(b43i 
 
IC 28 19U 
 
 GEOMETRIC PROPERTIES COMPLETELY 
 CHARACTERIZING ALL THE CURVES 
 IN A PLANE ALONG WHICH THE CON- 
 STRAINED MOTION IS SUCH THAT THE 
 PRESSURE IS PROPORTIONAL TO THE 
 NORMAL COMPONENT OF THE ACTING 
 FORCE. 
 
 BY 
 
 SARAH ELIZABETH CRONIN 
 
 f o-ftu-b; 
 
 ' DNIVSRSXXy 
 
 Submitted in Partial Fulfilment of the Requirements for 
 
 THE Degree of Doctor of Philosophy, in the Faculty 
 
 OF Pure Science, Columbia University 
 
 PRESS OF 
 
 THE NEW ERA PRINTING COMPANY 
 
 LANCASTER, PA. 
 
 1917 
 
GEOMETRIC PROPERTIES COMPLETELY 
 CHARACTERIZING ALL THE CURVES 
 IN A PLANE ALONG WHICH THE CON- 
 STRAINED MOTION IS SUCH THAT THE 
 PRESSURE IS PROPORTIONAL TO THE 
 NORMAL COMPONENT OF THE ACTING 
 FORCE. 
 
 BY 
 
 SARAH ELIZABETH CRONIN 
 
 Submitted in Partial Fulfilment of the Requirements for 
 
 THE Degree of Doctor of Philosophy, in the Faculty 
 
 OF Pure Science, Columbia University 
 
 PRESS OF 
 
 THE NEW ERA PRINTING COMPANY 
 
 LANCASTER, PA. 
 
 1917 
 

CONTENTS. 
 
 Introduction. 
 
 Chapter I. The Differential Equation of the System 1 
 
 Chapter II. Geometric Properties of the System , 4 
 
 Section 1. Osculating Conies 4 
 
 2. Curvature of the Conic determined by Theorem 
 
 1 5 
 
 3. Second Center of Curvature of the Conic deter- 
 mined by Theorem 1 5 
 
 4. Tangents to the Parabola determined by The- 
 orem III 6 
 
 5. Center of the Conic determined by Theorem I . . 7 
 
 6. Hyperosculating Parabolas 8 
 
 7. Inverse Curve 10 
 
 8. Circles of Curvature Hyperosculating the Conies 
 determined by Theorem 1 10 
 
 9. Mid-point of the Chord of the Inverse Curve 
 cut from the Normal to the Lineal Element 11 
 
 10. Osculating Circles having Five-point Contact . . 12 
 
 Chapter III. Conversion of the Properties stated in The- 
 orems I-IX 14 
 
 Section 1. Conversion of Property 1 14 
 
 II 14 
 
 III 15 
 
 IV 16 
 
 V 17 
 
 VI 18 
 
 VII 20 
 
 VIII 21 
 
 IX 23 
 
 Chapter IV. Complete Characterization 25 
 
 Section 1. Relations existing among the Arbitrary Func- 
 
 iii 
 
 *\ i'^ y^ i\ (-x ■ - 
 
 2. 
 
 
 3. 
 
 
 4. 
 
 
 5. 
 
 
 6. 
 
 
 7. 
 
 
 8. 
 
 
 9. 
 
 
IV CONTENTS. 
 
 tions entering into the Differential Equation of 
 the System of Curves having Properties I-IX 
 if it is to be of the Special Form given in Chapter 
 
 1 25 
 
 2. Geometric Interpretations of the Relations of 
 Section 1 27 
 
INTRODUCTION. 
 
 In his " Differential-Geometric Aspects of Dynamics,"* 
 Kasner gives a set of five geometric properties which completely 
 characterize a system of curves in a plane field of force {(p, yp), 
 along which the constrained motion of a particle is such that 
 the pressure exerted by the particle on the curve is a given 
 multiple of the normal component of the acting force. The 
 defining equation of the system is P = kN, when P is the pres- 
 sure, N the normal component of the force, and k a given con- 
 stant. 
 
 Denoting the tangential component of the force by T, the 
 equations of motion are 
 
 where 
 
 -=T P^-'-N^kN 
 
 ^IT+Y" VrrP' y" ' 
 
 If at the initial time to the particle is at the point (ar©, yo) 
 moving in the direction yo' with the speed Vq, the path of the 
 particle is uniquely determined. By varying the initial direc- 
 tion 2/0' and the initial speed Vq, we obtain 00 2 curves of the 
 system through the given point (xo, yo). Since the path of the 
 particle is determined by taking any one of its 00 ^ points as the 
 initial point, the system contains in all 00 ^ curves. 
 
 The differential equation of the system in intrinsic form, 
 obtained by eliminating v between dv/dt = T and v^jr = (A + l)N, 
 is _ 
 
 Nr,= {n+l)T-rN, (1) 
 
 where 
 
 The equivalent equation in Cartesian coordinates is of the 
 third order and represents, for every value of k, a triply infinite 
 * Princeton Colloquium Lectures, page 91. 
 
VI INTRODUCTION. 
 
 system denoted by Sk- The triply infinite systems of trajectories, 
 brachistochrones, catenaries and velocity curves are but special 
 cases of this more general system, being obtained from it for 
 particular values of k as follows: 
 
 Sq, the system of trajectories. 
 Si, the system of brachistochrones, 
 Si, the system of catenaries, 
 (Soo, the system of velocity curves. 
 
 In a given field of force, there are oo^ of these triply infinite 
 systems corresponding to the oo^ values of k. The elimination 
 of k from the differential equation (1) gives the differential 
 equation of the quadruply infinite system obtained by com- 
 bining all the systems Sk in the given field. The intrinsic form 
 of this differential equation is 
 
 where 
 
 Nts + rN T 
 
 0, 
 
 
 It is the purpose of the present paper to obtain a complete 
 characterization of this oo^ system of curves. The differential 
 equation of the system in Cartesian form is obtained in Chapter I. 
 Geometric properties of the system are derived in Chapter II. 
 At any point (x, y) of the plane, there are oo ^ curves of the family 
 having a given direction y' and a given radius of curvature r. 
 If the osculating conic of each of these curves is constructed, the 
 locus of the centers of these conies is a conic passing through 
 the given point in the given direction. Applying this property 
 to the " four special cases of physical interest," Kasner restates 
 it as follows: " In any plane field of force select any fixed element 
 of curvature, corresponding to the initial values x, y, y', r so 
 given, construct the unique trajectory, unique brachistochrone, 
 unique catenary, the unique velocity curve, and the respective 
 centers of the osculating conies; the four centers so formed and 
 the given point {x, y) will lie on a conic passing through the 
 
INTRODUCTION. Vll 
 
 latter point in the given direction y' " The radius of curvature 
 of this conic is r/2. 
 
 The 00 2 curves of the family at the given point {x, y) in the 
 given direction y' have associated with them oo i of these conies. 
 The centers of these conies lie on a conic passing through the 
 given point, and their second centers of curvature lie on a parab- 
 ola passing through the given point and having its axis parallel 
 to the given direction. The angles (p, <pi and 6 which the conic, 
 the parabola and the direction of the acting force, respectively, 
 make with the given direction are related as follows: 
 
 tan <p = sin 20, 
 
 3 tan <pi = — sin 26. 
 
 One of the oo^ conies associated with the <»2 curves of the 
 family at the point {x, y) in the direction y' has four point contact 
 with its osculating circle at {x, y). The centers of the « ^ hyper- 
 osculating circles thus associated with all the curves of the family 
 through {x, y) lie on a cubic which has as tangents the minimal 
 lines at the given point. 
 
 Of the 00 1 curves of the family corresponding to a given curva- 
 ture element {x, y, y', r) there are two which are hyperosculated 
 by their osculating parabolas. The locus of the foci of these 
 hyperosculating parabolas as r varies in a bicircular quartic 
 with a node at the given point. One of the nodal tangents is 
 perpendicular to the direction of the acting force and the other 
 makes with this direction an angle which is bisected by the given 
 direction. 
 
 The inverse of this quartic is an hyperbola with asymptotes 
 parallel to the nodal tangents of the quartic. The locus of the 
 mid-point of the chord of this hyperbola cut from the normal to 
 the given direction at the given point is a circular cubic which 
 has a double point at the given point and its real asymptote 
 parallel to the direction of the acting force. 
 
 One of the oo^ curves of the family corresponding to a given 
 lineal element {x, y, y') has five-point contact with its osculating 
 fircle. The locus of the center of this five-point circle as y' 
 varies is a conic passing through the given point. Its tangent 
 at this point is perpendicular to the direction of the acting force. 
 
Vm INTRODUCTION. 
 
 If a quadruply infinite system of curves in a plane is given at 
 random, there exists in general no field of force in which the 
 pressure along the curves of this system is proportional to the 
 normal component of the force. The question of the suflficiency 
 of these properties to insure the existence of such a field of force 
 is next investigated, in Chapter III. 
 
 It is found that these properties belong to other quadruply 
 infinite systems of curves besides the system of curves along 
 which P = kN, and hence are not suJ0Bcient for a complete 
 characterization. 
 
 Additional properties are obtained in Chapter IV which 
 complete the characterization. 
 
 The entire set of sixteen properties obtained is shown to be 
 both necessary and sufficient for a complete characterization. 
 
 The writer is indebted to Professor Kasner for helpful sug- 
 gestions and criticisms. 
 
CHAPTER I. 
 
 DiFPEKENTIAL EQUATION OF THE SySTEM. 
 
 We consider the constrained motion of a particle in a plane 
 moving along a curve under the action of a positional force; that 
 is, a force whose rectangular components are functions only of 
 the coordinates of the point at which it acts, namely ip{x, y) 
 and xpixy y). Denoting by Sk the system of curves defined by 
 the equation P = kN for a given value of k, P being the pressure 
 and iV the normal component of the acting force, the problem is 
 to obtain geometric properties completely characterizing the 
 curves of all the systems Sk^ 
 
 The differential equation of the system Sk is 
 
 Nr,= (n-\-l)T-rN, (1) 
 
 where 
 
 ^~ k+1' ^^ ~ l + y" ^"^^ 
 
 and T is the tangential component of the acting force. Differ- 
 entiating equation (1) with respect to S, and eliminating n, we 
 obtain the differential equation, in an intrinsic form, of all the 
 systems Sk to be 
 
 where 
 
 Nts + rN T 
 
 ^ ~ l + y" 
 
 (3) 
 (4) 
 
 JTo obtain the equivalent of (3) in Cartesian coordinates, we 
 substitute for N and T the values given in (2) and (4), and for 
 N, T, r, Tg, Tas the values given by 
 
 1 
 
CURVES IN A PLANE. 
 
 ^ , (1 + y")y"' 
 
 2/' 
 
 _L,, .. [(1 + y")y'^ + 2y'y"y"'\ - 2(i + y")y"" \ 
 "r "^ y'" i 
 
 (5) 
 
 1 
 
 X 
 
 Making these substitutions in (3), we obtain 
 
 , r_3 3/(^^+^) 1 3 
 
 ■*" L 1 + 2/" (^ - 2/V)(^ + y'^)(l + 2/'') J ^ 
 
 L (^ + 2/V)(iA-2/V) J^ • 
 
 Introducing 
 
 Pi = ^x + (^» - <p^y' - <pvy''^y 
 P2= <Px+ {<Pv + ^r)y' + M\ 
 ^+^ 2y' 
 
 ^2-^ + y'^ ^-2/V' ^^ 
 
 „ 3 3y^(^^+^) 
 
 ^' ~ 1 + 2/'' (^ - y'<p){v> + 2/'^)(l + 2/'') ' 
 
 QP^y' ^P^y' + Pi 
 
 ^' " (^ - 2/V)(l + y") (^ + 2/'^)(l + 2/") ' 
 
 {<P + y'rP){rl^-y'<p) 
 
THE DIFFERENTIAL EQUATION OP THE SYSTEM. 3 
 
 (6) may be written 
 
 y^ = |-/ y"" + iQ^y" + Q-^)y"' + Q^y'" + Q^y"'' + Q^y"- («) 
 
 This is a differential equation of the fourth order and rep- 
 resents a quadruply infinite system of curves. 
 
CHAPTER II. 
 
 Geometeic Properties of the System. 
 
 Section 1. Osculating Conies. 
 
 Consider the curves of this system through a given point 
 (x, y) of the plane, in a given direction y', with a given curvature. 
 These form a system of oo^ curves, all of which have the same 
 first center of curvature, but each of which corresponds to a 
 different second center of curvature. Each of these curves has a 
 definite osculating conic at the given point; that is, a conic 
 having fourth order contact with the curve. The coordinates 
 of the center of the osculating conic, if the given point is taken 
 as the origin of coordinates, are 
 
 ^y"y"' , ^ ^y'y"y"' - ^y '" 
 
 5y"'^-dy"y^' 5y'"^ - Sy'Y 
 
 
 The locus of the centers of all the osculating conies correspond- 
 ing to the 00^ curves of the system is obtained by eliminating 
 y^^ and y'" between equations (8) and (9). 
 
 From (9) we have 
 
 y "y'h-k* y ~ y'h-k\_y'h-k h]' 
 Substituting these values in (8) and reducing, we obtain 
 
 [(3 + 3Qi y' + qzy")y"' + m^v' + Q^y")y"' + Q^y'YW 
 
 - [(3Qi + 2Q^y')y'" + (3^2 + 2Q,y')y"' + 2Q,yY]hk (10) 
 
 + [Qzy'" + Q^y'" + Q^y"W + ^yY'h - Sy'"k = o. 
 
 This is the equation of a conic passing through the given 
 point; the equation of its tangent at the origin is k — y'h = 0. 
 
 Theorem I. 7f, for each of the oo ^ curves of the system corre- 
 sponding to a given curvature element, we construct the osculating 
 conic, the locus of the centers of these conies is a conic passing through 
 the given point in the given direction. 
 
 4 
 
GEOMETEIC PEOPERTIES OP THE SYSTEM. 
 
 Section 2. Curvature of the Con,ic of Theorem L 
 
 Applying the formula 
 
 ^kfdh^ 
 K — 
 
 [1 + {dkldhff^ 
 
 to obtain the curvature at the given point of the conic (10), we 
 find 
 
 Theorem II. The curvature at the given point of the conic 
 corresponding, by theorem I, to a given curvature element is twice 
 the curvature of the element. 
 
 Section 3. Second Center of Curvature of the Conic Determined by 
 
 Theorem I, 
 For the conic (10), we find 
 
 The coordinates of the second center of curvature are ob- 
 tained by the formulas 
 
 - 4(1 + y")y' , {i + y'*)\ .„ 
 
 Applying these to the conic (10), we get 
 2(1 + y")y' 3(1+Y!)! 
 
 (1 + y'^){\ - Sy") 3 (1 + y")y'{q,y" + Q^) 
 2/2 - y„ 4 y//a 
 
 (11) 
 
 (11') 
 
 We now consider all curves of the system corresponding to a 
 given lineal element {x, y, y'). These form a system of oo^ 
 cm-ves. In accordance with theorem I, there are ooi conies 
 associated with this system of oo^ curves, each conic being as- 
 sociated, for different values of y", with the oo ^ curves corre- 
 sponding to a curvature element {x, y, y', y"). 
 
6 CURVES IN A PLANE. 
 
 The locus of the second centers of curvature of these conies, 
 with the given point taken as origin, is obtained by eliminating 
 y" between equations (11). 
 
 Multiplying the first of these equations by y' and then sub- 
 tracting from the second, we have 
 
 J_^ 2(y2 — y'xj) 
 y" (1 + 2/")' * 
 Substituting this in the first of the equations (11), we have, 
 after reduction, 
 
 6^2(2/2 - y'x^y + (1 + 2/")[3(l + y'^Qx + %y']yi 
 
 + (1 + y")[2 - Qy'' - 3Qi(l + y")y']x, = 0. ^^^^ 
 
 This is the equation of a parabola passing through the given 
 point; the axis of the parabola is parallel to the line 2/2 = y'x^. 
 
 Theorem III. The locus of the second centers of curvature of 
 the 00 1 conies associated, by theorem, I, with a given lineal element 
 (x, y, y') is a parabola passing through the given point; the axis of 
 the parabola is parallel to the given direction. 
 
 Section 4' The Equation of the Tangent to the Parabola. 
 The equation of the tangent to the parabola at the given point is 
 _ 2-62/-'-3Qi(l + y-V ^ .^„ 
 
 If we substitute for Qi its value given in (7) and take the x 
 axis in the direction y', we obtain 
 
 ± 
 
 slope of tangent = ~ o p • (14) 
 
 1 + 72 
 
 Calling the angle this tangent makes with the given direction 
 6\, and the angle the acting force makes with the given direction 
 di, (14) may be written 
 
 tan ^1 = — ^ sin 202- (15) 
 
 Theorem IV. At the given point, the tangent to the parabola 
 makes with the given direction an angle whose tangent is to the sine 
 of twice the angle the given direction makes with the acting force as 
 1 is to 3. 
 
GEOMETRIC PROPERTIES OF THE SYSTEM. 
 
 Section 6. Center of the Conic of Theorem I. 
 The coordinates of the center of the conic 
 
 ax^ + bxy -\- cy^ -{- dx -{- ey = 
 are given by the formulas 
 
 2cd —be „ 2ae — bd 
 
 a 
 
 /3 = iJ—JZT' (16) 
 
 6^ — 4ac ' b^ — 4ac * 
 
 Applying these formulas to conic (10), 
 
 3(to" + Q2) ,.-. 
 
 " - (3Qi2 - 4Qz)y'"+ {QQ1Q2 - 4.Q,)y"+(dQ2' - 4.Q,) ' ^''^ 
 
 P ~ (3Qi2 - 4^3)2/"' + {QQ1Q2 - ^Q4)y" + (3^2^ - 4Q6) * ^ ""^ 
 
 The locus of the centers of the <» ^ conies associated, by the- 
 orem I, with the 00^ curves corresponding to a given lineal 
 element is obtained by eliminating y" between equations (17) and 
 (18). To carry out this elimination, we take 
 
 _ i2-^Qiy')y"+Q2y' 
 
 a Qiy"-\-Q2 
 
 from which 
 
 „ _ Q2W - y'ot) 
 
 y 2a- Q,W - y'cc) ' 
 Substituting this value of y" in (17), we obtain 
 2[(Q2^Q3 - Q1Q2Q4 + Qm,)y" - 2(^2^4 - 2qmy' 
 
 - (3Q22 - 4Q6)]a2 _ 4[(Q2^Q3 - Q1Q2Q4 + Qi^q,)y' 
 
 - (Q2Q4 - 2QiQ5)]a^ + 2[Q2=^Q3 - Q1Q2Q4 + q^Q,,W 
 
 - 3[2Q2 + QiQ22/']a + 3Q1Q2/3 = 0. 
 
 This is a conic passing through the given point. The equa- 
 tion of the tangent at the given point is 
 
 , 2 + Qiy' 
 
 If we substitute for Qi its value from (7), and take the x axis 
 in the direction y' , 
 
O CUKVES IN A PLANE. 
 
 the slope of the tangent = jp . (20) 
 
 Callmg the angle this tangent makes with the given direction 
 Oi, and the angle the acting force makes with the given direction 
 62, (20) may be written, 
 
 tan di = sin 2^2- (21) 
 
 Theokem V. The locus of the centers of the <x>i conies asso- 
 ciated, by theorem I, with a given lineal element is a conic passing 
 through the given point. The tangent to this conic at the given point 
 makes with the given direction an angle whose tangent is equal 
 to the sine of twice the angle the acting force makes with the given 
 direction. 
 
 Section 6. Hyperosculating Parabolas. 
 
 We now determine all the curves of the system through the 
 point {x, y) which are hyperosculated by their osculating parab- 
 olas. The differential equation of all parabolas in the plane is 
 
 The hyperosculating parabola has contact of the fourth order 
 with its curve, hence its derivatives up to the fourth order at 
 the given point are the same as those of its curve. Substituting 
 the value of y^ from (22) in equation (8), we find 
 
 y""+ Sy"(Qiy" + ^2)2/'"+ Sy"iQ,y"'+ Q^'"+ Q,y") = 0. (23) 
 
 This is an equation of the second degree in y'". Hence two 
 curves of the system of 00 ^ curves corresponding to a given curv- 
 ature element are hyperosculated by their osculating parabolas. 
 
 The coordinates of the focus of the osculating parabola, 
 referred to the given point {x, y) as origin, are given by the 
 formulas 
 
 a = 
 
 ^=- 
 
 dyV W"(y" - 1) + 2y'{Sy" - y'y'")] 
 2 y""-\-(^y"'-y'y"r ' 
 
 ^y" [(3y " - y'y"')iy"- D - 2yy^1 
 
 ///2 _i_ (o,,n2 „,/„"'\2 
 
 y"" + W - y'y'") 
 
GEOMETRIC PROPERTIES OP THE SYSTEM. 
 
 (26) 
 
 From these we have 
 
 (ay' - )8)(1 + y'') 
 
 (25) 
 
 ,„ ^ _ 3(a2/^ - ^)(1 + y")[2^y' + a(l - y'^\ 
 y 4(a2 4- (82)2 
 
 To obtain the locus of the focus of the hyperosculating parabola 
 as the curvature of the element changes, its direction remaining 
 unchanged, we eliminate y" and y'" between (23) and (25). 
 The result of this elimination, after substituting the values of 
 Qu Qi, Qs, Qi, Qb, given in (7), and reducing, is 
 
 4PiP2(a2+/3T+{[12Pi(^+2/V)-2(3P2+Piy')(^-2/V)]« 
 
 - [(6P22/'- 2Pi) (,A- 2/V) - 12Pi2/'(^+2/V)]i8 } («'+^') 
 
 +m+y")[(<pW+2v>Y- <P^W- (^+tA')(l-2/'')«/3 
 
 -^(<p4^y''-2rPY-cpxpm = 0. 
 
 This is the equation of a bicircular quartic having a node at 
 the given point. The equations of the tangents at the origin are 
 
 /3[(1 -/')?'+ 2y VI + «[(1 - !/'V - 2!/Vl = 0. 
 
 Each of these tangents has second order contact with the 
 quartic at the given point, cutting it in three coincident points, 
 two on one branch and one on the other. 
 
 If we take the x axis in the direction y', the equations of the 
 tangents reduce to 
 
 ^xl^-\-a<p= 0, 
 
 0(p -\- a\l/ = 0. 
 
 Hence the first tangent is perpendicular to the direction of 
 acting force, and the second tangent makes with this direction 
 an angle which is bisected by the given direction. 
 
 Theorem VI. Corresponding to each curvature element, there 
 are two curves of the system that are hyperosculated by their osculating 
 parabolas. The hcus of the foci of these hyperosculating parabolas 
 as the curvature of the element varies, the direction of the element 
 remaining unchanged, is a bicircular quartic having a node at the 
 
10 CURVES IN A PLANE. 
 
 given point. One of the tangents at the given point is perpendicular 
 to the direction of the force acting at that point, and the other makes 
 with thai direction an angle which is bisected by the given direction. 
 
 Section 7. The Inverse Curve. 
 
 The inverse of this quartic with respect to the origin is ob- 
 tained by the transformation, 
 
 « = ^2 I ■ 2» /3 = 
 
 Substituting these in (26), we obtain the conic 
 3(1 + y"){My"+2<pY - ^rp]e - (^^H- ^)(1 - y")^v 
 
 + My" - 2^l^y' - <prl^W + [12Pi(v? + t/V) 
 
 - 2(3P2 + Pi2/')(^ - y'<pm - mP2y' - 2Pi)(^ - yV) ^^^^ 
 
 - 12P^y'i<p + 2/V)]7/ + 4P1P2 = 0. 
 The discriminant of (28) is 
 
 9(1 + yy[(<p' - rl^)a - y") + ^<p^y'f > 
 
 and the conic is an hyperbola. The asymptotes of this hyper- 
 bola are parallel to the lines 
 
 WrPy'' + 2<p'y' - <pyp]e - {<p' + ^2)(i _ y'')^^ 
 
 + [<prh" - 2Vy' - <pW = 0. 
 
 Hence the asymptotes of the hyperbola are parallel to the 
 tangents to the quartic at the origin. It follows that the axes 
 of the hyperbola make with the given direction angles of ± 45 
 degrees. 
 
 The inverse of the quartic of thereom VI is an hyperbola. The 
 asymptotes of the hyperbola are parallel to the tangents to the quartic 
 ai the origin. 
 
 Section 8. Determination of the Conies, Obtained in Accordance 
 
 vrith Theorem I, which are Hyperosculated by Their Circles of 
 
 Curvature at the Origin. 
 
 The differential equation of all the circles in a plane is 
 
 y'" = r^7- (29) 
 
GEOMETRIC PROPERTIES OF THE SYSTEM. 11 
 
 If the conic is hyperosculated by its circle of curvature at the 
 origin, the first three derivatives are the same for both curves 
 at that point. 
 
 For the conic (10), we find 
 
 fh=y'- i=2,". g=6(to"+w. (30) 
 
 Substituting these values in (29), we obtain 
 
 -[Qiy"+Q2](l-hy") = 2yy'. (31) 
 
 This is linear in y". Hence in the system of oo^ conies cor- 
 responding to a lineal element, by theorem I, there is one which 
 is hyperosculated by its circle of curvature at the origin. 
 
 The coordinates of the center of this hyperosculating circle 
 are 
 
 The locus of the center of this hyperosculating circle as y' 
 varies, obtained by eliminating y" and y' between (30) and (31), 
 is 
 {xf^y<p - 2<pyyP)X^ + {<py<p + 2<p^^P - 4^^<p - rP,rP)X^Y 
 
 - {<pyyp - 2xl^y<p - xl^^rP + <Px<p)XY' + {<p,yp - 2^x^)P (33) 
 
 This is a cubic having a conjugate point at the given point: 
 the tangents at the given point are the two minimal lines. 
 
 Theorem VII. Of the oo ^ conies eorresponding, in aceordance 
 with theorem I, to a given lineal element, there is one which is hyper- 
 osculated by its osculating circle at the given point. The locus of 
 the center of this hyperosculating circle, as y' varies, is a cubic with 
 a conjugate point at the given point. The tangents at this point 
 are the minimal lines. 
 
 Section 9. Coordinates of the Mid-point of the Chord of the 
 Hyperbola {28) Cut from the Normal to the Corresponding 
 Lineal Element. 
 The equation of the normal is 
 
 ^=-^^ (34) 
 
12 CURVES IN A PLANE. 
 
 Regarding (28) and (34) as simultaneous equations, we obtain 
 
 3(1 + yy{<p + 2/V) (^ - y'<p)e 
 
 The discriminant of this quadratic, 
 
 4(1 + y'W\^ - 2/V)Pi[Pi(^ - 2/V) + 12P2(^ + yV)], 
 is a polynomial of even degree in y', with the real linear factor 
 ^ ~ y'<P' Hence corresponding to each point of the plane 
 there is a range of values of y' for which the discriminant is 
 > 0. Throughout this range of values of y', (34) intersects its 
 corresponding hyperbola (28) in two real and distinct points. 
 From (35) and (34) we find the coordinates of the mid-point 
 of the chord to be 
 
 _ 2Pyy' ^ 2Px 
 
 3(^ + t/V)(i + y'')' ^{<P^y'^){i + y")' ^ ^ 
 
 With each lineal element through a given point, we may as- 
 sociate the mid-point of the chord of the hyperbola corresponding 
 to the element cut from the normal to the element. The locus 
 of this mid-point, as the lineal element revolves about the given 
 point, obtained by eliminating y' between equations (36), is 
 3(<p7-^X)(Z2+ p)_2[^,y2 _ (^^ _ ^,)XY- VyX^] = 0. (37) 
 
 This is a circular cubic with a double point at the given point. 
 The real asymptote to this cubic is parallel to the direction of 
 the force acting at the given point. 
 
 Theorem VIII. The inverse of the quartic of theorem VII is 
 an hyperbola. The locus of the mid-point of the chord of this 
 hyperbola cut from the normal to the lineal element, as the direction 
 of the element varies, is a circular cvhic with a double point at the 
 given point. The real asymptote of the cubic is parallel to the 
 direction of the force acting at the given point. 
 
 Section 10. Curves of the System which Have Five-Point Contact 
 with Their Osculating Circles. 
 
 The differential equation of all circles in the plane is 
 
 !'"' = f$7- (38) 
 
GEOMETRIC PROPERTIES OP THE SYSTEM. 13 
 
 DiJBFerentiating this, we have 
 
 y '- (1+7^2+ r+p. (38) 
 
 If a curve has five-point contact with its osculating circle, 
 the first four derivatives at the point of contact are the same for 
 both curves. Substituting the values of y'" and y^ from (38) 
 and (380 in the differential equation of the system (8), we have 
 
 [r|^2+^4]2/"+Q5=0. (39) 
 
 Hence corresponding to each lineal element there is one curve 
 of the system which has five-point contact with its circle of 
 curvature. If we eliminate y' and y" between 
 
 X^-^r^, Y^'-±^ (39') 
 
 y y 
 
 and (39), we get the locus of the centers of these five-point circles, 
 as the direction of the element varies, to be 
 
 ^xP - {<Py + ^.)XY + 4'yX' +m+ <pX) = 0. (40) 
 
 This is a conic passing through the given point. Its tangent 
 at this point is perpendicular to the direction of the force acting 
 at the point. 
 
 Theorem IX. Of the oo^ curves of the system corresponding to 
 each lineal element, there is one which has five-point contact with 
 its osculating circle at the given point. The locu^ of the centers of 
 these circles, as the direction of the element varies, is a conic passing 
 through the given point. Its tangent at this point is perpendicular 
 to the direction of the force acting at the point. 
 
CHAPTER III. 
 
 Conversion of the Properties Stated in Theorems I to IX. 
 
 The quadruply infinite system of curves defined by (8) pos- 
 sesses the properties stated in the theorems I to IX. We now 
 consider the converse question, if a quadruply infinite system of 
 curves possesses these properties, does there exist a field of force 
 such that the pressure on any curve of the family is some constant 
 multiple of the normal component of the acting force? 
 
 Section 1. Conversion of Property I. 
 
 The differential equation of any oo* family of curves in the 
 plane is y^ = G{x, y, y', y", y'"), when G is an arbitrary function 
 of its arguments. 
 
 If this family possesses property I, the centers of the osculating 
 conies of the oo ^ curves of the family defined by any curvature 
 element {x, y, y', y") lie upon a conic through the point {x, y) 
 in the direction y'. 
 
 The most general equation of such a conic, referred to the 
 point {x, y) as origin, is 
 
 Ayo? + A^a^ + Az^ + {ay' - ^) = 0, (41) 
 
 where A\, A2, Az are arbitrary functions of x, y, y', y". 
 The coordinates of the center of the osculating conic are 
 
 ^y"y"' o ^y'y"y"' - %'" 
 
 ^ K'l.f'f^ Q-..".iiIV ' P 
 
 by'"^ - Sy'Y"^' '^ ~ 5y"'^ - Sy"y^ ' 
 
 Substituting these in (41), we have after reduction 
 
 y"^ = B^y"" -\- B^y'" + Bz, (42) 
 
 where the B's are arbitrary functions of x, y, y', y" . Hence if a 
 system of oo^ curves of the plane has property I, its defining 
 equation must be of type (42). 
 
 Section 2. Conversion of Property II. 
 We now find those systems of type (42) which have property 
 
 II. 
 
 14 
 
CONVERSION OF PROPERTIES. 15 
 
 The locus of the centers of the o?^ osculating conies of the 
 system (42) corresponding to a curvature element {x, y, y', y") 
 is obtained by substituting 
 
 Making this substitution, we obtain 
 
 [Iby'" - ^B,y"' - 3B2y'y - B^y^W 
 
 (43) 
 + m^y" + 2Bzy')hk - Bzk^ - Sy'yh + dy"k = 0. 
 
 The curvature K of this conic is 
 
 2[3B^y'' - 5]y" 
 
 If the system (42) has property II, then 
 2[SBiy" - 5]y" 2y" 
 
 from which, Bi = 2ly". 
 
 The differential equation of all quadruply infinite systems 
 having properties I and II is then 
 
 y"^ = ^rV'" ■\- B^y" + Bz, (44) 
 
 when Bz and ^3 are arbitrary functions of x, y, y', y". 
 
 Section 3. Conversion of Property III. 
 
 The conic corresponding, in accordance with property I, to a 
 curvature element of the system (44), may be obtained from (43) 
 by replacing Bi by 2jy". This gives 
 
 W + 3B,y'y + Bzy")h? - {ZB^y"' + 2Bzy')}ik 
 
 + Bzk + Zy'yh - Zy"'k = 0. 
 For this conic, we have 
 
 d^k ^„ „ d^k „ „ dh 
 
 ^z=-^B,y, ^,= 2y, ^=y. 
 
 Substituting these in the formulas (11) for the second center 
 of curvature, 
 
16 CURVES IN A PLANE. 
 
 (45) 
 
 4(1 + y'')/ 6(1 + yyB2 
 
 ^ (1 + y'^jl - Sy") 6(1 + y")y'B2 
 2/2 2y" 8y"^ 
 
 If system (44) has property III, the coordinates of the second 
 center of curvature obtained in (45) must satisfy the equation 
 of a parabola passing through the given point with its axis 
 parallel to the given direction. 
 
 The most general equation of such a parabola is 
 
 (2/2 - y'x^y + Ciy2 4- C2X2 = 0, (46) 
 
 when X2, yz are the coordinates of any point on the parabola 
 referred to the given point (x, y) as origin, and C\, C2 are arbi- 
 trary functions of x, y, and y'. 
 Substituting the values from (45) in (46), we obtain 
 
 Solving this for B2, making a slight change in notation, we 
 obtain 
 
 B2 = Hiy"-{-H2, 
 
 where Hi and H2 are arbitrary functions of x, y, 3^. 
 
 All the quadruply infinite systems having properties I, II, 
 III are then defined by the differential equation 
 
 2/"^ = ^ y'"^ + ili^y" + H2)y'" + Bz, (47) 
 
 where Hi and H2 are arbitrary functions of x, y, y' and B% is an 
 arbitrary function of x, y, y' , y" . 
 
 Section 4- Conversion of Property IV. 
 In order to convert Theorem IV, we state it in a form which 
 does not assume the existence of a force, as follows: At each point 
 {x, y) of the plane, there exists a certain direction of slope co(x, y) 
 svxih that the sine of twice the angle this direction makes with the 
 given element is equal to three times the tangent of the angle the given 
 element makes with the parabola corresponding to it by theorem III. 
 
CONVERSION OF PROPERTIES. 17 
 
 The parabola corresponding, in accordance with property III, 
 to the 00 2 curves of system (47) passing through a given point 
 {x, y) in a given direction y', is found by eliminating y" between 
 
 4(l + y^V 6(1 + y-^)'^ 
 ^2 = 2y^' '^^ — ^^'^y + ^2;» 
 
 (1 + y") ,, . „, 6(i + y-W(giy" + g2) 
 
 2/2 = 22/" ^^ ~ ^^ ^ W" * 
 
 Carrying out this elimination, we obtain 
 
 6^2(2/2 - yW) + (1 + 2/'=')[3(l + y")Hr + 82/']z/2 
 
 + (1 + 2/")[2 - W' - 3Fi(l + y")y']x2 = 0. 
 
 The slope of the tangent to this parabola at the given point is 
 
 _ 2-Qy"-SHra-^y")y' 
 3(1 + y")Hi + 8y' ' 
 
 If the system (47) has property IV, we have 
 
 2(0, - y') 
 
 of 'J 2 - 6y^^ - 3gi(l + y- y i 
 
 ' ^L^-^ S{l-\-y")Hi-\-Sy' J _ 
 
 [2 - 6y-' - Bffid + y")y']y' f co-y- T' 
 
 ^ 3(1 + 2/'=^)^!+ 8/ ■^Ll + coy'J 
 
 Solving this for iTi, we find 
 
 1 + ic"^ 2y' 
 
 Hi 
 
 (CO - 2/')(l + W) 1 + 2/"' 
 where w is an arbitrary function of x and 2/- 
 The differential equation 
 
 defines all the quadruply infinite systems having properties I, 
 II, III, IV. 
 
 Section 5. Conversion of Property V. 
 
 Property V may be stated in a form that does not require the 
 existence of a field of force by replacing the direction of the 
 acting force by the function o){x, y) defined in Section 4. 
 
 The most general conic fulfilling the conditions of theorem V is 
 
 Gia^ + GiaP + Gs8'' + fi - ma = 0, (49) 
 
18 CURVES IN A PLANE. 
 
 where the G's are arbitrary functions of x, y, and y', and m is 
 determined from the relation 
 
 
 m 
 
 m 
 
 ^Ll + co/J 
 
 (1 + co2)(l + y")y' + 2(co - y'){\ + cot/') 
 
 to be 
 
 (1 + y")0. + d") - 2(co - y'){l + coy')2/'* 
 
 The center of the conic corresponding, according to property 
 I, to the system (48) is 
 
 Z{H,y"+my" 
 a = — 
 
 where 
 
 S{Hiy" + H,)Y^ - 
 
 453' 
 
 3(22/" + H^y'y + H,y')y" 
 
 SiH^y" + ^2)Y' 
 
 -4^3 
 
 1 + 0)2 
 
 22/' 
 
 (co-2/')(l + <^y') 1 + 2/''* 
 By property V, these satisfy (49). Substituting, we have 
 Liy'" + L2y"' + L,y" 
 
 + 2F2(co - 2/0(1 + co2/')[(3Fiy" + H^Yy" - 4^3] = 0, 
 
 when the L's are functions of Gu G2, G3, H2, x, y, and y' and there- 
 fore arbitrary functions of x, y, and y'. 
 Solving this for Bz, 
 
 Bz= Miy'"-\-M,y'"+Mzy", 
 
 when the M's are arbitrary functions of x, y, and y'. 
 
 Hence all systems possessing properties I, II, III, IV and V 
 have the form 
 
 2^ -y"^' +iL(l + co2/0(co-2/') l+2/'^J^+^^P (50) 
 
 + Miy"'+M2y"'+Mzy". 
 
 Section 6. Conversion of Property VI. 
 We state theorem VI without assuming the existence of a 
 force by replacing the direction of the force acting at the given 
 point by the function (a{x, y) defined in Section 4. 
 
CONVERSION OF PROPERTIES. 19 
 
 We determine the slopes mi and mi of the tangents to the 
 quartic of theorem VI from the conditions 
 
 1 (a— y' y' — tni 
 
 TOl = — 
 
 CO 
 
 1 + C02/' 1 + 2/'wi2 * 
 
 (51) 
 
 (52) 
 
 Solving the second of these equations for m2, we find 
 
 2y^+coy^'-co 
 
 We now find the locus of the foci of the hyperosculating 
 parabolas of the curves of (50) which correspond to a given lineal 
 element (ar, y, y'). It is obtained by substituting the values of 
 y", y"', y" from (22) and (25) in (50). The result is 
 
 m^{c? + ^f + {2[M2(1 + 2/") + 6ilf ii/']/3 
 
 + 2[3F2(1 - y'^) - Miy\\ + y'^)\a\ {o? + ^) 
 
 + [121/'=' + m^y'iX + y") + M i(l + y'^X^ (53) 
 
 + [12t/'(l-2/'^)-2Mi2/'(l+2/'^)2+3Fi(l+2/'=')(l-3y"')]a/3 
 
 + [3(1 - y'^) + iWi2/''(l + y'''? - ^H^y'a - y")W = 0, 
 
 where 
 
 l + co^^ 2y[_ 
 
 ^' (CO - 2/0(1 -I- coi/O l + 2/'='* 
 
 This is a bicircular quartic. Hence if an qo* system has 
 properties I to V, it also has the property that the foci of the 
 hyperosculating parabolas of the curves corresponding to a 
 lineal element lie upon a bicircular quartic. 
 
 In accordance with theorem VI, the slopes of the tangents to 
 (53) at the given point must equal mi and m2 of (51) and (52). 
 
 Forming the product of these slopes, we have 
 
 3(1 - y") + M^y'W + y^ - SH^y'd - y") 
 
 12y" + QHiy'a + y'') + Mi(l + y'Y 
 
 _ _ 2y' + <^y'^ 1 - CO 
 co(l + 2co2/'-i/'^)- 
 This solved for Mi gives 
 
 M,= ^ 32/'(l + co^) 
 
 (54) 
 
 1 + 2/'' (co-2/')(l + co2/0(l + 2/'')- 
 The differential equation of all the systems having properties 
 
HI 
 
 (55) 
 
 20 CURVES IN A PLANE. 
 
 I, II, III, IV, V, VI is of the form 
 
 when Hi, If 2, Mi are arbitrary functions of x, y, and y', and w 
 is an arbitrary function of x and y. 
 
 Section 7. Conversion of Property VII. 
 
 The most general cubic having the properties required by 
 theorem VII is 
 
 TiX^ + TiX^Y + TzXY' + T,r+X^+Y^ = 0, (56) 
 
 when the 7"s are arbitrary functions of x and y. 
 
 The conies of theorem I corresponding to system (55) may 
 be obtained from (10) by replacing Qi, Q2, Q3, Qi, Qh by Hi, H2, 
 Ml, Mi, Mz respectively. Hence dkjdh, (Phjdh^, d^kjdh? of the 
 conic may be obtained from (30) by replacing Qi and Q2 by Hi 
 and Hi respectively. We find 
 
 dh , d?k ^ ,, d?k ^,tx » ■ ttv .. 
 
 Substituting these in the differential equation of all the circles, 
 
 y 1 + 2,'*' 
 
 we have, after substituting for ^1 its value in (53), 
 
 r l + co^ ^y' 1 „ , „ _ 2yy^ 
 
 lio>-y'){\ + <.y')-l + y''\y + ^^ " " 1 + y'- ^^7) 
 
 In accordance with property VII, if we eliminate y' and y" 
 between (57) and equations (32), we get a cubic of the form 
 (56). 
 
 Substituting in (57) the values y'= - (Z/F), 2/" = (Z'+ P)/l^, 
 and denoting by Hi the function of X and Y which Hi becomes 
 on replacing y' by — (X/Y), we obtain 
 
 g,'[ ^^"^|j^>J-"^ J + X^+P=0. (58) 
 
CONVEESION OP PROPEKTIES. 21 
 
 In order that (58) may have the form (56), we must have 
 ^2' r Y(^y+^)(Y-o>X) -\ ^ y^^3_^ T2X'Y+ TzXY'+ T,Y\ 
 
 _ iTiX^+ T2X^Y+ TzXY'+ rP)(l + oy") 
 >^^ " F(a)y4-X)(F-coZ) 
 
 (a,+ f)(l-cof) 
 
 ^2' = 
 Hence, 
 
 Tj _ K,y"+K,Y"+KzY' + K, .^^. 
 
 ^' - (0,-2/0(1 + 0,/) ' ^^^^ 
 
 when the K's are arbitrary functions of x and y. 
 
 The differential equation defining all 00 ^ systems having the 
 first seven properties is 
 
 2/^ = 4 y"" + [Hiy" + my'" + M^y"' + M,y"' + ilf 32/", (60) 
 
 where 
 
 _ 1 + 0,2 22/' 
 
 ^' ~ (0, - 2/0(1 + 0,2/') ~ fTF' 
 
 __ K,y"-^K,y''+K^y' + K, .^^^ 
 
 H2 - («_ 2,0(1 +0,2/0 ' ^^^^ 
 
 ^ 3 32/'(l + o,2) 
 
 1 + 2/" (o,-2/)(l + 0,2/0(1 + 2/'*)' 
 
 Xi, X2, K3, Ki are arbitrary functions of x and 2/ and M2, Mz 
 are arbitrary functions of x, y, and 2/', 
 
 Section 8. Conversion of Property VIII . 
 
 We find the quartic corresponding, in accordance with 
 theorem VI, to (60) by substituting in (53) the particular values 
 of Hi, H2, and Mi given in (61). The inverse of this quartic is 
 the hyperbola 
 
22 CURVES IN A PLANE. 
 
 [3(1 - y") + Miy'W + y^ - 3H^y\l - y'*)]^ 
 + [Wil - y") - 2Miy'(l + yy 
 
 + SH,{1 + y'Yl - Sy")]^V 
 
 + [W + 6H^y'(l + y") + Mi(l + y'')]^^ (62) 
 
 + 2[M2il + y") + m,y']r} 
 
 + 2[3Zr2(l - y") - M,y'{l + 2/'^]^ + ^M, = 0, 
 
 where Hi, H2, and il/i have the values given in (61). 
 
 We find the coordinates of the mid-point of the chord of this 
 hyperbola cut from the line v = — (1/2/0^ to be 
 
 _ 2M,y' 2H,y" 
 ^~ 3 '^l + y''' 
 
 (63) 
 2M2 2H2y' 
 
 Y= - 
 
 1 + y'" 
 
 In accordance with theorem VIII (which we restate by re- 
 placing the direction of the force acting at the given point by 
 CO (a:, y)) these coordinates must satisfy a cubic of the form 
 
 (Z2 + Y^)io}X - Y) + AX^+ BXY + CP = 0. (64) 
 
 Substituting the values of X and Y from (63) in (64), we obtain 
 
 [^ + ff^] (1 + /')(1 + «/) + ^^" - By'+ C = 0. 
 
 Solving this for if 2 and introducing Ni = — ^A, N^ = }5, 
 Nz= — f C, we obtain 
 
 ^ ^Niy^+N^y'+Nz SH^y' 
 
 (1 + 2/'=')(l + coy') a + y")' 
 
 where « and the N*s are arbitrary functions of x and y, and Hi 
 has the value given in (61). 
 
 The differential equation of all 00 * systems possessing the first 
 eight properties is 
 
f'-Y'^"" 
 
 CONVERSION OF PROPERTIES. 23 
 
 "^lL("-2/')(H-coy') l-\-y"V' 
 
 ^ (CO -2/0(1+ cot/') \y 
 
 + 
 
 r 
 
 L (1 + 2/'')(l + CO2/0 
 
 (co- 2/0(1 + W2/0 J 
 
 when the iiC's, the N's, and co are arbitrary functions of x and y, 
 and ilf 3 is an arbitrary function of x, y, and 2/'. 
 
 Section 9. Conversion of Property IX. 
 We obtain the curve of system (65), corresponding to a 
 given lineal element, which has five point contact with its os- 
 culating circle, from (39) by replacing Q2, Q4, and Q5 by 
 
 Kxy" + K<,y" ^ K^y' + K, 
 
 H2 = 
 if2 = 
 
 (<0 - 2/0(1 + C02/0 
 
 (l + 2/'')(l + co2/0 1 + y" 
 and ikfa respectively. The result is 
 
 (1 + 2,")(1 + .,/) ^ +il/3-0. 
 Hence 
 
 _ il/3(l + y'^W + 1) .„, 
 
 y - N,y"+N,y' + N, ' ^^' 
 
 The center of the corresponding osculating circle, obtained 
 by substituting this value of y" in (390, is 
 
 y_ y'[Niy"+N2y' + Nz] 
 
 Mzil + C02/O 
 
 (67) 
 
 _N^y;^_±N2y^±Nz 
 
 Mzil + a;2/0 • 
 
24 CUKVES IN A PLANE. 
 
 In accordance with property IX (restated without assuming 
 the existence of a force), these coordinates satisfy a conic of 
 the form 
 
 EiZ2 - IkXY + Rzr + (X + wF) = 0, (68) 
 
 when Ri, Rz, R3 and w are arbitrary functions of x and y. 
 Substituting, we obtain 
 
 [Ni Y" + N^y' + N,][R^y" + R,y' + Rz] 
 
 + iy' -«)(! + o}y')M, = 0. 
 Solving for Mz, 
 
 ^ _ [Njy'' 4- Njy' + NzWR^y" + Riy' + Rz] 
 (CO -2/0(1 + "2/') 
 when the iJ's are arbitrary functions of x and y. 
 Hence the systems of type 
 
 IV _ A n,7A__l±jl 2y^l u 
 
 y y"y "^L(«- 2/0(1 +"2/0 i + y"r 
 
 T Kiy"^-K,y"■\-Kzy' + K, ■^ ,„ 
 ■^L (CO - /)(1 + C02,') J 2^ 
 
 4. r_J 3y-(l + co^) 1 
 
 ^ L 1 + 2/'' (1 + 2/'0(co - 2/0(1 + C02/O J ^ 
 
 
 
 ■^L(l + 2/")(l + co2/0 
 
 (69) 
 
 3(ii:i y^* + ^22/^' + Ji^ay^' + T^^v' 1 , 
 + 2/'0(«- 2/0(1 + C02/O J^' 
 
 + 
 
 (1 
 l^^y'^ + i\^22/' + iV^3][/?i2/'' + ^^22/' + M 
 
 \y". 
 
 (CO- 2/0(1 + C02/O 
 
 where co, iVi, iVz, ^3, ^1, -K^2, -K^s, -K^4, i^i, jR2, and Rz are arbitrary 
 functions of x and 2/, are completely characterized by properties 
 I, II, III, IV, V, VI, VII, VIII, IX. 
 
CHAPTER IV. 
 
 Complete Chaeacterization. 
 
 Types (69) and (6) involve the derivatives y', y", y'", y^ 
 in exactly the same way; but (69) is more general than (6) with 
 respect to the arbitrary functions of x and y appearing in the 
 coefficients. 
 Section 1. Relations Existing among the Arbitrary Functions 
 
 Entering into the Differential Equation of the System of Curves 
 
 Having Properties I-IX if it is to be of the Special Form given 
 
 in Chapter I. 
 
 We now determine the relations that must exist among these 
 arbitrary functions in order that (69) may be of the special 
 type (6). 
 
 By direct comparison of (69) and (6), we have 
 
 <a 
 
 Y 
 
 (70) 
 
 Ni 
 
 _<Py ^^^<P'-^v ^ >Px 
 <P <P <P 
 
 (71) 
 
 Ri 
 
 ^i T, ^X-h (Pv Jf <PX 
 
 <P <P <P 
 
 (72) 
 
 
 2(Py\l/ — \l/y<P ^^ (py(p " xf/ x<P " ^y^ + '^'(pX^ 
 
 
 ipyip — 2\py<p + (Pj,(P — yffgxf/ ^^ (p^xp — 2\l/x(p 
 
 ^2 > ^^4- ^2 
 
 (73) 
 
 itroc 
 
 lucing (f> = log <f) and substituting xp — aj0, we have 
 
 
 Ni 
 
 = <t)y, Ni = <f>x — W0y — Uy, Nz = — 03x — Oi4>x, 
 
 (74) 
 
 Ri- 
 
 = Ul^y + COj,, JB2 = 01/ + (^4>X + i>ix, RZ = <f>X, 
 
 (75) 
 
 Ki = W0I, — COy, iL2 = (1 — W )0J/ + W0a; — COs — C0CO«, 
 
 - - - (76) 
 
 Kz= {\ — (»)^)<f>x — oi(t>v ~ 2a)y — cowx, i^4= —2(ax—oi(f>x' 
 
 From the first and third equations of (74), we have 
 
 25 
 
26 CUEVES IN A PLANE. 
 
 <i>y=Nr, <!>:,= --^-5. (77) 
 
 CO 
 
 Substituting these values in the second equation of (74), it 
 becomes 
 
 wWi + U)N2 + Nz+0}^+ UUy = 0. (78) 
 
 From (77) we have 
 
 (78) and (79) are necessary conditions. To show that they are 
 also suflBcient: if (79) holds, we can find a function (f> which 
 satisfies both of the equations (77). Then on account of (78), 
 equations (74) hold. Finally (70) and <f> = log <f> determine a 
 pair of functions <f> and ^ in terms of which we can express Ni, 
 Nz, Nz and u in the forms given in (70) and (71). 
 
 From (75) and (77), we have 
 
 Ri = oiNi + oiy, R2=Ni-N3, Rs= - ^^+^" , (gQ) 
 
 CO 
 
 and from (76) and (77), 
 
 Kl = CoiVi — C0„, ^2 = (1 — CO^)Ni — N3— 2cOx — COCOy, 
 __ (1 — CO^) .^ ... 0)x „ rr HT ^^^^ 
 
 K3= - -Nz - coiVi 2uy, Ki= Nz- cox. 
 
 CO CO 
 
 If relations (80) and (81) hold, we can express Ri, R2, Rz, 
 Kl, K2, Kz, and K^ in terms of (p and \J/ in the forms given in 
 (72) and (73). 
 
 We now derive relations equivalent to (80) and (81) which admit 
 of geometric interpretations. 
 
 From (75) we have 0x = Rz, <f)y = {Ri — cS)yfo). 
 
 Substituting these in the second equation of (75), it becomes 
 
 ui^Rz — <aR2 -{- Ri — o}y-{- coco* = 0. (83) 
 
 From (80), 
 
 Ri = coiVTi + CO,, Rz= - ^^^^^t-^. (83') 
 
 CO 
 
 The equations (83) and (83') are equivalent to the equations (80). 
 From (76) we have 
 
 _ K i + o}y - Ki + 2co» 
 
COMPLETE CHABACTERIZATION. 27 
 
 Substituting these values in the second and third equations 
 of the set (81), we obtain 
 
 (1 - o)^)Ki - o)Ki - UK4 + uy- 2co2aj„ - Scoco^ = 0, (84) 
 uKi + ojKs + (1 - o}^)K4, + 2co, - oi'u}^ + 3ajco„ = 0. (85) 
 
 Multiplying (85) by w and adding to (84), we obtain 
 Ki - coiiTz + oi^Kz - o)'K, + (coj, - (acc^Kl + w2) = 0. (86) 
 
 Multiplying (84) by co and subtracting from (85), we obtain 
 
 u^Ki + 03^K2 + uKz + Ki + 2{o3^ + «a)„)(l + <a^) = 0. (87) 
 
 From (82) we have 
 
 Ki = uNi - o3y, Ki= N3- w,. (88) 
 
 Relations (86), (87), and (88) are equivalent to relations (82). 
 
 Section 2. Geometric Interpretations of the Relations of Section 1. 
 
 We now obtain geometric interpretation of relations (78), 
 (79), (83), (86), (87), (88). 
 
 Interpretation of {78). — The radius of curvature of the bi- 
 circular quartic 
 
 (^2 + ^2)2 _^ ^a<x + 6/3) (q:2 + ^2) + ca2 + ^^^ + e/32 = 
 
 at the origin is 
 
 {l-\-^"yi\d+2e^') 
 
 ^= W+W) • ^^^^ 
 
 If in the bicircular quartic (26) we take y' — rp/cp, the slopes 
 of the tangents at the origin are j8' = \l//(p and /3' = — (p/\l/. 
 
 We now apply formula (91) to the branch of this quartic for 
 which j3' = \l/(<p. We obtain, after replacing the direction of 
 the force acting at the given point by the (a(x, y) considered in 
 Section 4, Chapter III, 
 
 1 (1 + aj2)3/2 
 R^lr^. 1 T— n- (92) 
 
 £0 CO'' I 
 
 Substituting in (92) ^xlf = — Nz, {ipx — ^v)l^ = -^2, 
 <pj<p — Ni from (71), we obtain the radius of curvature of the 
 quartic corresponding to (69), by theorem VI, for 2/' = \A/v and 
 
28 CURVES IN A PLANE. 
 
 /3' = ^jip. This gives 
 
 1 (1 + oiy^ 
 
 Consider now the lines of force defined by, 
 
 y' = u{x, y). 
 
 The radius of curvature of the curve of this family passing 
 through the given point is 
 
 From (93), (94), and (98) we obtain 
 
 4E = pi. (94') 
 
 Theorem X. The slopes of the two branches of the bicircular 
 quartic corresponding, by theorem VI, to the lineal element (x, y, w) 
 at the given point, are co and — (l/w). The radius of curvature of 
 the branch of slope o) is ^ of the radius of curvature of the line of 
 force passing through the given point. 
 
 To each point of the plane there corresponds, by theorem 
 VIII, a definite cubic passing through the given point. From 
 (64) and (64') we obtain the cubic of 69 to be 
 
 3(^2 + P)(a,Z - 7) - 2[iViZ2 - N^XY + N^Y^] = 0. (95) 
 
 The line Y = — 1/coX meets this curve in the point N, 
 whose coordinates are 
 
 2 (Ni + (cN2 + coW3)co 2 (Ni + uN^ + C0W3) 
 
 ^3 (l + w2)2 ' ■'^ 3 (l + «2)2 
 
 The distance 
 
 3 (1 + «2)3/2 • Ky^) 
 
 From (96), (94), and (78), we have 
 
 iON = -. (97) 
 
 Pi 
 
 This relation is equivalent to the relation (94'). 
 
 Theorem XP. The cubic associated, by theorem VIII, with any 
 point intersects the line through perpendicular to its asymptote 
 at a distance equal to ^ of the curvature of the line of force passing 
 through 0. 
 
COMPLETE CHARACTERIZATION. 29 
 
 Interpretation of (79). — The intercepts of the cubic (95) are 
 
 O CO 
 
 From these we have 
 
 Ni=iu)' OA, N3= - iOB, (98) 
 
 Substituting these values in (79), it becomes 
 
 ^(a,-0^)-^(-j + 3 '^ ' =0. (99) 
 
 If through we draw OF in the direction u{x, y) 
 and let A' and B' denote the points at which this 
 line meets the perpendicular to the axes through 
 the points A and B respectively, (99) may be 
 written 
 
 S d 2i cocOt» — OirijOti 
 
 ai t-^^') - a-y f-^^') + 3 -^V^ = "• "««) 
 
 This is an intrinsic property, since it is true for any choice of 
 rectangular axes. 
 
 Theorem XI. When the point is moved, the cubic associated 
 ivith it by theorem VIII changes in the following manner. Take 
 any two fixed perpendicular directions for the x direction and the 
 y direction; through draw lines in these directions meeting the 
 cubic again in the points A and B. Construct the tangent to the 
 line of force at 0. At A draw a line parallel to the Y axis meeting 
 this tangent in the point A' and at B draw a line parallel to the x 
 axis meeting the tangent in B'. Then the distance AA' and BB' 
 and the slope a of the line of force satisfy relation (100). 
 
 Interpretation of (83). — The equation of the conic correspond- 
 ing to (69) by theorem IX may be obtained from (40) by 
 substituting 
 
 R3. 
 
 Making these substitutions, the result is 
 
 RiX' - R2XY + EsF^ + (coF + Z) = 0. (101) 
 
 The line Y = coX meets this conic in the point M whose coor- 
 dinates are 
 
 — /il. 
 
 — it2, 
 
 <Px 
 
 <p 
 
 <P 
 
 <P 
 
30 CURVES IN A PLANE. 
 
 y_ 1 + co^ „_ (l + «> 
 
 ■A — — rt ni or>t / — — 
 
 ill- coi^+ w2^3* ill - coilz + w'iJi* 
 
 The distance 
 
 <'^ = B^r^-i;«;- (102) 
 
 Now consider the orthogonal trajectories of the lines of force 
 defined by 
 
 y'=--r—\' (103) 
 
 ^ co(a:, y) 
 
 The radius of curvature of the one of this family passing 
 through the given point is 
 
 pi = . (104) 
 
 From (102), (104) and the first relation of (83), we have 
 
 OM = p2. (1040 
 
 Theorem XII. Of the oo^ curves of the system (6) which pass 
 through a given point in a direction normal to the direction of the 
 force acting at the point, there is one which has five point contact 
 with its osculating circle. The radius of curvature of this element 
 is equal to the radium of curvature of the orthogonal trajectory of the 
 lines of force which passes through the given point. 
 
 Again, consider the radius of curvature of the quartic of 
 theorem VI corresponding to the lineal element [x, y, — (1/co)] 
 for the branch of slope — (1/w). By formula (91) we obtain 
 
 (1 + w2)3/2 
 R = -r V, Tn • (105) 
 
 — w* w H I 
 
 <p <p <p J 
 
 Substitute Rz = <Pxl<p, R2 = i<Pu + ^x)l<p, Ri = ^vf<p in (105), 
 to get the radius of curvature of the quartic corresponding to 
 (69) for y' = - 1/w and /3' = - 1/w. This gives 
 
 (1 + 0)2)3/2 
 
 ^ " 4(ili - 0iR2 + o^'Ri) ' ^^^^^ 
 
 From (104), (106) and the first relation of (83), we find 
 
 4J? = P2. 
 This relation is equivalent to the relation (104'). 
 
COMPLETE CHAEACTEEIZATION. 31 
 
 Theorem XIP. The slopes of the two branches of the bicircular 
 quartic corresponding, by theorem VI, to the lineal element 
 [x,y, — (1/co)] are co and — 1/co. The radius of curvature of the 
 branch of slope — (1/w) is equal to ^ of the radius of curvature of 
 the orthogonal trajectory of the lines of force which passes through 
 the given point. 
 
 Interpretation of (83')- — The intercepts of the conic (101) are 
 
 ill il3 
 
 Then 
 
 _ 1 _ ^ 
 
 Substituting these values and the values of iVi and N3 from 
 (98) in (830, we have 
 
 30,2-0^ +2 r^+a)„) = 0, 3-OB + 2(^-a),)=0. (107) 
 
 These are intrinsic relations, since they hold for any choice of 
 rectangular axes. 
 
 Theorem XIII. The intercepts of the conic associated, by 
 theorem IX, with any point {x, y), and the intercepts of the cubic 
 associated, by theorem VIII, with the same point, satisfy the 
 relation (107). 
 
 Interpretation of (87). — The cubic corresponding to (69) by 
 theorem VII may be obtained from (33) by substituting 
 
 \l/y<P — 2^y^ 
 
 
 
 <P' 
 
 -Ki- ^ , 
 
 The cubic is 
 KiX'-K2X^Y+K3XY'-K,Y'- {X'+ F2)(l + w^) = 0. (108) 
 This cubic is intersected by 7 = — (l/w)X at the point Mi 
 
32 CURVES IN A PLANE. 
 
 whose coordinates are 
 
 ^ ^ i(l + C02)2C0 
 
 Y= - 
 
 (1 + c^r 
 
 The distance 
 
 From (109), (94), and (87), we obtain the relation 
 
 20M = pi. (110) 
 
 Theorem XIV. Of the oo ^ conies of theorem I which pass through 
 a given point in the direction of the line of force through that point, 
 there is one which is hyperosculated by its circle of curvature; the 
 radius of curvature of this conic is ^ of the radium of curvature of 
 the line of force passing through the given point. 
 
 Interpretation of (86). — The cubic (108) is intersected by 
 Y = wX at the point M^ whose coordinates are 
 
 y = 
 
 The distance 
 
 (111), (104) and (86), give the relation 
 
 OM2 = P2. (112) 
 
 Theorem XV. Of the 00 ^ conies of theorem I which pass 
 through a given point in a direction normal to the direction of the 
 line of force through that point, the radium of curvature of the one 
 hyperosculated by its circle of curvature is equal to the radiums of 
 curvature of the orthogonal trajectory of the lines of force which 
 passes through the given point. 
 
 Interpretation of (88). — The intercepts of the cubic (108) are 
 
 1+0)2 Q I 2) 
 
 0^, = ^!^^, 0B2=-'^^-^, 
 
 ^1 
 
 -coK2-{-co'Kz- o>^K^ 
 
 
 a;(l + co2)2 
 
 Kr 
 
 -oiK2 + o>'Kz-oi^Ki 
 
 
 (1 + 0)2)5/2 
 
COMPLETE CHAKACTERIZATION. 33 
 
 Then 
 
 rr _ L+^' K -- i±^' 
 
 Substituting these values and the values of Ni and Nz from (98) 
 and (88), we have 
 
 ^•^^-^W'-'^^]^'- 
 
 (113) 
 
 This is an intrinsic relation. 
 
 Theorem XVI. The intercepts of the cubic associated, by 
 theorem VI, with any point (x, y), and the intercepts of the cubic 
 associated by theorem VIII with the same point, satisfy the relation 
 (113). 
 
 Any quadruply infinite system of curves in a plane along 
 which the pressure is proportional to the normal component of 
 the acting force possesses properties I, II, III, IV, V, VI, VII, 
 VIII, IX, X, XI, XII, XIII, XIV, XV, XVI; and, conversely, 
 if a quadruply infinite system possesses these properties (restated 
 by replacing the direction of the acting force by the function 
 o){x, y) defined in section 4, chapter III, there is a field of force in 
 which this system represents the family of curves along which 
 the pressure is proportional to the normal component of the 
 acting force. 
 
VITA 
 
 Sarah Elizabeth Cronin, Bachelor of Science, University of 
 Iowa, 1903; Master of Science, University of Iowa, 1905; In- 
 structor in Mathematics, Iowa State College, 1905-1907; In- 
 structor in Mathematics, Iowa State University, 1907-1913; 
 Graduate student at Columbia University, 1913-1915. 
 
 84 
 
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