LIBRARY THE UNIVERSITY OF CALIFORNIA MISS ROSE WHITING. Deceived September, 1896. Accession No.btoO . Chns No. UNITS AND PHYSICAL CONSTANTS. UNITS AND PHYSICAL CONSTANTS. BY J. D. EVERETT, M.A., D.C.L., F.R.S., F.R.S.E, PROFESSOR OF NATURAL PHILOSOPHY IN QUEEN'S COLLEGE, BELFAST. UHIVBBSIT7 IP oribon : MACMILLAN AND CO. 1879. [The right of translation and reproduction is reserved. ~\ GLASGOW : PRINTED AT THE UNIVERSITY PRESS BY ROBERT MACLEUOSE. PREFACE TO FIRST EDITION. THE quantitative study of physics, and especially of the relations between different branches of physics, is every day receiving more attention. To facilitate this study, by exemplifying the use of a system of units fitted for placing such relations in the clearest light, is the main object of the present treatise. A complete account is given of the theory of units ab initio. The Centimetre-Gramme-Second (or C.G.S.) system is then explained; and the remainder of the work is occupied with illustrations of its application to various branches of physics. As a means to this end, the most important experimental data relating to each subject are concisely presented on one uniform scale a luxury hitherto unknown to the scientific calculator. I am indebted to several friends for assistance in special departments but especially to Professor Clerk Maxwell and Professor G. C. Foster, who revised the entire manuscript of the work in its original form. Great pains have been taken to make the work correct as a book of reference. Readers who may discover any errors will greatly oblige me by pointing them out. trilVBHSITY PREFACE TO SECOND EDITION. THIS Book is substantially a new edition of my " Illustrations of the C.G.S. System of Units" published in 1875 by the Physical Society of London, supplemented by an extensive collection of physical data. The title has been changed with the view of rendering it more generally intelligible. Additional explanations have been given upon some points of theory, especially in connection with Stress and Strain, and with Coefficients of Diffusion. Under the former head, I have ventured to introduce the terms "resilience" and "coefficient of resilience," in order to avoid the multiplicity of meanings which have become attached to the word " elasticity." A still greater innovation has been introduced in an extended use of the symbols and processes of multiplica- tion and division, in connection with equations which express not numerical but physical equality. The ad- vantages of this mode of procedure are illustrated by its application to the solution of the most difficult problems on units that I have been able to collect from standard text-books (chiefly from Wormell's ' Dynamics '). A correction has been made in the definition of the Weber (p. 139). viii PREFACE TO SECOND EDITION. I am indebted to several friends for contributions of experimental data. A Dutch translation of the first edition of this work has been made by DR. C. J. MATTHES, Secretary of the Royal Academy of Sciences of Amsterdam, and was published in that city in 1877. Though the publication is no longer officially con- nected with the Physical Society, the present enlarged edition is issued with the Society's full consent and approval. J. D. EVERETT. BELFAST, June, 1879. nfXVEBSITY CONTENTS. PAGES Tables for reducing other measures to C. G. S. measures, xiii xvi CHAPTER I. GENERAL THEORY OF UNITS, . . . . 115 Units and derived Units, 1-5. Dimensions, 6-9. Meaning of "per," 10. Extended sense of "Multipli- cation" and "Division," 11-12. Examples, 13. Dimensions of mechanical and geometrical quantities, 14. CHAPTER II. CHOICE OF THREE FUNDAMENTAL UNITS, . 1620 Three independent units, 15. Their selection, 16. Standards of mass, 17. Standards of length, 18. Standard of time, 19. -Necessity for one common scale, 20. The C.G.S. system, 21. Powers of 10 as factors, CHAPTER III. MECHANICAL UNITS, 21 -29 Acceleration ; value of g; seconds' pendulum, 23. Force ; the dyne ; gravitation measure of force, 24-26. The poundal, 27. Work and energy ; the erg, 28. Kinetic energy, 29. Gravitation-measure of work, 30. Rate of working ; horse-power, 31. Examples in dyna- mics, p. 25. Centrifugal force, 32. Examples on centri- fugal force, p. 27. x CONTENTS. CHAPTER IV. PAGES HYDROSTATICS, 3043 Relative density of water at various temperatures, 33. Absolute density of water, 34. Formulas for ex- pansion of water, 35. Table of densities of solids and liquids, 36. Volume by weighing in water, 37. Examples in hydrostatics, p. 33. Barometric pressure ; C.G.S. unit of pressure ; standard atmosphere adopted in this volume, 38. Examples on barometric pressure, p. 35. Density of dry air, with example, 39. Absolute densities of gases, 40. Pressure-height at a point in the air '(height of homogeneous atmosphere) 41, 42. Exam- ples on pressure-height, p. 39. Variation of density with height in the atmosphere, 43. Examples on height at which density is halved, p. 41. Pressure of aqueous vapour, 44. Pressures of various vapours, 45. Super- ficial tensions of liquids, 46. Correction of barometer for capillarity, 46 A. CHAPTER V. STRAIN, STRESS, AND RESILIENCE, . . . 4456 Strain, 47-49. Stress, 50, 51. Coefficients of resilience, 52. Resilience of volume ; Young's modulus ; simple rigidity, 53. Shear, 54-58. Shearing stress, 59-6o. Resistance to shearing, 61. Resilience of volume of liquids, 62, 63. Resilience of solids, 64-69. CHAPTER VI. ASTRONOMY, 57 61 Size and figure of the earth ; lengths of day and year, 70. Attraction ; sun, earth, and moon, 71. Attraction of a given number of grammes at a given distance, 72. The three fundamental units reducible to two, 73-75. System of units based on a given spectrum-line, 76. CONTENTS. xi CHAPTER VII. PAGES VELOCITY OF SOUND, 6266 General formula, 77. Gases, 78. Liquids, 79. Solids, 80-82. Musical strings, with example, 83. Faintest audible sound, 84. CHAPTER VIII. LIGHT, 6777 Velocity, 85. Wave-lengths, 86. Index of refrac- tion of air, 87. Vibrations per second, 88. Indices of refraction; glass, 89. Liquids, 90, 91. Indices of double refraction, 92. Indices of refraction of miscel- laneous substances, 93. Gases, 94. Dispersion in gases, 95, 96. CHAPTER IX. HEAT, 78119 Unit of heat, 97-99. Capacity and specific heat, 98-102. Table of specific heats and atomic weights of elements, 103. Variation of specific heat with tempera- ture, 104. Specific heats in solid and liquid form, 105. Specific heats of gases, * 106, 107. Of vapours, 108. Melting points, 109. Change of volume from liquid to vapour, no. Latent heats of fluidity, and melting points, IIT. Latent heats of vaporization, 112. Latent and total heat of steam, 113. Effect of temperature on gases, 114. Boiling points of water, 115. Departures from Boyle's law, 116. Specific heats of the same substances in different states, 117. Boiling points of various liquids, 118. Change of volume in melting, 119. Dry-bulb, wet-bulb, and dew-point, 120. Conductivity; definition, 121. Dimensions, 122. Thermometric conductivity, , 123. Analogous to co- efficient of diffusion, 124, 125. Coefficients of diffusion CONTENTS. of certain gases, 126. Conductivity of air, 127. Results of experiments on conductivity of solids, 128-135. J. D. Forbes, 128. Neumann, 129. Results from underground thermometers, 130. Angstrom, 131. G. Forbes, 132. A. S. Herschel and Lebour, 133. Pe"clet 134, 135- Emission and surface-conduction, M'Farlane, 136. Tait, 137. Mechanical equivalent of heat, 138, 139. Heat and energy of combination, 140. Two specific heats of a gas, 141. Change of freezing- point with pressure, 142. Change of temperature pro- duced by adiabatic compression, 143. Resilience as affected by heat of compression, with examples, 144. Tables of expansions, 145. CHAPTER X. MAGNETISM, 120 127 Magnetic units and their dimensions, 146-150. Examples, pp. 122-125. Gauss's pound magnet, p. 122. Maximum of permanent magnetism, p. 123. Maximum magnetization of iron, nickel, and cobalt, p. 123. Moment and magnetization of earth, p. 124. Different units em- ployed by Gauss, p. 125. Distribution of magnetic potential and force over surface of earth, 151. Magnetic ele- ments at Greenwich, 152, 152*. Magneto-optic rota- tions, 153. CHAPTER XL ELECTRICITY, 128161 Electrostatic units and their dimensions, 154-159. Electromagnetic units and their dimensions, 160-164. Table of dimensions in both systems, 165. Heat gene- rated by current, 166. Ratios of the two sets of electric units expressed in terms of a velocity, 167, 168. Deter- minations of this velocity, and comparison with velocity of CONTENTS. xiii PAGES light, 169. Dimensions in terms of density, length, and time, 170. Specific inductive capacity, 171. Of gases, 172. Ohm, theoretical and practical, 173. Volt, Weber, and Farad, 174. Earth-quadrant per second, 175. Length of spark for various differences of potential, 176, 177. Resistance, and specific resistance, 178. Tables of specific resistance, 179, 180. Resistance of insulators, 1 8 1. Resistance of water and ice at various tempera- tures, 182. Electro-motive forces of various cells, 183. Electro- motive forces of contact, 184. Thermoelectric force, with examples, 185, 186. Electro-chemical equivalents, 187. Computation of electromotive force from heat of combination, 188. Examples on electricity, 189, pp. 155-158. Capacity of earth, p. 156. Electromotive force due to revolving coil, p. 158. Problem on selection of fundamental units, 190. Electrodynamics. Ampere's formula, with example, APPENDIX, ..... .... 163169 Reports of Units Committee of British Association. INDEX, ........ 171175 TABLES FOR REDUCING OTHER MEASURES TO C.G.S. MEASURES. The abbreviation cm. is used for centimetre or centimetres, m ' gramme or grammes, scc - second m seconds, S 2- square, b. cubic. Length. J ;. nch > - - = 2 -5400 cm. I foe*, j? yard, - . - 91-4392 innle, - . = 160933 i nautical mile, - = 185230 More exactly, according to Captain Clarke's com- parisons of standards of length (printed in 1866), the metre is equal to 1-09362311 yard, or 3-2808693 feet, or 39370432 inches, the standard metre being taken as correct at o C, and the standard yard as correct at i6f ience the inch is 2-5399772 centimetres. Area. I square inch, - . . 6-4516 sq. cm. I square foot, - - = o 2 o - O i I square yard, - . =8361-13 i square mile, - . =2'59xio 10 I cubic inch, I cubic foot, I cubic yard, I pint, i gallon, - Volume. = 16-387 cub. cm. - - 28316 4541 TABLES. Mass. i grain, - - = '0647990 gm. i ounce avoirdupois, - = 28 '3495 , , i pound ,, - = 453'59 i ton, - - - =i'oi6o5xio 6 ,, More exactly, according to the comparison made by Professor W. H. Miller in 1844 of the "kilogramme des Archives," the standard of French weights, with two English pounds of platinum, and additional weights, also of platinum, the kilogramme is 15432*34874 grains, of which the new standard pound contains 7000. Hence the kilogramme is 2*2046212 pounds, and the pound is 453'59 26 5 grammes. Velocity. i foot per second, - - =30*4797 cm. per sec. I statute mile per hour, - =44704 ,, I nautical mile per hour, - =51 '453 I kilometre per hour, - - =27777 Density. Pure water at temperature of / , maximum density, - .- j = ' OOOI 3 m - P er cub * cm ' I pound per Cubic foot, ' - = '016019 Force (assuming -=981). Weight of i grain, = 63-57 dynes, i ounce avoirdu- =278x10* pois, ] pound avoirdu- pois, =4-45x105 cwt. , =4-98x107 ton, - =9'97xio 8 gramme, - = 981 kilogramme, =9-81 x io 5 tonne, =9-81 xio 8 TABLES. foot-pound, foot-grain, foot-ton, - milligram-millimetre, gramme-centimetre, - kilogrammetre, - tonne-metre, Work (assuming -=981). - = i '356 xio 7 ergs, nearly. - = i -937 xio 3 . =3-04 x io 10 =9-81 x io- 2 =9-81 xio 2 =9-81 xio 7 =9-81 xio 10 Work in a second by one ) , .- f,Vol T,.c =746 theoretical "horse Pressure (assuming "=981). i pound per square foot, - = 479 dynes per sq. cm., nearly, i pound per square inch, - =6 '9 xio 4 ,, ., i kilogramme per square ( _ o metre, - - - l kilogramme per square) g . decimetre, - - ) I kilogramme per square g . centimetre, - - ) I kilogramme per square g 7 millimetre, - - ~ y Pressure of 760 millimetres _ T . m . x Tn c of mercury at o C, - ~ J 14 X IO Pressure of 30 inches of ) 6 mercury at o C., - \ ) mercury Pressure of I inch of mercury ) _ .,.~gg x Io t Heat. i gramme-degree Centigrade, =4 '2 x io 7 ergs = 42 million ergs. i pound-degree, ,, = 1*91 x io 10 ergs. i ,, Fahr., - - = i -06 x io 10 ergs. F JhH A * ** &sjw83fiJ* CHAPTER I. GENERAL THEORY OF UNITS. Units and Derived Units. i. THE numerical value of a concrete quantity is its ratio to a selected magnitude of the same kind, called the unit. Thus, if L denote a definite length, and / the unit length, is a ratio in the strict Euclidian sense, and is called the numerical value of L. The numerical value of a concrete quantity varies directly as the concrete quantity itself, and inversely as the unit in terms of which it is expressed. 2. A unit of one kind of quantity is sometimes defined by reference to a unit of another kind of quantity. For example, the unit of area is commonly defined to be the area of the square described upon the unit of length; and the unit of volume is commonly defined as the volume of the cube constructed on the unit of length. The units of area and volume thus defined are called derived units, and are more convenient for calculation than indepen- dent units would be. For example, when the above definition of the unit of area is employed, we can assert 2 UNITS AND PHYSICAL CONSTANTS. [CHAP. that [the numerical value of] the area of* any rectangle is equal to the product of [the numerical values of] its length and breadth ; whereas, if any other unit of area were employed, we should have to introduce a third factor which would be constant for all rectangles. 3. Still more frequently, a unit of one kind of quantity is defined by reference to two or more units of other kinds. For example, the unit of velocity is commonly defined to be that velocity with which the unit length would be described in the unit time. When we specify a velocity as so many miles per hour, or so many feet per second, we in effect employ as the unit of velocity a mile per hour in the former case, and a foot per second in the latter. These are derived units of velocity. Again, the unit acceleration is commonly defined to be that acceleration with which a unit of velocity would be gained in a unit of time. The unit of acceler- ation is thus derived directly from the units of velocity and time, and therefore indirectly from the units of length and time. 4. In these and all other cases, the practical advantage of employing derived units is, that we thus avoid the intro- duction of additional factors, which would involve needless labour in calculating and difficulty in remembering.' 1 ' * An example of such needless factors may be found in the rules commonly given in English books for finding the mass of a body when its volume and material are given. " Multiply the volume in cubic feet by the specific gravity and by 62 '4, and the product will be the mass in pounds ; " or " multiply the volume in cubic inches by the specific gravity and by 253, and the product will be the mass in grains." The factors 62 '4 and 253 here employed would be avoided that is, would be replaced by unity, if the unit volume of water were made the unit of mass. i.] GENERAL THEORY OF UNITS. 3 5. The correlative term to derived is fundamental. Thus, when the units of area, volume, velocity, and acceleration are denned as above, the units of length and time are called the fundamental units. Dimensions. 6. Let us now examine the laws according to which derived units vary when the fundamental units are changed. Let V denote a concrete velocity such that a concrete length L is described in a concrete time T ; and let v, /, t denote respectively the unit velocity, the unit length, and the unit time. The numerical value of V is to be equal to the numerical value of L divided by the numerical value of V L T T. But these numerical values are -, -> ', hence we must have V L / This equation shows that, when the units are changed (a change which does not ^affect V, L, and T), v must vary directly as / and inversely as t ; that is to say, the unit of velocity varies directly as the unit of length, and inversely as the unit of time. y Equation (i) also shows that the numerical value - of a given velocity varies inversely as the unit of length, and directly as the unit of time. 7. Again, let A denote a concrete acceleration such that the velocity V is gained in the time T', and let a denote the unit of acceleration. Then, since the 4 UNITS AND PHYSICAL CONSTANTS. [CHAP. numerical value of the acceleration A is the numerical value of the velocity V divided by the numerical value of the time T, we have A=Y L a vT' But by equation (i) we may write for . We thus obtain A = L / t_ a I T T' (2) This equation shows that when the units a, /, / are changed (a change which will not aifect A, L, T or T'), a must vary directly as /, and inversely in the duplicate A ratio of // and the numerical value will vary inversely a as /, and directly in the duplicate ratio of /. In other words, the unit of acceleration varies directly as the unit of length, and inversely as the square of the unit of time ; and the numerical value of a given acceleration varies inversely as the unit of length, and directly as the square of the unit of time. It will be observed that these have been deduced as direct consequences from the fact that [the numerical value of] an acceleration is equal to [the numerical value of] a length, divided by [the numerical value of] a time, and then again by [the numerical value of] a time. The relations here pointed out are usually expressed by saying that the dimensions of acceleration* are - en ^ .^ or (time) 2 that the dimensions of the unit of acceleration* are * Professor James Thomson ('Brit. Assoc. Report,' 1878, p. 452) objects to these expressions, and proposes to substitute the follow- I.] GENERAL THEORY OF UNITS. 5 unit of length (unit of time) 2 ' 8. We have treated these two cases very fully, by way of laying a firm foundation for much that is to follow. We shall hereafter use an abridged form of reasoning, such as the following : length velocity = T 5 - ; time velocity length acceleration = . = . . * w time (time)" 1 Such equations as these may be called dimensional equations. Their full interpretation is obvious from what precedes. In all such equations, constant numerical factors can be discarded, as not affecting dimensions. 9. As an example of the application of equation (2) we shall compare the unit acceleration based on the foot and second with the unit acceleration based on the yard and minute. Let / denote a foot, L a yard, / a second, T a minute, T a minute. Then a will denote the unit acceleration based on the foot and second, and A will denote the unit acceleration based on the yard and minute. Equation (2) becomes 6 = M-) 1 = ~; . . (i) a i 60' T2oo **' that is to say, .an acceleration in which a yard per minute Change-ratio of unit of acceleration = This is very clear and satisfactory as a full statement of the meaning intended ; but it is necessary to tolerate some abridgment of it for practical -working. 6 UNITS AND PHYSICAL CONSTANTS. [CHAP. of velocity is gained per minute, is i of an acceleration 1200 in which a foot per second is gained per second. Meaning of "per" 10. The word per, which we have several times employed in the present chapter, denotes division of the quantity named before it by the quantity named after it. Thus, to compute velocity in feet per second, we must divide a number of feet by a number of seconds.* If velocity is continuously varying, let x be the number of feet described since a given epoch, and t the number of seconds elapsed, then is what is meant by the dt number of feet per second. The word should never be employed in the specification of quantities, except when the quantity named before it varies directly as the quantity named after it, at least for small variations as, in the above instance, the distance described is ultimately proportional to the time of describing it. Extended Sense of the terms "Multiplication " and 11 Division" 11. In ordinary multiplication the multiplier is always a mere numerical quantity, and the product is of the same nature as the multiplicand. Hence in ordinary division either the divisor is a mere numerical quantity and the quotient a quantity of the same nature as the dividend; * It is not correct to speak of interest at the rate of Five Pounds per cent. It should be simply Five per cent. A rate of five pounds in every hundred pounds is not different from a rate of five shillings in every hundred shillings. i.] GENERAL THEORY OF UNITS. 7 or else the divisor is of the same nature as the dividend, and the quotient a mere numerical quantity. But in discussing problems relating to units, it is con- venient to extend the meanings of the terms " multiplica- tion " and " division." A distance divided by a time will denote a velocity the velocity with which the given distance would be described in the given time. The dis- tance can be expressed as a unit distance multiplied by a numerical quantity, and varies jointly as these two factors ; the time can be expressed as a unit time multi- plied by a numerical quantity, and is jointly proportional to these two factors. Also, the velocity remains unchanged when the time and distance are both changed in the same ratio. 1 2. The three quotients i mile 5280 ft. 22 ft. i "hour* 3600 sec. ' 15 sec all denote the same velocity, and are therefore to be regarded as equal. In passing from the first to the second, we have changed the units in the inverse ratio to their numerical multipliers, and have thus left both the distance and the tirrfe unchanged. In passing from the second to the third, we have divided the two numeri- cal factors by a common measure, and have thus changed the distance and the time in the same ratio. A change in either factor of the numerator will be compensated by a proportional change in either factor of the denom- inator. Further, since the velocity ------ - is of the velo- 15 sec. 15 city J-*r_ we are entitled to write 22 tj 2 i sec. 15 sec 15 sec. 8 UNITS AND PHYSICAL CONSTANTS. [CHAP. thus separating the numerical part of the expression from the units part. In like manner we may express the result of Art. 9 by writing yard i foot (minute) 2 1200 (second) 2 ' Such equations as these may be called " physical equations," inasmuch as they express the equality of physical quantities, whereas ordinary equations express the equality of mere numerical values. The use of physical equations in problems relating to units is to be strongly recommended, as affording a natural and easy clue to the necessary calculations, and especially as obviating the doubt by which the student is often embarrassed as to whether he ought to multiply or divide. 13. In the following examples, which illustrate the use of physical equations, we shall employ / to denote the unit length, m the unit mass, and t the unit time. Ex. i. If the yard be the unit of length, and the acceleration of gravity (in which a velocity of 32-2 ft. per sec. is gained per sec.) be represented by 2415, find the unit of time. We have / = yard, and 32>2 = 24r5 * = ' sec/ .> t = 32-2 'Ex. 2. If the unit time be the second, the unit density 162 Ibs. per cub. ft, and the unit force* the weight of an * For the dimensions of density and force, see Art. 14. [.] GENERAL THEORY OF UNITS. We have / m sec., ~ 4 = 162 _ 5> ounce at a place where g (in foot-second units) is 32, what is the unit length ? m , Ib. 7' = l62 (ft) 3 and jf!L = 32 . oz ^, or ml = 32 oz. ft. - 2 Ib. ft. sec. 2 sec. 2 Hence by division /* = Q r - (ft.) 4 , / - 1 ft. = 4 in. ol Ex. 3. If the area of a field of 10 acres be represented by 100, and the acceleration of gravity (taken as 32 foot-second units) be 58?, find the unit of time. We have 48400 (yd.) 2 = 100 / 2 , whence /= 22 yd. ; whence / 2 m I7 22 sec. 2 - 121 sec. 2 , /- n sec. 32 Ex. 4. If 8 ft. per sec. be the unit velocity, and the acceleration of gravity (32 foot-second units) the unit acceleration, find the units of length and time. We have the two equations / ft / ft. *- 8 sb: / 2 : 32 ^. 2 ' whence by division / | sec., and substituting this value of/ in the first equation, we have 4 / = 8 ft, / = 2 ft. Ex. 5. If the unit force be 100 Ibs. weight, the unit length 2 ft, and the unit time J sec., find the unit mass, the acceleration of gravity being taken as 32 foot-second units. We have / - 2 ft, / = J sec., ,, ft. ;;// m 2 ft. 100 Ib. 32 = - = , sec. 2 / 2 T V sec. 2 that is 100 x 32 Ib. = 32 ;;/, m 100 Ib. io UNITS AND PHYSICAL CONSTANTS. [CHAP. Ex. 6. The number of seconds in the unit of time is equal to the number of feet in the unit of length, the unit of force is 750 Ibs weight [g being 32], and a cubic foot of the standard substance [substance of unit density] con- tains 13500 oz. Find the unit of time. Let t = x sec., then /= x ft. ; also let m =y Ib. Then we have ml _ y Ib. x ft. . y_ Ib. ft. ^ Ib. ft. /* ' x* sec. 2 3 x sec. 2 " 75 * 32 sec. 2 or ? - 750 x 32. oc .1 771 V ID. AIso p = ^ ?T = I35 ?T' * c-v 1L. 1 L. m v Ib. oz. 73 = 77 Z7 3 = J 35 * c-v AL whence = 13500 x . x* 1 6 Hence by division 7so x 72 x 16 i6 2 16 16 #2 = 15 6 = x = , /= sec. 13500 3 2 3 3 Ex. 7. When an inch is the unit of length and / the unit of time, the measure of a certain acceleration is a ; when 5 ft. and i min. are the units of length and time respectively, the measure of the same acceleration is io a. Find /. Equating the two expressions for the acceleration, we have a = io a 5 f 2 (mm.) whence f> = (min.) 2 = ' = 6 (sec). 2 50 ft. 600 / P J6 sec. Ex. 8. The numerical value of a certain force is 56 when the pound is the unit of mass, the foot the unit of length, and the second the unit of time ; what will be the I.] GENERAL THEORY OF UNITS. 11 numerical value of the same force when the hundredweight is the unit of mass, the yard the unit of length, and the minute the unit of time ? Denoting the required value by x we have , Ib. ft. cwt. yard . , Ib. ft. /min.\ 2 5 cwt. ydT \sec7 ) = 56 x L- x x 6o 2 = 600. 112 O Dimensions of Mechanical and Geometrical Quantities. 14. In the following list of dimensions, we employ the letters L, M, T as abbreviations for the words Length, Mass, Time. The symbol of equality is used to denote sameness of dimensions. Area = L 2 , Volume = L 3 , Velocity = ^ , Acceleration = , Momentum = - . M Density = , density' being defined as mass per unit J / volume. ML Force = -
an d the force acting on the bodv is
r \T /
/27T\ 2 ,
mr(~\ dynes.
If n revolutions are made per minute, the value of T is
, and the force is mr( \ dynes.
\3/
Examples.
i. A body of m grammes moves uniformly in a circle
of radius 80 centims., the time of revolution being \ of a
second. Find the centrifugal force, and compare it with
the weight of the body.
Ans. The centrifugal force is ;;/ x / 2 ^ J x 80 = m x 647^
x 80 = 50532 m dynes.
The weight of the body (at a place where g is 981)
is 981 m dynes. Hence the centrifugal force is about
52 J times the weight of the body.
28 UNITS AND PHYSICAL CONSTANTS. [CHAP.
2. At a bend in a river, the velocity in a certain part
of the surface is 170 centims. per second, and the radius
of curvature of the lines of flow is 9100 centims. Find
the slope of the surface in a section transverse to the
lines of flow.
Ans. Here the centrifugal force for a gramme of the
water is iZ2Z =3*176 dynes. If^be 981 the slope will
be - ' = - ; that is. the surface will slope upwards
981 309'
from the concave side at a gradient of i in 309. The
general rule applicable to questions of this kind is that
the resultant of centrifugal force and gravity must be
normal to the surface.
3. An open vessel of liquid is made to rotate rapidly
round a vertical axis. Find the number of revolutions
that must be made per- minute in order to obtain a slope
of 30 at a part of the surface distant 10 centims. from
the axis, the value of g being 981.
Ans. We must have tan 30 - , where f denotes the
&
intensity of centrifugal force that is, the centrifugal force
per unit mass. We have therefore
lnir\ 2 . n denoting the number of
981 tan 30 = lol ) . .
\3o/ revolutions per minute,
90
Hence n- 71-9.
4. For the intensity of centrifugal force at the equator
due to the earth's rotation, we have r = earth's radius
= 6-38 x io 8 , T = 86164, being the number of seconds in
a sidereal day.
in.]
MECHANICAL UNITS.
29
/2Y
(x) = 3 ' 39 '
This is about of the value of r.
289
If the earth were at rest, the value of g at the equator
would be greater than at present by this amount. If the
earth were revolving about 17 times as fast as at present,
the value of g at the equator would be nil.
UBI7BRSITY
CHAPTER IV.
HYDROSTATICS.
33. THE following table of the relative density of water
at various temperatures (under atmospheric pressure), the
density at 4 C. being taken as unity, is from Rossetti's
results deduced from all the best experiments (Ann. Ch.
Phys. x. 461 ; xvii. 370, 1869) :
Temp.
Cent.
Relative
Density.
Temp.
Cent.
Relative
Density.
Temp.
Cent.
Relative
Density.
o
o
999871
i3
999430
35
99418
I
999928
H
999299
40
99235
2
999969
15
999160
45
99037
3
999991
16
999002
50
98820
4
I '000000
17
998841
55
98582
5
999990
18
998654
60
98338
6
999970
19
998460
65
98074
8
999933
999886
20
22
998259
997826
70
75
97794
97498
9
10
999824
999747
11
997367
996866 ;
80
85
97194
96879
ii
999655
28
996331 j
90
96556
12
999549
30
995765 1
100
95865
34. According to Kupffer's observations, as reduced
by Professor W. H. Miller, the absolute density (in
grammes per cubic centimetre) at 4 is not i, but
HYDROSTATICS.
1*000013. Multiplying the above numbers by this
factor, we obtain the following table of absolute den-
sities :
Temp.
Density.
Temp. Density.
Temp.
Density.
999884
13
"999443
35
99469
I
999941
14
999312
40
99236
2
999982
15
999173
45
99038
3
I '000004
16
999015
5
98821
4
I -OOOOI3
17
998854
55
98583
5
I -000003
18
998667
60
98339
6
999983
19
998473
65
9 8075
7
999946
20
998272
70
'97795
8
999899
22
997839
75
'97499
9
999837
24
997380
80
97195
10
999760
26
996879
85
96880
ii
999668
28 ^96344
90
96557
12
999562
30 '99S77 8
100
95866
35. The volume, at temperature t, of the water which
occupies unit volume at 4, is approximately
! + A(/- 4 ) 2 -B(/- 4 ) 2 - 6 + C(/- 4 ) 3 ,
where
A = 8-38 x io- ,
B - 379'' x i~ 7 >
C 2*24 x io~ 8 ;
and the relative density at temperature f is given by the
same formula with the signs of A, B, and C reversed.
The rate of expansion at temperature f is
2 A (/- 4 )-2-6B .(/- 4)1-6 + 3 C (/- 4 ) 2 .
In determining the signs of the terms with the frac-
tional exponents 2-6 and r6, these exponents are to be
regarded as odd.
UNITS AND PHYSICAL CONSTANTS. [CHAP.
36. Table of Densities (chiefly taken from Rankine's
" Rules and Tables," pp. 149 and 150) :
Solids.
, , wire
8-1:4.
Brick
O "
2 to 2*17
Bronze
Brickwork
1-8
Copper, cast
8-6
Chalk
I '8 tO 2'i
,, sheet.. . .
8-8
Clay
I '92
,, hammered..
Gold
8-9
10 to I0'6
Glass, crown
,, flint .
Iron, cast
, , wrought
6 '95 to 7-3
7 '6 to 7 '8
Quartz (rock-cry-
stal)
2'6-
Lead
1 1 -4
Sand (dry)
I '42
Platinum
21 tO 22
Fir, spruce
48 to 7
Silver ....
Oak, European . .
69 to "99
Steel
7 '8 to 7 '9
Lignum vitse
65 to i 'V
Tin .
7 '3 to 7 '5
Sulphur, octahedral
Zinc
6 "8 to 7 "2.
,, prismatic.
1-98
Ice ..
02
Liquids at o C.
Sea- water, ordinary i '026
Alcohol, pure 791
,, proof spirit ... '916
Ether 716
Mercury 13 -596
Naphtha '848
Oil, linseed '940
olive -915
whale -923
,, of turpentine '870
37. If a body weighs m grammes in vacuo and m'
grammes in water of density unity, the volume of the body
is m m cubic centims.; for the mass of the water dis-
placed is m - m grammes, and each gramme of this
water occupies a cubic centimetre.
Examples.
i. A glass cylinder, / centims. long, weighs m grammes
in vacuo and m grammes in water of unit density. Find
its radius.
iv.] HYDROSTATICS. 33
Solution. Its section is 7r;- 2 , and is also m ; hence
2 m m'
~^T
2. Find the capacity at o C. of a bulb which holds m
grammes of mercury at that temperature.
Solution. The specific gravity of mercury at o being
13-596 as compared with water at the temperature of
maximum density, it follows that the mass of i cubic
centim. of mercury is 13*596 x 1-000013 = 13-59618, say
13-596. Hence the required capacity is - - cubic
centims.
3. Find the total pressure on a surface whose area is A
square centims. when its centre of gravity is immersed to
a depth of h centims. in water of unit density, atmos-
pheric pressure being neglected.
Ans. A/i grammes weight ; that is gKh dynes.
4. If mercury of specific gravity 13*596 is substituted
for water in the preceding question, find the pressure.
Ans. 13-596 Kh grammes weight- that is, 13-596 ghh
dynes.
5. If h be 76, and A be unity in example 4, the
answer becomes 1033-3 grammes weight, or 1033-3^-
dynes.
For Paris, where g is 980-94, this is 1-0136 x io r>
dynes.
Barometric Pressure.
38. The C.G.S. unit of pressure intensity (that is, of
pressure per unit area) is the pressure of a dyne per
square centim.
34 UNITS AND PHYSICAL CONSTANTS. [CHAP.
At the depth of h centims. in a uniform liquid whose
density is d [grammes per cubic centim.], the pressure
due to the weight of the liquid is ghd dynes per square
centim.
The pressure-intensity due to the weight of a column of
mercury at o C, 76 centims. high, is found by putting
^ = 76, d= 13*596, and is 1033-3^-. It is therefore
different at different localities. At Paris, where 'g is
980-94, it is i -0136 x io 6 ; that is, rather more than a
megadyne * per square centim. To exert a pressure of
exactly one megadyne per square centim., the height of
the column at Paris must be 74*98 centims.
At Greenwich, where gis 981*17, the pressure due to 76
centims. of mercury at o C. is 1*0138 x io 6 ; and the
height which would give a pressure of io 6 is 74*964
centims., or 29*514 inches.
Convenience of calculation would be promoted by
adopting the pressure of a megadyne per square centim.,
or io 6 C.G.S. units of pressure-intensity, as the standard
atmosphere.
The standard now commonly adopted (whether 76
centims. or 30 inches) denotes different pressures at
different places, the pressure denoted by it being pro-
proportional to the value of g.
We shall adopt the megadyne per square centim. as our
standard atmosphere in the present work.
Examples.
i. What must be the height of a column of water of
* The prefix mega denotes multiplication by a million. A
megadyne is a force of a million dynes.
iv.] HYDROSTATICS. 35
unit density to exert a pressure of a megadyne per square
centim. at a place where g is 981 ?
Ans. I00 000 = 1019-4 centims. This is 33*445 f eet -
981
2. What is the pressure due to an inch of mercury at
o C. at a place where g is 981. (An inch is 2-54
centims.)
Ans. 981 x 2-54 x 13*596 =33878 dynes per square
centim.
3. What is the pressure due to a centim. of mercury at
o C. at the same locality ?
Ans. 981 x 13-596 = 13338.
4. What is the pressure due to a kilometre of sea-water
of density 1*027, g being 981 ?
Ans. 981 x io 5 x 1-027 IP 75 x io 8 dynes per square
centim., or 1*0075 x r 2 niegadynes per square centim. ;
that is, about 100 atmospheres.
5. What is the pressure due to a mile of the same
water ?
Ans. i '62 14 x io 8 C.G.S. units, or 162 '14 atmospheres
[of a megadyne per square xTentim.].
Density of Air.
39. Regnault found that at Paris, under the pressure of
a column of mercury at o, of the height of 76 centims.,
the density of perfectly dry air was -0012932 gramme per
cubic centim. The pressure corresponding to this height
of the barometer at Paris is 1-0136 x io 6 dynes per square
centim. Hence, by Boyle's law, we can compute the
density of dry air at o C. at any given pressure.
36 UNITS AND PHYSICAL CONSTANTS. [CHAP.
At a pressure of a megadyne (io 6 dynes) per square
centim. the density will be OOI2 93 2 _ -ooi^^o.
1-0136
The density of dry air at o C. at any pressure / (dynes
per square centim.) is
/x 1-2759 x io- 9 . . . - - (4)
Example.
Find the density of dry air at o C., at Edinburgh,
under the pressure of a column of mercury at o 9 C., of
the height of 76 centims.
Here we have p = 981-54 x 76 x 13-596= 1-0142 x io 6 .
Ans. Required density = 1*2940 x io~ 3 =-0012940
gramme per cubic centim.
40. Absolute Densities of Gases, in grammes per cubic
centim., at o C., and a pressure of io 6 dynes per
square centim.
Mass of a cubic Volume of a gramm
centim. in grammes. in ubic centims.
Air, dry, -0012759 783*8
Oxygen, -0014107 708*9
Nitrogen, '0012393 806*9
Hydrogen, '00008837 11316-0
Carbonic acid, -0019509 512*6
,, oxide -0012179 821-1
Marsh-gas, '0007173 I394'i
Chlorine, '0030909 323*5
Protoxide of nitrogen,... '0019433 5 r 4*6
Binoxide ,. ... '0013254 754*5
Sulphurous acid, '0026990 37o*5
Cyanogen, '0022990 435'
Olefiant gas '0012529 798*1
Ammonia, '0007594 1316*8
iv.] HYDROSTATICS. 37
The numbers in the second column are the reciprocals
of those in the first.
The numbers in the first column are identical with the
specific gravities referred to water as unity.
Assuming that the densities of gases at constant pres-
sure and temperature are directly as their atomic weights,
we have for any gas at zero
pvp 1-1316 x io w m ;
v denoting its volume in cubic centims., m its mass in
grammes,/ its pressure in dynes per square centim., and
/* its atomic weight referred to that of hydrogen as unity.
Height of Homogeneous Atmosphere.
41. We have seen that the intensity of pressure at
depth /i, in a fluid of uniform density d, is ghd when the
pressure at the upper surface of the fluid is zero.
The atmosphere is not a fluid of uniform density ; but
it is often convenient to have a name to denote a height
H such that/=-HD, where/ denotes the pressure and
D the density of the air at a given point.
It may be defined as the height of a column of uniform
fluid having the same density as the air at the point
which would exert a pressure equal to that existing at the
point.
If the pressure be equal to that exerted by a column of
mercury of density 13 -5 96 and height /*, we have
/ = g#x 13-596;
/.HD = Ax 13-596, H = ^LIp6.
If it were possible for the whole body of air above the
point to be reduced by vertical compression to the
38 UNITS AND PHYSICAL CONSTANTS. [CHAP,
density which the air has at the point, the height from the
point up to the summit of this^compressed atmosphere
would be equal to H, subject to a small correction
for the variation of gravity with height.
H is called the height of the homogeneous atmosphere at
the point considered. Pressure-height would be a better
name.
The general formula for it is
and this formula will be applicable to any other gas
as well as dry air, if we make D denote the density
of the gas (in grammes per cubic centim.) at pressure/.
If, instead of/ being given directly in dynes per square
centim. , we have given the height h of a column of liquid
of density d which would exert an equal pressure, the
formula reduces to
(6)
42. The value of - in formula (5) depends only on the
nature of the gas and on the temperature; hence, for
a given gas at a given temperature, H varies inversely
as.g-.
For dry air at zero we have, by formula (4),
g
At Paris, where g is 980-94, we- find
H = 7-990 x io 5 .
iv.] HYDROSTATICS. 39
At Greenwich, where g is 981-17,
H = 7-988 xio.
Examples.
1. Find the height of the homogeneous atmosphere at
Paris for dry air at 10 C., and also at 100 C.
Ans. For given density, p varies as i + "00366 /, /
denoting the temperature on the Centigrade scale.
Hence we have, at 10 C.,
H = 1-0366 x 7-99 x io 5 = 8-2825 x io 5 ;
and at 100 C..
H= 1-366 x 7-99 x io 5 1*0914 x io 6 .
2. Find the height of the homogeneous atmosphere for
hydrogen at o, at a place where g is 981.
Here we have
Diminution of Density with increase of Height in the
Atmosphere.
43. Neglecting the variation of gravity with height, the
variation of H as we ascend in the atmosphere would
depend only on variation of temperature. In an atmos-
phere of uniform temperature H will be the same at
all heights. In such an atmosphere, an ascent of i
centim. will involve a diminution of the pressure (and
therefore of the density) by -^ of itself, since the layer of
H
air which has been traversed is -^ of the whole mass of
H
superincumbent air. The density therefore diminishes
40 UNITS AND PHYSICAL CONSTANTS. [CHAP.
by the same fraction of itself for every centim. that we
ascend; in other words, the density and pressure dim-
inish in geometrical progression as the height increases
in arithmetical progression.
Denote height above a fixed level by x, and pressure
by/. Then, in the notation of the differential calculus,
, dx dp
we have = - -^ ,
H /
and if p v / 2 are the pressures at the heights x v x z , we
deduce
* 2 - x l = H log e - - H x 2-3026 Iog 10 i ... (7)
fi Pi
In the barometric determination of heights it is usual
to compute H by assuming a temperature which is the
arithmetical mean of the temperatures at the two heights.
For the latitude of Greenwich formula (7) becomes
x% Xi = (i + '00366 /) 7-988 x io 5 x 2*3026 log^ 1
A
= (i + '00366 /) 1,839,300 log A . . . (8)
A
t denoting the mean temperature, and the logarithms
being common logarithms.
To find the height at which the density would be
halved, variations of temperature being neglected, we
must put 2 for ^ in these formulae. The required height
P\
will be H \og e 2, or, in the latitude of Greenwich, for
temperature o C., will be
1-8393 x io 6 x '30103 = 553700.
The value of log e 2, or 2-3026 Iog 10 2, is
2-3026 x -30103 = '69315.
iv.j HYDROSTATICS. 41
Hence for an atmosphere of any gas at uniform tempera-
ture, the height at which the density would be halved is
the height of the homogeneous atmosphere for that gas,
multiplied by '69315. The gas is assumed to obey
Boyle's law.
Examples.
1. Show that if the pressure of the gas at the lower
station and the value of g be given, the height at which
the density will be halved varies inversely as the density.
2. At what height, in an atmosphere of hydrogen at
o C., would the density be halved, g being 981 ?
Ans. 7 '9954 x io 6 .
44. Pressure of Aqueous Vapour at various temperatures,
in dynes per square centim.
-20 1236
-15 1866
-io 2790
- 5 415
o 6133
5 8710
10 12220
50 i '226 x io 5
60 1-985
80 4729
loo 1-014 x Ic6
120 1-988 ,,
140 3-626
6-210
15 1693 ! J 8o 1-006 x io 7
20 23190 I 200 i '560
25 3HOO
30 42050
40 73200
The density of saturated steam, at any temperature /,
is approximately
622 x -0012759 /
i -f '00366 / 10 '
p denoting the pressure as given in the above table.
UNITS AND PHYSICAL CONSTANTS. [CHAP.
45. Pressure of Vapour of various Liquids, in dynes per
square centim.
Alcohol.
Ether. S cS D on. f Chloroform.
\
o
20
4455
9-19 x io 4 6*31 x io 4
10
8630
i -53 x io 5 , i -058 x io 5
16940
2-46
i -706
10
32310
3-826
2-648
20
593io
5-772
i 3 '975
j 2*141 x io 5
30
1-048 x lo 5 ! 8-468
I 5799
! 3-3oi
40
1783
I-2IO X
io 6 j 8-240
! 4-927
50
2-932
1-687
1-144 x
io 6 7-14
60
4-671
2-30I
i '554
1-007 x
IO 6
So
I '084 x
io 6 ; 4-031
2-711
1-878
100
2-265
6-608
4-435
3-24
120
4'3i
1-029 x J 7
6-87
5-24
46. The phenomena of capillarity, soap-bubbles, &c.,
can be reduced to quantitative expression by assuming a
tendency in the surface of every liquid to contract. The
following table exhibits the intensity of this contractile
force for various liquids at the temperature of 20 C. The
contractile force diminishes as the temperature increases.
Superficial Tensions at 20 C., in dynes per linear centim,,
deduced from Qiiincke's results.
Density.
Tension of surface separating
the liquid from
Air.
Water.
Mercury.
Water,
0-9982
13-5432
I -2687
1-4878
7906
9136
8867
7977
i'i
1-1248
81
540
32-1
30-6
25-5
36-9
297
3 1 7
70-1
77-5
O
418
4^75
29'5
20-56
H'55
27-8
418
372-5
399
399
335
250-5
284
377
442-5
Mercury, ...
Bisulphide of carbon, .. .
Chloroform,
Alcohol,
Olive-oil,
Turpentine,
Petroleum,
Hydrochloric acid,
Solution of hyposulphite )
of soda, }
[IV.
HYDROSTATICS.
43
46 A. Depression of the barometrical column due to
capillarity, according to Pouillet :
Internal
Internal
1 Internal
diameter
of tube.
Depression.
Diameter
of tube.
Depression.
Diameter
of tube.
m.m.
m.m.
m.m.
m.m.
m.m.
2
4'579
8-5
604
15
2'5
3-595
9
'534
15-5
3
2 '9O2
9-5
'473
16
3'5
2'4I5
10
419
16-5
4
2-053
10-5
372
17
4'5
1752
ii
330
I7'5
5
I-507
*5
293
18
5'5
I-306
12
260
18-5
I-I36
12-5
230
19
6'5
'995
13
204
I9'5
7
877
I3-5
181
20
7'5
775
14
161
20'5
8
684
I4-5
143
21
Depression.
m.m.
127
"112
099
087
077
068
060-
53-
047
041
036
032-
028
44
CHAPTER V.
STRESS, STRAIN, AND RESILIENCE.
47. IN the nomenclature introduced by Rankine and
adopted by Thomson and Tait, any change in the shape
or size of a body is called a strain, and an action of force
tending to produce a strain is called a stress. We shall
always suppose strains to be small; that is, we shall
suppose the ratio of the initial to the final length of every
line in the strained body to be nearly a ratio of equality.
48. A strain changes every small spherical portion of
the body into an ellipsoid ; and the strain is said to be
homogeneous when equal spherical portions in all parts of
the body are changed into equal ellipsoids with their
corresponding axes parallel. When the strain consists in
change of volume, unaccompanied by change of shape,
the ellipsoids are spheres.
When strain is not homogeneous, but varies con-
tinuously from point to point, the strain at any point
is defined by attending to the change which takes place
in a very small sphere or cube having the point at its
centre, so small that the strain throughout it may be
regarded as homogeneous. In what follows we shall
suppose strain to be homogeneous, unless the contrary is
expressed.
STRESS, STRAIN, AND RESILIENCE. 45
49. The axes of a strain are the three directions at
right angles to each other, which coincide with the
directions of the axes of the ellipsoids. Lines drawn in
the body in these three directions will remain at right
angles to each other when the body is restored to its
unstrained condition.
A cube with its edges parallel to the axes will be
altered by the strain into a rectangular parallelepiped.
Any other cube will be changed into a parallelepiped not
in general rectangular.
When the axes have the same directions in space after
as before the strain, the strain is said to be unaccompanied
by rotation. When such parallelism does not exist, the
strain is accompanied by rotation, namely, by the
rotation which is necessary for bringing the axes from
their initial to their final position.
The numbers which specify a strain are mere ratios,
and are therefore independent of units.
50. When a body is under the action of forces which
strain it, or tend to strain it ; if we consider any plane
section of the body, the portions of the body which it
separates are pushing each other, pulling each other, or
exerting some kind of force^-upon each other, across the
section, and the mutual forces so exerted are equal and
opposite. The specification of a stress must include a
specification of these forces for all sections, and a body is
said to be homogeneously stressed when these forces are
the same in direction and intensity, for all parallel
sections. We shall suppose stress to be homogeneous, in
what follows, unless the contrary is expressed.
51. When the force-action across a section consists of
a simple pull or push normal to the section, the direction
46 UNITS AND PHYSICAL CONSTANTS. [CHAP.
of this simple pull or push (in other words, the normal to
the section) is called an axis of the stress. A stress (like
a strain) has always three axes, which are at right angles
to one another. The mutual forces across a section not
perpendicular to one of the three axes are in general
partly normal and partly tangential one side of the sec-
tion is tending to slide past the other.
The force per unit area which acts across any section
is called the intensity of the stress on this section, or
simply the stress on this section. The dimensions of
"force per unit area," or ~ are - 1 , , which we shall
area LT 2
therefore call the dimensions of stress.
52. The relation between the stress acting upon a
body and the strain produced depends upon the resilience
of the body, which requires in general 21 numbers for its
complete specification. When the body has exactly the
same properties in all directions, 2 numbers are sufficient.
These specifying numbers are usually called coefficients of
.elasticity ; but the word elasticity is used in so many
senses that we prefer to call them coefficients of resilience.
A coefficient of resilience expresses the quotient of a
stress (of a given kind) by the strain (of a given kind)
which it produces. A highly resilient body is a body
which has large coefficients of resilience. Steel is an
example of a body with large, and cork of a body with
small, coefficients of resilience.
In all cases (for solid bodies) equal and opposite strains
(supposed small) require for their production equal and
opposite stresses.
53. The coefficients of resilience most frequently
referred to are the three following :
v.] STRESS, STRAIN, AND RESILIENCE. 47
(1) Resilience of volume, or resistance to hydrostatic
compression. If V be the original and V - v the strained
volume, ^- is called the compression, and when the body
is subjected to uniform normal pressure P per unit area
over its whole surface, the quotient of P by the compres-
sion is the resilience of volume. This is the only kind of
resilience possessed by liquids and gases.
(2) Young's modulus, or the longitudinal resilience of
a body which is perfectly free to expand or contract
laterally. In general, longitudinal extension produces
lateral contraction, and longitudinal compression produces
lateral extension. Let the unstrained length be L and
the strained length L /, then is taken as the measure
J_<
of the longitudinal extension or compression. The stress
on a cross section (that is, on a section to which the stress
is normal) is called the longitudinal stress, and Young's
modulus is the quotient of the longitudinal stress by the
longitudinal extension or compression. If a wire of cross
section A sq. cm. is stretched with a force of F dynes,
and its length is thus altered from L to L + /, the value
" F T
of. Young's modulus for the wire is - . ~.
A /
(3) " Simple rigidity " or resistance to shearing. This
requires a more detailed explanation.
54. A shear maybe defined as a strain by which a sphere
of radius unity is converted into an ellipsoid of semiaxes
i, i+e, ie; in other words, it consists of an extension
in one direction combined with an equal compression in
a perpendicular direction.
55. A unit square (Fig. i) whose diagonals coincide
4 8
UNITS AND PHYSICAL CONSTANTS. [CHAP.
with these directions is altered by the strain into a
rhombus whose diagonals are (1+^)^/2 and (1^)^/2,
and whose area, being half the product of the diagonals,
is i -e 2 , or, to the first order of small quantities, is i,
the same as the area of the original square. The length
of a side of the rhombus, being the square root of the
Fig.1.
sum of the squares of the semi-diagonals, is found to be
J i + e 1 or _+i, and is therefore, to the first order of
small quantities, equal to a side of the original square.
56. To find the magnitude of the small angle which a
side of the rhombus makes with the corresponding side of
the square, we may proceed as follows : Let acb (Fig. 2)
be an enlarged representation of one of the small tri-
angles in Fig. i. Then we have ab = J, cb = \e ^2 = ~-
angle cba - - .
4
Hence the length of the perpendicular cd
is cb sin = - = ; and since ad is ultimately
equal to ab, we have, to the first order of small quan-
tities,
angle tf = -^-= 4~ = e -
aa *
v.]
STRESS, STRAIN, AND RESILIENCE.
The semi-angles of the rhombus are therefore - e,
4
and the angles of the rhombus are - ze ; in other
words, each angle of the square has been altered by the
amount 2e. This quantity 2e is adopted as the measure
of the shear.
57. To find the perpendicular distance between oppo-
site sides of the rhombus, we have to multiply a side by
the cosine of 2*, which, to the first order of small quan-
tities, is i. Hence the perpendicular distance between
opposite sides of the square is not altered by the shear,
and the relative movement of these sides is represented
Fig 3.
by supposing one of them to remain fixed, while the
other slides in the direction of its own length through a
distance of 2^, as shown in pig. 3 or Fig. 4. Fig. 3, in
fact, represents a shear combined with right-handed rota-
tion, and Fig. 4 a shear combined with left-handed rota-
tion, as appears by comparing these figures with Fig. i,
which represents shear without rotation.
58. The square and rhombus in these three figures may
be regarded as sections of a prism whose edges are per-
pendicular to the plane of the paper, and figures 3 and 4
show that (neglecting rotation) a shear consists in the
D
50 UNITS AND PHYSICAL CONSTANTS. [CHAP.
relative sliding of parallel planes without change of dis-
tance, the amount of this sliding being proportional to the
distance, and being in fact equal to the product of the
distance by the numerical measure of the shear. A good
illustration of a shear is obtained by taking a book, and
making its leaves slide one upon another.
It may be well to remark, by way of caution, that the
selection of the planes is not arbitrary as far as direction
is concerned. The only planes which are affected in
the manner here described are the two sets of planes
which make angles of 45 with the axes of the shear
(these axes being identical with the diagonals in Fig. i).
.59. Having thus denned and explained the term
" shear," which it will be observed denotes a particular
species of strain, we now proceed to define a shearing
stress.
A shearing stress may be defined as the combination of
two longitudinal stresses at right angles to each other,
these stresses being opposite in sign and equal in magni-
tude ; in other words, it consists of a pull in one direction
combined with an equal thrust in a
D r perpendicular direction.
60. Let P denote the intensity
of each of these longitudinal
stresses; we shall proceed to cal-
culate the stress upon a plane in-
I B clined at 45 to the planes of these
. stresses. Consider -a unit cube so
taken that the pull is perpendicular
to two of its faces, AB and D C (Fig. 5), and the thrust
is perpendicular to two other faces, AD, B C. The
forces which hold the half-cube ABC in equilibrium are
v.] STRESS, STRAIN, AND RESILIENCE. 5*
(1) An outward force P, uniformly distributed over the
face A B, and having for its resultant a single force P
acting outward applied at the middle point of AB.
(2) An inward force P, having for its resultant a single
force P acting inwards at the middle point of B C.
(3) A force applied to the face A C.
To determine this third force, observe that the other
two forces meet in a point, namely the middle point ot
A C, that their components perpendicular to A C destroy
one another, and that their components along A C, or
P '
rather along C A, have each the magnitude ; hence
V 2
their resultant is a force P ^/2, tending from C towards A.
The force (3) must be equal and opposite to this. Hence
each of the two half-cubes ABC, ADC exerts upon the
other a force P ^2, which is tangential to their plane of
separation. The stress upon the diagonal plane A C is
therefore a purely tangential stress. To compute its
intensity, we must divide its amount P J2 by the area of
the plane, which is ^2, and we obtain the quotient P.
Similar reasoning applies to the other diagonal plane B D.
P is taken as the measure of the shearing stress. The
above discussion shows that it may be defined as the
intensity of the stress either on the planes of purely normal
stress, or on the planes of purely tangential stress.
6 1. A shearing stress, if applied to a body which has
the same properties in all directions (an isotropic body),
produces a simple shear with the same axes as the stress;
for the extension in the direction of the pull will be equal
to the compression in the direction of the thrust ; and in
the third direction, which is perpendicular to both of
these, there is neither extension nor contraction, since
52 UNITS AND PHYSICAL CONSTANTS. [CHAP.
the transverse contraction due to the pull is equal to
the transverse extension due to the thrust.
A shearing stress applied to a body which has not the
same properties in all directions, produces in general a
shear with the same axes as the stress, combined with
some other distortion.
In both cases, the quotient of the shearing stress by
the shear produced is called the resistance to shearing.
In the case of an isotropic body, it is also called the
simple rigidity.
62. The following values of the resilience of liquids
under compression are reduced from those given in
Jamin, ' Cours de Physique,' 2nd edition, torn. i. pp. 168
and 169 :
Temp.
Cent.
1
Coefficient of
Resilience.
Compression for
one Atmosphere
(megadyne per
square centim.)
Me
Wa
rcury,
o
O'O
O'O
I -5
4'i
10-8
I3'4
18-0
25-0
34'5
43'o
53'o
o-o)
i 'C
f 14-0 \
7'3
(I3'i i
i7'5
3'436 x
2'02 X
i '97
2-03
2'II
2'13
2'2O
2'22
2-24
2'29
2-30
9-2 x
7-8
7-2
I '22 X
I '12
2'33
[O 11
I0 1 *
O 9
O io
2-91 x
4-96 x
5-08
4.92
473
470
4'55
4'5o
4 '47
4-36
4'35
i '09 x
1-29
1-38
8-17
8-91 x i
4-30 ,
[o- 6
to- 5
ter,
-
';.
o *
o- 6 !
i
Eth
Ale
Sea
er,
ohol,
water, .
STRESS, STRAIN, AND RESILIENCE.
53
63. The following are reduced from the results ob-
tained by Amaury and Descamps, ' Comptes Rendus,'
torn. Ixviii. p. 1564 (1869), and are probably more
accurate than the foregoing, especially in the case of
mercury :
Coefficient of
Resilience.
Compression for
one megadyne per
square centim.
Distilled water,.
1C
2 '22 X IO 10
s
4-51 x io~
Alcohol
o
I '21 ,,
S'24.
1C
I'll ,,
8'99 ,,
Ether,
o
9*30 x io 9
I "08 x io
7 '02
1*26
Bisulphide of carbon,..
Mercury,
14
1C
I -60 X IO 10
C/42 X IO 11
6-26 x lo-jj
I '84 X IO~
64. The following values of the coefficients of resilience
for solids are reduced from those given in my own papers
to the Royal Society (see ' Phil. Trans.,' Dec. 5th, 1867, p.
369), by employing the value of g at the place of obser-
vation, namely 981*4.
Young's
Modulus.
Simple
Rigidity.
*
Resilience of
Volume.
Density
Glass flint,
Another specimen
Brass, drawn,
Steel
6-03 xio 11
574 ,,
i -075 x io 12
2'IIQ
2-40 x io 11
2'35
3-66
8'IQ
4-15 xio 11
3'47
I '841 X IO 12
2-942
2*935
8'47I
7-840
Iron, wrought, ...
,, cast,
Copper, .
I'963
1-349
I '2^4
7-6 9
5'32
4- '4-7
1-456
9 '64 x io 11
I '684 X IO 12
7-677
7-235
8-841
65. The resilience of volume was not directly ob-
served, but was calculated from the values of " Young's
54 UNITS AND PHYSICAL CONSTANTS. [CHAP.
modulus "' and " simple rigidity," by a formula which
is strictly true for bodies which have the same properties
in all directions. The contraction of diameter in lateral
directions for a body which is stretched by purely longi-
tudinal stress was also calculated by a formula to which
the same remark applies. The ratio of this lateral con-
traction to the longitudinal extension is called " Poisson's
ratio," and the following were its values as thus calculated
for the six bodies experimented on :
Glass, flint, '258 Iron, wrought, ... "275
Another specimen, '229 ,, cast, '267
Brass, drawn, '469 (?) Copper, '378
Steel, "310
Kirchhoff has found for steel the value '294, and Clerk
Maxwell has found for iron '267. Cornu (' Comptes
Rendus,' Aug. 2, 1869) has found for different
specimens of glass the values '225, '226, "224, '257,
236, -243, -250, giving a mean of '237, and maintains
(with many other continental savants) that for all isotropic
solids (that is, solids having the same properties in all
directions) the true value is J.
66. The following are reduced from Sir W. Thomson's
results (Troc. Roy. Soc.,' May, 1865), the value of g being
981-4:
Simple Rigidity.
Brass, three specimens, ... 4 '03 3^48 3*44 \
Copper, two specimens, ... 4*40 4 '40
Other specimens of copper in abnormal states gave
results ranging from 3*86 x io n to 4*64 x lo 11 .
67. The following are reduced from Wertheim's re-
sults ('Ann. de Chim.,' ser. 3. torn, xxiii), g being taken as
981 :
v.j STRESS, STRAIN, AND RESILIENCE. 55
Different Specimens of Glass (crystal}.
Young's modulus, 3-41 to 4-34, mean 3*96 )
Simple rigidity, 1*26 to 1*66, ,, 1*48 V X io 11
Volume resilience, ... 3*50 to 4*39, ,, 3'^9 )
Different Specimens of Brass.
Young's modulus, 9*48 to 10*44, mean 9*86 \
Simple rigidity, 3 -53 to 3-90, ,, 3-67 V x io' 1
Volume resilience, 10*02 to 10*85, ,, 10*43 J
68. Savart's experiments on the torsion of brass wire
('Ann. de Chim.' 1829) lead to the value 3-61 x io 11 for
simple rigidity.
Kupffer's values of Young's modulus for nine different
specimens of brass, range from 7-96 x io 11 to 11-4 x
io 11 , the value generally increasing with the density.
For a specimen, of density 8-4465, the value was 10*58
X 10 11 '
For a specimen, of density 8*4930, the value was 11-2
x ro 11 .
The values of Young's modulus found by the same
experimenter for steel, range from 20*2 x io 11 to 21*4
x io 11 .
69. The following are reduced from Rankine's c Rules
and Tables,' pp. 195 and ^196, the mean value being
adopted where different values are given :
Tenacity. Young's Modulus.
Steel bars, 7*93 x io 9 2*45 x io 12
Iron wire, $'86 ,, I *745 >
Copper wire, 4*14 ,, 1*172 ,,
Brass wire, 3*38 ,, 9'8i x io 11
Lead, sheet, 2*28 x io 8 5-0 x io 10
Tin, cast, 3*17 ,,
Zinc, 5*17
56 UNITS AND PHYSICAL CONSTANTS.
Tenacity. Young's Modulus.
Ash, I-I72XI0 9 i'io xio 11
Spruce, 8*55 x io 8 i'io ,,
Oak, i*o26xio 9 i'O2 ,,
Glass, 6-48 xio 8 5*52 xio 11
Brick and cement, ... 2*0 xio 7
The tenacity of a substance may be denned as the
greatest longitudinal stress that it can bear without tear-
ing asunder. The quotient of the tenacity by Young's
modulus will therefore be the greatest longitudinal exten-
sion that the substance can bear.
57
CHAPTER VI.
ASTRONOMY.
70. Size and Figure of the Ea
ACCORDING to the latest determination, as published by
Capt. Clarke in the ' Philosophical Magazine ' for August,
1878, the semiaxes of the ellipsoid which most nearly
agrees with the actual earth are, in feet,
a 20926629, b 20925105, c = 20854477,
which, reduced to centimetres, are
a = 6*37839 x io 8 , 3 = 6-37792 x io 8 , c = 6*35639 x io 8 ,
giving a mean radius of 6*3709 x io 8 , and a volume of
1*0832 x io 27 cubic centims.
The ellipticities of the two principal meridians are
T and _ T _
289-5 295-8
The longitude of the greatest axis is 8 15' W. The mean
length of a quadrant of the meridian is 1*00074 x io 9 .
The length of a minute of latitude is approximately
185200-940 cos. 2 lat. of middle of arc.
The mass of the earth, assuming Baily's value 5*67 for
the mean density, is 6*14 x io 27 grammes.
58 UNITS AND PHYSICAL CONSTANTS. [CHAP.
Day and Year.
Sidereal day, 86164 mean solar seconds.
Sidereal year, 31,558,150 ,,
Tropical year, 3 I >55 6 >9 2 9 >,
Angular velocity of earth's rotation, - 71 " -- =
80164
Velocity of points on the equator ) ,
due to earth's rotation,. . 1 46510 centims per second.
Velocity of earth in orbit, about... 2960600 ,,
Centrifugal force at equator due ) ,
to earth's rotation,.. ( 3'39o8 dynes per gramme.
Attraction in Astronomy.
7 1 . The mass of the moon is the product of the earth's
mass by '01 1364, and is therefore to be taken as 6-98 x io 25
grammes, the doubtful element being the earth's mean
density, which we take as 5*67.
The mean distance of the centres of gravity of the
earth and moon is 60*2734 equatorial radii of the earth
that is, 3-8439 x io 10 centims.
The mean distance of the sun from the earth is about
1-487 x io 13 centims., or 92-39 million miles, correspond-
ing to a parallax of 8*848 *
The intensity of centrifugal force due to the earth's
motion in its orbit (regarded as circular) is ( ?? j *i r de-
noting the mean distance, and T the length of the sidereal
year, expressed in seconds. This is equal to the accele-
ration due to the sun's attraction at this distance. Putting
for r and T their values, 1-487 x io 13 and 3*1558 x to 7 ,
(27T\ 2
~T~) r = *5*94- : ]
* This is the value of the mean solar parallax determined by Pro-
fessor Newcomb, and is adopted in the ' Nautical Almanac ' for
1882.
vi.] ASTRONOMY. 59
This is about ~ of the value of F at the earth's sur-
1660
face.
The intensity of the earth's attraction at the mean dis-
tance of the moon is about
081
-z or -2701.
(6o-27) 2
This is less than the intensity of the sun's attraction upon
the earth and moon, which is '5894 as just found. Hence
the moon's path is always concave towards the sun.
72. The mutual attractive force F between two masses
m and m', at distance /, is
F = C
where C is a constant. To determine its value, consider
the case of a gramme at the earth's surface, attracted by
the earth. Then we have
F = 981, m = i, m 6*14 x io 27 , / = 6*37 x io 8 ;
whence we find
c = 6-48 ^ _j_
io s 1-543 x io 7 '
To find the mass m which, at the distance of i centim.
from an equal mass, would- 'attract it with a force of i
dyne, we have i = Cm 2 ;
whence m = /I = 3928 grammes.
N, C
73. To find the acceleration a produced at the distance
of /centims. by the attraction of a mass of m grammes,
i F r^m
we have a = - C -,
m P
where C has the value 6*48 x io~ 8 as above.
60 UNITS AND PHYSICAL CONSTANTS. [CHAP.
72
To find the dimensions of C we have C = a , where the
m
dimensions of a are LT~ 2 .
The dimensions of C are therefore
L'M-'LT- 2 ; that is, L'M-'T-*.
74. The equation a = C^- shows that when a = i
and / = i, m must equal -*, that is to say, the mass
T^S
which produces unit acceleration at the distance of i
centimetre is 1*543 x io 7 grammes. If this were taken
as the unit of mass, the centimetre and second being
retained as the units of length and time, the acceleration
produced by the attraction of any mass at any distance
would be simply the quotient of the mass by the square
of the distance.
It is thus theoretically possible to base a general
system of units upon two fundamental units alone ; one
of the three fundamental units which we have hitherto
employed being eliminated by means of the equation
mass = acceleration x (distance) 2 ,
which gives for the dimensions of M the expression
L 3 T~ 2 .
Such a system would be eminently convenient in
astronomy, but could not be applied with accuracy to
ordinary terrestrial purposes, because we can only roughly
compare the earth's mass with the masses which we weigh
in our balances.
75. The mass of the earth on this system is the
product of the acceleration due to gravity at the earth's
surface, and the square of the earth's radius. This
product is
vi.] ASTRONOMY. 61
981 x (6-37 x io 8 ) 2 = 3-98 x I0 20 ,
and is independent of determinations of the earth's
density.
The new unit of force will be the force which, acting
upon the new unit of mass, produces unit acceleration.
It will therefore be equal to 1*543 x io r dynes; and its
dimensions will be
mass x acceleration = (acceleration) 2 x (distance) 2
= L 4 T~ 4 .
76. If we adopt a new unit of length equal to /
centims., and a new unit of time equal to / seconds, while
we define the unit mass as that which produces unit
acceleration at unit distance, the unit mass will be
/V~ 2 x i '543 x i o 7 grammes.
If we make / the wave-length of the line F in vacuo r
say,
4-86 x io~ 5 ,
and / the. period of vibration of the same ray, so that -
is the velocity of light in vacuo, say,
3 x io 10 ,
the value of / 3 /~ 2 or /(-) is
4*374 -* i 16 >
and the unit mass will be the product of this quantity
into i '543 x io 7 grammes. This product is 675 x io 23
grammes.
The mass of the earth in terms of this unit is
3-98 x io 20 + (4'374 x i 16 ) = 9 IOO >
and is independent of determinations of the earth's
density.
62
CHAPTER VII.
VELOCITY OF SOUND.
77. THE propagation of sound through any medium is
due to the elasticity or resilience of the medium ; and
the general formula for the velocity of propagation s is
where D denotes the density of the medium, and E the
coefficient of resilience.
78. For air, or any gas, we are to understand by E
the quotient
increment of pressure
corresponding compression '
that is to say, if P, P + p be the initial and final pres-
sures, and V, V - v the initial and final volumes, / and
^ being small in comparison with P and V, we have
v v
V
If the compression took place at constant temperature,
-we should have
VELOCITY OF SOUND. 63
But in the propagation of sound, the compression is
effected so rapidly that there is not time for any sensible
part of the heat of compression to escape, and we have
where y= i 41 for dry air, oxygen, nitrogen, or hydrogen.
p
The value of for dry air at / Cent, (see p. 38) is
(i + -00366*) x 7-838+ io s .
Hence the velocity of sound through dry air is
s= io 4 x/i'41 x (i + -00366/) x 7-838
= 33240 n/i + 00366 /;
or approximately, for atmospheric temperatures,
* 33240 + 60*.
79. In the case of any liquid, E denotes the resilience
of volume.*
For water at 8-i C. (the temperature of the Lake of
Geneva in Colladori's experiment) we have
E - 2-08 x i o 10 , D - i sensibly ;
" \'L> = N/E^ 1 44ooo,
the velocity as determined by Colladon was 143500.
80. For the propagation of sound along a solid, in the
form of a thin rod, wire, or pipe, which is free to expand
or contract laterally, E must be taken as denoting Young's
modulus of elasticity.* The values of E and D will be
* Strictly speaking, E should be taken as denoting the resilience
for sudden applications of stress so sudden that there is not time for
changes of temperature produced by the stress to be sensibly
6 4
UNITS AND PHYSICAL CONSTANTS. [CHAP.
different for different specimens of the same material
Employing the values given in the Table ( 64), we have
Values of E.
Values
ofD.
,E
Values of v D '
or velocity.
Glass, first specimen,
,, second specimen,..
Brass, .
6*03 x io 11
574
I'O7C X 1 1 12
2-942
2*935
8 "47 1
4-53 xio 5
4-42
Steel,
2'I^Q
T22
Iron, wrought,
1*96^
7'677
,
5'06
, , cast,
I "34.Q
Copper, .
1-234 ,,
8*84^
374
81. If the density of a specimen of red pine be *5, and
its modulus of longitudinal elasticity be 1*6 x io 6 pounds
per square inch at a place where g is 981, compute the
velocity of sound in the longitudinal direction.
By the table at the commencement of the present
volume, a pound per square inch (g being 981) is 6-9
x io 4 dynes per square centim. Hence we have for the
required velocity
. > '5
centims. per second.
82. The following numbers, multiplied by io 5 , are the
velocities of sound through the principal metals, as
determined by Wertheim :
diminished by conduction. This remark applies to both 79 and
80. For the amount of these changes of temperature, see a later
section under Heat.
VII.]
VELOCITY OF SOUND.
At 20 C.
At 100 C.
At 200 C.
Lead,
1*23
I'2O
Gold
I "16.
I '72
I "71
Silver,
2'6l
2'64.
2-4.8
Copper,. .,
3*6
3 '20
2'Q^
Platinum, .
J O w
2-60
2'C7
y ->
2*4.6
Iron,
C'l?
C'3O
4.'72
Iron wire (ordinary) , . . .
Cast steel,.
Steel wire (English), ..
4-92
4'99
is
5'10
4-92
5^4
TOI
479
5-00
The following velocities in wood are from the ob-
servations of Wertheim and Chevandier, ' Comptes
Rendus,' 1846, pp. 667 and 668 :
Along
Fibres.
Radial
Direction.
Tangential
Direction.
Pine,
3*32 x IO 5
2*83 x IO 5
I '^9 x IO 5
Beech
V34.
v67
2'87
Witch-elm, .
VQ2
^'4.1
* O 5
2"?Q
Birch
4. '4.2
2 '14.
7 Q'7
Fir,
4*64.
2'67
o u o >'
I '^7
Acacia,
4'7I
1 j/ >'
Aspen,
To8
83. Musical Strings.
Let M denote the mass of,a string per unit length,
F stretching force,
L length of the vibrating portion ;
then the velocity with which pulses travel along the
string is /F
VM'
and the number of vibrations made per second is
v
n =
2L'
66 UNITS AND PHYSICAL CONSTANTS.
Example.
For the 4 strings of a violin the values of M in grammes
per centimetre of length are
00416, '00669. '0106, '0266.
The values of n are
660, 440, 293!, 1955*-:
and the common value of L is 33 centims. Hence the
values of v or 2Ln are
43560, 29040, 19360, 12910
centims. per second ; and the values of F or Mz> 2 , in
dynes, are
7-89 x io 6 , 5-64 x io 6 , 3-97 x 10, 4-43 x io 6 .
84. Faintest Audible Sound.
Lord Rayleigh (' Proc. R.S..' 1877, vol. xxvi. p. 248),
from observing the greatest distance at which a whistle
giving about 2730 vibrations per second, and blown by
water-power, was audible without effort in the middle of
a fine still winter's day, calculates that the maximum
velocity of the vibrating particles of air at this distance
from the source was '0014 centims. per second, and that
the amplitude was 8'i x io~ 8 centims., the calculation
being made on the supposition that the sound spreads
uniformly in hemispherical waves, and no deduction being
made for dissipation, nor for waste energy in blowing.
CHAPTER VIII.
LIGHT.
85. ALL kinds of light have the same velocity in vacuo.
According to the most recent experiments by Cornu (see
'Nature,' February 4, 1875) this velocity is 3*004 x io ](>
centims. per second. Foucault's determination was
2-98 x io 10 .
The velocity of light of given refrangibility in any
medium is the quotient of the velocity in vacuo by the
absolute index of refraction for light of the given refrangi-
bility in that medium. If then ^ denote this index, the
velocity will be 3 . 004 x IQ io
J*
Light of given refrangibility is light of given wave-
frequency. Its wave-length in any medium is the quotient
of the velocity in that mediurn by the wave-frequency. If
;/ denote the wave-frequency (that is to say, the number
of waves which traverse a given point in one second), the
wave-length will be 3-004 x i 10
*/i
86. The following are the wave-lengths adopted by
Angstrom for the principal Fraunhofer lines in air at 760
millims. pressure (at Upsal) and i6C. :
68 UNITS AND PHYSICAL CONSTANTS. [CHAP.
Centims.
A 7-604 x io- 5
B 6-867
C 6-56201 ,,
Mean of lines D 5-89212 ,,
E 5-26913 ,,
F 4-86072 ,,
H 1 ......... 3-96801
These numbers will be approximately converted into
the corresponding wave-lengths in vacuo by multiplying
them by 1-00029.
87. The formula established by the experiments of
Biot and Arago for the index of refraction of air was
p - i = >0002 943 . _^_
i + at 760
/ denoting the temperature Centigrade, a the coefficient
of expansion "00366, and h the pressure in millims. of
mercury at zero. As the pressure of 760 millims. of such
mercury at Paris is 1-0136 x io 6 dynes per square centim.,
the general formula applicable to all localities alike will
be _ i = -0002943 P
I + '00366 / 1*0136 x 10'
where P denotes the pressure in C.G.S. units. This can
be reduced to the form
-0002903 P_. ()
i + -00366 / io 6
88. Adopting 3^Lllf^ that is 3-0033 x io 10 , as the
1*00029
velocity of light in air, and neglecting the difference of
velocity between the more and less refrangible rays, we
VIIL] LIGHT. 69
obtain the following quotients of velocity in air by wave-
length :
Vibrations per second.
A 3-950 X IO U
B 4'373
c 4-577
D 5'97 ,.
E 5700 ,,
F 6-179
G 6-973 ,<
H 1 7-569
H 2 7-636
INDICES OF REFRACTION.
89. Dr. Hopkinson ('Proc. R. S.,' June 14, 1877,) has
determined the indices of refraction of the principal
varieties of optical glass made by Messrs. Chance, for the
fixed lines A, B, C, D, E, b, F, (G), G, A, H r By D is
to be understood the more refrangible of the pair of
sodium lines ; by b the most refrangible of the group of
magnesium lines ; by (G) the hydrogen line near G.
In connection with the results of observation, he
employs the empirical formula
//. - i = a {i + bx (i + ex) },
where x is a numerical name for the definite ray of which
//. is the refractive index. In assigning the value of x,
four glasses hard crown, soft crown 1 , light flint, and dense
flint were selected on account of the good accord of
their results ; and the mean of their indices for any given
ray being denoted by /*, the value assigned to x for this
ray is /Z - /ip where ji? denotes the value of p for the
line F.
70 UNITS AND PHYSICAL CONSTANTS. [CHAP.
The value of fi as a function of A, the wave-length in
io~ 4 centimetres, was found to be approximately
/* = 1-538414 4- 0-0067669 p - 0-0001734 - 4
+ 0-000023 j -
The following were the results obtained for the different
specimens of glass examined :
Hard Crown, 1st specimen, density 2*48575.
a = 0-523145, 3=1-3077, ^-=-2-33.
Means of observed values of fi.
A 1-511755; B 1-513624; C 1-514571; D 1-517116;
E 1-520324; b 1-520962; F 1-523145; (G) 1-527996;
G i -528348 ; h i -530904 5 Hj i -532789-
Soft Crown, density 2 '55035.
a = 0-5209904, b = i -4034, c = - I -58.
Means of observed values of /u.
A 1-508956; B 1-510918; C 1-511910; D 1-514580;
E 1-518017; b 1-518678; F 1-520994; (01*526208;
G 1-526592; h 1-529360; H! 1-531415-
Extra Light Flint Glass, density 2-86636.
a = 0-549123, b= 17064, c= -0-198.
Means of observed values of /i.
A 1-534067; B 1-536450; C r537682;
D 1-541022; 1-545295; ^1-546169;
F i -549125 ; (G) i -555870 ; G i -556375 ;
h I-559992; H! 1-562760.
Light Flint Glass, density 3 '20609.
a = 0-583887, b = I -9605, c - 0-53.
Means of observed values of /u.
B 1-568558; C 1-570007; D 1-574013;
E 1-579227; b 1-580273; F 1-583881;
(G) 1-592184; G 1-592825; h r597332;
H! 1-600717.
vin. J LIGHT. 71
Dense Flint, density 3*65865.
a 0*634744, b 2*2694, c 1*48.
Means of observed values of /*.
B 1*615704; C 1-617477; D 1*622411;
E 1*628882; b 1-630208; F 1*634748;
(0)1*645268; 01*646071; / 1-651830;
H! 1*656229.
Extra Dense Flint, density 3*88947.
a = 0*664226, b 2*4446, c 1*87.
Means of observed values of /x.
A 1-639143; B 1-642894; C 1-644871;
D 1*650374; E 1-657631; b 1-659108;
F 1-664246; (O) 1*676090; G 1-677020;
h 1-683575; H! 1-688590.
Double Extra Dense Flint, density 4-42162.
a 0*727237, b 2*7690, c 2*70.
Means of observed values of /t.
A 1*696531; B 1-701080; C 1*703485;
D 1-710224; E 1-719081; b 1-720908;
F 1-727257; (0)1742058; 01*743210;
h 1751485.
INDICES OF REFRACTION FOR LIQUIDS.
90. The following values of indices of refraction for
liquids are condensed from Fraunhofer's determinations,
as given by Sir John Herschel ('Enc. Met. Art./ Light,
P- 415):
Water > density I -ooo.
B 1*3309; C 1-3317; D 1-3336;
E I-3358; F 1-3378; 1-3413;
H 1-3442.
Oil of Turpentine, density 0*885.
B 1-4705; C I-47I5; D I-4744; E 1-4784;
F I -481 7; 01-4882; H 1-4939.
72 UNITS AND PHYSICAL CONSTANTS. [CHAP.
91. The following determinations of the refractive
indices of liquids are from Gladstone and Dale's results,
as given in Watts' ' Dictionary of Chemistry/ iii., pp.
629-631 :
Sulphide of Carbon, at temperature 11.
A 1-6142; B 1-6207; C 1-6240; D 1*6333;
E 1-6465; F 1-6584; G 1-6836; H 17090.
Benzene, at temperature 10-5.
A 1-4879; B i '4913; C 1-4931; D i '4975;
E 1-5036; F 1-5089; G 1-5202; H 1-5305.
Chloroform, at temperature 10.
A 1-4438; B 1-4457; C 1-4466; D 1-4490;
E 1-4526; F 1-4555; G 1-4614; H 1-4661.
Alcohol, at temperature 15.
A 1-3600; B 1-3612; C 1-3621; D 1-3638;
E 1-3661; F 1-3683; G 1-3720; H 1-3751.
Ether, at temperature 15.
A 1-3529; B i -3545; C 1-3554; 01-3566;
E 1*3590; F 1-3606; G 1-3646; H 1-3683.
Water, at temperature 15.
A 1-3284; B 1-3300; C 1-3307; D 1-3324;
E i'3347; F i '3366; G 1-3402; H 1-3431-
DOUBLE REFRACTION.
92. The following indices of doubly refracting crystals
are from the table at the end of Lloyd's ' Light and
Vision ' :
Diamond, 2-439 to 2755
Chromate of lead (least refraction), - 2-500
(greatest ), - 2-950
Zircon (least refraction), - - - 1*961
(greatest ), - - - 2-015
VIII.]
LIGHT.
73
Carbonate of lead (least refraction),
,, (greatest ,, ),
Brazilian topaz (ordinary index),
,, (extraordinary index),
Quartz (ordinary index),
,, (extraordinary index),
Arragonite (extraordinary index),
(ordinary ,, ),
Sulphate of copper (least refraction),
,, (greatest ,, ),
Iceland spar (least refraction),
,, (greatest ), -
Nitre (least refraction),
,, (greatest ,, ),
1-813
2-084
632
640
548
558
'535
693
531
552
w
665
335
514
93. The two following tables are from Watts' 'Dic-
tionary of Chemistry/ vol. iii., p. 615. The indices given
are for the yellow rays, except Wollaston's, which are for
the extreme red :
Indices of Refraction of Solids.
Index. Observer.
Chromate of lead, - 2*50 to 2 '97 Brewster.
Diamond, - - - 2*47 to 275 Brewster ; Rochon.
Phosphorus, - - 2^224 Brewster.
Glass of antimony, 2 '216 ,,
Sulphur (native), 2 '115 ,,
Zircon, - - - 1*95 Wollaston.
Nitrate of lead, - - I '866 Herschel.
Carbonate of lead, - i'8i to 2*08 Brewster.
Ruby, 1779
Felspar, - - - ^764 ,,
Tourmalin,- - - i'668 ,,
Topaz, colourless, - i'6io Biot.
Beryl, I -598 Brewster.
Tortoise-shell, - - 1-591 ,,
Emerald, - - - 1*585 ,,
Flint glass, - - - I -57 to I -58 Brewster ; Wollaston.
74
UNITS AND PHYSICAL CONSTANTS. [CHAP
Index.
Observer.
Rock-crystal,
1*547
Wollaston.
Rock-salt,
1-545
Newton.
Apophyllite,
1-543
Brewster.
Colophony,
1-543
Wollaston.
Sugar,
1-535
,,
Phosphoric acid,
1-534
Brewster.
Sulphate of copper,
1-531 to 1-552
>?
Canada balsam, - . *
I-532
Young.
Citric acid,
1-527
Brewster.
Crown glass,
i -525 to 1-534
,,
Nitre,
i"5H
,,
Plate glass, - -
1-514 to 1-542
Spermaceti,
l'503
Young.
Crown glass,
1*500
Wollaston.
Sulphate of potassium,
1*500
Brewster.
Ferrous sulphate,
1-494
,,
Tallow ; wax,
1-492
Young.
Sulphate of magnesium,
1-488
Brewster.
Iceland spar,
1-654
Malus.
Obsidian, - - -
1-488
Brewster.
Gum,
1-476
Newton.
Borax, ^ - -
1-475
Brewster.
Alum, - - -
1*457
Wollaston.
Fluorspar, - - -
1-436
Brewster.
Ice, - - - .
1-310
Wollaston.
Tabasheer, - -
1-1115
Brewster.
Indices of Refraction of Liquids.
Sulphide of carbon,
Oil of cassia,
Bitter almond oil,
Nut oil,
Linseed oil,
Oil of naptha, -
Rape oil, -
Olive oil, -
Oil of turpentine,
I '678 Brewster.
1-031 Young.
"603 Brewster.
5oo
485 Wollaston.
475 Young.
-475 Brewster; Youn<
470 Brewster.
-470 Wollaston.
VIII.]
LIGHT.
75
Oil of almonds, -
Oil of lavender, -
Sulphuric acid (sp. gr. 17),
Nitric acid (sp. gr. I "48), -
Solution of potash (sp. gr. I '410),
Hydrochloric acid (concentrated),
Sea-salt (saturated), -
Alcohol (i-ectified),
Ether,
Alum (saturated),
Human blood, -
White of egg, - - -
Vinegar (distilled), - -
Saliva, -
Water, ....
Index.
Observer.
1-469
Wollaston.
1-457
Brewster.
1-429
Newton.
1-410
Young ; Wollaston.
1-405
Fraunhofer.
1-410
Biot.
1-372
Herschel.
1-358
Wollaston.
1-356
Herschel.
1-354
Young.
1-351
Enler, jun.
1-372
Herschel.
1-339
Young.
1-336
Wollaston; Brewster.
INDICES FOR GASES.
94. The following indices of refraction of gases are
from the determinations of Dulong. They are for the
temperature oC, and the pressure of 76 c.m. of mercury
.at Paris :
Vacuum, - -
Hydrogen,
Oxygen,
Atmospheric air,
Nitrogen,
Nitric oxide,
Carbonic oxide,
Ammonia,
Carbonic acid gas, -
Nitrous oxide,
Sulphurous acid gas,
Chlorine,
oooooo
000138
000272
000294
000300
000303
000340
i -000385
i -000449
i -000503
i -000665
i -000772
76
UNITS AND PHYSICAL CONSTANTS. [CHAP.
DISPERSION IN GASES.
95. Croullebois ('Ann. de. Chim.', 1870, vol. xx., p.
185) has made the following determinations of the
indices of refraction of gases for the rays corresponding
to the fixed lines C, E, and G :
Indices.
Dispersion.
f
C
E G
G-C
Air, - --..'- 4
1-0002578
I -000305 1 I "0003 147
0000569
Nitrogen,
I -000258
1-000302 1-000321
000063
Oxygen, - - -
I '000255
i -000294 i -0003 1 5
000060
Hydrogen, -
i '000129
1*000140
000153
000024
Carbonic acid,
i -000395
i -000456
000496
oooioi
Chlorine,
I '000699
i -000792
000840
000141
Cyanogen,
I '000804
i -000834
000895
-000091
Sulphuretted hydrogen,
1-000599
i -000647
000691
000092
Ammonia, -
1-000374
i -000399
000444
000070
Carbonic oxide,
I -000301
i -000350
000391
000090
Olefiant gas,
1-000652
i -000694
000722
000070
Marsh gas, -
1-000412
1-000471
000502
000090
The " dispersive powers," as computed by the formula
G C
klj^ *W**WTT*U M*V*^
of refraction for white
light (as determined
by M. Croulle-
bois) are appended.
Dispersive
Index for
Power.
White Light.
Air, *
1864
I -0002943
Nitrogen, -
2086
1-0003019
Oxygen,
2040
I -OOO27O
Hydrogen, - -
1714
I-OOOI37
Carbonic Acid, -
2214
I '000440
Chlorine, - -
- - -1780
I -000774
Cyanogen, -
- -1091
I '000829
viii.]
LIGHT.
77
Sulphuretted hydrogen,
Ammonia, -
Carbonic oxide, - -
Olefiant gas, - -
Marsh gas, - - -
Dispersive
Power.
'1421
'1754
'2571
'1008
'1910
Index for
White Light.
'000639
"000390
'000344
'000669
'000449
96. The following very different determinations of the
indices of refraction of air for the principal fixed lines
were obtained by Ketteler (' Pogg. Ann./ vol. cxxiv., p.
390 ; ' Phil. Mag.,' 1866, vol. xxxii., p. 336) :
A 1-00029286
B 1*00029350
C 1-00029383
D 1-00029470
E 1-00029584
F 1-00029685
G 1-00029873
H 1-00030026
CHAPTER IX.
HEAT.
97. THE unit of heat is usually defined as the quantity
of heat required to raise, by one degree, the temperature
of unit mass of water, initially at a certain standard tem-
perature. The standard temperature usually employed is
o C; but this is liable to the objection that ice may be
present in water at this temperature. Hence 4 C. has
been proposed as the standard temperature ; and another
proposition is to employ as the unit of heat one hundredth
part of the heat required to raise the unit mass of water
from o to 1 00 C.
98. According to Regnault (' Mem. Acad. Sciences/
xxi. p. 729) the quantity of heat required to raise a given
mass of water from o to t C. is proportional to
/ + '00002 t~ + '0000003 / 3 (T)
The mean thermal capacity of a body between two stated
temperatures is the quantity of heat required to raise it
from the lower of these temperatures to the higher,
divided by the difference of the temperatures. The mean
thermal capacity of a given mass of water between o C.
and f is therefore proportional to
I + 'OOOO2 / + '0000003 / 2 . . . .,.'. (2)
HEAT. 79
The thermal capacity of a body at a stated temperature
is the limiting value of the mean thermal capacity as the
range is indefinitely diminished. Hence the thermal
capacity of a given mass of water at t is proportional to
the differential coefficient of (i), that is to
i + '00004 / + -0000009 t- (3)
Hence the thermal capacities at o and 4 are as i to
1*000174 nearly; and the thermal capacity at o is to the
mean thermal capacity between o and 100 as i to
1-005.
99. If we agree to adopt the capacity of unit mass of
water at a stated temperature as the unit of capacity, the
unit of heat must be defined as n times the quantity of
heat required to raise unit mass of water from this initial
temperature through - - of a degree when n is inde-
finitely great.
Supposing the standard temperature and the length of
the degree of temperature to be fixed, the units both of
heat and of thermal capacity vary directly as the unit of
mass.
In what follows, we adopt as the unit of heat (except
where the contrary is stated) the heat required to raise a
gramme of pure water through i C. at a temperature
intermediate between o and 4. This specification is
sufficiently precise for the statement of any thermal
measurements hitherto made.
100. The thermal capacity of unit mass of a substance
at any temperature is called the specific heat of the sub-
stance at that temperature.
The following determinations of specific heat by Dulong
8o UNITS AND PHYSICAL CONSTANTS. [CHAP.
and Petit agree very well with later determinations by
Regnault and other experimenters, except in the case of
platinum :
Mean Specific Mean Specific
Heat between Heat between
o and 100. o and 300.
Iron, .... -1098 . . -1218
Copper, - t49 - - -1013
Zinc, - '0927 - - -1015
Silver, - -0557 - - -06 11
Antimony, - - '0507 - - '0549
Platinum, - '0355 - -0355
Glass, .... -J770 - ... -1990
According to Pouillet's experiments, the mean specific
heat of platinum between
o and 1 00 is '0335
,, 300 ,, -0343
500 ,, -0352
,, 700 -0360
1000 ,, -0373
,, 1200 ,, -0382
101. Specific heat is of zero dimensions in length,
mass, and time. It is in fact the ratio
increment of heat in the substance
increment of heat in water
for a given increment of temperature, the comparison
being between equal masses of the substance at the actual
temperature and of water at the standard temperature.
The numerical value of a given concrete specific heat
merely depends upon the standard temperature at which
the specific heat of water is called unity.
102. The thermal capacity of unit volume of a substance
ix.] HEAT. 8 1
is another important element : we shall denote it by c.
Let s denote the specific heat, and d the density of the
substance ; then c is the thermal capacity of d units
of mass, and therefore c = sd. The dimensions of c in
length, mass, and time are the same as those of d, namely
M
. Its numerical value will not be altered by any
L 3
change in the units of length, mass, and time which
leaves the value of the density of water unchanged.
. In the C.G.S. system, since the density of water
between o and 4 is very approximately unity, the
thermal capacity of unit volume of a substance is the
value of the ratio
increment of heat in the substance
increment of heat in water
for a given increment of temperature, when the compari-
son is between equal volumes.
103. The following- table (from Miller's 'Chemical
Physics,' p. 313, fourth edition) exhibits the specific heats
of most of the elementary bodies, also their atomic
weights, and the product of the two :
Specific Atomic p ,
Heat. Weight. Product -
Diamond, - '1468 48 6*0464
Graphite, - /- - - * - -2018 33 6*6594
Wood Charcoal, - - - "2415
Silicon, fused, - - - '1750 35 6*125
,, crystallized, - - '1767
Boron, crystallized, - - - '250
Sulphur, native, ... -17760 32 5 '6832
Selenium, .... -08370 79-5 6*6541
Tellurium, .... '04737 129 6*1107
Magnesium, - - - - '2499 24 5 -9976
UNITS AND PHYSICAL CONSTANTS. [CHAP.
Zinc,
Cadmium,
Aluminium,
Iron,
Nickel, -
Cobalt, -
Manganese,
Tin,
Tungsten, . -.
Molybdenum, -
Copper, - % -
Lead,
Mercury, solid,
,, liquid,
Platinum,
Palladium,
Rhodium,
Osmium,
Iridium, -
Iodine, -
Bromine, solid,
,, liquid,
Potassium,
Sodium, - .-.
Lithium,
Phosphorus,
Arsenic, -
Antimony,
Bismuth,
Thallium,
Silver,
Gold,
104. Variation of Specific Heat with Temperature.
Bede's results (' Mem. couronnes de 1'Acad. de Brtix-
elles,' xxvii. i) have been summed up in the following
Specific
Heat.
Atomic
Weight.
Product.
-09555
65
6-2108
05669
112
6-3482
2143
27-5
5^730
II379
56
6-3722
10863
59
6 '4090
10696
59
63106
1217
55
6-6934
05623
118
6-6356
03342
184
6-1492
07218
96
6-931
09515
63-5
6-0419
03140
207
6-4999
03192
200
6-3840
03332
200
6 -6640
03243
197-2
6-3952
05927
1 06 -4
6-3072
05803
104-4
6-0582
'03063
198-8
6-0892
03259
197-2
6-4266
05412
127
6-8732
08430
So
67440
10600
80
8-4800
16956
39
6-6128
-29340
23
6-7480
9408
7
6-5856
18870
31
5 "8497
08140
75
6*1050
05077
122
6-1939
03084
2IO
6-4764
03255
2O4
6 '6402
05701
108
6-1570
03244
I96-6
6-3777
IX.]
HEAT.
formulae by Prof. G. C. Foster, who has communicated
them to the editor of this work :
Specific Heats at t.
Iron, - - - '1040 + "000144^
Copper, - - - '0892 + 'oooo65/
Tin, - - - '0512 + "000063^
Zinc, - - - '08595 + "000084^
Lead, - - - '0283 + 000036^
According to Violle, the specific heat of platinum
at f is '0317 + "000012 /, its latent heat of fusion
27*2, its melting point i775"5, an( ^ tne melting point of
silver 954.
According to H. F. Weber, the true specific heat of
diamond at t is
0947 + "000994 / "00000036 / 2 .
105. The following table (from Miller's 'Chemical
Physics,' p. 307) exhibits the specific heats of certain
substances in the solid form, as determined by Regnault,
along with the specific heats of the same substances
in the liquid form, as determined by Person :
Solid.
Liquid.
Sp. heat.
Temperature
between.
Sp. heat.
Temperature
between.
Ice,
5050
- 30 and
o
I 'OOOO
o and 20
Sodic nitrate, -
2782
j,
100
"4130
3 20 430
Potassic nitrate,
2387
o ,,
IOO
3318
35 >, 435
Sulphur, -
"2O26
o ,,
IOO
"2340
120 ,, 150
Phosphorus,
1788
-14
7
2045
50 ,, loo
Bromine, -
0843
-78
-20
"1 060
-12 ,, 4 8
Tin,
0562
o ,,
IOO
0637
250 350
Iodine,
0541
o ,,
IOO
1082
Not stated.
Lead,
0314
o ,,
IOO
0402
350 and 450
Bismuth, -
"0308
o
IOO
0363
280 380
Mercury, -
0319
...
...
0333
,, IOO
8 4
UNITS AND PHYSICAL CONSTANTS. [CHAP.
1 06. The following table (from Miller's ' Chemical
Physics/ p. 308) contains the results ofRegnault's experi-
ments on the specific heat of gases. The column headed
" equal weights " contains the specific heats in the sense
in which we have defined that term. The column headed
" equal volumes" gives the relative thermal capacities of
equal volumes at the same pressure and temperature :
Thermal Capacities of Gases and Vapours.
Enua.1
Equal.
Gets or Vapour,
J -*H u - cti>
Gcis or Vapour.
Vols.
Weights.
Vols.
Weights
Air,
Oxygen,
2375
2405
2375
2175
Hydrochloric )
acid. \
2352
1842
Nitrogen, . -
Hydrogen,
Chlorine, .
2 3 68
2359
2964
2438
3-4090
'I2IO
Sulphuretted )
hydrogen, i
Water, -
2857
2989
2432
4805
Bromine,
3040
0555
Alcohol,
7171
'4534
Nitrous oxide,
'3447
****
2262
Wood spirit, -
5063
4580
Nitric oxide, -
'2406
2317
Ether, -
I -2266
4796
Carbonic )
oxide, \
2370
2450
Ethyl chloride,
,, bromide,
6096
7026
2738
1896
Carbonic }
anhydride, \
3307
2163
,, disul- )
phide, j
I -2466
4008
Carbonic di- )
sulphide, \
4122
1569
Ethyl cyanide,
Chloroform, -
8293
6461
4261
1566
Ammonia,
'2996
5084
Dutch liquid, 7911
2293
Marsh gas,
3277
5929
Acetic ether,
I '2184
4008
Olefiant gas, -
4106
4040
Benzol, -
I 'OII4
"3754
Arsenious )
chloride, \
Silicic chloride,
7013
7778
'1122
1322
Acetone, ^
Oil of tur- )
pentine, \
8341
2-3776
4125
5061
Titanic , ,
Stannic ,,
8564
86 39
I29O
0939
Phosphorus )
chloride, \
6386
1347
Sulphurous |
anhydride, \
'34 1
' r S4
107. E. Wiedemann ('Pogg. Ann.' 1876, No. i, p. 39)
has made the following determinations of the specific
heats of gases :
ix.] HEAT. 85
Specific
Heat
-p .
At o.
At 100.
At 200.
Density.
Air, - - -
0-2389
...
I
Hydrogen,
3-410
0*0692
Carbonic oxide,
0-2426
...
...
0*967
Carbonic acid,
0-1952
0-2169
0*2387
I*529
Ethyl, -
0-3364
0*4189
0*5015
0*9677
Nitric oxide, -
0*1983
0*2212
0-2442
1-5241
Ammonia,
0*5009
0-53I7
0*5629
0*5894
Multiplying the specific heat by the relative density,
he obtains the following values of
Thermal Capacity of Equal Volumes.
At o. At 100. At 200.
Air, - - - - 0-2389
Hydrogen, - - - 0*2359
Carbonic oxide, ' - 0*2346
Carbonic acid, *- - 0*2985 0*3316 0-3650
.Ethyl, - - ,- - 0-3254 0-4052 0-4851
Nitri' oxide, - - - 0-3014 0-3362 0*3712
Ammonia, - - 0*2952 0*3134 0*3318
108. The same author (' Pogg. Ann.' 1877, New Series,
vol. ii., p. 195) has made trje following determinations of
specific heats of vapours at temperature f :
Vapour.
Range of Temp,
in Experiments.
Specific Heat.
Chloroform,
26 -9 to 1 89 *8
1341 + -0001354^
Bromic ethyl,
27*9 to 189*5
1354 + -003560^
Benzine,
34-1 to 115-1
2237 + "OOIO228/
Acetone, -
26-2 to 179-3
2984 + -0007738^
Acetic ether,
32*9 to 113-4
2738 + *ooo87oo/
Ether,
25-4 to 1 88 -8
'37 2 5 + 'ooo8536/
36 UNITS AND PHYSICAL CONSTANTS. [CHAP.
Regnault's determinations for the same vapours were
as follows :
Mean Specific Heat for this Range.
Vapour.
Temperature.
According to
Regnault.
According
Wiedemani
Chloroform,
117 to 228
1567
1573
Bromic ethyl, -
777 to 196-5
1896
1841
Benzine, -
116 to 218
'3754
3946
Acetone, -
129 to 233
4125
3946
Acetic ether,
U5 to 219
4008
4190
Ether,
70 tO 220
'4797
'4943
Regnault's determinations for the specific heats of the
liquids corresponding to some of these vapours are as
follows :
Chloroform, - .- '23235 + '000101432^
Acetone, - - - - - - '5064 + "000793^
Acetic ether, - - * - - '52741 + '0010464^
Regnault has also determined the mean specific heat
of bisulphide of carbon vapour between 80 and 147 to
be '1534, and between 80 and 229 to be '1613, and
has found for the specific heat of liquid bisulphide of
carbon the expression
23523 + -00016303^.
Schuller has found the specific heat of liquid benzine
to be
37980 + -OOI44/.
All these results are quoted by E. Wiedemann in the
paper above referred to.
109. The following approximate table of melting points
is based on that given in the second supplement to
Watts' ' Dictionary of Chemistry/ pp. 242, 243.
HEAT.
Platinum, -
2000
I Tin, - - - 2 3o
Palladium,
Gold,
195
1 200
! Selenium, - - 217
| Cane sugar, - 160
Cast iron, -
Glass,
1 200
IIOO
Sulphur, - II1[
! Sodium, - - 9
Copper, -
Silver,
1090
IOOO
1 Wax, - . - 68
I Potassium, -
Borax,
1000
Paraffin, _ - - 54
Antimony,
Zinc,
43 2
360
! Spermaceti, 44
! Phosphorus, - - 43
Lead,
33
j Water, -
Cadmium, -
320
j Bromine,
Bismuth, -
265
I Mercury, - 4
TTO. The folk
nvins: tal
)le (from Miller's ' Chemical
Physics/ p. 344) exhibits the change of volume of certain
substances in passing from the liquid to the vaporous
conditionunder the pressure of one atmosphere :
i volume of water yields 1696 volumes of vapour.
,, alcohol 528 ,, ,,
,, ether 298 ,, ,,
,, oil of turpentine 193 ,,
in. The following table (from Watts' 'Dictionary of
Chemistry/ vol. iii., p. 77) exhibits the latent heats of
fluidity of certain substances, together with their melting
rnmtc
Melting Latent
Point. Heat.
Tin, - - - 235 14-25
Silver, - - 1000 21 -I
Zinc, - - - 433 28>I
Chloride of calcium
(CaC1.3H 2 0), 28-5 40-7
Nitrate of potassium, 339 47 '4
Nitrate of sodium, 310-5 63*0
The latent heat of fluidity of water was found by Reg-
nault, and by Provostaye and Desains, to be 79. Bunsen,
by means of his ice-calorimeter (' Pogg. Ann./ vol. cxli.,
p. 30) has obtained the value 80-025. He finds the
specific gravity of ice to be '9167.
1 1 2. The following table of latent heats of vaporization
1
Melting
Latent
Point.
Heat.
Mercury,
- -39
2-82
Phosphorus,
- 44
5'0
Lead, -
- 332
5 '4
Sulphur,
Iodine,
- H5
- 107
9 '4
ii>'
Bismuth,
- 270
12-6
Cadmium, -
- 320
13-6
UNITS AND PHYSICAL CONSTANTS. [CHAP.
at atmospheric pressure
Physics/ p. 342 :
is from Miller's ' Chemical
Latent Heat for
Unit Mass.
Equal Volumes.
Xj
Steam = icx
DO.
Water, -
536-67
1000
Regnault.
,, -
535'90
Andrews.
Wood spirit,
26370
872-9
Alcohol, - .- r
202*40
963-1
i>
Fousel oil,
121-37
1104-7
Favre & Silbermann.
Formic acid,
120-72
574-4
11
Methyl formiate,
117*10
726-6
Andrews.
Butyric acid,
114-67
1043-8
F. & S.
Methyl acetate, -
110-20
843-5
Andrews.
Formic ether, -
105-30
806-0
Valeric acid,
I03-52
1092-0
F. &S.
Acetic acid,
lOI-pI
632-3
ii
Acetic ether,
105-80
963-0
j>
.; "
92-68
843-5
Andrews.
Ether,
90*45
692-3
> ~
91-11
695-4
F. & S.
Methyl butyrate,
8733
921-5
it
Carbonic disulphide, -
86-67
681-4
Andrews.
Oil of lemons, -
70-02
986-1
F. &S.
"
80-00
1125-6
Brix.
Oil of turpentine,
74-00
1040-5
,,
,,
6873
966-9
F. & S.
Terebene,
67-21
945-0
Oxalic ether,
7272
1097-5
Andrews.
Amylic ether, -
69-40
1134*0
F. & S.
Ethal, -
58-44
1452-0
,,
Phosphorus chloride,
51-42
752-9
Andrews.
Ethyl iodide, -
46-87
756-8
Methyl iodide, -
46-07
671-8
>
Bromine, -
45-60
754-1
Stannic chloride,
30-53
820-0
,,
Iodine, ...
23-95
627-9
F. & S.
IX.]
HEAT.
89
113. Regnault's approximate formula for what he calls
"the total heat of steam at /," that is, for the heat
required to raise unit mass of water from o to f in the
liquid state and then convert it into steam at /, is
606*5 + '305 /.
If the specific heat of water were the same at all tem-
peratures, this would give
606*5 - '695 /
as the heat of evaporation at t. But since, according
to Regnault, the heat require^ to raise the water from
o to f is
/ + 'OO002 t 2 + "0000003 ^ 3 ,
the heat of evaporation will be the difference between
this and the " total heat," that is, will be
606*5 - '695 / - '00002 ft - '0000003 / 3 ,
which is- accordingly the value adopted by Regnault as
the heat of evaporation of water at t.
114. According to Regnault, the increase of pressure
at constant volume, and increase of volume at constant
pressure, when the temperature increases from o to 100,
have the following values for the gases named :
At Constant
At Constant
Gas.
Volume.
Pressur
Hydrogen, - . *'
3667
3 66l
Air, - -
3665
3670
Nitrogen, -, . .-
3668
...
Carbonic oxide,
3667
3669
Carbonic acid,
'3688
3710
Nitrous oxide,
3676
3719
Sulphurous acid,
3845
3903
Cyanogen,
3829
3877
UNITS AND PHYSICAL CONSTANTS. [CHAP.
00366957
00367430
00365620
0036677
0037060
0037067
Jolly has obtained the following values for the co-
efficient of increase of pressure at constant volume :
Air,
Oxygen, -
Hydrogen,
Nitrogen,
Carbonic acid, -
Nitrous oxide, -
Mendelejeff and Kaiander have determined the co-
efficient of expansion of air at constant pressure to be
0036843.
115. The following table, showing the pressure of
aqueous vapour near the ordinary boiling point, is based
on Regnault's determinations, as revised by Moritz
(Guyot's tables, second edition, collection D, table
xxv.) :
Temperature.
o
99 -o
99*i
99*2
99 '3
99 '4
99 '5
99-6
997
99-8
99 "9
lOO'O
lOO'I
IOQ'2
I00'3
1 00 '4
100-5
iOQ'6
Centims. of
Mercury
at Paris.
73-3I9
74-382
74-650
74-9I8
75-I87
75*457
757 2 8
76*000
76-273
76-546
76-820
77-095
77-371
77-647
Dynes per
sq. cm.
9779
9-814
x io 5
9-885
9-920
9-956
9*992
i '0028 x
0064
oioo
-0136
0173
0209
0245
0282
0319
0356
ix.] HEAT. 91
iperature.
Centims. of
Mercury
at Paris.
Dynes per
sq. cm.
I00'7
77-925
1-0393 x io
100-8
78-203
1-0430
100-9
78-482
1-0467
lOI'O
78-762
I - 0505
1 1 6. Regnault's results as to the departures from
Boyle's law are given in the form
Mi = j A (m - i) B (m - i)*,
v o-to
V l denoting the volume at the pressure P b V the volume
at atmospheric pressure P , and m the ratio -.
For air, the negative sign is prefixed to A and the posi-
tive sign to B, and we have
log A - 3-0435120,
logB = 5-2873751.
For nitrogen, the signs are the same as for air, and we
have
log A = _4 '8399375*
log B = 6*8476020.
For carbonic acid, the negative sign is to be prefixed
both to A and B, and we have
log A = 3*9310399,
log B = 6'862472i.
For hydrogen, the positive sign is to be prefixed both to
A and B, and we have
log A = 4-7381736,
log B = 6-9250787.
92 UNITS AND PHYSICAL CONSTANTS. [CHAP.
117. The following determinations of the specific heat
of the same substance in different states are from Reg-
nault's experiments (' Mem. Acad. Sciences/ xxvi., pp.
327-332) :
Ice, mean sp. heat from - 78 to o, - - 0*474
,, - 20 to o, - - 0-504
Water, at temperatures below 100, - - I *
Steam, mean sp. heat between 128 and 220, 0-4805
Bromine, solid, mean sp. heat from 77 '8
to - 25, - - - - 0-0833
,, liquid, mean from 7 -3 to 10, - 0*1060
,, gaseous, mean from 83 to 228, - 0*0555
Alcohol, liquid, at - 20, .... -5053
o, - '5475
+ 20, ---- -5951
,, 40, - >6 479
60, .--. -7060
80, ... - 7694
,, gaseous, mean from 105 to 220, - "4534
Ether, liquid, at - 30, - - - - -5113
o, -5290
+ 30> - -5467
,, gaseous, mean from 70 to 220, - '4797
Sulphide of carbon, liquid, at 30, - - '2303
o, - - -2352
+ 3> - - '2401
45, - - "2426
,, gaseous, mean from 73 to
192, .... -1570
Benzene, liquid, mean from 20 to 71, - '43^0
gaseous, Ii6to2i8, - -3754
Oil of turpentine, liquid, at o, - - -- "4106
40, - -4538
120, - - - -5019
160, - - - -5068
,, gaseous, mean from 179
to 249, - - - -5061
ix.] HEAT. 93
Boiling Points.
1 1 8. The following table gives the temperatures (by
air thermometer) at which according to Regnault's ex-
periments ('Mem. Acad. Sciences/ xxvi., 658,) the
vapours of the liquids named exert a pressure equal to
that of 76 c.m. of mercury at Paris:
Nitrous oxide,
Carbonic anhydride,
Sulphydric acid, -
Ammonia, - - -
Chlorine,
Sulphurous anhydride,
Ether, ....
-87-90
-78-2
-61-8
-38-5
-33'6
10*08
34 '97
Sulphide of Carbon,
Chloroform, -
Alcohol,
Benzene,
Oil of turpentine, -
Mercury,
- 46 "2O
- 60-16
- 78-26
- 80-36
- I59-I5
- 357 >2 5
119. Change of volume in melting, from Kopp's ex-
periments (Watt's ' Diet.,' art. Heat, p. 78):
Phosphorus. Calling the volume at o unity, the volume at the
melting point (44) is 1*017 in the solid, and 1*052 in the
liquid, state.
Sulphur. Volume at o being I, volume at the melting point (115)
is 1*096 in the solid, and 1*150 in the liquid, state.
Wax. Volume at o being I, volume at melting point (64) is 1*161
in solid, and 1*166 in liquid, state.
Stearic acid. Volume at o being I, volume at melting point (70)
is 1*079 i n solid, and 1*198 in liquid, state.
Rose's fusible metal (2 parts bismuth, I tin, I lead). Volume at o
being I, volume at 59 is a maximum, and is 1*0027. Volume
at melting point (between 95 and 98) is greater in liquid
than in solid state by 1*55 per cent.
120. Temperature of evaporation and dew-point
(Glaisher's Tables, second edition, page iv). The fol-
lowing are the factors by which it is necessary to mul-
tiply the excess of the reading of the dry thermometer
94 UNITS AND PHYSICAL CONSTANTS. [CHAP.
over that of the wet, to give the excess of the tempera-
ture of the air above that of the dew-point :
Reading of
Dry Bulb Factor.
Therm.
- 10 C. = I4F. 876
- 5 23 7-28
o 32 3-32
+ 5 41 2-26
+ 10 50 2 '06
Reading of
Dry Bulb Factor.
Therm.
o o
20 68 1 79
25 77 170
30 86 i -65
35 95 i '60
Conductivity.
121. By the thermal conductivity of a substance
at a given temperature is meant the value of k in the
expression
where Q denotes the quantity of heat that flows, in time
/, through a plate of the substance of thickness x, the area
of each of the two opposite faces of the plate being A,
and the temperatures of these faces being respectively
i\ and z> 2 , each differing but little from the given temper-
ature. The lines of flow of heat are supposed to be
normal to the faces, or, in other words, the isothermal
surfaces within the plate are supposed to be parallel
to the faces ; and the flow of heat is supposed to be
steady, in other words, no part of the plate is to be gaining
or losing heat on the whole.
Briefly, and subject to these understandings, con-
ductivity may be denned as the quantity of heat that passes
in unit time, through unit area of a plate whose thickness is
unity, when its opposite faces differ in temperature by on?
degree.
ix.j HEAT. 95
122. Dimensions of Conductivity. From equation (i)
we have
*=^ * (2>
v 9 -f>t A/
The dimensions of the factor -^ are simply M, since
z> 2 - v^
the unit of heat varies jointly as the unit of mass and the
length of the degree. The dimensions of the factor
- X - are ; hence the dimensions of k are - . This is
Ar J_< 1 J_/ 1
on the supposition that the unit of heat is the heat
required to raise unit mass of water one degree. In
calculations relating to conductivity it is perhaps more
usual to adopt as the unit of heat the heat required to
raise unit volume of water one degree. The dimensions of
O L 2
^ will then be L 8 , and the dimensions of k will be
v^-v T
These conclusions may be otherwise expressed by
saying that the dimensions of conductivity are when
\ j L
the thermal capacity of unit mass of water is taken as
L 2
unity, and are - when the capacity of unit volume
of water is taken as unity. In the C.G.S. system the
capacities of unit mass and unit volume of water are
practically identical.
123. Let c denote the thermal capacity of unit volume
of a substance through which heat is being conducted.
Then - denotes a quantity whose value it is often neces-
sary to discuss in investigations relating to the transmis-
sion of heat. We have, from equation (2),
96 UNITS AND PHYSICAL CONSTANTS. [CHAP.
k Q ; x
c
_
A/'
where Q' denotes -. Hence - would be the numerical
c c
value of the conductivity of the substance, if the unit of
heat employed were the heat required to raise unit volume
of the substance one degree. Professor Clerk Maxwell
proposes to call - the thermometric conductivity, as dis-
tinguished from k, which is the thermal or calorimetric
conductivity.
Coefficient of Diffusion.
124. There is a close analogy between conduction and
diffusion. Let x denote the distance between two
parallel plane sections A and B to which the diffusion is
perpendicular, and let these sections be maintained in
constant states. Then, if we suppose one substance to be
at rest, and another substance to be diffusing through it,
the coefficient of diffusion K is denned by the equation
_
where y denotes the thickness of a stratum of the mixture
as it exists at B, which would be reduced to the state
existing at A by the addition to it of the quantity which
diffuses from A to B in the line /.
When the thing diffused is heat, the states at A and B are
the temperatures z\ and z> 2 , and y denotes the thickness of
a stratum at the lower temperature which would be raised
to the higher by the addition of as much heat as passes
in the time /. This quantity of heat, for unit area, will be
kt , x
ix.] HEAT. 97
which must therefore be equal to
whence we have
The "thermometric conductivity "- may therefore be re-
garded as the coefficient of diffusion of heat.
125. When we are dealing with the mutual inter-
diffusion of two liquids, or of two gases contained in a
closed vessel, subject in both cases to the law that the
volume of a mixture of the two substances is the sum of
the volumes of its components at the same pressure, the
quantity of one of the substances which passes any section
in one direction must be equal (in volume) to the quantity
of the other which passes it in the opposite direction,
since the total volume on either side of the section re-
mains unaltered ; and a similar equality must hold for the
quantities which pass across the interval between two
sections, provided that the absorption in the interval
itself is negligible. Let x as before denote the distance
between two parallel plane sections A and B to which the
diffusion is perpendicular. Let the mixture at A consist
of m parts by volume of the first substance to i - m of the
second, and the mixture at B consist of n parts of the
second to i - n of the first, m being greater than i - , and
therefore n greater than i - m. The first substance will
then diffuse from A to B, and the second in equal
quantity from B to A. Let each ol these quantities be
such as would form a stratum of thickness z (the vessel
being supposed prismatic or cylindrical, and the sections
G
98 UNITS AND PHYSICAL CONSTANTS. [CHAP.
considered being normal sections), then z will be pro-
portional to
m - ( i - n) . ^, ^ - m + n - i .
- : - tf. that is, to -- f,
x x
and the coefficient of interdiffusion K is defined by
the equation
rr Ml + 11 I . i \
z = K - -/. (2)
The numerical quantity m + ni may be regarded as
measuring the difference of states of the two sections
A and B.
Ify now denote the thickness of a stratum in the con-
dition of B which would be reduced to the state existing
at A by the abstraction of a thickness z of the second
substance, and the addition of the same thickness of the
first, we have (in)y + z as the expression for the
quantity of the first substance in the stratum after the
operation. This is to be equal to my. Hence we have
. ' ''**' * (3)
and substituting for z its value in (2) we have finally
which is of the same form as equation (i), y now denot-
ing the thickness of a stratum of the mixture as it exists
at B, which would be reduced to the state existing at A
by the addition to it of the quantity of one substance
which diffuses from A to B in the time /, and the removal
from it of the quantity of the other substance which
diffuses from B to A in the same time.
126. The following values of K in terms of the centi-
metre and second are given in Professor Clerk Maxwell's
ix.] HEAT. 99
' Theory of Heat,' 4th edition, p. 332, on the authority of
Professor Loschmidt of Vienna.
Coefficients of Interdiffusion of Gases.
Carbonic Acid and Air, .... "1423
,, ,, Hydrogen, - ... '5614
,, ,, Oxygen, ... '1409
,, ., Marsh Gas, - - - '1586
,, ,, Carbonic Oxide, - - '1406
,, ,, Nitrous Oxide, - - '0982
Oxygen and Hydrogen, - - - - 7214
,, ,, Carbonic Oxide, - - - '1802
Carbonic Oxide and Hydrogen, ... '6422
Sulphurous Acid and Hydrogen, - - '4800
k
127. These may be compared with the value of - for
air, which, according to Professor J. Stefan of Vienna, is
256.
The value of k for air, according to the same authority,
is 5-58 x io~ 5 , and is independent of the pressure. Pro-
fessor Maxwell, by a different method, calculates its value
at 5*4 x io~ 5 .
Results of Experiments on Conductivity of Solids.
128. Principal Forbes' results for the conductivity of
iron (Stewart on Heat, p. 261, second edition) are ex-
pressed in terms of the foot and minute, the cubic foot
of water being the unit of thermal capacity. Hence the
value of Forbes' unit of conductivity, when referred to
C.G.S., is , or 15-48; and his results must be
60
multiplied by 15*48 to reduce them to the C.G.S. scale.
His observations were made on two square bars ; the
side of the one being ij inch, and of the other an
loo UNITS AND PHYSICAL CONSTANTS. [CHAP.
inch. The results when reduced to C.G.S. units are as
follows :
Temp.
Cent. ij-inch bar. i-inch bar.
o
o - - -207 - - -1536
25 - - -1912 - - -1460
50 - , - -1771 - - -1399
75 . - ; - -1656 - - -1339
loo - - ... '1567 - - '1293
125 - ; - '1496 -' - -1259
150 - - "1446 - - '1231
175 - ; . - ' '1399 - - -1206
200 -- \ - V I3S6 T - "1183
225 - - '1317 - - '1160
250 - - ' -1279 - - -1140
275 - - '1240 - - 'II2I
129. Neumann's results ('Ann. de. Chim.' vol. Ixvi., p.
185) must be multiplied by '000848 to reduce them to
our scale. They then become as follows :
Conductivity.
Copper, .... i-ioS
Brass, - .- - - ^ ** "302
Zinc, - - - - '307
Iron, '164
German silver, ... -109
Ice, i - - - '0057
In the same paper he gives for the following substances
k k
the values of - or ; that is, the quotient of conductivity
sa c
by the thermal capacity of unit volume. These require
the same reducing factor as the values of k, and when
reduced to our scale are as follows :
ix.] ,-. HEAT. ioi
Values of -.
c
Coal, '00116
Melted sulphur, - - - '00142
Ice, *oi 14
Snow, .... -00356
Frozen mould, - - - '00916
Sandy loam, - - - '0136
Granite (coarse), - - - '0109
Serpentine, .... '00594
130. Sir W. Thomson's results, deduced from observa-
tions of underground thermometers at three stations at
Edinburgh ('Trans. R. S. E.,' 1860, p. 426), are given in
terms of the foot and second, the thermal capacity of a
cubic foot of water being unity, and must be multiplied
by (3 0-48) 2 or 929 to reduce them to our scale. The
following are the reduced results :
k, or k
Conductivity, ~ c '
Trap-rock of Calton Hill, - - - '00415 - '00786
Sand of experimental garden, - - '00262 - '00872
Sandstone of Craigleith Quarry, - - '01068 - '02311
k
My own result for the value of - from the Greenwich
underground thermometers ('Greenwich Observations,'
1860) is in terms of the French foot and the year. As
a French foot is 32-5 centifns., and a year is 31557000
seconds, the reducing factor is (32-5)% + 31557000; that
is> 3'347 x I0 ~ 5 - The result is
I
c
Gravel of Greenwich Observatory Hill, - '01249
Professors Ayrton and Perry ('Phil. Mag./ April, 1878)
determined the conductivity of a Japanese building stone
(porphyritic trachyte) to be '0059.
102
UNITS AND PHYSICAL CONSTANTS. [CHAP.
131. Angstrom, in ' Pogg. Ann./vols. cxiv. (i86i)and
cxviii. (1863), employs as units the centimetre and the
minute ; hence his results must be divided by 60. These
results, as given at p. 429 of his second paper, will then
stand as follows :
Copper, first specimen,
,, second specimen, -
Iron,
Value of *.
c
i '216 (i - '00214 t)
I'l63 (I ~ 'OOI5I9 /)
'224 (i -'002874 /)
He adopts for c the values
"84476 for copper ; "88620 for iron,
and thus deduces the following values of k :
Conductivity.
Copper, first specimen, - - i '027 (i - '00214
,, second specimen, - - -983 (i - '001519 t]
Iron, -199 (i - '002874/5
132. In Professor George Forbes's paper on conduc-
tivity ('Proc. R. S. E.,' February, 1873) the units are the
centim. and the minute; hence his results must be divided
by 60. Thus reduced, they are :
Ice, along axis, -
00223
Kamptulikon, -
oooi i
Ice, perpendicular to /
axis, - - \
00213
Vulcanized india- }
rubber, - - * ]
000089
Black marble,
00177
Horn,
000087
White marble, - -\
'00115
Beeswax, -
000087
Slate, - - \-
00081
Felt,
000087
Snow, - -
00072
Vulcanite,
0000833
Cork,
000717
Haircloth,
0000402
Glass, -
0005
Cotton-wool, divided,
0000433
Pasteboard, - -
000453
,, pressed,
0000335
Carbon, - -
000405
Flannel, -
0000355
Roofing-felt,
000335
Coarse linen,
0000298
Fir, parallel to fibre, -
0003
Quartz, along axis, -
000922
Fir, across fibre and \
'000088
,,
00124
along radius, - \
>
00057
Boiler-cement, -
000162
00083
Paraffin, -
00014
Quartz, perpendicular )
Sand, very fine, -
000131
to axis, - - \
'0040
Sawdust, ...
000123
,,
0044
ix.] HEAT. 103
Professor Forbes quotes a paper by M. Lucien De la
Rive ('Soc. de Ph. et d'Hist. Nat. de Geneve/ 1864) in
which the following result is obtained for ice,
Ice, ... "00230.
M. De La Rive's experiments are described in
* Annales de Chimie,' ser. 4, torn, i., pp. 504-6.
133. A Committee, consisting of Professors Herschel
and Lebour, and Mr. J. "F. Dunn, appointed by the British
Association to determine the thermal conductivities of
certain rocks, have obtained results, of which the follow-
ing (communicated to me in May, 1877, by Professor
Herschel) with some additions, within brackets, of later
determinations, are deemed the most reliable :
Substance. ^I'S" [f '
Iron pyrites, more than - - '01 more than '0170
Rock salt, rough crystal, - - "0113 '0288
Fluorspar, rough crystal, - - '00963 '0156
Quartz, opaque crystal [and
quartzites], .... '0080 to '0092 '017510-0190
[Siliceous sandstones (slightly wet), '00641 to '00854] '0130 to "0230
Galena, rough crystal, [inter-
spersed with quartz,] - - '00705 '0171
Sandstone and hard grit, dry, - '00545 to '00565 '0120
Sandstone and hard grit, thor-
oughly wet, - <- - -* '00590 to '00610 -oioo
[Micaceous flagstone, along the
cleavage, - i - - '00632 '0116
[Micaceous flagstone, across cleav-
age, '00441] '0087
Slate, along cleavage, - - '00550 to "00650 '0102
Do., across cleavage, - - '00315 to "00360 "0057
Granite [various specimens, about "00510 to "00550 "oiooto"Oi2O
Marbles, limestone, calcite, and
compact dolomite, - - - "00476 to '00560 "0085 to "0095
io 4
UNITS AND PHYSICAL CONSTANTS. [CHAP.
Substance.
Red serpentine (Cornwall),
[Caen stone (building limestone),
Whinstone, trap rock [and mica
schist], - - - *.
Clay slate (Devonshire),
[Tough clay- (sun-dried),
Do., soft (with one-fourth
of its weight of water,
Chalk, -
[Calcareous sandstone (firestone),
Plate-glass [German and] English,
[German glass toughened, -
Heavy spar, opaque rough crystal,
Fire-brick, -
Fine red brick, "* *
Fine plaster of Paris, dry plate,
Do., thoroughly wet,
[White sand, dry, -
Do., saturated with
water, about - * '*
House coal and cannel coal,
Pumice stone, -
Conductivity in
C.G.S. Units.
e-
- '00441
0065
), '004331
0089
ci __ ^
- -00280 to -00480
0055 to '0095
- -00272
0053
- -00223
0048
- -00310]
0035
- 'OO2OO tO 'OO33O
0046 to "0059
), 'OO2II
0049
h, [-00198 to] '00234
00395 to ?
- -00185]
00395
.1, -00177
...
- -00174
0053
- -00147
0044
- -00120
'0060 ) .
:, -00160
> about
0025 ]
- -00093
'0032
- "00700]
0120 about
- '00057 to '00113
0012 to '0027]
- -00055
...
134. Peclet in ' Annales de Chimie,' ser. 4, torn, ii., p.
114 [1841], employs as the unit of conductivity the trans-
mission, in one second, through a plate a metre square
and a millimetre thick, of as much heat as will raise a
cubic decimetre (strictly a kilogramme) of water one
degree. Formula (2) shows that the value of this conduc-
tivity, in the C.G.S. system, is
10000
100
ix.] HEAT.
His results must accordingly be divided by 100 ; and
they then become :
Gold, , -
Conductivity.
2128
Marble, -
Conductivity.
0048
Platinum, -
2095
Baked earth,
- ' -0023
Silver,
Copper, -
I9II
Iron,
0795
Zinc,
0774
Lead,
- ' -0384
The value given for lead was from direct experiment.
The values given for the other metals were not from
direct experiment, but were inferred from the value for
lead taken in conjunction with Despretz's results for the
relative conductivity of metals.
135. The same author published in 1853 a greatly
extended series of observations, in a work entitled
1 Nouveaux documents relatifs aux chauffage et a la
ventilation.' In this series, the conductivity which is
adopted as unity is the transmission, in one hour, through
a plate a metre square and a metre thick, of as much
heat as will raise a kilogramme of water one degree.
This conductivity, in C.G.S. units, is
1000 100 i , - . i
- . - - . - ; that is, --
i 10000 3600 360
The results must therefore be divided by 360 ; and
they then become as follows :
Density. Conductivity.
Copper, - ... . ... - I7 8
Iron, - - - "x - i - ... -081
Zinc, ..... ... -078
Lead, - - - - - - ... -039
Carbon from gas-retorts, - - i'6l "0138
io6
UNITS AND PHYSICAL CONSTANTS.
Density.
Conductivity.
Marble, fine-grained grey, - .-
2-68
0097
,, sugar-white, coarse-grained,
277
0077
Limestone, fine-grained,
2-34
0058
>, - -
2-27
0047
55 " "
2-17
0035
Lias building-stone, coarse-grained
2-24
0037
f
2 '22
0035
Plaster of Paris, ordinary, made up,
00092
,, very fine, ,,
1-25
00144
,, for casts, very fine,
made up,
H
'00122
Alum paste (marble cement), ,, -
173
00175
Terra-cotta,
1-98
00192
1-85
00142
Fir, across fibres,
48
00026
along fibres,
48
00047
Walnut, across fibres, -
00029
,, along fibres -
...
00048
Oak, across fibres
...
00059
Cork,
'22
00029
Caoutchouc, -
...
00041
Gutta percha, ....
'00048
Starch paste,
I'OI7
00118
Glass,
2 '44
002 1
> ~
2'55
0024
Sand, quartz, ....
i'47
00075
Brick, pounded, coarse-grained,
I'O
00039
, , passed through
silk sieve,
(.76
00046
Fine brickdust, obtained by decan-
J--55
00039
Chalk, powdered, slightly damp, -
)
92
00030
,, washed and dried,
8 5
00024
,, washed, dried, and
|
compressed, -
jl'02
00029
Potato-starch,
71
00027
Wood-ashes, - -
'45
00018
Mahogany sawdust, ...
3i
00018
IX.]
HEAT.
107
25
Density.
Wood charcoal, ordinary, powdered, "49
Bakers' breeze, in powder, passed
through silk sieve,
Ordinary wood charcoal, in powder,
passed through silk sieve, -
Coke, powdered, - - - '77
Iron filings, - - - - 2*05
Binoxide of manganese, - - I '46
Conductivity.
00022
OOOIQ
C00225
00044
'00044
00045
Woolly Substances.
Cotton Wool of all densities, -
Cotton swansdown (molleton de
coton), of all densities,
Calico, new, of all densities, -
Wool, carded, of all densities,
Woollen swansdown (molleton de
laine), of all densities,
Eider-down, - - - - ...
Hempen cloth, new ... -54
old --- -58
Writing-paper, white - - - '85
Grey paper, unsized ... -48
oooi 1 1
000139
000122
000067
000108
000144
000119
000119
000094
Emission and Surface Conduction.
136. Mr. D. M'Farlane has published (' Proc. Roy. Soc/
1872, p. 93) the results of experiments on the loss of heat
from blackened and polished copper in air at atmospheric
pressure. They need no reduction, the units employed
being the centimetre, gramme, and second. The general
result is expressed by the formulae
x -'000238 + 3'o6 x io~ 6 / 2'6 x io~ 8 / 2
for a blackened surface, and
x ='000168 + 1*98 x io~ 6 / 1*7 x io~ 8 / 2
for polished copper, x denoting the quantity of heat lost
joS
UNITS AND PHYSICAL CONSTANTS. [CHAP.
per second per square centim. of surface of the copper,
per degree of difference between its temperature and that
of the walls of the enclosure. These latter were blackened
internally, and were kept at a nearly constant temperature
of 14 C. The air within the enclosure was kept moist
by a saucer of water. The greatest difference of tempera-
ture employed in the experiments (in other words, the
highest value of /) was 50 or 60 C.
The following Table contains the values of x calculated
from the above formulae, for every fifth degree, within the
limits of the experiments.
Value
of jr.
Difference of
Rcitio.
Temperature.
Polished Surface.
Blackened Surface.
o
5
000178
OOO252
707
10
OOOI86
OOO266
699
15
OOOI93
000279
692
20
000201
000289
695
25
OOO2O7
000298
6 94
30
000212
000306
693
35
OOO2I7
000313
6 93
40
'OOO22O
000319
693
45
000223
000323
6 9 o
5o
OOO225
'000326
690
55
000226
000328
690
60
OOO226
000328
690
137. Professor Tait has published ('Proc. R. S. E.'
1869-70, p. 207) observations by Mr. J. P. Nichol on the
loss of heat from blackened and polished copper, in air,
at three different pressures, the enclosure being blackened
internally and surrounded by water at a temperature of
IX.]
HEAT.
109
approximately 8 C.* Professor Tait's units are the grain-
degree for heat, the square inch for area, and the hour for
time. The rate of loss per unit of area is
heat emitted
area x time
The grain-degree is -0648 gramme-degree.
The square inch is 6 '45 14 square centims.
The hour is 3600 seconds.
Hence Professor Tait's unit rate of emission is
0648
= 279
10
6-4514 x 3600
of our units. Employing this reducing factor, Professor
Tait's Table of Results will stand as follows :
Pressure 1*014 * Io6 [7^o millims. of mercury].
Blackened.
-LJlclClVtl
Temp. Cent.
Loss per sq. cm.
Temp. Cent.
-LJ1 It'lll.
Loss per sq. en
6l''2 - J /
per second.
- -01746
63'8 -
per second.
- -00987
50-2 - \-
- '01360
57'i -
- ; - -00862
41-6 -
- -01078
50-5 -
- -00736
34*4 - ) -
- -00860
44-8 -
- -00628
273 -
- '00640
40-5 -
00562
20-5 -
- '00455
34'2 -
- -00438
29-6 -
- -00378
23-3 -
- -00278
iS'6 -
4T
- -00210
Pressure
1-36 X io 5 [102 millims.
of mercury].
62-5 - -
- -01298
67-8 -
- -00492
57'5 -
"01158
61-1 -
- "00433
53'2 -
- -01048
55
- - - -00383
47'5 - '
- -00898
497 -
- -00340
43
- -00791
44 -9 -
- -00302
28-5 - -
- -00490
40-8 -
- -00268
* This temperature is not stated in the "Proceedings," but has
been communicated to me by Professor Tait.
no UNITS AND PHYSICAL CONSTANTS. [CHAP.
Pressure 1-33 X lO 1 [10 millims. of mercury].
Blackened.
Temp. Cent. Loss per sq. cm.
per second.
Bright.
Temp. Cent. Loss per sq. m.
o per second.
62-5 - -
01182
65 -
- -00388
S7'5 ' -
01074
60
- -00355
54'2
. '
01003
5o
- -00286
417
00726
40
00219
37*5
"
00639
30
- -00157
341
*
00569
23-5 - - - -00124
27-5
< .- '00446
24-2
- -00391
Mechanical Equivalent of Heat.
138. The value originally deduced by Joule from his
experiments on the stirring of water was 772 foot-pounds
of work (at Manchester) for as much heat as raises a
pound of water through i Fahr. This is 1389-6 foot-
pounds for a pound of water raised i C, or 1389-6 foot-
grammes for a gramme of water raised i C. As a foot
is 30-48 centims., and the value of g at Manchester is
981-3, this is 1389-6 x 30-48 x 981-3 ergs per gramme-
degree ; that is, 4-156 x io 7 ergs per gramme-degree.
A later determination by Joule (* Brit. Assoc. Report/
1867, pt. i., p. 522, or ' Reprint of Reports on Electrical
Standards,' p. 186) is 25187 foot-grain-second units of
work per grain-degree Fahr. This is 45337 of the same
units per grain-degree Centigrade, or 45337 foot-gramme-
second units of work per gramme-degree Centigrade;
that is to say,
45337 x (3'48) 2 = 4*212 x io 7
ergs per gramme-degree Centigrade.
At the meeting of the Royal Society, January, 1878
(' Proceedings,' vol. xxvii., p. 38), an account was given by
Joule of experiments recently made by him with a view
ix.] HEAT. in
to increase the accuracy of the results given in his former
paper. ('Phil. Trans., 1850.') The result he has now
arrived at from the thermal effects of the friction of water,
is, that taking the unit of heat as that which can raise a
pound of water, weighed in vacuo, from 60 to 61 of the
mercurial Fahrenheit thermometer ; its mechanical equiva-
lent, reduced to the sea-level at the latitude of Greenwich,
is 77 2 '55 foot-pounds.
To reduce this to water at o C. we have to multiply
by 1*00089,* giving 773-24 ft. Ibs., and to reduce to ergs
per gramme-degree Centigrade we have to multiply by
Q
981-17 x 30*48 x .
The product is 4*1624 x io 7 .
139. Some of the best determinations by various experi-
menters are given (in gravitation measure) in the following
list, extracted from Watt's ' Dictionary of Chemistry,'
Supplement 1872, p. 687. The value 429*3 in this list
corresponds to 4*214 x io 7 ergs :
Him, - 432 - - Friction of water and brass.
, , * 433 - - Escape of water under pressure.
- 441*6 - - Specific heats of air.
,, * 4 2 5' 2 - Crushing of lead.
Joule, - 429*3 - - | He^produced by an electric
Violle,
435*2 (copper) - '
434*9 (aluminium)
435 '8 (tin)
Heat produced by induced
currents.
437*4 (lead) -
Regnault, 437 - - Velocity of sound.
We shall adopt 4*2 x io 7 ergs as the equivalent of
* This factor is found by giving / the value 15*8 (since the tem-
perature 60*5 Fahr. is 15*8 Cent.) in formula (3) of art. 98.
ii2 UNITS AND PHYSICAL CONSTANTS. [CHAP.
i gramme-degree ; that is, employing J as usual to denote
Joule's equivalent, we have
J = 4'2 x io 7 = 42 millions.
140. Heat and Energy of Combination with Oxygen.
i gramme of
Compound
Gramme-
degrees of heat
Equivalent
Energy, in
produced.
ergs.
Hydrogen, -
Carbon,
H 2 O
CO 2
34000 A F
8000 A F
1-43 x io 12
3-36 x io 11
Sulphur, - - .
SO 2
2300 A F
9-66 x io 10
Phosphorus,
P-2Q5
5747 A
2 '41 X IO 11
Zinc, -
ZnO
1301 A
5-46 x io 10
Iron, ...
Fe 3 O
1576 A
6-62 x io 10
Tin, -
SnO 2
1233 A
5-18
Copper,
CuO
602 A
2'53
Carbonic oxide, -
CO 2
2420 A
I'O2 X IO 11
Marsh-gas, -
C0 2 andH 2
13100 A F
5'5
Olefiant gas,
?>
11900 A F
S'oo .
Alcohol, -
6900 A F
2 '9 j >
Combustion in Chlorine.
Hydrogen, -
HC1
23000 F T
9 '66 X io 11
Potassium, -
KC1
2655 A
I'I2
' Zinc, -
ZnCP
1529 A
6-42 x io 10
Iron, - -
Fe 2 Cl
1745 A
7 '33
Tin, -
SnCl 4
1079 A
4'53
Copper,
CuCl 2
961 A
4*04
The numbers in the last column are the products of
the numbers in the preceding column by 42 millions.
The authorities for these determinations are indicated
by the initial letters A (Andrews), F (Favre and Silber-
mann), T (Thomsen). Where two initial letters are
given, the number adopted is intermediate between those
obtained by the two experimenters.
ix.] HEAT. 113
141. Difference between the two specific heats of a gas.
Let S-L denote the specific heat of a given gas at
constant pressure,
s 2 the specific heat at constant volume, '
a the coefficient of expansion per degree,
v the volume of i gramme of the gas in cubic
centim. at pressure/ dynes per square centim.
When a gramme of the gas is raised from o to i
at the constant pressure /, the heat taken in is $i t the
increase of volume is az>, , and the work done against
external resistance is