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TREATISE ON DYNAMICS. 
 
 BY W. P. WILSON, M.A., 
 
 FELLOW OF SAINT JOHN'S COLLEGE, CAMBRIDGE; 
 AND PROFESSOR OF MATHEMATICS IN QUEEN'S COLLEGE, BELFAST. 
 
 ?<-' -— ^^^.. 
 juiormy 
 
 ia^ambrOrge : MACMILLAN AM 
 ilonl>on; GEORGE BEIX. Oubltn • TIODGEh 
 

¥ 
 
 The following pages form the first portion of a Treatise 
 on Dynamics, and contain the fundamental principles of 
 the science, with their application to the motion of parti- 
 cles, and to the simpler cases of the motion of bodies of 
 finite magnitude. The remainder, which is in course of 
 preparation, will contain the higher investigations, and 
 the application of the principles to physical Astronomy, 
 together with a history of the discovery of the Laws of 
 Motion, and an account of the principal experiments that 
 have been made for the pm'pose of testing their accuracy, 
 and determining the attraction and mean density of the 
 earth. 
 
 Saint John's College, 
 Oct. 12, 1850. 
 
 3 CO. , 
 
 ) 
 VI) s. 
 
CONTENTS. 
 
 CHAPTER I. 
 
 PAGE 
 
 Elementary Notions — Laws of Motion — Equations of Motion . 1 — 35 
 
 CHAPTER n. 
 Methods of Integrating the Equations of Motion when the 
 
 Motion is in one line — and in one plane . . . 36 — 64 
 
 CHAPTER HI. 
 Methods of Integrating the Equations of Motion when the 
 
 Force is Central — Elliptic Motion .... 65 — 86 
 
 CHAPTER IV. 
 
 Properties of Motion not in one plane — Motion in a Resisting 
 Medium — Constrained Motion — Principle of Least Ac- 
 tion 87 — 112 
 
 CHAPTER V. 
 Motion of a System of Particles under their Mutual Attractions 
 
 — General Properties ...... 113 — 128 
 
 CHAPTER VI. 
 
 Motion of Bodies of Finite Magnitude — D'Alembert's Principle 
 — Motions of Translation and Rotation — 'Motion about a 
 Fixed Axis 129—148 
 
 CHAPTER VII. 
 
 Motion of a System of Bodies — Conservation of the Motion 
 of the Center of Gravity — and of Areas — and of Vis Viva 
 — Examples — Centrifugal Force .... 149—107 
 
 CHAPTER VIII. 
 
 Nature of Impact — Determination of the Motion after Impact 
 
 — ^Examples ........ 168—176 
 
TREATISE ON DYNAMICS. 
 
 CHAPTER I. 
 
 1. Mechanics is the science which treats of the effects produced 
 by force acting on material bodies. When the different forces acting 
 on any body counteract each other so that the body remains at rest, 
 the forces are said to be in equiHbrium. The consideration of the 
 conditions to which the forces must be subject that this may be the 
 case, is the object of the science of Statics. 
 
 When these conditions are not fulfilled by the forces, the body 
 will not remain at rest. The investigation of the laws which regulate 
 the motion which takes place, and of the nature of the motion itself, 
 will form the subject of the present treatise. 
 
 Before we proceed, however, there are certain ideas of which it 
 is necessary to form an accurate conception ; and, in order to be 
 definite, we will at present confine our attention to bodies so small 
 that they may without sensible error be treated as geometrical points, 
 but we must at the same time consider them to be possessed of all the 
 properties of matter. This is what must be understood when par- 
 ticles, or material points, or molecules are spoken of. 
 
 2. It would be useless to attempt to define space and time. 
 No explanation could in any way render the ideas clearer. The 
 measures of them, on the contrary, require the greatest degree of 
 attention. In Dynamics we are only concerned with linear space, or 
 length, or distance, and this is always to be understood when the 
 term space is used. Now every concrete magnitude must be mea- 
 sured by some definite magnitude of the same kind; thus, space must 
 be measured by space, time by time. 
 
 1 
 
2 A TREATISE ON DYNAMICS. [cHAP. 
 
 With respect to space nothing can be easier. We can fix on some 
 definite length, and can take a rule or a piece of string of that length, 
 and apply it over and over again to the space which we wish to 
 measure to find how often it is contained in it ; and we consider that 
 we know the magnitude of that space w^hen we know the number of 
 times that our measure is contained in it. Thus, if it be the distance 
 between two points A and B that we wish to determine, we consider 
 that we know it when we have found that our measure will go in it 
 a times, a being whole or fractional ; and we say that 
 
 AB = a times the measure, 
 
 or more commonly, suppressing the measure, we say that AB = a. 
 In this case our measure is called the " unit of length," and the space 
 AB is said to be numerically represented by a. It is quite obvious 
 that the greater or less our measure or unit is chosen, the less or 
 greater will be the numerical representation of any given space AB. 
 The choice of this unit is perfectly arbitrary ; but we must always 
 bear in mind that it is a space. 
 
 3. We cannot apply the same method of proceeding to " time :" 
 for we are not able to take an interval of time and apply it to other 
 intervals to determine how often it is contained in them. An instant 
 of time, corresponding to a point in space, can only be marked by 
 the occurrence of some event. Now we can easily conceive a number 
 of events happening one after the other in such a manner that the 
 interval between any two shall be of the same duration as the interval 
 between any other two. It is possible and easy to conceive, a priori, 
 this equality of intervals, but it is impossible, a priori, to fix on any 
 series of events which we can be sure will so occur at equal intervals. 
 We shall see, when we have advanced somewhat further, that such 
 a series of events can be procured, but till then we must rest satisfied 
 with being able to conceive such a series. The possibility or impos- 
 sibility of such a series existing will in no wise affect the accuracy of 
 the notion of equal times. If Ave take one of these intervals as our 
 measure, we shall have any interval which lasts during n of those 
 intervals expressed by ?^ times the interval, where « may be whole or 
 fractional. And after this interval is agreed on, we consider the 
 length of any other interval determined when n is known, and w^e 
 express it simply by n: in other words, we take the agreed-on 
 interval as our unit. The duration of this " unit of time" is perfectly 
 arbitrary, and as it is greater or less, h the numerical representation 
 of any proposed interval will be less or greater. 
 
I.j A TREATISE ON DYNAMICS. 3 
 
 4. Having now explained the method of measuring time and 
 space, and of representing them numerically, we come to the motion 
 of a material point. The simplest kind of motion that we can con- 
 ceive is what is called " uniform rectilinear motion." When a point 
 moves so that at every instant during the whole duration of the 
 motion it is found in the same straight line, the motion is said to be 
 rectilinear. If, moreover, it moves so as always to pass over equal 
 spaces in equal intervals of time, at what part soever of the motion 
 those intervals be taken, or however long or short their duration, 
 then the motion is said to be uniform. Hence if it pass over a space 
 s in one interval, it would pass over a space 2* in two such intervals, 
 and a space ns in n such intervals. 
 
 5. Like space and time ''velocity" is a tei'ra which cannot be 
 defined. We may say it is the ''rate" of motion or the "pace" or 
 " speed," but we are only giving other words of the same meaning, 
 not explaining the idea. We can however, as in those cases, explain 
 accurately how it is measured. 
 
 Suppose two points to be moving uniformly as described above, 
 and suppose that the space which one describes in any interval of 
 time is equal to the space which the other describes in the same 
 interval, then the velocities of these two points are the same. 
 
 Now before we can express velocity numerically, it is necessary 
 to know what is meant when one velocity is said to be twice another. 
 We saw in the case of space, that if we took any given length, and at 
 the end of that took another length equal to the former, the whole 
 length so taken was twice the original length. 
 
 Similarly, if we supposed an interval of any definite duration, 
 and then at the end of it another interval of the same duration, the 
 whole interval would be twice one of the first intervals. 
 
 We cannot however adopt the same method with velocity, we 
 cannot form any distinct conception of what is meant by one velocity 
 being the sum of two other velocities without bringing to our aid 
 ideas which tacitly assume the point in question. The common 
 notion, however, is very simple and sufficiently exact. 
 
 Generally one thing is said to move twice as fast as another, or 
 to have twice the velocity of another when it passes over twice the 
 space in the same time. This is the foundation of the method of 
 representing velocity numerically. And this definition of double 
 velocity, or of "twice as fast," is at once applicable to any multiple 
 of the velocity. Thus, if a particle moving with a given velocity 
 passes over in a given time a space s (that is, a space whose nume- 
 
 1—2 
 
4 A TREATISE ON DYNAMICS. [cHAP. 
 
 rical representation is s), a particle moving with twice that velocity 
 would pass over in the same interval of time a space 2*; and a 
 particle moving with n times the given velocity would in the same 
 interval pass over a space 7is. If the first-mentioned velocity be 
 that chosen as a unit, the latter velocity would be represented nume- 
 rically by n. 
 
 The definition just given, of one velocity being ?? times another, 
 is also expressed by saying that the velocity varies as the space 
 described in a given interval of time. 
 
 Now suppose a point moving with a velocity represented as 
 above explained by v to pass over the space * in a given interval of 
 time t, and suppose another point to move so as to pass over an 
 equal space s in an n^^ part of that interval of time, then this latter 
 point would pass over a space 7is in this interval of time t, and 
 therefore its velocity would be represented by )iv. 
 
 This is expressed by saying that when two points describe equal 
 spaces their velocities are inversely as the times of describing them. 
 
 If a point describes uniformly a known space in a known time, 
 the velocity of that point is known as much as we can conceive a 
 velocity to be. Suppose then that the velocity by which we measure 
 other velocities, or which we take as our unit of velocity, is that 
 with which a point would move through a space s^ in a time /,. 
 And suppose that a body moving with v' times this velocity would 
 describe a space s in the same time i^, then we have seen that 
 
 And suppose that a body moving with v" times this last velocity 
 would move over the space s in time /, then we have seen that 
 
 V 
 
 Also this last velocity is v'v" times the velocity which we have 
 taken as our measure. Let v'v"=v, then the last velocity is v times 
 our measure, and with it our point moves over the space s in the 
 time /• And referring to our equations we see that 
 , „ s t^ s /i 
 
 Si t t Si 
 
 If we choose as our measure such a velocity that the ratio — is 
 
 unity, then we have ^ = j' 
 
 This will be the case if we have /i = 1 and .Jj = 1, which is the 
 same thing as taking for our measure the velocity with which a 
 body would uniformly describe the unit of space in the unit of time. 
 
I.] A TREATISE ON DYNAMICS. 5 
 
 This for the future we shall always do. In that case the equation 
 
 v = -, which we shall consider as our fundamental equation, expresses 
 
 that the numerical representation of the velocity of a point is the 
 fraction whose numerator and denominator are respectively the 
 numerical representations of the space described and of the time 
 in which it is described. 
 
 6. We may observe that the particular length which we fix on 
 as our unit or measure of space, and the particular interval whose 
 duration we fix on as the unit or measure of time, are both perfectly 
 arbitrary and perfectly independent, but that when we have fixed 
 on them, we shall have fixed on the particular velocity which we 
 take as our unit of velocity. In different investigations different 
 units of time and space are chosen, but it is obviously essential that 
 throughout the same investigation the same units should be ad- 
 hered to. 
 
 7. We have hitherto considered the case of a material point 
 moving uniformly, and have seen how its velocity is measured and 
 numerically represented, and have obtained our fundamental equa- 
 tion V = T > which gives the same numerical value to v however large 
 
 or small t be taken. We will now consider the case of a body whose 
 velocity is changing from one instant to another. 
 
 The first question that arises is, " What do we mean when we 
 speak of the velocity of the point at any instant?" A little con- 
 sideration however will shew that our idea of velocity is indepen- 
 dent of the supposition of its being uniform. We can suppose a 
 body moving uniformly to be moving just as fast as another body, 
 whose motion is not uniform, was at some particular instant: in 
 other words, that at some particular instant their velocities were 
 equal. 
 
 If then at any instant we suppose the motion of a body to 
 become uniform, the velocity at that instant remaining unaltered, 
 the numerical representation of this uniform velocity will be the 
 numerical representation of the variable velocity at that instant. 
 
 Suppose now for distinctness that the velocity of a body at a 
 certain instant is increasing, and that its numerical representation 
 estimated as we have explained is v; and suppose that after an 
 interval 0/ has elapsed the velocity is v + lv, and that the space 
 which has been described in that time is ?.v. 
 
6 A TREATISE ON DYNAMICS. [cHAP. 
 
 (The expressions It, 6v, hs must be understood as single symbols 
 expressing no more than we have hitherto done by /, v, and j, that 
 is, they represent numbers, and are used as single symbols or single 
 letters.) 
 
 Also let S,?! be the space that would have been described, in the 
 time ht if the body had moved uniformly during that time with the 
 velocity v, and CS2 the space that would have been described in the 
 same time S t had the body moved uniformly with the velocity v + hv. 
 Then, from what has been shewn before, we have 
 
 V = -^ , and V + cv = -^ ' . 
 ct ct 
 
 Now the space hs which is actually described will be greater 
 than the space Isi and less than the space Is^. Therefore we shall 
 have 
 
 the fraction ^ greater tlian-j^, 
 
 and less than ^ f , 
 dt ' 
 
 that is, we shall have the fraction 
 
 ht 
 
 and this is true however small S^ be taken ; but by diminishing li we 
 may make hv less than any assignable quantity, and S* will also 
 be diminished at the same time ; if, therefore, in accordance with 
 
 the notation of the diiferential calculus, we represent by -j- the 
 
 di 
 
 it 
 
 limit to which the fraction -^ approaches when Zt is diminished 
 
 indefinitely, we shall have 
 
 ds 
 
 Tt = '- 
 
 This is another equation of the utmost importance. Let us stop 
 for a moment to consider its meaning. 
 
 Suppose that the distance of the body from some fixed point in 
 the line of its motion at the instant under consideration is s, and 
 that the whole time that has elapsed since some fixed epoch is t. 
 Had we considered the body at some different time the position 
 would have been different, that is, any change in the value of t is 
 accompanied by some corresponding change in the value of s, or 
 in analytical language, s is a function of f. 
 
 Now this being the case, we see that when the particle moves 
 forward through a space hs, its distance from the fixed point be- 
 
I.] A TREATISE ON DYNAMICS. 7 
 
 comes s + ls, or is increased by S*; similarly, the time that has 
 elapsed since the fixed epoch is t + cf, or t has been increased by It. 
 
 Hence ds and S< are the corresponding increments of s and t, and 
 
 g „ 
 
 their ratio is — and the limit of this ratio, which we have shewn 
 ci 
 
 to be equal to v, is the differential coefficient of s with respect to 
 t, consistently with the notation we have used for it. Hence then, 
 when it is known that a body moves so that the distance from a 
 fixed point is always represented by a certain function of the time 
 which has elapsed since a definite instant, the differential coeffi- 
 cient of this function, with respect to t, will express the velocity 
 of the particle at any time. And, conversely, if we know the velocity 
 of a particle at any time as a function of the time, and can find 
 a quantity of which this function is the differential coefficient, this 
 quantity will express the distance of the particle at any time from 
 some fixed point in its line of motion. 
 
 In the case of motions arising from natural causes these functions 
 always exist ; it would, however, be possible by artificial means to 
 cause motions which should follow no law whatever, or be perfectly 
 irregular ; in these cases we should still have v equal to the limit of 
 
 7^ , but since in this case v, and therefore the limit of -7- which is 
 
 ct i>t 
 
 equal to it, would vary from one instant to another arbitrarily, it 
 
 would be impossible that it should be represented by any function, 
 
 and consequently could not be the differential coefficient of any 
 
 function. 
 
 Motions of this irregular description are, however, never the 
 subject of mathematical investigation, we may therefore, in all cases 
 that will come under our consideration, adopt the equation ^--jft 
 
 considering — to be, as the notation indicates, the differential coeffi- 
 cient of s with respect to /. 
 
 It must be carefully borne in mind that, though in all these 
 investigations we have spoken of s, v, and /, as space, velocity, and 
 time, we only mean the numerical' representations of these quantities 
 expressed on the principles before laid down, and such is always to 
 be understood whenever such language is used, unless the contrary 
 be expressly stated. 
 
 8. We will now proceed to describe another kind of motion. 
 We have already considered the case of uniform rectilinear motion, 
 and have seen that the characteristic of this kind of motion is, that 
 at every instant the velocity remains the same ; and from the consi- 
 
8 A TREATISE ON DYNAMICS. [cHAP 
 
 deration of this kind of motion, we have obtained our measures 
 and numerical representations of velocity. We have also obtained 
 an expression for the velocity in the case where it changes from one 
 instant to another, but we have not at all considered the case of that 
 change taking place according to any law. 
 
 Now, conceive a body moving in such a manner that the differ- 
 ence of its velocities at the beginning and end of any interval is 
 equal to the difference of its velocities at the beginning and end of 
 any other equal interval, whatever the duration of the intervals, or 
 at whatever parts of the motion they may be taken. Such motion is 
 called uniformly accelerated motion. 
 
 Suppose, for instance, that the velocity at any instant is ?>„, that 
 after a time t it is ^i, after another time t it is v^y and so on. 
 
 Then v^, fj, v,. . .are the velocities at instants separated by equal 
 intervals t. 
 
 Hence then, by the definition of this kind of motion, 
 
 V-^ — Vq = V2—Vi = V3 — Vs, &c., 
 
 if the velocity be increasing, or, 
 
 z;„ — ^1 = ^1-^2 = ^2 — ^3j &c., 
 if it be diminishing. We may, however, consider the second case 
 as included in the first by the ordinary conventions of negative 
 quantities. 
 
 If we add n of these together, we have 
 
 and v„, % are the velocities at instants separated by an interval nt. 
 
 nt nt t 
 
 and this is true whatever the magnitudes of n and /. We see, then, 
 that in this kind of motion, the ratio of the increments or decrements 
 of the velocity in any intervals of time, is equal to the ratio of 
 those times. 
 
 Or, if we consider the numerical representations of the incre- 
 ments of the velocity and of the times in which these increments 
 take place, the ratio of the increment of the velocity to the time in 
 which it takes place is independent of the time. 
 
 Let then v be the velocity at a time t from some fixed epoch. 
 And let i; + St) be the velocity at a time t + ll from the same epoch, 
 
 then we have ^- constant for all values of It, large or small. This 
 
 o t 
 
 is the characteristic property of this kind of motion. Since this ratio 
 
I.] A TREATISE ON DYNAMICS. 9 
 
 is constant for all values of ^Mt will be the same when we pass to 
 the limit, and suppose it indefinitely diminished, in Avhich case the 
 
 ratio — becomes -j-, the differential coefficient of v with respect 
 
 to /. This differential coefficient is, however, in this kind of 
 motion, constant. Now conceive two bodies moving each with 
 uniformly accelerated motion and so that the increase of the velocity 
 of one of them in any time is equal to the increase of the velocity of 
 
 the other in the same time, and consequently so that the ratio ^^ 
 
 6 t 
 
 and its limit -7- is the same for both, then the motions of these 
 at 
 
 two bodies are said to be equally accelerated, or the accelerations of 
 
 the motions to be equal. Of course it does not follow from this that 
 
 the velocities are equal at the same time, any more than that two 
 
 bodies moving with equal velocities are equidistant from the same 
 
 fixed point or from the fixed points from which their positions are 
 
 estimated. But whatever difference there is between the velocities 
 
 at any one time, there will always be the same difference at any 
 
 other time, because the increase of velocity in the interval is the same 
 
 for each body. This is the idea we must bear in mind when we 
 
 say that the motions of two bodies are equally accelerated. 
 
 We will now proceed to find a measure for the acceleration of 
 any motion : and first we will explain what is meant when the 
 acceleration of the motion of one body is said to be twice as great 
 as the acceleration of the motion of another. 
 
 Here the manner of estimating velocity will supply us with an 
 analogy. 
 
 The velocity of one body is twice that of another when the one 
 body passes over in any given time twice the space which the other 
 passes over in the same time. 
 
 In a similar manner the acceleration of the motion of one body is 
 said to be twice the acceleration of the motion of another body when 
 the increase of the velocity of the one body in any time is twice the 
 increase of the velocity of the other in the same time. 
 
 Thus at any given instant let the velocity of one body be ii^ and 
 of another Vq, and after a time / let the velocity of the one be v^ and 
 of the other be v/, then the increments of the velocities of the two 
 bodies in the time t are respectively Vy — Vo and v,' — 1;„'. If u,'— «„' 
 be twice v^ — v^ the motion of the second body is twice as much 
 accelerated as that of the first. This explanation of what is meant, 
 when one motion is said to be twice as much accelerated as another. 
 
10 A TREATISE ON DYNAMICS. [cHAP. 
 
 must be considered as a definition. It follows at once from the 
 nature of the motion that if this relation holds for any value of t it 
 will hold for all values of t. 
 
 "Let then o v and 6 v be the increments of velocity in the same 
 time It of two bodies moving with uniformly accelerated motion, if 
 the acceleration of the latter is twice that of the former Iv = ^lv 
 and vice versa. Hence we have the equations 
 
 ^v _ Iv 
 Jt^'^lt' 
 
 - dv dv 
 
 ^''^-dt-^-Tt' 
 
 And the same reasoning is immediately applicable to any multiple. 
 So that if the acceleration of the motion of one body is n times the 
 acceleration of the motion of another, we have 
 
 Iv _ Bu 
 
 , dv dv 
 
 ''''^ dt^''-Tr 
 
 or, since the ratio remains constant, whatever the magnitude of It, 
 we need not have it the same on both sides, so that 
 
 Iv _ Iv 
 
 Jl'^'-zt' 
 
 dv' dv 
 
 li'^^^'Tt' 
 
 It now remains to find a numerical representation for the degree 
 of acceleration of the motion of any body. If the acceleration of the 
 motion of any body be considered to be known when the increment 
 of the velocity in any specified time is known, and some particular 
 degree of acceleration be fixed on, then the magnitude of any other 
 accelei'ation will be determined, when the ratio it bears to that par- 
 ticular degree of acceleration which has been chosen as our standard 
 is determined. Let this particular degree of acceleration be repre- 
 sented by the letter a^ , and let any other acceleration be represented 
 
 by a, and let ^ and t^- be the corresponding ratios of the incre- 
 ^ ' oil dt r » 
 
 ments of the velocity and time; then if we have 
 
 S« CVi 
 
 we have also a = n. a,. 
 
I.] A TREATISE ON DYNAMICS. 11 
 
 From which we have « = -—.«), 
 It, 
 
 Or, suppressing a which amounts to taking our standard acceleration 
 as our unit, we have the numerical representation of the other 
 acceleration 
 
 If then we take as our unit that particular degree of acceleration 
 for which ^= 1, we have the equation 
 _6v _dv 
 
 This unit is always adopted. 
 
 The letter / will in future be used to denote the numerical 
 lepresentation of the acceleration, so that our equation is 
 _ Iv _dv 
 
 9. All we have said respecting uniformly accelerated motion is 
 equally applicable to uniformly retarded motion, if throughout the 
 whole reasoning we use the decrement of the velocity instead of the 
 increment. In this case we have, if/ be the retardation, and Zv the 
 decrement of the velocity in time ht, 
 
 J'= —. as before. 
 
 Or our reasoning will hold if we still take Sv to represent the 
 increment of the velocity in time ol, and consider it negative when 
 the velocity is diminishing or the motion is retarded : that is, essen- 
 tially negative, not, having a negative sign prefixed. This is merely 
 the ordinary algebraical generalization. 
 
 In this case our equation 
 
 6v _dv 
 
 gives for f a negative value when the motion is retarded, agreeably 
 to the opposition expressed by the signs + and — . 
 
12 A TREATISE ON DYNAMICS. [cHAP. 
 
 If then in the result of any investigation the expression for the 
 acceleration should be negative, we must conclude from that cir- 
 cumstance that the motion is retarded, and the magnitude of the 
 expression for the acceleration, independently of its sign, will give 
 the magnitude of the retardation. 
 
 We have dwelt at some length on this particular kind of motion, 
 because, as will be seen afterwards, it is of great importance. 
 
 10. In considering the motion of a body moving with variable 
 velocity, we saw at once that at every instant the body was moving 
 with some definite velocity, and it only remained to express that 
 velocity in terms of the space described and the time of describing 
 it : which was easily done . 
 
 It is not, however, so easy to see that when a body moves in any 
 manner whatever (excepting that sort of motion which we have 
 termed irregular) there is, at every instant, some definite degree of 
 acceleration of the motion ; that is, to conceive some uniformly acce- 
 lerated motion in which the velocity is being increased at the same 
 rate as in the proposed motion at the instant under consideration. 
 
 That this is the case will nevertheless be seen by a little careful 
 consideration of the nature of acceleration. It may perhaps be ren- 
 dered clearer by the following analogy. 
 
 Velocity is the rate at which the space described by the body 
 increases ; the acceleration is the rate at Avhich the velocity acquired 
 by the body increases. When the space described increases uniformly, 
 the motion is said to be uniform; when the velocity increases uni- 
 formly, the motion is said to be uniformly accelerated. Carrying 
 the analogy one step farther, when the motion is variable, the velo- 
 city at any instant is the rate at which the space described is in- 
 creasing at that instant ; when the motion is not uniformly accele- 
 rated, the acceleration at any instant is the rate at which the velocity 
 is increasing at that instant. 
 
 This must not be considered as a proof, since, in fact, there is 
 nothing to be proved, but merely as an explanation tending to facili- 
 tate the formation of the idea. 
 
 Let then jT be the acceleration at some instant at which the velo- 
 city is V, and after an interval o^, letj'+ If be the acceleration, and 
 V + hv the velocity. 
 
 Then j- will lie between / andf+ If. 
 
 % 
 
I-] A TREATISIiJ ON DYNAMICS. 13 
 
 But when it is indefinitely diminished, Sy is also indefinitely 
 diminished, and ultimately vanishes, and we have therefore, 
 
 ,. . ^ Su dv „ 
 
 limit of —=-—=:/. 
 
 ht (It ^ 
 When the motion is uniformly accelerated, it is indifferent whe- 
 ther we take ^ , or the limit of that quantity -j- , since the quan- 
 tity being constant is equal to its limit. When, however, the accele- 
 ration is not uniform, the ratio i^- is no longer independent of the 
 magnitude of It, and we must take as our numerical representation 
 
 he acceleration -7- , the lim 
 at 
 
 Hence we have generally, 
 
 of the acceleration -7- , the limit of the ratio -^-- 
 at ot 
 
 -^ ~Tt' 
 Also, in uniformly accelerated motion, 
 
 •^ ot 
 11. We have then in uniform motion, 
 
 also we have, whether the motion be uniform or not, 
 
 ds \ 
 
 ' = Tt' 
 
 and whether the motion be uniformly accelerated or not, 
 
 -^ ~Tt- 
 From this last equation we obtain at once, 
 
 d^ 
 •^ df 
 
 When the motion is uniformly accelerated, f, and therefore -p and 
 
 d^s 
 
 -7-5 will be constant. When the motion is not uniformly accelerated, 
 
 f will vary from one instant to another, and will therefore be a 
 function of /, the time which has elapsed since some fixed epoch. 
 
 It does not always happen that -j- and -j-, are expressed explicitly 
 
 as functions of ^ ; but they must be either functions of I, or of some 
 quantity which is itself a function of t. 
 
 
14 A TKEATISK ON DYNAMICS. [cHAP. 
 
 When we know the expressions for these quantities, and are 
 able to integrate them, we can find the values of the velocity and 
 of the space described at every instant throughout the whole dura- 
 tion of the motion. 
 
 12. Hitherto we have only considered rectilinear motion ; we will 
 now proceed to discuss the method of representing analytically motion 
 which is not rectilinear. When the term Velocity was first used, 
 no definition was given of it, and it will appear from a little con- 
 sideration, that the idea employed is equally applicable whether the 
 motion is in a straight line or a curved one. We can conceive 
 a point moving along a curved line Avith different degrees of quick- 
 ness, and our idea of its pace or velocity is as definite as if its path 
 were a straight line. And if s is its distance at time t from a fixed 
 
 ds 
 point in its path, measured along that path, -j- is its velocity at that 
 
 d's 
 time, and j-^ is the measure of the acceleration of its motion. In this 
 
 case, however, there is something besides the velocity required to 
 complete our knowledge of the state of motion of the body : we must 
 know the direction of its motion at every instant. Now to determine 
 the position in space of any point we use three co-ordinates, that is, 
 the distances from some fixed point of its projections on three 
 fixed lines passing through 0. Call the three lines Ox, Oij, Oz, and 
 let L, M, N be the projections of the point P on them made by planes 
 parallel respectively to yOz, zOx, xOy. Then when OL, OM, ON 
 are known, the position of P is completely determined ; and when the 
 velocities of L, M, iV along Ox, Oy, Os, that is, the rates of increase 
 of Oh, OM, ON are known, the velocity and direction of P's motion 
 can be found from the geometry. 
 
 In the simple case where Ox, Oy, Oz are mutually at right 
 angles to each other this is easily expressed. 
 
 Calling the coordinates of P, x, y, z, the velocities of L, M, and 
 N will be 
 
 dx dy J dz 
 
 Tt' Tt ^^"^Tf 
 
 and if v be the velocity of P, a, /3, 7 the angles which its direction 
 makes with Ox, Oy, Os, 
 
 ds /7d^' AW 7^ 
 
 \ dx ^1 dy 1 dz 
 
 -cos a = -.-77, cos/i = -. jTT-, cos 7 =-.-7-; 
 V dt V dl ' V di 
 
l.J A TUEATISE ON DYNAMICS. 15 
 
 -J , -^ , and -J- , are called the resolved parts of the velocity of P 
 
 in the directions Ox, Oij, Oz. 
 
 dv 
 When Ox, Oj/, Oz are not at right angles to each other, -^ ^ 
 
 ~L, -j^ are called the components in those directions. Hence it 
 
 appears that the component of a velocity in any direction depends on 
 the directions in which the other components are taken ; when, how- 
 ever, the resolved part in any direction is spoken of, the other com- 
 ponents are understood to be at right angles to it. 
 
 13. The propriety of the term components will be better seen 
 from the following proposition called the parallelogram of velocities. 
 This proposition may be stated as follows : 
 
 If a point be moving in any direction with any velocity, and 
 if to this motion another motion be superadded in any direction, then 
 if the two simple velocities be represented in magnitude and direction 
 by lines drawn from any point, the actual velocity will be represented 
 in magnitude and direction by the diagonal of the parallelogram 
 described on these two lines. 
 
 What is meant by superadding a motion will be best understood 
 by an illustration. Suppose a point to be moving uniformly across 
 a table in a straight line. This will be the first motion. Now while 
 this motion relatively to the table continues, suppose the table itself 
 to be moved uniformly in some other direction, this will be the second 
 motion superimposed on the particle : neither the one nor the other 
 will be the motion of the particle relatively to the floor of the room. 
 
 It must not be supposed that we here assert that if a ball were 
 rolling or sliding across a table, and the table were to be pushed 
 forward, the motion of the ball relatively to the table would be 
 unaffected ; whether this would or would not be the case, is a subject 
 for after-investigation : all we suppose is, that a point, a merely 
 geometrical point if you please, is constrained artificially to advance 
 uniformly in a straight line relatively to the table. 
 
 Let AB be a line chosen 
 arbitrarily to represent in 
 magnitude and direction the 
 first velocity of the point, and 
 let / be the time in which the 
 particle would describe JB 
 with this velocity. 
 
16 A TREATISE ON DYNAMICS. [cHAP. 
 
 Now, in order to impress on it the second velocity, suppose it 
 inclosed in a tube which originally coincides with AB. Then from 
 the first motion the point would move uniformly from the end A of 
 the tube to the end B in the time t, and any velocity in any direction 
 would be superimposed on the former velocity by moving the tube 
 parallel to itself in that direction and with that velocity, the other 
 motion relatively to the tube being supposed to continue unaffected 
 by the motion of the tube. 
 
 Let the velocity of the tube be such as would carry it uniformly 
 from the position AB to the position CD in the time t. Then A C 
 will represent in magnitude and direction the second velocity super- 
 imposed on the former: it is to be shewn that the diagonal AD will 
 represent the actual velocity of the particle resulting from these two. 
 At the end of the time t, the point will be at D : at the end of any 
 shorter time t^, let a 6 be the position of the tube: then, since its 
 motion is uniform, we have 
 
 t^ : t = Aa : AC 
 
 ^aP : CD by similar triangles, 
 = aP : ab. 
 therefore, since the motion of the point in the tube is uniform, P is 
 the position of the point, that is, the point at every instant is in the 
 diagonal and therefore moves along it. Also 
 AP : AD = Aa : AC, 
 -^t, : t, 
 
 which shews that the point moves uniformly along the diagonal in 
 the time t. Therefore AD represents the resultant velocity in mag- 
 nitude and direction. Which was to be shewn. 
 
 From this it follows that if a particle be moving in any direction, 
 we may suppose the velocity to be the resultant of two velocities in 
 any two directions in the same plane with the actual velocity, or, if 
 we extend the parallelogram of velocities to a parallelepiped, of three 
 velocities in any three directions. 
 
 Since the sum of the squares of three adjacent sides of a right 
 solid is the square of the diagonal, if w^, Vy^ v^ represent three 
 velocities in directions at right angles to each other coexisting in a 
 body, V the actual velocity, 
 
 v^ = v^ + v/ + v^, 
 and if a, /3, 7 be the angles between the direction of v and those of 
 v^, Vy, and v^, 
 
 v^ = V cos a, Vy = V cos /3, v^ = V cos 7. 
 
I.] A TREATISE ON DYNAMICS. 17 
 
 It must not be supposed that the parallelogram of velocities and 
 what follows are in reality different from the method in Art. 12. It 
 has, howevei*, afforded an opportunity for explaining the sense in 
 which we shall afterwards speak of adding one velocity to another, 
 and of any number of velocities coexisting. 
 
 14. If any number of velocities be superadded at the same time 
 to a body (in the sense which we have just explained) the re- 
 sultant velocity may be easily found. 
 
 We may take the resultant of any two, and by combining this 
 resultant with another, obtain the resultant of three, and so on to 
 any number. 
 
 Or we may proceed as follows : 
 
 Fixing arbitrarily on three directions, we may resolve each 
 velocity into its components in these three directions, and add 
 together the components in each of the three directions. We shall 
 then have the resultant velocity expressed in terms of three compo- 
 nents, and can find its magnitude and direction at once by combining 
 these three. 
 
 15. Having explained certain terms which will constantly 
 occur, and described certain kinds of motion which will continu- 
 ally come under our notice, we will now proceed to investigate 
 the causes which would produce those motions, and to establish 
 rules for determining the nature of the motions which would result 
 from the action of specified causes. 
 
 We have hitherto used the terms point, particle, body, merely to 
 denote a position in space. A geometrical point supposed capa- 
 ble of motion would have answered our purpose equally well. We 
 will now, however, confine our attention to such bodies or points as 
 we have described in Art. 1. And this is to be understood what- 
 ever term is used to express it. 
 
 Force is defined to be " any cause which produces, or tends to 
 produce, any change in a body's state of rest or motion." 
 
 In the science of Statics, however, we are only concerned with 
 forces which tend to produce a change in a body's state of rest. In 
 the present subject the whole of the definition is required. 
 
 The first inquiry that suggests itself is. What will become of 
 a body if left to itself, that is, if not influenced by any bodies 
 external to itself? 
 
 Suppose a body in motion ; we are unable to say, d priori, 
 whether if left to itself the motion will gradually die away and the 
 body ultimately stop ; whether it will move in a straight line or be 
 
18 A TREATISE ON DYNAMICS. [cHAP. 
 
 deflected from it in any direction ; whether or not it will have a 
 tendency to move in a circle; in fact, we cannot say any thing 
 about it. It is found, however, that it will move in obedience to the 
 following law, which is called the First Law of Motion. 
 
 A body in motion not acted on by any external force will move 
 in a straight line with uniform velocity. 
 
 This law assures us of two facts. 
 
 First, that matter has no property inherent in itself which 
 enables it to change the direction of its motion, or to alter or 
 destroy its velocity ; and 
 
 Secondly, that the molecular forces which keep together the 
 ultimate atoms of which our particle is composed have no such 
 tendency. 
 
 It follows from the definition of force, that if the body be not 
 acted on by any force, no change can take place in its motion, and 
 therefore it must move on uniformly in a straight line. For any 
 change must have some cause, and by the definition, the name 
 " force " is given to that cause, whatever it be. 
 
 The First Law of Motion, then, assures us that when there is no 
 external force acting on the body, there is no force acting at all 
 which can avail to change the motion. 
 
 We will, at present, say nothing about the proof of this law. 
 The true nature of the proof, and the true bearing of the experi- 
 ments which suggested the law, will be better appreciated when 
 farther progress has been made in the subject. 
 
 16. Before proceeding farthei", we will make a remark which 
 must never be lost sight of. It is this. Force, by whatever means 
 exerted, or from whatever cause arising, is always necessarily essen- 
 tially of the same nature. 
 
 Forces may differ from one another in their intensity, and in 
 their directions, and in the points at which they are exerted, but 
 they are always forces, and as such are always magnitudes of the 
 same kind. 
 
 Thus, a force may be exerted by means of a string, in which 
 case it is called tension. It may be exerted by pushing one body 
 against another, in which case it is called pressure or reaction. We 
 may have the force of friction, pressure exerted by a spring, by a 
 body's weight which arises from the attraction of the earth, by any 
 other attraction or repulsion whatever, but still all are the same. 
 
 Forces may produce equilibrium, or they may produce motion, 
 but still the force itself is the same. 
 
I.] A TREATISE ON DYNAMICS. 19 
 
 When, therefore, we use tlie term " force," we always mean such 
 a force as a pressure or tension. 
 
 Two forces are equal to one another when a point on which they 
 act in opposite directions continues at rest under their action. 
 
 Two equal forces acting on the same point in the same direction, 
 constitute together a foi'ce double of either of them. 
 
 From these two definitions we are able to represent a force 
 numerically, by referring it to some standard force as a unit. 
 
 17. We will now consider the effect of a force when acting on a 
 material point. 
 
 Suppose the point at rest originally ; when the force acts it will 
 generate a velocity in the particle, and if the force acts for a certain 
 time and then ceases, we know from the first law of motion that the 
 particle will continue to move in a straight line with the velocity 
 which it had when the force "ceased acting. 
 
 Now suppose a force exactly equal to this one to act for exactly 
 the same time on another particle originally at rest, exactly similar 
 and equal to the other one ; by the end of the time this particle will 
 liave acquired, the same velocity as the other, and will continue to 
 move on with this same velocity when the force ceases acting. 
 
 Or, in other words, when a given force acts on a given particle, 
 originally at rest, for a given time, there is always some definite 
 velocity which it will generate in the time. 
 
 Now suppose that a force acts for a certain time on a particle and 
 produces a certain velocity, if it goes on acting for another equal 
 time in the same direction, it will increase the velocity, but we 
 cannot, a priori, say by how much. Here then we are stopped again. 
 
 Also, suppose that together with our force another equal force 
 acts on the body for the time specified, in the same direction with 
 it, thus amounting to a double force, we cannot say, (i priori, what 
 proportion the velocity generated in any given time, by these two 
 forces, will bear to that which would have been generated in the 
 same time by one only. 
 
 To meet these two difficulties we have another rule to guide us, 
 called The Second Law of Motion, which may be thus stated. 
 
 When any number of forces act upon a particle in motion, the 
 effect of each force on the velocity of the particle is the same in 
 magnitude and direction as if it acted singly on the particle at rest. 
 
 The best commentary on this law will be the manner in which 
 it is applied. When a force is designated by a letter (as P) that 
 letter must be considered as representing numerically the intensity 
 
20 A TREATISE ON DYNAMICS. [cHAP. 
 
 of the force, estimated by reference to some standard unit. All 
 forces whose intensities are equal and which act in the same direction 
 will be considered as the same force, from whatever different causes 
 they may arise. For instance, a body pulled by a string, and an- 
 other attracted by a magnet in the same direction and with the 
 same intensity, would be considered as acted on by the same force. 
 Forces of different intensities, even though they arise from the same 
 cause (as from the attraction of the same body at different distances), 
 are considered different. 
 
 18. Suppose then a force P to act on a particle for a time t in 
 which it generates a velocity v; then if it acts during another 
 interval t it will, by our law, produce the same effect as during the 
 first interval, and therefore during this second interval t it will 
 generate an additional velocity v, so that after a time 9,1 the particle 
 will be moving with a velocity 'Zv, and generally after a time nt \t 
 will be moving with a velocity 7iv, which may be expressed in 
 words by saying that when a constant force acts upon a particle, the 
 velocities generated from rest in different times are to one another in 
 the same ratio as the times in which they are generated. 
 
 From the manner in which the velocity of the particle increases, 
 we see that its motion will be of that kind which we have called 
 uniformly-accelerated motion. 
 
 Hence then we have the conclusion, that a constant force acting 
 on a particle will produce uniformly-accelerated motion. And this 
 result will of course be true for every constant force, and for every 
 pai'ticle. We will however at present confine our attention to the 
 same particle or to particles which are alike in every respect. 
 
 19. Now suppose two forces each, P, to act together in the same 
 direction on the same particle for the time t. Each would in this 
 time, if it acted separately, generate from rest the velocity v. But 
 by our law the effect of each force will be produced as if the other 
 did not act. Each therefore will generate its velocity v; so that 
 the whole velocity generated in the time t will be 9.v: and these two 
 forces P constitute a force 2 P. Hence then a force 2 P generates 
 in any time twice the velocity which a force P would generate : and 
 by similar reasoning it appears that a force nP generates n times 
 the velocity which a force P would generate in the same time. And 
 from what has preceded we know that the motion of the particle 
 under the action of this force n P will be uniformly accelerated : and 
 the increment of the velocity in any time will be n times the in- 
 
I.] A TREATISE ON DYNAMICS. 21 
 
 crement in the same time under the action of the force P: or, in 
 other words, the acceleration of the motion under the action of the 
 force M P is h times the acceleration under the action of the force P. 
 Hence then, if P and P' be any two forces, andy and/' the acce- 
 lerations of the motions which they produce in the same particle, 
 we shall have 
 
 Here then we have come to the following conclusion. When a 
 constant force acts on a particle it produces uniformly-accelerated 
 motion during its action. And the accelerations of the motions 
 which different forces produce in the same or equal particles are to 
 each other in the same ratio as the forces which produce them. 
 
 20. We have hitherto considered the action of forces on particles 
 exactly similar and equal in all respects, and, consequently, with 
 exactly the same properties. It remains to consider the action of 
 forces on different particles, and to do this we must first endeavour 
 to convey an idea of what is meant by the term " mass." 
 
 The definition generally given is that the " mass " of a body is 
 the quantity of matter in it. Unless, however, it be accurately stated 
 how this quantity of matter is to be estimated, we are still as far off 
 as ever from knowing what is meant by the term "mass." 
 
 We will take the above definition, and to render it definite will 
 join it with the following. 
 
 The masses of two particles are said to be equal when the 
 accelerations of the motions generated in them by the action of 
 equal forces are equal. This may or may not be the same thing as 
 saying that their volumes are equal or that their weights are equal. 
 That must be determined by after considerations. We here give 
 the definition that will be of most service to us, being perfectly at 
 liberty to give whatever arbitrary definitions we please, on the sole 
 condition of adhering to them throughout. 
 
 If we join together two particles whose masses are equal, we 
 shall have a particle whose mass is double that of either of the 
 constituent particles. This is our definition of a double mass, and 
 so on for any multiple. And exactly as was the case with respect to 
 space and time we shall have the numerical representation M of 
 any mass, that number which expresses the ratio which its mass 
 bears to that particular mass which we have chosen as our unit. 
 
 21. Now, suppose a force P acting on a mass M to produce a 
 motion whose acceleration is J\ and suppose n such particles to be 
 arranged side by side close together, and each to be acted on by a 
 
22 A TREATISE ON DYNAMICS. [cHAP. 
 
 force P in the same direction. Then it follows from our definition 
 of equal masses that the acceleration of the motion of each will be^^ 
 and therefore since they start together they will move on together 
 as one body. 
 
 It will not affect this motion if we suppose all these particles 
 united so as to form one particle, in which case we have a motion 
 Avhose acceleration is / produced by the action of a force 71 P on a 
 mass nM. 
 
 Now a motion whose acceleration is / is produced by the action 
 of a force P on a mass M, and therefore from what has been proved 
 before, a motion whose acceleration is 7if would be produced by the 
 action of a force n P on a mass M. 
 
 And this is true whatever be the magnitude of n. 
 
 Hence the accelerations of the motions produced in different 
 particles by the action of the same force nP are inversely propor- 
 tional to the masses of those particles. 
 
 Or, generally, if_/andy' be the accelerations of the motions 
 produced in masses M and M' by forces P and P', and/j the accele- 
 ration produced in the mass 31' by the force P, we have 
 
 And it was shewn in Art. 19 that 
 
 f P" 
 
 f P M' 
 whence it follows that "iy = irj • "p7 » 
 
 P P' 
 
 22. It has been shewn in the last few articles that when a con- 
 stant force P acts on a particle whose mass is M, it produces uni- 
 formly-accelerated motion, and that the amount of the acceleration 
 
 P 
 varies as the fx-action .^y. If then two forces P and P' act on two 
 
 P P' 
 
 particles whose masses M and M'are such that -=r>= ^s-r, , the motions 
 
 M M 
 
 of these two particles will be equally accelerated, or the power 
 
 which the force P has of accelerating the motion of M is equal to 
 
 the power which the force P' has of accelerating the motion of M'. 
 
 . P P' 
 
 And if ^ = ?z — , , the power which P has of accelerating the motion 
 
 of M is n times as great as the power which P' has of accelerating 
 the motion of M' This power which a force has of accelerating 
 
I.] A TREATISE ON DYNAMICS. 23 
 
 the motion of a particle is called the accelerating-force of that force 
 on the particle ; and in the first of the two cases above we say that 
 the accelerating-force of P on M is equal to the accelerating-force 
 of P' on M', and in the second the accelerating-force of P on M is 
 71 times the accelerating-force of P' on M'. From this definition it 
 appears that the accelerating-force of any force on any particle is 
 proportional to the acceleration of the motion which that force, acting 
 alone, would produce in the particle, and for convenience the iniit 
 of accelerating-force is so chosen that the same number represents 
 the two. 
 
 It may seem at first sight to have been unnecessary to make this 
 distinction between the accelerating-force of a force and the accele- 
 ration of the motion produced by the force; but a little consideration 
 will shew that the idea of acceleration can be formed without any 
 reference to force and mass, while the accelerating-force on a definite 
 mass is a property of the force which exists even though the effect 
 of the force may be counteracted or modified by other causes. 
 
 The term "accelerating-force" will be constantly used as an 
 abbreviation of the longer expi'ession "^the accelerating-force of a 
 force on a particle ;" it must not however be concluded from this 
 independent use of the expression, that accelerating-force is itself 
 a force of the kind referred to in Art. l6. The term is a bad one, 
 inasmuch as it favours this misconstruction, but will lead to no 
 error if the preceding explanation is borne in mind, and the term 
 considered as one word, equivalent to some such term as accele- 
 rativeness. 
 
 23. It has been shewn that the acceleration /of the motion pro- 
 
 P 
 
 duced in a mass M by a force P is proportional to -p.. To simplify 
 
 our expression, such a relation is assigned between the units offeree 
 and of mass that 
 
 •^ M 
 
 If we consider the unit of mass as the arbitrary quantity in this 
 case, it amounts to defining the unit of force as that force which 
 will produce the unit of acceleration in the unit of mass, or the force 
 whose accelerating-force on the unit of mass is unity. 
 
 Combining the preceding equation with those obtained before, 
 we have 
 
 ds 
 ' = dl' 
 
 ^~ M~ dt~ de' 
 
24 A TREATISE ON DYNAMICS. [cHAP. 
 
 24. We have hitherto confined our attention to the action of a 
 constant force. The force P which we have supposed to act did not 
 vary from one instant to another, and we have shewn from the 
 second law of motion, that the motion produced in a particle by such 
 a force was uniformly accelerated. We will now consider the action 
 of a variable force, that is, a force whose intensity is continually 
 changing. 
 
 Suppose, for the sake of definiteness, that the force is increasing; 
 and at a time t from some fixed epoch let its intensity be P, and at 
 a time t + ct suppose it to be P + 2 P. 
 
 Let M be the mass of the particle on which it is acting, and v the 
 velocity with which it is moving at the time /, v + ^v the velocity 
 with which it is moving at the time t + dt, and w + d v, and v + ^Vg the 
 velocities with which it would have been moving at the time t + ht, 
 had the force remained constant during the time hi, with the re- 
 spective intensities P and P+cP. Then the velocity v + hv will he 
 between v + Zvi and v+hv2, or hv will lie between Bi'i and hvz and 
 
 therefore t— will lie between 1=-^ and ~ . 
 bt Of ct 
 
 Now from our investigations with reference to a constant "force 
 
 we know that 
 
 h^ P 
 
 ht ^ M' 
 
 , aUa P + cP 
 
 and -^ 
 
 It M 
 
 Hence then ^r- always lies between -^ and -=-= + — - . 
 
 ht ^ MM M 
 
 But as dt decreases oP decreases, since the intensity of the force 
 
 is supposed to vary continuously : and in the limit ^— will become 
 
 dv 
 
 ■J- , the two quantities between which its magnitude always lies will 
 
 coincide, and it must therefore be equal to either of them ; we have 
 therefore the equation 
 
 p 
 
 M" 
 
 dv 
 
 P 
 M'- 
 
 d'i 
 
 = 17' 
 
 and, consequently, -Trf = 
 
 This equation is true at every instant during the motion, P re- 
 presenting the magnitude of the force at that instant. If the letter 
 P be considered as standing for such a function of /, or quantities 
 depending on /, as will express the magnitude of the force at every 
 proposed instant, the equations 
 
1.] A TREATISE ON DYNAMICS. 25 
 
 P d^s , ds 
 M rf^' dt 
 
 when solved Avill give the velocity of the body and the space it has 
 moved over, in terms of the time elapsed since a fixed epoch. 
 
 When forces arising from different causes act on a particle in the 
 direction of its motion, P in the preceding equation must be con- 
 sidered to represent the resultant of all such forces ; or the equation 
 might be written 
 
 Pi, P2, Sec. being essentially positive or negative as they tend 
 respectively to increase or diminish s. 
 
 25. Suppose a body whose mass is M to be moving with a 
 velocity v, then the product of the numbers M and v, viz. Mv, is 
 called the momentum of the body. 
 
 The assignment of this name to this particular product may be 
 considered perfectly arbitrary. As, however, the product presents 
 itself in a very extensive class of problems, as will be seen hereafter, 
 it is found convenient to have a name expressing it. If we put the 
 equation 
 
 M J 
 under the form Mf = P, 
 we see that the product of the numerical representatives of the mass 
 and the accelerating-force of the force P on it, is the numerical 
 representative of the force P. The name of moving-force is given 
 to this product. The terms, force, moving-force, and pressure, are 
 however used indiscriminately. 
 
 Since f=--r, and M is constant, 
 ■^ dt 
 
 •KT r -KIT dv d .Mv 
 
 Hence, the moving-force Mf, bears exactly the same relation to 
 the momentum Mv, that the accelerating-force of the force P, viz./, 
 does to the velocity v. 
 
 This, however, is not of much importance. 
 
 26. When a pressure P acts on a body whose mass is M, and 
 generates motion in it, if v be the velocity at time /, 
 
 p_d.Mv 
 dt ' 
 
26 A TREATISE ON DYNAMICS. [cHAP. 
 
 where P may be either constant or variable, and, when the latter is 
 the case, must be either explicitly or implicitly a function of t. 
 Integrating this equation, we have 
 
 Mv=fPdt: 
 
 at the times /j and t.^, let i\ and Vo be the velocities of the body, 
 then 
 
 or the definite integral L ^Pdt expresses the change in the momen- 
 tum of the particle which takes place between the times /„ and ^, 
 from the action of the force P. 
 
 When P is known as a function of t, this integration can be 
 effected, and the change of momentuna deduced from it. 
 
 It sometimes happens that, although P is not known as a func- 
 tion of t, and although the interval t^— ti is not known, the value of 
 the definite integral is known. Or, in other words, we sometimes 
 know the whole change in velocity or momentum which is caused by 
 a certain force, when we do not know the law of the force, or the 
 time during which it acts. When this is the case, although from the 
 velocity of the particle before the action of the force commenced, we 
 can determine the velocity when it ceased to act, or the converse, we 
 cannot determine the position of the body, because we are ignorant 
 of the nature of its motion during the time tz — tv 
 
 In the cases, however, of this kind which come under our notice, 
 the interval <2 - h is extremely short, so that we may neglect without 
 sensible error the change of position of the body which takes place 
 during that interval, or consider it in the same position at the time 
 ^2 as it was at the time ^i. 
 
 The force P, on the contrary, is generally so great as to produce 
 a considerable change in the velocity v, or the momentum Mv. 
 
 In these cases the change of velocity from v to V2 is considered 
 to take place instantaneously : the action of the force is said to be 
 
 impulsive, and the definite integral J 'Pdt is called the "impulse," 
 
 or " blow," perhaps an abbreviation for " effect of the impulse," or 
 " measure of the impulse." 
 
 When we consider the definite integral L 'Pdt, or the change of 
 
 momentum M (v-j-v^), as expressing the magnitude of the impulse, we 
 fix on the particular magnitude of the impulse which we take as our 
 
1.] A TREATISE ON DYNAMICS. 27 
 
 unit, namely, that impulse which if applied to a unit of mass at rest 
 would cause it to move with the unit of velocity. Thus, if we 
 denote the impulse by B, and suppose the body originally at rest, we 
 have 
 
 and R will equal unity when 
 
 iV/=l, and f= 1. 
 
 The term "impulse" must not be confounded with the term 
 '• impulsive- force." 
 
 The impulsive-force is the force P, which is generally very large 
 and not known, whicif acting through the finite but extremely short 
 time fi — /j, produces a finite effect. 
 
 The impulse is the whole action of the impulsive force during 
 the interval t.^ - ti, and is, as we have seen, generally known. 
 
 The impulsive force P is of the same nature as all other forces, 
 and is, of course, comparable with them in magnitude. 
 
 The impulse R is entirely different in its nature from forces, and 
 can only be compared in magnitude with other impulses. 
 
 The magnitude of R depends jointly on P and ^2 — U) and though 
 the latter is very small, yet its value in one case may bear any 
 ratio to its value in another, without violating this condition. 
 
 Since an impulsive-force is not different from any other force, 
 all the results that we shall arrive at for forces generally will be 
 true of impulsive forces, unless there is some particular consideration 
 which excludes them. 
 
 It would be premature at present to describe the nature of the 
 action which takes place between bodies when an impulse is pro- 
 duced, or, as it is said, when there is "impact" or "collision." All 
 this will be fully discussed hereafter. The class of problems to which 
 it leads are particularly beautiful, and have this advantage, that all 
 the differential equations to which they lead are of the first order 
 instead of the second. 
 
 27. From the identity of our ideas of force, whether considered 
 as in equilibrium or producing motion, it follows that when any 
 number of forces arising from different causes act at the same time 
 on a particle in motion, Ave may replace these forces by their re- 
 sultant calculated on the principles of statics, and if we suppose this 
 force to change from instant to instant, so as always to be the 
 resultant of the variable forces which act on the particle, the effect 
 of this single force will be the same as the effects of those forces of 
 Avhich it is the resultant. Or, which is more convenient, Ave may 
 
28 A TREATISE ON DYNAMICS. [c'HAP. 
 
 replace the forces by the three components of that resultant in three 
 constant directions. 
 
 Let u, V, w be the components at time t of the velocity of the 
 particle in the direction of three axes ; X, Y^ Z the sums of the 
 components in directions of the axes of all the forces which act on 
 the particle at time t. 
 
 X+tX, Y+IY, Z + hZ the same quantities at time t + ct. cX, 
 3F, SZ may depend on 2/ explicitly, and also on the change of 
 position and velocity of the particle, but in all cases they will vanish 
 with ht. 
 
 Now we are told by the second law of motion, that each of these 
 forces will produce the same effect on the velocity of the particle 
 during the time 0/ as if the particle were at rest at the commence- 
 ment of ht, and that force were the only one acting. 
 
 Hence the variable force X will produce in that time a velocity 
 
 cu which lies between -^ and ^^ ^jr^-^ — , and the other forces 
 
 will produce effects in their own directions, namely, 
 
 , , ^ YU .(Y + hY)U 
 d V between -^y and ^r? > 
 
 M M 
 
 , . , Zot ^ (Z + lZ)ht 
 and 6 7V between ^rj- and ^r~ — . 
 
 so that the components of the velocity at the time t + ht will be 
 ti + ^u, v + dv, fv + Zw, where 2?<, hv, Ziv are properly the increments 
 of u, V, and w. 
 
 Hence, passing to the limit, we have 
 
 M -r = X, M -7-= F, and M -i- = Z. 
 
 dt dt ' dt 
 
 If X, y, z are the coordinates of the particle at time t, 
 dx dy dz 
 
 '' = Tr'=dt''' = Tt' 
 
 d^r d^7i d^z 
 
 These equations must be considered as the fundamental equations of 
 dynamics where the motion of a particle only is considered. 
 
 28. It may be objected to what has preceded, that we have 
 used terms which have in themselves a meaning in ordinary lan- 
 guage, and that we have assigned to these terms a sense differing 
 
I,] A TREATISE ON DYNAMICS. 29 
 
 from, or only partially agreeing with, their ordinary meaning, and 
 that this sense has been assigned arbitrarily. 
 
 To this we reply that we are perfectly at liberty to give any 
 arbitrary definitions that we please, provided only that we adhere to 
 them throughout the subject. 
 
 The Science of Mechanics, however, is particularly unfortunate 
 in this respect, that the terms used in it have, in addition to the 
 meaning given them by definition, a meaning in common conversa- 
 tion. It arises from the fact, that in the early ages of the science 
 erroneous, very erroneous notions Avere entertained of the principles 
 of the science, and the phraseology adopted expressed those erro- 
 neous notions. When the true principles of the science were 
 gradually developed, it was found convenient to retain the old 
 names expressing the same analytical combinations and numerical 
 quantities as before, though all idea of the name expressing any 
 principle was given up. 
 
 In popular language, however, the old notions still cling to the 
 words. 
 
 Such terms are " momentum," " accelerating-force," " vis viva," 
 &c. 
 
 We caution the student, once for all, to take the words in the 
 sense assigned them by definition and in no other. 
 
 29. It is a matter of every-day experience, that bodies of any 
 material if left unsupported fall to the ground, and that some amount 
 of force is requisite to countei-act this tendency. This is caused by 
 the attraction of the earth on the body. This force, with which the 
 earth pulls the body, is called the weight of that body, and it is 
 found by experiment that the weight of a given volume of any 
 particular substance (as lead) is very nearly the same at all points on 
 the surface of the earth, and for small distances above it. Assuming, 
 for the present, that it is accurately so, a heavy particle when aban- 
 doned to itself in vacuo is acted on only by this constant force, and 
 will consequently, as has been shewn in the preceding articles, move 
 with uniformly-accelerated motion. It must not be imagined that we 
 assert here that we have proved that a particle abandoned to itself m 
 vacuo will move with uniformly-accelerated motion, but we have 
 proved it on the assumption of the two laws of motion and of the 
 fact that the weight of a body at the same place is constant. 
 
 If we take two similar and equal particles, these will have 
 the same weight and the same mass, and consequently the accele- 
 rating forces of their weights will be the same, and if the particles 
 
30 A TREATISE ON DYNAMICS. [CHAP. 
 
 are let loose together they will move on together: and this will not 
 be altered if we suppose them joined, and so for any number. That 
 is, for the same substance the accelerating force of the attraction of 
 the earth is constant. 
 
 This might have been deduced at once from the consideration 
 that both the masses and weights of different portions of the same 
 substance would be proportional to the volume and therefore to each 
 other. 
 
 It is found by experiment that, for bodies of all substances, and 
 not for bodies of the same substance only, the accelerating-force of 
 the earth's attraction is the same, and such as to generate in any body 
 whatever, i?i vacuo, in a second, a velocity with which it would move 
 over 32-2 feet in a second. If then we take a second as the unit of 
 time and a foot as the unit of space, the numerical representation of 
 the accelerating-force of the earth's attraction will be 32-2. This 
 is written g, and is called the accelerating-force of gravity. 
 
 If then W be the weight of a body and M its mass, we have the 
 equation W - M.g 
 
 By the weight we mean the force with which it presses down- 
 wards or which is requisite to support it. 
 
 Since the quantity g is the same for all bodies, we see that the 
 weight and mass of a body are proportional. The quantity g, though 
 very nearly constant, is not accurately so. Its magnitude is different 
 in different latitudes, and at different altitudes above the earth's 
 surface. The variations, however, for positions within our reach are 
 so small that they are generally omitted, and g is considered constant. 
 
 When we are concerned with very great heights on the earth, or 
 with bodies at distances from the earth, we are obliged to take into 
 account the variations in its magnitude. The law of its variation, and 
 the great principle of which it forms a part, will all be fully explained 
 in their places. They have however more to do with the facts than 
 with the principles of dynamics. 
 
 30. The fact that the accelerating-force of the attraction of the 
 earth on any body is the same whatever the weight of the body, has 
 led in the first class of problems that we are concerned with, viz. 
 falling bodies, to the neglect of the weight and mass of the bodies 
 and the consideration only of the accelerating force of that weight, 
 viz. g. And this has extended itself very'much to other problems, 
 so that we constantly meet with the term accelerating-force applied 
 absolutely, without any reference to the force or mass on which 
 it acts. If in all such cases we understand by the term "accelerating- 
 
I.] A TREATISE ON DYNAMICS. 31 
 
 force" such an expression as "a force whose accelerating-force" it can 
 create no ambiguity, and is a very admissible abbreviation. For 
 instance, -sve should find it said, "A body descends under the action 
 
 of a constant accelerating-force g " Instead of "A body 
 
 descends under the action of a force, whose accelerating-force is 
 
 constant and equal g " The term "accelerating-force" is in 
 
 constant use in this sense, and, provided this meaning is always 
 attached to the word, there is no objection to its use. In Dynamics 
 the weight of a body is scarcely ever used, we employ instead M.g, 
 because it very often happens that the factor M may be divided out 
 from both sides of our equations. 
 
 31. The unit of force has been chosen so that the equation 
 F — MJ" may hold. In common affairs the unit of force is chosen 
 arbitrarily, and this unit is generally used in the science of Statics. 
 It is necessary, therefore, to explain how the relation between the 
 two may be found. For this purpose, we must be able to express 
 the weight of the unit of mass in terms of the common standard; in 
 pounds, for instance. 
 
 Let then the unit of mass weigh ?i lbs. and let TV be its weight 
 in terms of the dynamical unit; from the equation P — Mfwe have 
 
 W=Mg = g, 
 and therefore g and n express the same weight referred to different 
 units. Hence, to reduce any dynamical force P to lbs. we must 
 
 multiply it by the factor - . 
 g 
 
 32. We will now proceed to explain the theory of gravitation 
 which was mentioned above, and the nature of the reasoning on 
 which the truth of it, and of the laws of motion, depends. 
 
 When one particle of matter is said to attract another, it is 
 meant that if these particles be placed at a distance from each other 
 and then abandoned to themselves, they will commence moving 
 towards each other, or, that if they be not so abandoned to them- 
 selves, a certain degree of force must be applied to them to prevent 
 their approaching each other. The intensity of this force for 
 different particles at different distances depends on the law of at- 
 traction and its intensity. 
 
 For instance, every substance is attracted to the earth, and we 
 see that if any substance is left to itself it immediately commences 
 moving towards the earth, or if not, a certain degree of force is 
 required to support it. 
 
 The law of gravitation is this. 
 
32 A TREATISE ON DYNAMICS. [cHAP. 
 
 Every particle of matter attracts every other particle of matter 
 with a force which vai-ies directly as the product of the masses of 
 the two particles, and inversely as the square of the distance between 
 them. 
 
 Thus if m and in! be the masses of two particles, and r the 
 distance between them, the force with which they attract each 
 other, or whicli it would be necessary to apply to each of them to 
 
 keep them asunder, will be C . — \ — , where C is some constant 
 
 quantity which is independent of the masses of the particles and of 
 
 the distance between them. 
 
 ^ • , <. ■ , . . . ^ m.m' 
 
 Smce the force actmg on m to move it towards ot is C . — ^— , 
 
 the accelerating-force of this force on m' is C .-^, which is indepen- 
 dent of the mass of the attracted particle. 
 
 That mass is frequently chosen for the unit of mass whose 
 attraction at the unit of distance has the unit of accelerating-force ; 
 in this case C^l, and the attraction between two particles is 
 
 - , m . m' 
 expressed by — 5— , 
 
 The determination of this mass, that is, the expression of it in 
 terms of a given volume of some specified substance, requires most 
 difficult and delicate experiments. It has, however, been effected 
 with great accuracy. An account of the experiments will be given 
 hereafter. 
 
 33. Since, then, every particle of matter in the universe attracts 
 every other particle of matter according to the law just explained, 
 we are able by this law and the equations of motion which we 
 have obtained, to calculate to any degree of accuracy the motions 
 of any one of the heavenly bodies, and to predict the exact direc- 
 tion in which it will be seen from the earth at any proposed 
 future instant, however remote. 
 
 These calculations are very intricate and laborious, and involve 
 many complicated considerations. Astronomical Instruments have 
 also arrived at extreme perfection, so that we are able also to 
 observe at any instant the directions in which these heavenly bodies 
 are seen from the earth. And the more exact our calculations are 
 made, and the more perfect our instruments and methods of 
 observing, the more minute are found to be the agreements be- 
 tween these results of calculation and observation. 
 
I.] A TREATISE ON DYNAMICS. 33 
 
 Nothing can afford a more complete proof of the truth of our 
 assumptions than this. In order, however, that the proof may be 
 fully appreciated, the whole of the processes of calculation and obser- 
 vation should be familiarly known. It is impossible, without some 
 acquaintance with an observatory, to realize the degree of accuracy 
 to which observations can be carried, and it is this accuracy which 
 conveys the most perfect conviction to the mind. 
 
 Perhaps the recent discovery of the planet Neptune may afford 
 a more striki?ig proof of the truth of these laws. Some minute 
 disagreements between the results of calculation and observation had 
 long been noticed in the positions of the planet Uranus ; and it had 
 been suspected that there was some other body in our system, to the 
 neglect of whose action these differences might be due. But it was 
 long deemed past the powers of calculation to discover where a body 
 must be to produce exactly such differences. Till at length the 
 labour was undertaken and completed by Mr. Adams, in England, 
 and shortly after by M. Leverrier, in France ; and their efforts 
 were crowned with success by the consequent discovery of the 
 planet Neptune by Dr. Galle, at Berlin, and, almost, on the same day 
 by Professor Challis, at our own Observatory. 
 
 34. When the term " mass" was first introduced, it was spoken 
 of as the " quantity of matter" of a body. The propriety of this 
 expression appears from the following consideration. 
 
 The mass of a body remains unaltered whatever changes of state 
 the body undergoes, provided nothing is added to or taken from it. 
 
 If a lump of iron be heated so that its volume is increased, its 
 mass remains unaltered. If it were removed to the Moon, where its 
 weight would be diminished to one- sixth, or to Jupiter, where it 
 would be increased to two and a half times its amount, its mass would 
 remain unaltered. 
 
 If a quantity of water be converted into ice or steam, or decom- 
 posed into its component gases, the mass still remains unaltered. We 
 see then that mass, as it has been defined, has two important pro- 
 perties besides that which is taken as the basis of the definition, and 
 which are by no means consequences of the definition. The one, 
 that which has been just described, which entitles it to the name 
 " quantity of matter," and the other, that in the law of gravitation 
 the attraction of two particles varies as their masses jointly. 
 
 35. We will conclude this chapter by explaining a condition 
 which any equation expressing a relation between concrete quanti- 
 
34 A TREATISE ON DYNAMICS. [cHAP. 
 
 ties must satisfy. It must be homogeneous with respect to each of 
 the independent concrete units that enter into it, provided no parti- 
 cular unit has been assumed in obtaining the equation. 
 
 Since every letter represents a number, any combination of letters 
 will also represent a number, and any equation is algebraically correct 
 when the number on one side of it is the same as that on the other. 
 When, however, a letter represents a concrete magnitude expressed 
 numerically, and the unit to which the magnitude is referred 
 changes, the number representing the magnitude must change in 
 the inverse ratio. Now in this subject certain of the units are 
 defined with reference to others, so that three only are independent, 
 and this must be considered in estimating the dimensions of any 
 term of an equation. Ihe independent units are those of duration, 
 length, and mass. If the unit of length be increased ?^-fold the units 
 of velocity and acceleration will also be increased w-fold. If the 
 unit of duration be increased w-fold, the unit of velocity will be 
 diminished to one m* of its magnitude, and the unit of acceleration 
 to one («^)'^. And similarly the other units will vary. This is what 
 is meant, when velocity is said to be of one dimension in space and 
 minus one dimension in time, and when accelerating-force is said to 
 be of one dimension in space and minus two dimensions in time : 
 when letters referring to these quantities occur in an equation they 
 must be estimated in this manner; and when so estimated the 
 dimensions of every term of the equation in each of the independent 
 units must be the same. If this were not so, by changing one of 
 the units for which it did not hold, we should change the several 
 terms of the equation in different ratios, and the equality would be 
 destroyed. But the relation expressed by the equation is true in- 
 dependently of any units. 
 
 Let us examine, for example, the equation 
 
 Mk'^ = -Wh sine. 
 
 M is a mass, and W which is a force is of one dimension in mass, 
 so that the condition is satisfied with reference to the unit of mass. 
 Again, A; is a line and it enters to the second power, W is of one 
 dimension in space, and h is also a line thus making two dimensions, 
 and the condition is satisfied with reference to the unit of length. 
 Again, dt enters to the second power in the denominator, and 
 W which is a force is of minus two dimensions in time, and the 
 condition is satisfied in this case also : sin d is a ratio and of no 
 dimensions. This equation also furnishes an exception : on the left 
 
^•] 
 
 A TREATISE ON DYNAMICS. 
 
 35 
 
 hand side there is in the numerator d^d, or the angle enters to the 
 first power, on the right hand side it does not enter at all: and 
 what is the cause of this? The equation is only true when the 
 angle subtended by an arc equal to the radius is used as the angular 
 unit. Any equation may be deficient in this respect, if it be re- 
 stricted to one particular unit. 
 
 Library, )) 
 
 Of 
 
 Oajlft.ri)^?' 
 
 3— a 
 
36 A TREATISE ON DYNAMICS. [CHAP. 
 
 CHAPTER 11. 
 
 36. Having found in the last chapter the equations of motion of 
 a particle, the object of the present one is to explain the manner of 
 proceeding so as to determine from them the nature of the motion 
 which will take place. 
 
 The simplest case is when the motion is in one line and all the 
 forces act in that line. 
 
 Let M be the mass of the particle, x its distance at the time t 
 from some fixed point in its line of motion, v its velocity, P the 
 resultant of all the forces which act on it : then the equations of 
 motion are 
 
 ^■^-^'' 
 
 dx 
 
 Since, however, the mass of the particle is constant, we will divide 
 
 p 
 both sides of the first equation by iVf, and write y instead of -^. 
 
 f is the accelerating-force of P on M. We have then 
 
 dt' "-'' 
 dx 
 '' = dt- 
 Now the motion of the particle will be completely determined 
 when we are able to assign at every instant the position of the body, 
 and the velocity with which it is moving ; that is, when v and x 
 are expressed as functions of t and known quantities. When this is 
 done the velocity in any position may be found by eliminating t 
 between the two equations giving v and x. 
 
 37. As a particular case suppose the body to be acted on by a 
 constant force: in this case /is constant, and we have 
 
 W-r: 0) 
 
 •■-4r/'+C' (^> 
 
 I and x = ifl'+CH-C' (S) 
 
II.] A TREATISE ON DYNAMICS. 37 
 
 We have here obtained the expressions for v and x in terms of t, 
 but these expressions contain unknown constant quantities C and C, 
 which have been introduced by integration : to determine these it is 
 necessary to know the circumstances of the motion at some specified 
 time. Suppose, for instance, it is given that at a time /j the body is 
 at a distance x^ from the origin, and moving with a velocity i\ ; 
 making these substitutions in the above equation, we have 
 v,=/.t,+ C 
 
 from which to determine C ancf C. When these are determined 
 and substituted in equations (2) and (3) the values of u and x will be 
 completely expressed in terms of t and known quantities. 
 
 The constants C and C might be equally well determined from 
 the position at one time and the velocity at another ; or from the 
 positions at two different times ; or from other conditions under 
 different forms. Variations of this sort constitute the difference 
 between one problem and another. 
 
 Eliminating t between the equations (2) and (3) we have an 
 equation between v and x. This might also be found as follows : 
 
 de ~^ ' 
 
 dx d'x _ c p dx 
 
 ''' ^Tt dt^^^-^'Tt' 
 
 d-fy-/- 
 
 c 
 
 or v^ = 2f.x + C"; (4) 
 
 and C" must be determined from conditions analogous to those 
 already alluded to. Such as that the velocity is y, when x = x^, 
 from which vi' = 2fxi + C" 
 
 and.-. v^= «,'+ 2/. (x-x,). 
 When a body moves in a vertical line acted on only by the 
 attraction of the earth, within moderate distances, it may, without 
 sensible error, be considered as acted on by a constant force. In 
 this case, if x be measured upwards, and the accelerating force of 
 the earth's attraction be written as usual ^, we shall have J'- — g 
 since the force acts in the negative direction, or tends to diminish x. 
 The preceding equations become 
 
 v = -gt + C, (2) 
 
 x = -lgt'+Ct + C', (3) 
 
 and v' = -2gx+C" (4). 
 
38 A TREATISE ON DYNAMICS. [cHAP. 
 
 Suppose now that the body is projected upwards from the 
 origin with the velocity V, then, if t be measured from the time of 
 projection, we have v=V when t = and x = 0, and therefore our 
 equations give 
 
 o = c\ 
 
 and therefore v = V — gt (5) 
 
 ^=Ft-^ge (6) 
 
 v'=V'--2^x (7). 
 
 From equation (5) we see that as t increases v diminishes, that 
 J/ 
 when t = —, V is zero, and that afterwards v becomes negative and 
 
 increases in actual magnitude ; also from equation (6) we see that 
 X commencing at zero increases till t = — when it equals — , that 
 
 2 V 
 
 it then diminishes, becomes zero when t = - — , and after this 
 
 g 
 becomes negative and continues to increase in actual magnitude. 
 From this it follows that the body will move upwards at first with 
 
 V- 
 a continually decreasing velocity till it attains a height , when 
 
 ''to 
 
 it comes to rest and immediately commences moving down- 
 wards with an increasing velocity; that the time of attaining its 
 
 V . 
 
 greatest height is — , and the time of returning to the point from 
 
 which it started is twice this. Equation (7) shews that the velocity 
 at each point in its descending course is the same as at the corres- 
 ponding point in its ascending course. It is unnecessary to dwell 
 longer on this case ; the reader will be able to frame for himself 
 endless variations of it. 
 
 38. If the force be not constant, f will have different values 
 at different times, and consequently will be a function of the time. 
 
 Suppose f expressed explicitly as a function of t, in this case the 
 proceeding is as follows : 
 
 (Px _ r 
 
 He' J' 
 
 x=fJfdi' + Ct + C', 
 and the determination of the constants is the same as in the preced- 
 ing case. 
 
II.] A TREATISE ON DYNAMICS. 39 
 
 30. If/ does not depend directly on t it must depend on the 
 position oi- velocity of the body, or on some circumstances external 
 to the body, or on some combination of them. The first of these, 
 where / depends on the position of the body, is the only case to 
 which any general principles of solution are applicable : in the 
 others, except in some simple cases, the equations can only be solved 
 approximately, though it must be borne in mind that they are 
 themselves strictly accurate. 
 
 When the force depends only on the position of the particle, 
 it can only vary with x, and therefore y will be a function of x; 
 let this bey(.i*); so that the equation of motion is 
 cFx „ 
 
 ^ dx drx ^ rf ^ dx 
 
 and integrating this, we have 
 
 This equation gives the velocity of the particle in any position. 
 
 To determine C we must know the velocity is some particular 
 position, or have some equivalent condition. 
 
 Suppose the integration on the right hand side of the equation 
 
 effected, as it generally can be ; v^ is then given as a function of 
 
 X and constant quantities ; 
 
 ^dxV . 
 
 Fix); 
 
 Q 
 
 and to determine the position at any time, we have 
 di__^ 1 
 
 where the upper or lower sign must be used according as x is in- 
 creasing or diminishing with t. 
 
 Integrating this we get 
 
 C: 
 
 = i. 
 
 or, supposing the integration on the right hand side effected, and 
 the constant included 
 
 l^iPix), 
 and consequently x = \//(/), 
 and the problem is completely solved. 
 
4^ A TREATISE ON DYNAMICS. [cHAP. 
 
 The different forms that may be given to f{x) and the different 
 conditions that may be assigned for the determination of the con- 
 stants, are the points in which one problem differs from another. 
 Readiness in performing the operations, in expressing analytically 
 the conditions given for the determination of the constants, and in 
 interpreting the results obtained is only to be acquired by the solu- 
 tion of a great number of problems. 
 
 drx 
 The equation -rp=fi^) 
 
 can sometimes be solved at once as a differential equation ; in this 
 case it is generally the best method of solving the problem. We 
 thus get at once 
 
 and hence v = -j- = -4^' (t), 
 
 by differentiation: in this case \/^(0 will contain two unknown con- 
 stants, which have to be determined as before explained. 
 
 40. We will take the case where 
 f{x)=-nx, 
 fx being constant, as affording an example of both methods of solu- 
 tion, and being itself most important. It is the case in which the 
 force varies directly as the distance of the body from some fixed 
 point from which x is measured, and acts towards that point. 
 d'x . . 
 
 -d? — ^^' (') 
 
 dx d^x ,, dx 
 
 ^dxV 
 
 Tf dt'~ '^^''■'dt 
 
 , fdx\^ 
 
 fXX 
 
 Suppose now that when the particle is at a distance x^ from the 
 origin it is moving from it with a velocity Vi ; then we have 
 v,' = -iJiX,'+C; 
 
 and .-. v' = v,'-fx(x'-x,') (2) 
 
 This equation gives the velocity in any position- From it we 
 have 
 
 ^^=^Jv,^-^{x^-xO, 
 
 we must take the upper sign because we suppose the body to be 
 
 dx . 
 moving from the origin, and therefore -j- is positive. 
 
"•] A TREATISE ON DYNAMICS. 41 
 
 we have therefore -r- = , ■ , 
 
 ■h 
 or altering the form of the equation. 
 
 from which t = - _ sin~^ ^^'^ 
 
 J/J- Jvr+fx. 
 
 ^s/f 
 
 x,^ .smj~n{t-c'); (3) 
 
 suppose that when / = 4 the value of x is x.,, we then have 
 
 1 . , Xzjui 
 
 t, = -j^. sin-' - j^^^ + c', 
 
 which gives a value of c': we will not substitute this value because 
 it is complicated, and the letter c' may stand as its representative. 
 Equation (3) shews that the value of x can never exceed 
 
 J' 
 
 — +Xi- : this is a known quantity ; call it a ; then equations 
 (2) and (3) may be written 
 
 v^ = ix(a-- X-), (4) 
 
 x = a.&inj^(t-c') (5). 
 
 Equation (5) shews that as t increases x will increase till 
 J^{i -c') first becomes an odd multiple of -; x will then be equal 
 
 to a ; and equation (4) shews that v will then be zero or the body 
 will come to rest. As t goes on increasing x will diminish and the 
 body will move in the opposite direction ; when Jfx (i - c') becomes 
 a multiple of tt, x will be zero and the body will be at the origin 
 moving with a velocity a Jjx in the negative direction : as x in- 
 creases negative the velocity will decrease, and when x = -a or 
 
 Jix{t-c') is again an odd multiple of ^j ^ will again be zero, and 
 
 th body will be at rest at a distance a on the negative side of the 
 origin. After this it will again move in the positive direction, and 
 will continue moving backwards and forwards between the limits 
 X = a and x = — a. Any motion of this kind is called oscillatory. 
 
 We saw that the body came to rest whenever Jfx {t - c') was an 
 odd multiple of ^ ; hence if t', t", &c. be the successive values of/ 
 for which this is the case, we must have 
 
42 A TREATISE ON DYNAMICS. [cHAP. 
 
 JJi(t"'-c')^(2 7i + 5)~, 
 
 .: t"-t' = t"'-l" = 8zc.= ^. 
 
 This result is curious, inasmuch as it shews that the time of 
 moving from rest to rest is independent of the distance between the 
 points of rest. 
 
 The time from rest to rest is called the time of an oscillation, the 
 distance between the points of rest is called the amplitude of the 
 oscillation. The peculiarity of this particular law of force is that the 
 time of oscillation is independent of the amplitude. 
 
 41. We will now apply the other method of solving the equation 
 rfF-"/^^ = ^ (^)- 
 
 The integral of this is known to be 
 
 X = A sin{J]x . t + B), (2) 
 
 where A and B are unknown constants. 
 Differentiating (2) we have 
 
 V = -£ = A Jil. cos(Jii J + B), (3) 
 
 Equations (2) and (.3) are exactly of the same form as those 
 obtained before for a: and v. The constants may be determined in a 
 similar manner and the interpretation is exactly the same. 
 
 Whenever an equation appears under the preceding form, this 
 latter method should always be adopted in integrating it. The 
 equation is one which presents itself continually, and should be 
 familiar to every one. 
 
 If the equation is of the form 
 
 which corresponds to a repulsive force varying according to the same 
 law, the integral is 
 
 X = C, e VJ^- « + Ca eV^r. <, 
 and the motion will not be oscillatory at all. 
 
11. J A TREATISE OX DYNAMICS. 
 
 43 
 
 42. Let us now consider the case where the force varies as the 
 
 «"' power of the distance ; in this case 
 
 
 
 d'x 
 
 -11^ = -^'='' 
 
 •0) 
 
 
 dx d^x „ „ dx 
 
 
 
 „ (dxV ^ ^fxx"^' 
 
 
 ^; 
 
 If I' = 111 when x - a, we have 
 
 w + 1 
 
 
 
 O ,1 
 
 r-).. 
 
 ....(2) 
 
 cy 
 
 which gives the velocity in any position. 
 
 The next integration which would give the relation between x 
 and t cannot generally be effected. 
 
 If t>i and a are both positive the body is then moving from the 
 origin, and equation (2) shews that as x increases v diminishes; let 
 c be the value of x that makes v = 0, then c will be given by the 
 equation 
 
 and equation (2) may be replaced by 
 
 ^,^^ _ 
 
 There is a peculiarity about this expression for the velocity when n 
 is even which is worthy of attention, as it illustrates a point re- 
 quiring great care when physical conditions are to be expressed 
 analytically. 
 
 When x = c, i; = 0, and the particle is at rest at a distance c from 
 the origin, acted on by a force tending towards the origin ; it will 
 therefore commence moving in that direction, and its velocity at any 
 distance will be given by equation (3). 
 
 First let ?« + 1 be positive : then if V be the velocity of the body 
 when it reaches the origin, 
 
 «+ 1 
 
 So far the force has been increasing the velocity of the particle, its 
 direction now changes, since it is supposed to act towards tlie point 
 
44 A TREATISE ON DYNAMICS. [CHAP. 
 
 chosen as origin, and it will therefore tend to diminish the velocity ; 
 and since the intensity of the force is the same at equal distances 
 on opposite sides of the origin, it is to be expected that the velocity 
 will be destroyed by exactly the same steps by which it was gene- 
 rated. This conclusion follows from the similarity of the action of 
 forces when they accelerate and retard the motion of a particle. It 
 also follows from the equation 
 
 ^,^J±_ (c«+._j,n+n /gX 
 
 w+ 1 ^ ^ ^ ' 
 
 when 71 + \ is even, since in this case the equation gives the same 
 value to V for values of x equal in magnitude and of opposite signs, 
 and therefore as x increases negative the velocity will gradually 
 diminish, being always the same as it was at an equal distance on 
 the opposite side, and will ultimately equal zero when x = — c. 
 
 When, however, w + 1 is odd, negative values of a; substituted in 
 equation (3) give for v values greater than V. Now it is impossible 
 that a force acting in a direction opposite to the motion of a particle 
 can increase its velocity : therefore equation (3) cannot correctly 
 represent the velocity on the negative side of the origin. Referring 
 to the equation 
 
 -di^^-'^' ^') 
 
 from which we started, we find that - fxx"^ the analytical expression 
 for the force, represents correctly a force tending towards the origin, 
 both for positive and negative values of x, when n is odd ; but that 
 when n is even it represents a force tending towards the origin for 
 positive values of x only, and therefore conclusions derived from it 
 will not be true for negative values of x. For negative values of x 
 the correct equation is 
 
 d'x 
 
 from which v^ = 1- C, 
 
 ?i+ 1 
 
 and making v ^- . / ~ , 
 
 when x = 0, which amounts to supposing the particle to pass through 
 the origin in the negative direction with the velocity V, we have 
 
 as the equation to be used in this case instead of equation (3). 
 
II.] A TREATISE ON DYNAMICS. 45 
 
 This equation shews that the velocity gradually diminishes as x 
 changes from to - c when it equals zero, consistently with what 
 takes place when ti is odd. 
 
 Now let 71 be negative, and ^ - 7/1. Equation (3) becomes 
 
 „.=^(_i,_A^) (5) 
 
 m-1 \x" ^ c"^V ' 
 
 and we see that the velocity increases without limit as the body 
 approaches the origin. This was to be expected since the force 
 which produces the motion itself increases without limit. As in the 
 previous case, when ?« - 1 is even, this equation shews that the 
 velocity decreases, as the body recedes from the origin in the nega- 
 tive direction, till it comes to rest at a distance c. When 7n - 1 is 
 odd, negative values of x substituted in (5) give impossible values to 
 V. The explanation in this case is the same as before: when m is 
 
 odd — ^ represents the force correctly on both sides of the origin, 
 when m is even - ^ must be used for positive values of x, and -^for 
 
 negative values, and the velocity on the negative side of the origin 
 will be given by the equation 
 
 2m / 1 J_\ 
 ^ ~ m-l \x'"-' "^ c"-7 ■ 
 
 In all these cases then the body will pass through the origin and 
 move in the negative direction, losing its velocity at the same rate 
 at which it acquired it, and will come to rest when x=-c. It will 
 then move towards the origin and pass through it as before, con- 
 tinuing to oscillate between the limits x ^c and x = - c. 
 
 43. In the cases of rectilinear motion which have hitherto been 
 considered, the forces which acted on the particle were either 
 constant, or some functions of the position of the particle. 
 
 The force may also be some function of the velocity with which 
 the particle is moving; that is, the equation of motion which has 
 hitherto always been of the form 
 
 d'x .. . 
 
 d'x Jdx\ 
 may now become 'Trr=J\jj)> 
 
 d'x „{ dx\ 
 
 ""' di' 
 
46 A TREATISE ON DYNAMICS. [cHAP. 
 
 These equations when they occur must be solved by the ordinary 
 methods applied to differential equations. 
 
 We will solve two or three of them to exhibit the methods. 
 Let the equation of motion be 
 
 Ti 
 
 ^-a)" (■) 
 
 that is, suppose the only force which acts on the body to be a 
 retarding force varying as the w* power of the velocity. The above 
 equation may be written 
 
 1 dv 
 
 The integral of which is 
 
 Let V = Di when t = 0, then 
 
 1 
 
 C, 
 
 and — -r ;rT=(«-l)M^- 
 
 This equation shews that as / increases the velocity will con- 
 tinually diminish, but will never be actually zero. From this 
 equation 
 
 1+V"~^. (}l — l)fxt' 
 
 and therefore -tt = v 
 at 
 
 from which C + .-^^l+^'"~'-("-^>'t 
 
 1 + Vi"-^.(n- l)fjii]"-^ 
 t),"-'.(«-l )M 
 
 which gives a; as a function of t. 
 
 The above solution becomes nugatory when 7i=l ; in this case 
 the solution of the differential equation takes a different form ; 
 we have 
 
 d'x _ dv 
 
 "de^'^Tt' 
 
 dx ^ 
 let Ui be the velocity when x^a, then 
 
 (1) 
 
II.] A TREATISE ON DYNAMICS. 47 
 
 dx 
 
 dt 
 
 -v,=(x{a-x); (2) 
 
 1 iI^^ . 
 
 fxa + Vi — nx ' dt 
 .-. log {n{a-x) + v,} = -fxt + C, 
 
 let t = when x = a, then 
 
 C = log v„ 
 
 and /i (a - x) + ?;,=??, e"**', (3) 
 
 which gives x as a function of t. 
 
 Equation (1) might have been integrated as follows: 
 
 1 dv 
 
 .: log v= — nt + C, 
 log Vi = C; 
 .-. t' = v,6-'^' (4). 
 
 44. Cases of motion of this sort are more curious than useful. 
 The only case known to exist in nature of a force depending on the 
 velocity of the moving body, is when the body moves in a fluid, or, 
 as it is commonly called, a resisting medium. In this case it is 
 found that the fluid exerts a pressure on the particle in a direction 
 opposite to that in which it is moving, and varying directly as the 
 square of the velocity. If the body is acted on by no other force the 
 solution of this is included in the general case just discussed. Let 
 us consider the case where the body is acted on by a constant force 
 as well. 
 
 The equation of motion is 
 
 £^=/-*"'. 0) 
 
 dv 
 
 or -y- = f-kv^ ; 
 dt ^ 
 
 _J_ ^- 
 •*• f-k^-^ ' dt~ ' 
 
 l=.log^^C±H?=^+C. 
 
 2 Jfl^ J/- V J/c 
 
 Let v = Vi when t = 0, then 
 
48 A TREATISE ON DYNAMICS. [CHAP. 
 
 or \//+ ^ V^ ^ J/+VjJ^ ^2 ViS . ' 
 Jf-vJk-Jf-vJk' ' 
 
 =y 
 
 
 where m = ^'^^4 !-^ : 
 
 we may also solve equation (l) as follows : 
 
 
 
 dv 
 dt 
 
 dv dx 
 
 ^Tx -Ji^ 
 
 dv 
 
 '■Tx- 
 
 So that 
 
 (1) becomes 
 
 
 
 
 
 
 dv , , 
 
 V ^f- + kv' = 
 dx 
 
 /• 
 
 Let 2 w = ^;^ then 
 
 dm 
 dx 
 
 dv 
 -Tx' 
 
 
 
 
 and 
 
 .■.p-,2k 
 dx 
 
 
 
 
 or 
 
 »' = |.2C 
 
 . e-'*-. 
 
 Let v = 
 
 Vj when ar 
 
 — a, 
 
 then 
 
 
 
 
 f- 
 
 kv' = (f-kv 
 
 ')e-^'^-' 
 
 (3). 
 
 Equations (2) and (3) comprise the complete solution of the 
 problem ; they give two relations between v, t and x. 
 
 It appears from an examination of either of these equations that 
 
 the velocity continually approaches kJ r, as its limit; if the original 
 
 velocity Vi is greater than this it will continue diminishing, but will 
 
 never become so small as a/t; if the original velocity is less than 
 
 Kj T it will continually increase, but never become so great as ^/ r ; 
 
 the name "terminal velocity" has been given to ,/ j . 
 
II.} A TREATISE ON DYNAMICS. 49 
 
 In motion of this kind considered as motion in a resisting medium, 
 the resistance is always in the direction opposite to that in which the 
 body is moving, so that if the forces whicli act on the body are such 
 as cause it to come to rest and then commence moving in the opposite 
 direction, the direction of the resistance will change. In any case of 
 this sort the problem must be separated into two, the one commenc- 
 ing where the other left off, at the point where the discontinuity- 
 takes place. The following is an instance. 
 
 45. Let a constant force act on the body in a direction opposite 
 to that in which the body is moving. The equation of motion is 
 
 de- J ^"^ 
 
 dv J. J 2 - ^ / 
 
 The integral of this is 
 
 1 
 
 Let i\ be the initial velocity, then 
 
 • tan-y^.^^C-^ 
 
 t-^n-' ^ J. v-tan-\^ J. v, = -Jfk.t (1). 
 
 As t increases v diminishes, and becomes zero when 
 
 Adopting the other method of integration, we have 
 dv 
 
 v^^kv' = -/; -r— - ^""^ '. ^ L^\^^ 
 
 dx 
 
 .H.X. 
 
 f-.w^-Ir^C.r^ 
 
 2 k 
 
 .: f+kv^=9.kC.e-"'\ 
 Let X be measured from the starting point, then 
 
 f+kv;' = 2kc, 
 
 and/ + /.V=(/4-^06-*- (2), 
 
 which gives the velocity of the body in any position. 
 
 By elimhiating v between (l) and (2) we may obtain a relation 
 between x and /. If in equation (2) we put u = 0, we have 
 
 e"^ = y^+l (3), 
 
50 A TREATISE ON DYNAMICS. [cHAP. 
 
 which gives the distance to which the body will move before it 
 comes to rest. After this it will commence moving in the opposite 
 direction, and the equations which determine the velocity and po- 
 sition in terms of the time, will be deduced from the case previously 
 discussed, by putting »>, = ; we thus get 
 
 and v-' = ^{l-e-"'% (5) 
 
 in equation (5) x is measured in the new direction of motion from 
 the point where the body came to rest. 
 
 If a be the value of x which satisfies equation (3), equation (5) 
 may be written 
 
 i;2 = /{l_e-^^C«-)}^ (6) 
 
 in which x is measured from the original starting point in the 
 direction of projection. 
 
 When a; = in this equation we have 
 
 or, substituting for a its value given by equation (3) 
 
 which gives the velocity with which the body returns to the point 
 from which it started. 
 
 This is the case of a body projected upwards in the air : writing 
 g for / the results may be stated as follows. 
 
 A body projected upwards with the velocity »j, will rise to a 
 height a given by the equation 
 
 g.^'-^g + kv,^ 
 in the time /, given by the equation 
 
 Ujgk = t&n-' ^-.v,, 
 
 it will then return in the time t^ given by the equation 
 
 Jg + kv^'-v.Jk' 
 and reach the starting point with the velocity v, */ — ~—^ . 
 
n.] A TREATISE ON DYNAMICS. ol 
 
 These examples will be sufficient to shew how cases of motion of 
 this kind are to be treated ; it will be seen at once that the difficulties 
 they present are entirely analytical. 
 
 Before leaving the subject of resistances, however, we will make 
 one remark which will be understood at once by any one familiar 
 with the nature of fluid pressure. 
 
 The actual force of resistance exercised by the fluid will be the 
 same for all bodies of the same size and shape. Consequently the 
 accelerating, or rather retarding, force of the resistance will vary 
 inversely as the mass of the body in motion. For bodies of the same 
 shape and size may have very different masses if composed of diffe- 
 rent materials. Now it is with the retarding force that we are 
 concerned in dynamics. We draw attention to it in this case because 
 it is apt to be overlooked, from the fact that most of the forces with 
 which we ai'e concerned in dynamics vary directly as the masses of 
 the bodies on which they act, and consequently their accelerating 
 forces are independent of those masses. 
 
 46. The preceding examples will be sufficient to shew how any 
 problem on the rectilinear motion of a particle is to be treated. The 
 first step is to express analytically the forces Avhich act on the 
 particle, and to form the equation of motion; the next step is to 
 integrate this equation ; the third is to express analytically the con- 
 ditions given for determining the constants introduced by integration ; 
 and the last and by no means least important is to interpret the 
 equations thus obtained, that is, to examine them for different values 
 of the variable quantities which enter into them, and so to trace the 
 motion of the particle through any peculiarities it may present. 
 
 47. Let us now proceed to the case of curvilinear motion, and 
 first, for the sake of simplicity, we will consider motion in one 
 plane. 
 
 The equations we have obtained are 
 
 If X = and F=0, the particle will move on in a straight line Ijy 
 the first law of motion. 
 
 Let X= and F = - Mg. This will be the case of a body pro- 
 jected from the surface of the earth and acted on by gravity, the 
 
 4—2 
 
52 A TREATISE ON DYNAMICS. [cHAP. 
 
 axis of X being measured horizontally and the axis of j/ vertically 
 upwards. The equations of motion are 
 
 (1) 
 
 
 
 
 
 d'x 
 
 df 
 
 = 0, 
 
 
 _J......... 
 
 Integrating 
 
 these 
 
 we 
 
 hav 
 dx 
 dt 
 
 e 
 
 
 
 
 
 dt 
 
 -c- 
 
 •«'• 
 
 Suppose the body to be projected from the origin with a velocity 
 V, in a direction making an angle a with the axis of x, and let t be 
 measured from that instant ; then we have 
 dx 
 
 (2) 
 
 , - FCOS a, 
 
 at 
 
 -~ = ^sin a — £•/. 
 dt 
 
 And integrating again, we have 
 
 X — Fcos a.t + C", 
 
 y =V s,\n a. t-\gf + C", 
 or since x and 3/ are zero when ^ = 0, we have 
 
 w= Fcosa J ) /g-\ 
 
 ^ = Fsin a .^- ^gt^ J 
 
 Equations (2) give the resolved parts of the velocity, and equa- 
 tions (3) the position at any time. 
 
 From (2) -/ = tana-77-^ 
 
 ^ ^ dx v cos a 
 
 which gives the direction of motion, 
 
 = JV'-2gtV^\na-^gH\ 
 which gives the velocity at any time. 
 
 Eliminating t between equations (3) we have 
 
 ^■*' 
 
 y = tan a .x- —rj^ j- , 
 
 ^ 2 F^ cos'- a 
 
 a relation between the co-ordinates of the particle independent of the 
 time, and therefore the equation to its path. 
 
"•] A TREATISE ON DYNAMICS. 53 
 
 This equation shews that the curve in which the particle moves 
 is a parabola whose axis is vertical, and concavity downwards; 
 putting it in the form 
 
 / _ ^-sina cos a Y_ 2F-cos'« / V'sm' a 
 
 we see that the co-ordinates of the vertex are 
 
 F* sin a cos a , F^sin^a 
 
 and — , 
 
 g ^g 
 
 , ,, , . • 2 F^ cos- a 
 
 and the latus rectum is . 
 
 g 
 
 The height of the directrix above the origin is 
 
 r^sin^a F^cos^a - . , V' 
 -i which 
 
 2g 2g 2g 
 
 If the body fell from rest vertically through this height it would 
 acquire the velocity T; and since any point of the body's course 
 may be considered the starting point, it follows that the velocity at 
 any point in the path is that which the body would acquire in falling 
 verticall}'^ from the directrix to that point. 
 
 We see from equations (2) that the resolved part of the velocity 
 in a horizontal direction is constant throughout the motion, and that 
 the vertical component varies as it would do if the body were 
 moving in a vertical line. This consideration is useful in discussing 
 many points in the motion of projectiles. 
 
 From these equations there will be no difficulty in obtaining the 
 " range" of the projectile, that is, the distance of the point at which 
 it will strike a horizontal or inclined plane passing through the point 
 of projection ; and the time that will be occupied in it, which is 
 called " the time of flight." 
 
 Sometimes it will happen that V and a are not given, and have 
 to be determined by the conditions of the problem, as for instance, 
 to find V and a, that the path may pass through two given points. 
 
 By varying the conditions of this sort, an endless number of 
 problems may be formed, all of which may be solved by the appli- 
 cation of the above equations, either in their present or in a modified 
 form. 
 
 If instead of X=0 we had X constant, the case would not be 
 altered, for the two constant forces X and 1' would be equivalent to 
 some constant force in some constant direction ; and no force would 
 act in a direction at right angles to this. 
 
54 A TREATISE ON DYNAMICS. [ciIAP. 
 
 48. It is unnecessary to consider the case of X and Y being 
 functions of t explicitly as this never occurs in nature. 
 
 Let then X and Y depend on the position of the particle, and 
 first let 
 
 X be a function of (x) alone 
 
 and Y a function of (y) alone. 
 In this case we have 
 
 ~ dt • dl' ^y^ dt ' 
 
 0) 
 
 (2). 
 
 These two equations give the resolved parts of the velocity, and 
 therefore the actual velocity and direction in any position. C and C 
 must be determined from the velocity and direction in some known 
 position. 
 
 From equations (2) we have 
 
 \A'xl ~ 2jf{x)dx+C' ^-"^ 
 
 which gives the direction of motion at any instant, or the position of 
 the tangent to the path. 
 
 If we can integrate equations (2), we shall obtain two relations, 
 between x and t, and between 7/ and t ; each of these will contain 
 a new constant which must be determined from the position of the 
 particle at some instant : if between these two equations we eliminate 
 t, we shall obtain a relation between x and ?/ which will be the 
 equation to the path of the particle. 
 
 The equation to the path may also be found at once by inte- 
 grating equation (3). The constant in this case will be determined 
 from any corresponding values of x and y, or, in other words, any 
 point through which the curve passes. We may remark that equa- 
 tion (3) will always be integrable when equations (2) are, and never 
 when they are not. 
 
II.] A TREATISE ON DYNAMICS. 55 
 
 dx , dy 
 
 pressed as functions of x and y ; we also have x and y as functions 
 
 of <; we may therefore by elimination find -7- and —- as functions 
 
 of ^; we shall then know the position, velocity, and direction of 
 motion of the particle at every instant, and the problem will be 
 completely solved. 
 
 49. As an example, 
 
 let X = -ixx, Y = -iiy, 
 so that our equations are 
 
 d^x \ 
 
 d^y 
 
 d¥=-^y 
 
 'dx 
 
 (1) 
 
 m 
 
 ., =G-«.. 
 
 whenx = /«, and^ = ^, let Vhe the velocity of the particle and a 
 the angle which the direction of motion makes with the axis of x, 
 then we have F^cos^a = d —fxh^, 
 V'sin-a = C2-fxk', 
 
 from which (-jjj = F'cos^a + fxk'-fxx'', 
 
 {^^'=V'-shva+,.k^-j,y^; 
 
 d^ =fcl 
 
 " d^~ jF'cos'a + fxh'-^x'' 
 
 dl ±1 
 
 dy ~ J V'sin^ a + fxk'-ixy' ' 
 
 Taking the upper sign in each case and integrating, we have 
 
 - '~ 
 J^ . < + C3 = sin" 
 
 JJ^.t + C.= 
 
 JV^ cos- a + [xh ' 
 
 JV'Jm^a + fxk' 
 and therefore J/x . x = JV'^ cos" a + fx h' sin {J~ix . / + C3), 
 Jf^-y = JV-s>\n^a + (xk- . sin {JJi . t + CJ. 
 
56 A TREATISE ON DYNAMICS, [cHAP. 
 
 If in these equations we substitute corresponding values oi x, y, 
 and t we sh^ll determine C3 and d, and x and 1/ will then be com- 
 pletely known as functions of t, and also -^ and --^ . Also by elimi- 
 nating t we should obtain an equation between x and y, which would 
 be the equation to the curve described by the body. It will be 
 found on elimination that this curve is an ellipse whose centre is the 
 origin. 
 
 We might have integrated equations (1) at once, as linear equa- 
 tions, and that would in this case have been the easier method of 
 solution though not so generally applicable. We will illustrate this 
 method with particular values of the constants h, k and a. 
 
 Suppose the particle to be projected from a point in the axis of .r 
 at a distance a from the origin in a direction parallel to the axis of 3^, 
 with a velocity F. The equations are 
 d'x 
 
 77?-^'^^ = ^) 
 
 The integrals of which are 
 
 x = A^ cos {Jn . 1 4 Bi), 
 y = A., cos {J'fi . t + Z?.), 
 
 and therefore -jj = - A, Jn sin {Jn . t + B,), 
 -j- = - A, Jn sin (Jn .t + B.): 
 
 when / = 0, we have 
 
 dx_ ihj_ 
 
 making these substitutions, we have the equations 
 
 a = 7^1 cos B„ (2) 
 
 0=^ocos5„ (3) 
 
 = -A,J~n&mB„ (4) 
 
 V=-A,/llsmB, (5) 
 
 From (2) and (4), we have 
 
 B,=0, A^^a. 
 
 From (3) and (5), we have 
 
II.J A TREATISE ON DYNAMICS. 57 
 
 Substituting these values we have 
 
 X = a cos (sfi^ . t) 
 
 y = -^sin(VM.0|' ^^^ 
 
 -j-:=-aJnsm{J^.t) 
 
 "^^ [; (7) 
 
 ^=Fcos(JJ..t) 
 
 ^■^•'^""-.1 (8). 
 
 and eliminating i between equations (6) we have 
 
 a' ' F' 
 
 The equation to an elhpse whose semiaxes are a and ( 'nj; oi* 
 putting (b) for the last, we have 
 
 x= a cos ^t, 
 ij=:b sin Jfx t, 
 
 ■£ = bJ',IcosJfxt, 
 
 a' b' ' 
 
 In these equations / is the time from the extremity of that axis 
 which coincides Avith the axis of x. 
 
 These equations are very often useful and are worth remem- 
 bering. 
 
 Ill the preceding example* the resultant of the forces X and Y 
 always passes through the origin, and is equal to n times the 
 distance from the origin. This is a particular case of a class of 
 forces called central forces which will shortly occupy a large share 
 of our attention. 
 
 The example we have given will be sufficient to illustrate the 
 method of proceeding in problems of this class. In particular cases, 
 artifices will frequently suggest themselves which will render the 
 solution much easier; these however are best acquired by practice. 
 
 50. We will now enter upon the consideration of the case where 
 X and Y are each functions of both x and i/. 
 
 The above method of solution evidently will not apply, nor can 
 we offer any that will be generally applicable. The following how- 
 ever will often be found useful. 
 
58 
 
 
 
 A 
 
 TREATISE 
 
 ON 
 
 
 The 
 
 equations 
 
 are 
 
 df 
 
 df 
 
 = F 
 
 [chap. 
 
 •(1) 
 
 " ^\Tt' dt'^dfdej~~\^dt ^^ dtj' 
 
 or d.v- = ^{Xdx+Ydy) (2) 
 
 When the right hand side of this equation is a perfect differential 
 of X and y considered as independent variables, we have by inte- 
 gration 
 
 If F be the velocity when x = a, and y=-h, 
 V'=c+f{a,b); 
 .-. v^-V'=fix,y)-fia,h) 
 which shews that the change in the velocity in passing from any one 
 point to any other depends only on the co-ordinates of those points, 
 and is independent of the path by which the body has passed from 
 one to the other ; that is, if from any point (a, h') we can project the 
 body with a velocity V in any number of different ways so as to 
 pass through the point (x, y), it will in each case pass through it 
 with the velocity v. 
 
 Again, referring to equations (l), we have 
 d^y d'x 
 
 ''d¥--ydw='=^--y^- 
 
 If the right-hand side of this equation is constant and equal to 
 c we have by integration 
 
 dy dx ^ , 
 
 dt -^ dt 
 The only case in which this method of integration is useful is 
 when c = 0, in this case the resultant of the forces X, Y passes 
 through the origin, and we have 
 
 dy dx J 
 dt ^ dt 
 
 If A be the area swept out by the line joining the origin and the 
 particle, we have 
 
 ^ dA dy dx J 
 
 .-. 2A = ht+ C, 
 
II.] A TREATISE ON DYNAMICS. 59 
 
 or if A be reckoned from the time when t = 0, 
 
 2A= hi, 
 that is, the area described in any time is proportional to the time of 
 describing it. 
 
 This is true whenever the resultant force which acts on the par- 
 ticle passes through the origin ; that is, through any fixed point 
 which may be taken as the origin. 
 
 These equations when obtained are only the first integrals of the 
 equations of motion ; the second must be obtained by artifices sug- 
 gested by the forms of the equations in each particular case. 
 
 51. There is a class of problems the inverse of those we have 
 been considering, viz. where it is required to find what must be the 
 forces under whose action a particle would move in a certain speci- 
 fied manner. 
 
 If the co-ordinates x, y of the particle were given as functions 
 of t we should obtain the resolved parts of the force at once by two 
 differentiations, this would be the simplest form of the pi'oblem. A 
 more common form of it is to find the force under the action of 
 which a particle would move in a certain given curve. 
 
 Let F(x,j/) = (1) 
 
 be the equation to the given curve : differentiating this equation 
 we have 
 
 If we differentiate this again, we have 
 
 Now our object is to find -^- and -~^ and we see that from 
 
 equation (1) we are able to obtain only a single relation (3) between 
 these quantities and others : some other condition therefore is neces- 
 sary to render the problem definite. We might, for instance, assign 
 one of the forces arbitrarily as a function of x and y, and equation 
 (3) would then enable us to determine the other : thus let 
 
60 A TREATISE ON DYNAMICS. [ciIAP. 
 
 eliminating y between this and (1) we obtain 
 
 from which we may find -7- . 
 •^ at 
 
 dn d 2J 
 
 Substituting this value in equation (2) we obtain -jj , and ■— may 
 
 then be found by differentiation, or from equation (3). 
 
 In this case we had to integrate -r-^ to determine -7- ; and gene- 
 rally, whatever condition is given in addition to the equation to the 
 curve, it will be necessary to express it in the form 
 
 /(-^'§''J)-^ w 
 
 that is, in the form of an equation involving one or both of the 
 first differential coefficients and neither of the second differential 
 coefficients. 
 
 From (1), (2) and (4) we can always deduce equations of the 
 form 
 
 from which we obtain 
 
 The resolved parts of the force are then known. 
 
 Problems of this kind seldom present any difficulty, as the 
 operations consist for the most part of differentiation, and not of 
 integration. 
 
 52. For example, let it be required to find under the action of 
 what force a body would describe an ellipse with uniform velocity. 
 
 I-' ^^l'=» (■) 
 
 be the equation to the ellipse, v the constant velocity, then 
 
 (syns)'-' (^) 
 
 , . X dx V dy ^ fo\ 
 
 from equation (1) -.-+^.^ = (3) 
 
II.] A TREATISE ON DYNAMICS. 61 
 
 Eliminating y and ~ from these three equations we have 
 
 \dt) a*-(fl»-6^)a:' ^^ 
 
 Differentiating (4) Ave have 
 
 Similarly we may obtain 
 
 Y^_ d^y _ c^h^v'y 
 
 M~dP~~ \v^{p~ra:ijf\^' 
 
 X and Y are the resolved parts of the force parallel to the axes. 
 Since l-^ i a*-(a^-b^)x' Y_a^y 
 
 we]|see that the resultant of X and Y coincides with the normal to the 
 ellipse at every point. 
 
 Let a = b and the ellipse be a circle ; then 
 
 and the resultant, which acts in the normal, and therefore always 
 passes through the centre 
 
 = JX'+Y-' = M-; 
 
 that is, a body will describe a circle under the action of a constant 
 
 force M— tending to the centre. 
 
 We may shew, generally, that when a body moves with uniform 
 velocity, the resultant force on it acts in direction of the normal : for 
 since the velocity is uniform 
 
 i^hm 
 
 a constant quantity ; 
 
 dx d^x dy 
 
 •'• df'd^^'di' 
 
 ■g=- 
 
 Y de 
 
 •''X = d^" 
 
 dx 
 
 dt^ 
 
 
 which proves the proposition. 
 
62 A TREATISE ON DYNAMICS. [CHAP. 
 
 53. It is sometimes convenient to employ polar co-ordinates in 
 the solution of problems. 
 
 In this case the force is resolved in direction of, and perpen- 
 dicular to the radius vector. 
 
 We will conclude this Chapter by making the requisite trans- 
 formations. 
 
 Let P be the part of the force tending to the pole, T the part 
 perpendicular to that direction, 
 
 X = r cos d, y -f sin Q, 
 then we have P = - X cos - F sin 0, 
 
 r = - X sin + F cos Q. 
 
 The equations of motion are -r-y = X, 
 
 cosaJ|-sina^! = r. 
 
 dt^ dt^ 
 
 -^ dx ^dr . ^dd 
 
 NoWj -r- = cos t^ J- - r sm o -j-r, 
 ' dl dt dt 
 
 dy . .dr .de 
 
 -yf = sm -r- + r cos -T- ; 
 dt dt dt 
 
 fdev . .d'd 
 
 d^x .d'r ^ . .dr de 
 
 -^,=cosa^-2sm0^.^-. 
 
 d'v . „d'r ^dr dd . . {ddV . d'd 
 
 ^ = sm0^4-2cos0^.^-rsmay ...cosa-. 
 
 Hence substituting 
 
 '■r fdey 
 7-'\dt)=- 
 
 de 
 
 dr de d'e_ 
 '~~d'f'dt^''-dt'~-^' 
 
 These are the polar equations of motion. 
 
 The preceding transformation is the most direct, and leaves the 
 problem still in the form of two differential equations of the second 
 order between r, 6 and t. 
 
 The following transformation is more useful though more indi- 
 rect : we have 
 
II.] 
 
 A TREATISE ON DYNAMICS. 
 
 63 
 
 ~ = -Pcos0-rsme 
 ^,=- P sine +T COS 
 
 From these 
 
 
 dy dx , 
 Let X -f- -y -rT = "i 
 dt ^ dt 
 
 J . odd dy dx , 
 
 and since K-r-=x~r--y-r- = h, 
 dt dt ^ dt 
 
 dh_dh dd_h dh 
 dt~ dd' dt ~r'' dd 
 
 and integrating 
 
 where - is written for r. 
 
 dd. 
 
 Again, 
 
 dr 
 dt 
 
 df 
 
 (1). 
 
 (2) 
 
 (3) 
 
 1 du do du 
 
 u'-Jd 'Tt^~''Td' 
 
 dh du .„ J d^u 
 "di'TQ'''''' 'W 
 
 Substituting this value of -j-5 in the equation 
 
 , dh dii d-ic ,„ 3 _ ^ 
 
 we have -rr . -rz+ h^u^ . -r^ + «' ?r - P = ; 
 
 dt ' dd 
 
 dd' 
 
 , ^, . d^u P T du ^ 
 
 and therefore, _ + „-_+ ^^,-^^3- • _ = O; 
 
 and substituting for hr the vahie given by (3) we obtain 
 P T du 
 
 d'u h.'ii'' h.-u""' de 
 
 1 +2 
 
 
 (4), 
 
 de 
 

 de 
 Tt'- 
 
 h 
 
 A TREATISE ON 
 
 \ DYNAMICS. 
 
 and 
 
 = Kn-Jl^2^ 
 
 L^l.a 
 
 64 A TREATISE ON DYNAMICS. [cilAP. 
 
 (5). 
 
 Equations (4) and (5) though very complicated in appearance 
 will not be so in practice, since in the cases which occur the forms 
 of P and T will be such as to introduce considerable simplifications. 
 
 When the whole force which acts on the body is central, we have 
 T =0, and these equations become much simpler. We have in 
 this case 
 
 d'u P 
 
 . dt 1 
 
 These equations, however, and the class of problems depending 
 on them deserve an independent consideration. 
 
III.] A TREATISE ON DYNAMICS. 65 
 
 CHAPTER III. 
 
 54. When the direction of the force that acts on a particle 
 always passes through a fixed point the force is said to be central, 
 and that point is called the center of force. In the cases that will 
 present themselves the intensity of the force will generally be a 
 function of the distance of the particle from the center and of 
 nothing else. Many of the properties of motion round centers of 
 force are true, whether this is or is not the case. The student will, 
 however, see from the proof whether this is requisite or not. 
 
 We will first shew, that however a body be projected, if it is 
 subject to the action of a central force only, it will always move in 
 one plane: and we shall afterwards confine our attention to that 
 plane. Let P be the accelerating-force to the center, x, y, z the 
 co-ordinates of the particle at time t, r its distance from the origin 
 which is the center of force. Then the equations of motion are 
 d^x _ Px 
 de~ r ' 
 
 de r ' 
 
 Combining these equations two and two, we obtain ^^^ O/ p.,.- y^ 
 
 d'z d'y „ "* *"" '^ 
 
 d^x d'2 
 ^ df^'^'W'-^' 
 
 d'y d'x 
 
 Integrating these, we have 
 
 dz dy , 
 dx dz . 
 
 'irr'-dt = ^''' 
 
 dy dx , 
 
 ""dt-yTt^^'^^ 
 
66 A TREATISE ON DYNAMICS, [cHAP. 
 
 where h^, h^, h^ are constants introduced in integration. Multiply- 
 ing them by x, y, and z respectively and adding, we get 
 
 = ^1 X + h-^y + h^z, 
 
 a relation to which or, y, and z are always subject. 
 
 But this is the equation to a plane passing through the origin, 
 therefore the body is at every instant in the same plane, and this is 
 its equation. 
 
 The curved line in which a body moves round a center of force 
 is called its orbit. 
 
 It may be seen from the above equations that the areas described 
 on the co-ordinate planes by the projections of the radius vector are 
 proportional to the times of describing them. 
 
 We will for the future consider the plane of motion as that of xy, 
 and retain the rest of the notation. 
 
 55. The equations of motion are 
 
 ^ = -P- = - Pcos^l 
 r 
 
 g--f-— r '' 
 
 X = r cos 6, 7/ = rsmd, (2) 
 
 2 , „2 _ ,.2 
 
 X + 
 
 f = ^,..-..^ (3) 
 
 before, a: --^--1/-^ = h. 
 
 dt ^ dt 
 ■ivT dy dx .dd 
 
 ■-'fr" w- 
 
 It is found convenient to use the reciprocal of r instead of r, and 
 to denote it by u, so that 
 
 rr"" (=)• 
 
 Now since x=^- cos Q ; 
 u 
 
 dx __sme de cos d du d^ 
 •*• It' u dt u' dd dt 
 
 — — hu sin 6 — h cos B -r^ ; 
 av 
 
III.] A TREATISE ON DYNAMICS. 67 
 
 (Px J add J ad'u dB 
 
 .-. -,=-/„,cos0^-/.COS0^^ ^ 
 
 = - Jl^U^ COS Q - h' U^ cos Q -TTi . 
 
 av 
 
 Substituting this in the first of equations (1), and dividing by 
 cos 0, we have 
 
 Equations (5) and (6) are the polar equations of motion : they are 
 equivalent to the two equations (1). 
 
 Since however equations (l) are both of the second order, their 
 integrals will contain four arbitrary constants. Equation (5) is of 
 the first order, consequently only three constants will be introduced 
 in the solution of equations (5) and (6). The remaining one h has 
 been already introduced in the process of transformation. 
 
 These two may be considered as fundamental equations by which 
 all questions relating to central forces may be solved. The constants 
 which are introduced in integration are determined by various con- 
 ditions which form part of the data of the problem. The quantity 
 h which occurs in these equations is twice the sectorial area swept 
 out by the radius vector in a unit of time. It is constant throughout 
 the motion, and must be known in order that the problem may be 
 completely solved. It will therefore be found useful to express it in 
 terms of some of the other quantities that enter our equations. 
 
 We have /e = r*-r- 
 at 
 
 dt 
 
 Now V- 
 
 i_ /ddv ^ 1 /dev 
 
 ^ p'u* \dt) ~ tt« sin> \dt) ' 
 
 5—2 
 
6S A TREATISE ON DYNAMICS. [cHAP. 
 
 Where p and (p axe, as usual, the perpendicular on the tangent, 
 and the angle between the tangent and radius vector. 
 From these equations we have the following relations : 
 
 t;^sm-0 o , . 2 
 
 m 
 
 .(7). 
 
 These relations are useful in solving the equations 
 ^"=rf^' ^5) 
 
 rfa^ + ^'-AV = ^ (^)- 
 
 Though equations (5) and (6) are generally preferable, as being 
 the most direct, and giving the solutions under the form of an 
 equation between r and Q, there are some other relations which in 
 particular cases are advantageous. We have 
 
 ^JB _ -p X 
 
 df ~~ r' 
 
 dC r' 
 
 " dt df dt de~ 'r\ dt^ dtj' 
 
 dv y^dr ,„, 
 
 '''''Tr-^-dt («^- 
 
 From this equation the velocity can at once be determined as a 
 function of the distance. We have by integrating it 
 
 v"-=f{r) + a 
 If V be the velocity at distance R we have 
 
 ... v^-F^=f{r)-f(R). 
 
 This equation is a particular case of the more general one 
 obtained in Art. 50. 
 
 Equation (8) may be written 
 
 dr 
 and is easily remembered under that form. 
 
III.] A TREATISE ON DYNAMICS. 69 
 
 Again, from (7) we have 
 
 h 
 
 V =- ; 
 P 
 
 .: log V = log k - log p, 
 
 and difFerentiatine - . -j- = . -^ • 
 
 ^ V dt p dt' 
 
 and from (8) 4^ = -P^(; 
 
 ••-•'•p-"! (» 
 
 If q be the chord of curvature of the orbit through the center of 
 force 
 
 therefore equation (9) may be written 
 
 «^ = 2P.| (10) 
 
 which shews that the velocity at any point is that which would be 
 acquired in falling through a distance equal to a quarter of the chord 
 of curvature of the orbit at that point, under the action of a constant 
 force equal in intensity to the force at that point. 
 Again, combining the equation 
 
 p- 
 with equation (9) we have 
 
 pA^> (11) 
 
 p^ dr ^ ' 
 
 another relation which is sometimes found useful. 
 
 The results here obtained agree with those arrived at by inde- 
 pendent considerations in The Pri?icipia, Book I. Section 2, with 
 which they should be carefully compared. 
 
 56. We will now apply these equations to a very important 
 example ; namely, where the force varies inversely as the square of 
 the distance. 
 
 This, it will be remembered, is the law of attraction in nature, and 
 it is from this fact that it derives its importance. 
 
 We have in this case P = fxu', 
 and substituting this in the equation 
 d'u P 
 
70 A TREATISE ON DYNAMICS. [cHAP. 
 
 we get the equation 
 
 The integral of this equation is 
 
 u = p{l + ecos{e-a)} (2). 
 
 This is well known as the polar equation to a conic section, the 
 focus being the pole, and — a the angular distance from the nearer 
 vertex. 
 
 Hence then a body moving about a center of force which varies 
 inversely as the square of the distance will move in some conic 
 section. 
 
 The constant quantities e and a which have been introduced in 
 integration must be determined from the circumstances of the motion 
 at some known epoch, or other equivalent data; h also must be 
 determined from similar considerations. For example, suppose it 
 known that, when 6 — O, u = c^, the velocity = V and the direction of 
 motion makes an angle (3 with the radius vector : differentiating 
 equation (2) we get 
 
 and .-. cot = - 1 . ^ /^r /^ ^ - ^£^ 
 
 ^ u dd ■ , ' ' - 
 
 = l.^.esin(0-«). 
 
 
 Hence we get Cj = ^ . (1 + e cos a), . ,- /jr \ '■ ''^^ '^'Ct '-r/l,^ 
 
 J. r> 1 M 
 
 cot /i = , y5 . c sm a, , , - , 
 
 The last equation determines h, the other equations give — -^ 
 
 e cos a = — 1, 
 
 IXC, 
 
 e sin a = . sin ft cos ft ; 
 
 fxc. 
 
 „ V'sWft Vsln'ft 
 M c/ nci 
 
 which gives the magnitude of e, and it was assumed to be positive 
 
HI.] A TREATISE ON DYNAMICS. 71 
 
 when 6 — a was considered as measured from the nearer vertex : a 
 may then be found without ambiguity from the two preceding 
 equations. 
 
 The constants which enter into equation (2) are then determined 
 and the equation to the orbit is completely known. 
 
 If we had not substituted for h' we should then have had 
 e cos a = 1, 
 
 e sm a = — - — . cot S ; 
 
 c ^k* c h' 
 
 and .-. e^ = -^ .cosec^/3-2.-^— + 1, 
 
 which is convenient when k and not V is known. V, Cj, /3 are 
 called the circumstances of projection. 
 
 The nature of the conic section will of course depend on the 
 magnitude of e. If e = 0, the orbit is a circle. That this may be 
 the case we must have 
 
 5 o -~ 2 t 1- 1 — 0. 
 
 To satisfy this equation we must have ft = -^ s (a condition which 
 is also evident independently) and V'^ = jxc^. 
 
 This condition agrees with that deduced previously for motion in 
 a circle. 
 
 The velocity of a body moving in a circle is often taken as a 
 standard by comparison with which the velocities of bodies in their 
 orbits are estimated. Thus the velocity of a body is sometimes 
 expressed by saying that it is q times that in a circle at the same 
 distance. The substitution of q^jxci for V^ will simplify the equa- 
 tions. It gives 
 
 e' = 5^sin^y^-2g*sin'/3+l. 
 
 The most important case is where e is less than unity, or the 
 orbit is elliptical. 
 
 Now e^ ^ (q- - 1 y sin- f3 + cos*^. 
 
 Hence that e may be less than unity q' must be less than 2, 
 or the velocity at every point is less than ^2 x that in a circle at the 
 same distance. 
 
72 A TREATISE ON DYNAMICS. [cHAP. 
 
 Let a be the semi-axis major of the ellipse ; then from equation (2) 
 
 >? 
 
 a h' 
 
 " V'sin'(3 \ IXC, ix'c,' ) 
 
 
 an important equation, -which shews that the axis-major of the orbit 
 is independent of the direction of projection, and depends only on 
 the distance and velocity. 
 
 If we write v for V, and - for c„ we have. 
 
 \r a)' 
 
 which gives the velocity at any distance in a simple and useful form. 
 
 a determines the position of the axis-major of the orbit: when 
 the body is at the extremity of the axis-major its motion is perpen- 
 dicular to the radius- vector : all places in any orbit where the 
 direction of the motion of the body is perpendicular to the radius- 
 vector are called " apsides," or, more commonly, " apses." a is the 
 angular distance of the apse from the line corresponding to 6 = 0, or, 
 as it is commonly called, the '^ longitude " of the apse. 
 
 6 is the "longitude " of the body ; e, the eccentricity, determines 
 the form of the orbit, and a, the semi-axis major, determines its 
 magnitude. 
 
 a, e and a are called the " elements " of the orbit ; when they are 
 known, the form, magnitude, and position of the orbit are completely 
 determined. 
 
 The first object of the direct problem, therefore, is to determine 
 the elements of the orbit from the circumstances of projection, or 
 other equivalent conditions. Sometimes it is required to determine 
 the circumstances of projection from certain given conditions which 
 the motion must satisfy. 
 
 We have seen that for the orbit to be an ellipse we must have e 
 less than unity, which requires that q be less than J2, or V^ less 
 than SjuCp 
 
 When q = ^2, 
 
 or r^=2)UCi, 
 
in.] A TREATISE ON DYNAMICS. 73 
 
 we have e = 1, and the orbit is a parabola. The equation then 
 becomes 
 
 u = ^,{l + cos(d-a)}, 
 
 h^ _ F"sin'/3 ^ 2 sin' /3 
 
 is the semi-latus-rectura of the parabola, a, as in the previous case, 
 
 is the longitude of the apse. When these are known the orbit is 
 
 completely determined. 
 
 The velocity at any distance r in a parabolic orbit is given by the 
 
 very simple equation 
 
 „ 2m 
 v = — . 
 r 
 
 If 7 be greater than ^^2, or F greater than J^fxc^^ we shall have 
 e greater than unity, and the orbit will be an hyperbola. The 
 elements in this case will be determined by a process similar to that 
 used in the elhpse. This case, however, is of comparatively small 
 importance. 
 
 We have at present only found the equation to the orbit, and its 
 nature, form, magnitude and position; and these, we have seen, 
 remain constant. In order that the problem may be completely 
 solved, we must moreover determine the position in the oi'bit which 
 the body occupies at any instant: that is, we must find u and Q, or 
 r and d as functions of t. 
 
 To do this we must integrate the equation 
 
 having given u = j^{l + e cos (6 — a)}, 
 
 J a 2 
 
 from Avhich -j- = j-^ {I + e cos (6 - a)}^ 
 
 This could be integrated accurately in finite terms, the solution, 
 however, which is thus obtained is in a form which is practically 
 useless ; as, however, in the cases in which it is generally required 
 e is a small quantity, the solution is obtained in the form of a series 
 ascending by powers of e, and may be carried to any degree of 
 accuracy. 
 
 We are able, without integrating the equation at all, to determine 
 the time of a complete revolution. For since h is twice the area 
 
74 A TREATISE ON DYNAMICS. [cHAP. 
 
 swept out in the unit of time^ if we divide twice the whole area of 
 the elHpse by h the quotient will be the time of a complete revolu- 
 tion. Calling this T, we have 
 
 h 
 
 h" a{\-e')' 
 
 T is called the ''period" or "periodic time" of the body. 
 
 In the time T the longitude of the body increases by 2 ir, but 
 this increase does not take place uniformly. If it did take place 
 uniformly, the increase of longitude in time t would be 
 
 y.STT, 
 
 which 
 
 •yi^' 
 
 n is generally used for the quantity */ — , and therefore the increase 
 
 of longitude in time t on this false supposition is n/; n\% called the 
 " mean motion" of the body ; it is useful in simplifying some of the 
 equations. 
 
 It is connected with the other constants that have been used by 
 the equations 
 
 We will now proceed to determine as a function of t. To 
 facilitate this certain auxiliary quantities are used which we will 
 now define. 
 
 In Astronomy (on which this part of the subject more particu- 
 larly bears) the name "anomaly" is given to certain angles that are 
 frequently used. 
 
 Let AVA' be the ellipse which the body describes; AQA' a circle 
 on the axis-major; S the focus coinciding with the center of force; 
 P the position of the particle at the time t. 
 
III.] 
 
 A TREATISE ON DYNAMICS. 
 
 75 
 
 Then A is the nearer apse and 
 A' is the farther apse. The angle 
 ASP which is what has been 
 written d-a is the angular distance 
 from the apse. It is called the 
 " true anomaly," We will denote 
 it by the letter v. 
 
 If the ordinate iV^Pbe produced 
 to meet the circle in Q, the angle 
 ^CQis called the "eccentric ano- 
 maly," and is denoted by the letter u. Also the angle which a body 
 moving with the mean motion 7i would describe while the real body 
 is moving from A to P, is called the ''mean anomaly/' and is denoted 
 by the letter J7i. 
 
 „- , , m area ASP 
 
 We have then — - = ^~^j^. 
 
 Stt area ot elapse 
 
 area ASQ 
 
 Now area ASQ, = Sivea ACQ- area SCO, 
 = I a^u -^ae . a sin u; 
 .'. m = u-e sin u ; 
 also, r = a- e . CN 
 
 = a (1 - e cos u) ; 
 _ SN a (cos u — e) 
 
 cos V - 
 
 SP a(l-ecosM) l-ecosw 
 
 
 1 - cos V 1 + e 1 - cos M 
 
 
 1 + cos u ~ 1 - e ' 1 + cos 7< ' 
 
 ■' 
 
 V /l+e ^ u 
 
 
 Now V = Q - a; 
 
 
 dv dd h 
 
 
 '*' dt~ dt~ r' 
 
 
 h 
 
 nO 
 
 rt^(l —e cos tif 
 = «(l-e7'(l-ecos?<)-' 
 
 . .)(1 +2e cos u + 3e' cos'' « + 4 e' cos' u + kc.) 
 
 (6cos'?<-l) + &c.}. 
 
76 A TREATISE ON DYNAMICS. [CHAP. 
 
 From the equation m= u-e sin u 
 we must express cosm, cos*?^, &c. as functions of m by means of 
 Lagrange's theorem, and transform them so as to involve only simple 
 powers of cosines of multiples of ?n. 
 
 XT ^"^ 
 
 Now -y- = n ; 
 dt 
 
 .-. 7)1 = nt + C. 
 We now have -7- expressed in a series of simple powers of cosines 
 
 of nt + C and its multiples, and can therefore find v at once by 
 integration. 
 
 If we only proceed as far as e^ it is not necessary to employ 
 Lagrange's theorem. We have 
 
 u=m + e sin u. 
 To a first approximation, u = 7«, where the error committed is of 
 the same order of magnitude as e. 
 
 Therefore to a second approximation 
 u = tn+ e sin tn ; 
 .'. cos u = COS (m + e sin ?«) 
 
 = COS m . COS (e sin 7n) — sin m . sin (e sin m) 
 
 = cosm-e sin^m 
 
 = cos m - -(1 - cos 2 m), 
 
 the error being of the order e^. 
 
 1 + cos 2m 
 
 Also, cos^ u = 
 
 2 
 1 + cos 2 m 
 
 with an error of the order e. 
 
 Therefore, substituting, we have 
 
 -7- = w {1 + 2 e cos 7« + - e^ cos 2 7«} 
 dt '^ 2 ' 
 
 = ??{! +2ecos(«i + C) + -e-cos2(M/ + C)}, 
 
 where the error is of the order e' ; 
 
 .-. v = nt + C'+ 2esin(w^+ C) + -e'sin2(w/4 C). 
 
 Now u = when wz = 0, that is, when nt + C = ; 
 .-. C'=C; 
 
III.] A TREATISE ON DYNAMICS. 77 
 
 .-. e-a = v =nt + C + 2e sin (nf + C) + |e' sin 2(n< + C). 
 
 It is customary to use tii instead of a, and instead of C to write 
 c-w, so that 
 
 0=«/ + 6 + 2esin (nt + e-'CT) + — sin 2 (nt + e- m); 
 
 6 is the true longitude of the body ; we observe that it consists of a 
 part nt + € which increases uniformly, together with a number of 
 terms which are sometimes positive and sometimes negative, but 
 which always lie between certain limits ; the periods in which they 
 go through all their values being different. 
 
 nt + e is called the "mean longitude." 
 
 e is the mean longitude when « = 0, it is called the " epoch," it 
 is the new constant that has been introduced in the integration ; it 
 is of course known when the longitude of the body at any one instant 
 is known. 
 
 w is the longitude of the apse, «/ + e — «t is the mean anomaly. 
 
 V - m or 6 -(nt + e) is sometimes called the "equation to the 
 center," and sometimes the "elliptic inequality." 
 
 It still remains to express r the distance of the body from the 
 center as a function of ^. 
 
 This is easily done ; we have 
 
 r = a(l — e cos u). 
 
 Substituting for cos w its approximate value, we have 
 
 r =a {1 -e COS TO + — (1- cos 2 7tt)} 
 
 = a {1 - e COS (72 / + e - w) + - [1 - COS 2 («/ + e - w)]}, 
 
 where the error is of the order e'. 
 
 We have thus obtained an approximation to the complete solution 
 of the problem. 
 
 By using Lagrange's Theorem, we might have carried this ap- 
 proximation to any degree of accuracy. 
 
 The four constants introduced in integration which constitute 
 the four elements of the orbit are cr, e, a, and e. 
 
 The first determines the position of the orbit, the second its form, 
 the third its magnitude, and the fourth the position of the body in it. 
 
78 A TREATISE ON DYNAMICS. [cHAP. 
 
 When a and e are known^ n and h are also known. 
 
 In solving the problem, we have considered ju to be a known 
 quantity, when this is not the case it is usual to consider n as the 
 quantity to be determined, since when n and a are both known, fx is 
 known from the equation /x - n^a^. 
 
 The conditions for determining these elements will appear under 
 very different forms. One very important case is, when we know 
 the values of Q corresponding to four different values of t, that is, the 
 longitude at four different times. 
 
 These will give us four equations, 
 
 01 = w/i + 6 + 2e sin {nti + e - w) + &c., 
 Q., = nt2 + e + &c., 
 
 03 = w/3 + e + &c, 
 
 04 = 71^4+6+ &c. 
 
 These equations enable us to determine e, n, e, and w ; and if fx 
 is known, we then know a. If (x is not known we may remark that 
 more values of d will not assist in determining it, since the above four 
 quantities are the only ones which enter into the equations. 
 
 If we had the four longitudes, and the distance or value of r at 
 any given instant we could also find a and thence ft. 
 
 Or we might have three longitudes and two distances, or these 
 conditions might be varied in any way. 
 
 It is however necessary to have one distance at least, and one 
 longitude at least in order to determine a and e. 
 
 If fx is given the distance is not necessary. 
 
 The method of approximation which we adopted in obtaining 
 the above equations is one with which the student will do well to 
 make himself familiar as early as possible. It will be continually 
 occurring in the higher parts of physical and plane Astronomy, the 
 same in principle but with variations in the form of applying it. 
 
 57. There is also another method which is largely used in the 
 Planetary Theory, which we will illustrate by the problem which 
 is now before us. Let us first, however, collect the principal 
 equations which connect the elements of the orbit and the circum- 
 stances of projection. 
 
III.] A TREATISE ON DYNAMICS. 79 
 
 ^^Fw/j_^rw^ 
 
 = £!!l'cosec^/3-2^+l (2) 
 
 h-^^s\nl3 (3) 
 
 r*sin/3cos/3 
 •""" ^c,-F-sin-/3 W 
 
 0(1-^) = ^ (S) 
 
 
 «^ = ^ (8) 
 
 The question which we propose to consider is the nature and 
 magnitude of the change Avhich would be produced in the elements 
 of the orbit by a small change in the circumstances of projection, 
 or of the intensity of the force, or the converse. 
 
 The manner of doing this will be best shewn by taking two or 
 three particular cases. 
 
 Suppose that the velocity of projection is slightly increased, the 
 distance and direction remaining unaltered. We see, by inspecting 
 the preceding equations, that any change in V will be accompanied 
 by a change in most or all of the elements, and consequently that 
 these elements are functions of V. 
 
 If therefore we suppose V to be increased to V+IV, Ave must 
 substitute V -^ cV for F in the above equations, in order to obtain 
 the new values of the elements. We may expand these new values 
 by Taylor's Theorem in a series ascending by powers of 2 F : and 
 if, as we suppose, S F is small, we shall obtain these new values very 
 approximately by neglecting all the terms of the series which con- 
 tain powers of D r higher than the first; so that the new value of a 
 will be very approximately 
 
 From equation (l), we have 
 
 IXCy VC / 
 
80 A TREATISE ON DYNAMICS. [cHAP. 
 
 This shews that an increase of the velocity at any point would 
 increase or decrease the eccentricity according as V^ is greater or 
 less than fxc ; that is, according as the velocity is greater or less than 
 that in a circle at the same distance. From equation (6) we see 
 
 that V^ is greater or less than fxc^, as Cj is greater or less than -; 
 
 that is, as the distance is less or greater than a. Now the distance 
 is a when the body is at the extremity of the axis-minor. Hence 
 then an increase of the velocity will be accompanied by an increase 
 or decrease of the eccentricity according as the body is at the time 
 on the nearer or farther side of the axis-minor. Exactly opposite 
 results would follow a diminution of the velocity. 
 Again, from equation (6) 
 
 1 a ^" 
 a /JL 
 
 a ju 
 
 •which shews that an increase of the velocity is always accompanied 
 by an increase of the axis-major. 
 From equation (4) we have 
 
 sec- a.da= -f-l — „/. ^^.7 . S r. 
 
 Since cos /3 is the only factor of this expression which can change 
 its sign, we see that an increase of the velocity will cause an increase 
 or decrease of the longitude of the apse according as /3 is less or 
 
 greater than - ; that is, according as the body is moving from the 
 
 nearer apse to the farther, or from the farther to the nearer. 
 
 As another example suppose V to remain unaltered, and the 
 angle /3 to be slightly increased. 
 
 We have from equation (l) 
 
 e.le = — A 2 y sin ^. cos /3. 2/3. 
 
 Here, since V" is less than S^c,, e will be increased or diminished 
 according as cos ft is negative or positive, that is, as ft is greater or 
 
 less than - . An exactly opposite result would follow a diminution 
 
 of /3 ; so that we see in all cases e is increased or diminished as ft 
 is made farther from, or nearer to, a right angle. 
 
III.] A TREATISE ON DYNAMICS. 81 
 
 From equation (6) we see that a is unaffected by a change in /3 ; 
 a result which we have already remarked. 
 From equation (4) we get 
 
 (/xc, - F^ sm^fty ' 
 
 which shews that the longitude of the apse will be increased or 
 decreased by an increase of /3, according as 
 
 H c, cos"* (3 + (V — fiCt) sin^ /3, 
 or, fx(aci- sin-/3) is positive or negative. 
 
 When the body is on the nearer side of the axis-minor ac, is 
 greater than unity, and therefore this is positive ; when the body is 
 very near the farther apse a c, - sin* /3 is negative ; the determination 
 of the point Avhere (ac, — sin* ft) changes sign is a geometrical problem 
 of little importance. We see, therefore, that by an increase of ft 
 which takes place near the nearer apse the longitude of the apse is 
 increased, and diminished by an increase of ft which takes place near 
 the farther apse. 
 
 These will be sufficient to illustrate the method, which goes by 
 the name of the ''Variation of Parameters." 
 
 We have selected these examples as themselves of importance. 
 The results should be carefully compared with the Corollaries to the 
 66th Proposition of the eleventh Section of the Principia. 
 
 We have dwelt at considerable length on the motion in an ellipse 
 because it forms the basis of the calculations of the motions of the 
 heavenly bodies. 
 
 58. These methods of expressing d and r as functions of t 
 entirely fail when the motion is in a parabola or hyperbola, since 
 the convergence of the series depends on e being less than unity. In 
 the case of a parabola, however, the equation can be easily in- 
 tegrated. 
 
 iL-'l^^ 1 
 
 de~ h " / ' {1+ cos (0 - a)P 
 
 h' J- a 
 
 Let 2/ be the latus-rectum of the parabola, then h' = fxl, 
 
 and TTi = T A / - • ( 1 + tan'^ ^ i — 
 
 fZ^ 4 V M \ 2 7 2 
 
 „ 1 //'A e-a 1 30- aN 
 
 C = -./-.(tan +- tan'— -— 1 . 
 
 2V n \ 2 3 2 J 
 
 From this equation 6 may be expressed in terms of /. 
 
'4' 
 
 82 A TREATISE ON DYNAMICS. [cHAP. 
 
 59. The method of integrating the equation 
 dhi P 
 
 
 dd' 
 
 -^"-7?^- 
 
 = 0, 
 
 which has been 
 
 adopted in the case of 
 
 
 is not generally applicable. 
 
 P=HU% 
 
 
 Suppose P = 
 
 = M w" ; we must proceed 
 
 as follows 
 
 
 d'u 
 
 ^•■"-- 
 
 ...(1) 
 
 Multiplying both sides by ^^-r?, > and integrating, we have 
 Let V be the velocity of the particle when u = c, then 
 
 It will be convenient to express V in terms of the velocity which 
 a body would acquire in moving from rest at an infinite distance to 
 
 a distance - from the center of force : to find this we have 
 c 
 
 d'-x _ p. 
 
 d¥^~l^" 
 
 
 0=C; 
 
 w - 1 
 Let V^qV,, then 
 
 
 (2) 
 
 This equation can always be integrated when ^=1. In this 
 
 case it becomes 
 
 de 
 
 du u J^nu"-^-{n-\)ie 
 
 Let 
 
 {n--[)h' 
 
III.] A TREATISE ON DYNAMICS. 83 
 
 dO 2 1 . 
 
 then -J- = — I "; , > 
 
 dy n-3 r/ Jf-l 
 
 2 
 .-. 6 - a = — ^ sec"' y ; 
 
 71-3 -^ 
 
 the general equation to the orbit described. 
 
 This method of solution fails when n = 3, and when n = 1 . 
 When n = 3 equation (2) becomes 
 d^_ 1 
 
 The integral of this equation will be logarithmic, algebraical, or 
 trigonometrical as j-s is greater than, equal to, or less than unity. 
 In the first case. 
 
 In this case the value of q can be either greater or less than unity. 
 In the second case we have j2=l, and the integral is 
 
 ' — ej^l' 
 or u = c Jq^-l . (d - a), 
 in this case q^ can never be less than unity, for 
 
 '^ ,jic'~ fx sin' /3 sin-/3* 
 
 Lastly, when ^ is less than unity, we have 
 
 dl_ 1 
 
 dti ' 
 
 h . , / h--ix u 
 
 . 6 -a= — - ^;= sin ^ ^ / —1-1, — -T . - 
 
 J/i'-fx V m(9--1) c 
 
 6—2 
 
84 A TREATISE ON DYNAMICS. [cHAP. 
 
 h" . . 
 
 in this case also q^ = — ^~2~1d is necessarily greater than unity. 
 
 We might have obtained these equations at once from the general 
 equation 
 
 d'u P 
 
 ad- h ti 
 
 which in this case becomes a linear equation 
 
 ru ( u \ 
 
 When n = \, we have 
 
 •'• ^''{(^y+«'}=2Mlog« + C, 
 F^=2)ulogc+ C; 
 
 We cannot generally perform the next integration. These cases 
 however are of little importance. In all these cases after deter- 
 mining the equation to the orbit we must find the position of the 
 
 rl ft 
 
 body in the orbit from the equation ~ =hu^. 
 
 60. It was stated in Article 56 that a point in an orbit where the 
 
 motion of the body is at right angles to the radius-vector is called an 
 
 apse, and the corresponding radius-vector is called the apsidal line, 
 
 or apsidal distance. From the nature of an apse we must have at 
 
 such points 
 
 dr ^ . ^ . dti 
 
 TH" = : and therefore ^^ = 0. 
 
 dd ' do 
 
 Let P = ixu", then the equation to the orbit is 
 d^u mm"~* „ 
 
 and at an apse we must have 
 
 -G 
 
III.] A TREATISE ON DYNAMICS. 85 
 
 This equation cannot have more than two changes of sign, and 
 therefore cannot have more than two positive roots : so that in an 
 orbit round a center of force varying as any power of the distance 
 there cannot be more than two different apsidal distances. 
 
 The angle between two consecutive apsidal distances is called the 
 apsidal angle. When the orbit does not differ much from a circle 
 this angle can be found approximately, without finding the equation 
 to the orbit. Let P= n u^(p{u), then the differential equation of the 
 orbit is 
 
 ^.+«-^.0(«) = o (1) 
 
 Now since the orbit is nearly circular we have 
 n = c + X, 
 where x is small compared with u ; 
 
 .-. 0(«<) = 0(c) + ^'(c). X nearly, 
 . d'u d'x 
 "^^° rf0^ = rf0- 
 therefore equation (l) becomes 
 
 %^{^--i^-¥{o)]x^c-^,.cp{c)=^0 ...(2) 
 
 also the velocity cannot differ much from that in a circle at the same 
 distance, so that 
 
 Therefore the integral of equation (2) is 
 x = Aco%{kd + B) + C, 
 
 where k 
 
 =y'-^-"^4{^*w-4^ 
 
 dx 
 
 .'. j^ = - A k sin (kd + B). 
 
 Let 0j, 6.2, 08, &c. be consecutive values of 6 for which 
 ^=0, then 
 
 kd, + Br^n-n^ 
 
 
 ke^ + B = {ii + \)'K, 
 
 
 k0s + 5 = (n + 2)7r, 
 
 
 &c. ; 
 
 
 0, _ 0,= 0,-0, = &C. 
 
 ^k' 
 
 which gives the apsidal angle approximately. 
 
86 A TREATISE ON DYNAMICS. [cHAP. 
 
 For example^ let P = fx u' + — where fx' is small : here 
 
 0(«) = 
 
 
 .'.cp{c) = 
 
 -^ 
 
 <P'ic)- 
 
 
 ^j^j_c.0'(c)_^c^ + V 
 
 (p{c) fXC' + ^' 
 
 .'. the apsidal angle = tt . . / -^ ; 
 
 61. The equations 
 
 P^;a,2/^'« 
 
 
 enable us at once to solve the inverse problem of finding what must 
 be the law of force in order that the particle may describe a given 
 orbit. For example, let it be required to find the law of force that 
 the orbit may be the equiangular spiral, whose equation is 
 
 e cot < 
 
 
 r = ae , 
 
 
 or « = i.e-^^°t«; 
 a 
 
 
 , d'u 1 , ~Qf 
 here -ttt-, = - • cot'a . e 
 do'- a 
 
 
 = u . cot* a ; 
 
 
 ...P = ;,v(S..) 
 
 
 = A' cosec^ a . u^, 
 
 or thus, 
 
 in the equiangular spiral, 
 
 
 p = r sin a; 
 
 
 dp . 
 dr 
 
 '. P = — .-/- = . „ . -r , as before. 
 jr dr siTVa r^ 
 
IV.] A TREATISE ON DYNAMICS. 87 
 
 CHAPTER IV. 
 
 62. The integration of the equations 
 
 in the cases where the motion is not, as we have hitherto supposed 
 it, in one plane, is in general attended with great difficulties and can 
 rarely be effected except approximately. As moreover no principles 
 are involved in the solution of the equations in this case which have 
 not been exemplified in the cases of motion in one plane, it is 
 unnecessary to give any of the few instances in which the equations 
 can be completely solved. There are however a few general pro- 
 perties of the motion which can be readily exhibited. 
 
 The resultant of the forces X, Y, Z acts in the osculating plane 
 of the body's path. 
 
 This may be seen at once from general considerations. 
 
 The body at any instant is moving along the tangent to its path 
 at that instant, and the deflection from the tangent must take place 
 in the direction of the resultant force that acts on the particle at that 
 point ; but the plane passing through the tangent and the direction 
 of the deflection from the tangent is the osculating plane, which 
 therefore passes through the direction of the resultant force. 
 
 This may also be easily deduced from the equations. 
 
 The direction cosines of the normal to the osculating plane are 
 proportional to 
 
 (Py dz d^zdy d'z dx d'xdz . d''x dy d^y dx 
 d7Tt~'d?~di' Wdi ~ dF dt Jt^ ~di~ dp di ' 
 
 Or, considering the equations of motion, to 
 
 y^^_Z$, Z^^-X^, and X^J'-Y^, 
 dt dt ' dt dt ' dt dl ' 
 
88 A TREATISE ON DYNAMICS. [cHAP. 
 
 and the direction cosines of the resultant force at the point (x, 
 y, z) are 
 
 and 
 
 JX'-¥ Y^^ Z' JX'+ Y'+Z' JX'+ F'H- Z' ' 
 
 and if 6 be the angle between the direction of the resultant force and 
 the normal to the osculating plane, the numerator of cos 6 is zero, or 
 is a right angle ; that is, the resultant acts in the osculating plane. 
 
 Again, from the equations of motion we have 
 
 d2 
 
 \df dt de dt dedtj~ di dt dt 
 
 or since (^^y=(J)\(g)V(^ 
 
 ^dz 
 ^dt 
 
 at ds ds ds 
 
 The right hand side of this equation is the sum of the resolved 
 parts of the forces X, F, Z along the tangent, and this is the only 
 part that affects the velocity : when this is zero, or the whole re- 
 sultant force acts always in the normal plane, the velocity will be 
 unaltered thoughout. 
 
 When the expressions for the forces X, Y, Z are such as to make 
 Xdx + Ydy + Zdz a perfect differential of ;r, y, z considered as three 
 independent variables, that is, when they satisfy the conditions 
 dXdY dYdZ dX_dZ 
 dy ~ dx ' dz ~ dy' dz~ dx' 
 
 let F{x, y, z) + C=^j{Xdx + Ydy + Zdz), 
 then Mv^ = F {x, y, z) + C, 
 from which it appears that 
 
 F {x, y, z) = const, 
 represents a system of surfaces each of which has the property that 
 the body always crosses it with the same velocity : and if any two of 
 them be taken, as 
 
 F{x,y,z) = C,, 
 
 F{x,y,z) = C„ 
 
 the change of velocity in passing from one to the other is inde- 
 pendent of the points in the two surfaces, and of the path pursued 
 by the particle between them ; for if v, and u, be the velocities at the 
 two surfaces. 
 
IV.] 
 
 A TREATISE ON DYNAMICS. 
 
 89 
 
 Mvi = a+c, 
 
 so that M (v,' - v/) = C2 - C„ 
 in which neither x, y^ 2 nor any relation between x, y, and z, appear. 
 
 63. The three equations may be transformed to polar co-ordinates 
 as follows : 
 
 Let P be the position of 
 the particle, 
 
 OM = x; 
 MN = y, 
 NP = 2. 
 
 OP = r, 
 
 ON=p, 
 MON = d. 
 
 M 
 
 Let P', T' and <S" be the resolved parts of the forces on the par- 
 ticle in direction iVO, perpendicular to NO, and in PlSl respectively, 
 
 so that M^ = -P'--r'-^, 
 at p p 
 
 dr p p 
 
 (1) 
 (2) 
 (3). 
 
 
 
 
 
 M- 
 
 
 S'; 
 
 puttin 
 
 g^. 
 
 T, 
 
 ' f- Tl 
 
 T 
 ' Tl' 
 
 S' 
 
 TV 
 
 
 
 
 
 d'x 
 di' 
 
 P 
 
 -T^--, 
 
 
 P 
 
 , 
 
 
 
 
 dt' 
 
 d'z 
 dl'~ 
 
 p 
 -S 
 
 -r^, ( 
 
 
 p 
 ( 
 
 
 
 From 
 
 (1) and 
 
 (2) 
 
 
 d'x 
 
 = Tp. 
 
 
 
 
 Lei 
 
 ' "^ dt 
 
 dx 
 
 = h; 
 
 
 
 
 
 ^ dh 
 
 -Tp, 
 
90 A TREATISE ON DYNAMICS. [cHAP. 
 
 and h = p^ — ; 
 
 putting u for - 
 P 
 
 
 A^ = V.o|I^, (4) 
 
 = — h (cos 6 'j^ + 71 sin 6), 
 
 = - COS — -7^ - T Sin - A^?r cos ( -^^ + u). 
 
 ■ But^ = -Pcos0-rsm0; 
 
 ^ P_ T du_ 
 
 •'• dd''^''~h'u''^¥e de~^' 
 
 or, substituting for ^^ from (4), 
 
 P T^ Jm 
 
 ^""""TTT^^^ ^^ 
 
 and -73 = -} — 5 = , (o) 
 
 Again, let tan PON= s. 
 
 Then 2 = ps = - , 
 
 drz_ 
 dF—^- 
 Combining these two with equations (5) and (6), we get 
 S-Ps T du 
 
 d's Ku^ ^ h;'ii^ dd ^ . , 
 
 77^» + *+ TTir—'^ (7) 
 
 1 +2 
 
 fTdl 
 
IV.] A TREATISE ON DYNAMICS. 91 
 
 These equations though perfectly general are of little use except 
 when P, T and S are of particular forms. Their principal applica- 
 tion is in determining the motion of the moon about the earth when 
 acted on by the disturbing force of the sun. In this case they are 
 integrated by a series of approximations. 
 
 64. When the forces X, F, Z depend on the velocity of the par- 
 ticle as well as its position, the integration of the equations of motion 
 can seldom be completely effected. It frequently happens, however, 
 that they can be put into a form which will enable us, by means of 
 laborious calculation, to determine many points connected with the 
 motion to any required degree of approximation. 
 
 Let us take for an example the motion of a body in the air acted 
 on by gravity. The resistance of the air varies as the square of the 
 velocity of the body, so that the equations of motion are 
 
 de- ^'dS^ ^ .- ^rr^ 
 
 
 These may be written 
 
 d^x , dx ds ^ .. 
 
 j^ + A -J- -J- = 0, (1) 
 
 dt^ dt dt ^ ^ 
 
 g-4ii-^=« (^) 
 
 The integral of equation (1) is :^C 
 
 dx ^ _k. 
 -J- = Ce-*'. 
 
 dt 
 
 Let V be the initial velocity of the body, a the angle its direction 
 makes with the horizon, then 
 
 ^=rcosa6-*' (3) 
 
 Let p be written for -p, then -^=p^-f; substituting this in 
 equation (2), and reducing by means of (l), we have 
 
 (4) # 
 
 , . .i-. '" dx dp 
 
 dt dt 
 
 d^. ^ " cos* a 
 
 kh ' Now, 7rT7=^ 
 
 ^ 
 
 '^ ^ dx F^cos^a dx' 
 
92 A TREATISE ON DYNAMICS. [CHAP. 
 
 The integral of this equation is 
 
 pVTT7 + log(p + VTT7)=y-p,,|^^6^^...(5) 
 
 where 7 is a constant introduced by integration, and is given by the 
 equation 
 
 tan a sec a + log (tan a + sec a) = 7 - tttb^—t- • 
 From equations (4) and (5) 
 
 <^P y-pJl^'-logip + JT^'Y 
 
 .-. //^-y- -P ■ (7) 
 
 and Jkg^- = , , _ . ; (8) 
 
 these equations cannot be integrated in finite terms ; they give, how- 
 ever, the values o? x, y and t corresponding to any value of/>, in the 
 form of a definite integral, whose value may be found to any degree 
 of approximation by the ordinary methods applicable in such cases. 
 Thus any number of points in the path of the body, and the respec- 
 tive times of reaching those points may be determined. The velocity 
 corresponding to any value of p is given by the equation 
 
 .■4- ,,^':^,,.,^^ (9) 
 
 T- 
 
 pjl+ f- - log (p + ^1 +/) 
 
 When p=0 the body is at the highest point of its course, and at 
 that time 
 
 yk 
 Equation (4-) may be written 
 
 dx^ F'cos'a ' 
 
 which is the differential equation to the path of the body. We may 
 shew that this curve has a vertical asymptote. Since p becomes 
 negative and continues to increase in actual magnitude, let pi be a 
 very great value of p, and ^, the corresponding vahie of x; then in 
 equation (6), neglecting all powers of p except the highest, we have 
 approximately for values of p greater than pi 
 J dx 1 
 dp p" 
 
IV.] A TREATISE ON DYNAMICS. 
 
 KX = KX, -\ : 
 
 Pi P 
 
 which shews that x is finite when j) = -<x- 
 
 dp 
 
 '-if 
 
 tan a 
 
 Hence then - y / . , is finite 
 
 P \/l +/- log (p +Jl +/) 
 
 let this equal a, then x is always less than a, and approaches a as a 
 limit when p increases indefinitely ; a line parallel to the axis of ^ at 
 a distance a from the origin is therefore an asymptote to the curve. 
 
 65. Let us take as another example the case of a body describing 
 a nearly circular orbit round a center of force varying inversely as 
 the square of the distance, in a resisting medium of very small 
 density. 
 
 The polar equations of motion are 
 JP^ t du 
 d'u h;'u^ h.^ii" dd ^ 
 
 Je^'-'' 7[Tdr=''^ (^) 
 
 1 + 2 I ^2-^ 
 
 ^:-."V^ ■■■(^) 
 
 In this case if Arw* is the resistance, k is very small, and 
 
 --y"H^)'m « 
 
 2 
 
 Let -A = «^ 7-3 = ^h then 
 hi' K^ 
 
 T ka* / , /duy/dds,' , . 
 
 p r_ du _ 
 
 and equation (1) becomes 
 
 d^u « ^ /^ 
 
 'Jhru' 
 
 Neglecting small quantities of the first order, we have 
 dd 
 
2 
 
 94 A TREATISE ON DYNAMICS. [cHAP. 
 
 Substituting these values and neglecting small quantities of the 
 second order^ 
 
 T _ k^ 
 h^u^ ~ a ' 
 fTdd _ kd 
 •'■ j Vm^ ■" a ' 
 
 -y-^+u-a-2kd = ; 
 do 
 
 .'. u=a{l + — — + e cos (0 - a)], 
 
 where e is a small quantity, the orbit being supposed nearly circular ; 
 
 ^ = n{l + ^+2ecos(0-a)} (7) 
 
 Substituting these values and neglecting small quantities of the 
 third order, 
 
 ,03 = U -— ecosfU- a)\ ; 
 
 d^u 
 
 jj^ + u - a -2kd + 2ke sm (0-a) = O; 
 
 f, 2A:0 .. . kd .. ^, 
 
 .-. u = a {1 + + e cos (0 - a) + — e cos {Q - a)], 
 
 _ = „{!+__ +___ + 2ecosC0-a)+-^ecos(9-a) 
 
 k 
 + - e sin (0 - a) 4 e^ cos^ (0 - a)}. 
 
 By repeating the process the solution might be carried to a 
 higher degree of approximation; the labour, however, increases 
 very rapidly. This example has been selected to exhibit the use of 
 the equations of Art. 53 ; and also as an example of the method of 
 solution by successive approximation. Since terms multiplied by 
 occur in the expression for u, this expression will cease to be an 
 approximation at all when Q becomes large. 
 
 To express in terms of/, we must proceed in a similar manner: 
 
 <^^ a , 
 
 ~r,-n'> •'• V — nt + €. 
 at 
 
 Substituting this value of Q in equation (7) 
 
 —=n {I + — .{lit ■\-e) + 2ecos{nt+ e-a)}; 
 
IV.] A TREATISE ON DYNAMICS. 95 
 
 3k 
 .'. e = nt + € + -— (fit- + 2€t) + 2e sin (7it + € - a) 
 
 correctly to the first order of small quantities : by substituting this 
 
 dd 
 
 dt 
 
 value of d in the next value of -r- and integrating, we might obtain 
 
 a more approximate value of 0. 
 
 QQ. In the problems which have been hitherto considered the 
 forces which acted on the particle were known in terms of the 
 position, velocity, and direction of motion of the particle, which was 
 perfectly free to move as these forces would cause it to move; in 
 other words, in the cases in which we have integrated the equations 
 
 d^x d^y d^z „ 
 
 '^l[f=^' "^7?=^' "^1?-=^' 
 
 X, Y, and Z have been given functions of x, y, z and their first 
 differential coefficients. And j, y, and z have been subject to no 
 other relations than those furnished by the above equations. In 
 this case we have three equations which are theoretically sufficient 
 to determine the three unknown quantities x, y, z in terms of ^ ; or 
 by eliminating t to give two equations between x, y, and z. 
 
 There is, however, an extensive class of problems in which X, 
 Y, and Z contain, in addition to given forces, unknown forces 
 arising from geometrical conditions to which the motion is subject, 
 such, for instance, as the unknown tension of a string, the unknown 
 reaction of some curve, or surface. These forces will enter as 
 unknown quantities in the three equations of motion, but however 
 many unknown quantities of this sort may appear, there will always 
 be just so many additional equations expressing these geometrical 
 relations. 
 
 The methods to be pursued in cases of this sort will of course 
 depend on the particular geometrical conditions imposed on the 
 particle, they will, however, be generally very similar to those 
 pursued in other cases. The principal problems of this class are 
 those in which a particle is constrained to move on a particular 
 surface, or some particular curve line. We will first prove some 
 properties, and deduce some equations which are common to all 
 problems of this sort, and, at the same time, point out the methods 
 to be pursued in particular cases. 
 
 Let us first consider the case where the motion is in one plane. 
 
96 
 
 A TREATISE ON DYNAMICS. 
 
 [chap. 
 
 67. Let a particle be constrained to move on a smooth plane 
 curve and be acted on by any given forces in the plane of the 
 curve. 
 
 By the term smooth we understand that the curve is incapable of 
 exercising any reaction except in the direction of the normal. 
 
 Let y=f{x) (1) 
 
 be the equation to the curve ; X, Y the resolved parts parallel to 
 the axes of the forces which act on the particle at the time t. First 
 let these forces be functions of x, 
 y and constant quantities only ; 
 R the reaction of the curve, A 
 any fixed point in the curve, P 
 the position of the particle at 
 the time t, 
 
 AP = s, PTN=e. 
 
 The equations of motion are 
 (Fx 
 
 d'y 
 or since sin 6 ■■ 
 
 X-Rsin 
 
 Y+Rcos 0, 
 cos 6 = 
 
 dy 
 ds 
 
 dx 
 d~s' 
 
 These equations may be written 
 d'x ^ 
 
 ds 
 
 Y+R 
 
 dt 
 
 y=f{^) 
 
 Eliminating R from (£) and (3) we have 
 
 ( dxd^x dyd^y) ^^dx 
 "^{Tsdt'^TsTf 
 
 dxd'x 
 
 •(2) 
 .(3) 
 •(1) 
 
 ds ds 
 
 dtdt' dtdt' f dt dt 
 
 (4) 
 
 When X and Y are such functions of x and y that Xdx + Ydy is 
 the differential of some function F(a;, y) of a: and y considered as inde- 
 pendent, that is, when X and Y satisfy the condition 
 dXdY 
 dy dx ' 
 we may integrate (4) without reference to (1). 
 
IV.] A TREATISE ON DYNAMICS. 97 
 
 ^----m-m^m- 
 
 That equation may be written 
 
 dv ds d's d.F(x,y) 
 
 '"'Tr'^Ttdi^^—dt—'- 
 
 The integral of which is 
 
 mv'' = 2F{x,y) + C. 
 
 Let Vj, Xj,_yj, be corresponding values of v,x,y, then 
 
 mv,'' = 2F{x„y,) + C, 
 
 and .-. vi{v^ - v^) = 2F{x,y) -2F(x,, y,) (5) 
 
 This equation shews that the change of velocity in passing from 
 the point {x^y^ to the point {xy) is independent of the form of the 
 curve along which the particle has moved, and by a reference to ' 
 
 Art. 50 it will be seen that this change is the same as if the body had 
 been free and had moved from the one point to the other under the 
 action of the forces X and Y. 
 
 AVhen X and Y do not satisfy the above condition, this is not the 
 case. In that case we may integrate (4) by eliminating x or y from 
 the right-hand side by means of equation (1). These cases, however, 
 seldom occur, and are of little importance. 
 
 Equation (4) may be put under the form, 
 
 d^s .^dx trdy 
 
 m-r^= X-T-+Y -f-, 
 
 dr ds ds 
 
 d^s 
 or m -T73 = X cos + F sin d. 
 
 The right-hand side of this equation is the" resolved part of the 
 forces X, Y in the direction of the tangent: calling this T the 
 equation becomes 
 
 "'^-'T (6) />7^_ . 
 
 This form of the equation is useful in cases where T can be expressed J^ 
 
 easily as a function of s. // *-» ^' 
 
 Again, from equation (2) and (3) we have C 
 
 /f^ 
 
 dx d^y dyd^x\_^dx -ydy j^ds 
 Ttd?~Tt dp) Tt~ dt'^ df.' 
 
 r> V • a V a dtjdxd^y dyd^x) 
 7?=Asm0-Fcos0 + ..^|^-|--^^.| 
 
A TREATISE ON DYNAMICS. 
 
 [chap. 
 
 Now if p is the radius of curvature at the point P 
 \dt) 
 
 " dx d'y dy d^x ' 
 TttP~dt~df 
 
 .'. R = Xs\ne- rcos0 + 
 
 tnfds\' 
 P\dtj' 
 
 The first terms on the right-hand side of this equation are the 
 resolved parts of the forces X and Y along the normal : if we call 
 the sum of these N^ the equation becomes 
 
 R + N-. 
 
 mv 
 P 
 
 (7) 
 
 In this equation p is the absolute length of the radius of curva- 
 ture, and is always positive ; R is the pressure exerted by the curve 
 on the particle in a direction towards the centre of curvature, and N 
 is estimated in the same direction. 
 
 We have supposed that the curve is capable of exerting a pressure 
 on the particle in direction of the normal, either outwards or inwards, 
 as is the case when a particle is enclosed in a small tube ; if, how- 
 ever, the particle moves on the curve, R is restricted to being only 
 positive or only negative, according as the particle moves on the 
 concave or convex side of the curve ; and in either of these cases 
 when R becomes zero and changes sign, at that point the particle 
 leaves the curve and the motion becomes that of a free particle. 
 
 68. As an example, let us 
 take the case of a body moving 
 on a smooth curve under the 
 action of gravity. 
 
 Let the lowest point of 
 the curve be taken as origin, 
 and the axis of x be horizontal, 
 and let OP = s. The equations 
 of motion will be 
 
 (Fx 
 dt^' 
 
 R 
 
 d^u „ dx 
 
 •(2) 
 ,(3) 
 
IV.] A TREATISE ON DYNAMICS. 90 
 
 Proceeding here as in the general case, ^ve have 
 ^ ds d^s ^ dy 
 
 ^""didT^-'^'^'^dt'* 
 
 .: mv^ =C- ^mgy. 
 
 Let Vj be the vakie of v when y =y^, then we have 
 
 m if -vX) = 2 mg (^, -y), 
 
 or v''^v\ = 2g(yi-y). 
 
 This equation shews that the change of velocity will be the same as 
 
 if the body had moved through the same vertical height freely. It 
 
 will be useful to bear this result in mind. 
 
 It is sometimes convenient to put the preceding equation under 
 the form 
 
 d^s _ dy 
 de~~^Ts' 
 
 This is useful when -— can be expressed easily as a function of .y. 
 
 When this is the case this equation gives at once the motion along 
 the curve in terms of the time. 
 
 To find the pressure exercised by the curve, we have 
 dx v^ 
 p' 
 
 Suppqse the body to fall from rest at a point where y = h, 
 the equation 
 
 v'~v\ = 2g{y,-y) 
 
 becomes v'^ = 2g {h -y) ; 
 
 and if ?^ be the velocity at the lowest point 
 
 u'^2gk, 
 the body will move on and ascend the other side of the curve, the 
 velocity at any point being still given by the equation 
 
 v^=2g{h~y), 
 
 which will become zero when y = k. Or, whatever the form of the 
 curve, the body will rise to the same height as that from which it 
 started. 
 
 It is easily seen that the body will oscillate, the points of rest 
 being always at the same height above the horizontal line. 
 
 7-2 
 
 ^ = '"Sds 
 
100 A TREATISE ON DYNAMICS. [cHAP. 
 
 69. Let the curve be an inverted cycloid, whose equation is 
 x = a vers"' - + ./s ay —y^. 
 
 From which we have -7- = a. / — '> 
 
 dy \ y 
 
 ds _ /27i 
 " Ty~ S J' 
 
 from which we have s = zj^ay; 
 
 ds 4>a 
 
 Substituting this in the equation 
 
 d^s dy 
 
 'd?^~^'ts' 
 
 , d"s £rs 
 
 we have -7T2 + 1- = 0. 
 dr 4-a 
 
 The integral of this equation is 
 
 and.-4^ = -^y£-.si„(yA,^B). 
 
 Suppose the body to fall from rest from a point where s = Si, we 
 have then 
 
 Si = A cos B, 
 
 = -Ax/~ sinB 
 
 .-. 5 = 0, A = s„ 
 
 and,., cos yZ 
 
 V 4a 
 
 when s = 0, we must have 
 
 Hence the time of reaching the lowest point is tt x/ ~ > 
 
 and the whole time from rest to rest again is 2 tt a/ - . These are 
 both independent of the length s^. 
 
IV.] A TKEATISE ON DYNAMICS. 101 
 
 Hence we see that from whatever point the body falls it will 
 always reach the lowest point in the same time. On this account 
 the cycloid is called the " Tautochronous curve." 
 
 The equation '^=.-s, ^ f^ sin ^^ t 
 
 gives the velocity at any time; and since we know the position at 
 any time, Ave can find the velocity in any position. It may however 
 be more readily found from the equation 
 
 for we have s^^ = 8a h. 
 
 ay. 
 
 »'=lifr'-"> 
 
 The pressure on the curve is given by the equation 
 
 R. 
 
 dx mv^ 
 
 Practically it is impossible to obtain a perfectly smooth curve ; 
 the properties of the evolute, however, enable us to produce the 
 same dynamical effect. 
 
 Suppose AP to be the curve in 
 which it is required that the particle 
 should oscillate, and that QB is its 
 evolute. If a string be unwrapped 
 from BQ, its extremity will trace out 
 the curve PA, and since the only 
 dynamical effect of the curve PA is to 
 exercise a resistance in the direction 
 PQ of its normal, this effect will be 
 equally produced by the string PQ 
 exercising a tension ; and therefore the 
 dynamical circumstances of the body will be the same when moving 
 on the curve, and when attached to the string. 
 
 Now, in the case of the cycloid, the evolute is two semi-cycloids 
 in the position in the figure. 
 
102 
 
 A TREATISE ON DYNAMICS. 
 
 [chap. 
 
 Hence, if a string OP of length 4a is fastened at 0, and the body 
 P swings backwards and forwards so that the string wraps and 
 O 
 
 unwraps itself on the curves OA^ OB, the body P will describe the 
 curve AB in the manner we have just investigated. Such an 
 instrument is called a cycloidal pendulum. 
 
 70. Let us now consider the motion of a body in a circular 
 arc. The equation to the circle is 
 
 dx _a—y _ 
 dy~~x~' 
 ds a a 
 
 from which we have 
 
 dy 
 
 72^ 
 
 .-^l. 
 
 .'. y — a vers - . 
 
 dy . s 
 -7^ = sm - . 
 ds a 
 
 Hence the equation becomes 
 
 d's . s 
 
 dt^ = -S''''a' 
 
 .•.(^jy=2«gcos-%C. 
 
 If Si be the value of s when the body is at rest, we have 
 
 = 2a^cos- + C ; 
 
 (^;J=2a^(cos^-cos5). 
 
IV.] A TREATISE ON DYNAMICS. 103 
 
 We might also have obtained the velocity from the equation 
 ^ ds d^s ^ dy 
 
 '''"TtdW=-^'"STt' 
 
 from which l-j-j =2g{h-i/). 
 
 Neither of these equations can be integrated again in finite terms. 
 The time of reaching the lowest point may, however, be found from 
 them in a series which converges very rapidly when h is small. 
 
 If we require the time to a first approximation only, we can find 
 it at once from the equation 
 
 d's . s 
 
 de = -S''''a' 
 which is to a first approximation 
 
 d'j g 
 dt' a' 
 
 '^i- 
 
 and the time of a small oscillation will be t . / - , the same as in a 
 
 V g' 
 
 cycloid where the length of string is a. 
 
 When the oscillations are not small though we cannot find the 
 position at any time, we know the velocity in any position from 
 the equation 
 
 v' = 2g(h~i/). 
 
 [£21 
 
 be the 
 
 velocity 
 
 at the lowest point 
 
 and v"^ — u^ — 2gy> 
 
 If d be the 
 
 angular 
 
 distance from the lowest point. 
 
 
 
 
 t/ = a - a cos ; 
 
 
 
 
 .-. w* = ?r - 2 a^ + 2 ag cos Q. 
 
 
 
 Also, It = m — + mg -j- 
 
 
 
 
 = m — h m g cos Q 
 
 
 
 
 „2 
 
 = m 'Zmg + 3 mg cos 6. 
 
104 A TREATISE ON DYNAMICS. [cHAP. 
 
 Hence at the lowest point 
 
 K = m — h ms, 
 
 at highest point 
 
 Jti = ?)i 5 nig, 
 
 when the string is horizontal 
 
 R = m 2tng. 
 
 a 
 
 If R becomes zero and changes its sign, the body will leave the 
 curve. Now if ti^ is greater than 5 ag we shall never have R = 0, 
 since the least value of R is 
 
 (^=^)- 
 
 Also, the least value of v'^ is u^—^ag, so that the particle will 
 never come to rest, but will continue moving round and round. 
 
 If u^ = Sag we shall have jR = at the highest point, but it will 
 not change sign and therefore the body will not leave the curve. 
 Also V will never become zero, and therefore the body will move 
 round and round. If however u^ is less than Sag, R will become 
 zero before the body reaches the highest point, and the correspond- 
 ing value of 6 will be given by the equation 
 
 „ u^-2ag 
 
 cos = ^ . 
 
 Sag 
 
 When u^ is greater than 2ag this value of cos 6 is negative; and 
 as 6 increases, cos 6 will increase negatively, so that R would change 
 sign. The particle will leave the curve therefore at this point, and 
 its motion will be that of a body projected freely. 
 
 That it will reach this point is shewn by the equation 
 •- = u^ -2ag + 2ag cos 6, 
 which gives a greater value of 6 for the point at which v would 
 
 1 n u'^ — 2ag 
 
 vanish, namely, cos (^ = ° . 
 
 2ag 
 
 If u'^ = 2ag the values of 6, for which R = and v = are coin- 
 cident, 6 therefore will not increase, and R will not become negative. 
 Hence in this case the body will not leave the curve. If ii^ is less 
 than 2ag, we have v=0 for a smaller value of 6 than that which 
 would make R = 0, R therefore will never vanish. 
 
 We have dwelt on this case at considerable length, not from any 
 importance in the question itself; but because it exhibits very clearly 
 
IV.] A TREATISE ON DYNAMICS. 105 
 
 the mode of interpreting the equations to be adopted in all cases of 
 this sort. 
 
 We have two quantities R and v^, each a function of the angular 
 distance Q from the bottom, and each from its nature incapable of 
 becoming negative; the angle Q will go on increasing till one or 
 both become zero; and some change will take place in the motion 
 when either of these happens. If ?;^ = before R = 0, the motion 
 will be continuous, but Q will have attained its maximum and will 
 begin to diminish. If iv := first and an increase of would make 
 R negative there will be a discontinuity in the motion. 
 
 If no value of Q makes either R = or v = 0, the angle 6 will go 
 on increasing. 
 
 These remarks as far as the detail is concerned apply only to 
 this case, but are sufficiently general to exhibit the manner of inter- 
 preting the equations in other cases. 
 
 71. We will now consider the case where the motion is on a 
 curve of double curvature. The reaction of the curve will in this 
 case be in the normal plane, but we cannot assign, a priori, in what 
 direction in that plane. 
 
 Let R he the reaction, I, m, n the direction -cosines of the line in 
 which it acts. 
 
 Then the equations of motion are 
 
 (1) 
 
 M'^, = Y+Rm, 
 
 I, m, n are connected by the equation 
 
 l-+m!' + ii'=\ (2) 
 
 and also by the equation expressing that the direction of R is per- 
 pendicular to the tangent. This equation is 
 
 jdx dy dz ^ ,. 
 
 These five equations together with the two equations to the curve 
 are sufficient to determine x, y, z, /, m, n, and R at any instant. 
 Eliminating R from equations (1) by means of (3) we have 
 
106 A TREATISE ON DYNAMICS. [CHAP. 
 
 If Xdx + Ydy +Zdz\s a. perfect differential of some function of 
 X, y^ z considered as independent variables, that is, if X, Y, Z satisfy 
 the three equations 
 
 dX^clY dX^^dZ clY^dZ •- 
 dy ~ dx ' dz dx ' dz ~ dy ' 
 equation (4) can be integrated without making use of the relation 
 between a;, y and z given by the equations to the curve. 
 
 Let this function be M.F(x, y, z) then we shall have 
 v''^C + 2F(x,y, z), 
 and v" ~ Vi^ = 2 F (x, y, z)-2F (x^, y^, Si), 
 or the change of velocity in passing from the point {_X\y^ 2,) to the 
 point {xyz) will depend only on the positions of those points, and 
 not on the nature of the curve between them : and this change of 
 velocity will be the same as would have taken place if the particle 
 had moved freely from one point to the other. 
 
 We also see that the velocity is the same at all points at which 
 the value of F (x, y, z) is the same, or 
 
 F{x,y,z)=C 
 is the equation to a surface through which the particle will pass with 
 the same velocity at whatever point of the surface it arrives, and by 
 whatever path it has travelled, provided only that it started from 
 the surface F {x, y, z) ^ Ci with the same velocity i\. 
 
 Or the change of velocity in passing from any surface 
 F(x,y,z)=C, 
 to any surface F {x, y, z) = C^ 
 
 is the same, whatever the path between those surfaces. 
 
 U Xdx + Ydy + Zdz is not a perfect differential of three inde- 
 pendent variables, we cannot perform the integration without intro- 
 ducing the relations between x, y and z given by the equations to the 
 curve ; these equations will therefore modify the form of expression 
 for the velocity, and the preceding results will not follow. 
 
 Equation (4) may also be put into the form 
 
 dt^ ds ds ds 
 
 where T is the sum of the resolved parts in direction of the tangent 
 of the forces X, Y, Z. 
 
 In cases where this resolved part can be expressed easily in terms 
 of s this will give the motion along the curve at once. In the case 
 
IV.] A TREATISE ON DYNAMICS. 107 
 
 where no forces act we see that the velocity is constant. In this 
 case we can easily shew that the whole reaction is in the osculating 
 plane of the curve. The equations of motion in that case are 
 
 , dx dy dz ^ 
 I -J- + 711 -f- + n -r = 0. 
 as ds ds 
 
 Now the direction-cosines of the normal to the osculating plane 
 
 are proportional to 
 
 d^y dz d^z dy d^z dx d'x dz d^x dy d^y dx 
 ~df' di~TfTt^ le- Tt ~ If Tt ' Iftt'll- Jt' 
 
 and therefore, considering the equations of motion, proportional to 
 
 (dz dy\ f dx , dz\ f,dy dx\ 
 
 '''Tt-''di)' K'Tt-^Tt)' \!Tt-'''Tt)' 
 6 be the angle between this line and the direction 
 the numerator of cos 6 is 
 ,/ dz dy\ ( dx ,dz\ f,dy dx\ 
 
 \"'Tr''dt)'-'"VTt-^dt)'-''Vtt-"'dt) 
 
 which =^ 0, 
 and .-. = ^, 
 or R acts in the osculating plane. 
 
 72. Let us next consider the motion of a particle which is con- 
 strained to move on a given smooth surface. 
 
 In this case the whole reaction of the surface will be in the 
 direction of the normal. 
 
 Let u = 0, (1) 
 
 be the equation to the surface, and let /, 7n, n be the direction-cosines 
 of the normal at any point, then the equations of motion are 
 
 M^=X^Rl, (2) ^ 
 
 M^=Y+R7n, (3) 
 
 M~ = Z+Rn (4) 
 
108 A TREATISE ON DYNAMICS. [cHAP. 
 
 I, m, and n are known functions of x, y, and z, determined by equa- 
 tion (1), and these four equations will be sufficient to determine x, y, 
 z and Ji as functions of t. 
 We shaU have, as before, 
 
 and the same results may be deduced from this equation as were 
 deduced in the case of a curve line. 
 
 To find the equation which must be joined to (1) to determine 
 the path of the particle on the surface, we have 
 
 du 
 dx 
 
 //diiV fduV {diiV 
 s/\T.)^\Ty)^{Tz) 
 
 du 
 dy 
 
 /fdu\' /duV (duV' 
 
 ^/[Tx)^[Ty)-'[rJ 
 
 dz 
 
 //duV (duV fduV ' 
 \/{Tx)-'[dy)^[Tz) 
 
 Eliminating R from the equations (2), (3), (4), we shall have two 
 equations between x, y, z, and t; and these combined with (1) will 
 give X, y and z as functions of i : or will give another relation 
 between x, y and z by eliminating t ; R can then be found from any 
 one of the previous equations. 
 
 We can shew that whenever there are no forces acting on the 
 body, the osculating plane of its path will always pass through the 
 normal to the surface. The equations are 
 
 And, as before, we can shew that the direction-cosines of the 
 normal to the osculating plane are proportional to 
 
IV.] A TREATISE ON DYNAMICS. 109 
 
 . ('"s-40'(4:-'S).(4J-'«frO- 
 
 and it is therefore at right angles to the normal. 
 
 73. In the particular case where the proposed surface is one 
 of revolution, some of the preceding equations may be put under 
 a simpler form. 
 
 Let the axis of revolution be the axis of s, and let r =f(z) be the 
 equation to the generating curve. 
 
 X = r cos 0, y = r sin d. 
 
 The direction of the reaction R will in this case always pass 
 through the axis. 
 
 From the first two equations of motion we have 
 
 ^i-ff-^^n-^^-'^- 
 
 When X Y -yX=0 the integral of this equation is 
 
 This will be the case when X=0, and Y = 0, or when the whole 
 force is parallel to the axis of revolution ; it will also be the case 
 when the resultant of X, F and Z passes through the axis of revo- 
 lution. 
 
 Let (p be the angle which the direction of motion makes with the 
 generating curve through the particle. Then we shall have 
 
 . ^ rde h 
 sm(b = - -r- = — . 
 ^ V at vr 
 
 If no forces act, v will be constant, and sin cp will vary inversely 
 as the distance from the axis. 
 
 Again, suppose the axis of revolution to be vertical and the only 
 force acting to be gravity : we then have 
 
 which gives sin = — , — ■ . 
 
 In the cases of constraint that we have considered the curves 
 and surfaces on which we supposed the particle compelled to move 
 were fixed in space. We might vary the conditions by supposing 
 them in motion, either according to some given law, or in some 
 manner due to the action of the particle. Some of these cases 
 
110 A TREATISE ON DYNAMICS. [cHAP. 
 
 will occupy our attention afterwards. We have here given sufficient 
 to shew how such problems are to be treated when they occur. 
 
 (y 74. We will conclude this chapter by proving in the case of the 
 motion of a particle, a principle of very general application, called 
 *' The Principle of Least Action," 
 
 When a free particle moves under the action of forces X, Y, Z, 
 the equations of motion are 
 
 ^S=^' ^S=^' ^s=^ « 
 
 and if ZXdx + 2Ydy + 'ilZdz = Mdf{x, y, z).,.{2') 
 
 we have w* = V^ +f{x, y, z) -f{a^ h, c) ... (S) 
 
 Let ^vds be taken between limits corresponding to two fixed 
 points in the path of the body ; then this integral is less than the 
 corresponding integral would be if the particle were compelled to 
 describe any other path by forces in addition to X, Y, Z acting at 
 every instant in a direction at right angles to the direction of the 
 body's motion. Let X', Y', Z' be these forces, then they satisfy the 
 condition 
 
 X'dx+ Y'dy + Z'dz = 0, 
 
 and therefore v is still given by equation (3). 
 
 By the principles of the calculus of Variations we have 
 hfvds = J'h.vds = J{ds .^v + vhds) 
 ds = vdt ; 
 .'. ds .t>v = dt .vlv — ^dt .Iv^ 
 = ^{Xlx+ Yly + Zlz) dt by equations (2) and (3) 
 
 = dv, .Ix + dvo.ly + dvs.lz-^ {X'lx^ Y'ly + Z'lz)dt, 
 
 where f ,, v^, v^ are the resolved parts of the velocity in the directions 
 of the axes : 
 
 also ds^ = dx^ + dy^^dz^; 
 
 .'. ds .Ids ^dx.Zdx + dy .Idy + dz .Idz; 
 
 .'. vZds = V),ldx-¥v'ldy + V3ldz 
 
 = Vidlx -(- Vodly + Vzdlz; 
 
IV.] A TREATISE ON DYNAMICS. Ill 
 
 .-, ds,Zv + vhds = dvi.ix + dvo-^i/ + dv3.^z + Vid^x + v,dci/ + V3d6z 
 
 «= d (UiBx + Vohi/ + I'aSz) --^{X'lx + Y'hi/+Z'ds)dt ; 
 
 .'. fh.vds = v,ha; + v,l7/ + v,Zz-^f{X'lx+ Y'Zy + Z'l2)dt + C, 
 
 which is the indefinite integral. Now, since the extreme points are 
 supposed constant, Zx, ly and Iz are separately zero at each limit, 
 and therefore the definite integral fZ.vds between those points 
 
 = -^f{X'Zx+Y'Zy + Z'Zz)dt 
 
 between the same points. 
 
 When X' = 0, Y'=0, Z'=0, this definite integral is zero, so 
 that when the particle is resigned to the action of the forces X, Y, Z, 
 Z fvds becomes zero, shewing that, in this case, fvds is a maximum 
 or minimum, and from the nature of the case it cannot be a maxi- 
 mum, therefore it must be a minimum. 
 
 Again, let a particle be restricted to move on a smooth surface ; 
 the equations of motion are 
 
 M~=X+Rcos\,] 
 
 M^^=Y+ R cos, X., 
 
 d^z 
 M -T-^ = Z+ Rcos V. 
 
 where cos A, cos n, cos v are the direction-cosines of the normal. 
 Then, as before, we have 
 
 V' = V +f(x, y, z) -f{a, h,c) (2) 
 
 where Mdf{x, t/, 2) = 2 {Xdx + Ydy + Zdz). 
 
 Let the integral ^vds be taken between limits corresponding to 
 two fixed points in the path of the body ; then, in this case also, the 
 integral is less than the corresponding integral would be if the par- 
 ticle were compelled to describe any other path on the surface by 
 forces X', Y', Z' in addition to X, Y, Z the direction of whose resul- 
 tant was always at right angles to the direction of the body's motion. 
 We have, as before, 
 
 6 Jvds = j'h,.vds=: f(ds . cv + vcds), 
 
 ds= vdl; 
 
 .(1). 
 
112 A TREATISE ON DYNAMICS. [cHAP. 
 
 .-. ds.lv = dt.vZv = ^dt.Zv'' 
 = j^(Xtx + Yty + Zcv)dt from equation (2) 
 
 Udvi X' + RcosX\^ /dv2 Y'+Rcosn\^ 
 
 (dvs Z'+Rcosv\^ \ ,^ 
 
 - dv^.Zx + dvs.ly-^diV . lz-r^{X'lx+ Y'ly + Z'lz)dt 
 
 since cosx. Ix + cos fx.ly + cosv .lz = 0, the variation indicated by 
 Zx, ly, cz being along the surface. 
 
 And, as before, vlds = Vidlx + V2dly + ihdlz, 
 
 so that l.vds = d{vylx + V2ly ^v^lz)- -^j^iX'lx + Y'ly->rZ'lz)dt, 
 
 from which the conclusion follows as in the preceding case. 
 
v.] A TREATISE ON DYNAMICS. 113 
 
 CHAPTEE V. 
 
 75. Having described the methods of determining the motion 
 of a particle when acted on by forces either constant or depending 
 only on the position and motion of the particle under consideration, 
 we will now proceed to another extensive class of problems, which 
 can be solved (except so far as our analysis is deficient) by the aid of 
 the same principles. This class consists of the cases of the motion of 
 any number of particles under the action of their mutual attractions. 
 There is one condition to which we shall consider these attractions 
 always subject ; namely, that when two particles A and B attract 
 each other, either alone or constituting two out of a system of many, 
 the actual force of attraction exerted by ^ on B is equal to that 
 exerted by B on A, and these forces act in the line joining the two 
 particles, and in opposite directions. This is the case in all attractions 
 in nature with which we are acquainted, and is always assumed to 
 hold whenever two particles are said to attract each other. It is in 
 general assumed without any formal statement, though it is possible 
 to conceive that it should not be the case. Under the term attraction 
 is included both attraction and repulsion. 
 
 In treating this class of problems we shall not enter into the de- 
 tails of the solution of any of them, but shall confine our attention to 
 finding the equations of motion, and indicating the different ways 
 in which the solutions are usually effected. We shall also prove 
 certain properties which are common to the motions of all systems 
 of this class. 
 
 We in every case suppose the force of attraction to be a function 
 of the masses of the particles and of the distance between them, 
 and of nothing else. 
 
 76. First, let us consider the case of two particles moving in a 
 straight line under their mutual attraction. 
 
 Let m, m! be the masses of the particles ; P the force of attraction 
 between them, estimated so as to be positive when the force is 
 attractive, and negative when it is repulsive ; x, x' their respective 
 distances from some fixed point in their line of motion, at a time t 
 from some fixed epoch. Then P will be a function of m, m', and 
 X — x'. 
 
 8 
 
114 A TREATISE ON DYNAMICS. [cHAP. 
 
 Let X be supposed greater than x', then the equations of motion 
 will be 
 
 dt 
 d'x 
 
 f = -P 
 
 = P 
 
 •(1) 
 
 Adding these equations, we have 
 
 ^-df'-'''-de-=''' (~) 
 
 also, dividing by in and m' respectively and subtracting, we have 
 
 d"{x-x') _ 
 
 = -P(l+i,) (3) 
 
 df \m m'J ^ ' 
 
 Since x and x' enter P only in the form x-x' equation (3) is of 
 the same form as the equation for the motion of one particle only, 
 and may be integrated by the same methods. The integration of 
 equation (2) can be easily effected. 
 
 The integrals of equations (2) and (3) will be two relations between 
 Xy x', t and constant quantities, from which x and x' may be found 
 separately as functions of t, and the absolute motion of each of the 
 particles determined. The constants introduced in integration may 
 be determined, as before, by the positions of the particles and the 
 circumstances of the motion at some known instant. 
 
 This is the most direct though not the most convenient method of 
 obtaining the solution of the problem from equations (1). 
 
 Let X be the distance of the center of gravity of the two particles 
 from the fixed point, at the time t. Then 
 
 (??? + m') X = mx + m'x' (4) 
 
 Differentiating this equation twice, we have 
 
 ,. dx dx , dx , ^ 
 
 (,. + m)^ = ,«^+m^, (5) 
 
 ,.d^x d'x ,d'x' 
 and {m + m)-^,=7n^+m-^ (6) 
 
 Therefore, from equation (2) we have 
 
 d'x ^ 
 
 (7) 
 
 From which -5- = constant. 
 dt 
 
v.] A TREATISE ON DYNAMICS. 115 
 
 Now at some particular instant let the velocities of the two parti- 
 cles be V and v' respectively, then from equation (5) 
 
 [in + m)-j-=mv + mv , 
 
 , ^, « dTt mv + m'v' _ 
 
 and therefore, -j- = 7- = v suppose. 
 
 dt m + m' ^^ 
 
 We have obtained the following result. If a point move so as to 
 coincide at every instant with the center of gravity of the two parti- 
 cles m and m', it will advance with a uniform velocity v ; or, in 
 other words, the center of gravity moves with a uniform velocity v. 
 
 This property, which has been shewn to hold in this particular 
 case, will be proved to hold in a great many descriptions of mo- 
 tion. It suggests another method of solving the problem under 
 consideration. 
 
 77- This method is to determine the motions of the particles 
 relatively to their center of gravity considered as a fixed point. 
 If the relative position and velocity at any time is known, the 
 absolute position and velocity can be immediately determined from it. 
 
 Let then r and r' be the distances of the particles from their 
 common center of gravity ; then we have 
 
 ^_m'{x-a^) ^,_m{x-cc') 
 
 
 /■ 
 
 m + m' ' 7n+ m' ' 
 
 
 or, (x - x') = 7— r = r'. 
 
 ^ ^ vi' m 
 
 
 
 We may, therefore, put equation (3) into the 
 forms : 
 
 d'r P 
 de~ vi' 
 
 two 
 
 following 
 
 rfV_ p 
 
 de~~m'' 
 and since P is a function o£ x-x' and therefore of either r or /, 
 these two equations may be integrated, and the motion relatively 
 to the center of gravity determined. 
 
 In determining the constant after the first integration of the 
 equation 
 
 drr__T 
 
 de~ m' 
 
 dr 
 we have to substitute for j- its value at some known time, or in 
 
 8—2 
 
116 A TREATISE ON DYNAMICS. [cHAP. 
 
 some known position. It must be borne in mind that this value is 
 not the velocity of the particle m at that time, but its velocity rela- 
 tively to the center of gravity : that is, it is v~v, not v. 
 
 dr 
 Similarly, vfe should have to substitute for -r- the quantity 
 
 v-v', since it is estimated in a direction opposite to that of w'. 
 
 This method is sometimes stated as follows. When two particles 
 move in a straight line under their mutual attractions, the motion 
 relatively to the center of gravity may be found thus : impress on 
 each of the particles a velocity equal to that of the center of gravity, 
 and in an opposite direction ; this will reduce the center of gravity 
 to rest, and not affect the motion relatively to it; take now the center 
 of gravity as origin and determine the motion by the ordinary 
 equations for rectilinear motion. 
 
 78. The integration of equation (3) gives the motion of the two 
 particles relatively to each other. This is also sometimes stated 
 as an independent method, as follows: to find the motion of a particle 
 m relatively to a particle m' when they move in a straight line under 
 their mutual attractions, impress on the particle m' a force equal to 
 the force which m exerts on it, and in the opposite direction ; there 
 will then be no force acting on m'; also, in order that the relative 
 motion may not be affected, impress on m a force whose accelerating 
 force is equal to, and in the same direction as, that of the force 
 impressed on m'; also, impress on each particle a velocity equal and 
 opposite to the velocity of ?«' at some instant : m' will then remain at 
 rest, and the motion of m relatively to it may be found by the 
 ordinary equations of rectilinear motion. 
 
 It is easily shewn that this method will lead to equation (3) ; thus 
 let r be the distance of the particles ; the force which m exerts 
 on m' is P, therefore the force impressed on m' is — P, and its 
 
 p 
 accelerating force is j ; therefore the force which must be im- 
 
 mP 
 pressed on wi to have this accelerating force is ^ , and the force 
 
 that does act on it is - P ; therefore the equation for its motion 
 becomes 
 
 d'r „ mP 
 
 d'r „/l 1\ 
 d r \m m'J 
 
 which is the same as equation (3), with r in the place of x - x', 
 
 1 
 
v.] A TREATISE ON DYNAMICS. 117 
 
 Though in this case these two last methods are of little import- 
 ance, from the simplicity of the direct method of solution, they will 
 be seen to apply in other more general cases, where the direct 
 solution would be very complicated. 
 
 79. There is another method of combining the original equations : 
 
 which is sometimes of use ; we have 
 _ d'x dx 
 
 and adding these we have " '"' 
 
 ^f d'xdx ,d'x' dx'X ^^d{x-x') 
 
 from which we have 
 
 or, mv^-^ mV» = C - 2jPd(x - x'). 
 Since P is a function of x - x' this integration can generally be 
 effected. 
 
 80. Next, let there be any number of particles moving in a 
 straight line under their mutual attractions. 
 
 Let ?«!, 7/?2, 7ff„ be the masses of the particles. 
 
 a*!, Xj, x„ their distances from some fixed point in their 
 
 line of motion at time t. 
 
 jPo the force of attraction of 7)1., on m^, estimated as positive when 
 tending to increase x^, with a similar notation for the other forces, 
 then the equations of motion will be 
 
 ^.^ = .P. + ^P^+ +^Pn \ 
 
 ^"2-^'= 2^1 +2^3+ +2^. 
 
 f;"=„A + «P.+ +,P,_. 
 
 0) 
 
118 A TREATISE ON DYNAMICS, [cHAP. 
 
 where 1^2 + 2^1 = 
 
 ,P, + ,P, = \ (2) 
 
 
 
 and 1P2 is a function of x^-x^, and the other forces are in like 
 manner functions of the distances of the particles to which they 
 correspond. 
 
 The solution of these n equations would determine the n quan- 
 tities Xi, Xn,...x„ as functions of t, and thus completely determine 
 the motion of each of the 7i particles. 
 
 If we add together equations (1), and bear in mind equations (2), 
 we have 
 
 '"'-dF^'^'-dF^ + »«„^^,- = o...(3). 
 
 Now if X be the distance of the center of gravity of all the 
 particles from the fixed pointy we have 
 
 (rWi + ?«3 + . . . +^«„) 0? = 7«i .Ti + 7W2'^2 + • • • + ^»^n J 
 
 - d'^'x d^x, d^x. d^x„ ^ 
 
 _ dx 
 .•. t; = — - = const. 
 at 
 
 or the motion of the center of gravity is uniform. 
 
 We shall hereafter see that this is the case when particles move 
 in any way under their mutual attractions. 
 
 Again, from equations (1) and (2) 
 
 f d^Xi dx-i d'^Xs dxz d^x„ dxA 
 
 -r^ ~dF lu-^"^' -d^-dt'"-''-'''''U-dt ] 
 
 and integrating 
 
 or, as it is generally written, 
 
 2 mv' - C + 2 2 /.Pj (/ (a:i - x^). 
 
 These integrations can generally be effected. 
 
 We have thus obtained two integrals of the n equations (l); the 
 methods for obtaining others will depend on the forms of the func- 
 tions P, and must be left to the ingenuity of the analyst. 
 
v.] A TREATISE ON DYNAMICS. 119 
 
 81. Let US now take the case of two bodies moving in one plane, 
 but not in the same straight line. This is possible, for if at any 
 instant the directions of their motion lie in one plane, they will 
 always lie in that plane, since no force acts to move them out of it. 
 
 Let m, m' be the masses of the two particles x, x' and y, y' their 
 co-ordinates at time t ; r their distance ; P the force of attraction 
 between them ; then the equations of motion are 
 
 ~ = -Jf — 
 r 
 
 dt- 
 
 * dt- 
 
 r 
 
 = -P' 
 
 ^_ 
 
 df 
 
 = -P 
 
 y -y 
 
 (1) 
 
 with the geometrical relation 
 
 r'=(,x-xy + Q^-yy, 
 
 where P is a function of r and constant quantities. 
 From these equations we have 
 d'x ,d'x' 
 
 (2) 
 
 ' dt' 
 d'y 
 "df 
 
 de 
 df 
 
 0, 
 
 = 0, 
 
 ,(3) 
 
 from which it appears as in the preceding cases that -j- and -j- , the 
 
 resolved parts of the velocity of the center of gravity of the two 
 bodies, are constant ; and therefore the center of gravity moves in a 
 straight line with uniform velocity. 
 Again we have 
 
 dx d^ dys fclx^ dx' d^y' dy\ 
 
 Tt^dt' dt)^^ \de 'dJ^'dW Tt) 
 
 9.m 
 
 (cPx 
 \dt' 
 
 op 
 
 _,^ d(x-x') 
 
 '^ dt 
 
 + (y-y') 
 
 '^^Syjill 
 
 dt 
 
 = -2P 
 
 dt 
 
 {^ih(m 
 
 = C-2jPdr.... 
 
 = c 
 
 JPdr, 
 
 .(4) 
 
120 A TREATISE ON DYNAMICS. [ciIAP. 
 
 This is another integral of equations (l). We may obtain another 
 as follows : 
 
 f d'y cPx\ ,( ,d'ij' ,d'x'^ 
 
 '^{fd^-^-drO'-'''V'd¥-^ d? 
 
 From which we have 
 
 (4) and (5), together with the equations 
 dx ,dx' 
 
 '"Tt'-'''-dt=' 
 
 dy ,dy' f ^^^ 
 
 dt-^'^dt- 
 
 which we derive from (3), are the first integrals of equations (1). 
 If we can solve these the absolute motions of the particles m and m! 
 will be completely determined. 
 
 Generally, however, it is not the absolute motions of the two 
 particles that are required, but their motions relatively to their 
 center of gravity, or to each other. First, then, to find the motion 
 of m relatively to m', let x^y^ be the co-ordinates of wz considering 
 m' as origin, that is, let 
 
 x, = x-x', yi=y-y'. 
 Then we have, from equations (1), 
 
 d^ {x — x')_ -pffi + »«' x-r- x' 
 df mm' r ' 
 
 d^Xx ■n'm + m' Xi . 
 rfr mm r I 
 
 and^ = -P^^^J 
 
 at Tnm r ' 
 
 These equations are the same as those for the motion of a particle 
 round a fixed center of force : all the properties therefore which are 
 proved to be true in that case, are true also for the motion of one of 
 two bodies relatively to the other ; and the same methods of solution 
 
 apply in this case as in that. Writing P' for P ;- , we have the 
 
 two polar equations of motion 
 
 
v.] A TREATISE ON DYNAMICS. 121 
 
 These •will be the equations from which the solution will generally 
 be best obtained. This method may be enunciated in words thus. 
 
 To find the motion of m relatively to m', apply to m' a force equal 
 and in the opposite direction to that exerted by m, then there will 
 be no force acting on m' : in order that the relative motion may not 
 be disturbed apply to m a force such that its accelerating force shall 
 be equal to that of the force applied to m' : also apply to each of the 
 bodies a velocity equal and in the opposite direction to that with 
 which m' is moving, m' will then be reduced to rest and the relative 
 motion of ?« will be the absolute motion. 
 
 A little consideration will shew at once that this, which we have 
 given as the interpretation of equations (7), might have been assumed 
 a priori as true. . The motion of in' relatively to ?« will be exactly 
 similar to this. 
 
 To find the motion relatively to their center of gravity. 
 
 Let f, »7 be the co-ordinates of m relatively to their center of 
 gravity, p the distance of ?« from it ; then we have 
 
 ,(x-x'), t] = (w_y). 
 
 ?n + m 
 and equations (7) become 
 
 the eijuations of motion relatively to the center of gravity. 
 
 P, which is a function of r, will be a function therefore of p. 
 These are the equations of motion which we should have had if the 
 body had been moving round the center of gravity fixed, acted on 
 by the same force. The only points of difference will be in the 
 determination of the constants introduced in integration. We may 
 enunciate the method therefore as follows. 
 
 Impress on the system a velocity equal and opposite to that with 
 which the center of gravity is moving ; the center of gravity will 
 then be reduced to rest, and the motion about it may be determined 
 by the ordinary methods for determining the motion about a fixed 
 center, and all the conclusions arrived at in motion of that kind 
 will be true also in this. 
 
 If the absolute motion be required we can compound the relative 
 motion thus found with the motion of the center of gravity. 
 
122 
 
 A TREATISE ON DYNAMICS. 
 
 [chap. 
 
 82. Let us now consider the case where the motions of the two 
 particles are not in one plane. Using a notation similar to that we 
 have already adopted^ the equations of motion are 
 
 
 x' 
 
 d^ 
 d? 
 
 d^ 
 ■ dt' 
 
 r 
 
 ,d'x' 
 
 > y -y 
 
 r 
 
 '-Z 
 
 r 
 
 ...(1), 
 
 From these equations we deduce as in the preceding cases, the 
 
 equations _ _ _ 
 
 dx dy dz , . 
 
 -dt'='^' Tr'^' Tt='^ (2) 
 
 which shew that the center of gravity moves uniformly in a straight 
 line. 
 
 We may also obtain as before the equation 
 
 mv'' + m'v'"'=C-2JPdr (3) 
 
 bearing in mind that 
 
 r^ = ix-xy^{y-yy + {z-zy. 
 
 And we shall also have, in place of equation (5) of the preceding 
 case, the three equations 
 
 dy\ 
 
 f dz 
 Vdi 
 
 ( dy dx\ ,( ,dy' , dx'\ , 
 
 V^-^dt)'-'^V-dt-^-dF) = ^'^ 
 
 dx 
 Tt 
 
 dz\ /f ,dx' ,dz'\ 
 
 ...(4) 
 
 Equations (2), (3) and (4), are the first integrals of equations (1), 
 and when they can be again integrated, give the direct solution of 
 the problem. 
 
 We might deduce the equations giving the motion of w relatively 
 to m! or of either relatively to their common center of gravity. It is 
 also easily seen that the principles before stated for reducing the 
 motion of one relatively to the other, or to their center of gravity 
 to the case of motion about a fixed center will apply in this case 
 also. Hence it follows, that in whatever manner two bodies move 
 under their mutual attractions, the motion of one relatively to the 
 other, as also the motions of the two relatively to their center of 
 gravity will be in one plane. This plane however will not coincide 
 
v.] A TREATISE ON DYNAMICS. 123 
 
 with the direction of motion of the center of gravity, or of that body 
 to which the motion of the other is referred. 
 
 When we have by one of the principles above stated reduced the 
 motion to that about a fixed center, it will become only a particular 
 case of the motion of one particle, which has already been fully con- 
 sidered. 
 
 83. Let us now consider the case of any number of particles 
 moving under their mutual attractions. 
 
 Let nil, 1112, . . . m„ be the masses of the several particles ; a:,, 3/1, 2, ; 
 ^2, ^2) ^a', ••• ar,„ i/„, s„ their co-ordinates at time t; 1P2 the abso- 
 lute force of attraction between 7M, and m.^ ; Avith similar expressions 
 for the other forces ; ^r^ the distance between Wj and 7/13 with similar 
 expressions for the other distances. 
 
 The equations of motion are 
 
 d^Xi _ Xi — X., 
 mi ■j-^ = -iP2 - 
 
 dr ir, 
 
 m -f7r= - iP2-^ — - 
 df ii\ 
 
 d'si _ Z1-Z2 
 
 7«i -772- = - 1^2^ 
 
 dt^ ^ ira 
 
 with similar equations for all the particles. 
 Together with the geometrical conditions 
 ir^ = {xi - 0:2)- + (j/i -^2)' + (-. 
 and similar equations for the other distances. 
 From these equations, we have 
 
 1^3 
 
 ir„ 
 
 .p/'-"' ■ 
 
 
 
 .pr--'" 
 
 d'x, 
 
 '■-dt^-"" 
 
 d'x. 
 
 d\y, 
 
 
 d'vn : 
 
 THi ^^, +... 
 
 
 ■ "'" dt' "' 
 
 m — — - + , . 
 
 
 
 dl' 
 
 
 + v?„ ^^, V, 
 
 from which, if x, 1/, z are the co-ordinates of the center of gravity. 
 
 dx 
 -dt='^' 
 
 dy 
 
 dz 
 
 or the center of gravity moves in a straight line with uniform 
 velocity. 
 
 K 
 
124 A TREATISE ON DYNAMICS. [CHAP. 
 
 This property which we have seen to hold in all the particular 
 cases before considered, and have now proved to hold in the 
 general case of the motion of any number of particles under their 
 mutual attractions, is a particular case of a much more general 
 principle, called "the principle of the conservation of the motion of 
 the center of gravity," which will be stated and proved hereafter. 
 
 84. Again, multiplying each second differential coefficient by 
 twice the corresponding first differential coefficient and adding all 
 together, and bearing in mind the geometrical relations which give 
 
 (--)(S-^'). 
 
 + 2 
 we have 
 
 And we observe on the right-hand side that jPg is a function of 
 jTj and constant quantities, and, in like manner, the other forces of 
 the corresponding distances ; therefore integrating, we have 
 
 or, as it may be written, 
 
 ^{rnv^)=C-^^jPdr. 
 We have, in particular cases already considered, obtained equations 
 corresponding to this. 
 
 The name " vis viva" has been given to the product mv^, 1.{mv^) 
 which is the sum of the " vires vivae" of the several particles of the 
 system is called the " vis viva" of the system. 
 
 We will now ascertain what the last formed equation assures us of. 
 
 Let 2/,Po<Z,r2 be i/sGr^), 
 
 then it becomes '2.{mv^) = C -1. {f{r)]. 
 
 Now let Fi, F.2"-Vn be the velocities of the several particles at 
 
 the time when their mutual distances are lOa, lOg, sOa, &c. then 
 
 we have 
 
 2 0«n=C-2{/(a)}, 
 from which we have 
 
 2 ipuv') - 2 {m n = 2/(«) - 2/(r). _ 
 This equation shews that the change in the vis viva of the 
 system depends only on the relative positions of the particles at the 
 two instants when it is estimated, and is independent of the direc- 
 tions in which they are moving or the paths they have described. 
 
v.] A TREATISE ON DYNAMICS. 125 
 
 85. Again, recurring to our equations of motion, it will be seen 
 on examination that they give the following equations, 
 
 / cf'x, d-z\ f d^x^ d\^^\ „ 
 
 "'^ (^' rf^-^' rfF j -^ ^"^ (- rfT^ -^^:^ j ■" ^"- = ^^ 
 
 Integrating these equations, we have 
 
 / dsi dy^\ f dz„^ di/^\ 
 
 "^^ \y^-dt-'^dt) + ^"^ V'- -di --^) -^ ^^- =_!'^^ 
 
 ( rfx, dz\ ( dxz dzo\ . , 
 
 "^ V- -dt-^^-dt)'- '"^ ( - 77 - ^--77) -*- ^'- = ^'" 
 
 (c?Mi dxi\ t dy^ dx\ . , 
 
 or, as we may write them conveniently 
 
 ^ { dx 
 
 dz dy\ y 
 
 dx dz 
 Tt 
 
 where h^, kg, h^ are constant. 
 
 Let us now consider what these equations express. 
 
 If we conceive a line drawn from the origin of co-ordinates to a 
 particle m to generate an area by its motion, and if A be this area at 
 time t, and A^, A^, A.^ its projections on the three co-ordinate planes, 
 or, which amounts to the same thing, if we conceive that Ai, A^, Ag, 
 are the areas described on the co-ordinate planes by the projections 
 of this imaginary line, then it is known from geometry, that 
 
 dz 
 
 y-Tt- 
 
 Jy 
 
 -'dJ- 
 
 -~ dt 
 
 dx 
 
 dz 
 
 -~ dt 
 
 dy 
 
 dx 
 
 -^Ti- 
 
 '" dt ' 
 
126 A TREATISE ON DYNAMICS. [cHAP. 
 
 These three 
 
 equations then 
 
 give 
 
 
 
 
 22(7; 
 
 dt)' 
 
 -h, 
 
 
 
 21 fm 
 
 dt)- 
 
 -h„ 
 
 
 
 21 (m 
 
 dJ,\ 
 dt) = 
 
 /^3. 
 
 And integrating them we have 
 
 2'Z(9nAi)^hit, 
 2l{mA^)=h.2t, 
 2l.(niAs) = hst, 
 making the constants which are introduced by integration each 
 zero, which amounts to supposing that the description of areas com- 
 mences at the instant from which t is measured. 
 
 These equations shew that if the mass of each particle of the 
 system be multiplied by the area described by the projection on 
 each of the co-ordinate planes of the line joining it with the origin, 
 the sum of all these .products will be proportional to the time of 
 describing them, whatever point be assumed as origin. 
 
 This is a case of a general principle which will be proved here- 
 after, called the " Principle of the Conservation of Areas." 
 
 86. Let A, fx, I/, be the direction-cosines of the normal to a 
 plane, then the projection of the area A on this plane is 
 
 XAi+fxAz+vAa, 
 
 and a similar expression will give the projection of the area for 
 every particle. 
 
 Therefore, the sum of the products of each mass into the projec- 
 tion on this plane of the area described by it is 
 
 X 2 (?n Ai) + /A 2 (7rt A2) + vl (m A^. 
 
 Now, to find the plane on which this sum is a maximum at any 
 time we must make this expression a maximum by the variation of 
 A, Mj and V, subject to the single condition 
 
 We have then 
 
 1(mA,) lX + 1{mA^lfx + 1{mAs)lv = 0, 
 XlX + fxlix + vlv = ; 
 
v.] A TREATISE ON DYNAMICS. 127 
 
 therefore, using the indeterminate multiplier B we must have 
 2 (»w A^) +B\ = 0, 
 1.(7)1 As) + Bfx = 0, 
 2(?tt^3) + Bu =0; 
 
 and therefore =7 — -j- = _.^ . . = vT—TT > 
 2(ot^i) ^(wJig) l.{mAs)^ 
 
 X fx 1/ _ 
 
 and therefore, if /r = ^,^ + ^2^ + /^3^ we have 
 k, h, /«3 
 
 That is, the position of the plane is constant during the motion ; it 
 is called the plane of maximum areas, or the " Invariable plane." 
 
 We may remark that the position in space of the plane has 
 not been proved constant, but merely the direction of its normal ; 
 all planes parallel to this would have the same property. 
 
 If at any instant we know the positions, magnitudes, velocities, 
 and directions of motion of the several particles of such a system 
 as we have been considering, we can find the position of this invari- 
 able plane, with reference to co-ordinate axes arbitrarily chosen; 
 and if at any future time we take other co-ordinate axes arbitrarily 
 chosen, we can also determine with reference to them the position of 
 the invariable plane, and we know that these two positions must 
 be absolutely the same, as far as regards direction, whatever the 
 co-ordinates by which they are determined. Thus we see that the 
 system itself furnishes a plane of reference which is invariable in 
 direction, and can always be determined from the state of the system 
 at any instant. 
 
 The preceding are the principal general properties of a system 
 of particles moving under their mutual actions ; the actual determi- 
 nation of the motion of each particle in anything like the general 
 case far surpasses our powers of analysis. The solution of a number 
 of simple cases is the only means of acquiring a familiarity with the 
 treatment of problems of this sort. 
 
 87- We have hitherto supposed the system to be acted on by 
 no forces but those which arise from the mutual attractions of its 
 several particles ; in addition to these, all or any of the particles of 
 the system may be acted on by forces arising from causes extraneous 
 to the system, as, for instance, the attraction of some body not 
 
128 A TREATISE ON DYNAMICS. [cHAP. 
 
 forming a part of the system ; or by forces arising from geometrical 
 constraints, such as, that some of them move in tubes or on surfaces. 
 
 In these cases if the forces are given, they will enter our equa- 
 tions as known quantities, and we shall still have as many equations 
 as we have co-ordinates to determine. 
 
 If the forces are not given explicitly, but are known to arise from 
 the particles being compelled to satisfy certain geometrical conditions, 
 they will then enter the equations as unknown quantities; and, 
 corresponding to each unknown force, there will be an equation 
 expressing the geometrical condition from which it arises ; so that 
 the whole number of equations will in every case be the same as the 
 whole number of unknown quantities, and will thus be sufficient 
 to express every such unknown quantity as a function of t. 
 
 We shall not, however, enter upon any of these cases here, as our 
 object is not to obtain solutions of particular problems, but to explain 
 the principles by which those solutions are to be obtained, and to 
 investigate certain properties which belong to extensive classes of 
 such problems. 
 
VI.] A TREATISE ON DYNAMICS. 129 
 
 CHAPTER VI. 
 
 88. In the preceding pages the motion of a single material 
 particle, and also of a system of several particles has been consi- 
 dered, when the particles were acted on by various forces and subject 
 to different conditions; it remains to investigate the methods of 
 determining the motion of bodies of finite magnitude. 
 
 Now, when a body of finite magnitude is in motion, unknown 
 forces act on every particle of it arising from the action of every 
 other particle. The determination of these forces from the equations 
 expressing the conditions to which the system is subject presents 
 insuperable difficulties. The consideration of these forces is avoided 
 by making use of a principle first stated by D'Alembert, which we 
 will now proceed to explain. 
 
 When a material system is in motion under the action of forces 
 arising from causes external to the system, these external forces are 
 called "impressed forces;" and those of them which act on any one 
 particle of the system are called the impressed forces on that particle. 
 
 Every particle besides being acted on by the impressed forces, is 
 also acted on by forces arising from its connexion with the other 
 parts of the system ; these are called " internal forces." 
 
 The whole force acting on any particle is the resultant of the 
 impressed and internal forces on that particle, and is called the 
 "effective" force on that particle. 
 
 Conceive an equal isolated particle to be moving in the same 
 direction and with the same velocity as the proposed particle, and to 
 be acted on by a single force equal to this resultant and in the same 
 direction; the two particles Avill be in the same state, one being 
 acted on by a number of forces, the other by a single force which is 
 their resultant; the motions of the two particles will therefore be 
 the same. Hence then we sometimes have the following definition 
 of effective force. 
 
 That force which acting alone on any particle of a system sup- 
 posed isolated would cause it to move as it does when it forms part 
 of the system; that is, which would generate in the small time 8/ 
 the same change in velocity and direction of motion that takes place 
 when the particle forms part of the system, is called the " effective" 
 force on that particle. 
 
 9 
 
130 A TREATISE ON DYNAMICS. [cHAP. 
 
 Now D'Alembert's principle asserts that if at any instant we 
 apply to every particle of a system forces equal and opposite to the 
 eftective forces on that particle, the system, if it were at rest in the 
 position which it occupies at that instant, would remain in equili- 
 brium under the action of these together with the impressed forces. 
 
 We have enunciated this principle in the form in which it will be 
 most convenient for obtaining equations of motion for a system. We 
 will now explain the nature of the assertion contained in it. 
 
 Let mhe a particle of the system ; / the 
 resultant impressed force acting on that 
 particle ; M the resultant of the internal 
 forces on it; JE the resultant of M and /, 
 and therefore the effective force on the par- 
 ticle ; R the reversed effective force, that is, II 
 a force equal to E acting in the opposite direction. 
 
 Then if the particle m were at rest, and the forces /, M, and R 
 acted on it, they would keep it in equilibrium : and the same would 
 be true of every particle. 
 
 If therefore the whole system were at rest, and each particle 
 acted on by the impressed forces, the effective forces reversed, and 
 the same internal forces that acted on it when the system was in 
 motion, every particle would be separately in equilibrium, and 
 therefore the whole system would be in equilibrium. 
 
 Instead of this suppose the system to be at rest, and each particle 
 to be acted on by the impressed forces and reversed effective forces 
 that correspond to it, and by such internal forces as naturally arise 
 from this condition ; then D'Alembert's Principle asserts that the 
 system will in this case also be in equilibrium. 
 
 The Principle may also be considered in the following light, in 
 which it possibly appears less arbitrary. 
 
 A system is in motion under the action of impressed forces and 
 internal forces arising from the connexion of its parts. Let the 
 impressed forces be replaced by the effective forces: in this case, 
 since each particle will move under the action of its effective force 
 alone consistently with the connexion of the parts of the system, the 
 internal forces arising from this connexion will not be called into 
 action, and the change of motion in the small time ht will be the 
 same as under the action of the impressed forces. 
 
 Now, forces equal and opposite to the effective forces, acting 
 together with the effective forces on the system at rest, keep it in 
 equilibrium ; will they keep it in equilibrium when they act together 
 with the impressed forces ? D'Alembert's Principle asserts that they 
 
VI.] A TREATISE ON DYNAMICS. 131 
 
 will. It states that a set of forces which balances one of two sets that 
 produce the same change of motion in a system will also balance the 
 other. 
 
 D'Alembert's Principle, like the laws of motion and the theory 
 of gravitation, is proved by the agreement between the results of 
 calculation and observation. We are not, however, able in this case 
 to avail ourselves of Astronomical observation. The comparison 
 has been principally made by means of a machine invented by 
 Atwood, by which the motion of a system of bodies can be very 
 accurately observed in a great variety of cases. 
 
 89. To form the equations of motion by the aid of this principle, 
 
 we must express the effective force on each particle in terms of the 
 
 co-ordinates of that particle : if m be the mass of a particle, x, y, z 
 
 its co-ordinates, the resolved parts of this force at the time t will be 
 
 d-x d-y , d'z „, 
 m-T-j, m -— , and m -^ . We must now suppose the system to be at 
 
 rest in the position it occupies at the time t, and apply to every par- 
 ticle a force equal and opposite to the effective force on it The 
 system will then be in equilibrium under the action of these and the 
 impressed forces : and the equations expressing the conditions of 
 equilibrium of the system will be the equations of motion. 
 
 These equations will be different for different systems of bodies. 
 They will be different according as there is one body or more, as the 
 bodies are elastic or inelastic, solid or fluid, rigid or flexible. 
 
 The equations expressing the conditions of equilibrium assume 
 different forms in these different cases, and consequently the equa- 
 tions of motion obtained from them by the aid of D'Alembert's 
 principle are of different forms. 
 
 90. We will now apply this principle in the form in which we 
 have enunciated it to the solution of a problem ; viz. to calculate the 
 motion of a uniform cylinder with its axis horizontal, rolling down 
 an inclined plane so rough as to prevent all sliding. 
 
 Let the figure represent a section of the cylinder and inclined 
 plane; and let a be the radius of the cylinder, h its length, a the 
 inclination of the plane to the horizon. 
 
 Let any point B in the plane be the origin, BP the axis of x, a 
 normal to the plane atB the axis of ^ ; Q an element of the cylinder, 
 ^7)1 its mass, x, i/, z its co-ordinates ; then BN = x, QN=y. 
 
 Let BP^x, QC = r, QCA^tp. 
 
 ACP = 6 the angle through which the cylinder has rolled. 
 
 9—2 
 
132 ■ A TREATISE ON DYNAMICS. [cHAP, 
 
 Since z is constant -7-^ — , and the resolved parts of the effective 
 at' ^ 
 
 force on Q are Im -y— and Im ~~, parallel to the axes of a; and y ; 
 
 and the impressed force is g^tti vertically downwards. Also on the 
 line of particles in contact with the plane there will be other im- 
 pressed forces arising from the reaction of the plane : let the resolved 
 parts of one of these parallel to PC and PB be R' and F\ 
 
 Now apply to every particle the reversed effective forces on that 
 particle, and write down the equations of equilibrium : they ai*e 
 
 1.R' - "EZjn-— — ^^me^cosa — 0, 
 (It 
 
 1.F' + 1.^7)1 -j-^ ~ I-hm g sin a = 0. 
 
 1.F'a + IhynQc- x)—^^-^lm{y -")ji2 +'^^mg cos a (x - x) 
 
 + 28 mg sin « (^y — a) = 0. 
 To these equations we must add the geometrical relations 
 X ^x — r sin (6 + (p), y = a- r cos {Q + (p), 
 from which we obtain 
 
 •i , -.fdey . .d'0 
 
 r^-^'-^\dl)^^-'^-''^dF 
 
 de di- 
 
 d'y . .fdOy . rl^d 
 
 dF- ~(^-"Kdi)-^'-''^de' 
 
 Let 2/2' = 72, ^F'^F, 1.1m =M, then substituting these values 
 in the equations we have obtained, and bearing in mind that ^, y, 
 
VI.] A TUEATISE ON DYNAMICS. 133 
 
 and d refer to the whole cyhnder, and that the center of gravity of 
 the cylinder is in the axis, and therefore thSt 
 
 1.l7n(x-w) = 0, 1.d7n(i/-a)-0, 
 we have R - Mg cos a = (1 ) 
 
 M~ = Mgdna-F (2) 
 
 '^^hnr"-=Fa (3) 
 
 also X — aO + c (4). 
 
 Equation (l) determines the whole pressure on the plane, which 
 is constant. 
 
 Also 'Zcmr^^Ma% 
 
 therefore equation (3) becomes 
 
 Ma d^_ 
 
 2 de~ 
 
 Eliminating F between this equation and (2) and reducing by 
 means of (4), we have 
 
 d^O _ 9.g sin a ^ 
 
 dQ _2g sxna.t 
 " dt ~ Sa ' 
 
 — is called the angular velocity of the cylinder. 
 
 C and C may be determined from the values of 6 and -j- corre- 
 sponding to any value of t ; and the motion is then completely de- 
 termined. 
 
 We see from the preceding example, that even in a simple case 
 the equations given by the immediate application of the principle 
 are complicated, and require considerable reduction before they can 
 be integrated. In the case of rigid bodies, however, this reduction 
 can be effected generally, as follows: 
 
 91. Let there be one rigid body, and let 7/?, be the mass of a 
 particle, x,, i/i, ri its co-ordinates at time /, X, Yi Zj the resolved 
 parts of the impressed forces that act on it. The resolved parts of 
 the effective force on it are 
 
 d'x, d'y, d'z, 
 
 ""^Tt^' "''rfF' "'^di'- 
 
134 A TREATISE ON DYNAMICS. [CHAP. 
 
 If we apply these in the opposite directions, the resolved parts 
 of the whole force on the particle will be 
 
 
 ,„,--^andZ.-^,-^ 
 
 and the body will be in equilibrium under the action of these and 
 similar forces applied to every particle. 
 
 Hence then the six equations of equilibrium give 
 
 (I) 
 
 ^(i 
 
 mA-- 
 
 dt- 
 
 )} 
 
 (II) 
 
 These are the six equations of motion for one rigid body, and 
 when these equations are solved the motion of the body is com- 
 pletely determined. 
 
 92. The preceding equations contain the co-ordinates of every 
 particle of the body, the use of them is greatly facilitated by the 
 following reduction. 
 
 Let X, y, J be the co-ordinates of the center of gravity of the 
 body at the time t ; x' , y', z' the co-ordinates of a particle of the 
 body referred to axes whose origin is the center of gravity and which 
 are parallel to the original ones : then 
 
 and therefore 
 
 d'x d^x (fx' 
 
 dt' dt' 
 
 df 
 
 d^J^ d^ 
 
 de dt^ de 
 
 dt' 
 
 di'' "^ dt' 
 
VI.] A TREATISE ON DYNAMICS. 135 
 
 Substituting in equations (I), we have 
 
 dl^ dt^ 
 
 but since the origin of x' y' z' is the center of gravity 
 
 and therefore 
 
 „ d'x' ^ _ d'y' ^ ^ d'z' ^ 
 di' dl' dr 
 
 also X, y, z are the same for every "particle of the body, therefore 
 writing M for 2?h, we have 
 
 ^^§=-^4 (Ill) 
 
 dt' 
 
 These three equations are in the form in which they are most 
 available for determining the motion of the body. They are the 
 same as those for the motion of a particle whose mass is M acted on 
 by the forces 1.X, 1.Y, and 2Z, 
 
 Hence then, if a body of finite magnitude be acted on by any 
 forces, its center of gravity will move as a particle of equal mass 
 Avould if acted on by all the forces impressed on the body. 
 
 We also see that the motion of the center of gravity of the body 
 will not be affected by changing the points of application of any of 
 the impressed forces, provided their intensities and directions are 
 not altered. 
 
 If all the forces X, Y and Z be given explicitly as functions of 
 the variables, these equations will give the motion of the center 
 of gravity at once by integration. 
 
 When this is not the case, that is, when unknown forces enter, 
 arising from geometrical conditions to which the motion is subject, 
 it will generally be necessary to combine them with the remain- 
 ing three equations before the integration can be effected. 
 
136 
 
 93. Substituting a; + a;', 7/+ y, 2' + s for 
 (II) we have 
 
 X, y, an 
 
 2{(i + /)(x- 
 
 d'x 
 
 
 -(i + xo(z- 
 
 d'l 
 
 2|(3 + x0(f- 
 
 d'y 
 -""dP- 
 
 d'y'\ 
 
 -^de)- 
 
 .G^+y)(x- 
 
 
 ^)}- 
 
 d'y'- 
 dt 
 
 Now in these equations x, y, i and their differential coefficients 
 are common to all the particles of the system, they may therefore 
 be placed before the symbol, 2. 
 
 Also, 2 m x' = 0, 2 my' = 0, 1.mz' = ; 
 
 and therefore, 
 
 _ d'x' ^ _ n't/ ^ ^ d'2' ^ 
 
 By means of these relations, and also the equations (III), the 
 preceding equations may be reduced to 
 
 
 ,(IV) 
 
 Now we observe that the position of the center of gravity does not 
 enter into these equations either explicitly or implicitly. 
 
 If then the center of gravity of the body were fixed, and the body 
 were acted on at the same points by the same impressed forces that 
 act on it when it is free, the equations of motion would be the same, 
 since the forces introduced by the condition of the center of gravity 
 being at rest would all act at the center of gravity, the co-ordinates 
 of their points of application would be zero, and they would therefore 
 not enter into the equations. 
 
 Hence then we conclude that the motion of the body about its 
 center of gravity is the same as if the center of gravity were fixed, 
 and the body acted on by the same impressed forces. 
 
 These two results are expressed by saying that motions of 
 translation and rotation are independent. They are of the utmost 
 importance in the solution of every problem about the motion of one 
 rigid body. 
 
VI.] A TREATISE ON DYNAMICS. 137 
 
 We will for distinctness enunciate them again. 
 
 When a body is in motion under the action of any forces, its 
 center of gravity moves as if the whole mass were collected there and 
 acted on by iill the forces which act on the body. And the motion 
 of the body about its center of gravity is the same as if the center of 
 gravity were fixed, and the body acted on by the same forces that do 
 act on it 
 
 94. The equations (IV) involve the co-ordinates of every par- 
 ticle in the body. To determine from them the motion of the body, 
 they must be reduced to others containing only co-ordinates common 
 to the whole body. 
 
 We shall not enter upon this reduction in the general case at 
 present, as the process is complicated, but shall confine our attention 
 to the cases where all the particles of the body move in parallel planes. 
 
 Let the plane of xi/ be that to which the motion is parallel ; then 
 the ordinate parallel to z of every particle is constant. Equations 
 (IV) are therefore reduced to 
 
 or, 2,«(^x'— -y^j^2(x'I-yZ). 
 
 Let x' = r cos d, y' = r sin 0, 
 
 then for each particle r is constant ; so that we have 
 
 d-x' . .,rQ aM^\' 
 
 -^ = -rs.ne^-rcose[-), 
 
 cVy' .(f-d . ./ddV 
 
 dt^ dl- \dtj 
 
 Making these substitutions, we have 
 d^O 
 
 Now since it is a rigid body — , and therefore j-r is the same 
 
 for every particle of the body, we may therefore place it before 2. 
 So that we have 
 
 '^^j ^mr^ = ^{x'Y-y'X). 
 
 Now tlie right-hand side of this equation is the resultant moment 
 of the impressed forces round an axis through the center of gravity 
 
138 A TREATISE ON DYNAMICS. [CHAP. 
 
 perpendicular to the plane of motion; calling this L and putting 
 Mk^ for 2r«r^ we have 
 
 at 
 Combining with this the first two of equations (III), we have 
 
 
 (V) 
 
 These three equations are sufficient to determine the motion of a 
 rigid body which takes place in one plane, whenever the forces 
 which act on it are given as functions of the variables. 
 
 This is seldom the case. Unknown forces generally enter into 
 these equations, arising from conditions to which the motion of the 
 body is subject. There will, however, in every case be a geometrical 
 equation corresponding to each unknown force so introduced, so 
 that the number of equations will always be equal to the number of 
 unknown quantities. 
 
 In effecting this last transformation all the geometrical conditions 
 of the rigidity of the body were introduced when we considered r 
 
 to be constant for each particle, and -j- to be the same for all the 
 particles. 
 
 95. In the preceding reduction the expression j-^'Lmr^ occurs, 
 
 where r is the distance of the particle m from a certain fixed line 
 in the body, vir^ is called the "Moment of Inertia" of the particle 
 m round this line, and 'Zmr^ is the moment of inertia of the whole 
 body round the same line ; it is the sum of the moments of inertia 
 of every particle. This quantity will frequently occur; it is different 
 for different bodies and for different lines in the same body. It is 
 generally written MF, in which case k is called the "Radius of 
 Gyration" of the body round the particular line. The Moment of 
 Inertia of any body may be found by the ordinary methods of inte- 
 
 j a 
 
 gration. Again, — is called the angular velocity of the body ; if we 
 
 conceive a plane fixed in the body perpendicular to the plane of 
 . motion to be inclined at an angle to a fixed plane also perpen- 
 
VI.] 
 
 A TREATISE ON DYNAMICS. 
 
 139 
 
 dicular to the plane of motion, -7- is the rate at which the angle 6 is 
 increasing, and the propriety of the term angular velocity is manifest. 
 Sometimes -jt, is called the angular accelerating force. 
 
 96. Let us now take an example of the application of these 
 equations in the case of motion in one plane. 
 
 A uniform heavy rod slides down between a smooth vertical and 
 a smooth horizontal plane, to determine the motion. 
 
 Let the figure represent the 
 rod at the time t. 
 
 AB = 2a, 
 
 DN=x, NC = y, 
 
 ACN=d, 
 
 M the mass of the rod, 
 
 R, K' the reactions of the 
 planes, then from equations (V) 
 
 we have 
 
 >4-^'.. 
 
 
 Mk 
 
 de 
 
 Ra smd-R'a co&Q 
 
 (1) 
 •(2) 
 .(3) 
 
 and corresponding to the two unknown forces R, R' we have the 
 two geometrical relations 
 
 x = a5\nd, y = acosB, (4) 
 
 which express that the ends of the rod are in contact with the 
 planes. 
 
 Eliminating R and R' from the equations, we get 
 
 ^j^^fd^^dx d^ydj^ d^de\_ dy 
 
 ^^^ W dt'' dt' dt^^deTtJ-'^^^Tf 
 
 Integrating this, we have 
 and using equations (4), 
 
 <--')e 
 
 C — 2ag COS0. 
 
140 A TREATISE ON DYiSAMICS. [cHAP. 
 
 If we suppose the sliding to commence when the rod is vertical, 
 
 we have -r-=0 when 6 = 0: 
 at 
 
 0=C~2ag; 
 dey 2ag . .. 
 
 dtj a^ + k' 
 
 dd 
 dl 
 
 V a' + k' 
 
 (5) 
 
 Or, since k^ — -^ 
 
 dd_ /Si 
 dt~\ a 
 
 H 
 
 which gives the angular velocity in any position ; the equations 
 dx ^dd dt/ . „dd 
 
 dJ=''''''^irt^ 57=-^^^"^d7' 
 
 give the velocity of the center of gravity. 
 The integral of equation (5) is 
 
 log tan ? = . /5 t + C. 
 
 On attempting to determine C by the condition used beforej 
 we get C = — CO . This might have been expected since the position 
 from which the motion was assumed to commence is one of equi- 
 librium, so that the motion would not take place at all. We may, 
 however, suppose the motion to commence in a position differing 
 very slightly from that of equilibrium, in which case the velocity 
 we have obtained will only be affected by a small quantity of the 
 same order of magnitude, and C will be rendered finite : or we may 
 suppose a velocity equal to that indicated in the solution to have 
 been communicated to the rod in the corresponding position. 
 
 To find the pressures on the two planes in any position, we have 
 
 \-n) •= x^ (1 -cosy); 
 \dtj 2a ^ ^' 
 
 d'0 3g . . 
 dv 4« 
 
 also from (4) a' = a sin (), y — a cos Q ; 
 
 d^x So- . ^, 
 .•.-^=-^sm0(3cos0-2), 
 
 i| = -?l(l+2cosa-3 cos^ &), 
 at 4 ' 
 
VI.] A TREATISE ON DYNAMICS. 141 
 
 substituting these values in equations (1) and (2), we have 
 
 R'=.^-^ sm 6(3 cos 0-2), 
 4 
 
 R=—^(l-6cosd + 9 cos' e), 
 
 Mo- 
 = — ^ {1 + 3 cos e (3 cos 6 - 2)}, 
 
 which give the pressures on the planes corresponding to any value 
 of 0. 
 
 When S cos 6 — 2 = 0, R' = 0, and as 6 increases R' becomes 
 negative : this result shews that a force would be required to keep 
 the point B in contact with the vertical plane : as this force is not 
 supposed to exist the rod will at that point leave the plane, and the 
 motion will be different afterwards. 
 
 From the expression for R we see that it continues positive up to 
 this point. 
 
 To determine the motion after the rod leaves the plane BD we 
 have the equations 
 
 M2 = R-Mg, 
 
 Mk'~=Rasm0, 
 
 y — a cos 6. 
 
 dx 
 From the first equation it appears that -j- remains constant Avith 
 
 the value it had when the rod left the plane. 
 Now at that time 
 
 dx ,dd 
 
 Tt=''''''^dt' 
 
 = cos0y^(l_cos0), 
 
 and putting for cos 6 its value | we get 
 
 This will continue to be the velocity of the center of gravity in a 
 horizontal direction. 
 
142 A TREATISE ON DYNAMICS. [CHAP. 
 
 From the other equations we have 
 
 .-. d" (sin^ + 1) (^Y= C-^ag cos Q. 
 Now when the rod left the vertical plane 
 
 ... (3sin^0.l)Q^|f(8-9cos0), 
 
 which gives the value of -j- in any position, and we may find the 
 value of R as in the previous case. 
 
 97- When the motion of every particle is parallel to one plane, 
 we have only the three equations (V) instead of the six equations 
 (III) and (IV). 
 
 These six equations however must always be satisfied, let us 
 therefore consider what they become in this case. 
 
 The last of equations (III) becomes 
 2Z = 0, 
 which shews that the sum of the resolved parts parallel to the axis of 
 z of all the forces which act on the body must be zero. 
 
 If the body is free this is one of the conditions that must hold 
 among the forces acting on it that the motion may be of the kind we 
 have supposed. 
 
 If the body is constrained to move in the manner supposed this 
 will be one of the equations which determine the forces called into 
 action by this constraint. 
 
 The first two of equations (IV) become 
 
 2:,«.'g- = 2;(/7-yz), 
 
 ^mz' -y-^ = ^{z'X-x'Z). 
 
 Now from the relations 
 
 x' = r cos d, v' = r sin d. 
 
VI.] A TREATISE ON DYNAMICS. 143 
 
 the left-hand sides of these equations can be expressed in terms 
 
 of -J- and T— , which are known by (V) ; and the equations then 
 
 give two more conditions to be satisfied by the impressed forces. 
 
 Thus whenever the motion is of this sort, the six equations (III) 
 and (IV) are reduced by relations between the impressed forces to no 
 more than three independent equations. 
 
 98. It frequently happens that the conditions of equilibrium of 
 the system under consideration have been found in a form simpler 
 than the six general equations of equilibrium. Now, as in consi- 
 dering any particular case of equilibrium we may employ either the 
 six general equations, or the more simple ones that have been 
 deduced for the class to which the particular case under considera- 
 tion belongs, so we may employ either set of equations of equilibrium 
 to form the equations of motion. 
 
 The case of a body moving about a fixed axis affords an illus- 
 tration of this remark, and deserves consideration from its own 
 importance. 
 
 In the case of a body moveable about a fixed axis, we may 
 determine the conditions of equilibrium from the six general equa- 
 tions, in which case we introduce unknown forces for the pressures 
 exerted by the axis on the body ; or we may take the condition 
 which has been deduced from these, that the body will be in equi- 
 librium when the resultant moment round the fixed axis is zero. 
 
 We will consider the motion of a body about a fixed axis in both 
 these points of view. 
 
 Let r be the distance from the axis of a particle whose mass is m, 
 since its motion is at every instant perpendicular to the axis and the 
 radius vector, the resolved part of the effective force in this direc- 
 tion is 
 
 (Ps , . - cVe 
 
 m-, which = ^r^^^,. 
 
 If therefore we apply a force equal to this in the opposite direction, 
 
 72/1 
 
 its moment round the axis will be — mr^ —-^ . 
 
 Let L be the whole moment of the impressed forces, then the 
 condition that the whole moment round the axis is zero gives the 
 equation 
 
144 A TREATISE ON DYNAMICS. [cHAP. 
 
 or, since -y— /and therefore— -^ is common to every particle of the 
 system 
 
 or, putting Mk^ for 2m r' 
 
 iV«-^=L. 
 
 From this equation the motion of the body may be completely 
 determined. 
 
 We will now see how the same result may be obtained from the 
 six general equations. 
 
 Let the fixed axis be taken as the axis of z, and a plane perpen- 
 dicular to it through the center of gravity for the plane of xt/; let 
 X, y be the co-ordinates of the center of gravity, Q the angle which 
 a line joining the center of gravity and the origin makes with the 
 axis of .r. 
 
 We may suppose the body to be fixed to the axis at two points, 
 let these be at distances c, and c' from the origin, and let the re- 
 solved parts parallel to the axes of the forces which these points 
 exercise on the body be -R^, Ky, jR,, J?/, Hy, -R/. 
 
 Then we have from equations (III), since -r-j — 0, 
 M^ = 2X4-i?. + i?,' (1) 
 
 3f^ = 2:F+2?, + i?; (2) 
 
 = 2Z + 7i', + i?/ (3) 
 
 df 
 
 d^z 
 also from equations (II), since ,72 =0 foi* every particle, we have 
 
 -cE,-c'i?/+2(^Z-.y) + 27«.|^ = (4) 
 
 cR, + c'RJ + ^{zX-xZ)-l.mz^^ = (5) 
 
 ^{xY-yX)-^(^nx^,-my^:;) = (6) 
 
 equation (6) may be reduced to 
 
VI.] A TREATISE ON DYNAMICS. 145 
 
 This is the same as the equation 
 
 which was obtained by the other method : it is sufficient to deter- 
 mine the motion. 
 
 The remaining five equations enable us to determine the un- 
 known forces /?,, Ry, RJ , RJ , and R^ + R/ ; just as in the statical 
 problem the general method gives the pressures on the axis, while 
 the particular method tacitly eliminates them. 
 
 We will return to these equations, and put them into a more 
 convenient form for determining the unknown pressures in particular 
 cases, but for the present will consider the motion of the body. 
 
 99. A particular case of motion round a fixed axis worthy 
 of consideration is where the only impressed force is gravity, and the 
 axis is horizontal. 
 
 Let h be the distance of the center of gravity from the fixed 
 axis, 9 the angle between a vertical plane through the axis, and a 
 plane through the axis and the center of gravity. 
 
 Then L =-Mgh sin 6, so that the equation is 
 
 •••(; 
 
 :^:)'=^-f^-^ (^)- 
 
 C must be determined from the angular velocity corresponding to 
 some known value of 6. 
 
 Now the equation of motion of a point in a circular arc of radius 
 I is 
 
 comparing this with equation (l) we see that they are identical, if 
 
 '4- 
 
 Hence then the time of oscillation of the rigid body will be the 
 
 same as that of a particle attached to a string whose length is -j , 
 
 for the same amplitude. Tliis is called the isochronous simple pen- 
 dulum, the body itself being called a compound pendulum. 
 
 10 
 
146 A TREATISE ON DYNAMICS. [cHAP. 
 
 The equation . -rji+-jj sin = 
 
 can only be solved so as to give the i-elation between & and t \n a. 
 series. 
 
 When however Q is always small, so that powers higher than the 
 first may be neglected, we can find an approximate solution. 
 Writing for sin d, which amounts to neglecting 0\ we have 
 
 l-^4^^- (^)^ 
 
 Let the body start from rest when 6= a, then 
 
 a = A cos B ; . - 
 
 .-. jB = and A = a: 
 
 a COS . / ~ t ; 
 
 ■when 6 = we must have 
 
 A''=(^->>i= 
 
 let ^1, ts, &c. be the successive corresponding values of t, then we 
 have _ 
 
 '^-" SI Rh' 
 
 2 V gh 
 
 _S7r 11^ 
 
 ~ 2" V gh 
 _57r 111^ 
 
 ~ % SI gh 
 
 1^ 
 
 This shews that the center of gravity of the body will attain the 
 loAvest position after successive intervals of tt sj — j ' 
 
VI.] A TREATISE ON DYNAMICS. ^ 147 
 
 We also see that, to the order of approximation, to which we have 
 proceeded, the time is independent of the value of o, or the ampli- 
 tude of the oscillation. 
 
 We shall return to this subject afterwards when we treat of pen- 
 dula, and shall then shew how a more approximate value of the 
 time of oscillation may be obtained; before leaving it, however, there 
 are a few general properties which deserve notice. 
 
 Let the figure represent a section 
 of the body made by a plane through 
 its center of gravity perpendicular to the 
 axis round which it oscillates ; and let C 
 be the point in which the axis cuts this 
 plane, G the center of gravity. 
 
 The two equations 
 
 will be identical if Z = -7- . 
 h 
 
 If therefore we take in CG produced a point such that CO = I, 
 the position and motion at any time will be the same under the same 
 initial circuiftstances as if the whole mass were collected at 0. 
 
 O is called the center of oscillation. 
 
 If k^ be the radius of gyration round an axis through G parallel 
 to the fixed one through C, 
 
 and therefore I = -^ + h. 
 h 
 
 Now if the body were suspended by an axis through parallel 
 
 to the same axis, the length of the corresponding isochronous simple 
 
 pendulum would be 
 
 which is equal to I. 
 
 Hence then oscillations about this axis take place in the same 
 time as those of the same amplitude about the first axis through C. 
 
 C is called the center of suspension, and this property is ex- 
 pressed by saying that the centers of oscillation and suspension ai'e 
 reciprocal. 
 
 10-5 
 
148 A TREATISE ON DYNAMICS. [cHAP. 
 
 This property might also have been deduced in the following 
 manner. Suppose it required to find the distance from G of an 
 axis parallel to a given direction, about which the oscillations will 
 take place in the same time as those of a simple pendulum whose 
 length is /. 
 
 Let k be this distance; then h will be determined from the 
 equation 
 
 or h^-lh + ki'' = 0. 
 
 Now this being a quadratic equation gives two values of h, 
 hi and li^ such that hi + hi = /. 
 
 So that an oscillation about an axis at distance h^ takes place in 
 the same time as one about an axis at distance l-h^. 
 
 Also, since in this investigation nothing has been introduced to 
 indicate in which direction from G the required axis lies, we con- 
 clude that any direction will satisfy the condition. If therefore with 
 center G we describe circles in the plane of the paper at distances 
 GO and GC, small oscillations will take place in the same time about 
 any parallel axis through any point in either of these circles. 
 
 The value of h which will make /, and therefore the time of 
 
 oscillation a minimum may be easily determined : since 
 
 k ^ 
 l^^ + h, 
 
 that I may be a minimum, we have 
 
 k * 
 -^ + 1=0, 
 
 or h = ki, 
 and therefore l = 2h or S^i- 
 
 In this case therefore the two circles we have mentioned 
 coincide. 
 
 The axes determined by these conditions are not axes about 
 which the time of oscillation is the least possible for the body, but 
 only for axes in the body parallel to a given direction. To find those 
 about which it will be absolutely the least, we must select that 
 direction for which k is the least. This we know will be one of the 
 principal axes through the center of gravity of the body. 
 
A TREATISE ON DYNAMICS. 149 
 
 CHAPTER VII. 
 
 100. To find the conditions of equilibrium of a system of rigid 
 bodies we have for each body of the system six equations of equi- 
 librium, as if that particular body were the only one of the system. 
 And besides these we have equations expressing the geometrical 
 connexions of the bodies. 
 
 The same method must be adopted to determine the motion of a 
 system of rigid bodies ; we must write down for each body of the 
 system the six equations (III) and (IV), or the three equations (V), 
 and then the equations expressing the geometrical conditions which 
 the bodies satisfy. 
 
 When the equations are once written down the difficulties of 
 solving them are merely analytical, and such artifices must be used 
 as the forms of the equations suggest. 
 
 The constants introduced in integration must be determined in 
 the same way as in the case of a single body. 
 
 When any system is in equilibrium we may either consider each 
 body separately, and write down for it the six equations of equi- 
 librium ; in which case the actions of the other bodies of the system 
 on it will enter as external forces ; or we may consider the whole 
 system as one body and write down for it the six equations of equi- 
 librium; in which case the mutual actions of the different parts of 
 the system will not appear in the equations; or we may consider 
 any two or more of the bodies as one, and write down for them the 
 equations of equilibrium. 
 
 These different methods may also be adopted in Dynamics. The 
 dynamical equations, as first written down, are strictly equations of 
 equilibrium, and it is only from the analytical character of the 
 quantities that enter them that they enable us to determine the 
 motion of the system. 
 
 Though the methods to be employed in solving the equations 
 of motion must in each case be suggested by the forms of those 
 equations, there are certain artifices by which the first integrals may 
 often be obtained, the applicability of which can be determined at 
 once from an inspection of the system. The difficulty generally 
 arises from there being unknown forces which have to be eliminated 
 
150 A TREATISE ON DYNAMICS. [CHAP. 
 
 by means of geometrical relations. These artifices enable us in 
 certain cases to effect that elimination at once. 
 
 101. When a body or system of bodies is in motion under the 
 action of any forces, if x, y, i are the co-ordinates of the center of 
 gravity at the time t, and M the mass of the system, we have the 
 equations 
 
 
 (III) 
 
 in which no forces appear but such as arise from causes external to 
 the system ; that is, no pressure of one part of the system against 
 another enters, no mutual attraction, no tension of a string con- 
 necting two parts of the system. But all forces do enter which 
 arise from causes external to the system, as pressures of fixed sur- 
 faces, or fixed points, tensions of strings passing over fixed pulleys, 
 &c., together with the given external forces whatever they may be. 
 Now equations (III) shew that when 
 
 2X=0, 2r=0, 2Z = 0, 
 the center of gravity will move uniformly in a straight line. Thus, 
 whatever the internal forces of the system, so long as there are no 
 external forces the center of gravity will move in a straight line 
 with uniform velocity. This is called the Principle of the Con- 
 servation of the motion of the center of gravity. 
 
 dx 
 
 We see from equations (III) that if SX= 0, j- is constant, what- 
 ever 2 Y and 2Z are. Hence if the resolved parts of all the external 
 forces actino- on a system parallel to any line have a resultant zero, 
 the motion of the center of gravity parallel to that line will be 
 uniform. Similarly, if two of them vanish the resolved part of the 
 motion parallel to that plane will be uniform and rectilinear. Thus, 
 for instance, if any number of balls be piled up on a perfectly smooth 
 horizontal plane and then left to themselves, they will be acted on 
 by no external horizontal force, they will therefore fall down in 
 such a manner that their center of gravity will describe a vertical 
 line. 
 
 In the cases that will most frequently occur the center of gravity 
 of the system will be at rest at the commencement of the motion, 
 and will therefore continue so throughout. 
 
VII.] A TREATISE ON DYNAMICS. 151 
 
 102. The next principle that we shall mention depends on 
 equations (II), which may be written 
 
 Whenever the right-hand sides of these equations are zero the 
 equations themselves become 
 
 _ / d'x d'z\ ^ 
 ^ / d'y d'x\ ^ 
 
 the integrals of which are 
 
 ^ ( dz dy\ , 
 
 .(1) 
 
 Sot 
 
 (2) 
 
 Now if A^ be the area described in any time by the projection 
 on the plane of yz of the line joining the origin and the pai'ticle 
 whose co-ordinates are x, y, z, 
 
 ^ dt dt dt ' 
 Employing a similar notation for the other co-ordinate planes, 
 and substituting in equations (2), we have 
 
 from which 2 2rn^, = /«,< + C,, 
 
 (3) 
 
152 A TREATISE ON DYNAMICS. [CHAP. 
 
 or, if we suppose J^, &c., to be the areas described since the instant 
 from which t is measured, 
 
 2'2mA^ = hJ,[ (4) 
 
 2l.mA, = kst.) 
 
 In these equations or in equations (3), consists the principle 
 which is called the Principle of the Conservation of Areas. 
 
 We may state it in words as follows : 
 
 The area described by the projection on the plane o? yz of the 
 radius vector of any particle, is called the area described by the 
 particle round the axis of x. Since any fixed line may be taken as 
 the axis of x, this definition is applicable to any line. In certain 
 cases the sum of the products of the mass of each particle of the 
 system, and the area described by that particle round some fixed 
 line is proportional to the time; whenever this is the case, the 
 principle of the conservation of areas is said to hold for that system, 
 round that line. 
 
 This may be the case for only one line, or for any line whatever, 
 or for lines satisfying certain conditions ; let us consider generally 
 how to determine in what cases it does hold. 
 
 We see by the equations from which it is deduced, that it holds 
 for the axis of x whenever 
 
 ^{yZ-zY) = 0. 
 
 Now in this expression no mutual actions or other internal forces 
 enter. It is the expression for the resultant moment of the impressed 
 forces round the axis of x. The principle will therefore hold for any 
 line round which the moment of the impressed forces is zero. 
 
 First, let there be no external forces, or such as would keep the 
 system in equilibrium in any position, if placed at rest in that 
 position. In this case whatever line be chosen, the moment of the 
 forces round that line is zero, and consequently the principle holds 
 for any line whatever. 
 
 Again, let the resultant of the impressed forces always pass 
 through a fixed point. In this case the moment round any line 
 through that point is zero, and therefore the principle holds for any 
 line through that point. 
 
 If all the impressed forces which act on the system are parallel, 
 the principle will hold round any line parallel to their common 
 direction. 
 
VII.] A TREATISE ON DYNAMICS. 153 
 
 If the resultant of the impressed forces always passes through 
 a fixed line, the principle will hold round that line. It is needless 
 to enumerate any more particular cases. 
 
 103. When the resultant of the impressed forces acting on the 
 system is either zero, or passes always through a fixed point, we 
 have 
 
 2 2m J, = ^3^ 
 
 for any directions whatever of the axes ; and in the former case for 
 any origin, in the latter only when the fixed point is origin. 
 
 hi, h.2, hs, are constants introduced by integration, which may 
 be determined from the circumstances of the motion at some known 
 instant ; and will be different for different axes of co-ordinates. 
 
 If A, fx, V be the direction-cosines of any line passing through the 
 origin, the sum of the products of the masses and areas described 
 by them round this line 
 
 = \.2'2.mA^ + fx.2l.mAy-i-v.Q'2mA, 
 = (\hi + fxh2 + vh3)t 
 
 where ¥ = hi + /?/ + h^. 
 
 Now -T- J -r J -r i^^y he considered as the direction-cosines of 
 
 some line, and if be the angle between this line and that round 
 which the areas are reckoned, the sum in question is h I cos Q. 
 
 The greatest value of this is when cos0= 1, which is the case 
 when 
 
 hi K h, 
 
 ^ = J' "-^ir " = !' 
 
 Hence then the line whose direction-cosines are -j^ , ^, -^ is 
 
 h h h 
 
 such that the sum of the products of the areas round it and the 
 
 masses is a maximum. 
 
 Since its direction-cosines are independent of t its position is 
 
 constant, and from its nature its direction in space is independent of 
 
 the axes to which it is referred. We see therefore that in every 
 
 such system there exists a line whose direction in space is invariable 
 
154 A TREATISE ON DYNAMICS. [cHAP. 
 
 and can be determined at any instant;, from the circumstances of the 
 system at that instant. 
 
 A plane perpendicular to this line is called the " invariable plane/' 
 and the line itself is called the " invariable axis." 
 
 These results agree with those which were determined previously 
 in a particular case. 
 
 The sum of these products round any line inclined at an angle 6 
 to this is ?it cos ; and therefore becomes zero for any of the lines at 
 right angles to this one. 
 
 Many other curious properties of the motion connected with this 
 line might be deduced from these equations, these, however, are the 
 most important. 
 
 104. When a system is in equilibrium under the action of forces 
 X, F, Z, &c. "We have by the principle of virtual velocities 
 
 ^{Xlx+Yly + Zlz)=0. 
 
 We have therefore by D'Alembert's principle for a system in motion 
 
 We will make a few remarks on this equation. 
 
 No internal forces appear in it which arise from invariable 
 geometrical connexions of the parts, that is, which arise from con- 
 nexions of the parts which are geometrically the same before and 
 after the iiidefinitely small displacement which is supposed to take 
 place. Such, for instance, as the tensions of flexible and inextensible 
 strings ; the pressures of smooth surfaces which continue in contact, 
 or of rough surfaces where the displacement may have been sup- 
 posed to take place by rolling ; the pressures of fixed points, &c. 
 Also we may omit any external forces, the displacements of the 
 points of application of which are such that their virtual velocities 
 ai*e zero. 
 
 Now since in this equation the displacement and therefore the 
 values of Zx, oi/, &c, are arbitrary, being subject only to the condi- 
 tion of not violating the geometrical relations referred to above, we 
 may suppose the displacement to be that which actually takes place 
 in the indefinitely small time ht, that is, for ex, by, Iz 
 
 .^ dx^, dy ^, dz ^ 
 
 we mav write -7- d ^ , -~-ot, -y.ct, 
 
 dt at dt 
 
VII.] A TREATISE ON DYNAMICS. 155 
 
 provided the geometrical relations of the system at the beginning 
 and end of the time ^t are the same. The equation thus becomes 
 _ fcPx dx d'y dy d^z dz\^^ -f^dx ^dy rydz\^^ 
 
 the integral of which is 
 
 Hit) * (Mj - (s)} - ^ ^ ^ ^^ ('^''^ - ^''^ ^ ""^- 
 
 or 27W v»= C + 2 /2 (Xdx + Ydy + Zdz). 
 
 Now in this equation no forces appear which are either internal 
 forces such as we have already mentioned, or external forces such 
 that their virtual velocities arising from the actual displacement are 
 zero. Such forces are the tensions of inextensible strings attached to 
 fixed points ; pressures of smooth fixed surfaces ; pressures of fixed 
 points against smooth surfaces, &c., where the actual displacement 
 of the point of application of the force is perpendicular to the direc- 
 tion of the force ; and also forces where there is no displacement of 
 the point of application of the force, as when a body moves about a 
 fixed point or axis ; or rolls without sliding on a rough surface, &c. 
 
 We may remark that the internal forces do not enter into the 
 equation, because if they did for each force there would be an equal 
 force whose virtual velocity would have a contrary sign, so that they 
 would enter in pairs which would destroy each other ; and that the 
 external forces which we have mentioned do not enter because the 
 virtual velocity of each is zero. 
 
 The product of the mass of a particle and the square of the 
 absolute velocity with which it is moving is called the vis viva of 
 the particle. 
 
 Hence, then, ^mv" is the vis viva of the whole system, and 
 27«y= = C + 2/2 {Xdx + Ydtj + Zdz) 
 
 is an equation which gives the vis viva of the whole system in any 
 position, whenever the integration on the right-hand side can be 
 performed. This is easily done in most of the cases that will occur 
 in practice. 
 
 In order that the integration may be possible, the expression 
 2 {Xdx + Ydy + Zdz) 
 must be a perfect differential of some function of the co-ordinates of 
 the different particles. 
 
 This will be the case whenever the forces X, F, Z, &c. are 
 constant, or arise from the attractions of fixed centers, or from the 
 
156 A TREATISE ON DYNAMICS. [cHAP. 
 
 mutual attractions of the different particles of the system, with forces 
 
 varying as some powers of the distance. It will not be the case 
 
 when the forces arise from the attractions of moveable centers not 
 
 forming part of the system, or when the forces are functions of the 
 
 velocities, as when the motion takes place in a resisting medium, &c. 
 
 Let it be a perfect differential, and let its integral be 
 
 <P (-^i? ^i> Zi, a^s, t/s, Sg. . .), 
 
 then ^mv" = C + 2(p (or,, t/^, 0, . . .) 
 
 Let Oj, bi, Cj. . . be the values of .Tj, ?/„ ^,. . . when the velocities 
 of the different particles are F^, F^.. . then 
 
 Stwd^ - Stw F' = 20 (x„ y,...)-2<p («„ i, , . .) 
 
 This equation shews that the change in the vis viva of the system 
 which takes place in any time depends only on the co-ordinates of 
 the particles at the beginning and end of that time, and not on their 
 velocities or directions of motion. 
 
 This is called the Principle of vis viva. 
 
 If there are no forces external to the system but such as do not 
 enter into the equation of virtual velocites, that is, if 
 
 ^{Xdx + Ydy + Zdz) = 0, l.mv^= C, 
 
 or the vis viva of the system is constant. This is called the Principle 
 
 of the Conservation of vis viva. 
 
 It is convenient to express the vis viva of the system in terms of 
 
 that due to the motion of translation of the center of gravity, and 
 
 that due to the motion of rotation about it- 
 Preserving the notation already used, and writing Ic + x' for x, 
 
 &c., we have 
 
 dx 
 
 dx dx' 
 
 Tt 
 
 '^Tt'-'dl 
 
 dy 
 
 _A_l dy' 
 
 dt 
 
 dt dt 
 
 dz 
 
 dz dz' 
 
 dt 
 
 = Tt^-di 
 
 and substituting these, we get 
 
 .."^^^,4^}, 
 
 dt dt dt dt 
 
VII.] A TREATISE ON DYNAMICS. 157 
 
 as the expression for the vis viva ; or bearing in mind that x, 'y, z are 
 the same for every particle of the system, and also that 
 1.mx'=0, 'Lmy' = 0, 2wz'=0, 
 
 and therefore 2»j -y- = 0, 2 m -^- = 0, Srn -^- = 0, 
 at at at 
 
 we have 
 
 Now in whatever manner a body is moving, its motion at any 
 instant may be considered as composed of a motion of translation 
 of the center of gravity, and a motion of rotation romid some line 
 through the center of gravity, the direction of which will in some 
 instances be constant, in others will be continually changing. Let v 
 
 be the velocity of the center of gravity, -j- the angular velocity of 
 
 rotation, and r the distance of a particle from the line through the 
 center of gravity round which this takes place ; then the expression 
 for the vis viva becomes 
 
 or 3Iv'+Mk'(^J, 
 and the equation will be 
 
 M I F + k' (^J U C + 2/2 (Xrfo; + Ydy + Zdz). 
 It must be here carefully borne in mind, that in the general case 
 the axis about which -j- is estimated is continually changing its 
 
 position and direction in space. 
 
 This method of expressing the vis viva will be of use only when 
 we can tell, a jmori, the direction of this axis of rotation, as in the 
 case of motion in parallel planes ; or, as it is commonly called, space 
 of two dimensions. 
 
 The principles just proved will greatly assist us in the solution of 
 problems. We will now proceed to explain the manner in which 
 they should be used. 
 
 105. Suppose that the system consists of one rigid body, and 
 that the motion is in parallel planes. 
 
 We must first write down the equations (V) with the proper 
 forces expressed in them. We must then count how many unknown 
 
158 A TREATISE ON DYNAMICS. [cHAP. 
 
 quantities appear in thenij including co-ordinates and unknown 
 forces. Suppose the whole number to be n; then^ to determine 
 these n unknown quantities, we have the three equations (V) ; we 
 must therefore have n — 3 additional equations, expressing geo- 
 metrical relations which exist between the different parts of the 
 system. 
 
 The direct method of proceeding now is to solve these equations 
 by any analytical artifices that suggest themselves. The unknown 
 forces however may sometimes be eliminated very easily by means 
 of some or all of the preceding principles. 
 
 We must therefore examine w^hich of the above principles hold ; 
 or in other words, which of the equations expressing the above 
 principles will be free from unknown forces. These will give us 
 so many first integrals of the equations : that is, so many relations 
 between the positions and velocities of the different pai-ts of the 
 system. Sometimes we obtain all the first integrals by means of 
 these principles, sometimes it is necessary to combine particular 
 artifices wth them. 
 
 If we can perform the next integration the problem is completely 
 solved, that is, the position, velocity, and direction of motion, are 
 completely determined as functions of the time : this however can 
 seldom be effected. 
 
 No more exact rules than these can be given. A facility in 
 applying thera to particular cases is only to be acquired by practice. 
 
 If the system consists of more than one body, we must write 
 down the equations of motion for each separately, and then solve 
 them by the aid of the general principles, as in the case of a single 
 body. 
 
 We may remark that in the cases where the general principles 
 are applicable we might obtain the first integrals from them at once, 
 without using the differential equations of motion of the second 
 order. These however should always be written down. 
 
 106. We will now illustrate the application of these principles 
 by an example of the method of determining the motion of two 
 bodies. 
 
 A rough cylinder is placed with its axis horizontal on a rough 
 inclined plane, which is itself moveable on a smooth horizontal 
 plane ; to determine the motion of the system. 
 
 Let a be the radius of the cylinder, M its mass; a the inclination 
 of the plane AB, m the mass of the plane ; a fixed point in the 
 
VII.] A TREATISE ON DYNAMICS. 159 
 
 horizontal plane coinciding with A at the beginning of the motion, 
 when the point JE coincided with D. 
 
 O -"i 
 
 ON=x, 
 
 OA=x', 
 PCE = d, 
 AD^L 
 R and F the reactions of the plane on the cylinder along PC and 
 PD. Those of the cylinder on the plane will be equal and in the 
 opposite directions. 
 
 The equations of motion for the cylinder are 
 
 M^ =Fcosa 
 dt 
 
 M 
 
 Mk 
 
 d^ 
 df 
 
 df' 
 
 l^sina (1) 
 
 Fsma + Rco&a- Mg.. . ...(2) 
 
 F» (3) 
 
 and for the plane 
 
 m —j-^ = Rsina — F cos a , 
 at' 
 
 (4). 
 
 These equations contain six unknown quantities, we must there- 
 fore seek for two more equations. These will express that the 
 cylinder is in contact with the plane, and that it rolls without 
 sliding. 
 
 The first gives 
 
 (x — x') tan a + a sec a = i/ (5). 
 
 The second gives 
 
 (x — x') sec a +a tan a + ad = I (6). 
 
 These six equations when integrated will determine the motion 
 completely. Since we do not know Avhether R and F are constant 
 or not, it is necessary to eliminate them before we can integrate. 
 
160 
 
 A TREATISE ON DYNAMICS. 
 
 [chap. 
 
 Now in this case the principle of vis viva is applicable, and also 
 the principle of the conservation of the motion of the -center of 
 gravity in a horizontal direction. 
 
 These principles therefore guide us to the method of elimination. 
 Adding (l) and (4) we have 
 
 M 
 
 d'cc 
 df 
 
 dW 
 dt' 
 
 0, 
 
 the integral of which is 
 
 , -. dx dx' 
 dt dl 
 
 C = 0.. 
 
 •(7). 
 
 This is the expression of the latter of the two principles. 
 Again, from all the equations we have 
 
 ^YTt df^^ dtlii'^^'' dtde]^^'"" dt de- ^^^^ df 
 
 which when integrated gives 
 
 At the beginning of the motion 
 
 = C- SiV/g (Z sin a + a cos a) ; 
 
 This is the expression of the former principle. 
 From equations (5) and (6) we have 
 /dx dx'\ dy 
 
 '^"""[Tt-ltj^di' 
 
 fdx dx\ dd ^ 
 and sec«(^^--^J4-a^ = 0. 
 
 From these equations and (7) we obtain 
 ma cos a dd 
 
 dx 
 It 
 
 d£_ 
 dt 
 
 dy 
 dt' 
 
 M + m dt 
 Ma cos a dd 
 M + m U' 
 
 . dd 
 
 (9) 
 
 also k^ 
 
VII.] A TREATISE ON DYNAMICS. 161 
 
 Substituting these values in equation (8), we have 
 3ma + Ma 
 M 
 the integral of which is 
 
 3ma + Ma (1+ 2 sm^ a) /ddV , . 
 
 =rr^^ -j-J = ^sr sin a . d, 
 
 M + m \dtj * ' 
 
 t)= {M + 7n)gsma ^„ 
 
 3ma + Ma{l +2sin'a) 
 The constant is zero, since ^ — when t = 0. 
 g sin a 
 
 JfA = 
 
 3m a + Ma (1 + S sin* a) ' 
 d = A{M + m)t^; 
 
 .'. ~^=2A{M+m)t', 
 
 therefore, from equations (9), we have 
 
 -r- = — 2A7na cos a . t, 
 at 
 
 dx' 
 
 -7- = 2 AMa cos a . t, 
 
 ^-^ ==-2A{M + m)asina.t; » 
 
 from which x, x' and y may be found in terms of t. 
 
 From these equations it appears that the motion both of the plane 
 and cylinder is uniformly accelerated. Also, if we differentiate these, 
 and substitute in equations (3) and (1) we shall obtain F and R; and 
 it will be found that they are constant. 
 
 Again, from equations (9), we have 
 
 dy M+m^ 
 
 -f- = tan a ; 
 
 dx m 
 
 which shews that the center of gravity of the cylinder will descend 
 
 in a right line, making with the horizontal plane an angle whose 
 
 . M + m 
 tangent is tan a. 
 
 VI 
 
 Instead of making use of the principle of vis viva to guide us in 
 
 our elimination, we might have proceeded as follows: from (j), (2) 
 
 and (3) 
 
 <fx . d'y ,^d'0 
 
 a cos a -r-j + « sm a j^ — k" ~—- — ag sm a. 
 
 (Xt (It it L 
 
 Integrating this, we have 
 
 dx . dy ,,d6 
 
 dl dt dt ^ 
 
 .-. acosa .X + as\na.y-k^.d=C--agsina.l' ; 
 
 11 
 
162 
 
 A TREATISE ON DYNAMICS. 
 
 [chap. 
 
 also, the integral of (7) is 
 
 Mx + mx'= C, 
 
 from these two equations, with (5) and (6), we can find x, x, y and Q 
 in terms of t. 
 
 There is still another method of proceeding which is always 
 applicable in cases where the geometrical equations are linear with 
 respect to all the variable quantities, and where the equations of 
 motion involve the second differential coefficients only of those co- 
 ordinates, as is the case in the present example. 
 
 From (5) and (6) we have 
 
 tan a 
 
 '(Px _ rfV\ ^ ^ 
 
 M' 
 
 dfj~dt" 
 
 J d'x d'x' d'9 ^ 
 
 Substituting in these equations the values of the second differ- 
 ential coefficients given by equations (1), (2), (3) and (4), we 
 obtain equations which involve only F, R and constant quantities. 
 
 F and R therefore are constant and may be found at once 
 from these equations ; and the equations of motion may be inte- 
 grated at sight. 
 
 This is the shortest and easiest method of proceeding in cases 
 where it is applicable. 
 
 107. As another example we will take the following problem. 
 
 In a smooth tube moveable about one extremity in a horizontal 
 plane, a small ball is placed at a distance a from the fixed end, 
 and an angular velocity w is 
 communicated to the tube: 
 determine the motion. 
 
 Let AB be the tube of 
 length I; P the position of 
 the ball at time t; AC the 
 initial position of the tube; 
 PAN=e, AN=x, 
 NP=y, AP^r, 
 M the mass of the tube, m 
 the mass of the ball, R the ^ 
 reaction between tube and ball. 
 
VII.] A TREATISE ON DYNAMICS. 103 
 
 then for the motion of the ball we have 
 
 m^^ = -Rsme, (1) 
 
 m^ = Rcosd, (2) 
 
 Ma 
 
 and for the tube Mk--^ = -R.r (3) 
 
 We have omitted two of the equations of motion of the tube, 
 because they would introduce two additional unknown forces arising 
 from the condition that A is fixed. 
 
 Here then we have x, y, r, 6, and R connected by three equations, 
 we must therefore seek for two more ; they are 
 
 x—r cos 6, y = r sin 6 (4) 
 
 Now in this case the principles of the Conservation of Areas, and 
 of vis viva hold. 
 
 Conducting our eliminations accordingly we have 
 
 or, transforming to polar co-ordinates, 
 
 Now at the commencement of the motion 
 (7na' + Mk')(o'-=C; 
 
 'S+(mr'+M¥) (^J= {ma' + Mk^ u>' (5) 
 
 Again, "'{^^-y^^.| + ^W^=0. 
 
 From which, integrating and changing to polar co-ordinates, 
 we have 
 
 (mr' + Mk')j^ = C, 
 
 at the commencement of the motion 
 
 (7na^ + Mk')o>=C; 
 de ma' + Mk" 
 
 •■• "".57. 
 
 dt mr" + Mk 
 
 ■2 0) 
 
 (6) 
 11—2 
 
164 A TREATISE ON DYNAMICS. [cHAP. 
 
 J a 
 
 Eliminating -y- from equations (5) and (6), we have 
 
 
 fdr 
 \dt 
 
 Hence the velocity along the tube and the angular velocity cf 
 the tube are known for any position of the particle, and depend 
 only on its distance from A. 
 
 We cannot integrate these equations in finite terms so as to 
 obtain the position in terms of the time. 
 
 108. Hitherto the effective force on any particle forming part 
 of a system has been resolved in the directions of three rectangular 
 axes fixed in space. When the motion of the particle is in one 
 plane it is often convenient to employ polar co-ordinates, and the 
 resolved parts of the effective force in the direction of the radius 
 vector, and perpendicular to that direction. 
 
 The equations of motion of a single particle acted on by a force 
 P along the radius vector from the pole, and a force T perpendicularly 
 to that direction are 
 
 dr de d-6 „, 
 
 ^'''Ttdt^''''dt^-^' 
 
 Hence then from the definition of effective force if r and 6 are 
 the polar co-ordinates of a particle m forming part of a system, 
 the effective force along the radius vector is 
 
 and that in a direction perpendicular to it is 
 
 ^ dr de d'0 
 
 "-'"dtdt'-'"'d?- 
 Another mode of resolving the effective force is also useful, 
 namely, in the directions of the tangent and normal of the path of 
 the particle. These resolved parts are readily obtained as follows. 
 
 The parts parallel to the axes of x and y are »j -r^ and m -~„ . 
 
 ^ ^ -^ dt- df 
 
 Hence the part in direction of the tangent 
 
 ^ d^x dx d^y dy 
 
 dt^ ds dt- ds 
 
 ~^d^\dt^'dt'^d? dt 
 d's 
 
Til.] A TREATISE ON DYNAMICS. 165 
 
 And the part along the uoimal 
 
 d'x dy J-y dx 
 dl ds dl ds 
 
 dj^ ((£21 dx d'x dy\ 
 ~"' ds W dt df dtj' 
 
 Let p be the radius of curvature of the path of the particle, v its 
 velocity 
 
 " d^ dx d'x drf^ 
 dJ 'dl~'dJ~ dt 
 
 and the expression for the force along the normal becomes 
 
 vxv^ m (ds' 
 
 T "'■ p U 
 
 When the particle moves in a circle 7: = ^ and the two pairs of 
 
 expressions coincide Avith each other. 
 
 These expressions for the effective force can in any case be used 
 instead of those referred to rectangular co-ordinates. 
 
 109. These modes of resolving the effective force, afford an 
 explanation of a term, which, originally founded in error, has a ten- 
 dency to convey an erroneous impression, viz.. Centrifugal Force. 
 
 If a smooth straight tube is moved with uniform angular velocity 
 in a horizontal plane about one extremity, and a particle is placed in 
 it, the particle will commence moving from the fixed end of the tube, 
 and will move with accelerated motion till it ultimately flies out of 
 the tube. 
 
 If a particle be fastened by a string to a fixed point on a smooth 
 horizontal table, and then be projected so as to move round this 
 point, it will cause a tension of the string, depending on the mass of 
 the particle and the rapidity with which it moves. 
 
 From these and similar cases, it was concluded that bodies moving 
 round a center have a tendency to fly off from that center, and in 
 consequence exercise a force to which the name centrifugal force was 
 given: and its magnitude Avas found to be mro)', where 7* is the 
 distance from the fixed center, and w the angular velocity with which 
 the body is moving round that center. 
 
166 A TREATISE ON DYNAMICS. [cHAP. 
 
 The true explanation is found in the following method of view- 
 ing it. 
 
 In the former of the preceding examples, let R be the pressure 
 which the side of the tube exerts on the particle. This is the only 
 impressed force on it. 
 
 Then reversing the effective forces on it, we obtain the equations 
 of motion 
 
 „ ^ dr dO d'0 ^ 
 
 ^-^''TtTt-''''df=^' 
 From equation (1) 
 
 mj^ = mr.\ 
 
 which shews that the motion along the tube will be the same as if 
 the tube were at rest, and the particle were acted on by a force mrta- 
 along it. 
 
 Again, in the other case, let T be the tension of the string. 
 
 Applying the effective forces reversed we have 
 
 0, 
 
 : and from the latter 
 
 Hence the first equation becomes 
 T^mru>\ 
 
 That is, the tension of the string is the same as it would be if the 
 particle were at rest and acted on by a force mrio^. 
 
 A similar result will follow in any other case in which the 
 equations are applied to the ntiotion of a particle, either alone or 
 forming part of a system. So that though no such force as centri- 
 fugal force really exists, yet when a system in motion is supposed at 
 rest, and the effective forces are applied in the opposite directions to 
 balance the impressed forces, a portion of one of these effective forces 
 will correspond in direction and magnitude to the fabulous centri- 
 fugal force. 
 
 
 
 -T- 
 
 d'r fddV , 
 -'''7it^-''"'Kdt) =' 
 
 
 
 2 
 
 dr dd d'd ^ 
 
 Now 
 
 ris 
 
 constant, therefore -j- = 
 
 
 equation 
 
 dO 
 
 is constant. 
 
 
 
VII.] A TREATISE ON DYNAMICS. 107 
 
 Thus along the radius vectoi*, the term '"''(y:) in the expression 
 
 (Pr fdey J . ,, , .1, 1. , . mv' 
 -7M-7-5 +wirl — j, and m the normal the whole expression 
 
 correspond to the centrifugal forces in those directions respectively. 
 
 The name " Centrifugal force/' is very objectionable, from the 
 plausibihty of the reasoning by which the idea is supported. But it 
 is found convenient in several classes of problems to have a name for 
 the portion of the reversed effective force represented by inru^, and 
 with this meaning the term centrifugal force is retained. 
 
168 A TREATISE ON DYNAMICS. [cHAP. 
 
 CHAPTEE VIII. 
 
 110. In discussing the elementary principles, it was remarked 
 that there are cases in which the whole effect produced by a force is 
 known J when the magnitude of the force and the time during which 
 it acts are not known ; that is, when we know the definite integral 
 
 / ' Pdt without knowing either P or /o— /j. The name "impulse" 
 
 was given to this definite integral, and the force P was called an 
 impulsive force. 
 
 Let us now consider under what circumstances forces of this sort 
 are called into action. 
 
 We have used the term " rigid body/' and have investigated the 
 motions of rigid bodies in several cases, and have given the equations 
 for determining that motion in all cases. Now the idea which we 
 have attached to the term rigid is this : a body is said to be rigid 
 when all the points preserve the same invariable mutual distances, 
 whatever the forces which act on the different points of the body. 
 This idea of rigidity is suggested by the first touch of external 
 objects ; though a slight examination is sufficient to convince us that 
 it is not strictly applicable to anj' of them. 
 
 Different substances require different degrees of force to produce 
 any sensible change in their form, some require very great force to 
 do so. This approximate rigidity enables us to form the idea of the 
 perfect quality, even though there is no substance in existence 
 endued with that quality ; and a great many substances are so nearly 
 rigid as to convince us that calculations effected on the hypothesis 
 of their perfect rigidity cannot be affected with sensible errors on 
 account of the deviations from it. 
 
 In the branch of the subject however, which is now under con- 
 sideration, this deviation from rigidity forms a principal feature of 
 the problem. When pressure is exerted on a body by any means, 
 the body slightly changes its form, or is compressed ; also when the 
 pressure ceases to act, the body wholly or partially recovers its 
 original form. When a ball in motion strikes another ball at rest, a 
 pressure immediately takes place between the two balls, each ball 
 pressing on the other, and so flattening it at the point of contact. 
 This pressure is gradually communicated from one particle to 
 
Vm.] A TREATISE ON DYNAMIC'S. 1G9 
 
 another of each of the balls^, so that velocity is communicated to the 
 one which was at rest, and the velocity of that which was in motion 
 is lessened ; and this action continues as long as the hinder ball 
 moves faster than the other. When the balls have acquired the 
 same velocity, the flattening of the two is at its greatest, and if the 
 balls had no tendency to recover their original forms the pressure 
 between them would cease, and the two would move on together 
 with the same velocity. Most substances however have a tendency 
 to recover their original forms, and in consequence of this the action 
 between the two continues till they cease to touch each other ; the 
 one which was originally at rest having the greater velocity of the 
 two. 
 
 Now all this that we have been describing takes place in a very 
 short time indeed : so short as to be considered instantaneous with- 
 out any sensible error. 
 
 If our knowledge of the structure of matter were perfect, and if 
 also our mathematical analysis were perfect, we should be able to 
 investigate, from the principles already laid down, the exact nature 
 and magnitude of the action which takes place between the two 
 bodies, and also the degree and manner in which a change of form 
 takes place. As it is, however, we are obliged to rest on experiment 
 for the facts which we have stated, and for the laws which we are 
 going to state. 
 
 Let /i be the time when the first contact takes place, /„ the time 
 when the two bodies are moving with the same velocity, and ^3 the 
 time when they cease to touch at all. Then the whole action which 
 takes place during compression, as it is termed, will be represented 
 
 by I Pelt and the whole action during restitution (that is, during 
 
 the recovery of the original form) by / Pdl. 
 
 The experimental law which forms the basis of our calculations 
 is that 
 
 rh (t-2 
 
 \ Pdl = e Pdl: 
 
 where e is a multiplier less than unity, which is constant for all 
 values of P, so long as the substances between which the impact 
 takes place remain unchanged. 
 
 The less or the greater the change of form that takes place for a 
 
 given value of I Pdt, the harder or softer the body is said to be. 
 
170 
 
 A TREATISE ON DYNAMICS. 
 
 [chap. 
 
 The greater or less e is, the greater or less is said to be the 
 " elasticity" of the bodies. 
 
 If e = 1, the elasticity is said to be perfect. 
 
 e is called the coefficient of elasticity, or sometimes the elasticity. 
 The definite integrals are generally written R and B', so that 
 i2'= eR. 
 
 R and jR' are called the "impulses" during compression and 
 restitution, and R + R', or {\+e)R is called the whole impulse. 
 
 The law has been enunciated and the action between the bodies 
 explained in a particular case only ; it is however applicable, with a 
 very slight extension, to all cases. 
 
 111. Since an impulsive force is only a force of great intensity, 
 D'Alembert's principle is applicable to it, as to all other forces. 
 
 If we take the case of one rigid body, that is, rigid in the modified 
 sense in which we have explained the term, the equations of motion 
 will be the same as before, and may, as in that case, be reduced to 
 
 M 
 
 dt' 
 
 2X, 
 
 And 2 
 
 M^=2F, 
 
 
 de ^^' 
 
 
 {,(.-.S)-.(r-4|)}=o.| 
 
 {.(x-.$)-.(.-.g)}.0. 
 
 {.(r-.g)-,(x-, 
 
 '5f)}-.| 
 
 (III) 
 
 (IV) 
 
 Now in this case, 2X, 2F and 2Z include all the forces which 
 act on the body, impulsive or otherwise ; and if we take the definite 
 integrals of the first three equations between the times /j and tz, the 
 beginning and end of impact, we have 
 
 m(m,-«o = 2/ xd/, 
 
 M(v,-v,)=l. j^Ydi, 
 
 M{w„-Wi)- 
 
 Zdt, 
 
YIII.] A TREATISE ON DYNAMICS. 171 
 
 or using A'', Y', Z' to denote the " Impulses," 
 
 M{y,-v,^ = ^Y'\ (VI) 
 
 The limits t^ and ^ must be taken so as to include the whole of 
 every impulse, and consequently may include a longer time than is 
 occupied by some of them. This however will produce no error; 
 for suppose one of the impulses as X' to commence at t( and end at 
 ^2' both of Avhich times are between t^ and t^. 
 
 Then since 
 
 {h ffi' r^i ['2 
 
 Xdt = Xdt + Xdt + Xdt, 
 •'/, hi J ti Jt.j 
 
 and since X is zero between /j and //, and also between // and to, 
 
 we 
 
 
 have Xdt= Xdt = X' 
 
 ,•(■> 
 
 Also since 1 Xdt has a sensible magnitude in consequence of X 
 
 being very large ; this integral will not have a sensible magnitude 
 for those forces which are not impulsive ; in other words, these forces 
 will not produce a sensible effect on the velocity during the short 
 time of impact, and therefore do not appear in equations (VI). 
 
 In the same way we may integrate equations (IV) between /, and 
 t^; and since the interval to — t^ is extremely short x, y, z, &c., may 
 be considered constant during that interval, so that we have 
 
 '^{y\_Z'-m{io'-wY\-z [F'- m (?;'- v)]} = 0, "j 
 l.{z\X' -in{u' -xi)-\- x{Z' -m{w' -w)-^ = Q, 1 . . . (VII) 
 2 {x \Y' - m iy'- vY\ ~y \_X' - m (?/ - «)]} = 0. i 
 
 In these equations x, y, z are referred to the center of gravity as 
 
 dx 
 origin, ii is the value of-j- before impact, and u' its value after 
 
 impact, and similarly for the other letters. 
 
 (VI) and (VII) give the state of motion of the body immediately 
 after impact, without any integration beyond that expressed by 2. 
 
 When the motion of every particle before and after impact is 
 parallel to one plane, equations (VII) are reduced to the one equation 
 
 l.m{x{v'-v)-y{u'-u)\ = ^{xY' -yX'), 
 
172 A TREATISE ON DYNAMICS. [cHAP. 
 
 Let 0), and w. be the angular velocities of the body before and 
 after impact, then 
 
 11 =- t/w^, u' = — y w.^, v — xm^^ v' = xw.2. 
 
 Let L' be the resultant moment of the impulses, and let r^=x°+i/^, 
 then this equation becomes 
 
 1.1117'- (uy^— w,) -L'. 
 
 And the three equations in this case are 
 
 M(v,-v,) ^1Y', [ (VIII) 
 
 112. If the system consists of more than one body, the equations 
 must be written down for each body separately, and the unknown 
 forces which enter the equations, must be determined by the relations 
 existing between the velocities of the points at which impact takes 
 place. These will be different according as the bodies are elastic or 
 inelastic, and as their surfaces are rough or smooth. 
 
 When the bodies are inelastic and smooth, the whole impulse will 
 be in the direction of the normal to the surface at the point of con- 
 tact, and must be determined from the condition that the resolved 
 parts in the direction of this normal of the velocities of the points in 
 contact must be equal. If the surfaces are rough, the whole velocities 
 of the two points will be equal and in the same direction. 
 
 When the bodies are elastic, and the coefficient of elasticity is 
 given, the normal impulse may be found from the consideration that 
 the normal velocities of the points in contact are the same at the end 
 of compression, and that the impulse during restitution is in a con- 
 stant ratio to the impulse during compression : when the surfaces 
 are rough, the velocities of the points in contact resolved along the 
 tangent plane Avill be equal at the conclusion of the impact, while 
 the resolved parts along the normal will be equal only at the end of 
 compression. 
 
 If the surfaces are partially rough, as is always the case in nature, 
 let /A be the coefficient of friction and R the normal portion of the 
 impulsive force ; then the tangential portion of the impulsive force 
 cannot exceed fxR, and therefore the whole tangential impulse cannot 
 
 exceed/ ixRdt. 
 
 Little is known experimentally of the value of ^x for forces so 
 great as to be impulsive ; so far as the experiments go, however, 
 
Viri.] A TREATISE ON DYNAMICS. 173 
 
 they indicate a diminution of m for large values of the normal pres- 
 sure. Considering /,t to be approximately constant, we have 
 
 rt-2 rh 
 
 Rdl = nR', 
 
 where R' is the normal impulse. This is the greatest amount of 
 tangential impulse that can take place for a given amount of normal 
 impulse ; all will not necessarily be exerted in any particular instance. 
 The preceding remarks will be better understood by a consideration 
 of the following examples. 
 
 113. Let a ball whose mass is m^ moving with a velocity t\ over- 
 take a ball Avhose mass is vk moving with a velocity v^, and let e be 
 the coefficient of elasticity. 
 
 Let R be the impulse during compression, u the common velocity 
 of the two balls after compression, ?/, and j/g their velocities after 
 impact : then from equations (VIII), 
 
 7W, {u -?;,)=— R, 
 
 vi^ (m - t'g) = R, 
 
 from which Ave have u = =-^ , 
 
 nil + W'a 
 
 Vli + 7»2 
 
 the whole impulse is (I + e) R, and the velocities after impact are 
 given by the equations 
 
 7«, (?/i -vi) = -(l + e) -^ '^ , 
 
 ^ ^ ^ ^ nii + mg ^ 
 
 W2 (^2 - v'2) = (l+e) -^-^^' ^-'- . 
 
 If the balls are equal and the elasticity perfect, these equations 
 become Uy-Vi, and xi2=Vx. 
 
 114. Again, let a sphere of radius a revolving with the angular 
 velocity w about a horizontal axis fall vertically on a horizontal 
 plane ; and let /a and e be the coefficients of friction and elasticity 
 between the sphere and the plane. 
 
 Suppose, to fix the ideas, that the axis of x is horizontal, and the 
 plane of xt/ perpendicular to the axis of rotation. 
 
 Let M be the mass of the sphere, V the velocity of its center of 
 gravity before impact ; v^. , x\ the resolved parts of the velocity, and 
 
174 A TREATISE ON DYNAMICS. [CHAP. 
 
 to' the angular velocity after compression: %i^, iiy and w the same 
 quantities when the impact is concluded ; B. and F the normal and 
 tangential impulses during compression ; then 
 
 Mv, = F (1) 
 
 M(vy+F) = R (2) 
 
 Mk^{co'-w) = Fa (3) 
 
 and the condition that the point of contact is at rest gives 
 
 v^ + a)'a = 0, Vy=.0 (4) 
 
 we also have the condition that F cannot exceed n R. 
 From equations (2) and (4), we have 
 R = MV, 
 also from (1), (3) and (4), we have 
 
 F Fa' ^ 
 
 Ma Ir a, 
 ~ a^ + k- ' 
 
 provided this is not greater than MF. Let this be the case, then if 
 F' is the tangential impulse during restitution 
 
 Mu^=F + F' (5) 
 
 M(Uy+V) = (l + e)R (6) 
 
 iWF(w-(o) = (F + F')a (7) 
 
 with the condition Uj. + -aa^O (8) 
 
 Equation (6) gives Uy = eV, 
 also from (5), (7), and (8) 
 
 and therefore F' = 0, and from (5) and (7) 
 
 and the initial motion after impact is completely determined. 
 
 We may remark here that the whole change of angular velocity 
 
 took place during compression ; if — — ^ had been greater than V 
 
 but less 'than {l+e)V, part of this change would have taken place 
 during restitution, and the final result would have been the same. 
 
VIII.] A TREATISE ON DYNAMICS. 175 
 
 Let J — p be greater than (l+e) F; in this case instead of the 
 equation u^ + wa = 0, we have 
 
 F+F' = -fx{l + e)MF; 
 
 .'. n^ = - fx(\ +c) V and w = w - -^ — r— , 
 
 and Uy = eV as before. 
 
 115. As a conchiding example we will take the system described 
 in Art. 106, and preserve the same notation. 
 
 Let the cylinder fall from rest so as to strike the plane along a 
 horizontal line. 
 
 Let F be the velocity of the cylinder before impact; v^, Vy the 
 resolved parts of the velocity of its center of gravity after compres- 
 sion, 0) its angular velocity, v the velocity of the plane at the same 
 time; it^, %iy, tn and u the same quantities after restitution. 
 Then we have 
 
 Mv^ = F cosa — R sin a, 
 M(Vy+ F) = Fsma + R cos a, 
 Mk''<o = Fa, 
 
 mv = Rsina-F cos a. 
 
 Since the velocities of the points of the two bodies in contact are the 
 same, their resolved parts in any two directions will be the same, 
 therefore 
 
 V — v^ + au} cos a, 
 
 = t'y + rt £0 sin a, 
 
 M+ 3m 
 
 from which R = MV cos a 
 
 M (l + 2sin'a) + 37w 
 After restitution the equations are 
 
 Mii^ = F' cosa-{l + e) R sin «, ^ 
 
 M {Uy + V)= F' sin a + {\ + e) R cos a, 
 Mk''s: = F'a, 
 
 mu = (1 + e) 7? sin a — F' cos a, 
 
 and the condition in this case is that the velocities along the plane 
 shall be the same, which gives the equation 
 
 (k, — «) cos a + Vy sin a + a ■KT = 0. 
 R is already known, and from these equations we can determine F' 
 and the other unknown quantities. 
 
176 A TREATISE ON DYNAMICS. [cHAP. 
 
 116, An examination of the proof of the Principles of the 
 Conservation of Areas and of the Motion of the center of gravity, 
 will shew that these principles are true when the forces are im- 
 pulsive, in the same cases that they are true when the forces are 
 finite. The Principle of the Conservation of vis viva on the con- 
 trary is not so. In fact the idea of an impulse implies a change in 
 the geometrical relations of the system. 
 
 These principles, however, are of little use in the solution of 
 problems where the forces are impulsive, since the equations of 
 motion are all linear, and require no integration. 
 
 
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