub- 
 sequent experiments will change my values of the equivalent so much 
 as two parts in one thousand, and even outside those limits, say be- 
 tween 10 and 30, I doubt whether the figures will ever be changed 
 much more than that amount. 
 
 It is my intention to continue the experiments, as well as work up 
 the remainder of the old ones. I shall also use some liquids in the 
 calorimeter other than water, and so have the equivalent in terms of 
 more than one fluid. 
 
 Baltimore, 1878-79. FinisTied May 27, 1879. 
 
21 
 
 APPENDIX TO PAPEE ON THE MECHANICAL EQUIVALENT 
 OF HEAT, CONTAINING THE COMPARISON WITH DR. 
 JOULE'S THERMOMETER 
 
 [Proceedings of the American Academy of Arts and Sciences, XVI, 38-45, 1881] 
 Presented, March, 1880 
 
 In the body of this paper I have given an estimate of the departure of 
 Dr. Joule's thermometer from the air thermometer, based on the com- 
 parison of thermometers of similar glass. But as it seemed important 
 that the classical determinations of this physicist should be reduced to 
 some exact standard, I took to England with me last summer one of 
 my standards, Baudin, No. 6166, and sent it to Dr. Joule with a 
 statement of the circumstances. He very kindly consented to make 
 the comparison, and I now have the results before me. These confirm 
 the estimate that I had previously made, and cause our values for the 
 equivalent to agree with great accuracy. The following is the table of 
 the comparison : 
 
 Readings. 
 
 Temperatures. 
 
 
 
 By perfect Air 
 
 
 
 Baudin, No. 6166. 
 
 Joule. 
 
 Thermometer 
 according to 
 
 By Joule's 
 Thermometer. 
 
 Difference. 
 
 
 
 No. 6166. 
 
 
 
 21.88 
 
 22.62 
 
 8 
 
 8 
 
 o 
 
 
 41.930 
 
 59.410 
 
 1 . 590 
 
 1.578 
 
 .012 
 
 48.782 
 
 72.200 
 
 2.126 
 
 2.127 
 
 + .001 
 
 53.705 
 
 81.340 
 
 2.511 
 
 2.519 
 
 .008 
 
 58.916 
 
 90.877 
 
 2.918 
 
 2.928 
 
 .010 
 
 64.914 
 
 101.777 
 
 3.382 
 
 3.396 
 
 .014 
 
 73.374 
 
 117.291 
 
 4.039 
 
 4.061 
 
 .022 
 
 80.176 
 
 129.990 
 
 4.567 
 
 4.606 
 
 .039 
 
 85.268 
 
 139.255 
 
 4.961 
 
 5.003 
 
 .042 
 
 90.564 
 
 148.834 
 
 5.370 
 
 5.414 
 
 .044 
 
 94.243 
 
 155.460 
 
 5.654 
 
 5.698 
 
 .044 
 
 99.168 
 
 164.400 
 
 6.036 
 
 6.082 
 
 .046 
 
 104.030 
 
 173.140 
 
 6.413 
 
 6.457 
 
 .044 
 
 108.863 
 
 182.040 
 
 6.789 
 
 6.839 
 
 .050 
 
 113.706 
 
 190.885 
 
 7.165 
 
 7.218 
 
 .053 
 
 114.000 
 
 191.382 
 
 7.188 
 
 7.239 
 
 .051 
 
 '121.507 
 
 '219.497 
 
 '7.772 
 
 '8.445 
 
 
 1 Evidently a mistake in the readings. 
 
470 
 
 HENBY A. ROWLAND 
 
 Continued. 
 
 Readings. 
 
 Temperatures. 
 
 Baudin, No. 6166. 
 
 Joule. 
 
 By perfect Air 
 Thermometer 
 according to 
 No. 6166. 
 
 By Joule's 
 Thermometer. 
 
 Difference. 
 
 
 
 o 
 
 o 
 
 o 
 
 135.858 
 
 231.115 
 
 8.890 
 
 8.944 
 
 .054 
 
 140.467 
 
 239.939 
 
 9.249 
 
 9 . 309 
 
 .060 
 
 143.405 
 
 245.006 
 
 9.479 
 
 9.540 
 
 .061 
 
 146.445 
 
 250.566 
 
 9.717 
 
 9.778 
 
 .061 
 
 152.360 
 
 261.481 
 
 10.180 
 
 10.246 
 
 .066 
 
 158.770 
 
 273.239 
 
 10.681 
 
 10.751 
 
 070 
 
 164.635 
 
 283.957 
 
 11.138 
 
 11.211 
 
 .073 
 
 170.485 
 
 294 . 739 
 
 11 . 595 
 
 11.670 
 
 .075 
 
 175.436 
 
 303.682 
 
 11.979 
 
 12.057 
 
 .078 
 
 182.795 
 
 316.968 
 
 12.550 
 
 12.627 
 
 .077 
 
 188.705 
 
 327.746 
 
 13.008 
 
 13.089 
 
 .081 
 
 193.954 
 
 337.220 
 
 13.412 
 
 13.495 
 
 .083 
 
 199.558 
 
 347.294 
 
 13.844 
 
 13.928 
 
 .084 
 
 206.054 
 
 259.060 
 
 14.343 
 
 14.432 
 
 .089 
 
 211.528 
 
 368.953 
 
 14.764 
 
 14.857 
 
 .093 
 
 216.440 
 
 377.826 
 
 15.142 
 
 15.237 
 
 .095 
 
 221.858 
 
 387.562 
 
 15.560 
 
 15.655 
 
 .095 
 
 229.601 
 
 401.419 
 
 16.158 
 
 16.249 
 
 .091 
 
 235.598 
 
 412.367 
 
 16.623 
 
 16 . 719 
 
 .096 
 
 241.028 
 
 422.258 
 
 17.045 
 
 17.143 
 
 .098 
 
 247.436 
 
 433.800 
 
 17.541 
 
 17.638 
 
 .097 
 
 253.704 
 
 445.267 
 
 18.028 
 
 18.130 
 
 .102 
 
 259". 786 
 
 456.286 
 
 18.500 
 
 18.603 
 
 .103 
 
 266.086 
 
 467.817 
 
 19 . 991 
 
 19.097 
 
 .106 
 
 273 . 143 
 
 480.643 
 
 19.539 
 
 19.648 
 
 .109 
 
 280.176 
 
 493.442 
 
 20.086 
 
 20.197 
 
 .111 
 
 287.634 
 
 506.906 
 
 20.666 
 
 20.774 
 
 .108 
 
 294.927 
 
 520.052 
 
 21.232 
 
 21.338 
 
 .106 
 
 304.148 
 
 536.832 
 
 21.947 
 
 22.058 
 
 .111 
 
 310.397 
 
 548.152 
 
 22.432 
 
 22.544 
 
 .112 
 
 316.596 
 
 559.336 
 
 22.916 
 
 23.023 
 
 .107 
 
 321.271 
 
 568.051 
 
 23.282 
 
 23.397 
 
 .115 
 
 327.148 
 
 578.528 
 
 23.742 
 
 23.846 
 
 .104 
 
 333.661 
 
 590.661 
 
 24.251 
 
 24.367 
 
 .116 
 
 339.664 
 
 601.596 
 
 24.719 
 
 24.836 
 
 .117 
 
 346.557 
 
 614.004 
 
 25.254 
 
 25.369 
 
 .115 
 
 352.878 
 
 625.510 
 
 25.746 
 
 25.862 
 
 .116 
 
 359.986 
 
 638.526 
 
 26.299 
 
 26.421 
 
 .122 
 
 365.080 
 
 647 . 833 
 
 26.697 
 
 26.820 
 
 .123 
 
 371.811 
 
 660.071 
 
 27.225 
 
 27.345 
 
 .120 
 
 382.770 
 
 680.149 
 
 28.087 
 
 28.206 
 
 .119 
 
 We can discuss the comparison of these thermometers in two ways; 
 either by direct comparison at the points we desire, or by the repre- 
 sentation of the differences by a formula. 
 
 Joule's result in 1850 was referred to water at about 14 C., and in 
 1878 to water at 16 -5 C. Taking intervals in the above table of from 
 
APPENDIX TO THE MECHANICAL EQUIVALENT OF HEAT 471 
 
 6 to 12, so that the mean shall be nearly 14 and 16 -5, I find the 
 following for the ratios : 
 
 1-0044 1-0042 
 
 1-0042 1-0042 
 
 1-0049 1-0040 
 
 1-0047 1-0030 
 
 1-0047 1-0035 
 
 1-0052 1-0035 
 
 Mean, 1-0047 1-0037 
 
 So that we have the following for Joule's old and new values : 
 
 Old. New. 
 
 423-9 423-9 
 
 Correction for thermometer 2-0 1-6 
 
 Correction for latitude -5 -5 
 Correction for sp. ht. of copper -7 
 
 427-1 426-0 
 
 My value 427-7 427-1 
 
 Difference -6 1-1 
 
 or 1 in 700 and 1 in 390, respectively. 
 
 But the correction found in this way is subject to local irregulari- 
 ties, and it is perhaps better in many respects to get the equation giving 
 the temperature of Joule's thermometer on the air thermometer. Let 
 T be the temperature by Joule's thermometer, and t that by the air 
 thermometer. Then I have found 
 
 t = 0-002 + 1-00125 T -00013 \ 100 T\ \ 1 -003 (100 -f T) \ 
 
 The factor 1-00125 enters in the formula, probably because the ther- 
 mometer which Joule used to get the value of the divisions of his ther- 
 mometer was not of the same kind of glass as his standard. The rela- 
 tive error at any point due to using the mercurial rather than the air 
 thermometer will then be 
 
 E = 1 $** = 00125 + -00000039 \ 23300 666 t + 3 f\ 
 dT * 
 
472 
 
 HENRY A. ROWLAND 
 
 From this I have constructed the following table : 
 
 
 
 Approximate Addition to Equivalent 
 as measured on Joule's Thermometer. 
 
 Temperature. 
 
 
 
 
 
 
 Metric System. 
 
 English System. 
 
 
 
 .0078 
 
 3.3 
 
 6.0 
 
 5 
 
 .0066 
 
 2.8 
 
 5.1 
 
 10 
 
 .0054 
 
 2.3 
 
 4.2 
 
 15 
 
 .0042 
 
 1.8 
 
 3.2 
 
 20 
 
 .0031 
 
 1.8 
 
 2.4 
 
 25 
 
 .0021 
 
 .9 
 
 1.6 
 
 30 
 
 .0011 
 
 .5 
 
 .8 
 
 Corrected in this way we have, 
 
 Joule's value 
 
 Eeduction to air thermometer 
 Reduction to latitude of Baltimore 
 Correction for sp. ht. of copper 
 
 My value 
 Difference 
 
 Old. 
 
 423-9 
 1-9 
 
 5 
 
 7 
 
 427-0 
 
 427-7 
 
 New. 
 
 423-9 
 
 1-7 
 5 
 
 426-1 
 427-1 
 
 1-0 
 
 or 1 in 600 and 1 in 426, respectively. 
 
 But it is evident that all the other temperatures used in the experi- 
 ment must also be corrected, and I have done this in the following man- 
 ner. The principal other correction required is in the capacity of the 
 calorimeter, and this amounts to considerable in the experiments on 
 mercury and cast-iron, where no water is used. Dr. Joule informs me 
 that the thermometer with which he compared mine was made in 1844, 
 but does not give any mark by which to designate it, although it is evi- 
 dently the thermometer called "A" by him. I shall commence with the 
 experiments of 1847. The calorimeter was composed of the following 
 substances, whose capacities I recompute according to what in my paper 
 I have considered the most probable specific heats. 
 
 wai-o-ht Capacity accord- Most probable Most probable 
 ing to Joule. Specific Heat. Capacity. 
 
 Water 77617 grains 77617 1-000 77617 
 
 Brass 24800 grains 2319 -0900 2232 
 
 Copper 11237 grains 1056 -0922 1036 
 
 Tin (?) 363 363 
 
 Total capacity 
 
 81355 
 
 81248 
 
APPENDIX TO THE MECHANICAL EQUIVALENT OF HEAT 473 
 
 Equivalent found 781-5 at about 59 F. 
 
 Correction for thermometer 3-3 
 
 Correction for capacity 1-3 
 
 Correction for latitude -9 
 
 Corrected value 787-0 
 
 or 442-8 at 15 C. on the air thermometer. 
 
 The other experiment, on sperm oil, made at this time, is probably 
 hardly worth reducing. The experiments of 1850 are of the highest 
 importance and should be accurately reduced. 
 
 In the experiments with water the capacity of the calorimeter is cor- 
 rected as follows : 
 
 
 Weight. 
 
 Capacity used > 
 by Joule. S 
 
 [ost probable 
 peciflc Heat. 
 
 Most probable 
 Capacity. 
 
 Water 
 
 93229-7 
 
 93229-7 
 
 1-000 
 
 93229-7 ^ 
 
 Copper 
 
 25541- 
 
 2430-2 
 
 092 
 
 2349-8 * 
 
 Brass 
 
 18901- 
 
 1800-0 
 
 091 
 
 1720-0 
 
 Brass stopper 
 
 
 10-3 
 
 
 10-3 
 
 
 
 
 
 
 Total capacity 97470-2 97309-8 
 
 Therefore correction is -0016. 
 
 Hence the result with water requires the following corrections : 
 
 Joule's value 772-7 at 14 C. 
 Correction for thermometer 3-2 
 
 Correction for latitude -9 
 
 Correction for capacity 1-2 
 
 778-0 
 
 or 426-8 on the air thermometer in the latitude of Baltimore at the 
 temperature of 14 C., nearly. 
 
 In the next experiment, with mercury, Joule determined the capacity 
 of the apparatus by experiment. The mean of the experiments was that 
 the apparatus lost 20 -33155 F. in heating 143430 grains of water 
 3 13305 F. To reduce these to the air thermometer we must divide 
 respectively by 1-0042 and 1-0056. Therefore the capacity must be 
 divided by 1-0014. Therefore the corrected values are: 
 
 772-8 at 9 C. 775-4 at 11 C. 
 Correction for thermometer 4-4 4-0 
 
 Correction for capacity 1-1 1-1 
 
 Correction for latitude -9 -9 
 
 779-2 781-4 
 
474 HENEY A. ROWLAND 
 
 The reduction to the air thermometer was made for the temperatures 
 of 9 C. and 11 C. respectively, but they both refer to the temperature 
 of the water used when the capacity was determined; this was about 
 9 C. Hence these experiments gave 427-5 and 428-7 on the air ther- 
 mometer, with the water at about 9 C. 
 
 The next experiments, with cast-iron, can be corrected in the same 
 manner, and thus become 
 
 776-0 773-9 
 
 Correction for thermometer 4-2 4-3 
 
 Correction for capacity 1*1 !! 
 
 Correction for latitude -9 -9 
 
 782-2 780-2 
 
 and these are as before for water at 9. 
 
 The determination by the heating of a wire, whose resistance was 
 measured in ohms, can be thus reduced. The value found by Joule 
 was 429-9 in the latitude of Baltimore at 18 -6 C. 
 
 Using the capacity of the copper -0922, as I have done in my paper, 
 this quantity will be increased to 430-3. But I have given reasons in 
 my paper on the " Absolute Unit of Electrical Resistance " to show that 
 there should be a correction to the B. A. Committee's experiments, 
 which would make the ohm -993 earth quadrant -f- second, instead of 
 1-000 as it was meant to be, which nearly agrees with the quantity 
 which I found, namely, -991. Taking my value -9911, Joule's result 
 will reduce as follows : 
 
 429.9 at 18 -6 C. 
 
 Correction for thermometer -|- 1-5 
 
 Correction for capacity -|- -4 
 
 Corrected for ohm 3-8 
 
 Corrected value 428-0 at 18 -6 C. 
 
 The last determinations in the ' Philosophical Transactions ' of 1878 
 can be reduced as follows : 
 
 The capacity of the calorimeter was determined by experiment, in- 
 stead of calculated from the specific heat of copper given by Regnault, 
 as in the older experiments. The value used, 4842-4 grains, corre- 
 sponded to a specific heat of brass of about -090, which is almost exactly 
 what I have considered right. The reduction to the air thermometer 
 will decrease it somewhat, and the correction for the increase of the 
 
APPENDIX TO THE MECHANICAL EQUIVALENT OF HEAT 475 
 
 specific heat of brass and the decrease of the specific heat of water will 
 also change it somewhat. In all, the amount will be about 1 in 200. 
 Hence the reduction becomes as follows : 
 
 Joule's values 
 
 Correction for thermometer 
 Correction for capacity 
 Correction for latitude 
 Correction to vacuum 
 
 Corrected values 
 
 772-7 774-6 
 
 3-2 3-7 
 
 2 -2 
 
 9 -9 
 
 773-1 
 
 3-1 
 
 2 
 
 9 
 
 767-0 774-0 
 
 3-3 2-8 
 
 2 -2 
 
 9 -9 
 
 9 -9 
 
 776-1 778-5 776-4 770-5 777-0 
 at 14-7 atl2-7 at!2-5 at 14-5 at 17-3 
 
 To reduce the values in English measure to metres and the Centi- 
 grade scale, I have simply taken the reducing factor 1-8 X -304794, 
 although the barometer on the two systems is not exactly the same: 
 for this is taken into account in the comparison of the thermometers. 
 However, a barometer at 30 in. and 60 F. is equivalent to 759-86 mm. 
 at C. which hardly makes a difference of 0-01 C. in the temperature 
 of the hundred-degree point. 
 
 
 
 
 
 
 Joule's Value re- 
 
 
 
 
 
 
 
 
 
 duced to Air Ther- 
 
 <a 
 
 
 o . 
 
 No. 
 
 Date. 
 
 Method. 
 
 Tern, 
 of 
 
 Joule's 
 Value. 
 
 mometer and Lati- 
 tude of Baltimore. 
 
 q 
 
 J.-R. 
 
 11 
 
 
 
 
 
 
 
 
 o^ 
 
 
 to ^ 
 
 
 
 
 
 
 English 
 
 Metric 
 
 
 
 H 
 
 
 
 
 
 
 measure. 
 
 system. 
 
 
 
 
 
 
 
 o 
 
 
 
 
 
 
 
 1 
 
 1847 
 
 Friction of water 
 
 15 
 
 781.5 
 
 787.0 
 
 442.8 
 
 427.4 
 
 + 15.4 
 
 
 
 2 
 
 1850 
 
 water 
 
 14 
 
 772.7 
 
 778.0 
 
 426.8 
 
 427.7 
 
 .9 
 
 10 
 
 3 
 
 ' 
 
 mercury 
 
 9 772.8 
 
 779.2 
 
 427.5 
 
 428.8 
 
 1.3 
 
 2 
 
 4 
 
 ii 
 
 mercury 
 
 9 ! 775.4 
 
 781.4 
 
 428.7 
 
 428.8 
 
 .1 
 
 2 
 
 5 
 
 ii 
 
 iron 
 
 9 
 
 776.0 
 
 782.2 
 
 429.1 
 
 428.8 
 
 + .3 
 
 1 
 
 6 
 
 u 
 
 iron 
 
 9 
 
 773.9 
 
 780.2 
 
 428.0 
 
 428.8 
 
 - .8 
 
 1 
 
 7 
 
 1867 
 
 Elec ric heating 
 
 18.6 
 
 
 
 428.0 
 
 426.7 
 
 + 1.3 
 
 3 
 
 8 
 
 1878 
 
 Friction of water 
 
 14.7 
 
 772.7 
 
 776.1 
 
 425.8 
 
 427.6 
 
 - 1.8 
 
 2 
 
 9 
 
 u 
 
 u 
 
 12.7 
 
 774.6 
 
 778.5 
 
 427.1 
 
 428 . 
 
 .9 
 
 3 
 
 10 
 
 u 
 
 11 
 
 15.5 
 
 773.1 
 
 776.4 
 
 426.0 
 
 427.3 
 
 - 1.3 
 
 5 
 
 11 
 
 ii 
 
 u 
 
 14.5 
 
 767.0 
 
 770.5 
 
 422.7 
 
 427.5 
 
 - 4.8 
 
 1 
 
 12 
 
 " 
 
 ii 
 
 17.3 
 
 774.0 
 
 777.0 
 
 426.3 
 
 426.9 
 
 .6 
 
 1 
 
 In combining these so as to get at the true difference of Joule's and 
 my result, we must give these different determinations weights accord- 
 ing to their respective accuracy, especially as some of the results, as 
 No. 11, have very little weight. Joule rejected quite a number of his 
 results, but I have thought it best to include them, giving them small 
 weights, however. In this way we obtain a value for Joule's experiment 
 
476 HENEY A. ROWLAND 
 
 of 426-75 at 14 -6, my value at this point being 427-52. The difference 
 amounts to 1 in 550 only. Giving the observations equal weight, this 
 would have been 1 in 430 nearly. The quantity 426-75 is what I find 
 at 18 C. So that my result at this particular temperature differs from 
 that of Joule only the amount that water changes in specific heat in 
 3-4C. 
 
 Joule's value is less than my value to the amount given, but the value 
 from the properties of air, 430-7 at 14 C. is greater, although the 
 method can have little weight. 
 
 It might be well to diminish my values by 1 part in 1000 so as to make 
 them represent the mean of Joule's and my own experiments. It is 
 seen that the experiment by the method of electric heating agrees very 
 exactly with the other experiments, because I have reduced it to my value 
 of the ohm. Hence I regard it as a very excellent confirmation of my 
 value of that unit. 
 Baltimore, February 16, 1880. 
 
20 
 
 PHYSICAL LABORATOKY: COMPARISONS OF STANDARDS 
 
 [Johns Hopkins University Circulars, N~o. 3, p. 31, 1880] 
 
 In order to secure uniformity throughout the country in certain 
 physical standards, and to facilitate the use of the absolute system of 
 heat measurement, it has been thought advisable to organize in the 
 physical department of this University a sub-department, where com- 
 parisons of standards can be made. 
 
 Comparison of Thermometers. At present we are only able to make 
 comparisons of thermometers, and so to reduce their degrees to the abso- 
 lute scale of the perfect gas thermometer. 
 
 As the work is very laborious, it is proposed to make this sub-depart- 
 ment self-supporting, by a system of fees sufficient to cover the bare cost 
 of the labor, so that all may avail themselves of the facilities here 
 offered. 
 
 In a recent study of standard thermometers by Geissler, Baudin, 
 Fastre, Casella and from Kew, and the comparison of the same with 
 the air thermometer, the differences due to the variety of the glass 
 amounted to 0-2 or 0-3 C., and the differences from the air thermom- 
 eter were as high sometimes as 0-3 C. at the 40 point. 
 
 The error from using uncompared mercurial thermometers in calori- 
 metric investigations may amount to one or two per cent. For this 
 reason the air thermometer has been taken as the standard, and all com- 
 parisons will be reduced to the final absolute standard of the perfect 
 gas thermometer. 
 
 Very complete studies of thermometers have been made between 
 and 40 C., and a less complete study between and 100, and be- 
 tween 100 and 250. Up to 100 our thermometers have not only been 
 compared with the air thermometer, but also with standards by Fastre, 
 Geissler, Casella, Baudin and from Kew. 
 
 The study from to 40 has been published by the American Acad- 
 emy of Sciences, at Boston, in a memoir on the Mechanical Equivalent 
 of Heat. One of our thermometers is also now in the hands of Dr. 
 Joule, who has compared it with the original thermometers used by him 
 in the determination of the Mechanical Equivalent of Heat. 
 
478 HENKY A. EOWLAND 
 
 The apparatus for the comparison up to 100 C. is described in the 
 paper above referred to. The thermometers are totally immersed in 
 the water with their stems very near the bulbs of the air thermometers. 
 From 100 up to 250 an oil bath is used, the bulbs only being in the 
 oil, but the stems are heated to the same degree by being in contact with 
 a heavy copper bar, whose temperature is noted by separate thermome- 
 ters. 
 
 The ordinary comparison is made with the stems of the thermometers 
 in a vertical position. Where they are used in a horizontal position a 
 correction will have to be made, and this correction will be determined 
 when it is so desired. When the comparison is made only to 40, we 
 can compare them in a horizontal position, but we cannot then insure 
 the same accuracy as when they are vertical, and it is never advisable to 
 use them in that position. 
 
 Where desired, a study will be made of the changes of the zero point 
 as a function of the temperature to which it has been heated, and of the 
 time, but this study is not advised, as it does not lead to very valuable 
 results. 
 
 Thermometers with metal, wooden or paper scales are generally too 
 poor to be worth comparison, and would often be spoiled by the immer- 
 sion in the water. Thermometers with metal caps of Geissler's form 
 are often injured, especially when heated to 250 C. Therefore, com- 
 parisons of thermometers of these classes will not be undertaken, ex- 
 cept in the case of standards long used for some particular purpose, or 
 in that of fine G-eissler thermometers. 
 
 Three intervals for the comparison have been selected. 
 
 A. Between and 40 for thermometers used for meteorological 
 observations, determination of the temperature of standards of length, 
 calorimetric determinations, and all purposes where extreme accuracy is 
 desired within that limit. To obtain the full value of such a compari- 
 son, thermometers should be graduated at least as fine as 0-1 C. or 
 0-2F. 
 
 B. Between and 100 C. It is advised that the thermometers gent 
 be graduated at least as fine as 0-2 C. or 0-5 F. 
 
 C. Between 100 and 250 for thermometers used by chemists in the 
 determination of melting or boiling points. Thermometers should be 
 graduated to 1 C. or 1 F. 
 
 Three kinds of comparison will be made for each of the intervals 
 to 40, to 100, and 100 to 250, as follows: 
 
 1st. Direct comparison with the air thermometer, and also a primary 
 
PHYSICAL LABORATORY: COMPARISONS OF STANDARDS 479 
 
 standard. This comparison is very laborious, and is not recommended 
 except in very exceptional cases, as more than one comparison should 
 be made to insure good results. 
 
 2nd. Comparison with primary standards which have been compared 
 many times with the air thermometer. This is recommended where an 
 error of y^ is of some importance. 
 
 3rd. Comparison with secondary standards which have been com- 
 pared many times with the primary standards, and not very often 
 directly with the air thermometer. This is recommended in all ordi- 
 nary cases, where an error of yf^ can be tolerated. 
 
 When several comparisons are made, the following intervals will be 
 allowed between the experiments, so that the zero reading may be 
 allowed to return to its primitive value. 
 
 Thermometers heated to 40 C. about 1 week. 
 Thermometers heated to 100 C. about 6 weeks. 
 Thermometers heated to 250 C. about 4 months. 
 
 The latter interval is too small for an accurate return. 
 
 For the exact details of the method of comparison, I must refer to the 
 above mentioned paper on the Mechanical Equivalent of Heat. 
 
 It is advisable in all cases where great accuracy is desired, that a 
 numbers of comparisons be made, seeing that delicate thermometers are 
 constantly varying through slight limits, and the average state can only 
 be determined by repeated experiments. 
 
 Reports. In the report of the comparison, the original readings will 
 be given together with the reduced ones, and the plot of the curve of 
 errors of the thermometer at every point. From this curve, the error 
 of the thermometer at any reading can be found. 
 
 It is proposed to publish at the end of the year a complete report of 
 all the comparisons made during the year, together with all new deter- 
 minations of the errors of the standards, and to send it to any address 
 at a price which we will hereafter announce. 
 
 Fees. The comparators allow five thermometers only to be placed in 
 them, of which two are our own standards in ordinary comparisons, 
 and one in direct comparisons with the air thermometer. Therefore, 
 three thermometers can be compared as easily as one in ordinary cases, 
 and four in direct comparisons. Hence the following system of fees 
 has been made out. 
 
480 HENEY A. EOWLAND 
 
 A. When a number of Thermometers are sent 
 Comparison between and 40 C. for 3 or 4 thermometers. 
 
 Direct, probable error at each point =TOT $ 20 
 
 Primary Standards, probable error at each point C ^ T ^ T 11 00 
 Secondary Standards, probable error at each point = T f -g- 8 00 
 
 and 100 for 3 or 4 thermometers. 
 
 Direct, probable error at each point = T ^ $25 00 
 
 Primary Standards, probable error at each point = ^-3- 12 00 
 Secondary Standards, probable error at each point = T ^ 9 00 
 
 100 to 250 for 3 or 4 thermometers. 
 
 Direct, probable error at each point y 1 ^ $20 00 
 
 Primary Standards, probable error at each point = y 1 ^ 12 00 
 Secondary Standards, probable error at each point = -^ 9 00 
 
 B. For Single Thermometers 
 
 For single thermometers, the fees for the direct comparisons should 
 be reduced to one-third, and' for the ordinary ones to one-half the 
 above figures. But in this case the thermometer will have to remain 
 here until enough accumulate to fill the comparators. 
 
 Directions for Sending. With each thermometer, send the name of 
 maker, the date when made, purpose for which it is used, and the 
 highest temperature to which it has lately been heated, and the date 
 of such heating, together with the kind of comparison desired, and 
 whether the thermometer is generally used in the horizontal or the 
 vertical position. 
 
 In packing, the thermometer should be placed in a small box, which 
 should again be packed with straw in a larger box. 
 
 The thermometers, both during transit and while here, must be at 
 the owners' risk. Only sufficient fees have been charged to cover the 
 bare cost of the comparison, and we bear the risk of our own standards, 
 which are probably more valuable than any of those which will be sent 
 to us. But every care will be taken, and the probability of an accident 
 is very small. 
 
 We expect soon to be able to make other comparisons, and notice will 
 then be given of the fact by the issue of another circular. 
 
26 
 
 ON GEISSLEK THERMOMETERS: REMARKS BY PROFESSOR 
 ROWLAND ON THE PRECEDING LETTER, 1 IN A COMMU- 
 NICATION DATED JOHNS HOPKINS UNIVERSITY, APRIL 
 29, 1881 
 
 [American Journal of Science [3], XXI, 451-453, 1881] 
 
 Through the kindness of Dr. Waldo, I have been allowed to see the 
 above and would like to give a few words of explanation. 
 
 In reading what I had to say with respect to the Geissler thermom- 
 eter, the reader should remember that I was not writing on general 
 thermometry, but only on that part which should be useful to me in 
 measuring differences of temperature within the limits of and 45 C. 
 And so I merely made a study of thermometers, their change of zero 
 and other points, as it affected the problem which I had before me. I 
 am well aware that there are formulae for giving the changed readings 
 of thermometers due to previous heating, but, according to well known 
 principles in such cases, I preferred to eliminate such error by the 
 proper use of the thermometer rather than trust to an uncertain theory. 
 
 In the course of my investigation I discovered the fact that the 
 Geissler thermometers, especially the one I then used, departed more 
 from the air thermometer than any other. Now the Geissler ther- 
 mometer has been used for many years by physicists, principally Ger- 
 man, without any reduction to the air thermometer. And this correc- 
 tion was so great, amounting to over 0-3 C., for the specimen I used, at 
 the 45 point, that I thought it right to call attention to the point. 
 And I acknowledge that the picture was present in my mind of a physi- 
 cist reading a thermometer from a distance by a telescope to avoid the 
 heat of the body and parallax, and recording his results to thousandth 
 of a degree, and all this on a thermometer having an error of 0-3 C. ! 
 As Dr. Thiesen remarks: If one is to compare his thermometer with 
 the air thermometer, the amount of correction is of little importance: 
 but departure from the air thermometer is certainly not a recommenda- 
 tion and, indeed, must introduce slight errors. The most accurate 
 
 1 [By Dr. M. Thiesen, replying to Rowland's criticisms of the Geissler thermometers, 
 as expressed in his memoir 'On the Mechanical Equivalent of Heat.'] 
 31 
 
482 HENRY A. ROWLAND 
 
 readings which one can make on an air thermometer will vary several 
 hundredths of a degree. 
 
 Hence we can never use with accuracy the direct comparison with the 
 air thermometer but must express the difference of the two instruments 
 by some formula of the form: 
 
 J = a + bt + ci 1 + &c. 
 
 Should we take an infinite number of terms this formula would ex- 
 press all the irregularities of our observations. But by limiting the 
 number of terms the curve of differences becomes smoother and 
 smoother and the formula expresses less and less the irregularities of 
 the experiment. The number of terms to be used is a matter of judg- 
 ment, and this point I sought to determine by the use of the observa- 
 tions of Eegnault and others. The rejection of the higher powers of t 
 is more or less of an assumption founded on the fact that we are 
 reasonably certain that the curve of differences between the mercurial 
 and the air thermometer is a smooth curve. It is evident that the 
 less the correction to be introduced the less the rejection of the higher 
 powers of t will affect our results. 
 
 We now come to my criticism of the Geissler thermometer for not 
 having a reservoir at the top. Dr. Thiesen has in some way misunder- 
 stood my principal reason for its presence. My reason was not that 
 " es vermindert die Schadlichkeit der im Quecksilber zuriickgebliebenen 
 Spuren von Luft " but that only by its use can the mercury in the bulb 
 be entirely free from air. Take a thermometer and turn it with the 
 bulb on top. If the thermometer is large, in nine cases out of ten the 
 mercury will separate and fall down: allow it to remain and observe the 
 bubble-like vacuum in the bulb. Turn the bulb in various directions so 
 as to wash the whole interior of the bulb, as it were, and then bring 
 the thermometer into a vertical position, keeping the bubble in sight. 
 As the mercury flows back, the bubble diminishes and finally, in a good 
 thermometer, almost disappears: but in most thermometers a good 
 sized bubble of air, in some cases as large as the wire of a pin, remains. 
 It is the most important function of a reservoir at the top to permit 
 such manipulations as to drive all such air into the top reservoir and to 
 make the mercury and the glass assume such perfect contact that the 
 bulb can be turned uppermost without the mercury separating, even in 
 thermometers of large size and with good generous bulbs. In many 
 Geissler thermometers such a test might succeed, not on account of the 
 freedom from air, but because the capillary tube and bulb are so small 
 
Ox THE GEISSLER THERMOMETEKS 483 
 
 and the column so short that the capillary action is sufficient to prevent 
 the fall. Now I think that a thermometer in which there is this layer 
 of air around the mercury in the bulb must be uncertain in its action; 
 hence my opinion is unaltered that all thermometers in which we can- 
 not remove this layer or at least make certain of its absence should be 
 rejected. 
 
 Furthermore, with respect to calibration, the reservoir is not essen- 
 tial to the calibration of thermometers whose range is and 100 C. 
 But my remarks apply better to those whose range is between and 
 30 C. or 40 C. Here calibration is impossible with a short column 
 at ordinary temperatures unless some of the mercury can be stored up 
 in the reservoir so as to allow the column to move over the whole scale. 
 And it is within this limit that thermometers are of the greatest value 
 in the physical laboratory. 
 
 The other defects of the Geissler thermometer, the scale which was 
 always coming loose, the metal cap which was never tight and always 
 allowe'd water to enter, the small capillary tube which wandered with 
 perfect irregularity from side to side over the scale, all these were so 
 obvious that I confined my remarks to the more obscure errors. 
 
 Furthermore, I believe there is some error in most Geissler ther- 
 mometers from the small size of the bulb and the capillary tube, and 
 this I have mentioned on p. 124 ' of the paper referred to. Pfaundler 
 and Platter, in a paper on the specific heat of water, in Poggendorff's 
 Annalen for 1870, found an immense variation within small limits. In 
 a subsequent paper 2 the authors traced this'error to the lagging of the 
 thermometer behind its true reading. 
 
 The authors used Geissler thermometers graduated to ^j- C. ! in a 
 series of experiments made by plunging the thermometer into water 
 after slightly heating or cooling the thermometer so that in one case 
 the mercury fell and the other rose to the required point. When the 
 thermometer fell about 6 or 8 C. it lagged behind 0-0654 and when 
 it rose 3 or 4 it lagged 0-022, making a difference of 0-087 C.! Now 
 my thermometers made by Baudin show no effect of this kind. They 
 indicate accurately the temperature whether they rise or fall to the 
 given point, provided the interval is not too great. The fact then 
 remains that a Geissler thermometer graduated to 7 V C. may be uncer- 
 tain to 0-087C., while a Baudin graduated to mm., one mm. being 
 from T V to T V C. is not uncertain to 0-01 or 0-02 C. May not the 
 
 1 [p. 393 this volume.! * Poggendorff's Annalen, cxli, p. 537. 
 
484 HENEY A. KOWLAND 
 
 cause be found in the layer of air around the mercury of the bulb 
 which cannot be removed without a reservoir at the top? Or may we 
 not also look for such an effect from the minute size of the bore of the 
 capillary tube which creates a different pressure in the bulb from a 
 rising or falling meniscus ? Possibly the two may be combined. 
 
PART IV 
 
 LIGHT 
 
29 
 
 PRELIMINARY NOTICE OF THE RESULTS ACCOMPLISHED 
 IN THE MANUFACTURE AND THEORY OF GRATINGS FOR 
 OPTICAL PURPOSES 
 
 [Johns Hopkins University Circulars, No. 17, pp. 248, 249, 1882 ; Philosophical Magazine 
 [4], XIII, 469-474, 1882; Nature, 26, 211-213, 1882; Journal de Physique, 
 II, 5-11, 1883] 
 
 It is not many years since physicists considered that a spectroscope 
 constructed of a large number of prisms was the best and only instru- 
 ment for viewing the spectrum, where great power was required. These 
 instruments were large and expensive, so that few physicists could pos- 
 sess them. Professor Young was the first to discover that some of the 
 gratings of Mr. Rutherfurd showed more than any prism spectroscope 
 which had then been constructed. But all the gratings which had been 
 made up to that time were quite small, say one inch square, whereas 
 the power of a grating in resolving the lines of the spectrum increases 
 with the size. Mr. Rutherfurd then attempted to make as large grat- 
 ings as his machine would allow, and produced some which were nearly 
 two inches square, though he was rarely successful above an inch and 
 three-quarters, having about thirty thousand lines. These gratings 
 were on speculum metal and showed more of the spectrum than had 
 ever before been seen, and have, in the hands of Young, Rutherfurd, 
 Lockyer and others, done much good work for science. Many mechanics 
 in this country and in France and Germany, have sought to equal 
 Mr. Rutherfurd' s gratings, but without success. 
 
 Under these circumstances, I have taken up the subject with the 
 resources at command in the physical laboratory of the Johns Hopkins 
 University. 
 
 One of the problems to be solved in making a machine is to make a 
 perfect screw, and this, mechanics of all countries have sought to do 
 for over a hundred years and have failed. On thinking over the matter, 
 I devised a plan whose details I shall soon publish, by which I hope to 
 make a practically perfect screw, and so important did the problem seem 
 that I immediately set Mr. Schneider, the instrument maker of the 
 university, at work at one. The operation seemed so successful that I 
 
488 HENRY A. ROWLAND 
 
 immediately designed the remainder of the machine, and have now had 
 the pleasure since Christmas of trying it. The screw is practically per- 
 fect, not by accident, but because of the new process for making it, and 
 I have not yet been able to detect an error so great as one one-hundred- 
 thousandth part of an inch at any part. Neither has it any appreciable 
 periodic error. By means of this machine I have been able to make 
 gratings with 43,000 lines to the inch, and have made a ruled surface 
 with 160,000 lines on it, having about 29,000 lines to the inch. The 
 capacity of the machine is to rule a surface 6^ x 4| inches with any 
 required number of lines to the inch, the number only being limited by 
 the wear of the diamond. The machine can be set to almost any num- 
 ber of lines to the inch, but I have not hitherto attempted more than 
 43,000 lines to the inch. It ruled so perfectly at this figure that I see 
 no reason to doubt that at least two or three times that number might 
 be ruled in one inch, though it would be useless for making gratings. 
 
 *A11 gratings hitherto made have been ruled on flat surfaces. Such 
 gratings require a pair of telescopes for viewing the spectrum; these 
 telescopes interfere with many experiments, absorbing the extremities 
 of the spectrum strongly; besides, two telescopes of sufficient size to 
 use with six inch gratings would be very expensive and clumsy affairs. 
 In thinking over what would happen were the grating ruled on a sur- 
 face not flat, I thought of a new method of attacking the problem, and 
 soon found that if the lines were ruled on a spherical surface the 
 spectrum would be brought to a focus without any telescope. This 
 discovery of concave gratings is important for many physical investiga- 
 tions, such as the photographing of the spectrum both in the ultra- 
 violet and the ultra-red, the determination of the heating effect of the 
 different rays, and the determination of the relative wave lengths of 
 the lines of the spectrum. Furthermore it reduces the spectroscope to 
 its simplest proportions, so that spectroscopes of the highest power may 
 be made at a cost which can place them in the hands of all observers. 
 With one of my new concave gratings I have been able to detect double 
 lines in the spectrum which were never before seen. 
 
 The laws of the concave grating are very beautiful on account of their 
 simplicity, especially in the case where it will be used most. Draw the 
 radius of curvature of the mirror to the centre of the mirror, and from 
 its central point with a radius equal to half the radius of curvature 
 draw a circle; this circle thus passes through the centre of curvature 
 of the mirror and touches the mirror at its centre. Now if the source 
 of light is anywhere in this circle, the image of this source and the 
 
GRATINGS FOR OPTICAL PURPOSES 489 
 
 different orders of the spectra are all brought to focus on this circle. 
 The word focus is hardly applicable to the case, however, for if the 
 source of light is a point the light is not brought to a single point on 
 the circle but is drawn out into a straight line with its length parallel 
 to the axis of the circle. As the object is to see lines in the spectrum 
 only, this fact is of little consequence provided the slit which is the 
 source of light is parallel to the axis of the circle. Indeed it adds to 
 the beauty of the spectra, as the horizontal lines due to dust in the slit 
 are never present, as the dust has a different focal length from the lines 
 of the spectrum. This action of the concave grating, however, some- 
 what impairs the light, especially of the higher orders, but the intro- 
 duction of a cylindrical lens greatly obviates this inconvenience. 
 
 The beautiful simplicity of the fact that the line of foci of the dif- 
 ferent orders of the spectra are on the circle described above leads 
 immediately to a mechanical contrivance by which we can move from 
 one spectrum to the next and yet have the apparatus always in focus; 
 for we only have to attach the slit, the eye-piece and the grating to three 
 arms of equal length, which are pivoted together at their other ends 
 and the conditions are satisfied. However we move the three arms the 
 spectra are always in focus. The most interesting case of this contriv- 
 ance is when the bars carrying the eye-piece and grating are attached 
 end to end, thus forming a diameter of the circle with the eye-piece at 
 the centre of curvature of the mirror, and the rod carrying the slit 
 alone movable. In this case the spectrum as viewed by the eye-piece 
 is normal, and when a micrometer is used the value of a division of its 
 head in wave-lengths does not depend on the position of the slit, but 
 is simply proportional to the order of the spectrum, so that it need be 
 determined once only. Furthermore, if the eye-piece is replaced by a 
 photographic camera the photographic spectrum is a normal one. The 
 mechanical means of keeping the focus* is especially important when 
 investigating the ultra-violet and ultra-red portions of the solar 
 spectrum. 
 
 Another important property of the concave grating is that all the 
 superimposed spectra are in exactly the same focus. When viewing 
 such superimposed spectra it is a most beautiful sight to see the lines 
 appear colored on a nearly white ground. By micrometric measurement 
 of such superimposed spectra we have a most beautiful method of 
 determining the relative wave lengths of the different portions of the 
 spectrum, which far exceeds in accuracy any other method yet devised. 
 In working in the ultra-violet or ultra-red portions of the spectrum we 
 
490 HENRY A. EOWLAND 
 
 can also focus on the superimposed spectrum and so get the focus for 
 the portion experimented on. 
 
 The fact that the light has to pass through no glass in the concave 
 grating makes it important in the examination of the extremities of 
 the spectrum where the glass might absorb very much. 
 
 There is one important research in which the concave grating in its 
 present form does not seem to be of much use, and that is in the exami- 
 nation of the solar protuberances; an instrument can only be used for 
 this purpose in which the dust in the slit and the lines of the spectrum 
 are in focus at once. It might be possible to introduce a cylindrical 
 lens in such a way as to obviate this difficulty. But for other work on 
 the sun the concave grating will be found very useful. But its principal 
 use will be to get the relative wave lengths of the lines of the spectrum, 
 and so to map the spectrum; to divide lines of the spectrum which are 
 very near together, and so to see as much as possible of the spectrum; 
 to photograph the spectrum so that it shall be normal; to investigate 
 the portions of the spectrum beyond the range of vision; and lastly to 
 put in the hands of any physicist at a moderate cost such a powerful 
 instrument as could only hitherto be purchased by wealthy individuals 
 or institutions. 
 
 To give further information of what can be done in the way of grat- 
 ings I will state the following particulars : 
 
 The dividing engine can rule a space 6| inches long and 4 inches 
 wide. The lines, which can be 4^ inches long, do not depart from a 
 straight line so much as nnnnnr inch, and the carriage moves forward in 
 an equally straight line. The screw is practically perfect and has been 
 tested to nnmnj" inch without showing error. Neither does it have any 
 appreciable periodic error, and the periodic error due to the mounting 
 and graduated head can be entirely eliminated by a suitable attachment. 
 For showing the production of ghosts by a periodic error, such an error 
 can be introduced to any reasonable amount. Every grating made by 
 the machine is a good one, dividing the 1474 line with ease, but some 
 are better than others. Eutherfurd's machine only made one in every 
 four good, and only one in a long time which might be called first-class. 
 One division of the head of the screw makes 14,438 lines to the inch. 
 Any fraction of this number in which the numerator is not greater 
 than say 20 or 30 can be ruled. Some exact numbers to the millimetre, 
 such as 400, 800, 1200, etc., can also be ruled. For the finest definition 
 either 14,438 or 28,876 lines to the inch are recommended, the first for 
 ordinary use and the second for examining the extremities of the 
 
GRATINGS FOR OPTICAL PURPOSES 491 
 
 spectrum. Extremely brilliant gratings have been made with 43,314 
 lines to the inch, and there is little difficulty in ruling more if desired. 
 The following show some results obtained: 
 
 Flat grating, 1 inch square, 43,000 lines to the inch. Divides the 
 1474 line in the first spectrum. 
 
 Flat grating, 2X3 inches, 14,438 lines to the inch, total 43,314. 
 Divides 1474 in the first spectrum, the E line (Angstrom 5269-4) in 
 the second and is good in the fourth and even fifth spectrum. 
 
 Flat grating, 2X3 inches, 1200 lines to one millimetre. Shows very 
 many more lines in the B and A groups than were ever before seen. 
 
 Flat grating, 2 X 3 inches, 14,438 lines to the inch. This has most 
 wonderful brilliancy in one of the first spectra, so that I have seen 
 the Z line, wave-length 8240 (see Abney^s map of the ultra-red region), 
 and determined its wave-length roughly, and have seen much further 
 below the A line than the B line is above the A line. The same may 
 be said of the violet end of the spectrum. But such gratings are only 
 obtained by accident. 
 
 Concave grating, 2X3 inches, 7 feet radius of curvature, 4818 lines 
 to the inch. The coincidences of the spectra can be observed to the 
 tenth or twelfth spectrum. 
 
 Concave grating, 2X3 inches, 14,438 lines to the inch, radius of cur- 
 vature 8 feet. Divides the 1474 line in the first spectrum, the E line 
 in the second, and is good in the third or fourth. 
 
 Concave grating, 3 X 5 inches, 17 feet radius of curvature, 28,876 
 lines to the inch, and thus nearly 160,000 lines in all. This shows 
 more in the first spectrum than was ever seen before. Divides 1474 
 and E very widely and shows the stronger component of Angstrom 5275 
 double. Second spectrum not tried. 
 
 Concave grating, 4 X 5f inches, 3610 lines to the inch, radius of cur- 
 vature 5 feet 4 inches. This grating was made for Professor Langley's 
 experiments on the ultra-red portion of the spectrum, and was thus 
 made very bright in the first spectrum. The definition seems to be 
 very fine notwithstanding the short focus and divides the 1474 line with 
 ease. But it is difficult to rule so concave a grating as the diamond 
 marks differently on the different parts of the plate. 
 
 These give illustrations of the results accomplished, but of course 
 many other experiments have been made. I have not yet been able to 
 decide whether the definition of the concave grating fully comes up to 
 that of a flat grating, but it evidently does so very nearly. 
 
30 
 ON CONCAVE GEATINGS FOE OPTICAL PUEPOSES * 
 
 [American Journal of Science [3], XXVI, 87-98, 1883 ; Philosophical Magazine 
 [5], XVI, 197-210, 1883] 
 
 GENERAL THEORY 
 
 Having recently completed a very successful machine for ruling 
 gratings, my attention was naturally called to the effect of irregularity 
 in the form and position of the lines and the form of the surface on 
 the definition of the grating. Mr. C. S. Peirce has recently shown, in 
 the American Journal of Mathematics, that a periodic error in the 
 ruling produces what have been called ghosts in the spectrum. At first 
 I attempted to calculate the effect of other irregularities by the ordi- 
 nary method of integration, but the results obtained were not commen- 
 surate with the labor. I then sought for a simpler method. Guided by 
 the fact that inverse methods in electrical distribution are simpler 
 than direct methods, I soon found an inverse method for use in this 
 problem. 
 
 In the use of the grating in most ordinary spectroscopes, the tele- 
 scopes are fixed together as nearly parallel as possible, and the grating 
 turned around a vertical axis to bring the different spectra into the 
 field of view. The rays striking on the grating are nearly parallel, 
 but for the sake of generality I shall assume that they radiate from a 
 point in space and shall investigate the proper ruling of the grating 
 to bring the rays back to the point from which they started. The wave 
 fronts will be a series of spherical shells at equal distances apart. If 
 
 J An abstract of this paper with some other matter was given at the Physical 
 Society of London in November last, the paper being in my hand in its present shape 
 at that time. As I wished to make some additions, for which I have not yet had 
 time, I did not then publish it. I was much surprised soon after to see an article 
 on this subject which had been presented to the Physical Society and was published 
 in the Philosophical Magazine. The article contains nothing more than an exten- 
 sion of my remarks at the Physical Society and formula; similar to those in this 
 paper. As I have not before Ihis published anything except a preliminary notice of 
 the concave gratings, I expected a little time to work up the subject, seeing that the 
 practical work of photographing the spectrum has recently absorbed all my time. 
 But probably I have waited too long. 
 
ON CONCAVE GRATINGS FOR OPTICAL PURPOSES 493 
 
 these waves strike on a reflecting surface, they will be reflected back 
 provided they can do so all in the same phase. A sphere around the 
 radiant point satisfies the condition for waves of all lengths and thus 
 gives the case of ordinary reflection. Let any surface cut the wave 
 surfaces in any manner and let us remove those portions of the surface 
 which are cut by the wave surfaces; the light of that particular wave- 
 length can then be reflected back along the same path in the same 
 phase and thus, by the above principle, a portion will be sent back. 
 But the solution holds for only one wave-length and so white light will 
 be drawn out into a spectrum. Hence we have the important conclu- 
 sion that a theoretically perfect grating for one position of the slit and 
 eye-piece can be ruled on any surface, flat or otherwise. This is an 
 extremely important practical conclusion and explains many facts which 
 have been observed in the use of gratings. For we see that errors of 
 the dividing engine can be counterbalanced by errors in the flatness of 
 the plate, so that a bad dividing engine may now and then make a 
 grating which is good in one spectrum but not in all. And so we often 
 find that one spectrum is better than another. Furthermore Professor 
 Young has observed that he could often improve the definition of a 
 grating by slightly bending the plate on which it was ruled. 
 
 From the above theorem we see that if a plate is ruled in circles 
 whose radius is r sin [JL and whose distance apart is dr / sin //, where Ar 
 is constant, then the ruling will be appropriate to bring the spectrum 
 to a focus at a distance, r, and angle of incidence, //. Thus we should 
 need no telescopes to view the spectrum in that particular position of 
 the grating. Had the wave surfaces been cylindrical instead of spher- 
 ical the lines would have been straight instead of circular, but at the 
 above distances apart. In this case the spectrum would have been 
 brought to a focus, but would have been diffused in the direction of 
 the lines. In the same way we can conclude that in flat gratings any 
 departure from a straight line has the effect of causing the dust in the 
 slit and the spectrum to have different foci, a fact sometimes observed. 
 
 We also see that, if the departure from equal spaces is small, or, in 
 other words, the distance r is great, the lines must be ruled at distances 
 apart represented by 
 
 r sin n 
 
 in order to bring the light to a focus at the angle p. and distance r, c 
 being a constant and x the distance from some point on the plate. If 
 f* changes sign, then r must change in sign. Hence we see that the 
 
494 HENKY A. ROWLAND 
 
 effect of a linear error in the spacing is to make the focus on one side 
 shorter and the other side longer than the normal amount. Professor 
 Peirce has measured some of Mr. Eutherfurd's gratings and found that 
 the spaces increased in passing along the grating, and he also found 
 that the foci of symmetrical spectra were different. But this is the 
 first attempt to connect the two. The definition of a grating may 
 thus be very good even when the error of run of the screw is consider- 
 able, provided it is linear. 
 
 CONCAVE G-KATINGR 
 
 Let us now take the special case of lines ruled on a spherical surface; 
 and let us not confine ourselves to light coming back to the same point, 
 but let the light return to another point. Let the co-ordinates of the 
 radiant point and focal point be y<=0, x = a and y = 0, x*+- a, and 
 let the centre of the sphere whose radius is p be at x r , y'. Let r be the 
 distance from the radiant point to the point x, y, and let R be that from 
 the focal point to x, y. Let us then write 
 
 2b = R -f re, 
 
 where c is equal to 1 according as the reflected or transmitted ray is 
 used. Should we increase b by equal quantities and draw the ellip- 
 soids or hyperboloids so indicated, we could use these surfaces in the 
 same way as the wave surfaces above. The intersections of these 
 surfaces with any other surface form what are known as Huyghens' 
 zones. By actually drawing these zones on the surface, we form a 
 grating which will diffract the light of a certain wave-length to the 
 given focal point. For the particular problem in hand, we need only 
 work in the plane x, y for the present. 
 
 Let s be an element of the curve of intersection of the given surface 
 with the plane x, y. Then our present problem is to find the width of 
 Huyghens' zones on the surface, that is ds in terms of db. 
 
 The equation of the circle is 
 
 (x-xy + (y-y'? = f>* 
 and of the ellipse or hyperbola 
 
 R + re = 2* 
 
 or (i 2 a 2 ) x 3 + fry 2 = tf(V a' i ) 
 
 in which c has disappeared. 
 
 dx y y' 
 
 - --- 
 
ON CONCAVE GRATINGS FOR OPTICAL PURPOSES 495 
 
 dzl (b z a 2 ) xPy ^^ } = b\W 
 
 - (a? 
 
 x x 
 
 . - ,b 
 " 
 
 (V + y* + a 2 ) 
 
 This equation gives us the proper distance of the rulings on the sur- 
 face, and if we could get a dividing engine to rule according to this 
 formula the problem of bringing the spectrum to a focus without tele- 
 scopes would be solved. But an ordinary dividing engine rules equal 
 spaces and so we shall further investigate the question whether there 
 is any part of the circle where the spaces are equal. We can then write 
 
 ds __ n 
 db~ 
 
 And the differential of this with regard to an arc of the circle must 
 be zero. Differentiating and reducing by the equations 
 
 dx _ _y y' . db _ p 
 ~dy ~ x=2' ~dy ~ G (x a/)' 
 we have 
 
 P { 2xb (y y'} - 2yb (x x'}- - [6i a - (a? + y 1 + a 1 )] } 
 
 It is more simple to express this result in terms of E, r, p and the 
 angles between them. 
 
 Let fi. be the angle between p and r, and v that between p and R. Let 
 us also put 
 
 Let /?, f and 3 also represent the angles made by r, R and p respec- 
 tively with the line joining the source of light and focus, and let 
 
 Then we have 
 
 _ R cos f + r cos ,5 _ R sin f + r sin p _r cos /3 R cos y 
 
 -I 2/ 9 9. " 
 
496 HENKY A. ROWLAND 
 
 (b* - a^(y -y'T + P (x - x'J = f ( 2 - 8 sin 2 3) , 
 I 1 a* = Rr cos 2 a , 
 
 R -\- r ir _ R 
 
 simj = ^ sin a; cos -n = - cos a, 
 2a 2a 
 
 = --, = -, 
 
 
 
 T cos 7] sin r sin ft Rr . 
 
 x=b - r ; v = a -. '- - - = r- sm in cos a , 
 
 COS a Sin a COS a 
 
 Vy (y -y'}+x (I* - a 2 ) (a; - aT) = (cos ,,. + cos 
 
 26 2 (V + */ 2 + O = #r, 
 
 - x')= (sin n + sin v) 
 
 sin /jt + sin v cos a sin e 
 2a cos 5 = r cos /j. R cos y , 
 2a sin 5 = r sin /* R sin v . . 
 On substituting these values and reducing, we find 
 
 2 2Rr cos a cos e 
 
 ~ r cos 2 y + R cos 2 n ' 
 
 ds 
 
 2 A more simple solution is the following: _ mnst be constant in the direction 
 
 do 
 
 in which the dividing engine rules. If the dividing engine rules in the direction of 
 the axis y, the differential of this with respect to y must be zero. But we can also 
 take the reciprocal of this quantity and so we can write for the equation of condi- 
 tion 
 
 d d(R+ r) _ 
 
 dy ds 
 
 Taking a circle as our curve we can write 
 
 (Z_X')2+ ( y yf)* = p* 
 
 and (x x")* + (y y"V = -R 2 , 
 
 (X - 2///)2 + (y - y'")1 = r 2 , 
 
 + r)_ i ( ,j*-x" x-x>\_ { ^_^ly-y" + y-v"'\) 
 
 ~~i\ (l/ y \2t - J \~~W~ ~r - j} 
 
 (R + r) _ 1 r x x"x x'" , \~ x x")(y y"} 
 
 dT~ ~yj~ R- ~T~ ~^~~ 
 
 \ _<r 
 
 Making x = 0, y = 0, y' = 0, x' p, 
 
 we have x" x f " I x //2 x /// ~i\ 
 
 ~ ' ~ P ~ + ~ = ' 
 
 _n cos p + cos v _ 2Rr cos a cose 
 
 r cos" v + R cos 2 u r cos 2 v + R cos 2 u ' 
 
Ox CONCAVE GRATINGS FOR OPTICAL PURPOSES 
 
 497 
 
 Whence the focal length is 
 
 
 pR cos' 
 
 COS a COS p COb v 
 
 For the transmitted beam, change the sign of R. Supposing p, R and v 
 to remain constant and r and // to vary, this equation will then give the 
 line on which all the spectra and the central image are brought to a 
 focus. 
 
 By far the most interesting case is obtained by making 
 
 since these values satisfy the equation. The line of foci is then a 
 circle with a radius equal to one-half p. Hence if a source of light 
 
 FIG. i. 
 
 exists on this circle, the reflected image and all the spectra will be 
 brought to a focus on the same circle. Thus if we attach the slit, the 
 eye-piece and the grating to the three radii of the circle, however we 
 move them, we shall always have some spectrum in the focus of the 
 eye-piece. But in some positions the line of foci is so oblique to the 
 direction of the light that only one line of the spectrum can be seen 
 well at any one time. The best position of the eye-piece as far as we 
 consider this fact is thus the one opposite to the grating and at its 
 centre of curvature. In this position the line of foci is perpendicular 
 to the direction of the light, and we shall show presently that the 
 spectrum is normal at this point whatever the position of the slit, pro- 
 vided it is on the circle. 
 
 Fig. 1 represents this case; A is the slit, C is the eye-piece, and B is 
 the grating with its centre of curvature at C. In this case all the con- 
 ditions are satisfied by fixing the grating and eye-piece to the bar BC 
 32 
 
498 HENRY A. ROWLAND 
 
 whose ends rest on carriages moving on the rails AB and AC at right 
 angles to each other; when desired, the radius AD may be put in to hold 
 everything steady, but this has been found practically unnecessary. 
 
 The proper formula? for this case are as follows: If ^ is the wave- 
 length and w the distance apart of the lines of the grating from centre 
 to centre, then we have 
 
 1 _ IN _ sin v 
 
 ~~d~ %w~ ~T~ 
 
 where N is the order of the spectrum. 
 
 w sin v 
 
 / = 
 
 Now in the given case p is constant and so NX is proportional to the 
 line AC. Or, for any given spectrum, the wave-length is proportional 
 to that line. 
 
 If a micrometer is fixed at C we can consider the case as follows : 
 
 1 )N 
 -tf ^^(sin^ + sinv), 
 
 d). w 
 
 7i~ = ~W cos /* 
 a/i N 
 
 If D is the distance the cross-hairs of the micrometer move forward 
 for one division of the head, we can write for the point C 
 
 A., = I- 
 
 !' 
 
 and for the same point ft is zero. Hence 
 
 But this is independent of v and we thus arrive at the important fact 
 that the value of a division of the micrometer is always the same for 
 the same spectrum and can always be determined with sufficient accu- 
 racy from the dimensions of the apparatus and number of lines on the 
 grating, as well as by observation of the spectrum. 
 
 Furthermore, this proves that the spectrum is normal at this point 
 and to the same scale in the same spectrum. Hence we have only to 
 photograph the spectrum to obtain the normal spectrum and a centi- 
 meter for any of the photographs always represents the same increase 
 of wave-length. 
 
 It is to be specially noted that this theorem is rigidly true whether 
 the adjustments are correct or not, provided only that the micrometer 
 is on the line drawn perpendicularly from the centre of the grating, even 
 if it is not the centre of curvature. 
 
Ox CONCAVE GRATINGS FOE OPTICAL PURPOSES 499 
 
 As the radius of curvature of concave gratings is usually great, the 
 distance through which the spectrum remains practically normal is very 
 great. In the instrument which I principally use, the radius of curva- 
 ture p, is about 21 feet 4 inches, the width of the ruling "being about 5-5 
 inches. In such an instrument the spectrum thrown on a flat plate is 
 normal within about 1 part in 1,000,000, for 6 inches and less than 1 in 
 35,000, for 18 inches. In photographing the spectrum on a flat plate, 
 the definition is excellent for 12 inches, and by use of a plate bent to 11 
 feet radius, a plate of 20 inches in length is in perfect focus and the 
 spectrum still so nearly normal as to have its error neglected for most 
 purposes. 
 
 Another important property of the concave grating is that all the 
 superimposed spectra are in focus at the same point, and so by micro- 
 metric measurements the relative wave-lengths are readily determined. 
 Hence, knowing the absolute wave-length of one line, the whole spec- 
 trum can be measured. Professor Peirce has determined the absolute 
 wave-length of one line with great care and I am now measuring the 
 coincidences. This method is greatly more accurate than any hitherto 
 known, as by a mere eye inspection, the relative wave-length can often 
 be judged to 1 part in 20,000 and with a micrometer to 1 in 1,000,000. 
 Again, in dealing with the invisible portion of the spectrum, the focus 
 can be obtained by examining the superimposed spectrum. Captain 
 Abney, by using a concave mirror in the place of telescopes, has been 
 enabled to use this method f or^ obtaining the focus in photographing the 
 ultra red rays of the spectrum. It is also to be noted that this theorem 
 of the normal spectrum applies also to the flat grating used with tele- 
 scopes and to either reflecting or transmitting gratings; but in these 
 cases only a small portion of the spectrum can be used, as no lens can 
 be made perfectly achromatic. And so, as the distance of the microme- 
 ter has constantly to be changed when one passes along the spectrum, 
 its constant does not remain constant but varies in an irregular man- 
 ner. But it would be possible to fix the grating, one objective and the 
 camera rigidly on a bar, and then focus by moving the slit or the other 
 objective. In this case the spectrum would be rigidly normal, but 
 would probably be in focus for only a small length and the adjustment 
 of the focus would not be automatic. 
 
 But nothing can exceed the beauty and simplicity of the concave gra j - 
 ing when mounted on a movable bar such as I have described and illus- 
 trated in Fig. 1. Having selected the grating which we wish to use, 
 we mount it in its plate-holder and put the proper collimating eye-piece 
 
500 HENRY A. EOWLAND 
 
 in place. We then carefully adjust the focus by altering the length of 
 D until the cross-hairs are at the exact centre of curvature of the grat- 
 ing. On moving the bar the whole series of spectra are then in exact 
 focus, and the value of a division of the micrometer is a known quan- 
 tity for that particular grating. The wooden way AC, on which the 
 carriage moves, is graduated to equal divisions representing wave- 
 lengths, since the wave-length is proportional to the distance AC. Wo 
 can thus set the instrument to any particular wave-length we may wish 
 to study, or even determine the wave-length to at least one part in five 
 thousand by a simple reading. By having a variety of scales, one for 
 each spectrum, we can immediately see what lines are superimposed on 
 each other and identify them accordingly when we are measuring their 
 relative wave-length. On now replacing the eye-piece by a camera, we 
 are in a position to photograph the spectrum with the greatest ease. 
 We put in the sensitive plate, either wet or dry, and move to the part 
 we wish to photograph; having exposed for that part, we move to 
 another part, raise the plate to another position and expose once more. 
 We have no thought for the focus, for that remains perfect, but simply 
 refer to the table giving the proper exposure for that portion of the 
 spectrum and so have a perfect plate. Thus we can photograph the 
 whole spectrum on one plate in a few minutes, from the F line to the 
 extreme violet in several strips, each 20 inches long. Or we may photo- 
 graph to the red rays by prolonged exposure. Thus the work of days 
 with any other apparatus becomes the work of hours with this. Fur- 
 thermore, each plate is to scale, an inch on any one of the strips repre- 
 senting exactly so much difference of wave-length. The scale of the 
 different orders of spectra are exactly proportional to the order. Of 
 course the superposition of the spectra gives the relative wave-length. 
 To get the superposition, of course, photography is the best method. 
 
 Having so far obtained only the first approximation to the theory of 
 the concave grating, let us now proceed to a second one. The dividing 
 engine rules equal spaces along the chord of the circular arc of the grat- 
 ing: the question is whether any other kind of ruling would be better, 
 for the dividing engine is so constructed that one might readily change 
 it to rule slightly different from equal spaces. 
 
 The condition for theoretical perfection is that C shall remain con- 
 stant for all portions of the mirror. I shall therefore investigate how 
 nearly this is true. 
 
 Let p be the radius of curvature and let R and r be the true dis- 
 tances to any point of the grating, R and r being the distances to the 
 
ON CONCAVE GRATINGS FOR OPTICAL PURPOSES 501 
 
 centre. Let fi and v be the general values of the angles and //<, and V Q 
 the angles referred to the centre of the mirror. The condition is that 
 
 o 
 
 -^ = sin // + sin v 
 L/ 
 
 shall be a constant for all parts of the surface of the grating. Let us 
 then develope sin // and sin v in terms of /* , v and the angle d between 
 the radii drawn to the centre of the grating and to the point under con- 
 sideration. Let d' be the angle between R and R . Then we can write 
 immediately 
 
 /> sin fi = p sin /./ cos 8' + R sin d' p cos // sin 8', 
 
 sin /j. = sin // cos d' \ 1 + r J l A tan 8 f i , 
 
 iOsmjH, y 
 
 where * _ -. _ p cos ,u 
 
 Developing the value of cos d' in terms of d, we have 
 cos " = cos S { 1 + A [l + '' 8 "'"| ' 
 
 As the cases we are to consider are those where A is small, it will be 
 sufficient to write 
 
 tan * : = 
 
 Whence we have 
 
 sin <,. = sin // cos d 
 
 
 
 + ,5 3 + &c. 
 
 \ - 
 We can write the value of sin v from symmetry. But we have 
 
 2 -7- = sin fj. + sin v . 
 as 
 
 In this formula, db can be considered as a constant depending on 
 wave-length of light, etc., and ds as the width apart of the lines on the 
 grating. The dividing engine rules lines on the curved surface accord- 
 ing to the formula 
 
 2 -7- = cos 8 (sin //,+ sin v ). 
 
 CL8 
 
 But this is the second approximation to the true theoretical ruling. 
 And this ruling will not only be approximately correct, but exact when 
 
502 HENRY A. ROWLAND 
 
 all the terms of the series except the first vanish. In the case where the 
 slit and focus are on the circle of radius %p, as in the automatic arrange- 
 ment described above, we have A = and the second and third terms of 
 the series disappear, and we can write since we have 
 
 TO r 
 
 t = cos fJL and - cos v , 
 P P 
 
 n db / . \/i i sin >j. tan // + sin v tan * 3 \ 
 
 2 = cos d (sin ,u + sin > ) 1 J - r+ &c. . 
 
 ds \ sm fj + sm > / 
 
 But in the automatic arrangement we also have v = 0, and so the 
 formula becomes 
 
 2 -j- = cos d (sin /; + sin K O ) { 1 J tan ^ ^ ! + &c. }. 
 
 6t5 
 
 To find the greatest departure from theoretical perfection, d must 
 refer to the edge of the grating. In the gratings which I am now mak- 
 ing, p is about 260 inches and the width of the grating about 5-4 inches. 
 
 Hence d = - approximately and the series becomes 
 
 Hence the greatest departure from the theoretical ruling, even when 
 ta.nfji ( f=2, is 1 in 1,000,000. Now the distance apart of the compon- 
 ents of the 1474 line is somewhat nearly one forty-thousandth of the 
 wave-length and I scarcely suppose that any line has been divided by 
 the best spectroscope in the world whose components are less than one- 
 third of this distance apart. Hence we see that the departure of the 
 ruling from theoretical perfection is of little consequence until we are 
 able to divide lines twenty times as fine as the 1474 line. Even in that 
 case, since the error of ruling varies as 3 s , the greater portion of the 
 grating would be ruled correctly. 
 
 The question now comes up as to whether there is any limit to the 
 resolving power of a spectroscope. This evidently depends upon the 
 magnifying power and the apparent width of the lines. The magnify- 
 ing power can be varied at pleasure and so we have only to consider the 
 width of the lines of the spectrum. The width of the lines evidently 
 depends, in a perfect grating, upon three circumstances, the width of 
 the slit, the number of lines in the grating and the true physical width 
 of the line. The width of the slit can be varied at pleasure, the number 
 of lines on the grating can be made very great (160,000 in one of mine), 
 and hence we are only limited by the true physical width of the lines. 
 
Ox COXCAVE GRATINGS FOR OPTICAL PURPOSES 503 
 
 We have numerous cases of wide lines, such as the C line, the compon- 
 ents of the D 3 and H lines and numerous others which are perfectly 
 familiar to every spectroscopist. Hence we are free to suppose that all 
 lines have some physical width, and we are limited by that width in the 
 resolving power of our spectroscope. Indeed, from a theoretical stand- 
 point, we should suppose this to be true : for the molecules only vibrate 
 freely while swinging through their free path and in order to have the 
 physical width one one-hundred-thousandth of the wave-length, the 
 molecule must make somewhat nearly one hundred thousand vibrations 
 in its free path: but this would require a free path of about sooVoo 
 inch ! Hence it would be only the outermost solar atmosphere that could 
 produce such fine lines and we could hardly expect to see much finer 
 ones in the solar spectrum. Again * it is found impossible to obtain 
 interference between two rays whose paths differ by much more than 
 50,000 wave-lengths. 
 
 All the methods of determining the limits seem to point to about the 
 150,000th of the wave-length as the smallest distance at which the two 
 lines can be separated in the solar spectrum by even a spectroscope of 
 infinite power. As we can now nearly approach this limit I am strongly 
 of the opinion that we have nearly reached the limit of resolving power, 
 and that we can never hope to see very many more lines in the spectrum 
 than can be seen at present, either by means of prisms or gratings. 
 
 It is not to be supposed, however, that the average wave-length of the 
 line is not more definite than this, for we can easily point the cross- 
 hairs to the centre of the line to perhaps 1 in 1,000,000 of the wave- 
 length. The most exact method of detecting the coincidences of a line 
 of metal with one in the solar spectrum would thus be to take micro- 
 metric measurements first on one and then on the other; but I suppose 
 it would take several readings to make the determination to 1 in 
 1,000,000. 
 
 Since writing the above I have greatly improved my apparatus and 
 can now photograph 150 lines between the H and K lines, including 
 many whose wave-length does not differ more than 1 in about 80,000. 
 I have also photographed the 1474 and b 3 and & 4 , widely double, and also 
 E just perceptibly double. With the eye much more can be seen, but 
 I must say that I have not yet seen many signs of reaching a limit. The 
 
 3 1 have recently discovered that each component of the D line is double probably 
 from the partial reversal of the line as we nearly always see it in the flame spectrum. 
 
 *This method of determining the limit has been suggested to me by Prof. C. 8. 
 Hastings, of this University. 
 
504 HE^RY A. EOWLAND 
 
 lines yet appear as fine and sharp as with a lower power. If my grat- 
 ing is assumed to be perfect, in the third spectrum I should be able to 
 divide lines whose wave-lengths differed, in about 150,000, though not 
 to photograph them. 
 
 The E line has components, about ^uwfrth of the wave-length apart. 
 I believe I can resolve lines much closer than this, say 1 in 100,000 at 
 least. Hence the idea of a limit has not yet been proved. 
 
 However, as some of the lines of the spectrum are much wider than 
 others we should not expect any definite limit, but a gradual falling off 
 as we increase our power. At first, in the short wave-lengths at least, 
 the number of lines is nearly proportional to the resolving power, but 
 this law should fail as we approach the limit. 
 
31 
 
 ON MR. GLAZEBROOK'S PAPER ON THE ABERRATION OF 
 CONCAVE GRATINGS 
 
 [American Journal of Science [3], XXVI, 214, 1883 ; Philosophical Magazine [5], 
 
 XVI, 210, 1883] 
 
 In the June number of the Philosophical Magazine., Mr. R. T. Glaze- 
 brook has considered the aberration of the concave grating and arrives 
 at the conclusion that the ones which I have hitherto made are too 
 wide for their radius of curvature. As I had published nothing but a 
 preliminary notice of the grating at that time, Mr. Glazebrook had not 
 then seen my paper on the subject, of which I gave an abstract at the 
 London Physical Society in November last. In this paper I arrive at 
 the conclusion that there is practically no aberration and that in this 
 respect there is nothing further to be desired. 
 
 The reason of this discrepancy is not far to seek. Mr. Glazebrook 
 assumes that the spaces are equal on the arc of the circle. But I do 
 not rule them in this manner; but the equal spaces are equal along 
 the chord of the arc. Again, the surface is not cylindrical, but spherical. 
 
 These two errors entirely destroy the value of the paper as far as my 
 gratings are concerned, for it only applies to a theoretical grating, ruled 
 in an entirely different manner from my own, and on a different form 
 of surface. 
 
 I am very much surprised to see the method given near the end of 
 the paper for constructing aplanatic gratings on any surface, for this 
 is the method by which I discovered the concave grating originally, and 
 the figure is the same as I put on the blackboard at the meeting of the 
 Physical Society in November last. I say I am surprised, for Mr. Glaze- 
 brook's paper was read at the Physical Society, where I had given the 
 same method a few months before, and yet it passed without comment. 
 Indeed, I have given the same method many times at various scientific 
 societies of my own country. However, as Mr. Glazebrook was not 
 present at the meeting referred to, he is entirely without blame in the 
 matter. 
 
33 
 
 SCEEW 
 
 [Encyclopedia Britannica, Ninth Edition, Volume XXI \ 
 
 The screw is the simplest instrument for converting a uniform motion 
 of rotation into a uniform motion of translation (see ' Mechanics/ vol. 
 xv, p. 754). Metal screws requiring no special accuracy are generally cut 
 by taps and dies. A tap is a cylindrical piece of steel having a screw 
 on its exterior with sharp cutting edges; by forcing this with a revolv- 
 ing motion into a hole of the proper size, a screw is cut on its interior 
 forming what is known as a nut or female screw. The die is a nut with 
 sharp cutting edges used to screw upon the outside of round pieces of 
 metal and thus produce male screws. More accurate screws are cut in 
 a lathe by causing the carriage carrying the tool to move uniformly for- 
 ward, thus a continuous spiral line is cut on the uniformly revolving 
 cylinder fixed between the lathe centres. The cutting tool may be an 
 ordinary form of lathe tool or a revolving saw-like disk (see ' Machine 
 Tools/ vol. xv, p. 153). 
 
 Errors of Screws. For scientific purposes the screw must be so regu- 
 lar that it moves forward in its nut exactly the same distance for each 
 given angular rotation around its axis. As the mountings of a screw 
 introduce many errors, the final and exact test of its accuracy can only 
 be made when it is finished and set up for use. A large screw can, how- 
 ever, be roughly examined in the following manner: (1) See whether 
 the surface of the threads has a perfect polish. The more it departs 
 from this, and approaches the rough, torn surface as cut by the lathe 
 tool, the worse it is. A perfect screw has a perfect polish. (2) Mount 
 upon it between the centres of a lathe and the slip a short nut which 
 fits perfectly. If the nut moves from end to end with equal friction, 
 the screw is uniform in diameter. If the nut is long, unequal resist- 
 ance may be due to either an error of run or a bend in the screw. 
 (3) Fix a microscope on the lathe carriage and focus its single cross- 
 hair on the edge of the screw and parallel to its axis. If the screw runs 
 true at every point, its axis is straight. (4) Observe whether the short 
 nut runs from end to end of the screw without a wabbling motion when 
 the screw is turned and the nut kept from revolving. If it wabbles the 
 
SCREW 507 
 
 screw is said to be drunk. One can see this error better by fixing a 
 long pointer to the nut, or by attaching to it a mirror and observing an 
 image in it with a telescope. The following experiment will also detect 
 this error: (5) Put upon the screw two well-fitting and rather short 
 nuts, which are kept from revolving by arms bearing against a straight 
 edge parallel to the axis of the screw. Let one nut carry an arm which 
 supports a microscope focused on a line ruled on the other nut. Screw 
 this combination to different parts of the screw. If during one revolu- 
 tion the microscope remains in focus, the screw is not drunk; and if 
 the cross-hairs bisect the lines in every position, there is no error of 
 run. 
 
 Making Accurate Screws. To .produce a screw of a foot or even a 
 yard long with errors not exceeding -nnn^h of an inch is not difficult. 
 Prof. Wm. A. Eogers, of Harvard Observatory, has invented a process 
 in which the tool of the lathe while cutting the screw is moved so as to 
 counteract the errors of the lathe screw. The screw is then partly 
 ground to get rid of local errors. But, where the highest accuracy is 
 needed, we must resort in the case of screws, as in all other cases, to 
 grinding. A long, solid nut, tightly fitting the screw in one position, 
 cannot be moved freely to another position unless the screw is very accu- 
 rate. If grinding material is applied and the nut is constantly tight- 
 ened, it will grind out all errors of run, drunkenness, crookedness, and 
 irregularity of size. The condition is that the nut must be long, rigid 
 and capable of being tightened as the grinding proceeds ; also the screw 
 must be ground longer than it will finally be needed so that the imper- 
 fect ends may be removed. 
 
 The following process will produce a screw suitable for ruling grat- 
 ings for optical purposes. Suppose it is our purpose to produce a screw 
 which is finally to be 9 inches long, not including bearings, and 1-| in. 
 in diameter. Select a bar of soft Bessemer steel, which has not the 
 hard spots usually found in cast steel, and about If inches in diameter 
 and 30 long. Put it between lathe centres and turn it down to one 
 inch diameter everywhere, except about 12 inches in the centre, where 
 it is left a little over 1 inches in diameter for cutting the screw. Now 
 cut the screw with a triangular thread a little sharper than 60. Above 
 all, avoid a fine screw, using about 20 threads to the inch. 
 
 The grinding nut, about 11 inches long, has now to be made. Fig. 1 
 represents a section of the nut, which is made of brass, or better, of 
 Bessemer steel. It consists of four segments, a, a, which can be drawn 
 about the screw by two collars, &, &, and the screw c. Wedges between 
 
508 
 
 HENEY A. ROWLAND 
 
 the segments prevent too great pressure on the screw. The final clamp- 
 ing is effected by the rings and screws, d, d, which enclose the flanges, e, 
 of the segments. The screw is now placed in a lathe and surrounded 
 by water whose temperature can be kept constant to 1 C., and the nut 
 placed on it. In order that the weight of the nut may not make the 
 ends too small, it must either be counterbalanced by weights hung from 
 a rope passing over pulleys in the ceiling, or the screw must be vertical 
 during the whole process. Emery and oil seem to be the only available 
 grinding materials, though a softer silica powder might be used towards 
 the end of the operation to clean off the emery and prevent future wear. 
 Now grind the screw in the nut, making the nut pass backwards and 
 forwards over the screw, its whole range being nearly 20 inches at first. 
 
 FIG. 1. Section of Grinding Nut. 
 
 Turn the nut end for end every ten minutes and continue for two weeks, 
 finally making the range of the nut only about 10 inches, using finer 
 washed emery and moving the lathe slower to avoid heating. Finish 
 with a fine silica powder or rouge. During the process, if the thread 
 becomes too blunt, recut the nut by a short tap so as not to change the 
 pitch at any point. This must, of course, not be done less than five 
 days before the finish. Now cut to the proper length; centre again in 
 the lathe under a microscope, and turn the bearings. A screw so ground 
 has less errors than from any other system of mounting. The periodic 
 error especially will be too small to be discoverefl, though the mountings 
 and graduation and centering of the head will introduce it; it must 
 therefore finally be corrected. 
 
 Mounting of Screws. The mounting must be devised most carefully, 
 and is, indeed, more difficult to make without error than the screw itself. 
 The principle which should be adopted is that no workmanship is per- 
 fect; the design must make up for its imperfections. Thus the screw 
 
SCREW 509 
 
 can never be made to run true on its bearings, and hence the device of 
 resting one end of the carriage on the nut must be rejected. Also all 
 rigid connection between the nut and the carriage must be avoided, as 
 the screw can never be adjusted parallel to the ways on which the car- 
 riage rests. For many purposes, such as ruling optical gratings, the 
 carriage must move accurately forward in a straight line as far as the 
 horizontal plane is concerned, while a little curvature in the vertical 
 plane produces very little effect. These conditions can be satisfied 
 by making the ways Y-shaped and grinding with a grinder some- 
 what shorter than the ways. By constant reversals and by lengthen- 
 ing or shortening the stroke, they, will finally become nearly per- 
 fect. The vertical curvature can be sufficiently tested by a short car- 
 riage carrying a delicate spirit level. Another and very efficient form 
 of ways is V-shaped with a flat top and nearly vertical sides. The 
 carriage rests on the flat top and is held by springs against one of the 
 nearly vertical sides. To determine with accuracy whether the ways 
 are straight, fix a flat piece of glass on the carriage and rule a line on 
 it by moving it under a diamond ; reverse and rule another line near the 
 first, and measure the distance apart at the centre and at the two ends 
 by a micrometer. If the centre measurement is equal to the mean of the 
 two end ones, the line is straight. This is better than the method with 
 a mirror mounted on the carriage and a telescope. The screw itself 
 must rest in bearings, and the end motion be prevented by a point bear- 
 ing against its flat end, which is protected by hardened steel or a flat 
 diamond. Collar bearings introduce periodic errors. The secret of 
 success is so to design- the nut and its connections as to eliminate all 
 adjustments of the screw and indeed all imperfect workmanship. The 
 connection must also be such as to give means of correcting any residual 
 periodic errors or errors of run which may be introduced in the mount- 
 ings or by the wear of the machine. 
 
 The nut is shown in Fig 2. It is made in two halves, of wrought iron 
 filled with boxwood or lignum vitae plugs, on which the screw is cut. 
 To each half a long piece of sheet steel is fixed which bears against a 
 guiding edge, to be described presently. The two halves are held to the 
 screw by springs, so that each moves forward almost independently of 
 the other. To join the nut to the carriage, a ring is attached to the 
 latter, whose plane is vertical and which can turn round a vertical axis. 
 The bars fixed midway on the two halves of the nut bear against this 
 ring at points 90 distant from its axis. Hence each half does its share 
 independently of the other in moving the carriage forward. Any want 
 
510 
 
 HENRY A. ROWLAND 
 
 of parallelism between the screws and the ways or eccentricity in the 
 screw mountings thus scarcely affects the forward motion of the car- 
 riage. The guide against which the steel pieces of the nut rest can be 
 made of such form as to correct any small error of run due to wear of 
 the screw. Also, by causing it to move backwards and forwards peri- 
 odically, the periodic error of the head and mountings can be corrected. 
 In making gratings for optical purposes the periodic error must be 
 very perfectly eliminated, since the periodic displacement of the lines 
 only one-millionth of an inch from their mean position will produce 
 
 m 
 
 FIG. 2. 
 
 " ghosts " in the spectrum. 1 Indeed, this is the most sensitive method of 
 detecting the existence of this error, and it is practically impossible to 
 mount the most perfect of screws without introducing it. A very prac- 
 tical method of determining this error is to rule a short grating with 
 very long lines on a piece of common thin plate glass ; cut it in two with 
 a diamond and superimpose the two halves with the rulings together 
 and displaced sideways over each other one-half the pitch of the screw. 
 On now looking at the plates in a proper light so as to have the spec- 
 
 1 In a machine made by the present writer for ruling gratings the periodic error is 
 entirely due to the graduation and centering of the head. The uncorrected periodic 
 error from this cause displaces the lines ^^fa^ih of an inch, which is sufficient to 
 entirely ruin all gratings made without correcting it. 
 
SCREW 511 
 
 tral colors show through it, dark lines will appear, which are wavy if 
 there is a periodic error and straight if there is none. By measuring 
 the comparative amplitude of the waves and the distance apart of the 
 two lines, the amount of the periodic error can be determined. The 
 phase of the periodic error is best found by a series of trials after set- 
 ting the corrector at the proper amplitude as determined above. 
 
 A machine properly made as above and kept at a constant tempera- 
 ture should be able to make a scale of 6 inches in length, with errors at 
 no point exceeding nnnnnrth of an inch. When, however, a grating of 
 that length is attempted at the rate of 14,000 lines to the inch, four days 
 and nights are required, and the result is seldom perfect, possibly on 
 account of the wear of the machine or changes of temperature. Grat- 
 ings, however, less than 3 inches long are easy to make. 
 
39 
 
 ON" THE RELATIVE WAVE-LENGTH OF THE LINES OF THE 
 
 SOLAE SPECTRUM 
 
 [American Journal of Science [3J, XXXIII, 182-190, 1887 ; Philosophical Magazine 
 [5], XXIII, 257-265, 1887] 
 
 For several years past I have been engaged in making a photographic 
 map of the solar spectrum to replace the ordinary engraved maps and 
 I have now finished the map from the extreme ultra violet, wave-length 
 3200, down to wave-length 5790. In order to place the scale correctly 
 on this map, I have found it necessary to measure the relative wave- 
 lengths of the spectrum and to reduce it to absolute wave-lengths by 
 some more modern determination. I have not yet entirely finished the 
 work, but as my map of the spectrum is now being published and as 
 
 O 
 
 all observers so far seem to accept the measures of Angstrom, I have 
 decided that a table of my results would be of value. For as they stand 
 now they have at least ten times the accuracy of any other determina- 
 tion. This great accuracy arises from the use of the concave grating 
 which reduces the problem of relative wave-lengths to the measure of 
 the coincidences of the lines in the different spectra by a micrometer. 
 
 The instrument which I have employed has concave gratings 5 or 6 in. 
 diameter, having either 7200 or 14,400 lines to the inch and a radius of 
 21 ft. 6 in. By my method of mounting, the spectrum is normal where 
 measured, and thus it is possible to use a micrometer with a range of 
 5 inches. The spectrum keeps in focus everywhere and the constant 
 of the micrometer remains unchanged except for slight variations due 
 to imperfections in the workmanship. The micrometer has no errors 
 of run or period exceeding the -J^TTF inch. The probable error of a 
 single setting on a good clear line is about ^nrVur ^ the wave-length. 
 1" of arc is about -0012 inch. The D line in the second spectrum is -17 
 inch or 4-4 mm. wide. Determinations of relative wave-length of good 
 lines seldom differ 1 in 500,000 from each other and never exceed 1 in 
 100,000, even with different gratings. This is, of course, for the prin- 
 cipal standard lines, and the chance of error is greater at the extremities 
 of the spectrum. The interpolation of lines was made by running the 
 micrometer over the whole spectrum, 5 inches at a time, and adding the 
 
KELATIVE WAVE-LENGTH OF LINES OF SOLAS SPECTEUM 513 
 
 readings together so as to include any distance, even the whole spec- 
 trum. The wave-length is calculated for a fixed micrometer constant 
 and then corrected so as to coincide everywhere very nearly with the 
 standards. I suppose the probable error of the relative determinations 
 with the weight 1 in my table to be not far from 1 in 500,000. Ang- 
 strom thinks his standard lines have an accuracy of about 1 in 50,000 
 and ordinary lines much less. 
 
 As to the absolute measure, it is now well determined that Angstrom's 
 figures are too small by about 1 part in 6000. This rests: 1st, on the 
 determination of Peirce made for the U. S. Coast Survey with Ruther- 
 furd's gratings and not yet completely published; 2d, on an error made 
 by Tresca in the length of the standard metre used by Angstrom 1 which 
 increases his value by about 1 in 7700; 3d, on a result obtained in my 
 laboratory with two of my gratings by Mr. Bell, which is published with 
 this paper. Mr. C. S. Peirce has kindly placed his grating at our dis- 
 posal and we have detected an error of ruling which affects his result 
 and makes it nearly coincide with our own. The wave-length of the 
 mean of the two E lines is 
 
 Angstrom (atlas) 5269-12 -5 
 
 Angstrom (Corrected by Thalen) 5269-80 l 
 
 Peirce 5270-16 
 
 Peirce (Corrected by Rowland and Bell) 5270-00 * 
 
 Bell 5270-04 
 
 These results are for air at ordinary pressures and temperatures. The 
 last is reduced to 20 C. and 760 mm. pressure. To reduce to a vacuum 
 multiply by the following : 
 
 Fraunhofer line A C E G H 
 
 Correction factor. .1-000291 1-000292 1-000294 1-000297 1-000298 
 
 o 
 
 The relation between my wave-lengths and those of Angstrom are 
 
 O 
 
 given by the following, Angstrom's value being from p. 31 of his 
 
 memoir: 
 
 A (edge) B (edge) C 
 
 Angstrom 7597-5 6867-10 6717-16 6562-10 6264-31 
 
 Rowland . . 7593-97 6867-38 6717-83 6562-96 6265-27 
 
 Difference 3-5 -28 -67 -86 -96 
 
 1 Thal6n, Sur Spectre du Fer, Societe Royale des Sciences d'Upsal, September, 
 1884, p. 25. 2 From one grating only. 
 
514 HENRY A. ROWLAND 
 
 Da A Peirce's line 
 
 Angstrom 5895-13 5889-12 5708-45 5623-36 5454-84 
 
 Eowland . 5896-08 5890-12 5709-56 5624-70 5455-68 
 
 Difference -95 1-00 1-11 1-34 -84 
 
 E E bi F 
 
 Angstrom 5269-59 5268-67 5183-10 5138-78 4860-74 
 
 Rowland , . 5270-43 5269-65 5183-73 5139-47 4861-43 
 
 Difference -84 -98 -63 -69 -69 
 
 o 
 
 Angstrom 4702-44 4307-25 
 
 Rowland , . 4703-11 4307-96 
 
 Difference -67 -71 * 
 
 The greatest variation in these differences is evidently due to the 
 poor definition of Angstrom's grating by which the numbers refer to 
 groups of lines rather than to single ones. Selecting the best figures, 
 we find that Angstrom's wave-lengths must be multiplied by 1-00016 to 
 agree with Bell, while the correction for Angstrom's error of scale 
 would be 1-000110. 
 
 It is impossible for me to give at present all the data on which my 
 determinations rest, but I have given in Table I many of the coinci- 
 dences as observed with several gratings, the number of single readings 
 being given in the parenthesis over each set. 
 
 Table II gives the wave-lengths as interpolated by the micrometer. 
 It is scarcely possible that any error will be found (except accidental 
 errors) of more than -02, and from the agreement of the observations 
 I scarcely expect to make any changes in the final table of more than 
 01, except in the extremities of the spectrum, where it may amount 
 to -03 in the region of A and H lines. The wave-lengths of weight 
 greater than 1 will probably be found more exact than this. The lines 
 can be identified on my new photograph of the spectrum down to 5790. 
 Below this there is little trouble in finding the right ones. All maps 
 of the spectrum, especially above F, are so imperfect that it is almost 
 impossible to identify my lines upon them. The lines can only be prop- 
 erly identified by a power sufficient to clearly divide & 3 and & 4 . Some of 
 them are double and most of these have been marked, but as the table 
 has been made for my own use, I have not been very careful to examine 
 each line. This will, however, be finally done. Micrometric measures 
 
KELATIVE WAVE-LENGTH OF LINES OF SOLAK SPECTRUM 515 
 
 have now been made of nearly all the lines below & with a view of mak- 
 ing a map of this region. 
 
 Table I gives the coincidences of the different orders of the spectra 
 as observed with several concave gratings on both sides of the normal, 
 the numbers in the brackets indicating the number of observations. The 
 observations have been reduced as nearly as possible to what I consider 
 the true wave-length, the small difference from the numbers given in 
 Table II being the variation of the observations from the mean value. 
 The true way of reducing these observations would be to form a linear 
 equation for each series and reduce by the method of least squares. A 
 simpler way was, however, used and the relative wave-length of the 
 standard lines, marked S in Table II, was obtained; however, some 
 other observations were also included. 
 
 Table II gives the wave-lengths reduced to Bell's value for the abso- 
 lute wave-length of the D line. These were obtained by micrometric 
 measurement from the standards as described before. The weights 
 are given in the first column and some of the lines, which were meas- 
 ured double, have also been marked. But the series has not yet been 
 carefully examined for doubles. 
 
 The method is so much more accurate than by means of angular 
 measurement that the latter has little or no weight in comparison. 
 
 This table is to be used in connection with my photographic map of 
 the normal spectrum to determine the error of the latter at any point. 
 The map was made by placing the photograph in contact with the scale, 
 which was the same for each order of spectrum, and enlarging the two 
 together. In this way the map has no local irregularities, although the 
 scale may be displaced slightly from its true position, and may be a little 
 too long or short, although as far as I have tested it, it seems to have 
 very little error of the latter sort. The scale was meant in all cases, 
 except the ultra violet, to apply to Peirce's absolute value and so the 
 correction is generally negative, as follows : 
 
 Approximate correction to the photographic map of the normal spectrum to 
 reduce to latest absolute value. 
 
 Strip 3200 to 3330 Correction -05 
 
 " 3275 to 3530 " -05 
 
 " 3475 to 3730 " -02 
 
 " 3675 to 3930 <* -10 
 
 " 3875 to 4130 " -16 
 
 " 4075 to 4330.. " ...-04 
 
516 HENRY A. KOWLAND 
 
 Strip 4275 to 4530 Correction -08 
 
 " 4480 to 4735 -10 
 
 " 4685 to 4940 " -18 
 
 " 4875 to 5130 " -14 
 
 " 5075 to 5330 " -15 
 
 " 5215 to 5595 " about -05 
 
 " 5415 to 5795 " about -04 
 
 " 3710 to 3910 " -20 
 
 " 3810 to 4000 " -14 
 
 It is to be noted that the third spectrum of the map runs into the 
 second, so that it must not be used beyond wave-length 3200, as it is 
 mixed with the second in that region. 
 
 [The tables are omitted.] 
 
41 
 TABLE OF STANDAKD WAVE-LENGTHS 
 
 [Johns Hopkins University Circulars, No. 73, p. 69, 1889 ; Philosophical Magazine [5], 
 
 XXVII, 479-484, 1889] 
 
 In the ' American Journal of Science ' for March, 1887, and the ' Lon- 
 don, Dublin and Edinburgh Philosophical Magazine ' for the same 
 month, I have published a preliminary list of standards as far as could 
 be observed with the eye, with a few imperfectly observed by photog- 
 raphy, the whole being reduced to Bell's and Peirce's values for absolute 
 wave-lengths. Mr. Bell has continued his measurements and found a 
 slightly greater value for the absolute wave-length of the D line, and I 
 have reduced my standards to the new values. 
 
 Nearly the whole list has been gone over again, especially at the ends 
 around the A line and in the ultra violet. The wave-lengths of the ultra 
 violet were obtained by photographing the coincidence with the lower 
 wave-lengths, a method which gives them nearly equal weight with 
 those of the visible spectrum. 
 
 The full set of observations will be published hereafter, but the pres- 
 ent series of standards can be relied on for relative wave-lengths to -02 
 division of Angstrom in most cases, though it is possible some of them 
 may be out more than this amount, especially in the extreme red. 
 
 As to the absolute wave-length, no further change will be necessary, 
 provided spectroscopists can agree to use that of my table, as has been 
 done by many of them. 
 
 By the method of coincidences with the concave grating the wave- 
 lengths have been interwoven with each other throughout the whole 
 table so that no single figure could be changed without affecting many 
 others in entirely different portions of the spectrum. The principal dif- 
 ference from the preliminary table is in the reduction to the new abso- 
 lute wave-length by which the wave-lengths are about 1 in 80,000 larger 
 than the preliminary table. I hope this difference will not be felt by 
 those who have used the old table because measurements to less than A- 
 
 o 
 
 division of Angstrom are rare, the position of the lines of many metals 
 being unknown to a whole division of Angstrom. As the new map of 
 the spectrum has been made according to this new table, I see no further 
 reason for changing the table in the future. 
 
518 HENRY A. ROWLAND 
 
 No attempt has been made to reduce the figures to a vacuum as the 
 index of refraction of air is imperfectly known, but this should be done 
 where numerical relations of time period are desired. 
 
 In the column giving the weight, the primary standards are marked 
 8 and the other numbers give the number of separate determination of 
 the wave-length and thus, to some extent, the weight. 
 
 Many of these standards are double lines and some of them have 
 faint components near them, which makes the accuracy of setting 
 smaller. This is specially the case when this component is an 
 atmospheric line whose intensity changes with the altitude of the sun. 
 The principal doubles are marked with d, but the examination has not 
 been completed yet, especially at the red end of the spectrum. 
 
 [A table of the standard wave-lengths is given on p. 78 J. H. U. Circ., 
 but is omitted in this volume.] 
 
42 
 
 A FEW NOTES ON THE USE OF GKATINGS 
 
 [Johns Hopkins University Circulars, No. 73, pp. 73, 74, 1889] 
 
 The ghosts are very weak in most of my gratings. They are scarcely 
 visible in the lower orders of spectra, hut increase in intensity as com- 
 pared with the principal line as the square of the order of the spectrum. 
 Hence, to avoid them, obtain magnification by increasing the focal dis- 
 tances instead of going to the higher orders. The distances from the 
 principal line in my gratings are the same as the distances of the spectra 
 from the image of the slit when using a grating of 20 lines to the inch. 
 They are always symmetrical on the two sides, and about -^ inch for 
 the violet and inch for the red in a grating of 21 ft. 6 in. radius in all 
 orders of spectra. When the given line has the proper exposure on the 
 photographic plate, the ghosts will not show, but over-exposure brings 
 them out faintly in the third spectrum of a 20,000 grating or the 6th of 
 a 10,000 one. They never cause any trouble, as they are easily recog- 
 nized and never appear in the solar spectrum. In some cases the higher 
 orders of ghosts are quite as apparent as those of the first order. 
 
 The gratings with 10,000 lines to the inch often have better definition 
 than those of 20,000, as they take half the time to rule, and they are 
 quite as good for eye observation. They can also be used for photo- 
 graphing the spectrum by absorbing the overlying spectra, but there 
 are very few materials which let through the ultra violet and absorb the 
 longer wave-lengths. The 10,000 gratings have the advantage, how- 
 ever, in the measurement of wave-lengths by the overlapping spectra, 
 although this method is unnecessary since the completion of my map of 
 the spectrum. By far the best is to use a 20,000 grating and observe 
 down to the D line by photography, using erythrosin plates from the F 
 line down to D. Below D, cyanine plates can be used, although the time 
 of exposure is from 10 to 60 minutes with a narrow slit. The solar 
 spectrum extends to wave-lengths 3000, and the map has been contin- 
 ued to this point. Beyond this, the coincidence with the solar spectrum 
 cannot be used, but those of the 1st and 2d or 2d and 3d spectra can be. 
 
 Some complaints have been made to me that one of my gratings has 
 no spectrum beyond 3400. even of the electric arc. I have never found 
 this the case, as the one I use gives w. 1. 2200, readily with 30 minutes 
 exposure on slow plates, requiring 5 minutes for the most sensitive 
 
520 HENRY A. KOWLAND 
 
 part and using the electric arc. With sensitive plates, the time can be 
 diminished to one-fifth of this. 
 
 For eye observations, a very low power eye-piece of 1 or 2 in. focus 
 is best. This, with a focus of 21 ft. 6 in. is equivalent to a plane grat- 
 ing with a telescope of a power of 100 or 200. 
 
 In measuring the spectra, an ordinary dividing engine with errors 
 not greater than 10*00 inch can be used, going over the measurements 
 twice with the plate reversed between the separate series. The plates 
 are on so very large a scale that the microscope must have a very low 
 power. The one I use has a 1 inch objective and a 2 inch eye-piece. 
 The measured part of the plate is about a foot long, the plates being 
 19 in. long. 
 
 All the spectrum photographs taken at different times coincide per- 
 fectly, and this can be used for such problems as the determination of 
 the atmospheric lines. For this purpose, negatives at high and low 
 sun are compared by scraping the emulsion off from half the plates and 
 clamping them together with the edges of the spectra in coincidence. 
 The two spectra coincide exactly line for line except where the atmo- 
 spheric lines occur. 
 
 This method is specially valuable for picking out impurities in metal- 
 lic spectra, using some standard impurity in all the substances to give 
 a set of fiducial lines; or better, obtaining the coincidence of all the 
 metals with some one metal, such as iron. Making the iron spectrum 
 coincide on the two plates, the other spectra can be compared. This is 
 specially possible because the focus of a properly set up concave grating 
 need not be altered in years of use, for, when necessary, it can be ad- 
 justed at the slit, keeping the distance of the grating from the slit con- 
 stant. 
 
 The spectrum of the carbon poles is generally too complicated for 
 use with anything except the more pronounced lines of metals, there 
 being, at a rough guess, 10,000 lines in its spectrum. However, in pho- 
 tographing metallic spectra but few of these show on the plate, as they 
 are mostly faint. The spark discharge gives very nebulous lines for 
 the metals. 
 
 Most gratings are ruled bright in the higher orders, but this is more 
 or less difficult, as most diamond points give the first spectrum the 
 brightest. Indeed, it is very easy to obtain ruling which is immensely 
 bright in the first spectrum. Such gratings might be used for gaseous 
 spectra. Short focus gratings of 5 ft. radius of curvature, very bright 
 in the first order, require only a fraction of a second exposure for the 
 solar spectrum and the spectrum of a gas can be obtained in less than 
 an hour. 
 
46 
 KEPOET OF PROGRESS IN SPECTKUM WORK 
 
 [Johns Hopkins University Circulars, No. 85, pp. 41, 42, 1891 ; American Journal of 
 Science [3], XLI, 243, 244, 1891 ; The Chemical News, LXIII, 133, 1891] 
 
 During the past year or two a great deal of work has been done in 
 the photography of the spectra of elements and the identification of the 
 lines in the solar spectrum, which it will take a long time to work up, 
 ready for publication. Hence, I have thought that a short account of 
 what has been done up to the present time might be of interest to work- 
 ers in the subject. In the prosecution of the work financial assistance 
 has been received from the Rumford Fund of the American Academy of 
 Arts and Sciences, as well as from the fund given by Miss Bruce to the 
 Harvard Astronomical Observatory for the promotion of research in 
 astronomical physics, and the advanced state of the work is due to such 
 assistance. 
 
 The work may be summed up under the following heads : 
 
 1st. The spectra of all known elements, with the exception of a few 
 gaseous ones, or those too rare to be yet obtained, have been photo- 
 graphed in connection with the solar spectrum, from the extreme ultra 
 violet down to the D line, and eye observations have been made on many 
 to the limit of the solar spectrum. 
 
 2d. A measuring engine has been constructed with a screw to fit the 
 above photographs, which, being taken with the concave grating, are all 
 normal spectra and to the same scale. This engine measures wave- 
 1-engtlis direct, so that no multiplication is necessary, but only a slight 
 correction to get figures correct to y^g- of a division of Angstrom. 
 
 3d. A table of standard wave-lengths of the impurities in the car- 
 bons, extending to wave-length 2000, has been constructed to measure 
 wave-lengths beyond the limits of the solar spectrum. 
 
 4th. Maps of the spectra of some of the elements have been drawn 
 on a large scale ready for publication. 
 
 5th. The greater part of the lines in the map of the solar spectrum 
 have been identified and the substance producing them noted. 
 
 6th. The following rough table of the solar elements has been con- 
 structed entirely according to my own observations, although, of course, 
 most of them have been given by others. 
 
522 
 
 HENEY A. ROWLAND 
 
 I do not know which are the new ones, but call attention to Silicon, 
 Vanadium, Scandium, Yttrium, Zirconium, Glucinum, Germanium and 
 Erbium, as being possibly new. 
 
 Silicon has lines on my map at wave-lengths 3905-7, 4103-1, 5708-7, 
 5772-3 and 5948-7. That at 3905-7 is the largest and most certain. 
 That at 4103-1 is also claimed by Manganese. 
 
 ELEMENTS IN THE SUN, ARRANGED ACCORDING TO THE INTENSITY 
 AND THE NUMBER OF LINES IN THE SOLAR SPECTRUM. 
 
 ACCOBDING TO INTENSITY. 
 
 Calcium. 
 
 Iron. 
 
 Hydrogen. 
 
 Sodium. 
 
 Nickel. 
 
 Magnesium. 
 
 Cobalt. 
 
 Silicon. 
 
 Aluminium. 
 
 Titanium. 
 
 Chromium. 
 
 Manganese. 
 
 Strontium. 
 
 Vanadium. 
 
 Barium. 
 
 Carbon. 
 
 Scandium. 
 
 Yttrium. 
 
 Zirconium. 
 
 Molybdenum. 
 
 Lanthanum. 
 
 Niobium. 
 
 Palladium. 
 
 Neodymium. 
 
 Copper. 
 
 Zinc. 
 
 Cadmium. 
 
 Cerium. 
 
 Glucinum. 
 
 Germanium. 
 
 ACCORDING TO NUMBER. 
 
 Iron (2000 or more). 
 
 Nickel. 
 
 Titanium. 
 
 Manganese. 
 
 Chromium. 
 
 Cobalt. 
 
 Carbon (200 or more). 
 
 Vanadium. 
 
 Zirconium. 
 
 Cerium. 
 
 Calcium (75 or more). 
 
 Scandium. 
 
 Neodymium. 
 
 Lanthanum. 
 
 Yttrium. 
 
 Niobium. 
 
 Molybdenum. 
 
 Palladium. 
 
 Magnesium (20 or more). 
 
 Sodium (11). 
 
 Silicon. 
 
 Strontium. 
 
 Barium. 
 
 Aluminium (4). 
 
 Cadmium. 
 
 Rhodium. 
 
 Erbium. 
 
 Zinc. 
 
 Copper (2). 
 
 Silver (2). 
 
REPORT OF PROGRESS IN SPECTRUM WORK 523 
 
 ACCORDING TO INTENSITY. ACCORDING TO NUMBER. 
 
 Rhodium. Glucinum (2). 
 
 Silver. Germanium. 
 
 Tin. Tin. 
 
 Lead. Lead (1). 
 
 Erbium. Potassium (1). 
 Potassium. 
 
 DOUBTFUL ELEMENTS. 
 
 Iridium. Ruthenium. Tungsten. 
 
 Osmium. Tantalum. Uranium. 
 
 Platinum. Thorium. 
 
 NOT IN SOLAR SPECTRUM. 
 
 Antimony. Caesium. Rubidium. 
 
 Arsenic. Gold. Selenium. 
 
 Bismuth. Indium. Sulphur. 
 
 Boron. Mercury. Thallium. 
 
 Nitrogen (vacuum tube). Phosphorus. Praeseodymium. 
 
 SUBSTANCES NOT YET TRIED. 
 
 Bromine. Oxygen. Holmium. 
 
 Chlorine. Tellurium. Thulium. 
 
 Iodine. Gallium. Terbium, etc. 
 Fluorine. 
 
 These tables are to be accepted as preliminary only, especially the 
 order in the first portion. However, being made with such a powerful 
 instrument, and with such care in the determination of impurities, they 
 must still have a weight superior to most others published. 
 
 The substances under the head of "Not in Solar Spectrum" are 
 often placed there because the elements have few strong lines or none 
 at all in the limit of the solar spectrum when the arc spectrum, which 
 I have used, is employed. Thus boron has only two strong lines at 2497. 
 Again, the lines of bismuth are all compound and so too diffuse to ap- 
 pear in the solar spectrum. Indeed, some good reason generally ap- 
 pears for their absence from the solar spectrum. Of course, this is 
 little evidence of their absence from the sun itself. 
 
 Indeed, were the whole earth heated to the temperature of the sun, 
 its spectrum would probably resemble that of the sun very closely. 
 
524 HENRY A. ROWLAND 
 
 With the high dispersion here used the "basic lines" of Lockyer are 
 widely broken up and cease to exist. Indeed, it would be difficult to 
 prove anything except accidental coincidences among the lines of the 
 different elements. Accurate investigation generally reveals some slight 
 difference of wave-length or a common impurity. 
 
 Furthermore, the strength of the lines in the solar spectrum is gen- 
 erally very nearly the same as that in the electric arc, with only a few 
 exceptions, as for instance calcium. The cases mentioned by Lockyer 
 are generally those where he mistakes groups of lines for single lines 
 or even mistakes the character of the line entirely. Altogether there 
 seems to be very little evidence of the breaking up of the elements in 
 the sun as far as my experiments go. 
 
 Even after comparing the solar spectrum with all known elements, 
 there are still many important lines not accounted for. Some of these 
 I have accounted for by silicon and there are probably many more. Of 
 all known substances this is the most difficult to bring out the lines in 
 the visible spectrum although it has a fine ultra-violet one. Possibly 
 iron may account for many more, and all the elements at a higher tem- 
 perature might develope more. Then, again, very rare elements like 
 scandium, vanadium, etc., when they have a strong spectrum, may cause 
 strong solar lines and thus we may look for new and even rare elements 
 to account for very many more. Indeed, I find many lines accounted 
 for by the rare elements in gadolinite, samarskite and fergusonite other 
 than yttrium, erbium, scandium, praeseodymium, neodymium, lantha- 
 num and cerium, which I cannot identify yet and which may be without 
 a name. For this reason, and to discover rare elements, I intend finally 
 to try unknown minerals, as my process gives me an easy method of 
 detecting any new substance or analyzing minerals however many ele- 
 ments they may contain. 
 
 The research is much indebted to the faithful and careful work of 
 Mr. L. E. Jewell who has acted as my assistant for several years. 
 Preliminary publications of results will be made in the ' University 
 Circulars.' 
 
 Among the lastest results I may mention the spectroscopic separation 
 of yttrium into three components, and the actual separation into two. 
 
49 
 GRATINGS IN THEORY AND PRACTICE l 
 
 [Philosophical Magazine [5], XXXV, 397-419, 1893 ; Astronomy and Astro -Physics, 
 
 XII, 129-149, 1893] 
 
 PART I 1 
 
 It is not my object to treat the theory of diffraction in general but 
 only to apply the simplest ordinary theory to gratings made by ruling 
 grooves with a diamond on glass or metal. This study I at first made 
 with a view of guiding me in the construction of the dividing engine 
 for the manufacture of gratings, and I have given the present theory 
 for years in my lectures. As the subject is not generally understood 
 in all its bearings I have written it for publication. 
 
 Let p be the virtual distance reduced to vacuo through which a ray 
 moves. Then the effect at any point will be found by the summation 
 of the quantity 
 
 A C08&O Vt) + Bsinb(p V) , 
 
 o 
 in which & = ~, I being the wave-length. V is the velocity reduced to 
 
 L 
 
 vacuo, and t is the time. Making 6 = tan" 1 - - we can write this 
 
 sin [0 + b ( p 
 
 The energy or intensity is proportional to (A 2 -f- B 2 ). 
 Taking the expression 
 
 (A +iB)g~ <!-"), 
 
 when i = V 1, its real part will be the previous expression for the 
 displacement. Should we use the exponential expression instead of the 
 circular function in our summation we see that we can always obtain 
 
 1 I am much indebted to Dr. Ames for looking over the proofs of this paper and 
 correcting some errors. In the paper I have, in order to make it complete, given 
 some results obtained previously by others, especially by Lord Rayleigh. The treat- 
 ment is, however, new, as well as many of the results. My object was originally to 
 obtain some guide to the effect of errors in gratings so that in constructing my 
 dividing engine I might prevent their appearance if possible. 
 
 5 [Part II was never written.] 
 
526 HENRY A. ROWLAND 
 
 the intensity of the light by multiplying the final result by itself with 
 i in place of -f- i, because we have 
 
 (A + iB} e~ ib (p ~ rt) x(A iff) e' b (f ~ rt] = A* + &, 
 
 In cases where a ray of light falls on a surface where it is broken 
 up, it is not necessary to take account of the change of phase at the 
 surface but only to sum up the displacement as given above. 
 
 In all our problems let the grating be rather small compared with 
 the distance of the screen receiving the light so that the displacements 
 need not be divided into their components before summation. 
 
 Let the point x' , y', z' be the source of light, and at the point x, y, z 
 let it be broken up and at the same time pass from a medium of index 
 of refraction I' to one of /. Consider the disturbance at a point x", y" , 
 z" in the new medium. It will be 
 
 where 
 
 S = x"* + y' n + z m + a? + f + z* - 2 (xx" + yy" + zz") , 
 p 2 = a/ 2 + y'* + z '* + x * + f + z* 2 (xx' + yy' + zz') . 
 
 Let the point x, y, z be near the origin of co-ordinates as compared 
 with x', y', z' or x" ', y" , z" and let a, /?, f and a!, fl, f be the direction 
 cosines of p and p. Then, writing 
 
 R = I' V of* + y" + z' 2 + /Vz" 2 + y m + z"*, 
 
 /I = la + I'a', 
 p. = 7/3 + /'/?, 
 
 we have, for the elementary displacement, 
 
 g ib [ R Vt AZ - ny vz + /tr j ] 
 
 1 
 n ] 
 
 where _ , [~ _ P_ _ _ / 
 
 L V z" + y" + z' z + V x"' + y" 3 + z' 
 and r 2 = z 2 + y* + z\ 
 
 This equation applies to light in any direction. In the special case 
 of parallel light, for which * = 0, falling on a plane grating with lines 
 in the direction of z, one condition will be that this expression must be 
 the same for all values of z. 
 
 Hence v = . 
 
 If N is the order of the spectrum and a the grating space we shall 
 see further on that we also have the condition 
 
GRATINGS IN THEORY AND PRACTICE 527 
 
 The direction of the diffracted light will then be defined by the 
 equations 
 
 ' 2 + p* + r * =0, 
 
 whence 
 
 Fff^J-Jf-If, 
 
 a 
 
 In the ordinary case where the incident and diffracted rays are per- 
 pendicular to the lines of the grating, we can simplify the equations 
 somewhat. 
 
 Let <p be the angle of incidence and (p of diffraction as measured from 
 the positive direction of X. 
 
 A = /' cos <f + I cos <p , 
 
 N = fi = /' sin y + / sin </> , 
 a 
 
 where I is the wave-length in vacuo. 
 In case of the reflecting grating 1 = 1' and we can write 
 A = I\coa<p + cos <^}, 
 
 N=. ii = I\ sin a> + sin <p\. 
 a 
 
 This is only a very elementary expression as the real value would 
 depend on the nature of the obstacle, the angles, etc., but it will be suffi- 
 cient for our purpose. 
 
 The disturbance due to any grating or similar body will then be very 
 nearly 
 
 (* r e ib[R- Vt to-ny-vz + KW + y' + tfrtclg^ 
 where ds is a differential of the surface. For parallel rays, K = 0. 
 
 PLANE GRATINGS 
 
 In this case the integration can often be neglected in the direction 
 of z and we can write for the disturbance in case of parallel rays, 
 
 aib(R Vt) I I (, il>[ AX ny] /7 
 J J 
 
528 HENRY A. ROWLAND 
 
 CASE I. SIMPLE PERIODIC RULING 
 
 Let the surface be divided up into equal parts in each of which one 
 or more lines or grooves are ruled parallel to the axis of z. 
 
 The integration over the surface will then resolve itself into an 
 integration over one space and a summation with respect to the num- 
 ber of spaces. For in this case we can replace y by na -\- y where a is 
 the width of a space and the displacement becomes 
 
 g-il)(R-Vt) v e + ibnan I I e +ib (Ax + Ml/) ds , 
 
 but ~bnit. 
 
 n-i - smw 
 
 v 0+ibpan 
 
 sin ba;i 
 Bin -- 
 
 Multiplying the disturbance by itself with i in place of -j- i we have 
 for the light intensity 
 
 I C e-n l * x + /> ds \ I /(.+ ib < Ax + *v) ds\ 
 
 sm - 
 The first term indicates spectral lines in positions given by the equation 
 
 with intensities given by the last integral. The intensity of the spec- 
 tral lines then depends on the form of the groove as given by the equa- 
 tion x = f(y) and upon the angles of incidence and diffraction. The 
 first factor has been often discussed and it is only necessary to call 
 attention to a few of its properties. 
 
 When bafjt*=%7rN, N being any whole number, the expression be- 
 comes n 2 . On either side of this value the intensity decreases until 
 ribdfj! '=2xN, wheniit becomes 0. 
 
 The spectral line then has a width represented by// / M"=T 2^ nearly; 
 on either side of this line smaller maxima exist too faintly to be ob- 
 served. When two spectral lines are nearer together than half their 
 width, they blend and form one line. The defining power of the spec- 
 troscope can be expressed in terms of the quotient of the wave-length 
 by the difference of wave-length of two lines that can just be seen as 
 divided. The defining power is, then, 
 
 3 An expression of Lord Rayleigh's. 
 
GRATINGS ix THEORY AND PRACTICE 529 
 
 Now na is the width of the grating. Hence, using a grating at a 
 given angle, the defining power is independent of the number of lines 
 to the inch and only depends on the width of the grating and the wave- 
 length. According to this, the only object of ruling many lines to the 
 inch in a grating is to separate the spectra so that, with a given angle, 
 the order of spectrum shall be less. 
 
 Practically the gratings with few lines to the inch are much better 
 than those with many, and hence have better definition at a given 
 angle than the latter except that the spectra are more mixed up and 
 more difficult to see. 
 
 It is also to be observed that the defining power increases with shorter 
 wave-lengths, so that it is three times as great in the ultra violet as 
 in the red of the spectrum. This is of course the same with all optical 
 instruments such as telescopes and microscopes. 
 
 The second term which determines the strength of the spectral lines 
 will, however, give us much that is new. 
 
 First let us study the effect of the shape of the groove on the bright- 
 ness. If N is the order of The spectrum and a the grating space we 
 have 
 
 Nl 
 
 /j. = /(sin <p + sin 0) = - 
 a 
 
 since sin*? = 
 
 <i 
 
 and the intensity of the light becomes proportional to 
 
 ^ ' + ^ y) ds e ~ K " (> + ^ v) 
 
 It is to be noted that this expression is not only a function of N but 
 also of I, the wave-length. This shows that the intensity in general 
 may vary throughout the spectrum according to the wave-length and 
 that the sum of the light in any one spectrum is not always white light. 
 
 This is a peculiarity often noticed in gratings. Thus one spectrum 
 may be almost wanting in the green, while another may contain an 
 excess of this color; again there may be very little blu^ in one spectrum 
 while very often the similar spectrum on the other side may have its 
 own share and that of the other one also. For this reason I have found 
 it almost impossible to predict what the ultra red spectrum may be, 
 for it is often weak even where the visible spectrum is strong. 
 
 The integral may have almost any form although it will naturally 
 tend to be such as to make the lower orders the brightest when the 
 diamond rules a single and simple groove. When it rules several lines 
 34 
 
530 HENRY A. KOWLAND 
 
 or a compound groove, the higher orders may exceed the lower in 
 brightness and it is mathematically possible to have the grooves of 
 such a shape that, for given angles, all the light may be thrown into 
 one spectrum. 
 
 It is not uncommon, indeed, very easy, to rule gratings with im- 
 mensely bright first spectra, and I have one grating where it seems as 
 if half the light were in the first spectrum on one side. In this case 
 there is no reflection of any account from the grating held perpendicu- 
 larly: indeed to see one's face, the plate must be held at an angle, in 
 which case the various features of the face are seen reflected almost 
 as brightly as in a mirror but drawn out into spectra. In this case all 
 the other spectra and the central image itself are very weak. 
 
 In general it would be easy to prove from the equation that want of 
 symmetry in the grooves produces want of symmetry in the spectra, a 
 fact universally observed in all gratings and one which I generally 
 utilize so that the light may be concentrated in a few spectra only. 
 
 EXAMPLE 1 SQUARE GROOVES 
 
 When the light falls nearly perpendicularly on the plate, we need 
 not take the sides into account but only sum up the surface of the plate 
 and the bottom of the groove. Let the depth "be X and the width equal 
 
 to*. 
 m 
 
 The intensity then becomes proportional to 
 
 'N T S T ~rn r T" 
 This vanishes when 
 
 N = m , 2m , 3m, etc., 
 
 or = 0, 1, 2, 3, etc. 
 
 The intensity of the central light, for which N = 0, will be 
 
 * - / * ]T\ 
 
 rein(* T XJ. 
 
 This can be made to vanish for only one angle for a given wave- 
 length. Therefore, the central image will be colored and the color 
 will change with the angle, an effect often observed in actual gratings. 
 The color ought to change, also, on placing the grating in a liquid of 
 different index of refraction since A contains 7, the index of refraction. 
 
 It will be instructive to take a special case, such as light falling per- 
 pendicularly on the plate. For this case 
 
GRATINGS IN THEORY AND PRACTICE 531 
 
 A77 
 
 <p = 0, I =1(1 + cos v'O and // = / sin = 11 . 
 
 The last term in the intensity will then be 
 
 As an example, let the green of the second order vanish. In this case, 
 Z= -00005. N = 2. Let a =-0002 cm. and 7=1. 
 
 Then, ^[20000 + V (20000) 2 - (10000) 2 ] = n. 
 
 Whence, -% _ n 
 
 ~ 37300. ' 
 
 where n is any whole number. Make it 1. 
 
 Then the intensity, as far as this term is concerned, will be as 
 follows : 
 
 Minima where Intensity is 0. Maxima where Intensity is 1. 
 
 Wave-lengths. Wave-lengths. 
 
 1st spec. -0000526 -0000268 -0001000 -00003544 -00002137 
 
 2nd " -0000500 -0000266 -0000833 -00003463 -00002119 
 
 3rd " -0000462 -0000263 -0000651 -00003333 -00002089 
 
 4th -0000416 -0000259 -0000499 -00003169 -00002050 
 
 5th " etc. etc. etc. 
 
 The central light will contain the following wave-lengths as a 
 maximum : 
 
 0001072 -00003575 -0000214, etc. 
 
 Of course it would be impossible to find a diamond to rule a rectangu- 
 lar groove as above and the calculations can only be looked upon as a 
 specimen of innumerable light distributions according to the shape of 
 groove. 
 
 Every change in position of the diamond gives a different light dis- 
 tribution and hundreds of changes may be made every day and yet the 
 same distribution will never return, although one may try for years. 
 
 EXAMPLE 2. TRIANGULAR GROOVE 
 
 Let the space a be cut into a triangular groove, the equations of the 
 sides being x = cy, and x = c'(y a), the two cuttings coming 
 together at the point y = u. Hence we have cu = c'(u a), and 
 ds = dy V 1 + <? or dy ^1+c 12 . Hence the intensity is proportional to 
 
532 HENRY A. ROWLAND 
 
 . cA) 
 
 1 J * sin 8 
 
 2 
 
 I Q + 
 
 A <-#)(> + 
 
 cos 
 
 -^- [(/* + c' A) (a w) w (// c/)] I . 
 
 This expression is not symmetrical with respect to the normal to the 
 grating, unless the groove is symmetrical, in which case c = c' and 
 
 .=. 
 
 In this case, as in the other, the colors of the spectrum are of vari- 
 able intensity, and some of them may vanish as in the first example, 
 but the distribution of intensity is in other respects quite different. 
 
 CASE II. MULTIPLE PERIODIC RULING 
 
 Instead of having only one groove ruled on the plate in this space a, 
 let us now suppose that a series of similar lines are ruled. 
 
 We have, then, to obtain the displacement by the same expression as 
 before, that is 
 
 sn 
 
 2 
 
 r 
 I I e ib ^ x + *) ds, 
 
 * 
 
 except that the last integral will extend over the whole number of lines 
 ruled within the space a. 
 
 In the spaces a let a number of equal grooves be ruled commencing 
 at the points y = 0, y lt y 2 , y z , etc., and extending to the points w, y l -f- w, 
 y z -f- w, etc. The surface integral will then be divided into portions 
 from w to y u from y l -f- w, to y z , etc., on the original surface of the 
 plate for which x = 0, and from w to 0, from y -\- w to y u etc., for 
 the grooves. 
 
 The first series of integrals will be 
 
 /e 
 
 dv = 4 ( 6 a >i iW + efoMi fc^(i/i+>) + gib^ etc. 
 tOft 
 
 But, e ib ^ a = 1 since &/* = 2^-JV for any maximum, and thus the inte- 
 gral becomes 
 
 f 
 
 < 1 4- fribnyi 4- gib^y^ -\- etc. 
 
GRATINGS IN THEORY AND PRACTICE' 533 
 
 The second series of integrals will be 
 
 / 
 
 The total integral will then be 
 
 8inw ^ri * 
 
 sin^i L *&, ^ Jo 6 JL 
 
 i 
 
 As before, multiply this by the same with the sign of i changed to 
 get the intensity. 
 
 EXAMPLE 1. EQUAL DISTANCES 
 The space, a, contains n' 1 equidistant grooves, so that y^ = y z y\ 
 
 = etc., = -, 
 n' 
 
 metals with some one metal, such as iron. Malting the iron spectrum 
 
 -. a 
 v tt>n^ n 
 
 Hence the displacement becomes 
 
 bttu 
 sin n . 
 
 As the last term is simply the integral over the space -, in a different 
 
 form from before, this is a return to the form we previously had except 
 that it is for a grating of nn' lines instead of n lines, the grating space 
 
 being . 
 
 EXAMPLE 2. Two GROOVES 
 
 But ba/jt = 2 ATT. Hence this becomes 
 
 . v\_ y 
 
 a 
 
 The square of the last term is a factor in the intensity. Hence the 
 spectrum will vanish when we have 
 
 ~n~ ' 
 4 A theorem of Lord Rayleigh's. 
 
534 HENRY A. ROWLAND 
 
 or N _ la 3 a 5 a , 
 
 " ~cT J ~~c\~ > TT" *"*" 
 
 2 y, 2 y, 2 y, 
 Thus when = 2, the 1st, 3d, etc., spectra will disappear, making 
 
 y\ 
 
 a grating of twice the number of lines to the cm. 
 
 When =4, the 2d, 6th, 10th, etc., spectra disappear. When 
 
 y\ 
 
 = 6, the 3d, 9th, etc., spectra disappear. 
 
 y\ 
 
 The case in which = 4, as Lord Rayleigh has shown, would be very 
 
 y\ 
 
 useful as the second spectrum disappears leaving the red of the first 
 and the ultra violet of the third without contamination by the second. 
 In this case two lines are ruled and two left out. This would be easy 
 to do but the advantages would hardly pay for the trouble owing to 
 the following reasons: Suppose the machine was ruling 20,000 lines 
 to the inch. Leaving out two lines and ruling two would reduce the 
 dispersion down to a grating with 5000 lines to the inch. Again, the 
 above theory assumes that the grooves do not overlap. Now I believe 
 that in nearly, if not all, gratings with 20,000 lines to the inch the 
 whole surface is cut away and the grooves overlap. This would cause 
 the second spectrum to appear again after all our trouble. 
 
 Let the grooves be nearly equidistant, one being slightly displaced. 
 
 In this case y t = ? -j- v - 
 
 , Ny, I 7TJV i:Nv . nN ff 
 
 cos 2 TT S3 = [ oos-s- cos - sin -4- am - 
 
 a \ 2 a % 
 
 For the even spectra this is very nearly unity, but for the odd it 
 becomes 
 
 Hence the grating has its principal spectra like a grating of space ^ 
 
 but there are still the intermediate spectra due to the space a, and of 
 intensities depending on the squares of the order of spectrum, and the 
 squares of the relative displacement, a law which I shall show applies 
 to the effect of all errors of the ruling. 
 
 This particular effect was brought to my attention by trying to use 
 a tangent screw on the head of my dividing engine to rule a grating 
 with say 28,872 lines to the inch, when a single tooth gave only 14,436 
 to the inch. However carefully I ground the tangent screw I never was 
 
GRATINGS IN THEORY AND PRACTICE 535 
 
 able to entirely eliminate the intermediate spectra due to 14,436 lines, 
 and make a pure spectrum due to 28,872 lines to the inch, although I 
 could nearly succeed. 
 
 EXAMPLE 3. ONE GROOVE IN m MISPLACED 
 
 Let the space a contain m grooves equidistant except one which is 
 displaced a distance v. The displacement is now proportional to 
 
 Multiplying this by itself with i in place of -+- i, and adding the 
 factors in the intensity, we have the whole expression for the intensity. 
 One of the terms entering the expression will be 
 
 sm 
 
 sin^ sin** 
 2m 2 
 
 Now the first two terms have finite values only around the points 
 
 _^= rw^Vrr, where mN is a whole number. But 2p m -\- 1 is also a 
 2 
 
 whole number, and hence the last term is zero at these points. Hence 
 the term vanishes and leaves the intensity, omitting the groove factor, 
 
 baa . . ba 
 
 sin ~ sin* - 
 
 2 in 2 
 
 The first term gives the principal spectra as due to a grating space 
 of and number of lines nm as if the grating were perfect. The last 
 
 term gives entirely new spectra due to the grating space, a, and with 
 lines of breadth due to a grating of n lines and intensities equal to 
 
 Hence, when the tangent screw is used on my machine for 14,436 
 lines to the inch, there will still be present weak spectra due to the 
 14,436 spacing although I should rule say 400 lines to the mm. This 
 I have practically observed also. 
 
 The same law holds as before that the relative intensity in these 
 
536 HENRY A. ROWLAND 
 
 subsidiary spectra varies as the square of the order of the spectrum and 
 the square of the deviation of the line, or lines from their true position. 
 
 So sensitive is a dividing engine to periodic disturbances that all the 
 belts driving the machine must never revolve in periods containing an 
 aliquot number of lines of the grating; otherwise they are sure to make 
 spectra due to their period. 
 
 As a particular case of this section we have also to consider 
 
 PERIODIC ERRORS OF RULING. THEORY OF " GHOSTS " 
 
 In all dividing engines the errors are apt to be periodic due to 
 " drunken " screws, eccentric heads, imperfect bearings, or other causes. 
 We can then write 
 
 y = a t n + a^ sin (e^ri) + a^ sin (e?n), + etc. 
 
 The quantities e 1? e z) etc., give the periods, and a 1} a 2 , etc., the ampli- 
 tudes of the errors. We can then divide the integral into two parts as 
 before, an integral over the groove and spaces and a summation with 
 respect to the numbers. 
 
 ds . 
 
 I I 'e~ ib < Ax + w) ds = le-tbw j " 
 
 Vy 1 */0 
 
 It is possible to perform these operations exactly, but it is less com- 
 plicated to make an approximation, and take y"- y r = a, a constant 
 as it is very nearly in all gratings. Indeed the error introduced is 
 vanishingly small. The integral which depends on tho shape of the 
 groove, will then go outside the summation sign and we have to per- 
 form the summation 
 
 sine^ + o s sine 2 
 
 Let J n be a Bessel's function. Then 
 
 cos (u sin ?) = 7 () + 2 [J" 2 (w) cos 2 y + J t (w) cos* ^ + etc.] 
 sin (w sin </>) = 2 [Ji (w) sin ^ + /, (w) sin 3 ^ + etc.] 
 
 But e~ iu sin<f> = cos (u sin ^ ) i sin (w sin ^>) . 
 
 Hence the summation becomes 
 
 X [Jo (^0 + 2 ( iJi (S/iOi) sin e^n + J t (ft/taj cos 'Ze^n etc.)] 
 X [J (bvctt*) + 2 ( iJ t (b/jifty) sin e z n + J t (J//a 2 ) cos Zeji etc.)] 
 X [/ (bra,*) + etc.] 
 X [etc.] 
 
GRATINGS IN THEORY AND PRACTICE 
 
 537 
 
 CASE I. SINGLE PERIODIC ERROR 
 In this case only a and a^ exist. We have the formula 
 
 Hence the expression for the intensity becomes 
 
 sn n 
 
 sin n 
 
 Mo e l } 
 
 + etc. 
 
 2 
 
 J 
 
 As n is large, this represents various very narrow spectral lines whose 
 light does not overlap and thus the different terms are independent of 
 each other. Indeed in obtaining this expression the products of quan- 
 tities have been neglected for this reason because one or the other is 
 zero at all points. These lines are all alike in relative distribution 
 of light and their intensities and positions are given by the following 
 table : 
 
 Places. Intensities. Designations. 
 
 Primary line 
 
 Ghosts of 1st order. 
 Ghosts of 2d order. 
 
 Ghosts of 3d order, 
 etc. etc. etc. 
 
 = I* 
 
 = ;*-E- 1 J.'QwJ 
 
 Hence the light which would have gone into the primary line now 
 goes to making the ghosts, so that the total light in the line and its 
 ghosts is the same as in the original without ghosts. 
 
 The relative intensities of the ghosts as compared with the primary 
 line is 
 
538 HENRY A. ROWLAND 
 
 This for very weak ghosts of the first, second, third, etc., order, 
 becomes 
 
 The intensity of the ghosts of the first order varies as the square of 
 the order of the spectrum and as the square of the relative displace- 
 ment as compared with the grating space a . This is the same law as 
 we before found for other errors of ruling, and it is easy to prove that 
 it is general. Hence 
 
 The effect of small errors of ruling is to produce diffused light around 
 the spectral lines. This diffused light is subtracted from the light of the 
 primary line, and its comparative amount varies as the square of the 
 relative error of ruling and the square of the order of the spectrum. 
 
 Thus the effect of the periodic error is to dimmish the intensity of 
 the ordinary spectral lines (primary lines) from the intensity 1 to 
 t7 2 (fy" a i)j and surround it with a symmetrical system of lines called 
 ghosts, whose intensities are given above. 
 
 When the ghosts are very near the primary line, as they nearly always 
 are in ordinary gratings ruled on a dividing engine with a large number 
 of teeth in the head of the screw, we shall have 
 
 f- + A) + Jftai (f* j^} = IJfta^ nearly. 
 oaj \ baj 
 
 Hence the total light is by a known theorem, 
 
 Thus, in all gratings, the intensity of the ghosts as well as the 
 diffused light increases rapidly with the order of the spectrum. This 
 is often marked in gratings showing too much crystalline structure. 
 For the ruling brings out the structure and causes local difference of 
 ruling which is equivalent to error of ruling as far as diffused light is 
 concerned. 
 
 For these reasons it is best to get defining power by using broad 
 gratings and a low order of spectra although the increased perfection of 
 the smaller gratings makes up for this defect in some respects. 
 
 There is seldom advantage in making both the angle of incidence 
 and diffraction more than 45, but, if the angle of incidence is 0, the 
 other angle may be 60, or even 70, as in concave gratings. Both 
 theory and practice agree in these statements. 
 
 Ghosts are particularly objectionable in photographic plates, especi- 
 
GRATINGS IN THEORY AND PRACTICE 539 
 
 ally when they are exposed very long. In this case ghosts may be 
 brought out which would be scarcely visible to the eye. 
 As a special case, take the following numerical results: 
 
 
 1 
 
 
 
 2 
 
 
 
 3 
 
 
 1 
 
 1 
 
 1 
 
 1 
 
 1 
 
 1 
 
 1 
 
 1 
 
 1 
 
 25' 
 
 50 ' 
 
 100 
 
 25' 
 
 50' 
 
 100 
 
 25' 
 
 50' 
 
 100' 
 
 1 
 
 1 
 
 1 
 
 1 
 
 1 
 
 1 
 
 1 
 
 1 
 
 1 
 
 63 ' 
 
 252' 
 
 1008 
 
 16' 
 
 63' 
 
 252 
 
 7 ' 
 
 28' 
 
 102* 
 
 In a grating with 20,000 lines to the inch, using the third spectrum, 
 
 we may suppose that the ghosts corresponding to a i=~ will be visible 
 
 a 50 
 
 and those for - 1 = -^ very troublesome. The first error is a, = T Tnrinnnr 
 a 25 
 
 in. and the second a^ = 5 0*0 o o in. Hence a periodic displacement of 
 one millionth of an inch will produce visible ghosts and one five hun- 
 dred thousandth of an inch will produce ghosts which are seen in the 
 second spectrum and are troublesome in the third. With very bright 
 spectra these might even be seen in the first spectrum. Indeed an over 
 exposed photographic plate would readily bring them out. 
 
 When the error is very great, the primary line may be very faint or 
 disappear altogether, the ghosts to the number of twenty or fifty or 
 more being often more prominent than the original line. Thus, when 
 
 bfia l = 2-405, 5-52, 8-65, etc. = 2*N -^ , 
 
 
 
 the primary line disappears. When 
 
 = 0, 3-83, 7-02, etc. = ZxN ^L , 
 
 the ghosts of the first order will disappear. Indeed we can make any 
 ghost disappear by the proper amount of error. 
 Of course, in general 
 
 r - 2 CM - 1) r j 
 
 U n -- - t/ B _i /_> 
 
 V 
 
 Thus a table of ghosts can be formed readily and we may always tell 
 when the calculation is complete by taking the sum of the light and 
 finding unity. 
 
540 HENRY A. ROWLAND 
 
 72 72 T2 TV 72 72 72 72 72 72 /2 72 72 72 72 
 
 t/0 "1 "2 "8 "4 "5 "6 "7 "8 "9 "10 "11 "12 "13 "U 
 
 
 
 a 
 
 i 
 
 1-000 
 
 
 
 
 
 
 
 
 2 
 
 980 
 
 010 
 
 
 
 
 
 
 
 4 
 
 
 038 
 
 
 
 
 
 
 
 6 
 
 832 
 
 089 
 
 002 
 
 
 
 
 
 
 8 
 
 716 
 
 136 
 
 005 
 
 
 
 
 
 1- 
 
 
 
 586 
 
 194 
 
 019 
 
 
 
 
 
 a 
 
 
 
 050 
 
 333 
 
 1 94 
 
 017 
 
 001 
 
 
 
 2 
 
 605 
 
 000 
 
 969 
 
 186 
 
 040 
 
 003 
 
 
 
 
 
 068 
 
 115 
 
 236 
 
 095 
 
 017 
 
 002 
 
 
 8 
 
 832 
 
 162 
 
 000 
 
 169 
 
 176 
 
 065 
 
 013 
 
 002 
 
 4 
 
 
 
 158 
 
 004 
 
 133 
 
 185 
 
 079 
 
 018 
 
 002 
 
 r , 
 
 
 
 031 
 
 107 
 
 009 
 
 133 
 
 153 
 
 068 
 
 017 -003 
 
 5 
 
 fi 
 
 520 
 
 
 000 
 022 
 
 116 
 077 
 
 etc. 
 059 
 
 013 
 
 128 
 
 131 
 
 061 -017 -003 
 
 7- 
 8 
 
 016 
 
 090 
 029 
 
 .000 
 055 
 
 090 
 013 
 
 etc. 
 085 
 
 Oil 
 
 035 
 
 114 -103 -050 -016 -003 -001 
 
 8' 
 
 10 
 
 654 
 
 000 
 060 
 
 075 
 002 
 
 etc. 
 065 
 
 003 
 
 048 
 
 055 
 
 002 -047 -101 -091 -051 -022 -Oil -009 -022 
 
 This table shows how the primary line weakens and the ghosts 
 strengthen as the periodic error increases, becoming at 2nJV a 2-405. 
 
 tt 
 
 It then strengthens and weakens periodically, the greatest strength 
 being transferred to one of the ghosts of higher and higher order as 
 the error increases. 
 
 Thus one may obtain an estimate of the error from the appearance 
 of the ghost. 
 
 Some of these wonderful effects with 20 to 50 ghosts stronger than 
 the primary line I have actually observed in a grating ruled on one of 
 my machines before the bearing end of the screw had been smoothed. 
 The effect was very similar to these calculated results. 
 
 DOUBLE PERIODIC ERROR 
 
 Supposing as before that there is no overlapping of the lines, we 
 have the following: 
 
 Places. Intensities. 
 
 [/ (ba^ ,/ (toirif } Primary line. 
 
 = ,,. - [7i (ba^J ,7 
 
 (. Ghosts of 1st order. 
 
 /> 
 
 = fi ~ [J (ba^) /! (ba^J 
 
GRATINGS IN THEORY AND PRACTICE 
 
 541 
 
 Places. 
 
 = /j. 
 
 Intensities. 
 
 g t 
 
 ba a 
 
 l4 = /JL ^L [J, (&z 1( J ^ (fo 2 ,O] 2 j- Ghosts of 2d order. 
 
 , 5 = ft |* [ J 
 
 'fi /* ^t 7 I 
 
 f Ghosts of 3d order. 
 
 &* 
 
 A* 9 = ,U T-^ 2 
 
 etc. 
 
 etc. 
 
 Each term in this table of ghosts simply expresses the fact that each 
 periodic error produces the same ghosts in the same place as if it were 
 the only error, while others are added which are the ghosts of ghosts. 
 The intensities, however, are modified in the presence of these others. 
 
 Writing ^ = ba lP . and c 2 = ba^. 
 
 The total light, is 
 
 
 
 
 7 
 
 / 
 
 + etc. 
 
 which we can prove to be equal to 1. 
 
 Hence the sum of all the light is still unity, a general proposition 
 which applies to any number of errors. 
 
 The positions of the lines when there is any number of periodic 
 errors can always be found by calculating first the ghosts due to each 
 error separately; then the ghosts due to these primary ghosts for it as 
 if it were the primary line, and so on ad infinitum. 
 
 In case the ghosts fall on top of each other the expression for the 
 intensity fails. Thus when e 2 = 2e lt e 3 = 3e^ etc., the formula will 
 need modification. The positions are in this case only those due to a 
 single periodic error, but the intensities are very different. 
 
 Places. Intensities. 
 
 P = - 
 ba a 
 
542 HENRY A. ROWLAND 
 
 Places. Intensities. 
 
 AI _ fJL A. [/! (K,"i) /o (fas.i) J 3 (ba^J 7 2 (ba&J + etc.] 2 
 
 *" + [</i C^iAti) t/x (ifl^x) <7 3 (>iAO /i (far,*0 + etc.] 8 , 
 etc. etc. 
 
 We have hitherto considered cases in which the error could not be 
 corrected by any change of focus in the objective. It is to be noted, 
 however, that for any given angle and focus, every error of ruling can 
 be neutralized by a proper error of the surface, and that all the results 
 we have hitherto obtained for errors of ruling can be produced by errors 
 of surface, and many of them by errors in size of groove cut by the dia- 
 mond. Thus ghosts are produced not only by periodic errors of ruling 
 but by periodic waves in the surface, or even by a periodic variation in 
 the depth of ruling. In general, however, a given solution will apply 
 only to one angle and, consequently, the several results will not be 
 identical; in some cases, however, they are perfectly so. 
 
 Let us now take up some cases in which change of focus can occur. 
 The term *r* in the original formula must now be retained. 
 
 Let the lines of the grating be parallel to each other. We can then 
 neglect the terms in z and can write r 2 = y 2 very nearly. Hence the 
 general expression becomes 
 
 where * depends on the focal length. This is supposed to be very 
 large, and hence K is small. 
 
 This integral can be divided into two parts, an integral over the 
 groove and the intervening space, and a summation for all the grooves. 
 The first integral will slightly vary with change in the distance of the 
 grooves apart, but this effect is vanishingly small compared with the 
 effect on the summation, and can thus be neglected. The displace- 
 ment is thus proportional to 
 
 K y*\ 
 
 CASE I. LINES AT VARIABLE DISTANCES 
 In this case we can write in general 
 
 y = an + atf + a^n 3 + etc. 
 
 As K, a u a 2 , etc., are small, we have for the displacement, neglecting 
 the products of small quantities, 
 
 (an + Oin a + a a n 8 + etc.) a 3 2] . 
 
GRATINGS IN THEORY AND PRACTICE 543 
 
 Hence the term a^n 2 can be neutralized by a change of forms ex- 
 pressed by fjia 1 =K a 2 . Thus a grating having such an error will have 
 a different focus according to the angle n, and the change will be -f- on 
 one side and on the other. 
 
 This error often appears in gratings and, in fact, few are without it. 
 
 A similar error is produced by the plate being concave, but it can 
 be distinguished from the above error by its having the focus at the 
 same angle on the two sides the same instead of different. 
 
 According to this error, a^n 2 , the spaces between the lines from one 
 side to the other of the grating, increase uniformly in the same manner 
 as the lines in the B group of the solar spectrum are distributed. For- 
 tunately it is the easiest error to make in ruling, and produces the least 
 damage. 
 
 The expression to be summed can be put in the form 
 
 ib (>! a 2 ) n 2 + ib/tatf + ib Oa 3 -f ib (/^ <*)'] n*+ etc.] 
 
 The summation of the different terms can be obtained as shown 
 below, but, in general, the best result is usually sought by changing 
 the focus. This amounts to the same as varying K until //a x *a 2 = 
 as before. For the summation we can obtain the following formula from 
 the one already given. Thus 
 
 Hence 
 
 vn -\ e Zipn sm n P e ip (n - 1). 
 
 sin p 
 
 = e p( -i) 
 
 m 
 
 dp J I amp 
 
 When n is very large, writing *^ = pn = n Nn -f q, we have 
 
 dq 
 Whence writing 
 
 c = 
 
 c' =. /JLCii, 
 
 c" = b &a 3 + i 
 
 c'" = etc., 
 
544 
 
 the summation is 
 
 HENRY A. ROWLAND 
 
 ( 
 
 + etc. 
 
 sn 
 
 dq 
 
 rf* sin <y __ 
 ~dq* q 
 
 _ <7 cos <y sin q 
 
 S * D 
 
 2q cos <y + (2 g 2 ) sin g 
 q* ' 
 
 g (6 g 2 ) cos q (6 3g 2 ) sin 
 ~~ 
 
 < 
 
 etc. 
 
 etc. 
 
 These equations serve to calculate the distribution of light intensity 
 in a grating with any error of line distribution suitable to this method 
 of expansion and at any focal length. For this purpose the above 
 summation must be multiplied by itself with -f- i in place of i. 
 
 The result is for the light intensity 
 
 j^ sin q 
 dq q 
 
 + 2c - + etc. 
 
 16 
 n* 
 
 Uq 3 
 
 9 
 
 sin q 
 
 16 
 
 As might have been anticipated, the effect of the additional terms is 
 to broaden out the line and convert it into a rather complicated group 
 of lines, as can sometimes be observed with a bad grating. At any 
 given angle the same effect can be produced by variation o'f the plate 
 from a perfect plane. Likewise the effect of errors in the ruling may 
 be neutralized for a given angle by errors of the ruled surface, as noted 
 in the earlier portions of the paper. 
 
50 
 A NEW TABLE OF STAND AKD WAVE-LENGTHS 
 
 [Johns Hopkins University Circulars, No. 106, p. 110, 1893; Philosophical Magazine [5], 
 XXXVI, 49-75, 1893; Astronomy and Astro- Physics, XII, 321-347, 1893] 
 
 PREFATORY NOTE 
 
 During the last ten years I have made many observations of wave- 
 lengths, and have published a preliminary and a final table of the wave- 
 lengths of several hundred lines in the solar spectrum. 
 
 For the purpose of a new table I have worked over all my old observa- 
 tions, besides many thousand new ones, principally made on photo- 
 graphs, and have added measurements of metallic lines so as to make 
 the number of standards nearly one thousand. 
 
 Nearly all the new measurements have been made on a new measur- 
 ing machine whose screw was specially made by my process 1 to cor- 
 respond with the plates and to measure wave-lengths direct with only 
 a small correction. 
 
 The new measures were made by Mr. L. E. Jewell, who has now be- 
 come so expert as to have the probable error of one setting about T ir?nF 
 division of Angstrom, or 1 part in 5,000,000 of the wave-length. Many 
 of these observations, however, being made with different measuring 
 instruments, and before such experience had been obtained, have a 
 greater probable error. This is especially true of those measurements 
 made with eye observations on the spectrum direct. The reductions of 
 the reading were made by myself. 
 
 Many gratings of 6 in. diameter and 21^ feet radius were used; and 
 the observations were extended over about ten years. 
 
 The standard wave-length was obtained as follows: Dr. Bell's value 
 of D 1 was first slightly corrected and became 5896-20. C. S. Peirce's 
 valfce of the same line was corrected as the result of some measurements 
 made on his grating and became 5896-20. The values of the wave-length 
 then become 
 
 See Encyc. Brit., art. Screw. 
 35 
 
546 HENKY A. EOWLAND 
 
 Weight. Observer. D. 
 
 o 
 
 1 Angstrom, corrected by Thalen 5895-81 
 
 2 Miiller & Kempf 5896-25 
 
 2 Kurlbaum . 5895-90 
 
 5 Peirce 5896-20 
 
 10 Bell . ..5896-20 
 
 Mean 5896-156 
 
 As the relative values are more important for spectroscopic work 
 than the absolute, I take this value without further remark. It was 
 utilized as follows: 
 
 1st. By the method of coincidences with the concave grating, the 
 wave-lengths of 14 more lines throughout the visible spectrum were 
 determined from this with great accuracy for primary standards. 
 
 2d. The solar standards were measured from one end of the spectrum 
 to the other many times; and a curve of error drawn to correct to these 
 primary standards. 
 
 3d. Flat gratings were also used. 
 
 4th. Measurements of photographic plates from 10 to 19 inches long 
 were made. These plates had upon them two portions of the solar 
 spectrum of different orders. Thus the blue, violet and ultra violet 
 spectra were compared with the visible spectrum, giving many checks 
 on the first series of standards. 
 
 5th. Measurements were made of photographic plates having the 
 solar spectrum in coincidence with metallic spectra, often of three 
 orders, thus giving the relative wave-lengths of three points in the 
 spectrum. 
 
 Often the same line in the ultra violet had its wave-length deter- 
 mined by two different routes back to two different lines of the visible 
 spectrum. The agreement of these to y-j^ division of Angstrom in 
 nearly every case showed the accuracy of the work. 
 
 6th. Finally, the important lines had from 10 to 20 measurements on 
 them, connecting them with their neighbors and many points in the 
 spectrum, both visible and invisible; and the mean values bound the 
 whole system together so intimately that no changes could be made in 
 any part without changing the whole. 
 
 This unique way of working has resulted in a table of wave-lengths 
 from 2100 to 7700 whose accuracy might be estimated as follows: 
 
 Distribute less than ^^ division of Angstrom properly throughout 
 
A NEW TABLE OF STANDARD WAVE-LENGTHS 547 
 
 the table as a correction, and it will become perfect within the limits 
 2400 and 7000. 
 
 The above is only a sketch of the methods used. The complete de- 
 tails of the work are ready for publication but I have not yet found any 
 journal or society willing to undertake it. 2 
 
 [The tables of wave-lengths are omitted.] 
 
 2 [These details were finally published in the Memoirs of the American Academy of 
 Arts and Sciences, XII, 101-186, 1896, under the title, ' On a Table of Standard Wave- 
 Lengths of the Spectral Lines.'] 
 
51 
 
 ON A TABLE OF STANDARD WAVE-LENGTHS OF THE 
 
 SPECTRAL LINES 1 
 
 
 
 [Memoirs of the American Academy of Arts and Sciences, XII, 101-186, 1896] 
 PRESENTED MAY 10, 1898 
 
 Investigations on Light and Heat, made and published wholly or in part with appro- 
 priation from the Rumford Fund 
 
 Some years since, having made a machine for ruling gratings and dis- 
 covered the concave grating, which placed in my hands an excellent 
 process for photographing spectra, I applied myself to photograph the 
 solar spectrum. The property of the concave grating, mounted in the 
 method which I use, of producing a normal spectrum gave me the 
 means of adding a scale of wave-lengths, and so producing a. photo- 
 graphic map of the solar spectrum on a very large scale and of great 
 accuracy. I soon after constructed a very much better ruling engine, 
 which is kept at a uniform temperature in the vault of the new physical 
 laboratory of the Johns Hopkins University, with which I have made 
 very much better gratings. I therefore went over the whole process 
 once more, extending the map to include B, and making new negatives 
 of the whole spectrum very much better than the old. This set of ten 
 photographic plates is now familiar to most spectroscopists. 
 
 In order to place the scale on the negatives, it was necessary to know 
 the wave-lengths of certain standard lines. Of course my first thought 
 was of Angstrom, whose measurements were the wonder of his time. 
 On trying to place my scale according to his figures, I found it impos- 
 sible to make them and my photographs agree ; and I finally was forced 
 to the conclusion that a new series of standards was needed before I 
 could go further. Here again the concave grating came to my rescue. 
 All the spectra are in focus at once, and relative measures can thus be 
 made at once by micrometric measures of the overlapping spectra. 
 Again, the spectrum is normal, and so a micrometer of very long range 
 could be used. To obtain the primary standards by means of overlap- 
 ping spectra, I have used gratings with from 3000 up to 20,000 lines to 
 
 1 An abstract of this paper has recently appeared in 'Astronomy and Astro-Physics,' 
 and in the 'London Philosophical Magazine.' 
 
TABLE OF STANDARD WAVE-LENGTHS OF THE SPECTRAL LINES 549 
 
 the inch, and from 13 to 21| feet focus. The first series made with the 
 13-foot grating by Mr. Koyl in 1882 was not found quite accurate 
 enough, and I have since made personally a long series with gratings 
 of 21| feet focus which is mnch more accurate. These long focus grat- 
 ings had from 7000 to 20,000 lines to the inch, and were ruled on two 
 dividing engines, while the 13-foot one had a less number, possibly 
 3000. There are two principal errors to guard against in this method, 
 the first peculiar to the method of coincidences, and the second to any 
 method where gratings are used. 2 The first is that, where spectra are 
 over each other and the lines therefore often on top of each other, the 
 line of one spectrum may be apparently slightly displaced by the 
 presence of one from another spectrum, although the latter may be 
 almost invisible. The use of proper absorbents obviates this difficulty. 
 The second source of error is more subtle, and arises from the diamond 
 ruling differently on different parts of the grating. It is more apt to 
 occur in concave gratings than plane ones, although few are perfectly 
 free from the error, as it is very difficult to get a diamond to rule a 
 concave grating uniformly. Looking at the grating in spectra of 
 different orders, the grating may appear uniform from end to end in 
 one, and possibly brighter at one end than the other in another spec- 
 trum. This gives a chance for any imperfection in the form of the 
 surface of the grating, or any errors in its ruling, or indeed the spheri- 
 cal aberration of the lenses or concave grating, to affect the measure- 
 ment of relative wave-length. 3 This error I have guarded against by 
 using only uniformly ruled gratings, reversing them, and using a great 
 number of them. I have also used the coincidence of only the lower 
 orders of spectra, such as the 2d, 3d, 4th, oth, and 6th. Coincidences 
 up to the 12th were, however, observed by Mr. Koyl with the 13-foot 
 concave, and probably have some errors of this nature. 
 
 In this way I established about fifteen points in the visible spectrum 
 which served as primary standards. These were so interwoven by the 
 coincidences that I have great confidence in the value of most of them. 
 
 2 The variation of the dispersion of the air with the thermometer and barometer 
 is probably not worth considering for the visible part of the spectrum, although it 
 might be worth investigating for the two extremities of the spectrum. 
 
 3 The error of using gratings of variable brightness in different parts, or those 
 with imperfect ruling of any kind, I have constantly guarded against. Such I be- 
 lieve to be the principal causes of the great errors in relative and absolute wave- 
 lengths in Vogel's tables, as the gratings he used, made by Wandschaft, were full of 
 errors of all kinds. 
 
550 HENEY A. ROWLAND 
 
 Indeed, no process of angular measurement could approach the accuracy 
 of this one. 
 
 Thus, using a line P to start with, I determine other groups of lines, 
 a', V, c', d', etc. From these again I find groups, some of which may 
 be the same as the first; then again from these, other groups. The 
 process can he continued further, hut we are apt to come hack to the 
 same lines again, and we are further limited by the visibility of the 
 lines. Thus the limit of great accuracy by eye observation in either 
 direction is practically 4200 and 7000; although in a dark room, especi- 
 ally in the first spectrum, one can see much further, even beyond the A 
 group, although it is difficult to set on the lines, and one is apt to mis- 
 take groups of lines for single lines. 4 When one uses a group as a 
 standard, and one or more of the group is an atmospheric line which 
 varies, the measures will of course vary also, unless the atmospheric 
 line is in the centre of the group. This is a very common source of 
 error, and has caused me. much trouble. In a grating with a very 
 bright second spectrum, I have, however, obtained the coincidence of A 
 with the region whose wave-length is about 5080, and have thus con- 
 firmed the value given in my preliminary table, which was obtained by 
 a very long interpolation passing from the first into the second spec- 
 trum. 
 
 The accuracy of these primary standards can be estimated from the 
 equations given in Table VII. It is there seen that there is scarcely 
 any difference in the different measures as derived from different lines. 
 
 It is to be specially noted that the wave-length of P and the lines 
 directly determined from it have no more weight than any of the 
 others. The table might just as well have been arranged with the D 
 line, or any other, first. The true way of discussing the results is to 
 form a series of linear equations, about twenty-six in all, and solve 
 them. This is the method I have used, although I have not discussed 
 them by the method of least squares. 5 
 
 Some miscellaneous observations not included in the table allowed 
 me to add a few more line? to these primary standards. 
 
 Having completed these primary standards, I then observed several 
 
 
 
 4 la a very bright grating I have faintly seen, and even measured, lines down to 
 wave-length 8500. My assistant, Mr. L. E. Jewell, can see far into what is called 
 the ultra violet, even to wave-length 3500 or beyond. 
 
 5 The calculations of this paper have involved about a million figures, of which I 
 have personally written more than half. Hence I am not anxious for more labor of 
 this kind. 
 
TABLE OF STANDARD WAVE-LENGTHS OF THE SPECTRAL LINES 551 
 
 hundred standard lines in the visible spectrum, including these primary 
 standards, with a micrometer having a range of five inches, and very 
 accurately made. The spectrum being strictly normal, the readings so 
 made were proportional to the wave-length. They could have been used 
 simply to interpolate between the primary standards, but I preferred 
 another method. The readings of the micrometer were made to over- 
 lap, so that, by adding a constant to each set,- a continuous series could 
 be formed for the whole spectrum which would be proportional to the 
 wave-length except for some slight errors due to the working of the 
 apparatus for keeping the focus constant. Making this series coincide 
 with two standards at the ends, the wave-lengths of all could be obtained 
 by simply multiplying the whole series by one number and adding a 
 constant. This usually gave the wave-lengths of the whole spectrum 
 within 0-1 or 0-2 divisions of Angstrom. The differences of this series 
 from the primary standards were then plotted, and a smooth curve 
 drawn through the points thus found. The ordinates of this curve 
 then gave the correction to be applied at any point. 
 
 It is to be noted that the departure from the normal spectrum was 
 very small, and the correction thus found was very certain. The cause 
 of the departure was not apparent, but may have been the slight tilting 
 of the spectrum, by which it was measured somewhat obliquely at 
 places. 
 
 The visible spectrum was thus gone over five or more times in this 
 manner, with several different gratings and in different orders of spectra. 
 The results are given in Table X, Columns C, R, p, q, m, 0, e, h, i, etc. 
 The spectrum from the green down to and including A was also ob- 
 served on a large instrument for flat gratings, having lenses six and 
 one-half inches in diameter and of eight feet focus. These latter 
 observations are marked C". This region I intend at some future time 
 to observe further. 
 
 It was now required to observe the ultra violet to complete the series. 
 For this purpose the coincidences of the 3d, 3d, 4th, 5th, and 6th 
 spectra of a 7000, 21$ feet radius, grating were photographed. My in- 
 strument will take in photographic plates twenty inches long, but there 
 will be a slight departure from a normal spectrum in so long a plate. 
 Hence plates ten inches long were mostly used for this special series. 
 Before the camera was placed a revolving plate of metal about three- 
 sixteenths of an inch thick, and having a slit in it of the same width.' 
 
 6 This is described in the Johns Hopkins Circular of May, 1889, by Dr. Ames. 
 
552 HENRY A. BOWL AND 
 
 When the flat side was parallel to the camera plate, a strip of the 
 spectrum three-sixteenths of an inch wide fell on the plate. When 
 turned ninety degrees, the plate shielded this portion and exposed the 
 rest. Using absorbents., it was thus possible to photograph a strip of 
 say the 4th spectrum between two strips of the 5th. This arrangement 
 is better than having only two edges come together. To correct any 
 movement of the apparatus during the time of exposure, I expose on 
 one spectrum, then on the other, and back again on the first. 
 Placing the negatives so obtained on a dividing engine with a micro- 
 scope of very low power and a tightly stretched cross-hair, the coin- 
 cidence of the two spectra can be measured. Owing to the large scale 
 of the photographs, about that of Angstrom, an ordinary dividing 
 engine having errors not greater than y^Vo" i ncn can be used, but the 
 negatives should be gone over at least twice, reversing them end for 
 end. Two screws were used in the engine and finally another com- 
 plete machine was constructed, giving wave-lengths direct with only a 
 slight correction. For determining the wave-length of metallic lines, 
 the same process can be used with wonderful accuracy. 
 
 The results are given in the columns marked PL with the number 
 of the plates. The accuracy is very remarkable, and I think the figures 
 establish the assertion that the coincidence of solar and metallic lines 
 can be determined with a probable error of one part in 500,000 by only 
 one observation. 
 
 This process not only gave me measures of the ultra violet, but also 
 new observations of the visible spectrum. So far in my work on these 
 coincidences, I have only used erythrosin plates going a little below D; 
 but cyanine plates might be used to B, or even in the ultra red, as Trow- 
 bridge has recently shown. One plate, No. 20, however, connects wave- 
 lengths 6400 and 3200. 
 
 Thus I have constructed a table of about one thousand lines, more 
 or less, which are intertwined with each other in an immense number 
 of ways. They have been tested in every way I can think of during 
 eight or nine years, and have stood all the tests; and I think I can 
 present the results to the world with confidence that the results of the 
 relative measures will never be altered very much. I believe that no 
 systematic error in the relative wave-lengths of more than about '01 
 exists anywhere except in the red end as we approach A. Possibly 
 -03, or even less, might cover that region. 
 
 The relative measures having thus been obtained, we have means in 
 the concave grating of obtaining the wave-lengths of the lines of metals 
 
TABLE OF STANDARD WAVE-LENGTHS OF THE SPECTRAL LIXES 553 
 
 to a degree of accuracy hitherto unknown, and thus of solving the great 
 problem of the mathematical distribution of these lines. 
 
 But for the comparison of spectra, as measured by different observers, 
 some absolute scale is needed. Hitherto Angstrom has been used. 
 But it is now very well known that his standard measure was wrong. 
 As his relative measures are also very wrong, I have concluded that the 
 time has come to change not only the relative measures, but the abso- 
 lute also. To this end Dr. Louis Bell worked in my laboratory for 
 several years with the best apparatus of modern science, using two 
 glass and two speculum metal gratings, ruled on two dividing engines 
 with four varieties of spacing, three of which were incommensurable 
 or nearly so, with two spectrometers of entirely different form, with a 
 variety of standard bars compared in this country and in Europe, and 
 with a special comparator made for the measure of gratings. His result 
 agrees very well with the next best determination, that of Mr. C. S. 
 Peirce of the U. S. Coast Survey. His final result agrees within 1 in 
 50,000 with his preliminary value. 7 This most recent value, combined 
 with those of Peirce, Miiller and Kempf, Kurlbaum and Angstrom, I 
 have adopted to reduce my final results to, although the calculations are 
 made according to Bell's preliminary value. See Appendix A. 
 
 But it rests with scientific men at large to adopt some absolute 
 standard. The absolute standard is, of course, not so important as the 
 relative, and possibly the average of Angstrom might be adopted. But 
 for myself I do not believe in continuing an error of this sort indefi- 
 nitely. All the results obtained before the concave grating came into 
 use were so imperfect, that they must be replaced by others very soon. 
 With a good concave grating one man in a few years could obtain the 
 wave-lengths of the elements with far greater accuracy than now 
 known. 
 
 As an aid to this work, I have constructed the table of wave-lengths 
 given in this paper, which have already been adopted by the British 
 Association and by the most noted writers of Germany and other 
 countries, and sincerely hope that it will aid in the work of making 
 the wave-length of a spectrum line a definite quantity within a few 
 hundredths of a division of Angstrom. 
 
 ABSOLUTE WAVE-LENGTH OF D 
 
 The following is an estimate of the absolute wave-length of the D line 
 from the best determinations. First, I shall recalculate the portion of 
 
 1 American Journal of Science, 1887. 
 
554 HENRY A. ROWLAND 
 
 Dr. Bell's paper s in which the calibration of the grating space is taken 
 into account. The method of correction is founded on the principle 
 that a linear error in the spaces only affects the focal length, and not 
 the angle, and that small portions which have an error, and thus throw 
 the light far to one side, should be rejected. The corrections Dr. Bell 
 has used seem to me very proper, except to grating III, which appears 
 to me to be twice too great. I find the following : 
 
 Grating. D. Correction. Final Values. 
 
 I. 
 
 5896-20 
 
 02 
 
 5896-18 
 
 II. 
 
 5896-14 
 
 + -09 
 
 5896-23 
 
 III. 
 
 5896-28 
 
 -06 
 
 5896-22 
 
 IV. 
 
 5896-14 
 
 -f -03 
 
 5896-17 
 
 Mean value, 5896-20. 
 
 This is very nearly the value given by Dr. Bell. 
 
 The determination of Mr. C. S. Peirce of the TJ. S. Coast Survey is 
 certainly a very accurate one. Dr. Bell and myself have made some 
 attempts to calibrate his gratings, which he sent to us for the purpose, 
 and to correct for the scale used by him. There is great uncertainty 
 in this process, as we had only a portion of the necessary data. The 
 correction of his scale was also uncertain, because the glass scales used 
 by him may have changed since he used them, in the manner thermom- 
 eter bulbs are known to change. Correcting, then, only for the error of 
 ruling in the gratings, we have: 
 
 Peirce's value 5896-27 
 
 Correction * -07 
 
 5896-20 
 
 The correction for the scale would be about as much more in the same 
 direction, provided the glass scales had not changed. But it is too 
 uncertain to be used, although I have applied it in my preliminary 
 paper. 
 
 Kurlbaum's result, made with two good modern gratings, has the 
 defect that the gratings were 42 and 43 mm. broad, quantities which 
 it is impossible to compare accurately with a metre. His small objec- 
 tives, one inch in diameter, could not take in light from the whole 
 grating, and so the grating space was not determined from the portion 
 
 8 American Journal of Science, 1888. 
 
 9 Bell, American Journal of Science, May, 1888, p. 365. 
 
TABLE OF STANDARD WAVE-LEN T GTHS OF THE SPECTRAL LINES 555 
 
 of the grating used. The spectrometer was poor, and the errors of 
 the grating undetermined. 
 
 Miiller and Kempf used four gratings, evidently of very poor quality, 
 as they give results which differ 1 in 10,000. 
 
 The result of Angstrom was a marvel at the time, but the Nobert 
 gratings used by him would now be considered very poor. Taking 
 Thalen's correction for error of scale, we have for the mean of the E 
 lines 5269-80, which gives, by my table of relative wave-lengths, D = 
 5895-81. It is rather disagreeable to estimate the relative accuracy 
 of observations made by different observers and in different countries, 
 but in the interest of scientific progress I have attempted it, as follows : 
 
 o Wt - 
 
 Angstrom 5895-81 1 
 
 Miiller and Kempf 5896-25 2 
 
 Kurlbaum 5895-90 2 
 
 Peirce 5896-20 5 
 
 Bell 5896-20 10 
 
 Mean, 5896-156 in air at 20 and 760 mm. pressure. 
 
 This must be very nearly right, and I believe the wave-length to be 
 as well determined as the length of most standard bars. Indeed, fur- 
 ther discussion of the question would involve a very elaborate discus- 
 sion of standard metres, a question involving endless dispute. I think we 
 may say that the above result is within 1 in 100,000 of the correct value, 
 which is very nearly the limit of accuracy of linear measurements. This 
 should be so, as the probable error of the angular measures affects the 
 wave-length only to 1 in 2,000,000, 10 and hence nearly the whole accuracy 
 rests on the linear measures. 
 
 RESUME OF PROCESS FOR OBTAINING RELATIVE WAVE-LENGTHS 
 
 1. Determination of about 20 lines in the visible spectrum by coin- 
 cidences by Koyl." 
 
 10 Is not a grating and spectrometer thus the best standard of length, and almost 
 independent of the temperature? Gratings of 10 cm. length can now be ruled on 
 my new engine with almost perfect accuracy, as seen in the calibration of Grating 
 IV in Dr. Bell's paper, and it seems to me the time has come for their practical use. 
 
 11 These observations of Mr. Koyl were finally given no weight, on account of the 
 inferior apparatus used. They serve a useful purpose, however, as checks on the 
 other work. 
 
556 HENEY A. ROWLAND 
 
 2. Determination of about 15 lines in the visible spectrum by coin- 
 cidences by Rowland, using several gratings of 21^ feet focus. 
 
 3. Interpolation by direct eye observations with concave gratings of 
 21 feet focus and micrometer of 5 inches range and of almost perfect 
 accuracy. 
 
 4. Interpolation by means of flat gratings. 
 
 5. Measurement of photographic plates from 10 to 19 inches long, 
 having two or three portions of the spectrum in different orders on 
 them, thus connecting the ultra violet and blue with the visible spec- 
 trum. The fact that nearly the same values are obtained for the violet 
 and ultra violet by use of different parts of the visible spectrum proves 
 the accuracy of the latter. 
 
 6. Measurement of photographic plates having the solar visible spec- 
 trum in coincidence with the metal lines of different orders of spectra. 
 The fact that the wave-lengths of the metal lines are very nearly the 
 same as obtained from any portion of the visible or ultra violet spec- 
 trum proves the accuracy of the latter, as well as that of the metallic 
 wave-lengths. 
 
 7. Measurement of plates having metallic spectra of different orders. 
 
 ADVANTAGES OF THE PKOCESS 
 
 The only other process of obtaining relative wave-lengths is by 
 means of angular measures. Supposing the angle to be about 45, an 
 error of 1" will make an error of about 1 in 200,000 in the sine of the 
 angle. When one considers the changes of temperature and barometer 
 measuring on one line and then another, together with the errors of 
 graduation, it would be a difficult matter to measure this angle to 2", 
 making an error of 1 in 100,000, or about ^ division of Angstrom. 
 
 Looking over the observations of principal standards made under 
 the direction of Professor Vogel in Potsdam, with very poor gratings 
 but an excellent spectrometer, we find the average probable error to 
 be about =b T -g- uVinr f ^ ne wave-length, which is not far from the other 
 estimate. This does not include constant errors, and I believe the 
 probable error to be really greater than this. 
 
 The method of coincidences by the concave grating gives far superior 
 results. The distance to be measured is very small, and the equivalent 
 focal length of a telescope to correspond would be very great (21 
 feet). Furthermore, all changes of barometer and thermometer are 
 eliminated at once, except the small effect on the dispersion of the air, 
 which, when known, can be corrected for. It is not to be wondered at 
 
TABLE OF STANDABD WAVE-LENGTHS OF THE SPECTEAL LINES 557 
 
 that this method is far superior to the former. The probable error is, 
 indeed, reduced to Tinnhnnr? or even ^ ess ^ or the best lines. Where 
 the interpolation can be made on photographs, this probable error is 
 scarcely increased at all ; but even taking it at twice the above estimate, 
 the method even then remains from three to five times as accurate as 
 that of angular measurement. Indeed, the impression made on my 
 mind in looking over Vogel's Potsdam observations is, that my tables 
 and process are ten times as accurate as theirs; and I think any careful 
 student of both processes will come to a similar conclusion. 
 
 The wonderful result that can be obtained by the measurement of 
 photographs on the new micrometer, which can measure plates over 
 twenty inches long, is partly seen in the table. Where the distance is 
 only a few inches, the wave-length of a series of lines can be measured 
 with a probable error of less than T ^ of a division of Angstrom. 
 Indeed, a series would determine any line so that the probable error 
 would be even -0000001 of the whole. This would detect a motion 
 in the line of sight of 140 feet per second! 
 
 From the tests I have made on my standards, I am led to believe 
 that down +o wave-length 7000, a correction not exceeding -01 
 division of Angstrom (1 part in 500,000), properly distributed, would 
 reduce every part to perfect relative accuracy. 
 
 To ascend to the next degree of accuracy would need many small cor- 
 rections which would scarcely pay. It is reasonable to assume that a 
 higher degree of accuracy will not be needed for twenty-five years, as 
 the present degree is sufficient to distinguish the lines of the different 
 elements from one another in all cases that I have yet tried. 
 
 DETAILS OF WOEK 
 
 To reduce all the observations in a given region to one line, relative 
 observations extending a short distance either side of the standard 
 region are necessary. Thus the mean of 4215 and 4222 can be taken as 
 the standard, and, if only one is observed, it can be reduced to the 
 standard by a correction -f 3-358 or 3-358. But it is not necessary 
 to take the mean of the lines as a standard, as any one of them may 
 be so taken, or even any other point where there is no line, as the point 
 is only to be used in the mathematical work, and finally disappears 
 altogether. 
 
 Table II gives results of this nature. The letters at the top of each 
 series, e, g, h, ;, etc., are the arbitrary names of the standards. The 
 first columns refer to the series of observations, " Co." being observa- 
 
558 HENRY A. KOWLAND 
 
 tions made at the time of measuring the coincidences; Plates 9, 10, etc., 
 refer to photographic plates; C, R, etc., refer to the series as given in 
 the final table, although they may differ very slightly from the latter, 
 as the final table contains slight corrections. Figures in parentheses 
 are the number of readings. The photographs were usually measured 
 from two to six times. 
 
 Table III gives the first series of observations made in 1884 with 
 a 21 foot concave, 14,436 lines to the inch. The numbers taken for 
 the standards are only preliminary, and agree as nearly as practicable 
 with my Table of Preliminary Standards. As only differences are 
 finally used, they are sufficiently near. The fractions give the order 
 of the spectra observed. 
 
 Thus, the first observation on Ji and t is worked up as follows : 
 
 4691-590 7027-778 
 
 Correction to standard. . . . 626 +2-785 
 
 4690-964 7030-563 
 
 4691-590 4690-326 7027-778 
 
 626 +-626 +2-785 
 
 4690-964 4690-952 7030-563 
 
 
 4691-590 
 626 
 
 7040-092 
 9-547 
 
 4690-964 
 
 7030-545 
 
 Weight. 
 1 
 
 h 
 
 4690-964 
 
 t 
 7030-563 
 
 2 
 
 4690-958 
 
 7030-563 
 
 2 
 
 4690-964 
 
 7030-545 
 
 4690-962 7030-556 
 
 The equation 3 Ji 2 t = 11-774 then readily follows. 
 
 Tables IV and V are from a 21 foot concave with 7218 lines to the 
 inch, used on both sides, and thus equivalent to two gratings used on 
 one side only. I have not yet determined theoretically whether the 
 minor errors are perfectly neutralized in this manner, but it would evi- 
 dently have a tendency in this direction. 
 
 The photographic coincidences are given in the main table (X), as 
 not only the standards are compared by this process, but whole regions 
 
TABLE OF STANDARD WAVE-LEXGTHS OF THE SPECTRAL LINES 559 
 
 are photographed side by side. Both a 10,000 and a 20,000 concave 
 were used for this work. 
 
 Table VI gives the collection of the equations relating to the visible 
 spectrum, the final results being given in Table VII. 
 
 The proper method of treating these twenty-six equations would be 
 by the method of least squares. But it would be so long and tedious, 
 and so liable to mistake, that I have adopted the method of starting at 
 one point and going forward until all the equations are reached. Thus 
 (Table VII), starting with an assumed value of e, we can calculate p, n, 
 1, 1c, ;', o, t. 
 
 Using the eight values thus found once more, from p we have g, Jc, Z; 
 from n we have h, t, g; with similar results for the others. Collecting, 
 we then have e, f, g, h, j, Tc, I, n, o, p, q, t. Using these once more, we 
 have values of all the standards. We could do this any number of 
 times, keeping the proper weights, but I thought this number was suffi- 
 cient. The second calculation is done in the same manner, starting from 
 o, however, and is given in Table VIII. 
 
 The results of the two calculations are given in Table IX. Taking 
 the mean and adding the results of local micrometer measurements, we 
 obtain the column marked " Eelative Wave-Lengths." 
 
 Reducing these values by 1 part in 200,000, we make them agree 
 with the absolute value of the standard as before agreed upon. Thus 
 the column of standards is obtained for use in the visible spectrum. 
 
 For ordinary interpolation with the short and imperfect micrometers 
 generally used, and working with a flat grating and a spectrum not nor- 
 mal, the standards would be too far apart. But with such a long and 
 perfect micrometer as I use, and working with the normal spectrum of 
 a concave grating, they are entirely sufficient. However, I have filled 
 in the interval from 7030 to 7621 by some extra substandards at 7230. 
 
 The micrometer for eye observations has a range of five inches, and 
 the machine for measuring photographs of more than twenty inches, 
 both with practically perfect screws made by my process. The eye ob- 
 servations are not an interpolation, in the ordinary sense, between the 
 standards, but the whole series is continuous, the micrometer observa- 
 tions overlapping so that they join together to any length desired. By 
 measuring from the D line in one spectrum to the D line in the next, 
 and including the overlapping spectra, no further standards would be 
 necessary, as all the lines of the spectrum would be determined at once, 
 knowing the wave-length of the D line. But I usually plotted the 
 difference of the standards from the micrometer determination, usually 
 
560 HEXEY A. ROWLAND 
 
 o 
 
 amounting to less than one- or two-tenths of a division of Angstrom, and 
 so corrected the whole series to the standards. Sometimes two, or even 
 three, overlapping spectra were measured at once. 
 
 To make Table X, the following process was used: 
 
 1st. From all the observations at my disposal, I determined a few 
 more lines around the main standards, and put them in the second col- 
 umn, marked St., so that I should have a greater number of points to 
 draw my curve through. 
 
 2d. I then put down a few observations which were made by meas- 
 uring overlapping spectra. 
 
 3d. Then the main eye observations were put down as follows: 
 
 p extending from 4071 to 7040, 3d spectrum, 14,436 grating. 
 q " 4999 to 7035, " " " " " 
 
 " " 4859 to 7040, " " " " " 
 c " " 4859 to 6079, (fragmentary^. 
 
 " 6855 to 6909, 2d spectrum, 14,436 grating. 
 
 5162 to 7201, " " " " " 
 
 5742 to 7628, 1st spectrum, 14,436 grating. 
 
 1 " " 6065 to 7671, " " '< " " 
 C' ' " 6855 to 7714, plane grating. 
 
 R' '< " 5139 to 5296, 2d spectrum, 14,436 grating. 
 
 t " " 6499 to 6929, " " " " " 
 
 a " " 6278 to 6322, " " " " " 
 
 E " " 4048 to 4824, " " " " " 
 
 4th. The series of photographs containing coincident spectra, mostly 
 on plates so short as to make the spectra nearly normal, were now in- 
 troduced. The plates were numbered from 1 to 20, ISTos. 7 and 19 being 
 rejected because imperfect. 
 
 This series of plates was obtained by photographing a narrow strip 
 of one spectrum between two strips of another, the overlapping spectra 
 being separated by absorption. In order to eliminate any change in 
 the apparatus during the exposure, the latter was divided into three 
 parts, the first and third being given to the same spectrum. 
 
 This series of plates gives me a continuous series of photographs from 
 wave-length 7200 to the extremity of the ultra violet spectrum, each 
 part being interwoven with one or two other parts of the spectrum. 
 Thus, wave-length 3900 comes from 5200 and 5850 with only a slight 
 difference in values. There is scarcely any difference in any wave- 
 length as derived from any portion of the spectrum; thus proving the 
 accuracy of the whole table. The description of the plates is as follows: 
 
TABLE OF STANDARD WAVE-LENGTHS OF THE SPECTRAL LINES 561 
 
 PHOTOGRAPHIC COINCIDENCES 
 CONCAVE, GRATING 10,000 LINES TO THE INCH 
 
 Spectra 
 
 Plate 
 
 
 
 
 
 Standard 
 
 f 
 
 1 
 
 4407 to 
 
 4643 and 
 
 3331 to 
 
 3486 
 
 f,9 
 
 it 
 
 2 
 
 4637 
 
 4890 i' 
 
 3478 
 
 3667 
 
 h >J 
 
 11 
 
 3 
 
 4823 " 
 
 5068 " 
 
 3612 
 
 3805 
 
 j, ft 
 
 tt 
 
 4 
 
 4919 " 
 
 5133 " 
 
 3683 " 
 
 3875 
 
 j, * 
 
 M 
 
 5 
 
 5050 'i 
 
 5288 " 
 
 3780 i 
 
 4005 
 
 k,l 
 
 II 
 
 6 
 
 5097 " 
 
 5333 " 
 
 3821 " 
 
 4157 
 
 ft, I 
 
 it 
 
 7 
 
 
 
 
 
 
 it 
 
 8 
 
 5242 1 1 
 
 5477 " 
 
 3937 " 
 
 4121 
 
 Z, m 
 
 tt 
 
 9 
 
 5405 " 
 
 5662 'i 
 
 4073 " 
 
 4222 
 
 m, n, e 
 
 ll 
 
 10 
 
 5582 'i 
 
 5816 
 
 4293 
 
 4376 
 
 n,f 
 
 It 
 
 11 
 
 5782 
 
 5934 " 
 
 4343 " 
 
 4447 
 
 >f 
 
 II 
 
 12 
 
 4157 " 
 
 4267 " 
 
 3129 " 
 
 3218 
 
 e 
 
 II 
 
 13 
 
 4157 " 
 
 4325 " 
 
 3094 " 
 
 3246 
 
 e 
 
 ll 
 
 14 
 
 
 
 3218 " 
 
 3318 
 
 
 ll 
 
 15 
 
 4391 i' 
 
 4643 'i 
 
 3292 " 
 
 3478 
 
 f,ff 
 
 i 
 
 16 
 
 5788 
 
 5977 " 
 
 3864 " 
 
 3977 
 
 
 
 
 17 
 
 5788 
 
 5977 " 
 
 3864 " 
 
 3984 
 
 o 
 
 ll 
 
 18 
 
 5715 " 
 
 5977 
 
 3875 " 
 
 3977 
 
 
 
 ll 
 
 19 
 
 
 
 
 
 
 20 
 
 5853 
 
 6569 
 
 3024 " 3267 
 
 Plates 7, 14 and 19 were imperfect, owing to clouds passing over the 
 sun, although a part (3218 to 3318) of Plate 14 was used for interpola- 
 tion, as observations were scanty in that region. 
 
 It is seen that some of the plates have only one standard upon them. 
 With a plane grating it would be impossible to work them up, but with 
 the normal spectrum produced by the concave grating only one is 
 necessary, as the multiplier to reduce readings to wave-lengths is nearly 
 a constant. In working up a whole series of plates, there is no trouble 
 in giving a proper value to the constant for any plate in the series 
 which has only one standard. 
 
 Plate 17 was measured twice by two dividing engines, and as it was 
 a specially good plate, each measure was given a weight equal to one 
 of the other plates. The principal error to be feared in these plates is 
 a displacement of the instrument between the time of the exposure on 
 the two spectra. This was guarded against by the method above de- 
 scribed. In Plates 17 and 20 there was a portion of the plate on which 
 both the spectra fell all the time, and thus gave a test of the displace- 
 ment. This was found to be zero. The other plates overlap so much 
 that there are generally two or more determinations of each line. A 
 36 
 
562 HEXRY A. EOWLAXD 
 
 comparison of these values shows little or no systematic variation in the 
 different plates exceeding ^ division of Angstrom. Plates 16, 17, 18, 
 and 5, 6, 8, all give the region 3900 as derived from 5200 and 5850, and 
 thus give a test of the relative accuracy of these latter regions. It is 
 seen that the two results of the region 3900 differ by about -015 division 
 of Angstrom. Were the wave-lengths of the region 5170 to 5270 to be 
 increased by -020 the discrepancy would cease. The amount of this 
 quantity seems rather large to be accounted for by any displacement of 
 the spectra on the plates, but still this may be the cause. Again, it is 
 possible that different gratings may give this difference of wave-length 
 from the cause I have mentioned above. This cause, as I have shown, 
 exists in the same degree in plane gratings as in concave. I have not 
 attempted to correct it in this case, but have simply taken the mean of 
 the two values for the region 3900, and so distributed the error. This 
 is the greatest discrepancy I have found in the results except in the 
 extreme red. 
 
 Thus the region 3100 to 3200, a portion for which Plate 20 is to be 
 relied upon, gives the wave-length of the ultra violet -01 division of 
 Angstrom higher from the region 4200 than from 6300. As the dis- 
 crepancies in this region before the invention of the concave grating were 
 often a whole division of Angstrom, I have regarded this result as satis- 
 factory. Indeed, until we are able to make all sorts of corrections due 
 to the change in the index of refraction of the air with the Barometer 
 and thermometer, it seems to me useless to attempt further accuracy. 
 
 With the advent of photographic plates into the table, especially the 
 longer ones required for metallic spectra, it becomes necessary to cor- 
 rect them for the departure from the normal spectrum due to the use 
 of long plates. The plates in the box are bent to the arc of a circle of 
 radius r. When afterwards straightened we measure the distance by a 
 linear dividing engine. Hence, what we measure is the arc with radius r. 
 Let and ft be the angles of incidence and diffraction from the grating. 
 We have then to express ft in terms of d. Let X be the wave-length, 
 and n and N the number of lines on the grating to 1 mm. and the order 
 of the spectrum respectively. Then 
 
 A = T7 (sin a + sin /? ) ; 
 
 nN 
 
 %r <5 / 
 
 sin j3 = - Tr sin cos [r + p ~ 
 H A \ 
 
 In these formula? a is the angle to the centre of the photographic 
 plate, and ft and d are also measured from the centre, f is the angle 
 
TABLE OF STANDARD WAVE-LENGTHS OF THE SPECTRAL LINES 563 
 
 between the radius from the centre of the photographic plate and the 
 line drawn from that point to the centre of the grating. When prop- 
 erly adjusted, f will be zero. Also, we make 2 r = R, to obtain perfect 
 focus throughout. So that 
 
 / = ^ (sin 4- sin -g-j . 
 
 nN\ 2 / 
 
 Calling ^ O the wave-length at the centre of the plate, we have ap- 
 proximately 
 
 * 
 
 The first quantity, - , is the value of / ^ , assuming the spectrum to 
 
 ^ ?l jLJ 
 
 be normal. The last term is the required correction expressed in terms 
 of the provisional wave-length. The correction in actual practice has 
 been made from a plot of the correction on a large scale, and never 
 amounted to more than a few hundredths of a division of Angstrom, even 
 for the longest plate. 
 
 In two or three plates the camera was displaced, so that 7- had a value. 
 In such cases no attempt was made to measure f , but the plates were 
 only used for local interpolation by drawing a curve through certain 
 points used as substandards. 
 
 These substandards Mere principally used for working up the last 
 set of photographic plates containing the solar spectrum and the metal 
 spectra of the same or higher orders, or both. Some of them contained 
 three metallic spectra. 
 
 Thus the region 3900 in the solar spectrum has been obtained from 
 both wave-lengths 5200 and 5850. The mean of these gave values of 
 the substandards for working up the plates taken at this point, and 
 containing also metallic lines at 2700. 
 
 Again, the boron lines 2496 and 2497 have been obtained from the 
 regions 4800, 3200 and 3600. The mean values give substandards for 
 working up the metallic spectra of that region. Also the near coinci- 
 dence in the values of the wave-lengths of these lines indicate the rela- 
 tive accuracy of the regions 2496, 3200, 3600, and 4800. 
 
 The use of these substandards is as follows: The photographic plates, 
 mostly 19 inches long, were measured mostly on a machine giving wave- 
 lengths direct. The differences of the results from the substandards 
 were then plotted on a paper having the curve of correction for length 
 upon it in such a way that the final marks should theoretically be a 
 straight line. This was actually the case in all but a few plates, in 
 
564 HENKY A. ROWLAND 
 
 which the camera was displaced. A straight line was then passed through 
 all the marks as nearly as may be, and the correction taken off. This 
 correction could thus be obtained to T^TF division of Angstrom, and 
 amounted to only a few hundredths of a division at most. Possibly T 1 - 
 division of Angstrom was the greatest correction required for length. 
 
 In this way each plate represents the average of all the wave-length 
 determinations throughout its extent, and will not admit of any correc- 
 tion save a linear one, should such ever be required in working over the 
 table again. 
 
 In every plate having a solar and metallic spectrum upon it, there is 
 often indeed always a slight displacement. This is due either to 
 some slight displacement of the apparatus in changing from one spectrum 
 to the other, or to the fact that the solar and the electric light pass 
 through the slit and fall on the grating differently. In all cases an at- 
 tempt was made to eliminate it by exposing on the solar spectrum, both 
 before and after the axe, but there still remained a displacement of 
 TTTF to yf-g- division of Angstrom, which was determined and corrected 
 for by measuring the difference between the metallic and coinciding solar 
 lines, selecting a great number of them, if possible. 
 
 The changes from sun to arc light are much more extensive than from 
 one order of solar spectrum to another. In two cases I have tested the 
 latter and found no displacement, and have no fear that it exists in 
 the others. 
 
 In working up the plates, I have started at the plates whose centre is 
 at wave-length 4600, and proceeded either way from that point. For 
 this purpose I have used the plates originally obtained for metallic 
 spectra, generally using the lines due to the impurities. The method, 
 I believe, is obvious from the table. For a long region no substandard^ 
 are necessary, but are used whenever they become so. 
 
 [The tables are omitted.! 
 
52 
 
 THE SEPAKATION OF THE EAEE EAETHS 
 
 [Johns Hopkins University Circulars, No. 112, pp. 73, 74, 1894] 
 
 In the course of several years' investigations of the so-called " rare 
 earths," such as yttrium, erbium, holmium, cerium, etc., I have devised 
 several methods for their separation. I wish to give an account of these 
 now, and hope soon to be able to publish a complete description of my 
 work and its results. 
 
 It was evident very early in the work that cerium, lanthanium, praseo- 
 dymium, neodymium and thorium differed from the yttrium group, and 
 I have seen no reason to suppose that they can be divided any further. 
 All of these "earths" appear, in varying proportions, in such minerals as 
 gadolinite, samarskite, yttrialite, cerite, etc. Besides the elements of 
 the cerium group here present there are at least seven other substances. 
 For the present I shall speak of them as 
 
 a, 6, i, d, h, n, c, fc. 
 Their properties are as follows: 
 
 PKOPEBTIES OF ELEMENTS 
 
 Substance a 
 
 This is the principal element of yttrium and may possibly be divided 
 into two in the future, as I have observed a variation in the arc spec- 
 trum on adding potash or soda. However, this is no more evidence than 
 occurs in the case of iron or zirconium. I give a process below for pro- 
 ducing this pure. 
 
 Properties. No absorption bands. Oxalate and oxide pure white. 
 It occurs in the sun. Its properties are those of yttrium as hitherto ob- 
 tained, but I am the first to obtain it with any approach to purity. 
 
 Mixture of I, i and d 
 
 These seem to be the principal ingredients in so-called "erbium." 
 Oxalate is red. Oxide is pure white. Absorption band is that of 
 "erbium." It colors the electric arc green, and shows the "erbium" 
 emission bands on heating white hot. The substance b is strong in gado- 
 
566 HENRY A. EOWLAISTD 
 
 Unite and weak in samarskite. The solution has the absorption bands 
 of " erbium " and most of these seem to belong to & rather than i. How- 
 ever, we can readily prove that the absorption bands of erbium belong 
 to two substances, as we can produce a decided variation in it. 
 
 I cannot reconcile this with my spectrum work without assuming a 
 fourth ingredient in " erbium." 
 
 Substance & is in the sun, but not i. With 6 and i the substance d 
 always occurs. 
 
 Substance d 
 
 This is the principal impurity of a sample of yttrium, kindly furnished 
 me by Dr. Kriiss, which my process of making yttrium separates out. It 
 has not been obtained pure, but occurs strongly in the yellow part of 
 the oxides. It is in the sun. 
 
 By aid of ferrocyanide of potassium the substance a can be obtained 
 pure from d. With this exception d occurs in all the preparations of 
 the yttrium group and cannot be separated from &, i, c, n, h, or any 
 of the other substances. Indeed, I have found it in some specimens of 
 cerium and lanthanium, although in traces only. 
 
 On account of the trouble caused by it and its universal presence, I 
 propose the name demonium for it. 
 
 Its principal spectrum line is at w. 1. 4000-6 nearly. 
 
 Substance h 
 
 This occurs mainly in samarskite. Hints toward its separation will 
 be given below, but I have otherwise obtained none of its properties. 
 
 Substances n, Ic and c 
 
 These always occur with d and form a group intermediate between the 
 yttrium and cerium groups. They can be separated from these by sul- 
 phate of potassium or sodium by always taking in intermediate portions 
 of the precipitate. They seem to have a weak absorption spectrum in 
 the visible spectrum and strong in the ultra violet, especially If. 
 
 Chemical Separation 
 
 The first process that suggests itself is that by the sulphates of soda 
 or potash. This is the usual method for separating the cerium from 
 the yttrium groups. When the solution of earth and the sulphate 
 solution are both hot and concentrated, everything except some scan- 
 dium comes down. When done in the cold with weaker solutions, there 
 is more or less complete separation of the cerium group. Let the mixed 
 
THE SEPARATION OF THE RARE EARTHS 567 
 
 earths be dissolved in a very slight excess of nitric acid and diluted some- 
 what (possibly 1 k. to 2 or 3 litres). Place in a warm place, add lumps 
 of sulphate of soda, and stir until no more will dissolve. Continue to 
 add and stir for a day or two until the absorption lines of neodymium 
 disappear from the solution. Filter off and call the solution No. 1. 
 Add caustic potash to the precipitated sulphates and wash so as to leave 
 the oxides once more. Dissolve in nitric acid and precipitate again with 
 sulphate of soda, calling the nitrate No. 2. Proceed in this way pos- 
 sibly 10 or more times. The nitrates contain less and less earths; and 
 the precipitate is more and more the pure cerium group; but a dozen 
 precipitations still leave some impurity. 
 
 The portions 1, 2, 3, etc., show decreasing "erbium" absorption bands, 
 and the spectrum shows that the substances a, 6, d, i are gradually sepa- 
 rated out with parts 1, 2, etc., while the numerous fine lines belonging to 
 d, n, c, etc., with the cerium group, fill the spectrum of the portions 
 8, 9, 10, etc. This intermediate group has only very weak absorption 
 bands and evidently has three or four elements in it, as I have produced 
 at least that number of variations in its spectrum. The group can be 
 obtained fairly free from , 5, and i, but the substance d persists in all 
 the filtrates and in the precipitated cerium group also. This interme- 
 diate group d, n, etc., seems to be in greater proportion in samarskite 
 than in gadolinite, and there seem to be more elements in samarskite 
 than in gadolinite. One of these I have called li. 
 
 The oxides, especially for samarskite, are very yellow and dark. 
 
 Sulphate of potash has a decided action in separating a and i from 6, 
 a and i coming down first. After two months, the solution gradually 
 drying, the proportion of & to a in the filtrate increased many times. 
 Sulphate of soda has an action of the same kind, but much weaker. 
 After leaving two months over sulphate of potash and soda, the follow- 
 ing was the result of analysis of the soluble part as compared with the 
 original mixture: 
 
 Sulphate of Potash. Sulphate of Soda. 
 
 Ge., La., etc. o o 
 
 a Weak Medium weak 
 
 b Much stronger Stronger 
 
 c oo 
 
 d Unchanged Unchanged 
 
 t Weaker Medium strong 
 
 o Stronger Weaker 
 
 The oxide of the members of this group which are only slightly pre- 
 cipitated by the sulphates of soda and potash is pure snow-white, and 
 hence those of & and i must be so. 
 
568 HENRY A. KOWLAND 
 
 The substance d comes down slightly sooner than a by sulphate of 
 soda, but slightly slower by sulphate of potash. Hence, in purifying 
 yttrium (substance a) for the last time from the ce. group, sulphate of 
 potash will increase d in the filtrate and sulphate of soda will decrease it. 
 
 Action of oxalic acid 
 
 When the oxalates of the mixed earths, free from the ce. group, are 
 boiled in water to which nitric acid is added, they are more or less dis- 
 solved, leaving a coarse, heavy, red oxalate yielding a pale yellow oxide. 
 The nitrate, set aside to cool, deposits more of the oxalates and leaves a 
 filtrate which contains several of the unknown elements, as also what re- 
 mains of the ce. group. On separating the ce. group the remainder is 
 quite different from the heavy red oxalate, but there is far from complete 
 separation. The analysis showed the following: 
 
 a, &, c, d, li, i, n. 
 
 I have not found the separation particularly useful, and it seems to be 
 more apparent than real as tested by the spectroscope. 
 
 Ferrocyanide of potassium 
 
 This is the most useful process and easily separates the element a, 
 pure and free from all others. To obtain pure a from the mineral gado- 
 linite, Fergusonite or Samarskite: 
 
 First obtain the crude mixed earths in the usual manner. Then sepa- 
 rate the cerium group as usual until the absorption bands of neodymium 
 no longer appear. For the complete separation without loss this must 
 be done several times, as much of the yttrium group is carried down 
 with the first precipitate, as we have before seen. 
 
 The separation of the yttrium (a) from the other elements is effected 
 by precipitating the latter from a weak acid solution by ferrocyanide of 
 potassium. For this purpose the filtrate, after separating the cerium 
 group, can be used at once by slightly acidulating with nitric acid, dilut- 
 ing and adding a weak solution of ferrocyanide of potassium. No pre- 
 cipitate should appear at once, but by standing for an hour or so some 
 will come down. Add more ferrocyanide of potassium and repeat until 
 the filtrate no longer shows the bands of so-called erbium. After this 
 it is best to precipitate with oxalic acid or oxalate of potassium and 
 ignite the precipitate so as to get the earth. Dissolve this in nitric acid 
 and add only water enough to make a very concentrated syrupy solution. 
 
THE SEPARATION OF THE RARE EARTHS 569 
 
 Place in a beaker at least three inches in diameter and examine with a 
 spectroscope of low power for absorption bands. Probably the bands of 
 neodymium and " erbium " will appear. Separate the first by sulphate 
 of sodium as usual, and the last by ferrocyanide of potassium from an 
 acid solution as above. The filtrate will then contain the pure yttrium 
 a, whose calcined oxalate will be pure white without trace of yellow. 
 After separation of iron, calcium, and possibly manganese, the earth will 
 be a pure element as far as I can tell spectroscopically. However, like 
 Zr, Fe and many other substances, the addition of Na or K to the elec- 
 tric arc while obtaining the spectrum will change the intensity of cer- 
 tain lines of the spectrum, while others are unchanged. If this is con- 
 sidered as evidence of the existence of two elements, then the same evi- 
 dence will apply to Fe and Zr. The reason for believing that the sub- 
 stance thus found is an element is based on the fact that its spectrum 
 remains unaltered in all minerals and after all chemical operations that 
 I have been able to devise. Furthermore, I believe that the new pro- 
 cess is not only more easy than any other, but also that it has given a 
 single element for the first time, as it eliminates the element d. The 
 yield will of course depend on the amount of purity required. From the 
 earths of gadolinite about one-tenth of quite pure yttrium (a) can be ob- 
 tained and about one-twentieth of very pure. 
 
 I have determined spectroscopically that when, by the above process, 
 the absorption band of "erbium" at last disappears from 3 in. of strong 
 solution, all the other elements have also disappeared. 
 
 By taking the first precipitate several times by ferrocyanide of potas- 
 sium from an acid solution, a mixture of many elements is obtained 
 which contains much of that element to which the so-called "erbium" 
 band is due. By dissolving a weighed quantity of this mixture in nitric 
 acid and water and examining the band spectrum, I have determined the 
 limit when the band can no longer be seen. Thus I have proved that 
 when the band vanishes from 3 inches of concentrated syrupy solution 
 of yttrium there cannot exist in it more than -| per cent of the mixed 
 element as compared with the yttrium, and there is probably less. 
 
 I have not found ferrocyanide of potassium useful in the further 
 separation of the elements, but only in separating out a from the others. 
 
 When the neodymium band has disappeared by use of sulphate of 
 sodium, all the other elements of the cerium group have disappeared. 
 The element thorium is sometimes present in the crude earths, but dis- 
 appears after a while from the purified earths. The conditions for its 
 disappearance I have not determined. 
 
570 HENRY A. ROWLAND 
 
 The elements which persist to the last by the ferrocyanide process are 
 & and i, while by Kriiss' process the element d persists the longest. As 
 & -J- i has an absorption spectrum and d probably not, the test of purity 
 by absorption bands is very complete in the new process. 
 
 Note. For help in this investigation my thanks are due to a large number of gen- 
 tlemen. Professor Schapleigh has sent me a large collection of substances, Mr. 
 Hidden, Professor Wolcott Gibbs, and Professor F. W. Clarke many minerals, Profes- 
 sor Kriiss several specimens, and Professor Barker and others have helped me in 
 many ways. 
 
57 
 
 NOTES OF OBSERVATION ON THE RONTGEN RAYS 
 
 BY HENRY A. ROWLAND, N. R. CARMICIIAEL, AND L. J. BRIGGS 
 
 [American Journal of Science [4], /, 247, 248, 1896 ; Philosophical Magazine |5], XLI, 
 
 381, 382, 1896] 
 
 The discovery of Hertz some years since that the cathode rays pene- 
 trated some opaque bodies like aluminium, has opened up a wonderful 
 field of research, which has now culminated in the discovery by Rontgen 
 of still other rays having even more remarkable properties. We have 
 confirmed, in many respects, the researches of the latter on these rays, 
 and have, repeated his experiment in photographing through wood, 
 aluminium, cardboard, hard rubber, and even the larger part of a milli- 
 meter of sheet copper. 
 
 Some of these photographs have been indistinct, indicating a source 
 of these rays of considerable extent, while others have been so sharp 
 and clear cut that the shadow of a coin at the distance of 2 cm. from 
 the photographic plate has no penumbra whatever, but appears perfectly 
 sharp even with a low power miscroscope. 
 
 So far as yet observed the rays proceed in straight lines and all efforts 
 to deflect them by a strong magnet either within or without the tube 
 have failed. Likewise prisms of wood and vulcanite have no action 
 whatever so far as seen, and, contrary to Rontgen, no trace of reflection 
 from a steel mirror at a large angle of incidence could be observed. In 
 this latter experiment the mirror was on the side of the photographic 
 plate next to the source of the rays, and not behind it, as in Rontgen's 
 method. 
 
 We have, in the short time we have been at work, principally devoted 
 ourselves to finding the source of the rays. For this purpose one of 
 our tubes made for showing that electricity will not pass through a 
 vacuum was found to give remarkable results. This tube had the 
 aluminium poles within 1 mm. of each other and had such a perfect 
 vacuum that sparks generally preferred 10 cm. in air to passage through 
 the tube. By using potential enough, however, the discharge from an 
 ordinary Ruhmkorff coil could be forced through. The resistance being 
 
572 HENEY A. ROWLAND 
 
 so high the discharge was not oscillatory as in ordinary tubes but only 
 went in one direction. 
 
 In this tube we demonstrated conclusively that the main source of 
 the rays was a minute point on the anode nearest to the cathode. At 
 times a minute point of light appeared at this point, but not always. 
 
 Added to this source the whole of the anode gave out a few rays. 
 From the cathode no rays whatever came, neither were there any from 
 the glass of the tube where the cathode rays struck it as Rontgen 
 thought. This tube as a source of rays far exceeded all our other collec- 
 tion of Crookes' tubes and gave the plate a full exposure at 5 or 10 cm. 
 in about 5 or 10 minutes with a slow-acting coil giving only about 4 
 sparks per second. 
 
 The next most satisfactory tube had aluminium poles with ends about 
 3 cm. apart. It was not straight, but had three bulbs, the poles being in 
 the end bulbs and the passage between them being rather wide. In this 
 case the discharge was slightly oscillatory, but more electricity went one 
 way than the other. Here the source of rays was two points in the tube, 
 a little on the cathode side of the narrow parts. 
 
 In the other tubes there seemed to be diffuse sources, probably due 
 in part to the oscillatory discharge, but in no case did the cathode rays 
 seem to have anything to do with the Rontgen rays. Judging from the 
 first two most definite tubes the source of the rays seems to be more 
 connected with the anode than the cathode, and in both of the tubes the 
 rays came from where the discharge from the anode expanded itself to- 
 ward the cathode, if we may roughly use such language. 
 
 As to what these rays are it is too early to even guess. That they and 
 the cathode rays are destined to give us a far deeper insight into nature 
 nobody can doubt. 
 
 Baltimore, Feb. 20, 1896. 
 
58 
 NOTES ON RONTGEN KAYS 
 
 BY H. A. ROWLAND, N. R. CARMICHAEL, AND L. J. BRIGGS 
 [Electrical World, XXVII, 452, 1896] 
 
 In the ' American Journal of Science ' for March we made a few notes 
 of our researches on the Rb'ntgen rays, reaching the provisional con- 
 clusion that the main source of the rays was at the anode, and that the 
 cathode rays seemed to have nothing to do with the phenomena pre- 
 sented. A further study of the source of the rays in many other tubes 
 has led us to modify this conclusion somewhat, for, while we still think 
 the anode or its equivalent is the main source of the rays, yet we now 
 have evidence in some of the tubes that it is necessary for the cathode 
 rays to fall on the anode in order that the Rontgen rays may be formed. 
 
 In our tubes with a very high vacuum the other sources of rays are 
 very faint indeed. We have never obtained any rays from the cathode 
 except in one case, where undoubtedly there were electrical oscillations 
 which made the cathode momentarily an anode. It can be readily proved 
 that these oscillations always exist in the case of low resistance tubes, 
 and these are probably the cause of many errors in estimating the 
 source of the rays. 
 
 In some cases we have found very faint sources of rays as Rontgen 
 found them, where the cathode rays struck the glass, but not where they 
 struck a piece of platinum kept at nearly zero potential. On the anode 
 theory, this might be explained by the fact that the bombarding cathode 
 rays, coming in periodical electrified showers, alternately raise and 
 lower the potential of the glass, thus making it alternately an anode and 
 cathode. In the case of the platinum, this could not occur to the same 
 extent. 
 
 That feeble Rontgen rays emanate from some bodies when bombarded 
 by the cathode rays, we are willing to admit, and, in fact, had long ago 
 come to that conclusion. But we do not agree with Prof. Elihu Thom- 
 son's general conclusion that these rays are always given out from bom- 
 barded surfaces, as we have a tube, with platinum in the focus of a con- 
 cave electrode, which emits no rays whatever from the platinum, even 
 
574 HENRY A. Rovv LAND 
 
 when the platinum is red hot from the bombardment, the concave elec- 
 trode being the cathode and a third wire the anode. 
 
 The same tube, with the platinum made an anode and the concave 
 electrode a cathode, produces a profuse radiation of Rontgen rays in all 
 directions on the side of the platinum bombarded by the cathode rays, 
 and none on the other side. In the first case we obtained no rays from 
 the cathode, no rays from the bombarded surface, and only a very weak 
 effect from the anode, indeed almost nothing. Hence the condition 
 for the production of the rays seems to be neither the one or the other 
 but a combination of the two, and we now believe as far as we can yet 
 see that the necessary condition for their production is an anode bom- 
 barded by the cathode discharge. The anode may be, however, an in- 
 duced anode formed on the glass, and the cathode rays may vary a great 
 deal and cease to present the usual appearance of cathode rays. 
 
 Thus, in the best tube that we have, originally made for showing that 
 electricity will not pass through a vacuum, the main source is a point on 
 the end of the anode, where a little point of light appears. Sometimes, 
 across the little interval of 1 mm. between the electrodes, a faint spark 
 or arc crosses from one electrode to the other, and we think that the 
 rays come out especially well under these conditions. Here the action of 
 the bombarding cathode discharge is rather obscure. This little point of 
 light also sometimes appears on the red hot platinum anode men- 
 tioned above, and we have seen it in other tubes, always at the place 
 where Rontgen rays are apparently found. 
 
 Prof. Elihu Thomson has kindly sent us some sketches of tubes hav- 
 ing the anode bombarded by the cathode, and we had previously de- 
 signed some tubes of similar shape, but have not yet found anybody 
 in this country capable of making a sufficiently good vacuum. In many 
 of our best tubes the vacuum is so perfect as to cause a resistance equal 
 to a five or six inch spark in the air. The better the vacuum the 
 greater the number of rays sent out. 
 
 However, for sharpness of detail, nothing equals the perfect vacuum 
 tube, having its electrodes one mm. apart. Such a tube has been de- 
 signed by one of us, but we have not been able to get the proper 
 exhaustion. 
 
 As to other sources of Rontgen rays, we have tried a torrent of elec- 
 tric sparks in air, from a large battery, and have obtained none. Of 
 course, coins laid on or near the plate under these circumstances, pro- 
 duce impressions, but these are, of course, induction phenomena. 
 
 As to sunlight, Tyndall, Abney, Graham Bell and others, have 
 
NOTES ox KONTGEN KAYS 575 
 
 shown that some of the rays penetrate vulcanite and other opaque 
 bodies, and we have only to look at an unpainted door, on the other 
 side of which the sun is shining, to convince ourselves that sunlight 
 penetrates wood to a considerable depth. 
 
 As to the theory of the Eontgen rays we know little. If the rays 
 are vibrations we can readily determine a rough limit to their length, 
 from the sharpness of the shadows. 
 
 Thus our photographs have such sharpness that the complete waves 
 cannot be more than -0005 cm. long, but are probably much shorter. 
 This is independent of whether the waves are longitudinal like sound 
 or transverse like light, and of course only applies to that portion of 
 them which affects the photographic plate. There may be others of 
 larger size that do not affect the plate. 
 
 All efforts to bend the rays from their course, either within or with- 
 out the tube, by means of a strong magnetic field, have failed, both in 
 our hands and in those of others, and thus, if the rays are radiant parti- 
 cles of matter, they cannot be highly charged particles like the cathode 
 rays. The rays are not refracted by any solid bodies so far tried, and 
 this seems to be against their being waves either in air or ether. They 
 pass through solid bodies, and thus their wave-lengths cannot be very 
 small. We have before seen that it cannot be very great. They cannot 
 be sound waves as they proceed for some distance through a very perfect 
 vacuum. 
 
 Altogether we are at a loss for a theory. If we have not yet got a 
 satisfactory theory of light after more than a hundred years of labor, 
 how can we hope to have a theory of the Kontgen rays after knowing 
 of them for only a few months? Let us suspend our judgment for a 
 while, and let us, above all things, be willing to alter our opinions at 
 any moment when fresh light appears. 
 
59 
 
 THE RONTGEN RAY, AND ITS RELATION TO PHYSICS 
 
 (A TOPICAL DISCUSSION) 
 
 [Transactions of the American Institute of Electrical Engineers, XIII, 
 403-410, 430, 431, 1896] 
 
 OPENING REMABKS BY PROF. HENRY A. ROWLAND 
 
 MR. PRESIDENT AND GENTLEMEN: A gentleman asked me a few mo- 
 ments ago if I knew anything about the X-ray. I told him no; that what 
 I was going to tell to-night was what I did not know about the X-ray. 
 I do not suppose anybody can do any more than that, because all of us 
 know very little about it. We were very much surprised, something 
 like a year ago, by this very great discovery. But I cannot say that we 
 know very much more about it now than we did then. The whole 
 world seems to have been working on it for all this time without having 
 discovered very much more with respect to it. 
 
 Now, I suppose it is not necessary for me to go into the history of 
 the thing. We all know it; how Lenard first, probably, discovered these 
 rays, or discovered something very similar to them; how Rontgen after- 
 wards found their particular use, their penetrating power, and so on, 
 although Lenard had found something similar to that before. It is 
 thus not necessary for me to go into the history of the matter, but 
 simply to go over, to some extent, what we know with regard to these 
 rays at the present time. First, there was some discussion, some time 
 ago, as to the source of these rays. Rontgen found that their source 
 was any point that, the cathode rays struck upon; and you will remember 
 that when we first knew about these rays they were often called cathode 
 rays. Many persons thought that the cathode rays came through the 
 glass, and Lenard first thought that they did come through his little 
 window, and it is probable that they do at the present time. But the 
 kind of rays that we are considering are very different from the cathode 
 rays. Six months ago there was quite a discussion in regard to the 
 source, and I believe it was finally determined that they came from 
 points where the cathode rays strike. At the same time I was rather 
 opposed to that. In one of my tubes I found that the rays came from 
 
THE RONTGEN RAY AND ITS RELATION TO PHYSICS 577 
 
 the anode. I had only the ordinary assortment of Crookes' tubes, and 
 one of the tubes had aluminum wires which were a millimeter apart. 
 In one of these the source of the rays was a point upon the anode 
 not upon the cathode at all. It was a very small point. The photo- 
 graphs which I obtained by that tube were sharper than any I had seen 
 before. They are so very sharp that in estimating the shadow of an 
 object I determined that the point could not have been a thousandth 
 of an inch in diameter. Therefore the source in this case was a very 
 minute point upon the anode, and that point was nearer the cathode, 
 and I suppose some of the cathode rays might have struck upon it, and 
 it might have obeyed the law that the point where these X-rays are 
 formed is the point on the anode where the cathode rays strike. 
 
 I had another very interesting tube, and I was going to bring some 
 of the photographs here to-night; but I thought they were so small that 
 it would be almost impossible to see them. I tried the three cases in 
 this tube: First, the case where the cathode rays strike upon the anode. 
 In that case I got very many Rontgen rays. Then I tried the case 
 where the cathode rays strike upon an object a piece of platinum. I 
 did not get any rays whatever then. Now, some people say that they 
 come from the point where the cathode ray strikes. I did not get any 
 whatever in that case. In this case the cathode ray struck upon a piece 
 of platinum in the centre of a bulb, and no rays were given out by the 
 anode either. Therefore I seemed to have a crucial experiment in each; 
 I seemed to have the case where the cathode ray strikes upon the anode, 
 and I got lots of rays. Then I had the case where the cathode rays 
 strike on a piece of platinum, and I did not get anything at all. Then 
 where the anode itself was free and no cathode rays struck it, I did not 
 get anything from it. It seemed to me as if the source was most abun- 
 dant when the cathode ray struck upon the anode; and that is the 
 theory, we know, upon which nearly all tubes are formed at the present 
 time. You have the focus tubes in which you focus the cathode rays 
 upon the anode, and in that case you have a very abundant source of 
 rays; but I do not believe you ever could get as small a source of rays 
 as I got with that first tube, where I had a source of a thousandth of an 
 inch diameter. Having such a small source of rays, it gave me a limit 
 to the wave-length, if there were waves at all; it would give me a limit 
 to the wave-length of which I will speak in a moment. As to whether 
 there are any rays where the cathode rays strike on any other objects, 
 we know that there are very feeble ones. It seems to be almost neces- 
 sary in order to get an abundant source that you should have cathode 
 37 
 
578 HENRY A. EOWLAND 
 
 rays strike on the anode. However, that is a point of discussion. Now, 
 as to the source of electricity, we have generally the Euhmkorff coil. 
 There is one source of which I saw a little note in ( Nature,' where a 
 man had used a large Holtz machine with very good effects. Now it is 
 very much easier for many persons to use a Holtz machine than to use 
 a Euhmkorff coil. There are many cases where one cannot have a large 
 battery; and this man said that with the Holtz machine he got as great 
 an effect as with the Euhmkorff coil. Then we have the Tesla coil, etc. 
 By the way, speaking of the Tesla coil, I am not sure but that you 
 might look back and find that it is very similar to the Henry coil. 
 Henry originally experimented on the induction of electricity, transmit- 
 ting a spark of electricity from one coil and getting a spark from an- 
 other, and the Tesla coil is something like that, except that it is made 
 so as to produce a much more voluminous spark. 
 
 We all know the properties of the Eontgen rays they go in a straight 
 line. Every effort to deviate them from a straight line, by any means 
 whatever, has failed, except that when they strike upon an object they 
 are reflected. Now, it is a question for discussion as to whether there is 
 any regular reflection. They strike upon an object, and you get some- 
 thing from that object which will affect a photographic plate. Are 
 those rays which you get from the object Eontgen rays still, or do the 
 Eontgen rays strike upon this object and generate in it some sort of 
 rays which come out, different from the Eontgen rays, and affect the 
 plate? We do not know that. Neither are we quite positive whether 
 there is any reflection of the rays. We know there is turbid reflection 
 you may call it rays strike on the object, and the object becomes a 
 source of rays of some kind. Nobody has ever found out what sort of 
 rays come from the object. Something comes from it, and we generally 
 imagine, and indeed we often state, that they are Eontgen rays that 
 come off the object. But we have good reason to suppose that they 
 may be something else; and they may or may not be regular reflections; 
 some persons say they are and some that they are not. I have seen 
 some photographs made in this city which indicated regular reflections. 
 At the same time I would not be positive as to whether there was any 
 regular reflection. It is rather doubtful. It is a point to be determined. 
 
 Then the fluorescence that is the way Eontgen originally found the 
 ray. You know the way they produce fluorescence the photographic 
 effect you all know that. You all know that the magnet does not 
 affect them does not turn these rays from a straight line. 
 
 The polarization of the rays: We have no evidence whatever as to 
 
THE RONTGEN KAY AND ITS RELATION TO PHYSICS 579 
 
 the polarization. If they were very small waves, transverse waves, like 
 light, we ought to be able to polarize them. Becquerel, by exposing 
 certain phosphorescent substances to the sun, obtained from them cer- 
 tain rays which penetrated objects like aluminium,. etc. But these rays 
 were evidently small rays of light, because he could polarize them, and 
 he could refract them, and they were probably very short waves of ultra 
 violet light. But we never have been able to discover that there was 
 any such effect in a Rontgen ray. Some persons have claimed that they 
 got polarization; but if there ever was any polarization, it is very small, 
 indeed. One of the principal advances in respect to these rays is that 
 made by J. J. Thomson, in considering the electric discharge of bodies. 
 He has published most valuable results with regard to the effect of 
 these rays upon gases. When the rays fall upon a gas, they affect the 
 gas in some way so that it becomes a conductor. Now, you can subject 
 the gas to these rays and allow the gas to go through a tube off into 
 another vessel, so that it will discharge an electrified body in that vessel. 
 But he has found the most interesting result that it will not continue 
 long to affect these bodies. After one has allowed a certain amount 
 of electricity to pass through it, it then becomes an insulator again. 
 It only allows a certain amount of electricity to go through it. That is 
 easily explained or you can explain it by the Rontgen rays liberating 
 the ions, and only a certain amount of them. Just as soon as these 
 are used up in the conduction of the gas, then it ceases to conduct. So 
 that a certain amount of gas will conduct a certain amount of electricity, 
 and then it stops conducting. That is a most interesting result. It is 
 one of the great advances we have made since Rontgen's discovery. 
 Rontgen knew nearly all we know now about these rays. We have 
 discovered very little indeed; but that point I think we have at least 
 discovered. 
 
 Then it is said that these rays affect a selenite cell in the same way 
 that light affects it it changes the resistance of the selenite cell. 
 
 Of course, we are only considering the theory to-night; at least I 
 am, and we do not have to consider the bones, and so on. I have had 
 some students at work in my laboratory, and it was with the utmost 
 difficulty that I kept them from photographing bones. Bones seemed 
 to be the principal object to be photographed by the Rontgen rays when 
 they were first discovered, and I suppose it is the same now. Most 
 people connect Rontgen rays with bones; but I do not intend to say very 
 much about them. 
 
 Now, one important point with respect to these rays is as to whether 
 
580 HENRY A. ROWLAND 
 
 they are homogeneous. Are they like light which can he divided up 
 into a large number of different wave-lengths, or are they homogeneous? 
 There seems to be a great deal of evidence that they are not all the 
 same; that one ought to get a spectrum of them in some way. We can 
 filter them a little bit through objects. After they are filtered through 
 an object, they are probably a little different from what they were 
 before, and some objects probably let through different rays from others. 
 In ' Nature ' Mr. Porter, I believe, has shown experiments upon that. He 
 divides rays into three kinds. At least he finds that under certain 
 circumstances the rays will penetrate bones better than in other cases 
 bones or any other object they have more penetrating power, and they 
 go through many of those objects that ordinarily stop them. By heat- 
 ing up the tube, and by various arrangements of his spark-gaps, etc,, 
 and putting little wires around his tubes, and so on, he can cause them 
 to generate different kinds of rays. That is a very important point, if 
 it is substantiated, and there seems to be little reason to doubt that a 
 number of rays really do exist; that whatever they are that come from 
 the object, they are not all the same; some of them penetrate bodies 
 better than others, and very likely some one will get up some sort of 
 filter that will filter them out, and allow us to use them and to find if 
 they have different properties. At the present we are rather in the 
 dark with regard to this point. 
 
 Now I come to the theory of these rays. What is the cause of all 
 these phenomena? There was a time when we were rather self- 
 satisfied, I" think, with regard to theories of light. We thought that 
 Fresnel and others had discovered what light was some sort of vibra- 
 tion in the ether; we called it ether; if it had these, waves going through 
 it, then it would produce light, and we were pretty well convinced that 
 the waves were transverse, because we would polarize them; so that we 
 began to be satisfied that we knew something about light. Then Max- 
 well was born, and he proved that these rays were electromagnetic 
 very nearly proved it. Then Hertz came along and actually showed us 
 how to experiment with these Maxwell waves, most of which were 
 longer than those of light. At the same time they were of the same 
 nature. Well, we got a rather complicated sort of ether by that time. 
 The ether had to do lots of things. One must put upon the ether all the 
 communication between bodies. For instance, what communication is 
 there between this earth and the sun? Why, you have light coming 
 from it and heat. Radiation you might call it all. We have radiation. 
 Then some people thought they discovered electromagnetic disturbance 
 
THE RONTGEN RAY AND ITS RELATION TO PHYSICS 581 
 
 from the sun. Sometimes they have seen a sun spot and noted a deflec- 
 tion of the magnetic needle on the earth. Very likely that is true. I 
 don't know that they have discovered any electrostatic effect. But we 
 know that electrostatic effects will be carried on through as perfect a 
 vacuum as you can get. Then we have gravitation action too. Now, 
 you have got all those things electromagnetic action, light which 
 would be an electromagnetic phenomenon, and then we have gravitation, 
 and we have got to load the ether with all those things. Then we have 
 got to put matter in the ether and have got to get some connection 
 between the matter and the ether. By that time one's mind is in a 
 whirl, and we give it up. 
 
 Now we have got something worse yet we have got Rontgen rays on 
 top of all that. Here is something that goes through the ether, and it 
 not only goes through the ether but shoots in a straight line right 
 through a body. Now, what sort of earthly thing can that be? A body 
 will stop light or do something to it as it goes through; but what on 
 earth can it be that goes through matter in a straight line? Why, our 
 imagination doesn't give us any chance to do anything with that pro- 
 blem. It is a most wonderful phenomenon. Now, we can suppose that 
 they are ultra violet light. Indeed, we can get a limit to the wave- 
 length to some extent. Nobody, however, has ever proved that the Ront- 
 gen rays are waves. But we can get a limit of the wave-length if they are 
 waves, because when I have a tube that gives me a shadow which is only 
 a thousandth of an inch broad, or rather from the greatest intensity 
 out to clear glass a thousandth of an inch broad, I can calculate the 
 wave-length of the thing that would produce such a shadow. It has 
 got to be very small indeed; one knows that right away, because any 
 ordinary light would make a few waves at the edge of the shadow, and 
 by measuring those waves you could get the wave-lengths of the light. 
 But there was no appearance whatever on any of my photographs of any 
 such phenomenon as that. I did not have any of these waves at the 
 edge of the shadow whatever. It went directly from blackness to light. 
 But putting it under the microscope and measuring from almost imag- 
 inary points, from lightness to darkness, I could get a limit to the wave- 
 length. Now, as to that limit, I published it in one of the journals 
 six months ago, or more, and it came at about one-seventh, I think, 
 that of yellow light. Others have determined the wave-length and got 
 even below one-seventh that of yellow light. Some have got one- 
 thirtieth that of yellow light, and so on. Some of them I am rather 
 doubtful about, because they say they have bands. If they have bands 
 
582 HENRY A. ROWLAND 
 
 and diffraction bands, that would prove instantly that the Rontgen rays 
 are waves. But I have never seen the slightest phenomenon of that 
 sort. It is very doubtful that it exists, and those persons who have had 
 it will have to show their photographs very clearly to make us believe 
 it. And therefore we have no evidence whatever that the rays are 
 waves. At the same time we have no evidence that they are not waves. 
 They might be very short waves infinitely short waves. Let us see 
 what would happen if they were infinitely short waves. They might 
 be so very short as to be too fine-grained for any of our methods of 
 polarization or reflection. Waves are reflected from a solid body 
 regularly reflected, because they interfere after they come from the 
 body. You can get the direction the angle of incidence equals the 
 angle of reflection; you can get that by means of considering them as 
 waves and as interfering after they come from the object. Well, if the 
 object, however, is a very rough sort of thing compared with the wave- 
 length, you will not get a regular reflection. That is what might hap- 
 pen in the case of Rontgen rays. And then again, with regard to 
 refraction of the light, the theory of refraction which comes from con- 
 sidering molecules imbedded in the ether will give you some limit. 
 When we go beyond that limit, we get no refraction. The bending of 
 the violet rays increases up to a certain point and then goes back. We 
 have a case of anomalous refraction very often in some substances like 
 fuchsine, aniline dyes, and so on. Therefore the action of refraction 
 can be accounted for by having very short waves. But when we treat 
 of the theory of the case we have the little molecules of a gas knocking 
 against each other, and they can only go a little distance. We call that 
 the free path of the gas a very small distance in the ordinary air. 
 Those molecules cannot go more than this very small distance before 
 they stop. Well, now, why should little, short waves of light pass 
 through the gas and not be stopped too? When the waves are very 
 short indeed, it seems to me that the object would be entirely opaque 
 to them, because they would strike upon those molecules, unless they 
 could pass directly through the molecules. You would therefore neces- 
 sarily have these little short waves going directly through the mole- 
 cules, which we generally think is almost impossible in case of light. 
 And that is one very great objection that I have to that theory. 
 
 Then we have another theory that these are not transverse waves 
 at all; that they are waves like sound, and very short indeed. Well, 
 what would happen then? If they are very short indeed, you have the 
 same objection: They would all strike against the molecules, and they 
 
THE ROXTGEN RAY AND ITS RELATION TO PHYSICS 583 
 
 would be dispersed very quickly. The shorter the wave-lengths, the 
 more they are dispersed. Take, for instance, short waves that bob 
 against a boat and are reflected back. Thus, if you have a big, long 
 ocean wave, it sweeps around a boat and goes on without being troubled 
 by the boat at all. The shorter the waves, the more they are bothered 
 by the boat, and so it is with respect to other waves the short waves 
 would probably be stopped by the molecules. So I do not see what we 
 can do with regard to it in that respect. According to Maxwell's law, 
 waves like sound do not exist in the kind of ether that he suggested. 
 But that is all based upon a certain theory that the lines of force were 
 always closed. He introduced into his equation an expression which 
 indicated that every line of force was a closed path coming back upon 
 itself or ending in electricity, one or the other. Now, if we throw out 
 that, then we can get this kind of compressional waves in the ether. 
 Now, it is not at all impossible that they exist, and as to whether they 
 would go through molecules any better than light waves do, nobody can 
 tell; but it is possible that they might. But if there are waves at all, 
 they must be very short waves. You cannot get over that fact if they 
 are waves at all, they must be short. 
 
 Then, of course, you have the other theory of little particles of 
 matter flying out from the body, passing through the glass and all other 
 bodies, until they reach a photographic plate or any other place where 
 we are notified of their presence, and these little particles make their 
 way through the air or any other substance. Now, why should not the 
 little particles be stopped very quickly by bodies as well as if the rays 
 were waves? You see we are in trouble here too. Why are not the 
 waves stopped? Why are not the little particles stopped? Stokes has 
 given some sort of a theory with regard to this that, instead of having 
 a wave motion in the ether, the rays are impulses a sudden impulse 
 one wave, for instance not a series of waves at all, but one impulse 
 coming out from the tube. I think if he had seen any very sharp 
 shadows obtained from the Rontgen rays he would not have given that 
 theory. He probably has seen only those very hazy outlines that very 
 many persons take for Rontgen photographs. But if he had seen any 
 very defined ones very sharp ones he probably would not have given 
 that theory, because if the Rontgen rays are waves at all, they must be 
 short, and there must be a long series of them to make sharp shadows. 
 This is why Newton gave up the wave theory of light. You remember 
 he gave up this theory because he found that light went straight past 
 an object instead of curving around into the shadow as much as sound 
 
584 HENRY A. ROWLAND 
 
 does. But he was not quite up to his usual pitch when he made that 
 statement, because if he had thought a moment he would have seen that 
 very short waves will go more nearly in a straight line than long ones. 
 But any single impulse, such as Stokes suggests, would go into the 
 shadow. The only wave motion that would go in a straight line is a 
 series of waves, one after another. Therefore, these rays cannot he 
 single impulses coming irregularly. 
 
 Prof. Michelson has suggested a theory of rays based on something 
 like vortex rings in the ether. Now, if we have an ether that can carry 
 on light waves and electromagnetic waves, it cannot be a perfect fluid; 
 it has got to be something else. You cannot very well imagine vortex 
 rings in such an ether. So that we are met at every point by some 
 objection. We have been studying light for hundreds of years; we are 
 not anywhere near satisfied with the theory yet, and we cannot very 
 well be expected to be satisfied with the theory of Rontgen rays in one 
 year. 
 
 Well, I think that is all I can say with regard to the subject, and I 
 hope the other gentlemen who are to carry on the discussion will satisfy 
 you on all these points that I have brought up and left unanswered. 
 
 [There followed a discussion by Professor Elihu Thomson, Professor 
 M. I. Pupin, and others.] 
 
 PROF. ROWLAND: I made a few notes with regard to what has been 
 said, but they are made in such a way that I do not believe that I can 
 interpret them myself, especially as the hour seems to be getting rather 
 late. One or two remarks, however, I would like to make. When 
 Prof. Thomson said that he got such a large amount of rays from an 
 insulated piece of platinum by letting the cathode rays fall upon it, 
 he made a sketch. With the exception of this end, which was flat, 
 that is the kind of thing that I used. Now, there was absolutely 
 no effect when this was made an anode and this a cathode, so that all 
 the cathode rays were striking on the platinum. I have the photo- 
 graph; I got no effect whatever. Now, if Prof. Thomson got an effect 
 in this case and I did not get an effect in that case, I have got a case, 
 at least, where none of these rays were produced by the falling of the 
 cathode rays upon the object. It doesn't make any difference how 
 many other persons have something in which they do get an effect. 
 If I did not get an affect, that is one case, understand. That is the 
 case where the cathode ray fell on an object and I got no Rontgen ray. 
 
THE RONTGEN RAY AND ITS RELATION TO PHYSICS 585 
 
 If other people got them in other ways, why, there is something else 
 coming in. I don't know what it is. 
 
 PROF. THOMSON: I should like to say just there, Professor, if you 
 would allow me, that I used exactly that arrangement first, and got 
 rays with the concave cathode. The anode at this end and the inter- 
 posed plate of platinum between, with that wire extending outward, 
 is the standard form of Crookes' tube the first tube, in fact, that I 
 used. I got not only sharp effects but rays. 
 
 THE CHAIRMAN: Was the platinum red? 
 
 PROF. THOMSON: The platinum was red yes, of course, and it was 
 a vigorous source of rays. I got rays with the same tube that Professor 
 Rowland does not get them. 
 
 PROF. ROWLAND: Well, that has nothing to do with the point. The 
 point that I raise is this, that there was certainly no doubt that I did 
 not get any, and the cathode rays were falling from the object. That 
 is the thing. Now, one thing that I wish to remark is that most people 
 draw a tube like that. They don't say where the wires go. Mine 
 generally went out, so that they were very far away from this object. 
 By curving wires around in different ways I can get an inductive action. 
 I don't doubt that I could fix up a tube so that I could get lots of rays 
 out of any part. However, the time is passing, and I will just say one 
 word with regard to the point Prof. Thomson raised with regard to 
 the fluorescence over the surface of the glass. He thought something 
 was stopped by the glass. I must say that Lenard, when he first experi- 
 mented upon this subject and I regard his experiments as quite as 
 valuable as Rontgen's, probably , he got several kinds of rays coming 
 out through an aluminium window. He got rays which were deflected 
 by the magnet, as well as others. He had not separated them, how- 
 ever. When the Lenard paper came to the laboratory I remarked to 
 my students: " That is the best discovery that has been made in many 
 a day." I immediately set somebody to work experimenting. He tried 
 to get some results and would probably have discovered the Rontgen 
 rays at that time if it had not been that the University of Chicago 
 called him off, and Johns Hopkins University was very poor and could 
 not call him back, and he had to stop in the midst of his work. They 
 always say in Baltimore that no man in that city should die without 
 leaving something to Johns Hopkins. Now, Dr. Pupin mentioned a 
 means of showing whether the rays were reflected a little reflector in 
 which he had them brought to a focus, as I recollect it. I have read an 
 account in which an experimenter did find the rays were brought to a 
 
586 HENRY A. EOWLAND 
 
 focus, showing, provisionally at least, that there was some regular reflec- 
 tion. But these experiments should all be repeated many times before 
 one actually believes them. We don't always believe what we read. 
 
 Now, as to Helmholtz's theory of the motion of ether and so on 
 well, as I said before, what is the motion of the ether? What is motion 
 of the whole ether? You cannot move the ether in the whole universe 
 all at once, and if you do not move the ether in the whole universe 
 all at once but only move a part, then it is a wave, so it amounts to the 
 theory that I gave an impulse, such as Stokes had. Now, an impulse 
 such as Stokes had does not go in a straight line it goes around cor- 
 ners and it does not go in. a straight line unless there are lots of 
 waves coming out. We can readily prove that an ordinary molecule, 
 vibrating to ordinary light, must give out a hundred thousand waves 
 without much diminution of amplitude, or else you cannot have the 
 sharp lines in the spectrum that we do. The molecule must vibrate a 
 long time longer than any bell that we can make. We cannot find a 
 bell that will give out a hundred thousand vibrations without much 
 diminution. For ethereal waves something must vibrate to produce 
 them. What it is I don't know that there is any necessity for discuss- 
 ing, because you can discuss it forever and never get any nearer to it. 
 Something vibrates. Now, the thing that vibrates we don't know. We 
 don't know whether it is electricity or whether it is mechanical motion. 
 We know nothing about it. I have often said to my students, when I 
 showed them the spectrum of some substance like uranium, in which 
 we were taking photographs which would be perhaps ten feet long so 
 fine in grain that you could not put the point of a pencil on it without 
 finding a line. There were thousands of lines. I said to them: " A 
 molecule of matter is more complicated a great deal than a piano. 
 Counting the overtones and everything, you would not probably get up 
 anywhere near the number of tones you get out of a single molecule of 
 uranium. Therefore it rather looks as if the uranium molecule was 
 very complicated." Of course, all those spectrum lines do not indicate 
 fundamental tones many are harmonics. Still it is rather a compli- 
 cated thing to get a spectrum in which there are many thousands of 
 lines. So when I come to think what a molecule is and try to get up 
 some theory of it, I quite agree with Dr. Pupin that we don't know any- 
 thing about it. 
 
64 
 
 DIFFRACTION GRATINGS 
 
 [Encyclopcenia Brltannica, New Volumes, III, 458, 459, 1902] 
 
 The grating is an optical instrument for the production of the spec- 
 trum ; it now generally replaces the prism in a spectroscope where large 
 dispersion is needed, or when the ultra-violet portion of the spectrum 
 is to be examined, or when the spectrum is to be photographed. The 
 transparent grating consists of a plate of glass covered with lampblack, 
 gold leaf, opaque collodion or gelatine, the coating being scratched 
 through in parallel lines ruled as nearly equidistant as possible. When 
 the lines are to be ruled very close together, a diamond ruling directly 
 on glass is used. Other transparent materials, such as fluor spar, are 
 sometimes substituted for glass. For certain researches on long waves 
 the grating is made by winding a very fine wire, l-1000th inch in diam- 
 eter, in the threads of two fine screws placed parallel to each other, 
 soldering the wire to the screws and then cutting it away on one side 
 of the screws. As the value of a grating is dependent upon the number 
 of lines ruled, it is very desirable to have their number great. Glass is 
 so hard that the diamond employed for the ruling wears away rapidly; 
 and hence the modern grating is generally a reflecting grating, which 
 is made by ruling on a speculum metal surface finely ground and pol- 
 ished. On such a surface it is possible to rule 100,000 lines without 
 damaging the diamond, although its point even then often wears away 
 or breaks down. The lines are generally so close together as 15,000 or 
 20,000 to the inch, although it is feasible to rule them even closer 
 say 40,000 to 50,000 to the inch. There is little advantage, however, 
 in the higher number and many disadvantages. 
 
 The grating produces a variety of spectra from a single source of 
 light, and these are designated as spectra of the first, second, etc., order, 
 the numbering commencing from the central or reflected image and 
 proceeding in either direction from it. The dispersion depends upon 
 the number of lines ruled in a unit of length^upon the order of the 
 spectrum, and upon the angle at which the grating is held to the source 
 of light. The defining power depends upon its width and the angles 
 
588 HENKY A. EOWLAND 
 
 made by the incident and diffracted rays, and is independent of the 
 number of lines per unit of length ruled on the grating. If this num- 
 ber is too small, however, the different order of the spectra will be too 
 much mixed up with each other for easy vision. A convenient number 
 is 15,000 to 20,000 lines to the inch, or from 6000 to 8000 to the 
 centimetre. The defining power is defined as the ratio of the wave- 
 length to the distance apart of the two spectral lines which can be just 
 seen separate in the instrument. Thus the sodium or D lines have 
 wave-lengths which differ from each other by -597 ftp, and their aver- 
 age wave-length is 589-3 pp. A spectroscope to divide them would 
 thus require a defining power of 988. The most powerful gratings have 
 defining powers from 100,000 to 200,000. Lord Eayleigh's formula for 
 the defining power is 
 
 D = Nn. 
 
 When D is the defining power, N is the order of the spectrum, and n 
 is the total number of lines ruled on the grating. As the defining 
 power increases with N, and since we can observe in a higher order as 
 the number of lines ruled in a unit of length decreases, it is best to 
 express the defining power in terms of the width of the grating, w. In 
 this case we have for the maximum defining power D' = 20,000 w for 
 small gratings, or D' = 15,000 w for extra fine large gratings, w being 
 the width of the gratings in centimetres. It is seldom that very large 
 gratings are perfect enough to have a defining power of more than 
 10,000 w, owing to imperfection of surface or ruling. The relative 
 brightness of the different orders of spectra depend upon the shape of 
 the groove as ruled by the diamond. No two gratings are ever alike 
 in this respect, but exhibit an infinite variety of distributions of bright- 
 ness. Copies of glass gratings can be made by photography, contact 
 prints being taken on collodiochloride of silver or other dry plates. 
 Eeflecting gratings can be copied by pouring collodion or gelatine over 
 the grating and stripping off the films thus formed. The latter warps, 
 however, and destroys the definition to a great extent. The grating 
 always produces a brighter spectrum in the violet than a prism. In 
 the green the reflecting speculum metal grating may be brighter than 
 a prism spectroscope of five prisms, and for higher dispersion surpasses 
 the prism spectroscope both in definition and brightness in all portions 
 of the spectrum. 
 
 To produce the pure spectrum from flat gratings, two telescopes are 
 generally used, as in Fig. 1. 
 
DIFFRACTION GRATINGS 
 
 589 
 
 The telescopes are fixed, and the grating is turned on its axis to pass 
 to different portions of the spectrum. As the glass of the telescopes 
 absorbs the ultra-violet light, this portion of the spectrum is cut off 
 
 FIG. 1. Method of using Flat Grating. A, source of light; , slit; C,<7, two tel- 
 escopes, movable or fixed; Z>, grating, movable about its centre; E, eye-piece. 
 
 entirely, unless quartz lenses are used. The concave grating avoids 
 this trouble, and produces a spectrum without the aid of lenses, the 
 lines being ruled on a concave surface instead of on a flat one. Such a 
 
 5<u-ee o 
 
 FIG. 2. Method of using Concave Grating. A, source of light; B, slit; D, grating 
 mounted in beam C, movable along the ways E, E; F, camera-box or eye-piece. 
 
 grating, properly mounted, produces what has been called a normal 
 spectrum, and is specially adapted to photographic purposes (Fig. 2). 
 
590 HENRY A. EOWLAND 
 
 A special form of grating of great defining power has been invented 
 by Professor Michelson of the University of Chicago, called the 
 ' echelon' spectroscope (see SPECTROSCOPY). It is, however, of very 
 limited application. 
 
 See an article on ' Gratings in Theory and Practice ' in Astronomy 
 and Astro-Physics, XII, p. 129, 1893. 
 
 (H. A. E.) 
 
ADDRESSES 
 
A PLEA FOR PURE SCIENCE l 
 
 ADDRESS AS VICE-PRESIDENT OF SECTION B OP THE AMERICAN ASSOCIATION FOR THE 
 ADVANCEMENT OF SCIENCE, MINNEAPOLIS, MINNESOTA, A0GUST 15, 1883 
 
 [Proceedings of the American Association for the Advancement of Science, XXXII, 105-126, 
 1883 ; Science, II, 242-250, 1883 ; Journal of Franklin Institute, CXVI, 279-299, 1883] 
 
 The question is sometimes asked us as to the time of year we like 
 the best. To my mind, the spring is the most delightful; for Nature 
 then recovers from the apathy of winter, and stirs herself to renewed 
 life. The leaves grow, and the buds open, with a suggestion of vigor 
 delightful to behold; and we revel in this ever-renewed life. But this 
 cannot always last. The leaves reach their limit; the buds open to the 
 full and pass away. Then we begin to ask ourselves whether all this 
 display has been in vain, or whether it has led to a bountiful harvest. 
 
 So this magnificent country of ours has rivalled the vigor of spring 
 in its growth. Forests have been leveled, and cities built and a large and 
 powerful nation has been created on the face of the earth. We are proud 
 of our advancement. We are proud of such cities as this, founded in a 
 day upon a spot over which but a few years since, the red man hunted 
 the buffalo. But we must remember that this is only the spring of 
 our country. Our glance must not be backward; for, however beautiful 
 leaves and blossoms are, and however marvelous their rapid increase, 
 they are but leaves and blossoms after all. Rather should we look 
 forward to discover what will be the outcome of all this and what the 
 chance of harvest. For if we do this in time, we may discover the worm 
 which threatens the ripe fruit, or the barren spot where the harvest is 
 withering for want of water. 
 
 I am required to address the so-called physical section of this asso- 
 
 1 In using the word " science," I refer to physical science, as I know nothing of 
 natural science. Probably my remarks will, however, apply to both, but I do not 
 know. 
 38 
 
594 HENRY A. EOWLAND 
 
 elation. Fain would I speak pleasant words to you on this subject; 
 fain would I recount to you the progress made in this subject by my 
 countrymen, and their noble efforts to understand the order of the 
 universe. But I go out to gather the grain ripe to the harvest, and I 
 find only tares. Here and there a noble head of grain rises above the 
 weeds; but so few are they, that I find the majority of my countrymen 
 know them not, but think that they have a waving harvest, while it is 
 only one of weeds after all. American science is a thing of the future, 
 and not of the present or past; and the proper course of one in my 
 position is to consider what must be done to create a science of physics 
 in this country, rather than to call telegraphs, electric lights, and such 
 conveniences, by the name of science. I do not wish to underrate the 
 value of all these things; the progress of the world depends on them, 
 and he is to be honored who cultivates them successfully. So also the 
 cook who invents a new and palatable dish for the table benefits the 
 world to a certain degree; yet we do not dignify him by the name of a 
 chemist. And yet it is not an uncommon thing, especially in American 
 newspapers, to have the applications of science confounded with pure 
 science; and some obscure American who steals the ideas of some great 
 mind of the past, and enriches himself by the application of the same 
 to domestic uses, is often lauded above the great originator of the idea, 
 who might have worked out hundreds of such applications, had his mind 
 possessed the necessary element of vulgarity. I have often been asked, 
 which was the more important to the world, pure or applied science. 
 To have the applications of a science, the science itself must exist. 
 Should we stop its progress, and attend only to its applications, we 
 should soon degenerate into a people like the Chinese, who have made 
 no progress for generations, because they have been satisfied with the 
 applications of science, and have never sought for reasons in what they 
 have done. The reasons constitute pure science. They have known 
 the application of gunpowder for centuries; and yet the reasons for its 
 peculiar action, if sought in the proper manner, would have developed 
 the science of chemistry, and even of physics, with all their numerous 
 applications. By contenting themselves with the fact that gunpowder 
 will explode, and seeking no farther, they have fallen behind in the 
 progress of the world; and we now regard this oldest and most numerous 
 of nations as only barbarians, and yet our own country is in this same 
 state. But we have done better, for we have taken the science of the 
 old world, and applied it to all our uses, accepting it like the rain of 
 heaven, without asking whence it came, or even acknowledging the 
 
A PLEA FOR PUEE SCIENCE 595 
 
 debt of gratitude we owe to the great and unselfish workers who have 
 given it to us; and, like the rain of heaven, this pure science has fallen 
 upon our country, and made it great and rich and strong. 
 
 To a civilized nation of the present day, the applications of science 
 are a necessity, and our country has hitherto succeeded in this line 
 only for the reason that there are certain countries in the world where 
 pure science has been and is cultivated, and where the study of nature 
 is considered a noble pursuit; but such countries are rare, and those who 
 wish to pursue pure science in our own country must be prepared to 
 face public opinion in a manner which requires much moral courage. 
 They must be prepared to be looked down upon by every successful 
 inventor whose shallow mind imagines that the only pursuit of man- 
 kind is wealth, and that he who obtains most has best succeeded in this 
 world. Everybody can comprehend a million of money; but how few 
 can comprehend any advance in scientific theory, especially in its more 
 abstruse portions! And this, I believe, is one of the causes of the small 
 number of persons who have ever devoted themselves to work of the 
 higher order in any human pursuit. Man is a gregarious animal, and 
 depends very much, for his happiness, on the sympathy of those around 
 him; and it is rare to find one with the courage to pursue his own ideas 
 in spite of his surroundings. In times past, men were more isolated 
 than at present, and each came in contact with a fewer number of 
 people. Hence that time constitutes the period when the great sculp- 
 tures, paintings and poems were produced. Each man's mind was com- 
 paratively free to follow its own ideals, and the results were the great 
 and unique works of the ancient masters. To-day the railroad and the 
 telegraph, the books and newspapers, have united each individual man 
 with the rest of the world; instead of his mind being an individual, a 
 thing apart by itself, and unique, it has become so influenced by the 
 outer world, and so dependent upon it, that it has lost its originality to 
 a great extent. The man who in times past would naturally have been 
 in the lowest depths of poverty, mentally and physically, to-day meas- 
 ures tape behind a counter, and with lordly air advises the naturally 
 born genius how he may best bring his outward appearance down to a 
 level with his own. A new idea he never had, but he can at least cover 
 his mental nakedness with ideas imbibed from others. So the genius 
 of the past soon perceives that his higher ideas are too high to be 
 appreciated by the world; his mind is clipped down to the standard 
 form; every natural offshoot upwards is repressed, until the man is no 
 higher than his fellows. Hence the world, through the abundance of 
 
,596 HENRY A. EOWLAND 
 
 its intercourse, is reduced to a level. What was formerly a grand and 
 magnificent landscape, with mountains ascending above the clouds, and 
 depths whose gloom we cannot now appreciate, has become serene and 
 peaceful. The depths have been filled, and the heights levelled, and 
 the wavy harvests and smoky factories cover the landscape. 
 
 As far as the average man is concerned, the change is for the better. 
 The average life of man is far pleasanter, and his mental condition 
 better, than before. But we miss the vigor imparted by the mountains, 
 "We are tired of mediocrity, the curse of our country; we are tired of 
 seeing our artists reduced to hirelings, and imploring Congress to protect 
 them against foreign competition; we are tired of seeing our country- 
 men take their science from abroad, and boast that they here convert 
 it into wealth; we are tired of seeing our professors degrading their 
 chairs by the pursuit of applied science instead of pure science, or sit- 
 ting inactive while the whole world is open to investigation; lingering 
 by the wayside while the problem of the universe remains unsolved. We 
 wish for something higher and nobler in this country of mediocrity, for a 
 mountain to relieve the landscape of its monotony. We are surrounded 
 with mysteries, and have been created with minds to enjoy and reason 
 to aid in the unfolding of such mysteries. Nature calls to us to study 
 her, and our better feelings urge us in the same direction. 
 
 For generations there have been some few students of science who 
 have esteemed the study of nature the most noble of pursuits. Some 
 have been wealthy, and some poor; but they have all had one thing in 
 common, the love of nature and its laws. To these few men the world 
 owes all the progress due to applied science, and yet very few ever 
 received any payment in this world for their labors. 
 
 Faraday, the great discoverer of the principle on which all machines 
 for electric lighting, electric railways, and the transmission of power, 
 must rest, died a poor man, although others and the whole world have 
 been enriched by his discoveries; and such must be the fate of the 
 followers in his footsteps for some time to come. 
 
 But there will be those in the future who will study nature from 
 pure love, and for them higher prizes than any yet obtained are waiting. 
 We have but yet commenced our pursuit of science, and stand upon the 
 threshold wondering what there is within. We explain the motion of 
 the planets by the law of gravitation; but who will explain how two 
 bodies, millions of miles apart, tend to go toward each other with a 
 certain force? We now weigh and measure electricity and electric cur- 
 rents with as much ease as ordinary matter, yet have we made any 
 
A PLEA FOR PURE SCIENCE 597 
 
 approach to an explanation of the phenomenon of electricity? Light is 
 an undulatory motion,, and yet do we know what it is that undulates? 
 Heat is motion, yet do we know what it is that moves? Ordinary matter 
 is a common substance, and yet who shall fathom the mystery of its 
 internal constitution? 
 
 There is room for all in the work, and the race has but commenced. 
 The problems are not to be solved in a moment, but need the best work 
 of the best minds, for an indefinite time. 
 
 Shall our country be contented to stand by, while other countries lead 
 in the race? Shall we always grovel in the dust, and pick up the crumbs 
 which fall from the rich man's table, considering ourselves richer than 
 he because we have more crumbs, while we forget that he has the cake, 
 which is the source of all crumbs? Shall we be swine, to whom the 
 corn and husks are of more value than the pearls? If I read aright the 
 signs of the times, I think we shall not always be contented with our 
 inferior position. From looking down we have almost become blind, 
 but may recover. In a new country, the necessities of life must be 
 attended to first. The curse of Adam is upon us all, and we must earn 
 our bread. 
 
 But it is the mission of applied science to render this easier for the 
 whole world. There is a story which I once read, which will illustrate 
 the true position of applied science in the world. A boy, more fond 
 of reading than of work, was employed, in the early days of the steam- 
 engine, to turn the valve at every stroke. Necessity was the mother of 
 invention in his case: his reading was disturbed by his work, and he 
 soon discovered that he might become free from his work by so tying 
 the valve to some movable portion of the engine, as to make it move its 
 own valve. So I consider that the true pursuit of mankind is intellec- 
 tual. The scientific study of nature in all its branches, of mathematics, 
 of mankind in its past and present, the pursuit of art, and the cultiva- 
 tion of all that is great and noble in the world, these are the highest 
 occupation of mankind. Commerce, the applications of science, the 
 accumulation of wealth, are necessities which are a curse to those with 
 high ideals, but a blessing to that portion of the world which has neither 
 the ability nor the taste for higher pursuits. 
 
 As the applications of science multiply, living becomes easier, the 
 wealth necessary for the purchase of apparatus can be obtained, and 
 the pursuit of other things besides the necessities of life becomes 
 possible. 
 
 But the moral qualities must also be cultivated in proportion to the 
 
598 HENRY A. ROWLAND 
 
 wealth of the country, before much can be done in pure science. The 
 successful sculptor or painter naturally attains to wealth through the 
 legitimate work of his profession. The novelist, the poet, the musician, 
 all have wealth before them as the end of a successful career. But the 
 scientist and the mathematician have no such incentive to work: they 
 must earn their living by other pursuits, usually teaching, and only 
 devote their surplus time to the true pursuit of their science. And 
 frequently, by the small salary which they receive, by the lack of instru- 
 mental and literary facilities, by the mental atmosphere in which they 
 exist, and, most of all, by their low ideals of life, they are led to devote 
 their surplus time to applied science or to other means of increasing 
 their fortune. How shall we, then, honor the few, the very few, who, in 
 spite of all difficulties, have kept their eyes fixed on the goal, and have 
 steadily worked for pure science, giving to the world a most precious 
 donation, which has borne fruit in our greater knowledge of the 
 universe and in the applications to our physical life which have enriched 
 thousands and benefited each one of us? There are also those who have 
 every facility for the pursuit of science, who have an ample salary and 
 every appliance for work, yet who devote themselves to commercial work, 
 to testifying in courts of law, and to any other work to increase their 
 present large income. Such men would be respectable if they gave up 
 the name of professor, and took that of consulting chemist or physicist. 
 And such men are needed in the community. But for a man to occupy 
 the professor's chair in a prominent college, and, by his energy and 
 ability in the commercial applications of his science, stand before the 
 local community as a newspaper exponent of his science, is a disgrace 
 both to him and his college. It is the death-blow to science in that 
 region. Call him by his proper name, and he becomes at once a useful 
 member of the community. Put in his place a man who shall by pre- 
 cept and example cultivate his science, and how different is the result! 
 Young men, looking forward into the world for something to do, see 
 before them this high and noble life, and they see that there is some- 
 thing more honorable than the accumulation of wealth. They are thus 
 led to devote their lives to similar pursuits, and they honor the professor 
 who has drawn them to something higher than they might otherwise 
 have aspired to reach. 
 
 I do not wish to be misunderstood in this matter. It is no disgrace 
 to make money by an invention, or otherwise, or to do commercial 
 scientific work under some circumstances; but let pure science be the 
 aim of those in the chairs of professors, and so prominently the aim that 
 
A PLEA FOR PURE SCIENCE 599 
 
 there can be no mistake. If our aim in life is wealth, let us honestly 
 engage in commercial pursuits, and compete with others for its posses- 
 sion; but if we choose a life which we consider higher, let us live up to 
 it, taking wealth or poverty as it may chance to come to us, but letting 
 neither turn us aside from our pursuit. 
 
 The work of teaching may absorb the energies of many; and, indeed, 
 this is the excuse given by most for not doing any scientific work. But 
 there is an old saying, that where there is a will there is a way. Few 
 professors do as much teaching or lecturing as the German professors, 
 who are also noted for their elaborate papers in the scientific journals. 
 I myself have been burdened down with work, and know what it is; and 
 yet I here assert that all can find time for scientific research if they 
 desire it. But here, again, that curse of our country, mediocrity, is 
 upon us. Our colleges and universities seldom call for first-class men 
 of reputation, and I have even heard the trustee of a well-known college 
 assert that no professor should engage in research because of the time 
 wasted. I was glad to see. soon after, by the call of a prominent scientist 
 to that college, that the majority of the trustees did not agree with him. 
 
 That teaching is important goes without saying. A successful teacher 
 is to be respected: but if he does not lead his scholars to that which is 
 highest, is he not blameworthy? We are, then, to look to the colleges 
 and universities of the land for most of the work in pure science which 
 is done. Let us therefore examine these latter, and see what the pros- 
 pect is. 
 
 One, whom perhaps we may here style a practical follower of Euskin, 
 has stated that while in this country he was variously designated by the 
 title of captain, colonel, and professor. The story may or may not be 
 true, but we all know enough of the customs of our countrymen not to 
 dispute it on general principles. All men are born equal: some men 
 title of captain, colonel, and professor. The story may or may not be 
 The logic is conclusive; and the same kind of logic seems to have been 
 applied to our schools, colleges, and universities. I have before me the 
 report of the commissioner of education for 1880. According to that 
 report, there were 389/ or say, in round numbers, 400 institutions, call- 
 ing themselves colleges or universities, in our country! We may well 
 exclaim that ours is a great country, having more than the whole world 
 beside. The fact is sufficient. The whole earth could hardly support 
 such a number of first-class institutions. The curse of mediocrity must 
 
 J 364 reported on, and 25 not reported. 
 
600 HENEY A. EOWLAND 
 
 be upon them, to swarm in such numbers. They must be a cloud of 
 mosquitoes, instead of eagles as they profess; and this becomes evident 
 on further analysis. About one-third aspire to the name of university; 
 and I note one called by that name which has two professors and 
 eighteen students, and another having three teachers and twelve stu- 
 dents! These instances are not unique, for the number of small insti- 
 tutions and schools which call themselves universities is very great. It 
 is difficult to decide from the statistics alone the exact standing of these 
 institutions. The extremes are easy to manage. "Who can doubt 
 that an institution with over eight hundred students, and a faculty of 
 seventy is of a higher grade than those above cited having ten or twenty 
 students and two or three in the faculty? Yet this is not always true; 
 for I note one institution with over five hundred students which is 
 known to me personally as of the grade of a high school. The statistics 
 are more or less defective, and it would much weaken the force of my 
 remarks if I went too much into detail. I append the following tables, 
 however, of 330 so-called colleges and universities: 
 
 218 had from to 100 students. 
 88 had from 100 to 200 students. 
 12 had from 200 to 300 students. 
 
 6 had from 300 to 500 students. 
 
 6 had over 500 students. 
 
 Of 322 so-called colleges and universities: 
 
 206 had to 10 in the faculty. 
 99 had 10 to 20 in the faculty. 
 17 had 20 or over in the faculty. 
 
 If the statistics were forthcoming, and possibly they may exist, 
 we might also get an idea of the standing of these institutions and their 
 approach to the true university idea, by the average age of the scholars. 
 Possibly also the ratio of number of scholars to teachers might be of 
 some help. All these methods give an approximation to the present 
 standing of the institutions. But there is another method of attacking 
 the problem, which is very exact, yet it only gives us the possibilities in 
 the case of the institutions. I refer to the wealth of the institution. 
 In estimating the wealth, I have not included the value of grounds and 
 buildings, for this is of little importance, either to the present or future 
 standing of the institution, as good work can be done in a hovel as in a 
 
A PLEA FOR PURE SCIENCE 601 
 
 
 
 palace. I have taken the productive funds of the institution as the 
 basis of estimate. I find: 
 
 234 have below $500,000. 
 
 8 have between $500,000 and $1,000,000. 
 8 have over $1,000,000. 
 
 There is no fact more firmly established, all over the world, than that 
 the higher education can never be made to pay for itself. Usually the 
 cost to a college, of educating a young man, very much exceeds what 
 he pays for it, and is often three or four times as much. The higher 
 the education, the greater this proportion will be; and a university of 
 the highest class should anticipate only a small accession to its income 
 from the fees of students. Hence the test I have applied must give a 
 true representation of the possibilities in every case. According to the 
 figures, only sixteen colleges and universities have $500,000 or over of 
 invested funds, and only one-half of these have $1,000,000 and over. 
 Now, even the latter sum is a very small endowment for a college; and 
 to call any institution a university which has less than $1,000,000 is to 
 render it absurd in the face of the world. And yet more than 100 of 
 our institutions, many of them very respectable colleges, have abused 
 the word "university" in this manner. It is to be hoped that the 
 endowment of the more respectable of these institutions may be in- 
 creased, as many of them deserve it; and their unfortunate appellation 
 has probably been repented of long since. 
 
 But what shall we think of a community that gives the charter of 
 a university to an institution with a total of $20,000 endowment, two 
 so-called professors, and eighteen students! or another with three 
 professors, twelve students, and a total of $27,000 endowment, mostly 
 invested in buildings! And yet there are very many similar institu- 
 tions; there being sixteen with three professors or less, and very many 
 indeed with only four or five. 
 
 Such facts as these could only exist in a democratic country, where 
 pride is taken in reducing everything to a level. And I may also say. 
 that it can only exist in the early days of such a democracy; for an 
 intelligent public will soon perceive that calling a thing by a wrong 
 name does not change its character, and that truth, above all things, 
 should be taught to the youth of the nation. 
 
 It may be urged, that all these institutions are doing good work in 
 education; and that many young men are thus taught, who could not 
 afford to go to a true college or university. But I do not object to the 
 
602 HENRY A. ROWLAND 
 
 
 
 education., though I have no doubt an investigation would disclose 
 equal absurdities here, for it is aside from my object. But I do object 
 to lowering the ideals of the youth of the country. Let them know that 
 they are attending a school, and not a university; and let them know 
 that above them comes the college, and above that the university. Let 
 them be taught that they are only half educated, and that there are 
 persons in the world by whose side they are but atoms. In other words, 
 let them be taught the truth. 
 
 It may be that some small institutions are of high grade, especially 
 those which are new; but who can doubt that more than two-thirds of 
 our institutions calling themselves colleges and universities are un- 
 worthy of the name? Each one of these institutions has so-called pro- 
 fessors, but it is evident that they can be only of the grade of teachers. 
 Why should they not be so called? The position of teacher is an 
 honored one, but is not made more honorable by the assumption of a 
 false title. Furthermore, the multiplication of the title, and the ease 
 with which it can be obtained, render it scarcely worth striving for. 
 When the man of energy, ability, and perhaps genius is rewarded by 
 the same title and emoluments as the commonplace man with the 
 modicum of knowledge, who takes to teaching, not because of any apti- 
 tude for his work, but possibly because he has not the energy to com- 
 pete with his fellow-men in business, then I say one of the inducements 
 for the first-class men to become professors is gone. 
 
 When work and ability are required for the position, and when the 
 professor is expected to keep up with the progress of his subject, and 
 to do all in his power to advance it, and when he is selected for these 
 reasons, then the position will be worth working for, and the successful 
 competitor will be honored accordingly. The chivalric spirit which 
 prompted Faraday to devote his life to the study of nature may actuate 
 a few noble men to give their lives to scientific work; but if we wish to 
 cultivate this highest class of men in science, we must open a career 
 for them worthy of their efforts. 
 
 Jenny Lind, with her beautiful voice, would have cultivated it to 
 some extent in her native village: yet who would expect her to travel 
 over the world, and give concerts for nothing? and how would she have 
 been able to do so if she had wished? And so the scientific man, what- 
 ever his natural talents, must have instruments and a library, and a 
 suitable and respectable salary to live upon, before he is able to exert 
 himself to his full capacity. This is true of advance in all the higher 
 departments of human learning, and yet something more is necessary. 
 
A PLEA FOR PUEE SCIENCE 603 
 
 It is not those in this country who receive the largest salary, and have 
 positions in the richest colleges, who have advanced their subject the 
 most: men receiving the highest salaries, and occupying the professor's 
 chair, are to-day doing absolutely nothing in pure science, but are striv- 
 ing by the commercial applications of their science to increase their 
 already large salary. Such pursuits, as I have said before, are honorable 
 in their proper place; but the duty of a professor is to advance his science, 
 and to set an example of pure and true devotion to it which shall demon- 
 strate to his students and the world that there is something high and 
 noble worth living for. Money-changers are often respectable men, and 
 yet they were once severely rebuked for carrying on their trade in the 
 court of the temple. 
 
 "Wealth does not constitute a university, buildings do not: it is the 
 men who constitute its faculty, and the students who learn from them. 
 It is the last and highest step which the mere student takes. He goes 
 forth into the world, and the height to which he rises has been influenced 
 by the ideals which he has consciously or unconsciously imbibed in his 
 university. If the professors under whom he has studied have been 
 high in their profession, and have themselves had high ideals; if they 
 have considered the advance of their particular subject their highest 
 work in life, and are themselves honored for their intellect throughout 
 the world, the student is drawn toward that which is highest, and 
 ever after in life has high ideals. But if the student is taught by what 
 are sometimes called good teachers, and teachers only, who know little 
 more than the student, and who are often surpassed and even despised 
 by him, no one can doubt the lowered tone of his mind. He finds that 
 by his feeble efforts he can surpass one to whom a university has given 
 its highest honor; and he begins to think that he himself is a born 
 genius, and the incentive to work is gone. He is great by the side of 
 the molehill, and does not know any mountain to compare himself with. 
 
 A university should have not only great men in its faculty, but have 
 numerous minor professors and assistants of all kinds, and should 
 encourage the highest work, if for no other reason than to encourage 
 the student to his highest efforts. 
 
 But, assuming that the professor has high ideals, wealth such as only 
 a large and high university can command is necessary to allow him the 
 fullest development. 
 
 And this is specially so in our science of physics. In the early days 
 of physics and chemistry, many of the fundamental experiments could 
 be performed with the simplest apparatus. And so we often find the 
 
604 HENKT A. KOWLAND 
 
 names of Wollaston and Faraday mentioned as needing scarcely any- 
 thing for their researches. Much can even now be done with the sim- 
 plest apparatus, and nobody, except the utterly incompetent, need stop 
 for want of it; but the fact remains, that one can only be free to investi- 
 gate in all departments of chemistry and physics, when he not only has 
 a complete laboratory at his command, but a fund to draw on for the 
 expenses of each experiment. That simplest of the departments of 
 physics, namely, astronomy, has now reached such perfection that 
 nobody can expect to do much more in it without a perfectly equipped 
 observatory; and even this would be useless without an income sufficient 
 to employ a corps of assistants to make the observations and computa- 
 tions. But even in this simplest of physical subjects, there is great 
 misunderstanding. Our country has very many excellent observatories, 
 and yet little work is done in comparison, because no provision has been 
 made for maintaining the work of the observatory; and the wealth 
 which, if concentrated, might have made one effective observatory which 
 would prove a benefit to astronomical science, when scattered among a 
 half-dozen merely furnishes telescopes for the people in the surrounding 
 region to view the moon with. And here I strike the keynote of at least 
 one need of our country, if she would stand well in science; and the 
 following item which I clip from a newspaper will illustrate the matter: 
 " The eccentric old Canadian, Arunah Huntington, who left $200,000 
 to be divided among the public schools of Vermont, has done something 
 which will be of little practical value to the schools. Each district will 
 be entitled to the insignificant sum of $10, which will not advance 
 much the cause of education." 
 
 Nobody will dispute the folly of such a bequest, or the folly of filling 
 the country with telescopes to look at the moon, and calling them 
 observatories. How much better to concentrate the wealth into a few 
 parcels, and make first-class observatories and institutions with it! 
 
 Is it possible that any of our four hundred colleges and universities 
 have love enough of learning to unite with each other and form larger 
 institutions? Is it possible that any have such a love of truth that they 
 are willing to be called by their right name? I fear not; for the spirit 
 of expectation, which is analogous to the spirit of gambling, is strong in 
 the American breast, and each institution which now, except in name, 
 slumbers in obscurity, expects in time to bloom out into full prosperity. 
 Although many of them are under religious influence, where truth is 
 inculcated, and where men are taught to take a low seat at the table 
 in order that they may be honored by being called up higher, and not 
 
A PLEA FOR PURE SCIENCE 605 
 
 dishonored by being thrust down lower, yet these institutions have thrust 
 themselves into the highest seats, and cannot probably be dislodged. 
 
 But would it not be possible so to change public opinion that no 
 college could be founded with a less endowment than say $1,000,000, 
 or no university with less than three or four times that amount. From 
 the report of the commissioner of education, I learn that such a thing 
 is taking place; that the tendency towards large institutions is increas- 
 ing, and that it is principally in the west and southwest that the multi- 
 plication of small institutions with big names is to be feared most, and 
 that the east is almost ready for the great coming university. 
 
 The total wealth of the four hundred colleges and universities in 1880 
 was about $40,000,000 in buildings, and $43,000,000 in productive 
 i'unds. This would be sufficient for one great university of $10,000,000, 
 four of $5,000,000, and twenty-six colleges of $2,000,000 each. But 
 such an idea can of course never be carried out. Government appro- 
 priations are out of the question, because no political trickery must be 
 allowed around the ideal institution. 
 
 In the year 1880 the private bequests to all schools and colleges 
 amounted to about $5,500,000; and, although there was one bequest of 
 $1,250,000, yet the amount does not appear to be phenomenal. It 
 would thus seem that the total amount was about five million dollars in 
 one year, of which more than half is given to so-called colleges and 
 universities. It would be very difficult to regulate these bequests so 
 that they might be concentrated sufficiently to produce an immediate 
 result. But the figures show that generosity is a prominent feature of 
 the American people, and that the needs of the country only have to 
 be appreciated to have the funds forthcoming. We must make the 
 need of research and of pure science felt in the country. "We must live 
 such lives of pure devotion to our science, that all shall see that we ask 
 for money, not that we may live in indolent ease at the expense of 
 charity, but that we may work for that which has advanced and will 
 advance the world more than any other subject, both intellectually and 
 physically. We must live such lives as to neutralize the influence of 
 those who in high places have degraded their profession, or have given 
 themselves over to ease, and do nothing for the science which they 
 represent. Let us do what we can with the present means at our dis- 
 posal. There is not one of us who is situated in the position best 
 adapted to bring out all his powers, and to allow him to do most for 
 his science. All have their difficulties, and I do not think that circum- 
 stances will ever radically change a man. If a man has the instinct of 
 
HENRY A. ROWLAND 
 
 research in him, it will always show itself in some form. But circum- 
 stances may direct it into new paths, or may foster it so that what 
 would otherwise have died as a bud now blossoms and ripens into the 
 perfect fruit. 
 
 Americans have shown no lack of invention in small things; and the 
 same spirit when united to knowledge and love of science, becomes the 
 spirit of research. The telegraph-operator, with his limited knowledge 
 of electricity and its laws, naturally turns his attention to the improve- 
 ment of the only electrical instrument he knows anything about; and his 
 researches would be confined to the limited sphere of his knowledge, 
 and to the simple laws with which he is acquainted. But as his knowl- 
 edge increases, and the field broadens before him, as he studies the 
 mathematical theory of the subject, and the electromagnetic theory of 
 light loses the dim haze due to distance, and becomes his constant com- 
 panion, the telegraph instrument becomes to him a toy, and his effort 
 to discover something new becomes research in pure science. 
 
 It is useless to attempt to advance science until one has mastered the 
 science: he must step to the front before his blows can tell in the 
 strife. Furthermore, I do not believe anybody can be thorough in any 
 department of science, without wishing to advance it. In the study of 
 what is known, in the reading of the scientific journals, and the discus- 
 sions therein contained of the current scientific questions, one would 
 obtain an impulse to work, even though it did not before exist; and the 
 same spirit which prompted him to seek what was already known would 
 make him wish to know the unknown. And I may say that I never met 
 a case of thorough knowledge in my own science, except in the case of 
 well-known investigators. I have met men who talked well, and I have 
 sometimes asked myself why they did not do something; but further 
 knowledge of their character has shown the superficiality of their 
 knowledge. I am no longer a believer in men who could do something 
 if they would, or would do something if they had a chance. They are 
 impostors. If the spirit is there, it will show itself in spite of circum- 
 stances. 
 
 As I remarked before, the investigator in pure science is usually a 
 professor. He must teach as well as investigate. It is a question which 
 has been discussed in late years, as to whether these two functions had 
 better be combined in the same individual, or separated. It seems to 
 be the opinion of most, that a certain amount of teaching is conducive, 
 rather than otherwise, to the spirit of research. I myself think that 
 this is true, and I should myself not like to give up my daily lecture; but 
 
A PLEA FOR PURE SCIENCE 607 
 
 one must not be overburdened. I suppose that the true solution, in 
 many cases, would be found in the multiplication of assistants, not only 
 for the work of teaching but of research. Some men are gifted with 
 more ideas than they can work out with their own hands, and the world 
 is losing much by not supplying them with extra hands. Life is short: 
 old age comes quickly, and the amount one pair of hands can do is very 
 limited. What sort of shop would that be, or what sort of factory, where 
 one man had to do all the work with his own hands? It is a fact in 
 nature, which no democracy can change, that men are not equal, that 
 some have brains, and some hands; and no idle talk about equality can 
 ever subvert the order of the universe. 
 
 I know of no institution in this country where assistants are supplied 
 to aid directly in research; yet why should it not be so? Even the 
 absence of assistant professors and assistants of all kinds, to aid in 
 teaching, is very noticeable, and must be remedied before we can expect 
 much. 
 
 There are many physical problems, especially those requiring exact 
 measurements, which cannot be carried out by one man, and can only 
 be successfully attacked by the most elaborate apparatus, and with a 
 full corps of assistants. Such are Eegnault's experiments on the funda- 
 mental laws of gases and vapors, made thirty or forty years ago by aid 
 from the French government, and which are the standards to this day. 
 Although these experiments were made with a view to the practical 
 calculation of the steam-engine, yet they were carried out in such a 
 broad spirit that they have been of the greatest theoretical use. Again, 
 what would astronomy have done without the endowment of observa- 
 tories? By their means, that science has become the most perfect of 
 all branches of physics, as it should be from its simplicity. There is no 
 doubt, in my mind, that similar institutions for other branches of 
 physics, or, better, to include the whole of physics, would be equally 
 successful. A large and perfectly equipped physical laboratory with its 
 large revenues, its corps of professors and assistants, and its machine- 
 shop for the construction of new apparatus, would be able to advance 
 our science quite as much as endowed observatories have advanced 
 astronomy. But such a laboratory should not be founded rashly. The 
 value will depend entirely on the physicist at its head, who has to 
 devise the plan, and to start it into practical working. Such a man will 
 always be rare, and cannot always be obtained. After one had been 
 successfully started, others could follow; for imitation requires little 
 brains. 
 
608 HENRY A. EOWLAND 
 
 One could not be certain of getting the proper man every time, but 
 the means of appointment should be most carefully studied so as to 
 secure a good average. There can be no doubt that the appointment 
 should rest with a scientific body capable of judging the highest work 
 of each candidate. 
 
 Should any popular element enter, the person chosen would be of the 
 literary-scientific order, or the dabbler on the outskirts who presents his 
 small discoveries in the most theatrical manner. What is required is 
 a man of depth, who has such an insight into physical science that he 
 can tell when blows will best tell for its advancement. 
 
 Such a grand laboratory as I describe does not exist in the world, at 
 present, for the study of physics. But no trouble has ever been found 
 in obtaining means to endow astronomical science. Everybody can 
 appreciate, to some extent, the value of an observatory; as astronomy 
 is the simplest of scientific subjects, and has very quickly reached a 
 position where elaborate instruments and costly computations are neces- 
 sary to further advance. The whole domain of physics is so wide that 
 workers have hitherto found enough to do. But it cannot always be 
 so, and the time has even now arrived when such a grand laboratory 
 should be founded. Shall our country take the lead in this matter, or 
 shall we wait for foreign countries to go before? They will be built in 
 the future, but when and how is the question. 
 
 Several institutions are now putting up laboratories for physics. 
 They are mostly for teaching, and we can expect only a comparatively 
 small amount of work from most of them. But they show progress; 
 and, if the progress be as quick in this direction as in others, we should 
 be able to see a great change before the end of our lives. 
 
 As stated before, men are influenced by the sympathy of those with 
 whom they come in contact. It is impossible to change public opinion 
 in our favor immediately; and, indeed, we must always seek to lead it, 
 and not be guided by it. For pure science is the pioneer who must not 
 hover about cities and civilized countries, but must strike into unknown 
 forests, and climb the hitherto inaccessible mountains which lead to 
 and command a view of the promised land, the land which science 
 promises us in the future; which shall not only flow with milk and 
 honey, but shall give us a better and more glorious idea of this wonder- 
 ful universe. We must create a public opinion in our favor, but it need 
 not at first be the general public. We must be contented to stand aside, 
 and see the honors of the world for a time given to our inferiors; and 
 
A PLEA FOR PURE SCIENCE 609 
 
 must be better contented with the approval of our own consciences, and 
 of the very few who are capable of judging our work, than of the whole 
 world beside. Let us look to the other physicists, not in our own town, 
 not in our own country, but in the whole world, for the words of praise 
 which are to encourage us. or the words of blame which are to stimulate 
 us to renewed effort. For what to us is the praise of the ignorant? Let 
 us join together in the bonds of our scientific societies, and encourage 
 each other, as we are now doing, in the pursuit of our favorite study; 
 knowing that the world will some time recognize our services, and 
 knowing, also, that we constitute the most important element in human 
 progress. 
 
 But danger is also near, even in our societies. When the average tone 
 of the society is low, when the highest honors are given to the mediocre, 
 when third-class men are held up as examples, and when trifling inven- 
 tions are magnified into scientific discoveries, then the influence of 
 such societies is prejudicial. A young scientist attending the meetings 
 of such a society soon gets perverted ideas. To his mind, a molehill is 
 a mountain, and the mountain a molehill. The small inventor or the 
 local celebrity rises to a greater height, in his mind, than the great 
 leader of science in some foreign land. He gauges himself by the 
 molehill, and is satisfied with his stature; not knowing that he is but 
 an atom in comparison with the mountain, until, perhaps, in old age, 
 when it is too late. But, if the size of the mountain had been seen at 
 first, the young scientist would at least have been stimulated in his 
 endeavor to grow. 
 
 We cannot all be men of genius; but we can, at least, point them out 
 to those around us. We may not be able to benefit science much our- 
 selves; but we can have high ideals on the subject, and instil them into 
 those with whom we come in contact. For the good of ourselves, for 
 the good of our country, for the good to the world, it is incumbent on 
 us to form a true estimate of the worth and standing of persons and 
 things, and to set before our own minds all that is great and good and 
 noble, all that is most important for scientific advance, above the mean 
 and low and unimportant. 
 
 It is very often said, that a man has a right to his opinion. This 
 might be true for a man on a desert island, whose error would influence 
 only himself; but when he opens his lips to instruct others, or even 
 when he signifies his opinions by his daily life, then he is directly 
 responsible for all his errors of judgment or fact. He has no right to 
 39 
 
G10 HENKY A. KOWLAND 
 
 think a molehill as big as a mountain, nor to teach it, any more than 
 he has to think the world is flat, and teach that it is so. The facts and 
 laws of our science have not equal importance, neither have the men 
 who cultivate the science achieved equal results. One thing is greater 
 than another, and we have no right to neglect the order. Thus shall 
 our minds be guided aright, and our efforts be toward that which is the 
 highest. 
 
 Then shall we see that no physicist of the first class has ever existed 
 in this country, that we must look to other countries for our leaders 
 in that subject, and that the few excellent workers in our country must 
 receive many accessions from without before they can constitute an 
 American science, or do their share in the world's work. 
 
 But let me return to the subject of scientific societies. Here Ameri- 
 can science has its hardest problem to contend with. There are very 
 many local societies dignified by high-sounding names, each having its 
 local celebrity, to whom the privilege of describing some crab with an 
 extra claw, which he found in his morning ramble, is inestimable. And 
 there are some academies of science, situated at our seats of learning, 
 which are doing good work in their localities. But distances are so 
 great that it is difficult to collect men together at any one point. The 
 American Association, which we are now attending, is not a scientific 
 academy, and does not profess to be more than a gathering of all who 
 are interested in science, to read papers and enjoy social intercourse. 
 The National Academy of Sciences contains eminent men from the 
 whole country, but then it is only for the purpose of advising the gov- 
 ernment freely on scientific matters. It has no building, it has no 
 library; and it publishes nothing except the information which it freely 
 gives to the government, which does nothing for it in return. It has 
 not had much effect directly on American science; but the liberality of 
 the government in the way of scientific expeditions, publications, etc., 
 is at least partly due to its influence, and in this way it has done much 
 good. But it in no way takes the place of the great Eoyal society, or 
 the great academies of science at Paris, Berlin, Vienna, St. Petersburg, 
 Munich, and, indeed, all the European capitals and large cities. These, 
 by their publications, give to the young student, as well as to the more 
 advanced physicist, models of all that is considered excellent; and to 
 become a member is one of the highest honors to which he can aspire, 
 while to write a memoir which the academy considers worthy to be pub- 
 lished in its transactions excites each one to his highest effort. 
 
A PLEA FOR PURE SCIENCE 611 
 
 The American Academy of Sciences in Boston is perhaps our nearest 
 representation of this class of academies, but its limitation of member- 
 ship to the state deprives it of a national character. 
 
 But there is another matter which influences the growth of our 
 science. 
 
 As it is necessary for us still to look abroad for our highest inspira- 
 tion in pure science, and as science is not an affair of one town or one 
 country, but of the whole world, it becomes us all to read the current 
 journals of science and the great transactions of foreign societies, as well 
 as those of our own countries. These great transactions and journals 
 should be in the library of every institution of learning in the country, 
 where science is taught. How can teachers and professors be expected 
 to know what has been discovered in the past, or is being discovered 
 now, if these are not provided? Has any institution a right to starve 
 mentally the teachers whom it employs, or the students who come to it? 
 There can be but one answer to this; and an institution calling itself a 
 university, and not having the current scientific journals upon its table 
 or the transactions of societies upon its library shelves, is certainly not 
 doing its best to cultivate all that is best in this world. 
 
 We call this a free country, and yet it is the only one where there is a 
 direct tax upon the pursuit of science. The low state of pure science 
 in our country may possibly be attributed to the youth of the country; 
 but a direct tax, to prevent the growth of our country in that subject, 
 cannot be looked upon as other than a deep disgrace. I refer to the 
 duty upon foreign books and periodicals. In our science, no books above 
 elementary ones have ever been published, or are likely to be pub- 
 lished in this country; and yet every teacher in physics must have them, 
 not only in the college library, but on his own shelves, and must pay the 
 government of this country to allow him to use a portion of his small 
 salary to buy that which is to do good to the whole country. All free- 
 dom of intercourse which is necessary to foster our growing science is 
 thus broken off, and that which might, in time, relieve our country of 
 its mediocrity, is nipped in the bud by our government, which is most 
 liberal when appealed to directly on scientific subjects. 
 
 One would think that books in foreign languages might be admitted 
 free; but to please the half-dozen or so workmen who reprint German 
 books, not scientific, our free intercourse with that country is cut off. 
 Our scientific associations and societies must make themselves heard in 
 this matter, and show those in authority how the matter stands. 
 
612 HENKY A. ROWLAND 
 
 In conclusion, let me say once more that I do not believe that our 
 country is to remain long in its present position. The science of physics, 
 in whose applications our country glories, is to arise among us, and make 
 us respected by the nations of the world. Such a prophecy may seem 
 rash with regard to a nation which does not yet do enough physical work 
 to support a physical journal. But we know the speed with which we 
 advance in this country: we see cities springing up in a night, and other 
 wonders performed at an unprecedented rate. And now we see physical 
 laboratories being built, we see a great demand for thoroughly trained 
 physicists, who have not shirked their mathematics, both as professors 
 and in so-called practical life; and perhaps we have the feeling, common 
 to all true Americans, that our country is going forward to a glorious 
 future, when we shall lead the world in the strife for intellectual prizes 
 as we now do in the strife for wealth. 
 
 But if this is to be so, we must not aim low. The problems of the 
 universe cannot be solved without labor; they cannot be attacked with- 
 out the proper intellectual as well as physical tools; and no physicist 
 need expect to go far without his mathematics. No one expects a horse 
 to win in a great and long race who has not been properly trained; and 
 it would be folly to attempt to win with one, however pure his blood 
 and high his pedigree, without it. The problems we solve are more diffi- 
 cult than any race; the highest intellect cannot hope to succeed without 
 proper preparation. The great prizes are reserved for the greatest 
 efforts of the greatest intellects, who have kept their mental eye bright 
 and flesh hard by constant exercise. Apparatus can be bought with 
 money, talents may come to us at birth; but our mental tools, our mathe- 
 matics, our experimental ability, our knowledge of what others have 
 done before us, all have to be obtained by work. The time is almost 
 past, even in our own country, when third-rate men can find a place as 
 teachers, because they are unfit for everything else. We wish to see 
 brains and learning, combined with energy and immense working 
 power, in the professor's chair; but, above all, we wish to see that high 
 and chivalrous spirit which causes one to pursue his idea in spite of all 
 difficulties, to work at the problems of nature with the approval of his 
 own conscience, and not of men before him. Let him fit himself for 
 the struggle with all the weapons which mathematics and the experi- 
 ence of those gone before him can furnish, and let him enter the arena 
 with the fixed and stern purpose to conquer. Let him not be contented 
 to stand back with the crowd of mediocrity, but let him press forward 
 for a front place in the strife. 
 
613 
 
 The whole universe is before us to study. The greatest labor of the 
 greatest minds has only given us a few pearls; and yet the limitless 
 ocean, with its hidden depths filled with diamonds and precious stones, 
 is before us. The problem of the universe is yet unsolved, and the mys- 
 tery involved in one single atom yet eludes us. The field of research 
 only opens wider and wider as we advance, and our minds are lost in 
 wonder and astonishment at the grandeur and beauty unfolded before 
 us. Shall we help in this grand work, or not? Shall our country do 
 its share, or shall it still live in the almshouse of the world? 
 
THE PHYSICAL LABOKATOKY IN MODEKN EDUCATION 
 
 ADDRESS FOR COMMEMORATION DAY OF THE JOHNS HOPKINS UNIVERSITY, 
 FEBRUARY 22, 1886 
 
 [Johns Hopkins University Circulars, No. 50, pp. 103-105, 1886] 
 
 From the moment we are born into this world down to the day when 
 we leave it, we are called upon every moment to exercise our judgment 
 with respect to matters pertaining to our welfare. While nature has 
 supplied us with instincts which take the place of reason in our infancy, 
 and which form the basis of action in very many persons through life, 
 yet, more and more as the world progresses and as we depart from the 
 age of childhood, we are forced to discriminate between right and wrong, 
 between truth and falsehood. No longer can we shelter ourselves behind 
 those in authority over us, but we must come to the front and each one 
 decide for himself what to believe and how to act in the daily routine 
 and the emergencies of life. This is not given to us as a duty which we 
 can neglect if we please, but it is that which every man or woman, con- 
 sciously or unconsciously, must go through with. 
 
 Most persons cut this Gordian knot, which they cannot untangle, by 
 accepting the opinions which have been taught them and which appear 
 correct to their particular circle of friends and associates: others take 
 the opposite extreme and, with intellectual arrogance, seek to build up 
 their opinions and beliefs from the very foundation, individually and 
 alone, without help from others. Intermediate between these two ex- 
 tremes comes the man with full respect for the opinions of those around 
 him, and yet with such discrimination that he sees a chance of error 
 in all and most of all in himself. He has a longing for the truth and is 
 willing to test himself, to test others and to test nature until he finds it. 
 He has the courage of his opinions when thus carefully formed, and 
 is then, but not till then, willing to stand before the world and proclaim 
 what he considers the truth. Like Galileo and Copernicus, he inaugu- 
 rates a new era in science, or like Luther, in the religious belief of man- 
 kind. He neither shrinks within himself at the thought of having an 
 opinion of his own, nor yet believes it to be the only one worth consid- 
 ering in the world; he is neither crushed with intellectual humility, nor 
 yet exalted with intellectual pride; he sees that the problems of nature 
 and society can be solved, and yet he knows that this can only come 
 
THE PHYSICAL LABORATOET IN MODERN EDUCATION 615 
 
 about by the combined intellect of the world acting through ages of time 
 and that he, though his intellect were that of Newton, can, at best, do 
 very little toward it. Knowing this he seeks all the aids in his power 
 to ascertain the truth, and if he, through either ambition or love of 
 truth, wishes to impress his opinions on the world, he first takes care 
 to have them correct. Above all, he is willing to abstain from having 
 opinions on subjects of which he knows nothing. 
 
 It is the province of modern education to form such a mind while at 
 the same time giving to it enough knowledge to have a broad outlook 
 over the world of science, art and letters. Time will not permit me to 
 discuss the subject of education in general, and, indeed, I would be 
 transgressing the principles above laid down if I should attempt it. I 
 shall only call attention at this present time to the place of the labo- 
 ratory in modern education. I have often had a great desire to know 
 the state of mind of the more eminent of mankind before modern science 
 changed the world to its present condition and exercised its influence 
 on all departments of knowledge and speculation. But I have failed 
 to picture to myself clearly such a mind while, at the same time, the 
 study of human nature, as it exists at present, shows me much that I 
 suppose to be in common with it. As far as I can see, the unscientific 
 mind differs from the scientific in this, that it is willing to accept and 
 make statements of which it has no clear conception to begin with and 
 of whose truth it is not assured. It is an irresponsible state of mind 
 without clearness of conception, where the connection between the 
 thought and its object is of the vaguest description. It is the state of 
 mind where opinions are given and accepted without ever being sub- 
 jected to rigid tests, and it may have some connection with that state of 
 mind where everything has a personal aspect and we are guided by 
 feelings rather than reason. 
 
 When, by education, we attempt to correct these faults, it is neces- 
 sary that we have some standard of absolute truth: that we bring the 
 mind in direct contact with it and let it be convinced of its errors again 
 and again. We may state, like the philosophers who lived before Gali- 
 leo, that large bodies fall faster than small ones, but when we see them 
 strike the ground together we know that our previous opinion was false 
 and we learn that even the intellect of an Aristotle may be mistaken. 
 Thus we are taught care in the formation of our opinions and find that 
 the unguided human mind goes astray almost without fail. We must 
 correct it constantly and convince it of error over and over again until 
 it discovers the proper method of reasoning, which will surely accord 
 with the truth in whatever conclusions it may reach. There is, however, 
 
616 HENRY A. ROWLAND 
 
 danger in this process that the mind may become over cautious and thus 
 present a weakness when brought in contact with an unscrupulous per- 
 son who cares little for truth and a great deal for effect. But if we 
 believe in the maxim that truth will prevail and consider it the duty 
 of all educated men to aid its progress, the kind of mind which I describe 
 is the proper one to foster by education. Let the student be brought 
 face to face with nature: let him exercise his reason with respect to the 
 simplest physical phenomenon and then, in the laboratory, put his opin- 
 ions to the test; the result is invariably humility, for he finds that nature 
 has laws which must be discovered by labor and toil and not by wild 
 flights of the imagination and scintillations of so-called genius. 
 
 Those who have studied the present state of education in the schools 
 and colleges tell us that most subjects, including the sciences, are taught 
 as an exercise to the memory. I myself have witnessed the melancholy 
 sight in a fashionable school for young ladies of those who were born 
 to be intellectual beings reciting page after page from memory, without 
 any effort being made to discover whether they understood the subject 
 or not. There are even many schools, so-called, where the subject of 
 physics or natural philosophy itself is taught, without even a class ex- 
 periment to illustrate the subject and connect the words with ideas. 
 Words, mere words, are taught and a state of mind far different from 
 that above described is produced. If one were required to find a sys- 
 tem of education which would the most surely and certainly disgust the 
 student with any subject, I can conceive of none which would do this 
 more quickly than this method, where he is forced to learn what he 
 does not understand. It is said of the Faraday that he never could 
 understand any scientific experiment thoroughly until he had not only 
 seen it performed by others, but had performed it himself. Shall we 
 then expect children and youth to do what Faraday could not do? A 
 thousand times better never teach the subject at all. 
 
 Tastes differ, but we may safely say that every subject of study which 
 is thoroughly understood is a pleasure to the student. The healthy 
 mind as well as the healthy body craves exercise, and the school room 
 or the lecture room should be a source of positive enjoyment to those 
 who enter it. Above all. the study of nature, from the magnificent uni- 
 verse, across which light itself, at the rate of 186,000 miles per second, 
 cannot go in less than hundreds of years, down to the atom of which 
 millions are required to build up the smallest microscopic object, should 
 be the most interesting subject brought to the notice of the student. 
 
 Some are born blind to the beauties of the world around them, some 
 
THE PHYSICAL LABORATOKY ix MODERN EDUCATION 61? 
 
 have their tastes better developed in other directions, and some have 
 minds incapable of ever understanding the simplest natural phenomenon; 
 but there is also a large class of students who have at least ordinary pow- 
 ers and ordinary tastes for scientific pursuits: to train the powers of 
 observation and classification let them study natural history, not only 
 from books, but from prepared specimens or directly from nature: to 
 give care in experiment and convince them that nature forgives no 
 error, let them enter the chemical laboratory: to train them in exact and 
 logical powers of reasoning, let them study mathematics: but to com- 
 bine all this training in one and exhibit to their minds the most perfect 
 and systematic method of discovering the exact laws of nature, let them 
 study physics and astronomy, where observation, common sense and 
 mathematics go hand in hand. The object of education is not only to 
 produce a man who Tcnows, but one who does; who makes his mark in 
 the struggle of life and succeeds well in whatever he undertakes: who 
 can solve the problems of nature and of humanity as they arise, and who, 
 when he knows he is right, can boldly convince the world of the fact. 
 Men of action are needed as well as men of thought. 
 
 There is no doubt in my mind that this is the point in which much 
 of our modern education fails. Why is it? I answer that the memory 
 alone is trained and the reason and judgment are used merely to refer 
 matters to some authority who is considered final, and worse than all, 
 they are not trained to apply their knowledge constantly. To produce 
 men of action they must be trained in action. If the languages be 
 studied, they must be made to translate from one language to the other 
 until they have perfect facility in the process. If mathematics be 
 studied, they must work problems, more problems and problems again, 
 until they have the use of what they know. If they study the sciences, 
 they must enter the laboratory and stand face to face with nature; they 
 must learn to test their knowledge constantly and thus see for them- 
 selves the sad results of vague speculation; they must learn by direct 
 experiment that there is such a thing in the world as truth and that 
 their own mind is most liable to error. They must try experiment after 
 experiment and work problem after problem until they become men of 
 action and not of theory. 
 
 This, then, is the use of the laboratory in general education, to train 
 the mind in right modes of thought by constantly bringing it in con- 
 tact with absolute truth and to give it a pleasant and profitable method 
 of exercise which will call all its powers of reason and imagination into 
 play. Its use in the special training of scientists needs no remark, for it 
 
618 HENKY A. EOWLAND 
 
 is well known that it is absolutely essential. The only question is 
 whether the education of specialists in science is worth undertaking at 
 all, and of these I have only to consider natural philosophers or physi- 
 cists. I might point to the world around me, to the steam engine, to 
 labor-saving machinery, to the telegraph, to all those inventions which 
 make the present age the "Age of Electricity," and let that be my 
 answer. Nobody could gainsay that the answer would be complete, for 
 all are benefited by these applications of science, and he would be con- 
 sidered absurd who did not recognize their value. These follow in the 
 train of physics, but they are not physics; the cultivation of physics 
 brings them and always will bring them, for the selfishness of mankind 
 can always be relied upon to turn all things to profit. But in the edu- 
 cation pertaining to a university we look for other results. The special 
 physicist trained there must be taught to cultivate his science for its 
 own sake. He must go forth into the world with enthusiasm for it and 
 try to draw others into an appreciation of it, doing his part to convince 
 the world that the study of nature is one of the most noble of pursuits, 
 that there are other things worthy of the attention of mankind besides 
 the pursuit of wealth. He must push forward and do what he can, ac- 
 cording to his ability, to further the" progress of his science. 
 
 Thus does the university, from its physical laboratory, send forth into 
 the world the trained physicist to advance his science and to carry to 
 other colleges and technical schools his enthusiasm and knowledge. 
 Thus the whole country is educated in the subject and others are taught 
 to devote their lives to its pursuit, while some make the applications to 
 the ordinary pursuits of life that are appreciated by all. 
 
 But for myself, I value in a scientific mind most of all that love of 
 truth, that care in its pursuit and that humility of mind which makes 
 the possibility of error always present more than any other quality. This 
 is the mind which has built up modern science to its present perfection, 
 which has laid one stone upon the other with such care that it to-day 
 offers to the world the most complete monument to human reason. This 
 is the mind which is destined to govern the world in the future and to 
 solve problems pertaining to politics and humanity as well as to inani- 
 mate nature. 
 
 It is the only mind which appreciates the imperfections of the human 
 reason and is thus careful to guard against them. It is the only mind 
 that values the truth as it should be valued and ignores all personal 
 feeling in its pursuit. And this is the mind the physical laboratory is 
 built to cultivate. 
 
ADDRESS AS PRESIDENT OF THE ELECTRICAL CONFER- 
 ENCE AT PHILADELPHIA, SEPTEMBER 8, 1884 
 
 [Report of the Conference, pp. 12-28, Washington, 1886] 
 
 To the student of science who has a disposition to look into the pages 
 of history, no life has greater interest than that of Archimedes, and yet 
 there are few men about whom so little is known. Living more than 
 two thousand years ago, the accounts of him which have come to us are 
 little short of fabulous, and yet they are of such a nature that we can 
 say without any doubt that he was a genius such as the world has sel- 
 dom seen. To him we owe some of the fundamental facts of mechanics, 
 such as the principle of the lever and the pulley, and the fact that a 
 body immersed in a liquid loses in weight as much as an equal volume 
 of the liquid weighs. And in military engineering his success was so 
 great that he prolonged the siege of Syracuse by the Romans from what 
 would probably have been a few days to three years. His engines shot 
 against the enemy immense numbers of darts and huge stones, which 
 mowed them down in columns, and falling on their ships destroyed 
 them. He thrust out huge beams from the walls over the ships and 
 drew them into the air, where they swung to and fro to the amazement 
 and terror of the Romans and were finally dropped and sunk to the bot- 
 tom of the sea. He is even said to have set them on fire by means of 
 the reflected light of the sun. But his principal work was in geometry, 
 and of this I only need to quote the words of Professor De Morgan re- 
 ferring to those geometrical works of Archimedes which have come 
 down to us. " Here," says Professor De Morgan, " he finds all that re- 
 lates to the surface and solidity of the sphere, cone and cylinder and 
 their segments. A modern work on the differential calculus would not 
 give more results than are found here." As to the quality of the indi- 
 vidual, the impression which his writings give us is that of a power 
 which has never been surpassed. No one has a right to say that New- 
 ton himself, in the place of Archimedes, could have done more. 
 
 Thus before the birth of modern science, in the dim ages of the past 
 when the light of history begins to fade and the mist of legend to cover 
 
620 HENEY A. ROWLAND 
 
 our view, there lived a man of almost superhuman intellect whose mind 
 seemed equally adapted to either pure or applied science. And yet Plu- 
 tarch says of him: "Archimedes possessed so high a spirit, so profound 
 a. soul, and such treasures of scientific knowledge, that, though the in- 
 ventions (referring to his military engines) had now obtained for him 
 the renown of more than human sagacity, he yet would not deign to 
 leave behind him any commentary or writing on such subjects, but, re- 
 pudiating as sordid and ignoble the whole trade of engineering, and 
 every sort of art that lends itself to mere use and profit, he placed his 
 whole affection and ambition in those purer speculations where there 
 can be no reference to the vulgar needs of life; studies, the superiority 
 of which to all others is unquestioned, and in which the only doubt can 
 be, whether the beauty and grandeur of the subjects examined, or the 
 precision and cogency of the methods and means of proof, most deserve 
 our admiration." 
 
 Here, then, at the dawn of science the question of the relative value 
 of pure and applied science had been brought up. To the people of 
 Syracuse, who had to defend themselves against an overwhelming enemy, 
 the military engines of Archimedes were of far more interest than the 
 whole of geometry, for the knowledge of the ratio of the solid contents 
 of a sphere and its circumscribed cylinder cannot bring a dead man to 
 life or restore wealth to a plundered city. And yet, from a point of 
 view distant more than two thousand years,, we are forced to admit that 
 Archimedes was right. Archimedes' engines of destruction have passed 
 away, but the geometrical and mechanical truths which he discovered 
 are to-day almost the axioms of the mathematician and the worker in 
 physical science, and the ratio of the circumference of a circle to its 
 radius is to-day the most important of our physical constants. 
 
 But this is only a meager part of the influence of this man. The 
 truths which he discovered have formed a part of the education of every 
 student of mathematics to the present time, and have given pure intel- 
 lectual enjoyment to all. They have helped to form the minds of all 
 those whom we consider great in our science, and they have done their 
 share in that march of progress which is gradually transforming the 
 world. 
 
 Great should be the honor in which we hold the intellect of Archime- 
 des, but greater should be our reverence when we approach that noble 
 spirit which could ignore all worldly considerations and prefer the truths 
 of geometry to the vast physical power given him by his other inven- 
 tions, which were his amusements for a moment. We now see that he 
 
ELECTRICAL CONFERENCE AT PHILADELPHIA 621 
 
 was right, but we cannot for a moment suppose that he foresaw, except 
 dimly, any so-called practical advantages from his discoveries. A thou- 
 sand times no! He preferred his geometrical labors because of a subtle 
 quality of his mind, an instinct toward that which was highest and 
 noblest and a faith that the pursuit of what is noble is the surest road 
 to the final happiness of the individual and of the world. Our highest 
 moral qualities are of this nature, and we despise as the lowest of the 
 low one who is honest because "honesty is the best policy," but esteem 
 him whose instincts lead him to honesty whatever the consequences. 
 
 So we reverence the noble and lofty spirit of Archimedes, and yet we 
 do not at the present day quite agree with his estimate of the relative 
 value of his works. His military inventions were far from worthy of 
 being despised, even though the only reason were that they gave the 
 world three more years of Archimedes' life. The world is not formed 
 of disembodied spirits, but of men, in whom there is a wonderful com- 
 bination of mind and matter, and a sound mind in a sound body is the 
 highest type of manhood. But we also know that the mind is hampered 
 by many considerations connected with the body. Archimedes recog- 
 nized this, and his noble spirit revolted at it. But to-day we see that 
 no progress can come from this method of treatment; the body still re- 
 mains, however much we may despise it, and the buzzing of a fly can 
 disturb the most profound thought of the philosopher. 
 
 We now study the laws of nature and seek thus to assist our bodies 
 in obeying the thoughts of our minds. Our railroads carry us hither 
 and thither on the earth with somewhat the facility of spirits, and our 
 thoughts pass with almost the speed of light to the uttermost portion 
 of the earth. The steam engine does our work, and labor-saving ma- 
 chinery takes the place of our hands. With a minimum amount of labor 
 we can to-day possess luxuries unknown even to kings in ancient times, 
 and our minds are free to study the order of nature or engage in any 
 intellectual pursuit we may desire. Instead of being the slaves of na- 
 ture and groveling in the dust before her to find the food which we 
 crave, we have now assumed the command, and find her a willing servant 
 to those who know her language. 
 
 But here we reach the keystone of the problem. To command her we 
 must know her language. Knowledge, then, is the price of her service, 
 and she obeys not the ignorant or degraded, but grinds them into dust 
 beneath her heel. 
 
 Knowledge, then, is power, and it is more than power; it is that 
 which the intellect most craves and is the object of many of our highest 
 
622 HENEY A. ROWLAND 
 
 aspirations. What truth is, is the goal of intellectual mankind in all 
 ages, and its pursuit leads not only to intellectual but also to physical 
 satisfaction. 
 
 The pursuit of the one leads to the other., and we shall see as we pro- 
 ceed that the only way for the world to progress in practical science is 
 by the cultivation of the theoretical science. 
 
 Pure science must exist before its applications, and the truths of pure 
 science are far more reaching in their effects than any of its applica- 
 tions; and yet the applications of science often have a much more im- 
 mediate interest for the world at large than many discoveries in pure 
 science, which will finally revolutionize it, both physically and mentally. 
 They both have their importance and both are at work in causing that 
 intellectual and material progress in which the world is now pushing 
 forward with giant steps. But there is this difference the names of the 
 great inventors are seen in every paper and their deeds are recounted 
 to the rising youth of the country as examples to be followed. And 
 yet the discoveries of the principles on which their inventions are based 
 may have died in comparative obscurity, with poverty knocking at the 
 door. We are in no danger of forgetting those who have been success- 
 ful in those applications of science which are in daily use, and it is use- 
 less to repeat the story of the telegraph or telephone, but it will be of 
 more interest for me to recall to your minds a few of the landmarks in 
 our science and then to consider the present state of our science, with 
 a possible glance into the future. 
 
 Thus we shall obtain a clearer view of how our science has been built 
 up and of the means which are necessary for its further progress. We 
 shall also see the relations between pure and applied science, and the 
 relative importance of the two in the progress of the world. 
 
 It is impossible for one here to discuss the reasons why the ancients 
 followed their science to so short a distance and the world had to wait 
 more than two thousand years before the light of modern science com- 
 menced to shine. It must be left to the psychologists and historians. 
 But this I may say, modern progress is cumulative. By the study of 
 the science of the past, the minds of men are trained for its further ad- 
 vance in the future, and so when there was no science to study there 
 could be but little training of the mind in the true methods of thought. 
 
 The average intellect of mankind has improved, and what could only 
 have been comprehended in past times by a few is to-day understood 
 by the majority of educated persons. And this increase has been most 
 apparent in the reason and moral sense of mankind, the two qualities of 
 
ELECTEICAL CONFERENCE AT PHILADELPHIA 623 
 
 the mind which come most into play in the study of science. To the 
 mind of the ancients, where the imagination ran riot without the guide 
 of reason or a warning from their moral sense to speak the truth, it was 
 easier to attribute the attraction of rubbed amber to an inherent soul 
 or essence, which, awakened by friction, went forth and brought back 
 the small particles floating around, than to examine and find out the 
 truth. 
 
 The simple experiment of the amber remained without investigation 
 for 2200 years. Had the reasoning of many modern persons been fol- 
 lowed, we should never have had a science of electricity. Why should 
 anybody investigate this phenomenon, this feeble force, which could 
 only attract a few particles of dust? The world could eat, drink, and 
 take its ease without doing anything in the matter, and it did so for 
 more than "two thousand years of intellectual, moral and physical degra- 
 dation. Then the awakening came, and men began to feel that they 
 were reasoning beings. They began to see that there were other pleas- 
 ures in the world besides animal pleasures, and that they had been placed 
 in this wonderful universe that they might exalt their intelligence by its 
 proper study. No question of gain entered into the minds of these 
 early investigators, but they were led by that instinct toward truth which 
 indicates the highest type of man. And yet their researches have trans- 
 formed the world, not only intellectually, but physically. Some would 
 say that science had been degraded by its applications, but who that 
 looks over the world at the present time can think so? There is no 
 danger of this view becoming general; the danger is in the other 
 direction, and that science shall be degraded in the estimate of the 
 world by the idea that its principal use is to be applied to the common 
 purposes of life. A thousand times no! Its use is in the intellectual 
 training of mankind and the high and noble pleasure it gives to those 
 who are born to understand it; to lift mankind above the level of the 
 brute and to make him appreciate the beauties and wonders of nature; 
 to cause him to stand in humiliation and awe before that universe 
 which the intellect of ages has attempted to understand and yet has 
 failed; to make even Newton say, " I know not what the world may 
 think of my labors, but to myself it seems to me that I have been but 
 as a child playing on the seashore; now finding some pebble rather more 
 polished, and now some shell rather more agreeably variegated than 
 another, while the immense ocean of truth extended itself unexplored 
 before me." 
 
 But the great moral law of the universe here enters. If the world 
 
624 HENKY A. EOWLAND 
 
 would only pursue those things which are high and right and noble its 
 reward would not be confined to the minds of men. Physical rewards 
 await it as well, and disease, that principal cause of human misery, 
 would almost pass away when the effect of inheritance from the present 
 generation had passed. So the pursuit of pure science brings not only 
 the rewards I have mentioned,, but the physical rewards of applied 
 science and the pursuit of applied science gives wealth which may be 
 again employed to further pure science. So the two react on each other 
 to produce that perfect whole, modern science, pure and applied. 
 
 This moral law of the universe is well illustrated by the well-known 
 story of Solomon: 
 
 " The Lord appeared to Solomon in a dream by night; and God said, 
 Ask what I shall give thee. 
 
 "And Solomon said, Thou hast made thy servant king instead of David 
 my father, and I am but a little child; I know not how to go out or come 
 in. Give therefore thy servant an understanding heart to judge thy 
 people, that I may discern between good and bad; for who is able to 
 judge this thy so great a people? 
 
 "And God said unto him, Because thou hast asked this thing, and hast 
 not asked for thyself long life, neither hast asked riches for thyself, nor 
 hast asked the life of thine enemies, but hast asked for thyself under- 
 standing to discern judgment, behold, I have done according to thy 
 words; lo, I have given thee a wise and an understanding heart, so that 
 there was none like thee before thee, neither after thee shall any arise 
 like unto thee. And I have also given thee that which thou hast not 
 asked, both riches and honor; so that there shall not be any among the 
 kings like unto thee all thy days." / 
 
 So the world, when it chose knowledge and truth above all things, 
 acquired not only the treasures of pure theoretical science, but also the 
 wealth and riches and honor which come from applied science such as 
 the world has never seen before and could see in no other way. 
 
 It is to William Gilbert, an English physician, that we owe the com- 
 mencement of the modern science of electricity. His book on the mag- 
 net was published in 1600, and contained his electrical experiments. 
 Thus, at this early date, the similarity of electrical to magnetic attrac- 
 tion was recognized. But how slowly did the subject advance! The 
 difference between conductors and non-conductors was discovered by 
 Gray. But not until 1746, 150 years after Gilbert, was the Leyden jar 
 invented. Then the remarkable nature of the phenomenon became ap- 
 parent, and the world was startled by it. The subtle spirit which went 
 
ELECTRICAL CONFERENCE AT PHILADELPHIA 625 
 
 forth from the amber, which was so feeble as only to attract dust, now 
 flashed forth with light and sound and heat, and could cause the strength 
 of the giant to vanish. To the world at large there was now something 
 worth looking into. But do we think that the spark from the Leyden 
 jar is more wonderful than the gentle attraction of the amber? By no 
 means, for, to the scientist, they are both equally remarkable, and be- 
 yond our powers of explanation. It is only to the vulgar and unedu- 
 cated taste that the tinsel and gewgaws of an electric spark appeal more 
 strongly than the subtle spirit of the amber. Nevertheless, despicable 
 as the means, the spark of the Leyden jar acted as a trumpet call to 
 Europe and even America to come to the study of the wonderful science 
 of electricity. At no other time has there been such excitement over 
 any electrical discovery, and electrical experiments became general. 
 
 It was only after the discovery of the Leyden jar that the idea of an 
 electric current occurred to mankind, and this current was even trans- 
 mitted to a distance by a wire and a shock given to a person across the 
 Thames, the water forming the return circuit. And the English ex- 
 perimenters even went so far as to form a circuit with the two observ- 
 ers two miles apart, using the earth as the return circuit. Thus the 
 fundamental fact which forms the basis of the telegraph was early ob- 
 served. 
 
 But isolated facts are of little value unless connected together by 
 something which we call a theory, and in this line we owe much to 
 Franklin, whose letters upon this subject appeared between 1747 and 
 1754. To him we owe the theory of positive and negative electricity, 
 and the fact that they are always generated in equal amounts, a law 
 whose importance can scarcely be estimated. He investigated the Ley- 
 den jar, and showed that the coatings had equal positive and negative 
 charges, and explained the fact that the jar cannot be charged when 
 the outside coating is insulated. He invented the charge and discharge 
 by cascade and showed that it was the glass of the jar and not the 
 coatings which contained the charge. He discovered the property of 
 points in discharging an electrified body, and the identity of lightning 
 with electricity. He also made the first experiments upon atmospheric 
 electricity. 
 
 To Canton is due the honor of giving the first experiments on induc- 
 tion, but Franklin is the first who gave the general law of this species 
 of action. Truly our country and this city should honor the memory 
 of this man. 
 
 But it is not my purpose to repeat to you in detail the familiar history 
 40 
 
 
626 HENRY A. EOWLAND 
 
 of our science. Thus far no important applications of electricity had 
 been discovered; there was nothing but pure science to attract inves- 
 tigators, and thus the science remained for many years after. 
 
 But no science is complete unless it is quantitative as well as quali- 
 tative. It is now very nearly one hundred years since Coulomb laid 
 the foundation of electrostatics and Aepinus and Cavendish commenced 
 to lay the foundation of mathematical electricity, and they were fol- 
 lowed by Laplace, Biot, Poisson, and Murphy. 
 
 The discoveries by Galvani and Volta in 1790 and 1800, and by 
 Oersted in 1820, gave us the galvanic battery and electro-magnetism, 
 and it was not until the latter date that any useful practical application 
 was possible. Then, so complete was the science that no factor of other 
 than minor importance was necessary to transmit intelligence from one 
 extremity of the earth to the other. 
 
 By the labors of the immortal Faraday, electro-magnetic induction 
 was discovered and the modern dynamo-electric machine became a cer- 
 tainty. 
 
 To his other labors, both experimental and theoretical, the modern 
 science of electricity owes much, but it is familiar to all. The name of 
 Faraday needs no eulogy from me, for it stands where it can never be 
 hidden, and the spark which Faraday first kindled now dazzles us at 
 every street corner. No wealth came to him, though he had only to 
 hold out his hand for it. But the holding out of one's hand takes time, 
 which Faraday could not spare from his labors, and so the wealth which 
 was rightly his went to others. Who will follow in his footsteps and 
 live such a life that the thought of it almost fills one with reverence? 
 It is not only his intellect which we admire; it is his moral qualities 
 which fill us with awe his noble and unselfish spirit. 
 
 The name of Faraday brings us down to modern times, whose history 
 it is unnecessary to repeat in detail, especially as there are some now 
 present who have contributed largely to bring the science to its present 
 perfection. 
 
 One of the principal features which we remark in our modern science 
 of electricity is the perfection of our means of measuring both electrical 
 and magnetic quantities. In this connection the great names of Gauss 
 and Weber appear, the fathers of the modern absolute system of elec- 
 trical and magnetic measurement, and that of Sir William Thomson, 
 in no less degree distinguished. On the laws of electric attraction we 
 base our electrostatic system of measurement, and on the magnetic ac- 
 tion of the current, the great discovery of Oersted, we base our electro- 
 
ELECTRICAL CONFERENCE AT PHILADELPHIA 627 
 
 magnetic system, and we connect these two systems by that great physi- 
 cal constant, the ratio of electro-magnetic to the electrostatic system of 
 units. 
 
 What can be simpler in theory than the electrostatic system, based, 
 as it is, on the law that electric attraction varies inversely as the square 
 of the distance? We only have to know how the electricity is dis- 
 tributed and its attraction is known. Hence we must select the simplest 
 possible case, such as two parallel disks, and to render the problem cal- 
 culable, we add a guard ring to the movable disk. We then have the 
 absolute electrometer of Thomson. This gives us a measure of the 
 electric potential. Knowing the capacity and difference of potential 
 of the surface of a condenser, we know its charge. But all these quan- 
 tities, the calculation of the electrometer and the capacity of the con- 
 denser, depend upon the mathematical theory of electric distribution. 
 Are we able to calculate the capacity of condensers of all forms? I am 
 sorry to say we are not. The modern method of treatment is due to 
 George Green, an English investigator, whose name should be held in 
 honor by all electricians. But this method is what is called an inverse 
 one. It is not a method by which we can calculate the distribution 
 on any body at random, but the shape of the body and the electrical 
 distribution on it are both found at once by a species, as it were, of 
 exploration and discovery. So that we cannot make our electrometers 
 and condensers of any shape and then calculate them, but we are forced 
 to make them of some simple geometrical form whose solution is 
 known. We fit our apparatus to the mathematics rather than the mathe- 
 matics to the apparatus. 
 
 But when we have satisfied all the conditions we measure out our 
 static charges as easily as a quantity of matter. The manufacturer sells 
 the oxygen and hydrogen in iron cylinders and determines the amount 
 by the product of the capacity of the cylinders by the pressure. Were 
 there any buyers of electricity we might sell them a Leyden jar full and 
 determine the amount by the product of the capacity of the jar by the 
 electric potential. According to this analogy, then, the electricity is 
 similar to matter and the potential fluid pressure, while the word ca- 
 pacity has a similar meaning in both. 
 
 In the electro-magnetic method of electrical measurement we make 
 use of the magnetic action of the current, either on a neighboring mag- 
 net or another current or portion of the same current. The laws of the 
 action of a current on a magnet were discovered by Biot and Savart, 
 and of two currents on each other by Ampere, and the results applied to 
 
628 HENKY A. ROWLAND 
 
 practical measurement to-day give us galvanometers of all kinds and 
 the electro-dynamometer of Weber. By the galvanometer we can meas- 
 ure the quantity of electricity passing at any moment, but by the elec- 
 tro-dynamometer we measure the integral square of the current, a 
 quantity on which the heating of the circuit and the energy expended 
 depend. 
 
 Thus the electro-dynamometer measures the energy from an alternat- 
 ing current dynamo-electric machine as easily as from one giving a con- 
 tinuous current, but to know this energy we must know something else 
 besides the integral square of the current, and this is either the resist- 
 ance of the circuit or the electromotive force. But the measurement of 
 electromotive force depends on a resistance. The question then comes 
 up as to what unit of resistance is the proper one. Here we have to 
 refer to the mathematical theory of the subject, and the great law of the 
 conservation of energy tells us that what is known as the absolute unit 
 of electrical resistance is the proper one for use in this case. Hence 
 the great practical use of determining this unit. The experiments of 
 Kirchhoff, Weber, Kohlrausch, and the British Association found a 
 value from 1 to 3 per cent too large. 
 
 Many years ago I myself experimented on the subject, and obtained 
 a result about 4 per cent too high. Recently Lord Rayleigh has taken 
 up the matter and made a series of experiments of unparalleled accu- 
 racy in this line. The International Commission, determined on by the 
 Electrical Congress in Paris in 1881, met in April of this year at Paris, 
 and has now given us a legal ohm defined as being the resistance of a 
 column of mercury 106 centimetres long and 1 millimetre in section at 
 C. The length best satisfying the experiments is about 106-25, but 
 it was considered best to use the round number. The experiments 
 which I have been making under an appropriation from the Government 
 are now barely completed, but they will probably agree very well with 
 the latter figure. Hence, we can say that we now know this unit of 
 resistance to one part in one thousand, at least. And so we are in a posi- 
 tion to measure the energy of a current to the same degree of accuracy, 
 as far as this quantity is concerned. 
 
 But to measure a current by the tangent galvanometer one requires 
 to know the intensity of the earth's magnetism, a quantity difficult to 
 determine and constantly varying with time and place. The electro- 
 dynamometer, when made with care, is excellent, but a good one is im- 
 mensely expensive. Our methods, then, of current measurement are 
 bad, unless carried out in a completely equipped physical laboratory. 
 
ELECTRICAL CONFERENCE AT PHILADELPHIA 629 
 
 With a practical standard of electromotive force, such as a Clark's 
 standard cell or a thermo-electric battery, this difficulty partially van- 
 ishes. Better, perhaps, we might make simple electro-dynamometers 
 with constants determined by comparisons with a more costly instru- 
 ment. 
 
 But where shall these standards be kept? Evidently the Govern- 
 ment, which decides on our standards of weights and measures, should 
 take in charge the electrical standards, and possibly also the thermo- 
 metric standards. The formation of such a Bureau of Physical Stand- 
 ards will be brought to the attention of this Conference. 
 
 Having given certain standards then, the measurement of currents 
 and current energy becomes easy. The amount of heat generated in a 
 wire of known resistance by a known current is also easily found from 
 the absolute system of electrical measurement. 
 
 Besides the two so-called absolute systems of measurement of elec- 
 tricity and electric currents, we have also one based on the chemical 
 action of the current whose laws were discovered by Faraday. Know- 
 ing the electro-chemical equivalent of some substance, we are able to 
 measure the time integral of the current or the total quantity of the 
 current which has passed. 
 
 The absolute measurement of magnetism is equally simple with that 
 of electricity, and it is a common observation to find the earth's magnetic 
 force. But Faraday has put in our hands a very simple method of meas- 
 uring a magnetic field, and to-day all are familiar with his beautiful 
 laws with respect to magnetic lines of force. We know the laws of 
 electro-magnetism, and just how many lines of force (better induction) 
 can pass through a piece of iron of given cross-section, and what is their 
 relative resistance when passing through air or iron. In fact, we have 
 all that is necessary for a complete theory of the dynamo-electric ma- 
 chine, and consequently we find that the latter agrees perfectly with 
 theory, and no fact has been observed with reference to it which could 
 not have been foreseen from theory by a person of proper intelligence. 
 
 This part of electrical science, the measurement of electrical and mag- 
 netic quantities, is thus in a very forward state, based, as it is, on the 
 mathematical theory of the subject. But, in reality, this forms but a 
 very small portion of our science. Shall we be contented with a simple 
 measurement of that of which we know nothing? I think nobody would 
 care to stop at this point, although he might be forced to do so. The 
 mind of man is of a nobler cast, and seeks knowledge for itself alone. 
 We are not so base as to be honest because " Honesty is the best policy," 
 
630 HENRY A. KOWLAND 
 
 neither are we so ignoble as to seek knowledge because " Knowledge is 
 power " two sayings which are certainly true, but low and sordid in 
 their tone. 
 
 We have, then, the beautiful fabric of mathematical electricity given 
 to the world by Poisson, Green, Helmholtz, Thomson, Maxwell, and 
 others whose names are immortal. No hypothesis as to the nature of 
 electricity rests at its base. Starting from the most simple laws of 
 electricity and magnetism, it rises from a stable foundation and rears 
 its form high in the air, never to be overturned, whatever the fate of 
 the so-called electric fluid or the ultimate theory of magnetism. On the 
 simple fact that there is no electric force inside a closed conductor, it is 
 proved that the electric attraction and repulsion varies inversely as the 
 square of the distance. The fact is sufficient to give us the whole theory 
 of electrostatic distribution on conductors. 
 
 From the simple fact that we can break a magnet up into parts which 
 are similar to each other, and that these parts attract and repel each 
 other in a certain manner, we derive many important facts with regard 
 to magnetism. 
 
 From the magnetic action of the current we find, by an application of 
 the great law of conservation of energy, all the laws of induced cur- 
 rents, either from magnets or other currents. By an almost superhu- 
 man effort of the intellect we detach our electric currents from matter, 
 and suppose them to take place in the ether of space, and we have the 
 grand electro-magnetic theory of light given to us by Maxwell. 
 
 But the subject is too vast to be treated in a moment. Suffice it to 
 say that no person at the present day has the right to express an opin- 
 ion on any theoretical question connected with electricity without a 
 knowledge of its mathematics. 
 
 This study has led us to alter our ideas on many questions. What 
 is the mechanism of electri'c or magnetic attraction? Faraday has 
 given us his idea of lines of force, and has made them play an important 
 part in the theory of magnetic induction. When treated mathemati- 
 cally, Maxwell has shown that all electric and magnetic attractions can 
 be explained by a tension along the lines of force and pressure at right 
 angles to them an idea due to Faraday. 
 
 The mathematical theory of these lines shows that all electrostatic 
 forces between either conductors or non-conductors can be explained in 
 this manner. As the laws of magnetic attraction are the same in every 
 way as electrostatic attraction, if we should do away with electric con- 
 duction, it follows that magnetic attraction is to be explained in exactly 
 
ELECTRICAL CONFERENCE AT PHILADELPHIA 631 
 
 the same manner. In obtaining this result Maxwell calculated the 
 forces acting on the medium at every point, and compares these with 
 imaginary stresses in a medium at the given point. Hence, the energy 
 stored up can be represented either as due to the mutual attraction of 
 the electricity at a distance, or to the stresses in the medium at every 
 point, and thus, as Thomson has shown, by a volume integral of the 
 square of the force at every point. Hence, we are at liberty to deny 
 the existence of all action at a distance, and attribute it to the inter- 
 vening medium, which, to be logical, we must assume to be continuous 
 and not molecular in constitution. 
 
 Thomson has pointed out that magnetism must be of the nature of ro- 
 tation, such as possibly vortex motion in a fluid, and Maxwell has done 
 something toward making a mechanical model of such a medium. Thom- 
 son's wonderful address at Montreal has also given us much to think of 
 in the same direction. 
 
 But here we have reached the limit of our science, and even that serv- 
 ant of our reason, imagination, fails us. We are yet unable to picture 
 to ourselves what takes place in a medium subject to electrostatic ac- 
 tion. We are face to face with the great problem of nature, and the 
 questions, What is matter? What is electricity? evoke no answer from 
 the wisest among us. Our mathematics has guided us safely up to a 
 certain point and will guide us still further; science will advance and 
 we shall know more. But, for the present, this is the limit which we 
 have yet attained in this direction. However, the idea of a medium is 
 still serviceable in other portions of our science. 
 
 We have seen that the medium explains the electrical and magnetic 
 attraction of bodies at rest. The question then comes up as to what 
 happens in the medium when these bodies move. Are the imaginary 
 stresses in the medium transmitted from place to place instantaneously 
 or do they require time? Mathematics in the hands of the immortal 
 Maxwell has answered this question, and we now know that any mag- 
 netic or electric distrubance is propagated through space with a velocity 
 equal to the ratio of the electro-magnetic to the electrostatic unit of 
 electricity. This great physical constant has now been found by experi- 
 ment to be equal to the velocity of light, and thus has arisen that great 
 modern theory, Maxwell's electro-magnetic theory of light. Indeed, at 
 the present day, so perfectly does this theory agree with experiment that 
 we can almost regard it as a certainty. The velocity of light and the 
 ratio of the units agree far within the limits of experimental error. The 
 fact that bodies having a true (not electrolytic) electric conduction are 
 
632 HENRY A. KOWLAND 
 
 always more or less opaque, the refraction and dispersion of light, dou- 
 ble refraction, and diffraction, all are explained on this theory with an 
 ease and simplicity wanting in all other theories; and, lastly, an elec- 
 tro-magnetic phenomenon has been discovered, which, when applied to 
 this theory of light, explains the rotation of the plane of polarization 
 produced by a magnet. There is no fact in nature seriously in disagree- 
 ment with this theory, and it serves to connect two of our most impor- 
 tant branches of physics, light and electricity. 
 
 But some physicists say that it is not a true theory, because it is not 
 mechanical, the object of these physicists being to reduce every phe^ 
 nomenon of nature to matter and motion. Whether this is necessary or 
 not I leave to the philosophers. But it is to be noted that the old me- 
 chanical theory that light is a vibration in a medium having the prop- 
 erties of an elastic solid is not entirely at variance with the new theory. 
 The medium we call ether. The electro-magnetic theory says that 
 the waves of light are waves of electric displacement, while the old 
 theory says they are waves of ether. Make electricity and the ether 
 equal to each other and the two theories become one. We have arrived 
 at that hazy and unsatisfactory theory of Edlund that ether and elec- 
 tricity are one, except that by this theory electricity is presented to us 
 as an elastic solid! 
 
 But the ground trembles beneath us, and we shall soon be plunged in 
 the mire of vague speculation if we do not draw back. 
 
 Among the other questions which depend for their solution on the 
 presence of a medium may be mentioned the mutual action of two elec- 
 trified bodies moving in space. It has been found that electricity car- 
 ried through space on a charged body has exactly the same magnetic 
 effect on a stationary magnetic needle as if it had been conducted. 
 
 But when electrified bodies move uniformly forward in space, we can 
 conceive of no mutual effect from such motion unless it is relative to a 
 medium, for we cannot even conceive of absolute motion. 
 
 Assuming the medium to exist, we then know that a positively and a 
 negatively charged body flying through space with the velocity of light 
 would have their electric attraction just balanced by their magnetic re- 
 pulsion, and so would exert no force on each other. 
 
 But it is a most wonderful fact that we have never been able to dis- 
 cover anything on the earth by which our motion through a medium 
 can be directly proved. Carried, as we suppose, by the earth with im- 
 mense velocity through regions of space filled with ether, we have never 
 yet been able to prove any direct influence from this ethereal wind. 
 
ELECTRICAL CONFERENCE AT PHILADELPHIA 633 
 
 The assumption of a medium allows us to solve in some cases that 
 problem so long under discussion by electricians namely, the true ve- 
 locity of an electric current. We now know that the term velocity 
 hardly applies to this case, and that the current arrives at different 
 points so gradually that we know not when to say it has arrived. But 
 there is certainly a minimum time when even an infinitesimal current 
 can reach a distant point. Suppose two wires stretched in space with 
 their ends near together at one end and a Leyden jar be discharged from 
 one to the other at the near end. The minimum possible time of obtain- 
 ing a spark at the distant end will evidently be the time required by 
 light to pass from the Leyden jar to the distant point, not around the 
 wire, but in a straight line. In this case the greatest maximum velocity 
 is thus twice that of light reckoned around the wire, and may be any 
 amount greater when we bend the wire. For all ordinary distances this 
 velocity may be considered infinite, and the retardation to depend 
 only on the electrostatic capacity and magnetic self-induction of the 
 wire. Treated in this way, we have Thomson's mathematical theory 
 of the propagation of an electric wave along a telegraph wire or cable, 
 a theory of great practical use in telegraphy and telephony. But until 
 the action in the external medium is also taken into account, it can only 
 be considered an approximation. For we can never move a magnet, 
 discharge a Leyden jar, or complete the circuit of a battery, without 
 causing a wave of electro-magnetic disturbance in the ether, and every 
 signal which is sent along a telegraph line is accompanied by a wave in 
 the ether, which travels outward into space with the velocity of light. 
 Truly the idea of a medium is to-day the keystone of electrical theory, 
 but we can hardly suppose that it has even yet attained a fraction of 
 the importance to which it is destined to rise. 
 
 Let me now call your attention to one of the most wonderful facts 
 connected with electrical science. When we are dealing with the elec- 
 trostatic action of electricity, we find that it is the so-called electric fluid 
 which attracts the opposite. Not only do we observe the attraction of 
 bodies oppositely charged, but the electricity itself on the two bodies is 
 displaced by its mutual action. But when we come to investigate the 
 mutual attraction or repulsion of electric currents on each other, we find 
 an entirely different law. In this case the conductors carrying the cur- 
 rents attract or repel each other, but the currents within those con- 
 ductors have no influence of attraction or repulsion to displace them- 
 selves within the body of the conductor. In other words, the current 
 is not displaced by the action of a neighboring magnet, but flows on 
 calmly as if it were not present. 
 
634 HENEY A. KOWLAND 
 
 This to me is one of the most wonderful facts in electrical science, and 
 lies at the foundation of our science. It cannot be ignored in any fur- 
 ther progress we may make in electrical theory, but points out a radical 
 difference between electrostatic and electro-magnetic action. 
 
 I have said there is no action of a magnet in displacing an electric 
 current, and have thus stated the broad general fact, and which is per- 
 fectly true in some metals. But in others there is a small action which 
 changes in direction with the material. The elements of the electric 
 current within the material are rotated around the lines of magnetic 
 force, sometimes in one direction and sometimes in the other, according 
 to the material. But the action is, in all cases, very weak. When ap- 
 plied to the electro-magnetic theory of light, this action leads to the 
 magnetic rotation of the plane of polarization of light. As to the ex- 
 planation of both these actions, Thomson has remarked in the case of 
 light, from dynamical considerations, the rotation can only come from a 
 true rotation of something in the magnetic field, and leads us to think of 
 all magnetic action as of the nature of vortex motion in a fluid. But 
 here our theory ends for the present. We have obtained a clew, but it 
 is not yet worked up. 
 
 I have now taken a rapid glance at some of the modern advances of 
 electrical science, and we have not yet had to give up the old idea that 
 electricity is liquid. To the profound thinker this idea is very vague, 
 and there are some facts at variance with it, but it is still useful. We 
 often hear persons say that this old idea is gone, and that electricity is 
 " force," whatever they may mean by that. But let us see. The work 
 or energy of an electric current between any two points is the quantity 
 of electricity passed multiplied by the potential; this work goes to 
 heating the wire. Let a curient of water be passing in a pipe, and the 
 quantity of water multiplied by the difference of pressure between two 
 points gives us the work which has been done in the intervening space, 
 and which has produced heat. The analogy is complete. No electricity 
 has been destroyed in the one case, or water in the other, but the work 
 has come from the fall of potential in the one case, and the fall of 
 pressure in the other; the resultant is the same in both heat. Again, 
 we can obtain work from the mutual attraction and repulsion of elec- 
 trified bodies, and the work in this case always comes from the change 
 of potential between the bodies while the electric charges remain undis- 
 turbed in quantity. Electricity, then, is not energy, but is more of the 
 nature of matter. 
 
 So far for electricity in the state of rest or steady flow. But when it 
 
ELECTRICAL CONFERENCE AT PHILADELPHIA 635 
 
 changes from rest to motion, all known liquids have a property known 
 as inertia; furthermore, they have weight. But the electric fluid has 
 neither inertia nor weight as far as we have yet experimented, and in 
 this respect differs from all known matter. Furthermore, we have never 
 yet been able to separate electricity from ordinary matter. When we 
 pass electricity through a vacuum, the resistance becomes less and less, 
 and one may have hopes of finally having an electric current through a 
 vacuum. But, as the exhaustion proceeds, we observe that the resist- 
 ance begins to increase until it reaches such a point that no discharge 
 can take place. Electricity cannot exist, then, without matter, a fact 
 fatal to the idea of a fluid, however useful that may be. We have but 
 one conclusion from this, and that is that electricity is a property of 
 matter. Do with it what we may, it can never be separated from matter, 
 and when we have an electrical separation the lines of force must always 
 begin and end in matter. 
 
 The theory of matter, then, includes electricity and magnetism, and 
 hence light; it includes gravitation, heat, and chemical action; it forms 
 the great problem of the universe. When we know what matter is, 
 then the theories of light and heat will also be perfect; then and only 
 then, shall we know what is electricity and what is magnetism. 
 
 It is the problem of the universe which looms up before us and before 
 which we stand in awe. The intellect of the greatest among us appears 
 but feeble and we all, like Newton, appear but as children on the sea- 
 shore. But how few of us find the shells which Newton did. and how 
 few of us try. The problem is vast and the means for its solution must 
 be of corresponding magnitude. Our progress so far has been but small. 
 AY hen we push our inquiry in any direction we soon reach a limit; the 
 region of the unknown is infinitely greater than the known, and there 
 is no fear of there not being work for the whole world for centuries to 
 come. As to the practical applications which await us, the telegraph, 
 the telephone, and electric lighting are but child's play to what the 
 world will see in the future. 
 
 But what is necessary to attain these results? We have seen how the 
 feeble spirit, which was waked up by friction in the amber and went forth 
 to draw in light bodies, has grown until it now dazzles the world by its 
 brilliancy, and carries our thoughts from one extremity of the world to 
 the other. It is the genius of Aladdin's lamp which, when thoroughly 
 roused, goes forth into the world to do us service, and returns bearing 
 us wealth and honor and riches. But it can never be the servant of an 
 ignorant or lazy world. Like the genius of Aladdin's lamp it appeared 
 
636 HENRY A. ROWLAND 
 
 to the world when the amber was rubbed, but the world knew not the 
 language in which to give it orders, and was too lazy to learn it. The 
 spirit of the amber appeared before them to receive its orders, but was 
 only gazed at in silly wonder, and retired in disgust. They had but to 
 order it and it would have gone to the uttermost parts of the earth with 
 'almost the velocity of light to do their bidding. But in their ignorance 
 they knew not its language. For two thousand years they did not study 
 it, and when they then began to do so it took them two hundred and fifty 
 years to learn the language sufficiently to make a messenger of it. And 
 even now we are but children studying its ABC. It is knowledge, 
 more knowledge, that we want. 
 
 I have briefly recounted the advances which we have now made in 
 one science, and, however beautiful it may appear, we have soon reached 
 the limit of the known, and have stood in wonder before the vast un- 
 known. For very much of our science we see no practical applications, 
 but we value it no less on that account. We study it because we have 
 been gifted with minds whose exercise delights us, and because it seems 
 to us one of the highest and noblest of employments. And we know by 
 the history of the past that the progress of the world depends on our 
 pursuit, and that practical applications, such as the world has never even 
 conceived of, await us. It is necessary that some should go before to 
 clear the way for the world's advance. 
 
 This is the work of the pure scientist; to him the problem of the uni- 
 verse is worth devoting his life, and he looks upon wealth as only add- 
 ing to his means of research. He hopes not to solve the problem him- 
 self, but is contented if he may add some small portion to human knowl- 
 edge; if he may but do his part in the march of human progress. He 
 looks not for practical applications, but he knows full well that his most 
 abstruse discoveries will finally be made useful to mankind at large, and 
 so troubles himself no further about it. 
 
 The science which he creates is studied by others. Their minds are 
 educated by it and their hearts entranced by its beauties. And some 
 are led to devote their lives to its further advancement. But the whole 
 world benefits by it intellectually. The wayward spirit of the amber 
 has vanished forever, and prosaic, law-abiding electricity has taken its 
 place even in the estimation of the most ignorant. The world has ad- 
 vanced, and in great part from the study of science. 
 
 Then comes the practical man, who sees that other benefits can be 
 reaped besides those of pure intellectual enjoyment. While the inves- 
 tigator toils to understand the problem of the universe, the practical 
 
ELECTKICAL CONFERENCE AT PHILADELPHIA 637 
 
 man seeks to make a servant of our knowledge. He seeks to increase 
 the power of our bodies and to make the bonds by which the mind is 
 united to it less irksome. It is he that increases the wealth of the world, 
 and thus allows those so disposed to cultivate their tastes and to elevate 
 themselves above the savages. The progress of the world depends upon 
 his inventions. 
 
 Let not, then, the devotee of pure science despise practical science, 
 nor the inventor look upon the scientific discoverer as a mere visionary 
 person. They are both necessary to the world's progress and they are 
 necessary to each other. 
 
 To-day our country, by its liberal patent laws, encourages applied 
 science. We point to our inventions with pride, and our machinery in 
 many of the arts is not surpassed. But in the cultivation of the pure 
 sciences we are but children in the eyes of the world. Our country has 
 now attained wealth, and this wealth should partly go in this direction. 
 We have attained an honorable position in applied science, and now let 
 us give back to the world what we have received in the shape of pure 
 science. Thus shall we no longer be dependent, but shall earn our own 
 science as well as inventions. 
 
 Let physical laboratories arise; let men of genius be placed at their 
 head, and, best of all, let them be encouraged to pursue their work by 
 the sympathy of those around them. Let the professors be given a 
 liberal salary, so that men of talent may be contented. Let technical 
 schools also be founded, and let them train men to carry forward the 
 great work of applied science. 
 
 Let them not be machines to grind out graduates by the thousand, 
 irrespective of quality. But let each one be trained in theoretical 
 science, leaving most of his practical science to be learned afterward, 
 avoiding, however, overtraining. Life is too short for one man to know 
 everything, but it is not too short to know more than is taught in most 
 of our technical schools. It is not telegraph operators, but electrical 
 engineers that the future demands. 
 
 Such a day has almost come to our country and we welcome its ap- 
 proach. 
 
 Then, and not till then, should our country be proud and point with 
 satisfaction to her discoveries in science, pure and applied, while she 
 has knowledge enough to stand in humiliation before that great undis- 
 covered ocean of truth on whose shores Newton thought he had but 
 played. 
 
THE ELECTEICAL AND MAGNETIC DISCOVERIES OF 
 
 FARADAY 
 
 ADDRESS AT THE OPENING OF THE ELECTRICAL CLUB HOUSE OF 
 NEW YORK CITY, 1888 
 
 [Electrical Review, New York, Feb. 4, 1888] 
 
 In the progress of all sciences there are epochs when men, thoroughly 
 fitted by nature, if not by education also, for the most successful study 
 and advancement of their science, are born into the world, and by their 
 natural talent, perseverance and love of their science, give it an impetus 
 which stamps their name forever on its history. But, however great 
 they may be, we know enough of the nature of scientific progress to be 
 sure that there never was one of such greatness as to be absolutely neces- 
 sary to human progress. The world would never have stood still on 
 account of the absence of any name from its annals, and even the place 
 of the immortal Newton would sooner or later have been filled by others, 
 and all the discoveries of his " Principia " have been known to us now, 
 even had he never existed. 
 
 Discoveries, then, have their origin not only in the presence of men 
 of exceptional genius in the world, but in a true and overwhelming 
 progress of science which marches forward to the understanding of the 
 universe, irrespective of the efforts of any single individual to promote 
 or retard it. It is a great fact, whose explanation we find in the craving 
 of mankind for knowledge of nature and power over her. 
 
 As men of genius are born, they find the discoveries of those who 
 have gone before them awaiting them. They join in the good work, 
 and add their efforts toward the advancement of knowledge. But in all 
 cases they start at the point where those who have gone before them 
 have left off; if their work is good they continue it; if it is bad they 
 replace it by better, that the structure of science may be reared on solid 
 foundations, and grow surely and steadily toward a perfect whole. 
 
 To understand, then, the place of any man like Faraday in the history 
 of science, we must also understand the state of that science at the time 
 when he did his work. 
 
 Michael Faraday, the son of a smith, was born in 1791, and was ap- 
 prenticed to a bookseller and bookbinder in 1804. He educated himself 
 by reading, and became the assistant of the great chemist, Sir Humphry 
 
ELECTRICAL AND MAGNETIC DISCOVEKIES OF FARADAY 639 
 
 Ihivy, when he was twenty-two years old. His attention was first given 
 to chemistry, but was finally attracted to electricity by the discovery of 
 electro-magnetism by Oersted, in 1820. At this period the subject of 
 electrostatics was very far advanced even as compared with modern 
 limes. 
 
 More than 200 years before, Gilbert had commenced the study of 
 electricity, and divided bodies into electrics and non-electrics, accord- 
 ing as they produced or did not produce electricity by friction. Nearly 
 100 years before, Stephen Gray had discovered the difference between 
 conductors and non-conductors, and had shown the means of carrying 
 electrical effects to a distance of several hundred feet by means of a con- 
 ducting thread or wire suspended by non-conducting threads of silk. 
 Otto von Guericke, du Fay and Wilke had shown that there were two 
 kinds of electricity resinous and vitreous. The Leyden jar had been 
 discovered by the Dutch philosophers. Franklin had written his cele- 
 brated series of letters on electricity, explaining the phenomenon of the 
 Leyden jar and induction as clearly as we can do it at present, giving 
 his theory of positive and negative electricity to the world, and demon- 
 strating in the most perfect manner the electrical nature of thunder 
 and lightning. 
 
 Aepinus and Cavendish had applied mathematics to the subject, and 
 the latter had discovered the law of inverse squares, and made for himself 
 a series of graduated condensers, by which he measured the capacity of 
 differently shaped bodies. They had been followed by Laplace, Pois- 
 son and Biot in mathematical electricity. Coulomb had introduced Jiis 
 torsion balance, the first accurate instrument for electrical measure- 
 ment. 
 
 Galvani and Volta had shown how to produce a current of electricity 
 by the galvanic battery. The chemical action of electricity had long 
 been known, and had been forcibly brought before the world by the 
 immortal experiments of Davy only a short time before, and Ritter had 
 discovered polarization and 1he storage battery. 
 
 But, although many persons had suspected that there was some con- 
 nection between electricity and magnetism it was not until Oersted, in 
 1820, discovered the nature of this connection, and Ampere had given 
 the laws of the attraction of currents, that the science of electro-mag- 
 netism became a subject of investigation. This new discovery aroused 
 the attention of the scientific world to another field of research, and 
 especially awakened in Faraday that sublime curiosity with respect to its 
 laws, which finally led him to his first discovery in this subject. 
 
640 HENRY A. ROWLAND 
 
 The new fact of electro-magnetism interested him. Soon he found 
 that the turning of the needle, as found by Oersted, could be accounted 
 for by the attempt of the north pole tp revolve around the wire in one 
 direction and the south pole in the other. Not content with demon- 
 strating the theory, he invented some pieces of apparatus by which 
 this revolution could be realized, and every collection of physical appar- 
 atus now has them. The little wires or magnets hanging in the cups of 
 mercury are familiar to all, and form the first notable instance of a 
 continuous rotary motion produced by the electric current; it was the 
 first form of electro-magnetic motor so common in our day. But we 
 can not call this a great discovery, as the principles were very apparent. 
 
 Eight or nine years now passed before Faraday gave anything of 
 importance to the world in the subject of electricity and magnetism. 
 
 Seebeck discovered thermo-electricity. Ohm discovered the law con- 
 necting electro-motive force, resistance and current, and the whole 
 scientific world was alert to discover new facts. Faraday brooded on 
 the subject: the electric current produced magnetism, why should not 
 magnetism produce an electric current? At the present age of the 
 world we could answer this question at once, by aid of the great law of 
 the conservation of energy. But fifty-seven years ago it was unknown, 
 except in a very vague manner; the foreshadowing of this great law 
 soon came into the mind of Faraday, but at this period he could only 
 grope blindly in the dark. He knew that a piece of soft iron became 
 magnetic in the presence of a magnet, and that a conductor was electri- 
 fied by induction when near a charged body. Reasoning by analogy, 
 why should not a conducting circuit have a current generated in it in 
 the presence of a wire carrying a current? This was Faraday's reason- 
 ing, and he proceeded to test it by experiment. Winding two wires 
 side by side, on a cylinder of wood, he passed strong currents of elec- 
 tricity through one of them, and attached the other at its two ends 
 to a galvanometer.Kttf'he slightest permanent deflection was observed, 
 and many a man would have pronounced the experiment a failure. 
 But Faraday was not of that nature; he tried again and again, and 
 while bending over the galvanometer in a vain effort to see a slight 
 permanent deflection, he noticed a little jerk of the needle, almost too 
 small to be noticed. His attention was arrested by this curious action, 
 and he proceeded to investigate it. 
 
 He found that this slight movement of the needle was in one direc- 
 tion on making the current, and the opposite direction on breaking it. 
 He substituted a helix, enclosing an unmagnetized needle for the gal- 
 
ELECTRICAL AND MAGNETIC DISCOVERIES OF FARADAY 641 
 
 vanometer, and he found that it was magnetized by this electrical wave, 
 at the moment of making or breaking the main circuit. 
 
 But Faraday was not content until he had discovered all the laws 
 of this new action; he placed two wires on boards, so that, when near 
 together, they were parallel to each other. He now found that the 
 action took place, not only when the current was interrupted, but also 
 when one wire was moved with respect to the other. 
 
 So far, the new effect had only been obtained near an electric current. 
 But Faraday did not forget the connection between electricity and 
 magnetism, but now proceeded to give a new aspect to his discovery. 
 
 For this purpose he chose a ring of wrought iron on which he wound 
 two coils of wire which he attached to a battery, and to a galvanometer, 
 as before. From the presence of the iron, however, he obtained an 
 immensely greater effect than at first, so that, instead of an almost 
 microscopical deflection, the needle of the galvanometer whirled around 
 three or four times, and on attaching two points of charcoal to the ends 
 of the secondary wire, he observed a minute spark between them on 
 completing the main current. The same increased effects occurred on 
 placing bars of iron in straight coils of wire, and Faraday had now 
 proved that the new effect was dependent on the magnetic action of 
 the current. 
 
 He now made one step further, and showed that these induced cur- 
 rents could be obtained from permanent magnets without the aid of 
 other currents, by the simple motion of a wire near a magnet, and that 
 they were specially intense when the wire was wound on a soft iron 
 cylinder, which was then moved near the poles of a magnet. Not con- 
 tent with observing these currents by a galvanometer, he obtained a 
 powerful permanent magnet and allowed his bar of iron, wound with the 
 coil, to come in contact with the poles, the circuit being broken at the 
 same instant. A spark was observed at this broken junction every time 
 the bar came down on the poles. Tyndall tells a very curious story of 
 this experiment which we can well recall. Faraday was attending a 
 meeting of the British Association in Oxford, in 1832, and was re- 
 quested to show some of his wonderful results to the scientists there 
 gathered. While he was thus occupied a dignitary of the University 
 entered and inquired what was going on. Prof. Daniell, who was 
 standing near, explained the matter in popular language. The Dean 
 listened with attention, and looked earnestly at the brilliant spark, but 
 a moment afterwards he assumed a serious countenance, and shook his 
 head: " I am sorry for it," said he, as he walked away; " I am sorry for 
 41 
 
642 HENRY A. KOWLAND 
 
 it; indeed I am sorry for it; it is putting new arms into the hands of the 
 incendiary." This occurred a short time after the papers had been 
 filled with the doings of the hayrick burners. 
 
 Now, after more than fifty years, the spark of Faraday blazes at every 
 street corner, but it has never been found more efficient than an ordinary 
 lucifer match in the burning of hayricks. 
 
 Faraday's attention was now called to the explanation of a curious 
 action discovered by Arago, who found that a rotating disk of copper 
 carried a magnetic needle with it when the latter was suspended over 
 it. The explanation had never been obtained, but Faraday now saw 
 that it was but an instance of his newly discovered action. In order 
 to show that currents were induced in the revolving plate, he mounted 
 it between the poles of a magnet and connected the centre with one 
 pole of a galvanometer; on pressing a wire from the other pole to the 
 edge, Faraday obtained a continuous current of electricity. This was 
 the first continuous current dynamo ever constructed. 
 
 But he rested not until he had obtained the laws of induced currents 
 and expressed them in such simple language that they have ever since 
 been the admiration of the scientific world. 
 
 In giving the law of the production of these induced currents, Fara- 
 day for the first time made use of his famous " lines of force," although 
 he here calls them magnetic curves. 
 
 He showed that a wire must cut these lines in order to have a current 
 induced in it. In order to account for the induction in neighboring 
 wires on making and breaking an electric current, he pictured in his 
 mind the lines of force moving. The current could only start gradually 
 after contact was made, and while it was increasing the lines of force 
 always closed on themselves in rings, were expanding outwards cutting 
 any wires near it, and inducing currents in them. When the current 
 was broken, the lines contracted and produced contrary induced cur- 
 rents. 
 
 In after years he made his law quantitative, and proved that the 
 integral induced current was in proportion to the number of lines of 
 force cut by the wire. 
 
 In his papers of 1831-2 I find these lines always called magnetic 
 curves, and his laws of induced currents are given in terms of these 
 curves. This idea of lines of force was ever after one of the principal 
 points around which the mind of Faraday revolved. He applied it to 
 electrical action as well as to magnetic, and we see him in after years 
 striving to do away with action at a distance, and substitute for it a 
 medium filled with these lines of force. 
 
ELECTRICAL AND MAGNETIC DISCOVERIES OF FARADAY 643 
 
 The medium subjected to electrical or magnetic forces is, according 
 to Faraday's idea, polarized in the direction of these lines of force, so 
 that each particle only has to act upon the one next to it in order that 
 the force may be transmitted to any distance. In Faraday's mind these 
 lines had not only an imaginary existence as being the direction in 
 which the north pole of a needle or an electrified particle tended to 
 move in space, but also a real existence. He imagined them as elastic 
 bands repelling each other laterally, and binding the north and south 
 poles of a magnet, or the positive and negative electricities, together. 
 
 It was only in after years that he discovered all the properties of these 
 lines, and I shall therefore return to them again. 
 
 Guided by these lines of force, he investigated the subject of in- 
 duced electric currents in so complete a manner that nothing of funda- 
 mental importance has ever been added to the subject. True, to-day 
 we understand the subject much better than Faraday ever did. The 
 mathematical researches of Helmholtz, Thomson, Maxwell and others 
 have thrown a flood of light upon the induction of electric currents, 
 and the law of the conservation of energy gives us means of proving all 
 its laws, and indeed of showing that magneto-electric induction is the 
 consequence of the magnetic action of the current as discovered by 
 Oersted. 
 
 But fifty years ago this law of the conservation of energy was too 
 little known to be used in this way. It required the support of just 
 such experiments as those of Faraday to bring into existence and to 
 prove it. Hence, Faraday had but little to guide him to the discovery, 
 except that subtle reasoning of a man of genius which almost amounts 
 to instinct. 
 
 The difference of common and voltaic electricity next engaged his 
 attention. A Leyden jar highly charged might have large sparks and a 
 loud sound; it might ignite alcohol and produce a strong shock when 
 passed through the human body, but it was almost incapable of decom- 
 posing water, and could scarcely affect a magnetic needle. The voltaic 
 battery, on the other hand, could produce the latter effects, but not the 
 former. 
 
 How did these two kinds of electricity differ? 
 
 Faraday answered this by producing all the effects with one kind of 
 electricity that could be obtained from the other. He showed that the 
 difference was caused by there being great tension, or, as we call it, 
 potential in one case, with very little quantity, while in the other there 
 was great quantity with low tension. By charging Leyden jar batteries 
 
644 HENRY A. ROWLAND 
 
 of different sizes with the same number of turns of his machine, and 
 discharging them through a galvanometer, he proved that the sudden 
 deflection of the instrument depended on the quantity, and not the 
 tension, of the electricity. He then arranged a little voltaic hattery out 
 of zinc and platinum wires, so that, when joined to the galvanometer for 
 three seconds, it gave the same swing to the needle as the Leyden jar 
 battery charged with thirty turns of his machine. By this means he 
 was able to estimate that a small battery which decomposed a grain of 
 water, furnished as much electricity as 800,000 discharges of his large 
 Leyden battery, and would form a powerful stroke of lightning, if dis- 
 charged at once. 
 
 The investigation gives us the first rough idea of the magnitude of the 
 quantities involved in frictional and voltaic electricity, and it may be 
 considered as the first rough approximation to the ratio of the electro- 
 magnetic to the electrostatic units of electricity. 
 
 But Faraday was a chemist. His associations with Davy had made 
 him familiar from the first with the chemical action of the battery, and 
 it is but natural that his attention should be directed to its investiga- 
 tion. In the progress of these researches he noted the curious fact that 
 all bodies which could be decomposed by electricity when a fluid, could 
 neither conduct the current nor be decomposed by it when they were 
 solidified by the cold. The conduction and decomposition went to- 
 gether. Rising from this to a general law, he finally proved, by im- ' 
 mense labor, that, for a given quantity of electricity, whatever the de- 
 composing conductor may be, the amount of chemical action is the 
 same. The current, the size of the electrodes and the strength of the 
 solution might vary, but the amount decomposed by a given quantity of 
 electricity remained the same. Furthermore, the amount of different 
 substances separated was in proportion to their chemical equivalents. 
 Hence, the voltameter for measuring the electric currents which, in 
 the form of the silver voltameter, is to-day one of our most accurate in- 
 struments. 
 
 As I have mentioned before, the leading idea in Faraday's mind was 
 the replacing of all action at a distance by curved lines of force which 
 had a definite physical existence. So, in attacking this subject of elec- 
 trolysis, he very quickly showed that Davy's idea that the poles sepa- 
 rated an electrolyte, by actually attracting its components, was false, 
 and that the theory, according to which decomposition and reeompo- 
 sition took place throughout the whole course of the current in the elec- 
 trolyte, was correct. 
 
ELECTRICAL AND MAGNETIC DISCOVERIES OF FARADAY 645 
 
 Faraday now took up an analogous subject the source of the elec- 
 tricity in the voltaic battery. He showed that the current from the 
 battery was proportional to the amount of zinc dissolved, and that the 
 direction of the current depended on the direction of the chomical 
 action. 
 
 The theory of Volta, that the contact of two metals was the source of 
 electricity, was thus effectually disposed of, so that even the recent at- 
 tempt to revive that ancient theory could only have met with the disas- 
 ter which befell it. 
 
 It is impossible for me, in a few minutes, to give account of all that 
 Faraday did on these subjects of electrolysis and the theory of the voltaic 
 battery. His work is a perfect mine of results not haphazard and dis- 
 connected, but each designed to elucidate some point in theory or dem- 
 onstrate some law, and his name must forever be associated with this 
 subject. His law of the definite chemical action of the current will 
 always form an enduring monument to his fame. 
 
 Every discovery that Faraday made only served as a guide to him in 
 making fresh ones. 
 
 We have seen that Faraday found that when an electrolyte was in the 
 solid state it no longer conducted the current. To most observers this 
 would only have been an interesting, but disconnected, fact. But the 
 far-sighted mind of Faraday perceived in this an explanation of no less 
 a subject than that of electric induction. As in the electrolyte, he con- 
 ceived the particles to be arranged in certain directions, decomposing 
 and recomposing along lines in the direction of the electric currents, so 
 in the solidified electrolyte there was some arrangement along the lines 
 in which the current wished to pass, that is, of electric force. Hence his 
 theory of the nature of electric induction and of electric force. It was 
 not action at a distance, but the action of contiguous particles on each 
 other. As in magnetism, so in electricity, the action was carried to a 
 distance by a medium. 
 
 Not content with merely giving the theory, he proceeded to prove 
 it. If it were true, then the nature of the medium should affect the 
 amount of the induction. We all know his beautiful apparatus for test- 
 ing this the two globular Leyden jars which could be filled with 
 air, glass, oil of turpentine, gases, etc., how he divided the charge of 
 one between the two and measured it on a Coulomb electrometer, and 
 thus discovered that his inference was correct, that each substance had 
 a specific inductive capacity, and that the charge of a condenser de- 
 pended not only on the area of the surface and the thickness of the 
 
646 HENRY A. ROWLAND 
 
 dielectric, but also on the nature of the latter, air or vacuum producing 
 the least condensing effect, and glass, sulphur, etc., a greater one. 
 
 To complete his mental vision of an electrified system, it was neces- 
 sary for him to test in a very complete manner the idea that positive 
 and negative electricities are generated in equal quantities. To accom- 
 plish this, he erected a room of twelve feet on a side out of a frame- 
 work covered with tinfoil, and the whole insulated. By generating 
 electricity inside of it, he was able to prove in a more complete manner 
 than had been done before that we never generate positive electricity or 
 negative electricity by itself, but always in equal quantities together. 
 Every complete electrostatic system contains equal quantities of posi- 
 tive and negative electricity, which are separated by a dielectric, through 
 which they are connected by the lines of electric induction, whose ten- 
 sion produced electric attraction. 
 
 To-day, when the mathematics of Maxwell have added clearness to the 
 subject, we see every electrostatic system made up of minute and equal 
 portions of positive and negative electricity, connected together by 
 tubes of induction as by elastic bands, these tubes repelling each other 
 laterally, so as to be held in position, we know that the attraction of all 
 electrified bodies is accounted for by such a system, which was roughly 
 conceived by Faraday, but in which the positions and form of every lino 
 can now be calculated. 
 
 It is impossible, on the present occasion, to follow Faraday through 
 all his researches on the different forms of electric discharge, and his 
 continued researches on electrolysis; but I will pass immediately to two 
 of his greatest discoveries, the action of magnetism on light and diamag- 
 netism. In his researches on optical glass he had discovered a variety of 
 heavy glass, called silicated borate of lead. On placing this between 
 the poles of a magnet, and looking through it along the lines of force, 
 he found that the plane of polarization was rotated. 
 
 Using other substances, he found that most of them had some effect 
 of this kind in the magnetic field. The laws of the magnetic rotation 
 he found very different from those of the ordinary rotation of turpen- 
 tine or sugar, and altogether it forms a most interesting and important 
 experiment when considering the theory of magnetism. 
 
 Not content with discovering this law with his piece of optical glass, 
 he now sought to discover whether there was any force of attraction 
 or repulsion between it and the magnet. Hanging it up between the 
 poles, he discovered that as iron was attracted by a magnet, so the heavy 
 glass was repelled. He called this property diamagnetism, and showed 
 
ELECTKICAL AND MAGNETIC DISCOVERIES OF FARADAY 647 
 
 that all bodies were acted upon by magnetism and could be classified as 
 magnetic or diamagnetic. Magnetism now had a universal significance 
 as applying to all bodies. It was universal in its action, and all bodies 
 responded to it to some extent at least. Even gases were acted on by it, 
 and the oxygen of the air was found quite strongly magnetic. 
 
 Quickly his mind seized another idea. , 
 
 As the intense magnetism of iron, nickel and cobalt was destroyed by 
 heat, might it not b possible that all bodies should become magnetic 
 when cold? He carefully tried the experiment, but never was able to 
 find any effect with the means of producing cold at his command. 
 
 In reading Faraday's papers we are surprised at the clearness with 
 which his laws are expressed. Although he naturally wished to bring 
 his lines of force into use in this case of diamagnetism, yet we now find 
 him making no use of them. His law says that magnetic substances in 
 the field of a magnet tend to the stronger part of the field, and the dia- 
 magnetic to the weaker, irrespective of the direction of the lines of 
 force. 
 
 Bismuth he found the most strongly diamagnetic of all bodies. In 
 using a crystal of this substance instead of a bar, he found that it 
 would set itself in a magnetic field, even if this was uniform. On using 
 other substances he proved the general law that all crystals possessed 
 this property and he called it magne-crystallic force. 
 
 The researches on diamagnetism and magne-crystallic force occupied 
 Faraday's time for five years, from 1845 to 1850, and he was now in the 
 sixtieth year of his age. No more great discoveries fell to his lot, but 
 his mind turned more and more to brooding over the consequences of 
 his past discoveries and following out their results. 
 
 The idea of lines of force was still on his mind, and the discovery of 
 diamagnetism had now given him a further insight into their nature. 
 He saw that the magnetic and diamagnetic nature of bodies could be 
 explained by considering them as good or bad conductors of these lines 
 of force. Iron was a good conductor and bismuth a bad one. When 
 soft iron was placed in a magnetic field, the lines of force, or, as we now 
 more exactly term them, the lines of induction, were more easily con- 
 ducted by it than by the air, and they were deflected toward and through 
 it; but a piece of bismuth was a poorer conductor and these lines of 
 force tended to pass around it rather than through it. By surrounding 
 a weak magnetic body by a strong magnetic fluid he found that it pos- 
 sessed all the properties of a diamagnetic one. Pursuing the subject, 
 he showed how the lines of induction were distributed around and within 
 
648 HENRY A. KOWLAND 
 
 a magnet, and how we are able to measure them by the induced current 
 in moving wires. The method of exploring the magnetic field is the only 
 exact method which has ever been devised for use in such cases as the 
 field of modern dynamo-electric machines, or in most of the problems 
 of modern electrical engineering. He also proved that the lines of in- 
 duction are always closed circuits, whether they are due to permanent 
 magnets or electric currents, thus forever destroying our hope of obtain- 
 ing a continuous current by induction without the use of a commutator. 
 
 When a soft iron bar was approached to the magnet, it drew the lines 
 in upon itself; they proceeded down the bar until they were forced into 
 the badly conducting air and the number which went further down the 
 bar to those which passed out into the air at any point was in proportion 
 to the conductivity of the two. A steel magnet was, in his eyes, like a 
 voltaic pile in water. As the current of electricity was forced forward 
 by the electromotive force of the pile and diffused itself in currents 
 through the water, so the lines of magnetic induction were formed by 
 the coercive power of the steel. It is now known to be a fact that the 
 distribution of magnetism on a steel magnet, or indeed in any case, can 
 be calculated by these principles Faraday laid down. The idea of a mag- 
 netic circuit is familiar now to all electrical engineers. 
 
 To Faraday's eye, a magnet not only consisted of a piece of steel or 
 loadstone which is apparent to our ordinary vision, but included all the 
 space around which was filled with lines of force; it was bounded only by 
 the limits of the universe. The steel served merely to bind together 
 the ring-like lines of induction which passed from the magnet to every 
 point of space. 
 
 Faraday was not a mathematician, and could not thus follow out the 
 consequences of his great ideas. This has been done for him by the im- 
 mortal Maxwell. He has taken up the idea that electrical and mag- 
 netic forces only proceed to a distance by aid of the intervening particles 
 of matter, or ether, as the case may be, and has given it a mathematical 
 basis. 
 
 To-day a body charged with electricity, a magnet or a wire carrying 
 an electrical current, all are incomplete without the space around them. 
 
 When we attach a battery to a wire and the current apparently flows 
 through it as if it were a current of water, Faraday's idea shows us that 
 we are only looking at the matter superficially; around that wire and 
 permeating space in every part are lines of magnetic force, and lines of 
 electrostatic force. At the moment of joining the battery to the wire 
 this whole complicated system of lines of force must be formed. At the 
 
ELECTRICAL AXD MAGNETIC DISCOVERIES OF FARADAY 649 
 
 moment of breaking circuit, the system must vanish, and we obtain the 
 energy stored up in this space surrounding the wire in the bright spark 
 known as the extra current. 
 
 What a flood of light this throws on many experiments such as those 
 of Wheatstone, on the velocity of electricity. With his wire arranged 
 in parallel loops around an ordinary room, he discharged a Leyden jar 
 through it, and assumed that the electricity passed through the whole 
 wire before a spark could form at the distant end. But we know that 
 whole room was instantly filled with moving lines of magnetic force, 
 which induced currents in every wire they crossed, and hence what 
 Wheatstone measured was merely the current induced from one wire 
 or those near it. 
 
 Thomson and Maxwell have shown that the medium around a wire 
 carrying an electric current is in motion, and that the vortex filaments 
 form Faraday's lines of magnetic force; for Faraday's discovery of the 
 magnetic rotation of the plane of polarization of light can be explained 
 in no other way. 
 
 Thus the discoveries of Faraday have been engrafted on our science, 
 and form one of its most essential features. They are among the foun- 
 dation stones of the edifice of our science. 
 
 We know far more than the electricians of that day, in the details of 
 the subject, and mathematics has given us a broad view of electricity 
 and magnetism, such as never before was obtained. In its practical use 
 and measurement we have made immense strides in devising methods 
 and instruments, and we now carry out our experiments on a scale which 
 Faraday could not attempt, seeing that subject, which has hitherto been 
 best adapted to the contemplation of a few philosophers, has become 
 of use to all, and electricity bids fair to become our most important 
 servant. 
 
 The spark, which Faraday more than fifty years ago observed in a 
 darkened room, now blazes out almost with the power of the sun, but it 
 is still the spark of Faraday. Though it is a thousand times as large, it 
 is still made on the principles which Faraday laid down, and nothing 
 except mechanical details has ever been added to its process. 
 
 How suitable, then, that we should remember his name on this 
 occasion, since his discoveries have served as the basis of all progress 
 in electrical engineering. Had Faraday not lived we should not have 
 been here to-night. True, as I have shown before, the progress of science 
 could only have been delayed by the absence of any one man, but how 
 long, in this case, we cannot tell. We can only receive with gratitude 
 
650 HENRY A. ROWLAND 
 
 what Faraday has given freely to us, and speak his name with the rever- 
 ence due, not only to his intellectual eminence, but to his character. 
 Too noble to leave science for the wealth held out to him, he persevered 
 in it to the end, and gave to the world the fruits of his labor in his 
 ' Experimental Researches in Electricity.' 
 
 He never obtained from the world the material reward for his labor, 
 but died a poor man, who had enriched the world. 
 
 We stand at an important epoch in the history of our science. We 
 have gone far enough into its practical applications to see some dis- 
 tance into the future. The arc light, which Davy brought into promi- 
 nence at the beginning of this century, fed by the machines of Faraday, 
 blazes throughout the night in all cities of the world. The incandescent 
 light, known long to scientists, has been improved and bids fair to rival 
 gas in cheapness, as it surpasses it in beauty. The secondary battery 
 discovered by Ritter eighty years or more ago, improved by Plante and 
 Faure in recent times, still struggles to fill the place assigned to it, to be 
 replaced by one before long which shall not waste fifty per cent of the 
 power given to it, and weigh tons for a few foot-pounds of energy stored 
 up. We see it in its new form replacing the laboring horses in the 
 streets, and serving in many cases where small power is needed. But the 
 transmission of energy seems to me to open one of the widest fields, and 
 the time is not very distant when a few large engines will replace the 
 numerous small ones in our cities; when also the power of waterfalls may 
 be made available at a distance. 
 
 The principle of the telephone also is destined to bear unseen fruit. 
 
 There is work for all, the practical and theoretical man alike. 
 
 The philosopher, studying the problems of the universe, deems himself 
 rewarded by some new fact discovered, some new law demonstrated. To 
 him the universe is a problem to solve, and his motto is, " Science is 
 knowledge." 
 
 He sees before him the time when man's insight into nature shall be 
 vastly increased, and esteems the science of to-day as but an atom to 
 what we shall know in the future. While not despising the wealth, he 
 seldom has time for its accumulation, as he considers other things of 
 vastly more importance; the truth is what he seeks; the truth as to this 
 wonderful universe in which we live. What is matter? what is electric- 
 ity, what is the medium which transmits light from one point to an- 
 other, how comes it that the earth, is magnetic? These are some of the 
 problems he is trying to solve. He knows that one man can do but little 
 toward it, even though he should surpass what Faraday has done, but 
 
ELECTRICAL AND MAGNETIC DISCOVERIES OF FARADAY 651 
 
 he trusts to the combined efforts of mankind, shown in the steady prog- 
 ress of science, to finally arrive at a solution. 
 
 The devotee of applied science, the so-called practical man, looks 
 upon the forces of nature as his servants, and strives to become their 
 master. The world must move, its work must be accomplished. We 
 are not satisfied to live as our fathers have done, and we must have 
 luxuries unknown to them. Our thoughts must fly to the farthest parts 
 of the earth in an instant, at our bidding, and we must pass from point 
 to point on the wings of the wind, for flesh and blood is too slow for us. 
 To accomplish this, the engineer harnesses the forces of nature and 
 compels them to work for him. He takes the discoveries of the phil- 
 osopher and uses them for the practical needs of daily life. His motto 
 is, " Science is power." As he ministers more directly to the present 
 generation of mankind than to the generations to come, as does the phil- 
 osopher, so he often reaps his reward in the present, and retains some 
 of that wealth which his inventions bring into the world. For the 
 source of the wealth of the world is labor, and the labor of the forces 
 of nature, in our behalf, surpasses very many fold that of human flesh 
 and blood. He who adds but the slightest to our power over these 
 forces enriches the world, and is entitled to its practical, as well as its 
 sentimental gratitude, be he philosopher or engineer. The great ques- 
 tion which we should ask ourselves is how our science can best be fur- 
 thered. The philosopher must precede the engineer. To have the ap- 
 plications of electricity, there must be a science of electricity. This 
 science cannot depend for its existence on practical men whose minds 
 are engrossed with other than theoretical problems. It nuist exist in 
 minds like Faraday, which are specially adapted to its reception and 
 advancement men who are willing to devote their lives to it, and who 
 have the ability to further it. We cannot create such men, but we can 
 give them our practical as well as our sentimental sympathy, when 
 found. The philosopher is made of flesh and blood as well as other 
 men. He must live and have his tastes gratified as well as others. 
 His place in the world as at present constituted is usually that of a pro- 
 fessor in our universities and colleges. Are only men like Faraday 
 chosen for these positions? Of the four hundred or more, how many 
 choose their professors on account of their eminence in theoretical 
 science? Are there a dozen? I doubt it. Furthermore, what facilities 
 and encouragement would they have in these institutions to do work? 
 Too far away from each other to be a mutual help, they have but an 
 incomplete scientific life. Faraday could not have been himself in 
 
652 HEXEY A. ROWLAND 
 
 Africa and would have languished in our own country. In London, in 
 contact with the science of Europe and encouraged by its atmosphere, 
 with the Royal Society at which to announce his discoveries and the 
 Royal Institution in which to make them, Faraday, in spite of poor 
 education, was stimulated to his best efforts. Alone in one of our iso- 
 lated colleges, cut off from intercourse with the rest of the world by a 
 so-called protective duty on his very life, books, with no journal spe- 
 cially devoted to theoretic physics, and no society like the Royal Society, 
 who can say whether his discoveries would have been made or not? The 
 endowment of research seems to me to offer the best means out of the 
 difficulty. Let professorships be endowed and funds to pay the expenses 
 of apparatus and assistants be formed in our universities, with the under- 
 standing that the research is to be the principal work; work, while teach- 
 ing is not to be neglected. The result will be the formation of a scien- 
 tific atmosphere in which men like Faraday can live and labor, and the 
 dry bones of the pedagogue be replaced by the fire and life of the orig- 
 inal investigator. And let not practical science be neglected. Let us 
 have scientific schools of the highest grade, where modern science is 
 taught, so that fifty years shall not again pass, as it has done, before a 
 discovery like that of Faraday is utilized. 
 
 Furthermore, let us have scientific societies and clubs like the pres- 
 ent, where men of like tastes can meet and interchange ideas. 
 
 Thus we meet together to-night, electricians all, practical and theo- 
 retical, at a time in the history of our science and of the world which 
 will in future be called the beginning of the age of electricity. 
 
 The feeble attraction of the amber has become a mighty force, which 
 is destined to make itself felt, and it is to be hoped that our mutual in- 
 tercourse in this Club may aid us all in our efforts to make an impress 
 on its future history. 
 
ADDRESS BEFORE THE AMERICAN INSTITUTE OF ELECTRICAL ENGINEERS, 
 NEW YORK, MAY 22, 1889 
 
 [Transactions of the American Institute of Electrical Engineers, VI, 342-357, 1889] 
 
 As, a short time since, I stood in a library of scientific books and 
 glanced around me at the works of the great masters in physics, my mind 
 wandered back to the time when the apparatus for a complete course 
 of lectures on the subject of electricity consisted of a piece of amber 
 and a few light bodies to be attracted by it. From that time until 
 now, when we stand in a magnificent laboratory with elaborate and 
 costly apparatus in great part devoted to its study, how greatly has the 
 world changed and how our science of electricity has expanded both in 
 theory and practice until, in the one case, it threatens to include within 
 itself nearly the whole of physics, and in the other to make this the age 
 of electricity. 
 
 Were I to trace the history of the views of physicists with respect 
 to electric currents it would include the whole history of electricity. 
 The date when the conception of an electric current was possible was 
 when Stephen Gray, about 170 years ago, first divided bodies into con- 
 ductors and non-conductors, and showed that the first possessed the 
 property of transmitting electrical attractions to a distance. But it 
 was only when the Leyden jar was discovered that the idea of a current 
 became very definite. The notion that electricity was a subtle fluid 
 which could flow along metal wires as water flows along a tube, was 
 then prevalent, and, indeed, remains in force to-day among all ex- 
 cept the leaders in scientific thought. It is not my intention to depre- 
 ciate this notion, which has served and still serves a very important pur- 
 pose in science. But, for many years, it has been recognized that it in- 
 cludes only a very small portion of the truth and that the mechanism by 
 which energy is transmitted from one point of space to another by means 
 of an electric current is a very complicated one. 
 
 Here for instance, on the table before me are two rubber tubes filled 
 with water, in one of which the water is in motion, in the other at rest. 
 It is impossible, by any means now known to us, to find out, without 
 moving the tubes, which one has the current of water flowing in it and 
 
654 HENRY A. EOWLAND 
 
 which has the water at rest. Again, I have here two wires, alike in all 
 respects, except that one has a current of electricity flowing in it and 
 the other has not. But in this case I have only to bring a magnetic 
 needle near the two to find out in which one the current is flowing. On 
 our ordinary sense the passage of the current has little effect; the air 
 around it does not turn green or the wire change in appearance. But 
 we have only to change our medium from air to one containing magnetic 
 particles to perceive the commotion which the presence of a current 
 may cause. Thus this other wire passes through the air near a large 
 number of small suspended magnets, and, as I pass the current through 
 it, every magnet is affected and tends to turn at right angles to the wire 
 and even to move toward it and wrap itself around it. If we suppose 
 the number of these magnets to become very great and their size small, 
 or if we imagine a medium, every atom of which is a magnet, we see that 
 no wire carrying a current of electricity can pass through it without 
 creating the greatest commotion. Possibly this is a feeble picture of 
 what takes place in a mass of iron near an electric current. 
 
 Again, coil the wire around a piece of glass, or indeed, almost any 
 transparent substance, and pass a strong current through the wire. 
 With our naked eye alone we can see no effect whatever, as the glass is 
 apparently unaltered by the presence of the current; but, examined in 
 the proper way, by means of polarized light, we see that the structure of 
 the glass has been altered throughout in a manner which can only be 
 explained by the rotation of something within the glass many millions 
 of times every second. 
 
 Once more, bring a wire in which no current exists nearer and nearer 
 to the one carrying the current, and we shall find that its motion in such 
 a neighborhood causes or tends to cause an electric current in it. Or, if 
 we move a large solid mass of metal in the neighborhood of such a cur- 
 rent we find a peculiar resistance unfelt before, and if we force it into 
 motion, we shall perceive that it becomes warmer and warmer as if there 
 was great friction in moving the metal through space. 
 
 Thus, by these tests, we find that the region around an electric cur- 
 rent has very peculiar properties which it did not have before, and 
 which, although stronger in the neighborhood of the current, still ex- 
 tend to indefinite distances in all directions, becoming weaker as the 
 distances increase. 
 
 How great, then, the difference between a current of water and a cur- 
 rent of electricity. The action of the former is confined to the interior 
 of the tube, while that of the latter extends to great distances on all 
 
MODERN VIEWS WITH EESPECT TO ELECTRIC CURRENTS 655 
 
 sides, the whole of space being agitated by the formation of an electric 
 current in any part. To show this agitation, I have here two large 
 frames with coils of wire around them. They hang face to face about 
 6 feet apart. Through one I discharge this Leyden jar, and immediately 
 you see a spark at a break in the wire of the other coil, and yet there is 
 no apparent connection between the two. I can carry the coils 50 feet 
 or more apart, and yet by suitable means I can observe the disturbances 
 due to the current in the first coil. 
 
 The question is forced upon us as to how this action takes place. How 
 is it possible to transmit so much power to such a distance across appar- 
 ently unoccupied space? According to our modern theory of physics 
 there must be some medium engaged in this transmission. We know 
 that it is not the air, because the same effects ta,ke place in a vacuum, 
 and, therefore, we must fall back on that medium which transmits light 
 and which we have named the ether. That medium which is supposed 
 to extend unaltered throughout the whole of space, whose existence is 
 very certain but whose properties we have yet but vaguely conceived. 
 
 I cannot, in the course of one short hour, give even an idea of the 
 process by which the minds of physicists have been led to this conclusion 
 or the means by which we have finally completely identified the ether 
 which transmits light with the medium which transmits electrical and 
 magnetic disturbances. The great genius who first identified the two is 
 Maxwell, whose electro-magnetic theory of light is the centre around 
 which much scientific thought is to-day revolving, and which we regard 
 as one of the greatest steps by which we advance nearer to the under- 
 standing of matter and its laws. It is this great discovery of Maxwell 
 which allows me, at the present time, to attempt to explain to you the 
 wonderful events which happen everywhere in space when one estab- 
 lishes an electric current in any other portion. 
 
 In the first place, we discover that the disturbance does not take place 
 in all portions of space at once, but proceeds outwards from the centre 
 of the disturbance with a velocity exactly equal to the velocity of light. 
 So that, when I touch these wires together so as to complete the circuit 
 of yonder battery, I start a wave of ethereal disturbance which passes 
 outwards with a velocity of 185,000 miles per second, thus reaching the 
 sun in about eight minutes, and continues to pass onwards forever or 
 until it reaches the bounds of the universe. And yet none of our senses 
 inform us of what has taken place unless we sharpen them by the use of 
 suitable instruments. Thus, in the case of these two coils of wire, sus- 
 pended near each other, which we have already used, when the wave 
 
656 HENRY A. EOWLAND 
 
 from the primary disturbance reaches the second coil, we perceive the 
 disturbance by means of the spark formed at the break of the coil. 
 Should I move the coils further apart, the spark in the second coil would 
 be somewhat delayed, but the distance of 185,000 miles would be neces- 
 sary before this delay could amount to as much as one second. Hence 
 the effects we observe on the earth take place so nearly instantaneously 
 that the interval of time is very difficult to measure, amounting, in the 
 present case, to only TT(nn j- 1 - {mro . of a second. 
 
 It is impossible for me to prove the existence of this interval, but I 
 can at least show you that waves have something to do with the action 
 here observed. For instance, I have here two tuning forks mounted on 
 sounding boxes and tuned to exact unison. I sound one and then stop 
 its vibrations with my hand, instantly you hear that the other is. in vibra- 
 tion, caused by the waves of sound in the air between the two. When, 
 however, I destroyed the unison by fixing this piece of wax on one of the 
 forks, the action ceases. 
 
 Now, this combination of a coil of wire and a Leyden jar is a vibrating 
 system for electricity and its time of vibration is about 10,000,000 
 times a second. This second system is the same as the first, and there- 
 fore its time of vibration is the same. You see how well the experiment 
 works now because the two are in unison. But let me take away this 
 second Leyden jar, thus destroying the unison, and you see that the 
 sparks instantly cease. Eeplacing it, the sparks reappear. Adding an- 
 other on one side and they disappear again, only to reappear when the 
 system is made symmetrical by placing two on each side. 
 
 This experiment and that of the tuning forks have an exact analogy 
 to one another. In each we have two vibrating systems connected by a 
 medium capable of transmitting vibrations, and they both come under 
 the head of what we know as sympathetic vibrations. In the one case, 
 we have two mechanical tuning forks connected by the air; in the other, 
 two pieces of apparatus which we might call electrical tuning forks, con- 
 nected by the luminiferous ether. The vibrations in one case can be 
 seen by the eye or heard by the ear, but in the other case they can only 
 be perceived when we destroy them by making them produce a spark. 
 The fact that we are able to increase the effect by proper tuning dem- 
 onstrates that vibrations are concerned in the phenomenon. This can, 
 however, be separately demonstrated by examining the spark by means 
 of a revolving mirror, when Ave find that it is made up of many succes- 
 sive sparks corresponding to the successive backward and forward move- 
 ments of the current. 
 
MODERN VIEWS WITH RESPECT TO ELECTRIC CURRENTS 657 
 
 The fact of the oscillatory character of the Leyden jar discharge was 
 first demonstrated by our own countryman, Henry, in 1832, but he pur- 
 sued the subject only a short distance, and it remained for Sir William 
 Thomson to give the mathematical theory and prove the laws according 
 to which the phenomenon takes place. 
 
 Thus, in the case of a charged Leyden jar whose inner and outer coat- 
 ings have been suddenly joined by a wire, the electricity flows back and 
 forth along the wire until all the energy originally stored up in the jar 
 has expended itself in heating the wire or the air where the spark takes 
 place and in generating waves of disturbance in the ether which move 
 outward into space with the velocity of light. These ethereal waves we 
 have demonstrated by letting them fall on this coil of wire and causing 
 the electrical disturbance to manifest itself by electric sparks. 
 
 I have here another more powerful arrangement for producing electro- 
 magnetic waves of very long wave-length, each one being about 500 
 miles long. It consists of a coil, within which is a bundle of iron wires. 
 On passing a powerful alternating current through the coil, the iron 
 wires are rapidly magnetized and demagnetized, and send forth into 
 space a system of electro-magnetic waves at the rate of 360 in a second. 
 
 Here, also, I have another piece of apparatus [a lamp] for sending 
 out the same kind of electro-magnetic waves; on applying a match, we 
 start it into action. But the last apparatus is tuned to so high a pitch 
 that the waves are only so ^ 00 inch long, and 55,000,000,000,000 are 
 given out in one second. These short waves are known by the name of 
 light and radiant heat, though the name radiation is more exact. Plac- 
 ing any body near the lamp so that the radiation can fall on it, we ob- 
 serve that when the body absorbs the rays it is heated by them; the 
 well-known property of so-called radiant heat and light. Is it not pos- 
 sible for us to get some substance to absorb the long waves of disturb- 
 ance, and so obtain a heating effect? I have here such a substance in 
 the shape of a sheet of copper, which I fasten on the face of a thermo- 
 pile, and I hold it where the waves are the strongest [near the coil while 
 the alternating current is passing through it]. As I have anticipated, 
 great heat is generated by their absorption, and soon the plate of copper 
 becomes very warm, as we see by this thermometer, by feeling it with 
 the hand, or even by the steam from water thrown upon it. In this ex- 
 periment the copper has not touched the coil or the iron wire core, 
 although if it did they are very much cooler than itself. The heat has 
 been produced by the absorption of the waves in the same way as a 
 42 
 
658 HENKY A. KOWLAND 
 
 blackened body absorbs the rays of shorter wave-length from the lamp; 
 and, in both cases, heat is the result. 1 
 
 But in this experiment, as in the first one, the wave-like nature of the 
 disturbance has not been proved experimentally. We have caused elec- 
 tric sparks, and have heated the copper plate across an interval of space, 
 but have not in either of these cases proved experimentally the progres- 
 sive nature of the disturbance; for a ready means of experimenting on 
 the waves, obtaining their wave-length and showing their interferences, 
 has hitherto been wanting. This deficiency has been recently overcome 
 by Professor Hertz, of Carlsruhe, who has made a study of the action of 
 the coil, and has shown us how to use it for experiments on the ethereal 
 waves, whose existence had before been made certain by the mathemat- 
 ics of Maxwell. 
 
 I scarcely know how to present this subject to a non-technical audience 
 and make it clear how a coil of wire with a break in it can be used to 
 measure the velocity and wave-lengths of ethereal waves. However, I 
 can but try. If the waves moved very slowly, we could readily measure 
 the time the first coil took to affect the second, and show that this time 
 was longer as the distance was greater. But it is absolutely inapprecia- 
 ble by any of our instruments, and another method must be found. To 
 obtain the wave-length Professor Hertz used several methods, but that 
 by the formation of stationary weaves is the most easily grasped. Mr. 
 Ames holds in his hand one end of a spiral spring, which makes a very 
 heavy and flexible rope. As he sends a wave down it, you see that it is 
 reflected at the further end, and returns again to his hand. If, how- 
 ever, he sends a succession of waves down the rope, the reflected waves 
 interfere with the direct ones, and divide the rope into a succession of 
 nodes and loops, which you now observe. So a series of sound waves, 
 striking on a wall, form a system of stationary waves in front of the wall. 
 With this in view, Professor Hertz established his apparatus in front of 
 a reflecting wall, and observed the nodes and loops by the sparks pro- 
 duced in a ring of wire. It is impossible for me to repeat this experi- 
 ment before you, as it is a very delicate one, and the sparks produced are 
 almost microscopic. Indeed, I should have to erect an entirely differ- 
 ent apparatus, as the waves from the one before me are nearly % mile 
 long, the time of vibration of the system being very great, that is 
 TWinnnnr ^ a second. To produce shorter waves we must use appa- 
 
 1 The thermopile was connected with a delicate mirror galvanometer, the de- 
 flections of which were shown on a screen. 
 
MODERN VIEWS WITH KESPECT TO ELECTRIC CURRENTS 659 
 
 ratus tuned, as it were, to a higher pitch, in which the same principle's, 
 however, employed, but the ethereal waves are shorter, and thus several 
 stationary waves can be contained in one room. 
 
 The testing coil is then moved to different portions of the room, and 
 the nodes are indicated by the disappearance of the sparks, and the 
 loops by the greater brightness of them. The presence of stationary 
 waves is thus proved, and their half wave-length found from the dis- 
 tance from node to node, for stationary waves can always be considered 
 as produced by the interference of two progressive waves advancing in 
 opposite directions. 
 
 However interesting a further description of Professor Hertz's experi- 
 ments may be, we have gone as far in that direction as our subject car- 
 ries us, for we have demonstrated that the production of a current in a 
 wire is accompanied by a disturbance in the surrounding space; and, 
 although I have not experimentally demonstrated the ethereal waves, yet 
 I have proved the existence of electric oscillations in the coils of wire 
 and the ether surrounding it. 
 
 Our mathematics has demonstrated, and experiments like those of 
 Professor Hertz have confirmed the demonstration, that the wave dis- 
 turbance in the ether is an actual fact. 
 
 The closing of a battery circuit, then, and the establishment of a cur- 
 rent of electricity in a wire is a very different process from the forma- 
 tion of a current of water in a pipe, though, after the first shock, the 
 laws of the flow of the two are very much alike. But even then, the 
 medium around the current of electricity has very strange properties, 
 showing that it is accompanied by a disturbance throughout space. The 
 wire is but the core of the disturbance, which latter extends indefinitely 
 in all directions. 
 
 One of the strangest things about it is that we can calculate with per- 
 fect exactness the velocity of the wave propagation and the amount of 
 the disturbance at every point and at any instant of time; but as yet we 
 cannot conceive of the details of the mechanism which is concerned in 
 the propagation of an electric current. In this respect our subject resem- 
 bles all other branches of physics in the partial knowledge we have of it. 
 We know that light is the undulation of the luminiferous ether, and yet 
 the constitution of the latter is unknown. We know that the atoms of 
 matter can vibrate with purer tones than the most perfect piano, and 
 yet we cannot even conceive of their constitution. We know that the 
 sun attracts the planets with a force whose law is known, and yet we 
 fail to picture to ourselves the process by which it takes our earth within 
 
660 HENKY A. KOWLAND 
 
 its grasp at the distance of many millions of miles and prevents it from 
 departing forever from its life-giving rays. Science is full of this half 
 knowledge, and the proper attitude of the mind is one of resignation 
 toward that which it is impossible for us to know at present and of ear- 
 nest striving to help in the advance of our science, which shall finally 
 allow us to answer all these questions. 
 
 The electric current is an unsolved mystery, but we have made a very 
 great advance in understanding it when we know that we must look out- 
 side of the wire at the disturbance in the medium before we can under- 
 stand it: a view which Faraday dimly held fifty years ago, which was 
 given in detail in the great work of Maxwell, published sixteen years 
 since, and has been the guide to most of the work done in electricity 
 for a very long time. A view which has wrought the greatest changes 
 in the ideas which we have conceived with respect to all electrical 
 phenomena. 
 
 So far, we have considered the case of alternating electric current in 
 a wire connecting the inner and outer coatings of a Leyden jar. The 
 invention of the telephone, by which sound is carried from one point to 
 another by means of electrical waves, has forced into prominence the 
 subject of these waves. Furthermore, the use of alternating currents 
 for electric lighting brings into play the same phenomenon. Here, 
 again, the difference between a current of water and a current of elec- 
 tricity is very marked. A sound wave, traversing the water in the tube, 
 produces a to and fro current of water at any given point. So, in the 
 electrical vibration along a wire, the electricity moves to and fro along 
 it in a manner somewhat similar to the water, but with this difference: 
 the disturbance from the water motion is confined to the tube and the 
 oscillation of the water is greatest in the centre of the tube, while, in 
 the case of the electric current, the ether around the wire is disturbed 
 and the oscillation of the current is greatest at the surface of the wire 
 and least in its centre. The oscillations in the water take place in the 
 tube without reference to the matter outside the tube 1 , whereas the elec- 
 tric oscillations in the wire are entirely dependent on the surrounding 
 space, and the velocity of the propagation is nearly independent of the 
 nature of the wire, provided only that it is a good conductor. 
 
 We have, then, in the case of electrical waves along a wire, a disturb- 
 ance outside the wire and a current within it, and the equations of 
 Maxwell allow us to calculate these with perfect accuracy and give all the 
 laws with respect to them. 
 
 We thus find that the velocity of propagation of the waves along a 
 
MODERN VIEWS WITH RESPECT TO ELECTRIC CURRENTS 661 
 
 wire, hung far away from other bodies and made of good conducting ma- 
 terial, is that of light, or 185,000 miles per second; but when it is 
 hung near any conducting matter, like the earth, or inclosed in a cable 
 and sunk into the sea, the velocity becomes much less. When hung in 
 space, away from other bodies, it forms, as it were, the core of a system 
 of waves in the ether, the amplitude of the disturbance becoming less 
 and less as we move away from the wire. But the most curious fact is 
 that the electric current penetrates only a short distance into the wire, 
 
 
 Or 
 
 
 - o 
 
 DIAGRAM 1. 
 
 being mostly confined to the surface, especially where the number of 
 oscillations per second is very great. 
 
 The electrical waves at the surface of a conductor are thus, in some 
 respects, very similar to the waves on the surface of the water. The 
 greatest motion in the latter case is at the surface, while it diminishes 
 as we pass downward and soon becomes inappreciable. Furthermore, 
 the depth to which the disturbance penetrates into the water increases 
 with increase of the length of the wave, being confined to very near the 
 surface for very short waves. So the disturbance in the copper pene- 
 trates deeper as the waves and the time of oscillation are longer, and the 
 disturbance is more nearly confined to the surface as the waves become 
 shorter. I have recently made the complete calculations with respect 
 
662 
 
 HENRY A. ROWLAND 
 
 to these waves, and have drawn some diagrams to illustrate the penetra- 
 tion of the alternating current into metal cylinders. The first diagram 
 represents the current at different depths in a copper cylinder, 45 cm. 
 diameter, or an iron one 144 cm. diameter, traversed by an alternating 
 current with 200 reversals per second. The first and second curves 
 show us the current at two different instants of time, and show us how 
 the phase changes as we pass downward into the cylinder. By reference 
 to the third curve we see that it may be even in the opposite direction in 
 the centre of the cylinder from what it is at the surface. The third 
 curve gives us the amplitude of the current oscillations at different 
 depths irrespective of the phase, and it shows us that the current at the 
 
 -^ 
 
 6 
 
 5 
 
 6-,.. 
 
 Y 
 
 '4 - 
 
 6 "* 
 
 Y" 
 
 
 3 
 
 3 
 
 3 
 
 
 2 
 
 a - 
 
 2 
 
 
 1 
 
 i 
 
 I 
 
 
 1 
 
 i 
 
 1 
 
 
 2 
 
 2 - 
 
 2 
 
 
 3 
 
 3 
 
 3 
 
 - --- " 
 
 } 
 "> 
 
 4 
 
 X 
 
 fi" 
 
 X 4 
 
 N.^ 
 
 DIAGRAM 2. 
 
 centre is only about 10 per cent of that at the surface in this case. The 
 second diagram shows us the distribution in the same cylinders when the 
 number of reversals of the current is increased to 1800 per second. Here 
 we see that the disturbance is almost entirely confined to the surface, for 
 at a depth of only 7 mm. the disturbance almost entirely vanishes. 
 
 There are very many practical applications of these theoretical results 
 for electric currents. The most obvious one is to the case of conductors 
 for the alternating currents used in producing the electric light. We 
 find that when these are larger than about half an inch diameter they 
 should be replaced by a number of conductors less than half an inch 
 diameter, or by strips about a quarter of an inch thick, and of any con- 
 venient width. But this is a matter to be attended to by the electric 
 light companies. 
 
 Prof. Oliver J. Lodge has recently, in the British Association, drawn 
 
MODERN VIEWS WITH RESPECT TO ELECTRIC CURRENTS 663 
 
 attention to the application of these results to lightning rods. Almost 
 since the time of Franklin there have been those who advocated the 
 making of lightning rods hollow, to increase the surface for a given 
 amount of copper. We now know that these persons had no reason for 
 their belief, as they simply drew the inference from the fact that elec- 
 tricity at best is on the surface. Neither were the advocates of the solid 
 rods quite correct, for they reasoned from the fact that electricity in a 
 state of steady flow occupies the whole area of the conductor equally. 
 The true theory, we now know, indicates that neither party was entirely 
 correct and that the surface is a very important factor in the case of a 
 current of electricity so sudden as that from a lightning discharge. But 
 increase of surface can best be obtained by multiplying the number of 
 conductors, rather than making them flat or hollow; and, at the same 
 time, Maxwell's principle of enclosing the building within a cage can. be 
 carried out. Theory indicates that the current penetrates only one- 
 tenth the distance into iron that it does into copper. As the iron has 
 seven times the resistance of copper, we should need 70 times the sur- 
 face of iron that we should of copper. Hence I prefer copper wire 
 about a quarter of an inch diameter and nailed directly to the house 
 without insulators, and passing down the four corners, around the eaves 
 and over the roof, for giving protection from lightning in all cases where 
 a metal roof and metal down spouts do not accomplish the same purpose. 
 Whether the discharge of lightning is oscillatory or not does not enter 
 into the question, provided it is only sufficiently sudden. I have re- 
 cently solved the mathematical problem of the electric oscillations along 
 a perfectly conducting wire joining two infinite and perfectly conducting 
 planes parallel to each other, and find that there is no definite time of 
 oscillation, but that the system is capable of vibrating in 'any time in 
 which it is originally started. The case of lightning between a cloud of 
 limited extent and the earth along a path through the air of great re- 
 sistance is a very different problem. Both the cloud and the path of the 
 electricity are poor conductors, which tends to lengthen the time. If I 
 were called on to estimate as nearly as possible what took place in a flash 
 of lightning, I would say that I did not believe that the discharge was 
 always oscillating, but more often consisted of one or more streams of 
 electricity at intervals of a small fraction of a second, each one continu- 
 ing for not less than 1 0*0 o o second. An oscillating current with 100,000 
 reversals per second would pentetrate about ^ inch into copper and ^-J-g- 
 inch into iron. The depth for copper would constitute a considerable 
 portion of a wire inch diameter, and, as there are other considerations 
 
664 HENRY A. BOWL AND 
 
 to be .taken into account, I believe it is scarcely worth while making 
 tubes, or flat strips, for such small sizes. 
 
 It is almost impossible to draw proper conclusions from experiments 
 on this subject in the laboratory such as those of Prof. Oliver J. Lodge. 
 The time of oscillation of the current in most pieces of laboratory ap- 
 paratus is so very small, being often the T70 000777 ^ a second, that 
 entirely wrong inferences may be drawn from them. As the size of 
 the apparatus increases, the time of oscillation increases in the same pro- 
 portion, and changes the whole aspect of the case. I have given 
 TT7Vr7 of a second as the shortest time a. lightning flash could proba- 
 bly occupy. I strongly suspect it is often much greater, and thus de- 
 parts even further from the laboratory experiments of Professor Lodge, 
 who has, however, done very much toward drawing attention to this 
 matter and showing the importance of surface in this case. All shapes 
 of the rod with equal surface are not, however, equally efficient. Thus, 
 the inside surface of a tube does not count at all. Neither do the corru- 
 gations on a rod count for the full value of the surface they expose, for 
 the current is not distributed uniformly over the surface; but I have 
 recently proved that rapidly alternating currents are distributed over the 
 surface of very good conductors in the same manner as electricity at 
 rest would be distributed over them, so that the exterior angles and cor- 
 ners possess much more than their share of the current, and corruga- 
 tions on the wire concentrate the current on the outer angles and dimin- 
 ish, it in the hollows. Even a flat strip has more current on the edges 
 than in the centre. 
 
 For these reasons, shape, as well as extent of surface, must be taken 
 into account, and strips have not always an advantage over wires for 
 quick discharges. 
 
 The fact that the lightning rod is not melted on being struck by 
 lightning is not now considered as any proof that it has done its work 
 properly. It must, as it were, seize upon the discharge and offer it an 
 easier passage to the earth than any other. Such sudden currents of 
 electricity we have seen to obey very different laws from continuous ones, 
 and their tendency to stick to a conductor and not fly off to other ob- 
 jects depends not only on having them of small resistance, but also on 
 having what we call the self-induction as small as possible. This latter 
 can be diminished by having the lightning rod spread sideways as much 
 as possible, either by rolling it into strips, or better, by making a network 
 of rods over the roof, with several connections to the earth at the corners, 
 as I have before described. 
 
MODERN VIEWS WITH RESPECT TO ELECTRIC CURRENTS 665 
 
 Thus we see that the theory of lightning rods, which appeared so sim- 
 ple in the time of Franklin, is to-day a very complicated one, and re- 
 quires for its solution a very complete knowledge of the dynamics of elec- 
 tric currents. In the light of our present knowledge the frequent fail- 
 ure of the old system of rods is no mystery, for I doubt if there are a 
 hundred buildings in the country properly protected from lightning. 
 With our modern advances, perfect protection might be guaranteed in all 
 cases, if expense were no object. 
 
 So much for the rod itself, and now let us turn to other portions of 
 the electrical system, for we have seen that, in any case, the conductor is 
 only the core of a disturbance which extends to great distances on all 
 sides. Were the clouds, the earth and the streak of heated air called the 
 lightning flash all perfect conductors we could calculate the entire dis- 
 turbance. It might then consist of a series of stationary waves between 
 the two planes, extending indefinitely on all sides but with gradually de- 
 creasing amplitude as we pass away from the centre. The oscillations, 
 once set up, would go on forever, as there would be no poor conductors to 
 damp them. But when the clouds and the path of the lightning both 
 have very great resistance, the energy is very soon converted into heat 
 and the oscillations destroyed. I have given it as my opinion that this 
 is generally the case and that the oscillations seldom take place, but I 
 may be wrong, as there is little to guide me except guesswork. If they 
 take place, however, we have a ready explanation of what is sometimes 
 called a back stroke of lightning. That is, a man at the other end of 
 the cloud a mile or more distant from the lightning stroke sometimes re- 
 ceives a shock, or a new lightning flash may form at that point and kill 
 him. This may be caused, according to our present theory, by the 
 arrival of the waves of electrical disturbance which might themselves 
 cause a slight shock or even overturn the equilibrium then existing and 
 cause a new electric discharge. 
 
 We have now considered the case of oscillations of electricity in a few 
 instances and can turn to that of steady currents. The closing of an 
 electric current sends ethereal waves throughout space, but after the 
 first shock the current flows steadily without producing any more waves. 
 However, the properties of the space around the wire have been per- 
 manently altered, as we have already seen. Let us now study these prop- 
 erties more in detail. I have before me a wire in which I can produce a 
 powerful current of electricity, and we have seen that the space around 
 it has been so altered that a delicately suspended magnetic needle can- 
 not remain quiet in all positions but stretches itself at right angles to 
 
666 HENRY A. ROWLAND 
 
 the wire, the north pole tending to revolve around it in one direction 
 and the south pole in the other. This is a very old experiment, but we 
 now regard it as evidence that the properties of the space around the wire 
 have been altered rather than that the wire acts on the magnet from a 
 distance. 
 
 Put, now, a plate of glass around the wire, the latter being vertical 
 and the former with its plane horizontal, and pass a powerful current 
 through the wire. On now sprinkling iron filings on the plate, they 
 arrange themselves in circles around the wire and thus point out to us 
 the celebrated lines of magnetic force of Faraday. Using two wires 
 with currents in the same direction we get these other curves, and, test- 
 ing the forces acting on the wire, we find that they are trying to move 
 towards each other. 
 
 Again, pass the currents in the opposite directions and we get these 
 other curves and the currents repel each other. If we assume that the 
 lines of force are like rubber bands, which tend to shorten in the direc- 
 tion of their length and repel each other sideways, Faraday and Maxwell 
 have shown that all magnetic attraction and repulsions are explained. 
 The property which the presence of the electric current has conferred on 
 the luminiferous ether is then one by which it tends to shorten in one 
 direction and spread out in the other two directions. 
 
 We have thus done away with action at a distance, and have account- 
 ed for magnetic attraction by a change in the intervening medium as 
 Faraday partly did almost fifty years ago. For this change in the sur- 
 rounding medium is as much a part of the electric current as any thing 
 that goes on within the wire. 
 
 To illustrate this tension along the lines of force, I have constructed 
 this model, which represents the section of a coil of wire with a bar of 
 iron within it. The rubber bands represent the lines of force which pass 
 around the coil and through the iron bar, as they have an easier passage 
 through the iron than the air. As we draw the bar down and let it go, 
 you see that it is drawn upward and oscillates around its position of 
 equilibrium until friction brings it to rest. Here, again, I have a coil 
 of wire with an iron bar within it with one end resting on the floor. 
 As we pass the current and the lines of magnetic force form around 
 the coil and pass through the iron, it is lifted upwards although if 
 weighs 24 pounds and oscillates around its position of equilibrium 
 exactly the same as though it were sustained by rubber bands as 
 in the model. The rubber bands in this case are invisible to our 
 eye, but our mental vision pictures them to us as lines of magnetic 
 
MODERN VIEWS WITH RESPECT TO ELECTRIC CURRENTS 667 
 
 force in the luminiferous ether drawing the bar upward by their con- 
 tractile force. This contractile force is no small quantity, as it may 
 amount, in some cases, to one or even two hundred pounds to the square 
 inch, and thus rivals the greatest pressure which we use in our steam 
 engines. 
 
 Thus the luminiferous ether is, to-day, a much more important factor 
 in science than the air we breathe. We are constantly surrounded by 
 the two, and the presence of the air is manifest to us all; we feel it, he 
 hear by its aid, and we even see it, under favorable circumstances, and 
 the velocity of its motion as well as the amount of moisture it carries is a 
 constant topic of conversation with mankind at large. The luminifer- 
 ous ether, on the other hand, eludes all our senses and it is only with 
 imagination, the eye of the mind, that its presence can be perceived. 
 By its aid in conveying the vibrations we call light, we are enabled to see 
 the world around us, and by its other motions which cause magnetism, 
 the mariner steers his ship through the darkest night when the heavenly 
 bodies are hid from view. "When we speak in a telephone, the vibra- 
 tions of the voice are carried forward to the distant point by waves in 
 the luminiferous ether, there again to be resolved into the sound waves 
 of the air. When we use the electric light to illuminate our streets, it 
 is the luminiferous ether which conveys the energy along the wires as 
 well as transmits it to our eye after it has assumed the form of light. 
 We step upon an electric street car and feel it driven forward with the 
 power of many horses, and again it is the luminiferous ether, whose im- 
 mense force we have brought under our control and made to serve our 
 purpose. No longer a feeble, uncertain sort of medium, but a mighty 
 power, extending throughout all space and binding the whole universe 
 together, so that it becomes a living unit in which no one portion can be 
 changed without ultimately involving every other portion. 
 
 To this, ladies and gentlemen, we have been led by the study of elec- 
 trical phenomena, and the ideas which I have set forth constitute the 
 most modern views held by physicists with respect to electric currents. 
 
G 
 
 ADDRESS DELIVERED AS PRESIDENT OF THE AMERICAN PHYSICAL SOCIETY, AT ITS 
 MEETING IN NEW YORK, OCTOBER 28, 1899 
 
 [American Journal of Science [4] VIII, 401-411, 1899; Science, X, 825-833, 1899J; 
 Johns Hopkins University Circulars, No. 143, pp. 17-20, 1900] 
 
 GENTLEMEN AND FELLOW PHYSICISTS OF AMERICA: We meet to-day 
 on an occasion which marks an epoch in the history of physics in Amer- 
 ica; may the future show that it also marks an epoch in the history of 
 the science which this society is organized to cultivate! For we meet 
 here in the interest of a science above all sciences which deals with the 
 foundation of the universe, with the constitution of matter from which 
 everything in the universe is made and with the ether of space by which 
 alone the various portions of matter forming the universe affect each 
 other even at such distances as we may never expect to traverse, what- 
 ever the progress of our science in the future. 
 
 We, who have devoted our lives to the solution of problems connected 
 with physics, now meet together to help each other and to forward the 
 interests of the subject which we love, a subject which appeals most 
 strongly to the better instincts of our nature and the problems which 
 tax our minds to the limit of their capacity and suggest the grandest 
 and noblest ideas of which they are capable. 
 
 In a country where the doctrine of the equal rights of man has been 
 distorted to mean the equality of man in other respects, we form a small 
 and unique body of men, a new variety of the human race, as one of 
 our greatest scientists calls it, whose views of what constitutes the great- 
 est achievement in life are very different from those around us. In this 
 respect we form an aristocracy, not of wealth, not of pedigree, but of 
 intellect and of ideals, holding him in the highest respect who adds the 
 most to our. knowledge or who strives after it as the highest good. 
 
 Thus we meet together for mutual sympathy and the interchange of 
 knowledge, and may we do so ever with appreciation of the benefits to 
 ourselves and possibly to our science. Above all, let us cultivate the 
 idea of the dignity of our pursuit so that this feeling may sustain us in 
 the midst of a world which gives its highest praise, not to the investiga- 
 
THE HIGHEST AIM OF THE PHYSICIST 669 
 
 tion in the pure ethereal physics which our society is formed to cultivate, 
 but to the one who uses it for satisfying the physical rather than the 
 intellectual needs of mankind. He who makes two blades of grass grow 
 where one grew before is the benefactor of mankind; but he who ob- 
 scurely worked to find the laws of such growth is the intellectual supe- 
 rior as well as the greater benefactor of the two. 
 
 How stands our country, then, in this respect? My answer must still 
 be now, as it was fifteen years ago, that much of the intellect of the 
 country is still wasted in the pursuit of so-called practical science which 
 ministers to our physical needs and but little thought and money is 
 given to the grander portion of the subject which appeals to our intellect 
 alone. But your presence here gives evidence that such a condition is 
 not to last forever. 
 
 Even in the past we have a few names whom scientists throughout the 
 world delight to honor: Franklin, who almost revolutionized the 
 science of electricity by a few simple but profound experiments; Count 
 Eumford, whose experiments almost demonstrated the nature of heat; 
 Henry, who might have done much for the progress of physics had he 
 published more fully the results of his investigations; Mayer, whose 
 simple and ingenious experiments have been a source of pleasure and 
 profit to many. This is the meager list of those whom death allows me 
 to speak of and who have earned mention here by doing something for 
 the progress of our science. And yet the record has been searched for 
 more than a hundred years. How different had I started to record 
 those who have made useful and beneficial inventions! 
 
 But I know, when I look in the faces of those before me, where the 
 eager intellect and high purpose sit enthroned on bodies possessing the 
 vigor and strength of youth, that the writer of a hundred years hence 
 can no longer throw such a reproach upon our country. Nor can we 
 blame those who have gone before us. The progress of every science 
 shows us the condition of its growth. Very few persons, if isolated in 
 a semi-civilized land, have either the desire or the opportunity of pur- 
 suing the higher branches of science. Even if they should be able to do 
 so, their influence on their science depends upon what they publish 
 and make known to the world. A hermit philosopher we can imagine 
 might make many useful discoveries. Yet, if he keeps them to himself, 
 he can never claim to have benefited the world in any degree. His un- 
 published results are his private gain, but the world is no better off 
 until he has made them known in language strong enough to call atten- 
 tion to them and to convince the world of their truth. Thus, to encour- 
 age the growth of any science, the best thing we can do is to meet 
 
670 HENEY A. EOWLAND 
 
 together in its interest, to discuss its problems, to criticise each other's 
 work and, best of all, to provide means by which the better portion of 
 it may be made known to the world. Furthermore, let us encourage 
 discrimination in our thoughts and work. Let us recognize the eras 
 when great thoughts have been introduced into our subject and let us 
 honor the great men who introduced and proved them correct. Let us 
 forever reject such foolish ideas as the equality of mankind and care- 
 fully give the greater credit to the greater man. So, in choosing the 
 subjects for our investigation, let us, if possible, work upon those sub- 
 jects which will finally give us an advanced knowledge of some great 
 subject. I am aware that we cannot always do this: our ideas will often 
 flow in side channels: but, with the great problems of the universe 
 before us, we may some time be able to do our share toward the greater 
 end. 
 
 What is matter; what is gravitation; what is ether and the radiation 
 through it; what is electricity and magnetism; how are these connected 
 together and what is their relation to heat? These are the greater 
 problems of the universe. But many infinitely smaller problems we 
 must attack and solve before we can even guess at the solution of the 
 greater ones. 
 
 In our attitude toward these greater problems how do we stand and 
 what is the foundation of our knowledge? 
 
 Newton and the great array of astronomers who have succeeded him 
 have proved that, within planetary distances, matter attracts all others 
 with a force varying inversely as the square of the distance. But what 
 sort of proof have we of this law? It is derived from astronomical 
 observations on the planetary orbits. It agrees very well within these 
 immense spaces; but where is the evidence that the law holds for smaller 
 distances? We measure the lunar distance and the size of the earth 
 and compare the force at that distance with the force of gravitation on 
 the earth's surface. But to do this we must compare the matter in the 
 earth with that in the sun. This we can only do by assuming the law 
 to be proved. Again, in descending from the earth's gravitation to that 
 of two small bodies, as in the Cavendish experiment, we assume the law 
 to hold and deduce the mass of the earth in terms of our unit of mass. 
 Hence, when we say that the mass of the earth is 5 times that of an 
 equal volume of water we assume the law of gravitation to be that of 
 Newton. Thus a proof of the law from planetary down to terrestrial 
 distances is physically impossible. 
 
 Again, that portion of the law which says that gravitational attrac- 
 
THE HIGHEST AIM OF THE PHYSICIST 671 
 
 tion is proportional to the quantity of matter, which is the same as 
 saying that the attraction of one body by another is not affected by the 
 presence of a third, the feeble proof that we give by weighing bodies in 
 a balance in different positions with respect to each cannot be accepted 
 on a larger scale. When we can tear the sun into two portions and prove 
 that either of the two halves attracts half as much as the whole, then 
 we shall have a proof worth mentioning. 
 
 Then as to the relation of gravitation and time what can we say? 
 Can we for a moment suppose that two bodies moving through space 
 with great velocities have their gravitation unaltered? I think not. 
 Neither can we accept Laplace's proof that the force of gravitation acts 
 instantaneously through space, for we can readily imagine some com- 
 pensating features unthought of by Laplace. 
 
 How little we know then of this law which has been under observa- 
 tion for two hundred years! 
 
 Then as to matter itself how have our views changed and how are 
 they constantly changing. The round hard atom of Newton which 
 God alone could break into pieces has become a molecule composed of 
 many atoms, and each of these smaller atoms has become so elastic that 
 after vibrating 100,000 times its amplitude of vibration is scarcely 
 diminished. It has become so complicated that it can vibrate with as 
 many thousand notes. We cover the atom with patches of electricity 
 here and there and make of it a system compared with which the plane- 
 tary system, nay the universe itself, is simplicity. Nay more: some of 
 us even claim the power, which Newton attributed to God alone, of 
 breaking the atom into smaller pieces whose size is left to the imagina- 
 tion. Where, then, is that person who ignorantly sneers at the study 
 of matter as a material and gross study? Where, again, is that man with 
 gifts so God-like and mind so elevated that he can attack and solve its 
 problem? 
 
 To all matter we attribute two properties, gravitation and inertia. 
 Without these two matter cannot exist. The greatest of the natural 
 laws states that the power of gravitational attraction is proportional to 
 the mass of the body. This law of Newton, almost neglected in the 
 thoughts of physicists, undoubtedly has vast import of the very deepest 
 meaning. Shall it mean that all matter is finally constructed of uniform 
 and similar primordial atoms or can we find some other explanation? 
 
 That the molecules of matter are not round, we know from the facts 
 of crystallography and the action of matter in rotating the plane of 
 polarization of light. 
 
672 HENRY A. EOWLAND 
 
 That portions of the molecules and even of the atoms are electrically 
 charged, we know from electrolysis, the action of gases in a vacuum 
 tube and from the Zeeman effect. 
 
 That some of them act like little magnets, we know from the mag- 
 netic action of iron, nickel and cobalt. 
 
 That they are elastic, the spectrum shows, and that the vibrating 
 portion carries the electrified charge with it is shown by the Zeeman 
 effect. 
 
 Here, then, we have made quite a start in our problem: but how far 
 are we from the complete solution? How can we imagine the material 
 of which ordinary or primordial atoms are made, dealing as we do only 
 with aggregation of atoms alone? Forever beyond our sight, vibrating 
 an almost infinite number of times in a second, moving hither and yon 
 with restless energy at all temperatures beyond the absolute zero of 
 temperature, it is certainly a wonderful feat of human reason and 
 imagination that we know as much as we do at present. Encouraged by 
 these results, let us not linger too long in their contemplation but pre?^ 
 forward to the new discoveries which await us in the future. 
 
 Then as to electricity, the subtile spirit of the amber, the demon who 
 reached out his glutinous arms to draw in the light bodies within his 
 reach, the fluid which could run through metals with the greatest ease 
 but could be stopped by a frail piece of glass! Where is it now? Van- 
 ished, thrown on the waste heap of our discarded theories to be replaced 
 by a far nobler and exalted one of action in the ether of space. 
 
 And so we are brought to consider that other great entity the ether: 
 filling all space without limit, we imagine the ether to be the only 
 means by which two portions of matter distant from each other can 
 have any mutual action. By its means we imagine every atom in the 
 universe to be bound to every other atom by the force of gravitation 
 and often by the force of magnetic and electric action, and we conceive 
 that it alone conveys the vibratory motion of each atom or molecule 
 out into space to be ever lost in endless radiation, passing out into 
 infinite space or absorbed by some other atoms which happen to be in 
 its path. By it all electromagnetic energy is conveyed from the feeble 
 attraction of the rubbed amber through the many thousand horse-power 
 conveyed by the electric wires from Niagara to the mighty rush of 
 energy always flowing from the sun in a flood of radiation. Actions 
 feeble and actions mighty from inter-molecular distances through inter- 
 planetary and inter-stellar distances until we reach the mighty dis- 
 tances which bound the universe all have their being in this wondrous 
 ether. 
 
THE HIGHEST AIM OF THE PHYSICIST 673 
 
 And yet, however wonderful it may be, its laws are far more simple 
 than those of matter. Every wave in it, whatever its length or inten- 
 sity, proceeds onwards in it according to well known laws, all with the 
 same speed, unaltered in direction from its source in electrified matter, 
 to the confines of the universe unimpaired in energy unless it is dis- 
 turbed by the presence of matter. However the waves may cross each 
 other, each proceeds by itself without interference with the others. 
 
 So with regard to gravitation, we have no evidence that the presence 
 of a third body affects the mutual attraction of two other bodies or 
 that the presence of a third quantity of electricity affects the mutual 
 attraction of two other quantities. The same for magnetism. 
 
 For this reason the laws of gravitation and of electric and magnetic 
 action including radiation are the simplest of all laws when we confine 
 them to a so-called vacuum, but become more and more complicated 
 when we treat of them in space containing matter. 
 
 Subject the ether to immense electrostatic, magnetic or gravitational 
 forces and we find absolutely no signs of its breaking down or even 
 change of properties. Set it into vibration by means of an intensely 
 hot body like that of the sun and it conveys many thousand horse-power 
 for each square foot of surface as quietly and with apparently unchanged 
 laws as if it were conveying the energy of a tallow dip. 
 
 Again, subject a millimeter of ether to the stress of many thousand, 
 nay even a million, volts and yet we see no signs of breaking down. 
 
 Hence the properties of the ether are of ideal simplicity and lead to 
 the simplest of natural laws. All forces which act at a distance, always 
 obey the law of the inverse square of the distance and we have also the 
 attraction of any number of parts placed near each other equal to the 
 arithmetical sum of the attractions when those parts are separated. So 
 also the simple law of ethereal waves which has been mentioned above. 
 
 At the present time, through the labors of Maxwell supplemented by 
 those of Hertz and others, we have arrived at the great generalization 
 that all wave disturbances in the ether are electromagnetic in their 
 nature. We know of little or no ethereal disturbance which can be set 
 up by the motion of matter alone: the matter must be electrified in 
 order to have sufficient hold on the ether to communicate its motion 
 to the ether. The Zeeman effect even shows this to be the case where 
 molecules are concerned and when the period of vibration is immensely 
 great. Indeed the experiment on the magnetic action of electric con- 
 vection shows the same thing. By electrifying a disc in motion it 
 appears as if the disc holds fast to the ether and drags it with it, thus 
 
 setting up the peculiar ethereal motion known as magnetism. 
 43 
 
674 HENRY A. KOWLAND 
 
 Have we not another case of a similar nature when a huge gravita- 
 tional mass like that of the earth revolves on its axis? Has not matter 
 a feeble hold on the ether sufficient to produce the earth's magnetism? 
 
 But the experiment of Lodge to detect such an action apparently 
 showed that it must be very feeble. Might not his experiment have 
 succeeded had he used an electrified revolving disc? 
 
 To detect something dependent on the relative motion of the ether 
 and matter has been and is the great desire of physicists. But we 
 always find that, with one possible exception, there is always some com- 
 pensating feature which renders our efforts useless. This one experi- 
 ment is the aberration of light, but even here Stokes has shown that it 
 may be explained in either of two ways: first, that the earth moves 
 through the ether of space without disturbing it, and second, that it 
 carries the ether with it by a kind of motion called irrotational. Even 
 here, however, the amount of action probably depends upon relative 
 motion of the luminous source to the recipient telescope. 
 
 So the principle of Doppler depends also on this relative motion and 
 is independent of the ether. 
 
 The result of the experiments of Foucault on the passage of light 
 through moving water can no longer be interpreted as due to the partial 
 movement of the ether with the moving water, an inference due to 
 imperfect theory alone. The experiment of Lodge, who attempted to 
 set the ether in motion by a rapidly rotating disc, showed no such result. 
 
 The experiment of Michelson to detect the ethereal wind, although 
 carried to the extreme of accuracy, also failed to detect any relative 
 motion of the matter and the ether. 
 
 But matter with an electrical charge holds fast to the ether and 
 moves it in the manner required for magnetic action. 
 
 When electrified bodies move together through space or with refer- 
 ence to each other we can only follow their mutual actions through very 
 slow and uniform velocities. When they move with velocities com- 
 parable with that of light, equal to it or even beyond it, we calculate 
 their mutual actions or action on the ether only by the light of our 
 imagination unguided by experiment. The conclusions of J. J. Thom- 
 son, Heaviside and Hertz are all results of the imagination and they all 
 rest upon assumptions more or less reasonable but always assumptions. 
 A mathematical investigation always obeys the law of the conservation 
 of knowledge: we never get out more from it than we put in. The 
 knowledge may be changed in form, it may be clearer and more exactly 
 stated, but the total amount of the knowledge of nature given out by 
 
THE HIGHEST AIM or THE PHYSICIST 675 
 
 the investigation is the same as we started with. Hence we can never 
 predict the result in the case of velocities beyond our reach, and such 
 calculations as the velocity of the cathode rays from their electro- 
 magnetic action has a great element of uncertainty which we should do 
 well to remember. 
 
 Indeed, when it comes to exact knowledge, the limits are far more 
 circumscribed. 
 
 How is it, then, that we hear physicists and others constantly stating 
 what will happen beyond these limits? Take velocities, for instance, 
 such as that of a material body moving with the velocity of light. There 
 is no known process by which such a velocity can be obtained even 
 though the body fell from an infinite distance upon the largest aggrega- 
 tion of matter in the universe. If we electrify it, as in the cathode 
 rays, its properties are so changed that the matter properties are com- 
 pletely masked by the electromagnetic. 
 
 It is a common error which young physicists are apt to fall into to 
 obtain a law, a curve or a mathematical expression for given experi- 
 mental limits and then to apply it to points outside those limits. This 
 is sometimes called extrapolation. Such a process, unless carefully 
 guarded, ceases to be a reasoning process and becomes one of pure 
 imagination specially liable to error when the distance is too great. 
 
 But it is not my purpose to enter into detail. What I have given 
 suffices to show how little we know of the profounder questions involved 
 in our subject. 
 
 It is a curious fact that, having minds tending to the infinite, with 
 imaginations unlimited by time and space, the limits of our exact 
 knowledge are very small indeed. In time we are limited by a few 
 hundred or possibly thousand years: indeed the limit in our science is 
 far less than the smaller of these periods. In space we have exact 
 knowledge limited to portions of our earth's surface and a mile or so 
 below the surface, together with what little we can learn from looking 
 through powerful telescopes into the space beyond. In temperature 
 our knowledge extends from near the absolute zero to that of the sun 
 but exact knowledge is far more limited. In pressures we go from the 
 Crookes vacuum still containing myriads of flying atoms to pressures 
 limited by the strength of steel but still very minute compared with the 
 pressures at the centre of the earth and sun, where the hardest steel 
 would flow like the most limpid water. In velocities we are limited to 
 a few miles per second; in forces, to possibly 100 tons to the square 
 inch; in mechanical rotations, to a few hundred times per second. 
 
676 HENRY A. ROWLAND 
 
 All the facts which we have considered, the liability to error in what- 
 ever direction we go, the infirmity of our minds in their reasoning 
 power, the fallibility of witnesses and experimenters, lead the scientist 
 to be specially skeptical with reference to any statement made to him 
 or any so-called knowledge which may be brought to his attention. The 
 facts and theories of our science are so much more certain than those of 
 history, of the testimony of ordinary people on which the facts of 
 ordinary history or of legal evidence rest, or of the value of medicines to 
 which we trust when we are ill, indeed to the whole fabric of supposed 
 truth by which an ordinary person guides his belief and the actions of 
 his life, that it may seem ominous and strange if what I have said of 
 the imperfections of the knowledge of physics is correct. How shall we 
 regulate our minds with respect to it: there is only one way that I 
 know of and that is to avoid the discontinuity of the ordinary, indeed 
 the so-called cultivated legal mind. There is no such thing as absolute 
 truth and absolute falsehood. The scientific mind should never recog- 
 nize the perfect truth or the perfect falsehood of any supposed theory 
 or observation. It should carefully weigh the chances of truth and 
 error and grade each in its proper position along the line joining abso- 
 lute truth and absolute error. 
 
 The ordinary crude mind has only two compartments, one for truth 
 and one for error; indeed the contents of the two compartments are 
 sadly mixed in most cases: the ideal scientific mind, however, has an 
 infinite number. Each theory or law is in its proper compartment indi- 
 cating the probability of its truth. As a new fact arrives the scientist 
 changes it from one compartment to another so as, if possible, to always 
 keep it in its proper relation to truth and error. Thus the fluid nature 
 of electricity was once in a compartment near the truth. Faraday's and 
 Maxwell's researches have now caused us to move it to a compartment 
 nearly up to that of absolute error. 
 
 So the law of gravitation within planetary distances is far toward 
 absolute truth, but may still need amending before it is advanced farther 
 in that direction. 
 
 The ideal scientific mind, therefore, must always be held in a state 
 of balance which the slightest new evidence may change in one direction 
 or another. It is in a constant state of skepticism, knowing full well 
 that nothing is certain. It is above all an agnostic with respect to all 
 facts and theories of science as well as to all other so-called beliefs and 
 theories. 
 
 Yet it would be folly to reason from this that we need not guide our 
 
THE HIGHEST AIM OF THE PHYSICIST 677 
 
 life according to the approach to knowledge that we possess. , Nature is 
 inexorable; it punishes the child who unknowingly steps off a precipice 
 quite as severely as the grown scientist who steps over, with full knowl- 
 edge of all the laws of falling bodies and the chances of their being 
 correct. Both fall to the bottom and in their fall obey the gravitational 
 laws of inorganic matter, slightly modified by the muscular contortions 
 of the falling object but not in any degree changed by the previous 
 belief of the person. Natural laws there probably are, rigid and un- 
 changing ones at that. Understand them and they are beneficent: we 
 can use them for our purposes and make them the slaves of our desires. 
 Misunderstand them and they are monsters who may grind us to powder 
 or crush us in the dust. Nothing is asked of us as to our belief: they 
 act unswervingly and we must understand them or suffer the conse- 
 quences. Our only course, then, is to act according to the chances of 
 our knowing the right laws. If we act correctly, right; if we act incor- 
 rectly, we suffer. If we are ignorant we die. What greater fool, then, 
 than he who states that belief is of no consequence provided it is sincere. 
 An only child, a beloved wife, lies on a bed of illness. The physician 
 says that the disease is mortal; a minute plant called a microbe has 
 obtained entrance into the body and is growing at the expense of its 
 tissues, forming deadly poisons in the blood or destroying some vital 
 organ. The physician looks on without being able to do anything. 
 Daily he comes and notes the failing strength of his patient and daily 
 the patient goes downward until he rests in his grave. But why has the 
 physician allowed this? Can we doubt that there is a remedy which 
 shall kill the microbe or neutralize its poison? Why, then, has he not 
 used it? He is employed to cure but has failed. His bill we cheerfully 
 pay because he has done his best and given a chance of cure. The 
 answer is ignorance. The remedy is yet unknown. The physician is 
 waiting for others to discover it or perhaps is experimenting in a crude 
 and unscientific manner to find it. Is not the inference correct, then, 
 that the world has been paying the wrong class of men? Would not 
 this ignorance have been dispelled had the proper money been used in 
 the past to dispel it? Such deaths some people consider an act of God. 
 What blasphemy to attribute to God that which is due to our own and 
 our ancestors' selfishness in not founding institutions for medical re- 
 search in sufficient number and with sufficient means to discover the 
 truth. Such deaths are murder. Thus the present generation suffers 
 for the sins of the past and we die because our ancestors dissipated their 
 wealth in armies and navies, in the foolish pomp and circumstance of 
 
678 HENRY A. ROWLAND 
 
 society, and neglected to provide us with a knowledge of natural laws. 
 In this sense they were the murderers and robbers of future generations 
 of unborn millions and have made the world a charnel house and place 
 of mourning where peace and happiness might have been. Only their 
 ignorance of what they were doing can be their excuse, but this excuse 
 puts them in the class of boors and savages who act according to selfish 
 desire and not to reason and to the calls of duty. Let the present gener- 
 ation take warning that this reproach be not cast on it, for it cannot 
 plead ignorance in this respect. 
 
 This illustration from the department of medicine I have given be- 
 cause it appeals to all. But all the sciences are linked together and 
 must advance in concert. The human body is a chemical and physical 
 problem, and these sciences must advance before we can conquer disease. 
 
 But the true lover of physics needs no such spur to his actions. The 
 cure of disease is a very important object and nothing can be nobler than 
 a life devoted to its cure. 
 
 The aims of, the physicist, however, are in part purely intellectual: 
 he strives to understand the universe on account of the intellectual 
 pleasure derived from the pursuit, but he is upheld in it by the knowl- 
 edge that the study of nature's secrets is the ordained method by which 
 the greatest good and happiness shall finally come to the human race. 
 
 Where, then, are the great laboratories of research in this city, in 
 this country, nay, in the world? We see a few miserable structures here 
 and there occupied by a few starving professors who are nobly striving 
 to do the best with the feeble means at their disposal. But where in 
 the world is the institute of pure research in any department of science 
 with an income of $100,000.000 per year? Where can the discoverer in 
 pure science earn more than the wages of a day laborer or cook? But 
 $100,000,000 per year is but the price of an army or of a navy designed 
 to kill other people. Just think of it, that one per cent of this sum 
 seems to most people too great to save our children and descendants 
 from misery and even death! 
 
 But the twentieth century is near may we not hope for better things 
 before its end? May we not hope to influence the public in this 
 direction? 
 
 Let us go forward, then, with confidence in the dignity of our pur- 
 suit. Let us hold our heads high with a pure conscience while we seek 
 the truth, and may the American Physical Society do its share now and 
 in generations yet to come in trying to unravel the great problem of 
 the constitution and laws of the universe. 
 
BIBLIOGRAPHY 
 
1. The Vortex Problem. 
 
 Scientific American XIII, 308, 1865. 
 
 2. Paine's Electro-magnetic Engine. 
 
 Scientific American XXV, 21, 1871. 
 
 3. Illustration of Resonances and Actions of a Similar Nature. 
 
 Journal of the Franklin Institute XCIV, 275-278, 1872. 
 
 4. On the Auroral Spectrum. 
 
 American Journal of Science (3), V, 320, 1873. 
 
 5. On Magnetic Permeability, and the Maximum of Magnetism of 
 
 Iron, Steel and Nickel. 
 
 Philosophical Magazine (4), XL VI, 140-159, 1873. 
 American Journal of Science (3), VI, 416-425, 1873 (abstract). 
 
 6. On the Magnetic Permeability and Maximum of Magnetism of 
 
 Nickel and Cobalt. 
 Philosophical Magazine (4), XL VIII, 321-340, 1874. 
 
 7. On a new Diamagnetic Attachment to the Lantern, with a Note on 
 
 the Theory of the Oscillations of Inductively Magnetized Bodies. 
 American Journal of Science (3), IX, 357-361, 1875. 
 
 8. Notes on Magnetic Distribution. 
 
 Proceedings of the American Academy of Arts and Sciences, XI, 
 191, 192, 1876. (Presented June 9, 1875.) 
 
 9. Note on Kohlrausch's Determination of the Absolute Value of the 
 
 Siemens Mercury Unit of Electrical Resistance. 
 Philosophical Magazine (4), L, 161-163, 1875. 
 
 10. Preliminary Note on a Magnetic Proof Plane. 
 
 American Journal of Science (3), X, 14-17, 1875. 
 
 11. Studies on Magnetic Distribution. 
 
 American Journal of Science (3), X, 325-335, 451-459, 1875. 
 
 Ibid., XI, 17-29, 103-108. 1876. 
 
 Philosophical Magazine (4), L, 257-277, 348-367, 1875. 
 
 12. On the Magnetic Effeot of Electric Convection. 
 
 American Journal of Science (3), XV, 30-38, 1878. 
 
 See also Monatsberichte Akad. Berlin, pp. 211-216, 1876. 
 
 American Journal of Science (3), XII, 390-394, 1876. 
 
 Philosophical Magazine (5), II, 233-237, 1876. 
 
 Annales de Chimie et de Physique (5), XII, 119-125, 1877. 
 
HENRY A. EOWLAND 
 
 13. Note on the Magnetic Effect of Electric Convection. 
 
 Philosophical Magazine (5), VII, 442-443, 1879. 
 
 14. Note on the Theory of Electric Absorption. 
 
 American Journal of Mathematics, I, 53-58, 1878. 
 
 15. Kesearch on the Absolute Unit of Electrical Eesistance. 
 
 American Journal of Science (3), XV, 281-291, 325-336, 430-439, 1878. 
 
 16. On the Mechanical Equivalent of Heat, with Subsidiary Eesearches 
 
 on the Variation of the Mercurial from the Air-Thermometer and 
 
 on the Variation of the Specific Heat of Water. 
 
 Proceedings of the American Academy of Arts and Sciences, XV, 
 
 75-200, 1880. 
 Atti del K. Institute, Venezia, VII, 1436, 1881. (Appendix.) 
 
 17. On Professors Ayrton and Perry's New Theory of the Earth's Mag- 
 
 netism, with a Note on a New Theory of the Aurora. 
 Philosophical Magazine (5), VIII, 102-106, 1879. 
 Proceedings of the Physical Society, III, 93-98, 1879. 
 
 18. On the Diamagnetic Constants of Bismuth and Calc-spar in Abso- 
 
 lute Measure. By H. A. Eowland and W. W. Jacques. 
 American Journal of Science (3), XVIH, 360-371, 1879. 
 
 19. Preliminary Notes on Mr. Hall's Eecent Discovery. 
 
 American Journal of Mathematics, II, 354-356, 1879. 
 Philosophical Magazine (5), IX, 432-434, 1880. 
 Proceedings of the Physical Society, IV, 10-13, 1880. 
 
 20. Physical Laboratory ; Comparison of Standards. 
 
 Johns Hopkins University Circulars No. 3, p. 31, 1880. 
 
 21. Appendix to Paper on the Mechanical Equivalent of Heat, Contain- 
 
 ing the Comparison with Dr. Joule's Thermometer. 
 
 Proceedings of the American Academy of Arts and Sciences, XVI, 
 
 38-45, 1881. 
 Johns Hopkins University Circulars No. 3, p. 30, 1880 (abstract). 
 
 22. On the Efficiency of Edison's Electric Light. By H. A. Eowland 
 
 and G. F. Barker. 
 American Journal of Science (3), XIX, 337-339, 1880. 
 
 23. On the Motion of a Perfect Incompressible Fluid when no Solid 
 
 Bodies are Present. 
 
 American Journal of Mathematics, III, 226-268, 1880. 
 
 24. On the General Equations of Electro-magnetic Action, with Appli- 
 
 cation to a New Theory of Magnetic Attraction and to the Theory 
 of the Magnetic Eotation of the Plane of Polarization of Light. 
 American Journal of Mathematics, III, 89-113, 1881. 
 
BIBLIOGRAPHY 683 
 
 25. On the New Theory of Magnetic Attractions, and the Magnetic 
 
 Rotation of Polarized Light. 
 Philosophical Magazine (5), XI, 254-261, 1881. 
 
 26. On Geissler Thermometers. 
 
 American Journal of Science (3), XXI, 451-453, 1881. 
 
 27. Electric Absorption of Crystals. By H. A. Rowland and E. L. 
 
 Nichols. 
 
 Philosophical Magazine (5), XI, 414-419, 1881. 
 Proceedings of the Physical Society, IV, 215-221, 1881. 
 
 28. On Atmospheric Electricity. 
 
 Johns Hopkins University Circulars No. 19, pp. 4, 5, 1882. 
 
 29. Preliminary Notice of the Results Accomplished in the Manufacture 
 
 and Theory of Gratings for Optical Purposes. 
 Johns Hopkins University Circulars, No. 17, pp. 248, 249, 1882. 
 Philosophical Magazine (4), XIII, 469-474, 1882. 
 Nature, 26, 211-213, 1882. 
 Journal de Physique, II, 5-11, 1883. 
 
 30. On Concave Gratings for Optical Purposes. 
 
 American Journal of Science (3), XXVI, 87-98, 1883. 
 Philosophical Magazine (5), XVI, 197-210, 1883. 
 
 31. On Mr. Glazebrook's Paper on the Aberration of Concave Gratings. 
 
 American Journal of Science (3), XXVI, 214, 1883. 
 Philosophical Magazine (5), XVI, 210, 1883. 
 
 32. On the Propagation of an Arbitrary Electro-magnetic Disturbance, 
 
 on Spherical Waves of Light and the Dynamical Theory of 
 
 Diffraction. 
 
 American Journal of Mathematics, VI, 359-381, isot. 
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 33. Screw. 
 
 Encyclopaedia Britannica, Ninth Edition, Vol. 21. 
 
 34. The Determination of the Ohm. Extract from a letter to the Inter- 
 
 national Congress at Paris, 1884. 
 
 Proces-Verbaux, Deuxieme Session, p. 37, Paris 1884. 
 
 35. The Theory of the Dynamo. 
 
 Keport of the Electrical Conference at Philadelphia in November, 
 
 1884, pp. 72-83, 90, 91, 104, 107. Washington, 1886. 
 Electrical Keview (N. Y.), Nov. 1, 8, 15, 22, 1884. 
 
 36. On Lightning Protection. 
 
 Report of the Electrical Conference at Philadelphia in November, 
 1884, pp. 172-174. 
 
684 HENRY A. ROWLAND 
 
 37. On the Value of the Ohm. 
 
 La Lumiere Electrique, XXVI, pp. 188, 477, 1887. 
 
 38. On a Simple and Convenient Form of Water-battery. 
 
 American Journal of Science (3), XXXIII, 147, 1887. 
 
 Philosophical Magazine (5), XXIII, 303, 1887. 
 
 Johns Hopkins University Circulars No. 57, p. 80, 1887. 
 
 39. On the Eelative Wave-lengths of the Lines of the Solar Spectrum. 
 
 American Journal of Science (3), XXXIII, 182-190, 1887. 
 Philosophical Magazine (5), XXIII, 257-265, 1887. 
 
 40. On an Explanation of the Action of a Magnet on Chemical Action. 
 
 By H. A. Eowland and Louis Bell. 
 American Journal of Science (3), XXXVI, 39-47, 1888. 
 Philosophical Magazine (5), XXVI, 105-114, 1888. 
 
 41. Table of Standard Wave-lengths. 
 
 Philosophical Magazine (5), XXVII, 479-484, 1889. 
 Johns Hopkins University Circulars No. 73, p. 69, 1889. 
 
 42. A Few Notes on the Use of Gratings. 
 
 Johns Hopkins University Circulars No. 73, pp. 73, 74, 1889. 
 
 43. On the Electro-magnetic Effect of Convection-Currents. By H. A. 
 
 Rowland and C. T. Ilutchinson. 
 Philosophical Magazine (5), XXVII, 445-460, 1889. 
 
 44. On the Ratio of the Electro-static to the Electro-magnetic Unit of 
 
 Electricity. By H. A. Rowland, E. H. Hall, and L. B. Fletcher. 
 American Journal of Science (3), XXXVIII, 289-298, 1889. 
 Philosophical Magazine (5), XXVIII, 304-315, 1889. 
 
 45. Electro-magnetic Waves and Oscillations at the Surface of Con- 
 
 ductors. 
 American Journal of Mathematics, XI, 373-387, 1889. 
 
 46. Report of Progress in Spectrum Work. 
 
 The Chemical News, LXIII, 133, 1891. 
 
 Johns Hopkins University Circulars No. 85, pp. 41, 42, 1891. 
 
 American Journal of Science (3), XLI, 243, 244, 1891. 
 
 47. Notes on the Theory of the Transformer. 
 
 Philosophical Magazine (5), XXXIV, 54-57, 1892. 
 
 Electrical World XX, 20, 1892. 
 
 Johns Hopkins University Circulars No. 99, pp. 104, 105, 1892. 
 
 48. Notes on the Effect of Harmonics in the Transmission of Power by 
 
 Alternating Currents. 
 Electrical World, XX, 368, 1892. 
 La Lumiere Electrique, XLVII, 42-44, 1893. 
 
BIBLIOGRAPHY 685 
 
 49. Gratings in Theory and Practice. 
 
 Philosophical Magazine (5), XXXV, 397-419, 1893. 
 Astronomy and Astro-Physics, XII, 129-149, 1893. 
 
 50. A New Table of Standard Wave-lengths. 
 
 Philosophical Magazine (5), XXXVI, 49-75, 1893. 
 
 Astronomy and Astro-Physics, XII, 321-347, 1893. 
 
 Johns Hopkins University Circulars No. 106, p. 110, 1893. 
 
 51. On a Table of Standard Wave-lengths of the Spectral Lines. 
 
 Memoirs of the American Academy of Arts and Sciences, XII, 101- 
 186, 1896. 
 
 52. The Separation of the Bare Earths. 
 
 Johns Hopkins University Circulars No. 112, pp. 73, 74, 1894. 
 
 53. Modern Theories as to Electricity. 
 
 The Engineering Magazine, VIII, 589-596, 1895. 
 
 54. A Preliminary Table of Solar Spectrum Wave-lengths. 
 
 Astrophysical Journal, I-V, 1895-1897. 
 
 55. Corrections and Additions to Professor H. A. Rowland's Table of 
 
 Solar Spectrum Wave-lengths. 
 Astrophysical Journal VI, 384-392, 1897. 
 
 56. The Arc-Spectra of the Elements. I. Boron and Beryllium. II. 
 
 Germanium. III. Platinum and Osmium. IV. Rhodium, Ru- 
 thenium and Palladium. By II. A. Rowland and R. R. Tatnall. 
 Astrophysical Journal, I, 14-17, 149-153, 1895; II, 184-187, 1895; m, 
 286-291, 1896. 
 
 57. Notes of Observations on the Rontgen Rays. By H. A. Rowland, 
 
 N. R. Carmichael and L. J. Briggs. 
 
 American Journal of Science (4), I, 247, 248, 1896. 
 
 Philosophical Magazine (5), XLI, 381-382, 1896. 
 
 58. Notes on Rontgen Rays. By H. A. Rowland, N. R. Carmichael and 
 
 L. J. Briggs. 
 Electrical World, XXVII, 452, 1896. 
 
 59. The Rontgen Ray and its Relation to Physics. 
 
 Transactions of the American Institute of Electrical Engineers, 
 XIII, 403-410, 430, 431, 1896. 
 
 60. Electrical Measurement by Alternating Currents. 
 
 American Journal of Science (4), IV, 429-448, 1897. 
 Philosophical Magazine (5), XLV, 66-85, 1898. 
 
 61. Arc-Spectra of Vanadium, Zirconium and Lanthanum. By H. A. 
 
 Rowland and C. N. Harrison. 
 
 Astrophysical Journal, VII, 273-294, 373-389, 1898. 
 
686 HENRY A. KOWLAND 
 
 62. Electrical Measurements. By H. A. Eowland and T. D. Penniman. 
 
 American Journal of Science (4), VIII, 35-57, 1899. 
 Johns Hopkins University Circulars No. 135, pp. 51, 52, 1898 
 (abstract) . 
 
 63. Eesistance to Ethereal Motion. By H. A, Eowland, N. E. Gilbert 
 
 and P. C. McJunckin. 
 
 Johns Hopkins University Circulars No. 146, p. 60, 1900. 
 
 64. Diffraction Gratings. 
 
 Encyclopaedia Britannica, New Volumes, III, 458, 459, 1902. 
 
 ADDEESSES 
 
 1. A Plea for Pure Science. Address as Vice-President of Section B 
 of the American Association for the Advancement of Science, 
 Minneapolis, August 15, 1883. 
 
 Proceedings of the American Association for the Advancement of 
 
 Science, XXXII, 105-126, 1883. 
 Science, II, 242-250, 1883. 
 Journal of the Franklin Institute, CXVI, 279-299, 1883. 
 
 2. The Physical Laboratory in Modern Education. Address for Com- 
 
 memoration Day of the Johns Hopkins University, February 
 
 22, 1886. 
 
 Johns Hopkins University Circulars No. 50, pp. 103-105, 1886. 
 
 3. Address as President of the Electrical Conference at Philadelphia, 
 
 September 8, 1884. 
 
 Report of the Electrical Conference at Philadelphia in September, 
 1884, Washington, 1886. 
 
 4. The Electrical and Magnetic Discoveries of Faraday. Address at 
 
 the Opening of the Electrical Club House of New York City, 
 
 1888. 
 
 Electrical Review, Feb. 4, 1888. 
 
 5. On Modern Views with Eespect to Electric Currents. Address 
 
 before the American Institute of Electrical Engineers, New 
 York, May 22, 1889. 
 
 Transactions of the American Institute of Electrical Engineers, VI, 
 
 342-357, 1889. 
 Electrical World, XIII, p. 319, 1889. 
 
 See also Electrical World, XIII, p. 142, 1889. 
 
BIBLIOGRAPHY 687 
 
 6. The Highest Aim of the Physicist. Address as President of the 
 American Physical Society, New York, October 28, 1899. 
 Science, X, 825-833, 1899. 
 
 American Journal of Science (4), VIII, 401-411, 1899. 
 Johns Hopkins University Circulars No. 143, pp. 17-20, 1900. 
 
 REPORTS AND BOOKS 
 
 1. Report of the Electrical Commission Appointed to Consider the 
 
 Location, Arrangement and Operation of Electric Wires in the 
 
 District of Columbia. Washington, 1892. 
 
 By Andrew Rosewater, H. A. Rowland, and Francis R. Skunk. 
 
 2. Elements of Physics. 
 
 By H. A. Rowland and J. S. Ames, New York, 1900, XIII + 263. pp. 
 
DESCRIPTION 
 
 OF 
 
 DIVIDING ENGINES 
 
 44 
 
UN' f.RSITY 
 
A DESCRIPTION OF THE DIVIDING ENGINES DESIGNED 
 BY PROFESSOR ROWLAND. 1 
 
 Three dividing engines were made under Professor Rowland's direc- 
 tion, all embodying the same general principles as given in his article 
 on the " Screw " in the Encyclopedia Britannica (this volume p. 506). 
 The screws of all three have approximately twenty threads to the inch; 
 and the number of teeth in the ratchet wheels of the first, second and 
 third machines is such that they rule 14,438, 15,020 and 20,000 lines in 
 an inch. The three machines are kept in the sub-basement of the 
 Physical Laboratory of the Johns Hopkins University under such con- 
 ditions as will secure a practically constant temperature for long 
 intervals of time. Each machine is driven by a separate water-motor 
 whose speed can be regulated at will. 
 
 The machines have been used almost exclusively for the ruling of 
 Diffraction gratings, although a few centimetre scales have been made. 
 The gratings have been, with only four or five exceptions, made of 
 " speculum metal/' having the composition, copper 126 Ibs. 4 oz., tin 
 58 Ibs. 9 oz., and as homogeneous as possible. The rough metal plates 
 were cast under Professor Rowland's direction, and were then figured 
 and polished. After the ruling was completed, the gratings were care- 
 fully tested in order to see if they were free from "ghosts," diffused 
 light and defective definition. 
 
 To test the screw, ratchet-head and thrust screw for periodic errors, 
 P-ofessor Rowland used the following method: he ruled a space of 
 about one centimetre on a polished surface, then pushed the carriage 
 ba-'k this distance, turned the grating-holder through a minute angle 
 ai again ruled a surface of about the same width as before. There is 
 th - produced a cross-ruling, the lines being slightly inclined to each 
 ot;'?r; and when examined by reflected light, a series of undulations is 
 
 1 Unfortunately Professor Rowland never published a description of these machines ; 
 &nC the Committee has failed to find any information concerning the inception of 
 the idea or the history of the construction of the first machine. It has been 
 thought best, therefore, to give, first, a general description of the design of the 
 engines with various necessary details of some of the working parts and, second, 
 drawings made to scale, showing all the connections of the intricate mechanism ; 
 both of these have been prepared under the direction of J. 8. Ames, Secretary of 
 the Committee, and have been approved by the Committee. 
 
692 HENRY A. KOWLAND 
 
 seen to cross the lines at right angles, corresponding to the points of 
 intersection of the two sets of rulings. This pattern resembles closely 
 in appearance that of watered silk. The corrector of the machine is 
 adjusted until this undulatory pattern is as regular and has as small 
 an amplitude as possible. 
 
 Any description of Eowland's dividing engines, however brief, would 
 be incomplete without some mention of Mr. Theodore Schneider who 
 for twenty-five years was Professor Eowland's mechanician and assistant 
 and who died only a few weeks before him. It was he who made the 
 screws and most of the working parts of the machines, and it was he 
 who superintended the ruling of every grating that has left the Physical 
 Laboratory of the Johns Hopkins University for use elsewhere in the 
 world. 
 
 GENERAL DESIGN OF DIVIDING ENGINE* 
 
 The object of this machine is to rule straight lines on metal or glass 
 surfaces, exactly parallel and at exactly equal distances apart. The sur- 
 face to be ruled is attached to a frame which is moved forward by a nut 
 as it is advanced by a screw; the ruling edge is generally a diamond 
 mounted in such a manner as to be drawn to and fro across the surface to 
 be ruled, but to be in contact with it during <only one of these motions. 
 
 Kotary motion is imparted to the main shaft (48 A) by means of a 
 driving pulley, operated by a belt attached to a water motor (not shown 
 in the cuts). Mounted on the main shaft are the cams (46, 47) for 
 operating the pawl-levers, which turn the screw and advance the nut; 
 the cam (55) controlling the mechanism for raising the diamond; and 
 the crank (50) which by means of the connecting rod and cross-head 
 impart a reciprocating motion to the ruling carriage and its diamond. 
 By means of adjustments in the crank and connecting rod, the length 
 of stroke of the diamond may be varied, and rulings of different lengths 
 are thus obtained. 
 
 In each revolution of the main shaft, the cycle of operations that occur 
 is as follows: Let the diamond be on the plate in a position to begin 
 ruling. It is moved forward, i. e. toward the shaft, by means of the 
 ruling frame and parts described, and a line is ruled. The stroke of 
 the engine being now about to reverse, the cam controlling the mechan- 
 ism for lifting the diamond performs its duty; and, while the engine 
 is on its return stroke, with the diamond off the plate, the latter is 
 
 2 The figures in the text refer to the numbered parts in the cuts which follow the 
 article. 
 
DESCRIPTION OF THE DIVIDING ENGINES 693 
 
 advanced a space equal to the desired distance between the rulings. 
 This is done by the cams operating the pawl-levers (26 and 40), which 
 cause the pawl (41) to rise to a pre-determined position corresponding 
 to one or more teeth of the graduated ratchet head, then to engage this 
 wheel and, being now forced down to its normal position, to cause the 
 wheel and the feed-screw, to which it is attached, to turn through a 
 small definite angle. The rotation of the screw causes the nut to 
 advance towards the ratchet head; and the nut pushes forward the 
 plate-carriage to which the plate to be ruled is secured. The engine 
 being now at the end of its return stroke, the diamond is lowered into 
 contact with the plate, and is ready for ruling the next line. These 
 operations are repeated until the requisite number of lines is ruled. 
 During each cycle of operations a slight additional motion is imparted 
 to the nut and thus to the plate-carriage by means of the corrector 
 mechanism, in order that any periodic errors of the screw, screw-head, 
 etc., may be eliminated. 
 
 The ruling-carriage with its diamond holder moves along truncated 
 V-ways, as shown in the cuts, the surfaces in contact being the 
 steel ways and the box-wood linings to the grooves on the carriage. 
 These box-wood linings press against both the sides and the top of the 
 ways and are adjustable. The plate-carriage moves along V-ways, the 
 surfaces in contact being the steel ways and the cast-iron carriage. 
 These two pairs of ways are accurately at right angles to each other. 
 
 DETAILED DESCRIPTIONS 
 
 I. Mechanism connecting the plate-carriage and the nut. See Fig. 5. 
 The plate-carriage carries a thrust collar (20) through which the 
 
 feed-screw passes freely. It is held in position by pins engaging in the 
 top and bottom of the plate-carriage. The thrust of the nut in advan- 
 cing is communicated by two lugs, one on each side of the nut casings 
 (21), to two correspondingly located screw-heads in the thrust collar; 
 and, finally, screw-heads in the top and bottom of the thrust-collar 
 transfer the thrust to correspondingly located lugs (22) in the plate- 
 carriage. 
 
 II. Pawl mechanism. See Fig. 4. 
 
 The degree of rotation imparted to the graduated ratchet-head de- 
 pends upon the number of teeth the pawl engages in each revolution 
 of the main-shaft and may be varied by altering the size of the cams 
 (46 and 47) on which the pawl-levers 26 and 40 rest. The pawl-lever 
 
694 HENRY A. ROWLAND 
 
 (26), to which the bell-crank (42) is pivoted, causes the pawl to rise to a 
 height corresponding to the number' of teeth to be engaged on the 
 graduated ratchet-head. The other lever (40) has the function of 
 engaging and disengaging the pawl. The cycle of operations that 
 occurs in one revolution of the main shaft is as follows: The pawl-lever 
 (26) is raised by the cam (47), and in so doing gauges the degree of 
 revolution to be imparted to the graduated ratchet-head and feed- 
 screw. The other lever (40), which is pivoted on the pawl-lever (26), 
 is raised further, and thereby permits cam (46) and the bell-crank (42) 
 to carry the pawl (41) forward into engagement with the graduated 
 ratchet-head. The weight (45) attached to the bell-crank arm insures 
 a positive engagement of the pawl. The depth to which the pawl enters 
 between the teeth of the graduated ratchet-head is governed by the 
 adjusting screw (43) and a stop on pa,wl-lever (26). The pawl being 
 engaged, both levers (26 and 40) now descend, causing the graduated 
 ratchet-head and feed-screw to turn to an extent governed by the 
 number of teeth engaged. Lever (40) now descends to a position coin- 
 cident with that of the lever (26), and in so doing causes the stop on 
 lever (40) to press against the adjusting screw (44) on the bell-crank, 
 and thereby withdraws the pawl from the teeth of the graduated ratchet- 
 head. 
 
 III. Diamond and ruling head. See Figs. 1 and 5. 
 
 The diamond (1) is firmly secured by means of solder in a holder 
 (2), which may be adjusted to different inclinations. The frame 
 carrying the diamond, holder and dash-pot has an axle, centering in 
 bearing screws (3) and contained in an adjustable support (4). This 
 support may be raised or lowered to meet the requirements of plates of 
 different thickness. Normally, the end of the frame carrying the 
 diamond and holder, owing to its predominance of weight, would cause 
 the diamond to be in contact with the plate continuously. In order to 
 raise it on the return stroke of the engine, a weighted lift rod (57) is 
 caused to press on the end of the frame near the dash-pot. The height 
 to which the diamond is thus lifted off the plate is governed by nuts, 
 which may be adjusted on the stem of the lift-rod and which on their 
 descent come to rest on the plate 56 A. 
 
 The raising of the weighted lift-rod is primarily caused by cam (55) 
 on the main shaft; the intermediate mechanism consists of the lever 
 (54), vertical oscillating rod (53), reciprocating rod (35), rocking stem 
 (34), and lifting lever (56). The action of the dashers and dash-pot 
 
DESCRIPTION OF THE DIVIDING ENGINES 695 
 
 filled with, oil is to dampen any vibrations of the frame which carries 
 the diamond, and to check its descent on the plate. 
 
 IV. Corrector mechanism. See Figs. 1, 4 and 5. 
 
 The wear of the threads contained in the lignum vitas plugs of the 
 split nut-casing is taken up by the screws in the adjusting rings (17), 
 bringing the two parts of the nut closer to the feed-screw. Each side 
 of the nut is provided with a wing-shaped lever, the lower ends of which 
 are confined in guides forming part of the lower corrector frame (39); 
 but they are free to travel in the direction that the nut moves. When 
 the screw is turning and the nut advancing, these wings are pressed 
 tight against the guide-plate (39 A) of the corrector frame; and thus 
 the nut will receive additional motions from any displacement of the 
 corrector. In this manner periodic errors of the screw may be neutral- 
 ized by the action of the corrector. The precise amount of correction 
 is controlled by the adjustments of the eccentric (25). This gives the 
 requisite amount of movement at the proper instants to the corrector 
 lever (28), which in turn moves the rocking shaft, corrector frame, 
 crank, lower frame and, finally, the wings of the nut. The disc (24) 
 may be adjusted and clamped, as shown in Fig. 4, in different positions 
 in the plane of the graduated ratchet-head; and the position of the 
 corrector eccentric (25) with respect to a fixed radius of the graduated 
 ratchet-head must be such as to make the phase of the correction oppo- 
 site that of the periodic error. The amount of eccentricity of the eccen- 
 tric can be varied by means of set-screws, as is evident from the cut; 
 and this must be regulated so that the amplitude of the correction 
 equals that of the periodic error. 
 
 DESCRIPTIVE DRAWINGS OF DIVIDING ENGINE No. 3 
 
 At the end of this article are five cuts of dividing engine No. 3, drawn 
 to scale, one quarter of the actual size, showing different views and 
 operations. They may be described as follows: 
 
 Fig. 1. Side elevation, showing the engine in a ruling position. 
 
 Fig. 2. Plan view of the foregoing. 
 
 Fig. 3. Plan view, showing the plate-carriage. The plate, plate- 
 holder and ruling-head are omitted. 
 
 Fig. 4. Side elevation opposite to Fig. 1, showing the engine in 
 the return stroke position. 
 
 Fig. 5. Transverse sectional elevation, showing the feed-screw, nut, 
 etc. The mechanism actuating the corrector-frame is shown as an 
 end-view. 
 
696 HENRY A. EOWLAND 
 
 Explanation of Numbers in the Cuts 
 (Similar numerals refer to like parts throughout the different views.) 
 
 1. Euling diamond. 
 
 2. Adjustable diamond holder. 
 
 3. Adjustable support for the axis of the diamond-frame. 
 
 4. Euling-head, carrying ruling mechanism. 
 
 5. Bods of the ruling carriage. 
 
 6. Plate to be ruled. 
 
 7. Adjustable box-wood slides of ruling carriage. (N. B. There are 
 
 box-wood slides pressed against the sides as well as the top of 
 the ways of the frame.) 
 
 8. Plate-holder. 
 
 9. Clamps for plate-holder. 
 
 10. Bed-plate. 
 
 11. Plate-carriage, which is moved by the nut and which rests on ways. 
 
 (N. B. The plate-carriage has a cross-beam below the feed- 
 screw. See Fig. 5.) 
 
 12. Feed-screw. 
 
 13. Hardened steel step in end of feed-screw. 
 
 14. Hardened steel thrust-screw. 
 
 15. Casing of the split nut, holding the plugs 16. 
 
 16. Lignum vitas plugs, tapped for engaging feed-screw. 
 
 17. Adjusting rings for nut, with their adjusting screws. 
 
 18 and 19. Wings of the nut, controlled by the corrector, 39 A. 
 
 20. Thrust collar, loosely attached to plate-carriage, 11. 
 
 21. Abutting lugs, rigidly attached to nut-casing 15, and in contact 
 
 with collar 20. 
 
 22. Abutting lugs of plate-carriage, in contact with screw-heads in 
 
 collar 20. 
 
 23. Graduated ratchet-head attached to the feed-screw. 
 
 24. Disc for phase-adjustment of corrector, being movable around the 
 
 axis of the screw in the plane of the ratchet wheel. 
 
 25. Eccentric for adjusting amplitude of corrector, being movable 
 
 around an axis near one end so as to vary the eccentricity. 
 
 26. Pawl-lever, which raises or lowers the pawl, when it is disengaged 
 
 or engaged, respectively, in the ratchet wheel by means of lever 
 40. 
 
 27. Hollow arbor, serving as pivot for pawl-lever. 
 
 28. Corrector lever, resting on 25, and pivoted at 31. 
 
 29. Corrector frame. 
 
DESCRIPTION or THE DIVIDING ENGINES 697 
 
 30. Hardened steel centres for corrector frame. 
 
 31. Eocking shaft, rotated by means of lever 28. 
 
 32. Bearing for wrist-pin of lower corrector frame. 
 
 33. Crank for rocking corrector; a slight rotation of the shaft 3?, thus 
 
 giving a slight sidewise motion to the frame 39. 
 
 34. Hocking stem, which moves the lifting-lever 56, of ruling head. 
 
 35. Eod to communicate reciprocating motion to 34. 
 
 36. Base-frame of engine. 
 
 37. Casings of ruling carriage, holding the adjustable box-wood slides, 7. 
 
 38. Adjustable weight for corrector lever. 
 
 39. Lower corrector frame, moved by the crank 33. 
 
 39 A. Corrector guide-plate, along which the wings of the nut move. 
 
 40. Lever for engaging and disengaging pawl, by means of bell-crank 42. 
 
 41. Pawl, driving ratchet wheel. 
 
 42. Bell-crank which is pivoted on 26; to one end the pawl is attached, 
 
 and the other is raised by the lever 40 and lowered by the 
 weight 45. 
 
 43 and 44. Adjusting screws attached to 42, for regulating the pawl 
 engagement. The stops are attached to 26 and 40. 
 
 45. Weight hanging from bell-crank. 
 
 46. Cam operating lever, 40; attached to main shaft. 
 
 47. Cam operating pawl-lever, 26; attached to main shaft. 
 
 (These two cams regulate the number of teeth of ratchet wheel 
 which the pawl clears each revolution of the main-shaft.) 
 
 48. Driving pulley, attached to main shaft. 
 48 A. Main shaft. 
 
 49. Connecting rod to give reciprocating motion to diamond-holder by 
 
 means of 52 and 37. 
 
 50. Crank arm, designed to vary the length of stroke of the diamond. 
 
 51. Bar connecting cross-head 52, and ruling frame 37. 
 
 52. Cross-head, driven by connecting rod 49. 
 
 53. Oscillating rod, connecting 35 and 54. 
 
 54. Lever operating stop mechanism for lifting diamond, resting on 55. 
 
 55. Cam attached to main shaft and operating the lever 54. 
 
 56. Lever for lifting rod 57; it is operated by the rocking-stem 34. 
 56 A. Stop-plate regulating drop of rod 57. 
 
 57. Rod for lifting diamond. 
 
 58. Dash-pot attached to the lever which carries the diamond-holder 2, 
 
 and which is pivoted at 3. 
 
 59. Adjustments for holding and regulating the dashers. 
 
FIG. i 
 
 Side elevation, showing the engine in a ruling position 
 
SIDE ELEVATION, SHOWING T 
 
L. 
 
 :NGINE IN A RULING POSITION. 
 
FIG. 2 
 
 Plan view of the foregoing 
 
LJ-T 
 
 FIG. 2. 
 PLAN VIEW OF THE FOREGOING. 
 
FIG. 3 
 
 Plan view, showing the plate-carriage. The plate, plate-holder and 
 ruling-head are omitted 
 
46 
 
 :0 ! (O) 
 
 -65 
 
 LnJ 
 
 FIG. 3. 
 
 PLAN VIEW, SHOWING THE PLATE-CARRIAGE. 
 THE PLATE, PLATE-HOLDER AND RULING-HEAD ARE OMITTED. 
 
FIG. 4 
 
 Side elevation opposite to Fig. i, showing the engine in the return 
 
 stroke position 
 
SIDE ELEVATION OPPOSITE TO FIG. 1, SHOWINi 
 
HE ENGINE IN THE RETURN STROKE POSITION. 
 
CO 
 
 z 
 < 
 
 X 
 
 o 
 
 LU 
 
 UJ 
 
 X . 
 
 ^ 
 
 UJ 
 
 d> 
 
 I- Q 
 
 u z 
 
 UJ 
 
 g. 
 
 -IS 
 
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INDEX 
 
 Numbers refer to pages. 
 
 Aberration Problems, 674. 
 Abney, Sir William de W., 491, 499, 
 
 574. 
 Absorption, Electric, 139, 297, 319, 
 
 321. 
 Absorption, Electric, of Crystals, 
 
 204. 
 Academy of Arts and Sciences, 
 
 American, 7, 343, 611. 
 Academy of Sciences, National, 1, 
 
 15, 610. 
 
 Academy, French, 411. 
 Aepinus, 626, 639. 
 Air-thermometer, 358, 366. 
 Alternating Currents, 276, 280, 294, 
 
 314, 661. 
 
 Amagat, E. H., 410. 
 Amaury (see Jamin), 344, 388. 
 Ames, J. S., 525, 551, 691. 
 Ampere, 627, 639. 
 Anderson's Method of Measuring 
 
 Resistance, 308. 
 Angstrom, A. J., 512, 513, 546, 553, 
 
 555. 
 
 Angstrom's Scale, 517, 553. 
 Arago, 642. 
 
 Archimedes, 619, 620, 621. 
 Atmospheric Electricity, 183, 212. 
 Aurora, Spectrum of the, 2, 31. 
 Aurora, Theory of the, 179. 
 Ayrton, W. E., 179, 182, 183, 213, 278. 
 
 Barker, George F., 3, 200, 364, 570. 
 Barometer, 362. 
 Basic Lines of Lockyer, 524. 
 Battery, Water, 241. 
 Baudin's Thermometers, 364, 386, 
 465. 
 45 
 
 Becquerel, A. C., 184, 214. 
 
 Beek, A. van, 411. 
 
 Bell, Graham, 574. 
 
 Bell, Louis, 242, 513 et seq., 545, 546, 
 
 553 et seq. 
 
 Benzenberg, J. F., 411. 
 Berard, J. E., 409, 410. 
 Berlin, University of, 4, 128. 
 Berlin Academy, 4. 
 Biot, J. B., 39, 90, 114, 116, 626, 627, 
 
 639. 
 
 Bosscha, J., 408, 465. 
 Boyle, Eobert, 7. 
 Brashear, J. A., 9. 
 Bravais, A., 411. 
 Briggs, L. J., 571, 573. 
 B. A. Unit, 82, 84, 145, 146, 156, 217, 
 
 239. 
 Bruce, Miss, 521. 
 
 O. 
 
 Calorimetry, 387. 
 
 Canton, John, 625. 
 
 Capacity, Electric, 297 et seq., 314 
 et seq. 
 
 Carmichael, N. E., 571, 573. 
 
 Cathetometer, 361. 
 
 Cavendish, Henry, 626, 639. 
 
 Cazin, A. A., 36, 48, 410. 
 
 Chapman (see Eutherfurd), 8. 
 
 Chemical Reaction, Action of Mag- 
 net on, 242. 
 
 Clarke, F. W., 570. 
 
 Clausius, E. J. E., 204, 205, 210. 
 
 Clement (see Desormes), 410. 
 
 Colardeau, 249. 
 
 Concave Gratings, 488, 492, 505. 
 
 Condenser, Standard, 267. 
 
 Convection, Electric, 128, 138, 179, 
 251. 
 
 Copernicus, 614. 
 
700 
 
 INDEX 
 
 Coulomb, C. A., 95, 96, 103, 119, 120, 
 
 123, 626, 639, 645. 
 Cremieu, V., 5. 
 Crystals, Electric Absorption of, 
 
 204. 
 Crystals, Magnetic Properties of, 
 
 187. 
 
 B. 
 
 Daniell, J. F., 641. 
 
 Davy, Sir Humphry, 638, 639, 644, 
 
 650. 
 
 De Morgan, 619. 
 Delaroche, F., 409, 410. 
 Deluc, J. A., 387. 
 Desormes, C. B., 410. 
 Diamagnetism, 75, 184. 
 Distribution, Magnetic, 80, 85, 89. 
 Dividing Engines, 487, 508, 693. 
 Doppler's Principle, 674. 
 Dub, C. J., 36. 
 Du Fay, 639. 
 Dulong, P. L., 438. 
 Duncan, Louis, 283. 
 Dupre, Athanase, 410. 
 
 Earths, The Rare, 565. 
 
 Echelon Spectroscope, 590. 
 
 Edelmann, M. T., 266. 
 
 Edison's Electric Light, 200. 
 
 Edlund, E., 408, 416, 632. 
 
 Electric Absorption, 139, 297, 319, 
 
 321. 
 Electric Absorption of Crystals, 
 
 204. 
 Electric Convection, 128, 138, 179, 
 
 251. 
 
 Electric Currents, Theory of, 653. 
 Electric Light, Edison's, 200. 
 Electric Units, 10. 
 Electric Units, Ratio of, 266. 
 Electrical Congresses, 10, 212, 217. 
 Electricity, Theories of, 285, 635. 
 Electricity, Atmospheric, 183, 212. 
 Electrodynamometer, 268, 284, 294, 
 
 314. 
 
 Electrometer, Absolute, 266. 
 Elements in the Sun, 522. 
 Ellis, Wm., 357. 
 
 Energy, Conservation of, 2, 6, 24. 
 Energy of Alternating Currents, 
 
 283. 
 
 Ether, Properties of the, 290 et 
 seq., 338, 580, 586, 632, 667, 673. 
 
 Ethereal Motion, Resistance to, 
 338. 
 
 Expansion of Air under Constant 
 Volume, 410. 
 
 F. 
 
 Fairbairn, Sir Wm., 416. 
 
 Faraday, M., 24, 26, 40, 43, 56, 89, 
 
 155, 184, 224, 242, 251, 286, 288, 
 
 289, 596, 604, 616, 626, 629, 630, 
 
 638 et seq., 660, 666. 
 Faraday's Lines of Force, 37, 127, 
 
 286. 
 
 Farrand, 12. 
 Fastre's Thermometers, 365, 386, 
 
 416. 
 
 Faure, 650. 
 
 Favre, P. A., 408, 410, 421. 
 Fiske, Lieut,, 238. 
 Fitzgerald, G. F., 229, 231. 
 Flaugergues, H., 387. 
 Fleming, J. A., 278. 
 Fletcher, L. B., 266. 
 Fortin-barometer, 362. 
 Foster, Henry, 411. 
 Foucault, J. B. L., 674. 
 Foucault-currents, 219, 234. 
 Frankfort - Lauffen Experiments, 
 
 884. 
 Franklin, Benjamin, 625, 639, 663, 
 
 665, 669. 
 
 Fraunhofer, J., 7. 
 Fresnel, A., 580. 
 Friction Brake, 423. 
 
 G. 
 
 Galileo, 614. 
 
 Galvani, 626, 639. 
 
 Galvanometers, 40, 159, 165, 268. 
 
 Gaugain, J. M., 42. 
 
 Gauss, 97, 148, 181, 626. 
 
 Gay Lussac, 410. 
 
 Geissler Thermometers, 465, 478, 
 
 481. 
 Ghosts in Spectra, 490, 492, 510, 519, 
 
 536. 
 
 Gibbs, O. Walcott, 364, 570. 
 Gilbert, N. E., 338. 
 Gilbert, William, 624, 639. 
 Gilman, D. C., 14, 15. 
 Glazebrook, R. T., 240, 505. 
 
INDEX 
 
 701 
 
 Goldingham, John, 411. 
 
 Gramme Armature, 222, 224, 227, 
 
 228. 
 
 Gratings, 7, 487, 492, 587, 525. 
 Gratings, Concave, 488, 492, 505. 
 Gratings, Nobert, 8, 555. 
 Gratings, Manufacture of, 487, 508, 
 
 693. 
 
 Gratings, Use of, 519. 
 Gratings, Wandschaft's, 549. 
 Grating-spectroscope, 489, 499, 512, 
 
 551, 588. 
 
 Gravitation, Cause of, 292. 
 Gravitation, Law of, 670. 
 Gray, Stephen, 624, 639, 653. 
 Green, George, 39, 90, 108, 114, 115, 
 
 116, 627, 630. 
 Green, James, 362. 
 Grooves in Gratings, Theory of, 
 
 529 et seq. 
 Guerricke, Otto v., 639. 
 
 H. 
 
 Hall, E. H., 197, 266. 
 
 Hall Effect, The, 197. 
 
 Harmonics in Alternating Cur- 
 rents, 276, 280, 300, 301. 
 
 Harris Unit Jar, 208, 209. 
 
 Harrison, C. N., 685. 
 
 Harvard University, 5. 
 
 Hastings, C. S., 7, 503. 
 
 Heat, Mechanical Equivalent of, 5, 
 343 et seq., 469. 
 
 Heaviside, Oliver, 674. 
 
 Helmholtz, H. von, 4, 29, 83, 128, 
 131, 138, 159, 167, 179, 251, 314, 
 586, 630, 643. 
 
 Henry, Joseph, 53, 578, 657, 669. 
 
 Hertz, H., 289, 580, 658, 659, 673, 674. 
 
 Herwig, H. A. B., 416. 
 
 Hidden, 570. 
 
 Himstedt, F., 5. 
 
 Him, G. A., 344, 388, 408, 410, 416, 
 418, 423, 424. 
 
 Holman, S. W., 364, 384. . 
 
 Hutchinson, C. T., 4, 251. 
 Hysteresis, 276 et seq., 281. 
 
 I. 
 
 Icilius, Quintus, 36, 408, 418. 
 Inductance, Measurement of, 294 
 
 et seq., 314, 325. 
 lonization of Gases, 579. 
 
 J. 
 
 Jacobi, M. H. v., 36. 
 
 Jacobi Unit, 147. 
 
 Jacques, W. W., 80, 81, 145, 174, 184, 
 
 193. 
 Jamin, J. C., 71, 80, 81, 89, 90, 96, 97, 
 
 122 et seq., 344, 388, 410. 
 Jenkin, Fleming, 150, 169. 
 Jewell, L. E., 524, 545, 550. 
 Johns Hopkins University, 4. 
 Jolly, P. G., 410. 
 Joule, 6, 7, 24, 27, 36, 52, 53, 146, 344, 
 
 381, 408, 414, 416, 417, 419, 421, 
 
 469. 
 Joule's Thermometers, 417, 469. 
 
 K. 
 
 Kelvin, Lord (see Thomson, Sir 
 
 William). 
 
 Kempf, P., 546, 553, 555. 
 Kew Thermometers, 363, 366, 381, 
 
 466. 
 
 Kimball, A. L., 239. 
 Kirchhoff, G. B., 145, 156, 239, 419, 
 
 628. 
 
 Koenig, Rudolph, 29, 217. 
 Kohlrausch, F. W., 4, 82, 83, 84, 146 
 
 et seq., 410, 421, 628. 
 Koyl, C. A., 549, 555. 
 Kriiss, Dr., 566, 570. 
 Kurlbaum, F., 546, 553, 554, 555. 
 
 Laboratories, Physical, 614. 
 Laboulaye, C. P. L. de, 410. 
 Langley, S. P., 491. 
 Laplace, 626, 639, 671. 
 Lecher, E., 4, 252. 
 Lenard, P., 576, 585. 
 Lenz, H. F. E., 36, 408, 418. 
 Lightning, 236. 
 Lightning-rods, 237, 663. 
 Lippmann, G., 5. 
 Lockyer, Sir J. Norman, 487, 524. 
 Lodge, Sir O. J., 662, 664, 674. 
 Lorenz, L. V., 146, 155, 156, 217, 239, 
 419. 
 
 Magnetic Circuit, 3, 38, 89, 225, 276. 
 Magnetic Distribution, 80, 85, 89. 
 
702 
 
 INDEX 
 
 Magnetic Induction, Measurement 
 
 of, 98. 
 
 Magnetic Permeability, 35, 56. 
 Magnetic Proof Plane, 85. 
 Magnetism of Earth, 179, 213. 
 Magnetism, Cause of, 673. 
 Magnets, Lifting Power of, 52. 
 Magnets and Chemical Reactions, 
 
 242. 
 
 Magnetization, Maximum, 35, 56. 
 Magnetization, Temporary, 49. 
 Magnus, H. G., 410. 
 Marcou, P. B., 216. 
 Marianini, S. G., 71. 
 Martins, C. F., 411. 
 Mascart, E., 240. 
 Masson, A. P., 410. 
 Matthiessen, A., 147. 
 *Maxwell, J. C., 3, 52, 57, 71, 83, 89, 
 
 114, 128, 139, 149, 170, 198, 199, 
 
 224, 251, 289, 580, 660, 673. 
 Maxwell's Electromagnetic The- 
 
 ory, 7, 198, 199, 289, 630, 631. 
 Mayer, Alfred M., 669. 
 Mayer, J. R., 24. 
 McFarlane, D., 437, 438. 
 McJunckin, P. C., 338. 
 Mechanical Equivalent of Heat, 
 
 343, 469. 
 
 Mendenhall, T. C., 1. 
 Michelson, A. A., 584, 590, 674. 
 Michie, Professor, 15. 
 Moll, G., 411. 
 
 Motors, Electric, 280, 281. 
 Miiller, G., 546, 553, 555. 
 Miiller, J. H. J., 35, 36, 48. 
 Miinchausen, v., 344, 389. 
 Murphy, Robert 626. 
 Myrback, v., 411. 
 
 National Academy of Sciences, 1, 
 
 15, 610. 
 Nesbit, 53. 
 
 Neumann, F. E., 146, 387. 
 Neumann's Coefficient, 35, 57, 73, 
 
 116. 
 Newton, Sir Isaac, 56, 286, 293, 615, 
 
 623, 638, 671. 
 
 Nichol, J. P., 435, 437, 438. 
 Nichols, E. L., 204, 249, 250. 
 
 Niven's Method of Measuring In- 
 ductance, 309. 
 Nobert Gratings, 8, 555. 
 
 O. 
 
 Oersted, 626, 639, 640. 
 
 Ohm, Determination of the, 217, 
 239, 419, 628. 
 
 Ohm's Law for Currents, 139, 141, 
 238, 640. 
 
 Ohm's Law for Magnetic Induc- 
 tion, 3, 38, 89, 90. 
 
 P. 
 
 Paine's Electromagnetic Engine, 
 
 24. 
 
 Parry, E., Capt., 411. 
 Peirce, C. S., 492, 494, 513 et seq., 
 
 545 et seq. 
 
 Penniman, T. D., 297, 298, 314. 
 Permeability, Magnetic, 35, 56, 73. 
 Perry, John, 179, 182, 183, 213. 
 Petit, P., 438. 
 
 Pfaundler, L., 344, 351, 388, 467. 
 Phillips Academy, Andover, 11. 
 Pickering, E. C., 364. 
 Pickering, W., 343. 
 Plante, G., 650. 
 Platter (see Pfaundler), 344, 351, 
 
 388, 467. 
 
 Pliicker, J., 184. 
 Poggendorff, J. C., 348. 
 Poisson, 626, 630, 639. 
 Porous Plug Experiment, 346. 
 Porter, A. W., 580. 
 Power, Transmission of, 280. 
 Proof Plane, Magnetic, 85. 
 Puluj, J., 408, 424. 
 Pupin, M. L, 584, 585, 586. 
 
 Radiation of Heat, 435. 
 
 Rankine, W. J. M., 381. 
 
 Rayleigh, Lord, 240, 294, 525, 528, 
 
 534, 588, 628. 
 
 Rays, Rontgen, 571, 573, 576. 
 Recknagel, G. F., 356, 358, 389. 
 Regnault, V., 344, 353 et seq., 365, 
 
 368, 376, 388 et seq., 409 et seq., 
 
 466, 607. 
 Remsen, Ira, 242 et seq. 
 
 * References to Maxwell are so numerous that only the more important ones are noted here. 
 
INDEX 
 
 703 
 
 Rensselaer Polytechnic Institute, 
 2, 12. 
 
 Resistance, Electrical; Effect of 
 Magnetic field on, 338. 
 
 Resistance, Electrical; Measure- 
 ment of, 313. 
 
 Resolving Power, 502, 528, 588. 
 
 Resonances, 2, 28. 
 
 Richard (see Jamin), 410. 
 
 Riecke, E., 36. 
 
 Ritter, J. W., 639, 650. 
 
 Rontgen, W. C.^4, 252^ 410, 414. 
 
 Rontgen-rays, 571, 573, 576. 
 
 Rogers, W. A., 441, 507. 
 
 Rosa, E. B., 266. 
 
 Royal Society of London, 3. 
 
 Ruling- Engines, 8, 487, 508, 691. 
 
 Rumford, Count, 6, 408, 416, 669. 
 
 Rumford-fund, 7, 343, 521, 548. 
 
 Rutherfurd, L. W., 8, 487, 494, 513. 
 
 Savart, F., 411, 627. 
 
 Schiller, N. N., 252. 
 
 Schneider, Theodore, 9, 487, 692. 
 
 Scott, C. F., 237. 
 
 Screws, Perfect, 8, 487, 506. 
 
 Sears, David, 80, 98. 
 
 Seebeck, L. F. W. A., 134, 640. 
 
 Shroder v. d. Kolk, 411, 414. 
 
 Siemens Armature, 219, 221,. 222, 
 228. 
 
 Siemens Unit, 4, 147, 152, 155, 156. 
 
 Silbennann, J. T., 408, 410, 421. 
 
 " Skin-Effect " of Alternating Cur- 
 rents, 283, 661. 
 
 Solar Spectrum, 9, 512, 521. 
 
 Sound, Velocity of, 411. 
 
 Specific Heats of Air, Ratio of, 410. 
 
 Specific Heats of Gases, 409, 410. 
 
 Specific Heat of Water, 387. 
 
 Spectroscope, Concave Grating, 489, 
 499, 512, 551, 589. 
 
 Spectroscope, Plane Grating 1 , 588. 
 
 Spectrum of the Aurora, 2, 31. 
 
 Spectrum, Solar, 512, 521. 
 
 Stampfer, S., 411. 
 
 Stefan, J., 69. 
 
 Steinheil, 160, 168. 
 
 Steinmetz, C. P., 278. 
 
 Stokes, Sir G. G., 674. 
 
 Stoletow, A. G., 36, 48, 50, 71, 73, 91, 
 
 105, 154. 
 Sturgeon, William, 53. 
 
 T. 
 
 Tate, T., 416. 
 
 Tatnall, R. R., 685. 
 
 Telegraph, Multiplex Printing, 10. 
 
 Temperature, Absolute Scale of, 
 
 381. 
 
 Temperature, Effect of, on Mag- 
 netization, 58, 65, 74. 
 Tesla, Nicola, 578. 
 Thalgn, T. R., 513, 546, 555. 
 Thermometers, Air, 358, 366. 
 Thermometers, Mercurial, 346, 363. 
 Thermometers, Mercurial and air, 
 
 352. 
 Thermometers, Comparisons of, 
 
 477. 
 
 Thermometers, Standard, 363. 
 Thermometry, 345, 439. 
 Thiessen, M. F., 481. 
 Thompson, S. P., 233, 234, 235. 
 Thomson, Elihu, 232, 235, 573, 574, 
 
 584, 585. 
 
 Thomson, J. J., 579, 674. 
 *Thomson, Sir William, 37, 77, 78. 
 
 79, 148, 213, 346, 381, 414, 421, 
 
 626, 649, 657. 
 
 ThiTnderstorms, Theory of, 183, 213. 
 Transformers, Theory of, 276, 280. 
 Tresca, H. E., 410, 513. 
 Trowbridge, John, 215, 364. 
 Tyndall, John, 26, 27, 97, 574, 641. 
 
 V. 
 
 Venetian Institute; Prize Essay, 7. 
 
 Verdet, M. E., 58, 79. 
 
 Violle, J. L. G., 408, 418. 
 
 Vogel, H. C., 549, 556, 557. 
 
 Volta, 626, 639, 645. 
 
 Vortex in Outlet of Water, 23. 
 
 Waldo, L., 481. 
 Waltenhofen, A. K, 421. 
 Wandschaft's Gratings, 549. 
 Water, Specific Heat of, 387. 
 Water Battery, 241. 
 
 * The references to Lord Kelvin are so numerous that only the important ones are noted 
 here. 
 
704 
 
 INDEX 
 
 Wave-leng-ths, Standard, 512, 517, 
 
 521, 545, 548. 
 Webb, F. C., 38, 
 Weber, 36, 48, 49, 125, 137, 147, 148, 
 
 152, 153, 156, 160, 170. 184, 240, 
 
 408, 418, 419, 626, 628. 
 Weber, H. F., 155, 408, 418, 419, 420. 
 Weisbach, J., 410. 
 Welsh's Thermometers, 365. 
 Welter, J. J., 410. 
 West Point Military Academy, 14. 
 Wheatstone, C., 649. 
 Wiedemann, E., 409, 415. 
 
 Wiedemann, G., 240. 
 Wilke, J. K, 639. 
 Wollaston, W. H., 604. 
 Wiillner, A., 368, 410. 
 
 Y. 
 
 Yale University, 11. 
 Young, C. A., 487, 493. 
 Young, Thomas, 7. 
 
 Z. 
 
 Zieman Effect, 672, 673 
 

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