Skip to main content

Full text of "An introduction to the infinitesimal calculus; notes for the use of science and engineering students"

See other formats


LIBRARY 


OF  THE 


University  of  California. 


Class 


.y^i 


^'"t-k 


'-■J 'r  ■,-».-•  .  . 

Ff^^J^:-:.  .... 


'^•-*:.: 


■m^ 


"  ■:,s>i. 


'■-<^^. 


vJ».v 


r-.''.*-'^''f-.. 


AN   INTRODUCTION 


TO    THE 


INFINITESIMAL  CALCULUS 

NOTES  FOR  THE  USE  OF  SCIENCE 
AND   ENGINEERING   STUDENTS 


BY 


H.  S.  CARSLAW,  M.A.,  D.Sc,  F.R.S.E. 

n 

PROFESSOR  OF  MATHEMATtCS  IN  THE  UNIVERSITY  OF  SYDNEY 

FORMERLY  FELLOW  OF  EMMANUEL  COLLEGE,  CAMBRIDGE 

AND  LECTURER  IN  MATHEMATICS  AT  THE  UNIVERSITY  OF  GLASGOW 


OF   THE 

UNIVERSITY 

OF 


LONGMANS,    GREEN,    AND    CO. 

39  PATERNOSTER  ROW,   LONDON 
NEW  YORK,   AND  BOMBAY 

1905 


Qf\3o3 

03? 


t-'a'f/jo 


PREFACE 

These  introductory  chapters  in  the  Infinitesimal  Calculus  were 
lithographed  and  issued  to  the  students  of  the  First  Year  in 
Science  and  Engineering  of  the  University  of  Sydney  at  the 
beginning  of  last  session.  They  form  an  outline  of,  and  were 
meant  to  be  used  in  conjunction  with,  the  course  on  The  Elements 
of  Analytical  Geometry  and  the  Infinitesimal  Calculus,  which  leads 
up  to  a  term's  work  on  Elementary  Dynamics. 

The  standard  text-books  amply  suffice  for  the  detailed  study 
of  this  subject  in  the  second  year,  but  the  absence  of  any  dis- 
cussion of  the  elements  and  first  principles  suitable  foi-  the  first 
year  work,  was  found  to  be  a  serious  hindrance  to  the  work  of 
the  class.  For  such  students  a  separate  course  on  Analytical 
Geometry,  Avithout  the  aid  of  the  Calculus,  is  not  necessary,  and 
the  exclusion  of  the  methods  of  the  Calculus  from  the  analytical 
study  of  the  Conic  Sections  is  quite  opposed  to  the  present 
unanimous  opinion  on  the  education  of  the  engineer.  It  has 
been  our  object  to  present  the  fundamental  ideas  of  the  Calculus 
in  a  simple  manner  and  to  illustrate  them  by  practical  examples, 
and  thus  to  enable  these  students  to  use  its  methods  intelli- 
gently and  readily  in  their  Geometrical,  Dynamical,  and  Physical 
work  early  in  their  University  course.  This  little  book  is  not 
meant  to  take  the  place  of  the  standard  treatises  on  the  subject, 
and,  for  that  reason,  no  attempt  is  made  to  do  more  than  give 
the  lines  of  the  proof  of  some  of  the  later  theorems.  As  an 
introduction  to  these  works,  and  as  a  special  text-book  for  such 


208534 


vi  PREFACE 

a  "  short  course  "  as  is  found  necessary  in  the  engineering  schools 
of  the  Universities  and  in  the  Technical  Colleges,  it  is  hoped  that 
it  may  be  of  some  value. 

In  the  preparation  of  these  pages  I  have  examined  most  of 
the  standard  treatises  on  the  subject.  To  Nernst  and  Schonflies' 
Lehrbuch  der  Differential-  und  Integral  -  Reclmung,  to  Vivanti's 
Complementi  di  Matematica  ad  uso  dei  Chemici  e  del  Naturalisti,  to 
Lamb's  Infinitesimal  Calculus,  and  to  Gibson's  Elementary  Treatise 
on  the  Calculus,  I  am  conscious  of  deep  obligations.  I  should 
also  add  that  from  the  two  last-named  books,  and  from  those 
of  Lodge,  Mellor,  and  Murray,  many  of  the  examples  have  been 
obtained. 

In  conclusion,  I  desire  to  tender  mj'  thanks  to  my  Colleagues 
in  the  University  of  Sydney,  Mr.  A.  Xewham  and  Mr.  E.  M. 
Moors,  for  assistance  in  reading  the  proof-sheets  ;  to  my  students, 
Mr.  D.  R.  Barry  and  Mr.  R.  J.  Lyons,  for  the  verification  of 
the  examples ;  also  to  my  old  teacher,  Professor  Jack  of  the 
University  of  Glasgow,  and  to  Mr.  D.  K.  Picken  and  Mr.  R.  J. 
T.  Bell  of  the  Mathematical  Department  of  that  University,  by 
whom  the  final  proofs  have  been  revised. 

H.  S.  CARSLAW. 


The  University  of  Sydney, 

Jime  1905. 


CONTENTS 

CHAPTEE    T 

CO-ORDINATE   GEOMETRY -THE   STRAIGHT    LIXE 

SECT.  PAGE 

1.  Cartesian  Co-ordinates         .               .               .               .  .1 

2.  The  Co-ordinates  of  the  Point  at  which  a  Line  is  divided  in 

a  "iven  Ratio    .               .               .               .               .  .1 

3.  The  Equation  of  the  First  Degree  .               .               .  .3 

4.  Lines  whose  Equations  are  given    .               .               .  .4 

5.  The  Gradient  of  a  Straight  Line      .               .               .  .5 

6.  Different  Forms  of  the  Equation  of  the  Straight  Line  .        5 

7.  The  Perpendicular  Form    .               .               .               .  .7 

8.  The  Point  of  Intersection  of  two  Straight  Lines        .  .        7 

9.  The  Angle  between  two  Straight  Lines         .               .  .8 
10.   The  Length  of  the  Perpendicular  from  a  given  Point  upon  a 

Straight  Line    .               .               .               .               .  .10 

Examples  on  Chapter  I              .              .             .  .12 


CHAPTEE    II 

THE   MEANING   OF   DIFFERENTIATION 

11.  The  Idea  of  a  Function       .  .  .  .  .14 

12.  Illustrations  from  Physics  and  Dynamics     .  .  .14 

13.  The  Fundamental  Problem  of  the  Differential  Calculus  .      16 

vii 


via 


CONTENTS 


SECT. 

14.   Rectilinear  Motion 


PAGE 

16 


15.  Limits.     Dift'erential  Coefficient  .17 

16.  Geometrical  Illustration  of  the  Meaning  of  the  Differential 

Coefficient         .  .  .  .  .  .20 

17.  Apjjroximate    Graphical   Determination   of   the    Differential 

Coefficient  .  .  .  .  .  .21 

18.  The  Shape  of  the  Curve  y  =/{.':)  deduced  from  the  Differential 

Coefficient  of/(a;)  .  .  .  .  .22 


Examples  on  Chapter  II. 


23 


CHAPTER    III 

DIFFEREXTIATIOX   OF   ALGEBRAIC    FUNCTIONS;    AND  SOME 
GENERAL  THEOREMS  IN  DIFFERENTIATION 

19.  Differentiation  of  cc"             .               .              .               .  .25 

20.  Some  General  Theorems — 

I.   Differentiation  of  a  Constant           .  .26 
II.   Differentiation  of  the  Product  of  a  Con.stant  and  a 

Function            .               .                             .  .26 

III.  Differentiation  of  a  Sum    .                             .  .27 

IV.  Differentiation  of  the  Product  of  Two  Functions  .      27 
V.   Differentiation  of  the  Quotient  of  Two  Functions  28 

VI.  Differentiation  of  a  Function  of  a  Function  .      29 

Examples  on  Chapter  III.          .                            .  .31 


CHAPTER    IV 


THE   DIFFERENTIATION   OF   THE   TRIGONOMETRIC  FUNCTIONS 


21.  Differentiation  of  sin  ;/■ 

22.  Differentiation  of  cos  .'■        .  .  , 

23.  Differentiation  of  tan  ,'■ 

24.  Geometrical  Proofs  of  these  Theorem.- 

25.  Difl'erentiatinn  of  pin"Vv     . 


33 
34 
34 
35 
36 


CONTENTS  ix 

SECT.  PAGE 

26.  Differentiation  of  COS" ^x     .               .  .36 

27.  Differentiation  of  tan "^x    .  .               .37 

Examples  ox  Chaptek  IV.  .              .38 


CHAPTEE    V 

THE   EXPONENTIAL  AND  LOGARITHMIC  FUNCTIONS;   MAXIMA 
AND  MINIMA  ;   PARTIAL  DIFFERENTIATION 


28.  Introductory  .... 

29.  Dift'erentiation  of  e^ 

30.  Differentiation  of  log  x        . 

31.  Logarithmic  Differentiation 

32.  Differentiation  of  e""'' sin  6.r 

33.  Maxima  and  Minima  of  Functions  of  one  Variable 

34.  Points  of  Inflection 

35.  Partial  Differentiation 

36.  Partial  Differentiation  {continued)    . 

37.  Total  Differentiation 

38.  Differentials  .... 

Examples  on  Chapter  V. 


40 
40 
41 
42 
42 
43 
45 
45 
46 
47 
48 

50 


CHAPTEE    VI 

THE  CONIC   SECTIONS 

39.  Introductory          .               .               .               .  .53 

40.  Discussion  of  the  Parabola  and  Examples     .  .  .53 

41.  Discussion  of  the  Ellipse  and  Examples       .  .56 

42.  Discussion  of  the  Hyperbola  and  Examples  .  .      59 

CHAPTEE   VII 

THE  INTEGRAL  CALCULUS— INTEGRATION 

43.  Definition  of  the  Indefinite  Integral  .  -  .64 

44.  Standard  Integrals  .  .  .  .  .65 


CONTENTS 


SECT. 

45.  Two  General  Theorems 

46.  Integration  by  Substitution 

47.  Integration  by  Substitution  {continued) 

48.  Integration  by  Part.s 

Examples  on  Chapter  VII. 


66 
67 
69 
72 


49. 
50. 

51. 
52. 

53. 
54. 

55. 
56. 
57. 

58. 


CHAPTEE    YIII 

THE   DEFIXITE   INTEGRAL   AXD   ITS   APPLICATIOXS 

Introductory  ...... 

Areas  of  Curves.      The  Definite  Integral  as  an  Expression 

for  the  Area     ...... 

The  Definite  Integral  as  the  Limit  of  a  Sum 

The  Evaluation  of  the  Definite  Integral  from  its  Definition 

as  the  Limit  of  a  Sum  ..... 


Properties  of 


J{x)dx 


XO 


Application    of    the    Definite    Integral   to    Areas    in    Polar 

Co-ordinates      ...... 

Application  of  the  Definite  Integral  to  Lengths  of  Curves 
Application  of  the  Definite  Integral  to  Volumes  of  Solids 
Application  of  the  Definite  Integral  to  Surfaces  of  Solids  of 

Revolution        ...... 

Application  of  the  Definite  Integral  to  the  Centre  of  Gra\-ity 

of  a  Solid  Body  ..... 

Application  of   the    Definite    Integral    to    the    Moment    of 

Inertia  of  a  Solid  Body  .... 

Examples  on  Chapter  VIII.       .... 


76 
79 

81 
83 

84 
85 
86 

87 

88 

90 
91 


Answers 


95 


Of   THE 

UNIVERSITY 

OF 


CHAPTEE    I 

THE   ANALYTICAL   GEOMETRY    OF    THE    STRAIGHT    LINE* 

§  1.  Cartesian  Co-ordinates. 

The  position  of  a  point  on  a  plane  may  be  fixed  in  ditt'erent 
ways.  In  particular  it  is  determined  if  its  distances  from  two 
fixed  perpendicular  lines  in  the  plane  are  known,  the  usual  con- 
ventions with  regard  to  sign  lieing  adopted.  These  two  line.^ 
Ox  and  0^  are  called  the  axes  of  x  and  y ;  and  the  lengths  OM 
and  OX,  which  the  perpendiculars  from  the  point  P  cut  off  from 
the  axes,  are  called  the  co-ordinates  of  the  point  P  and  denoted 
by  X  and  //.  OM  and  OX  are  taken  positive  or  negative  accord- 
ing as  they  are  measured  along  Ox  and  Oij,  or  in  the  opposite 
directions. 

Ex.  1.  ilark  on  a  piece  of  squared  paper  the  position  of  the  points 
(±2,  ±3). 

2.  Prove  that  the  distance  between  the  points  (2,   -3),   and  (-2,   -3)  is 

■2\/l3. 

3.  Prove  that  tlie  distance  d  between  the  points  {xi,  t/i),  (.v.i,  2/2)  i''  given 
by  d-  =  {Xi- x^f  4- (yj  -  y.,f. 

4.  Prove  that  the  co-ordinates  of  any  point  (.r,  y)  upon  the  circle  whose 
centre  is  at  the  point  (a,  h)  and  whose  radius  is  r,  satisfy  the  equation 

^  2.  The  Co-ordinates  of  a  Point  dividing  the  Line  joining  two 
given  Points  in  a  given  Ratio  1 :  m. 

Let  P^  and  1'.,  be  the  two  given  points  {j\,  y^,  (./■.„  //.,)  ;  and 
let  P  (.r,  y)  divide  P^P.,  in  the  ratio  /  :  m  (see  Fig.  1). 

*  The  student  is  recommended  to  read  pp.  1-25  of  Hall's  Introduction  to 
Graphical  Algebra  (2nd  ed.)  before  commencing  this  work. 
0 


THE  ANALYTICAL  GEOMETRY 


Draw  P^Mp  PM,  and  P^Mo  perpendicular  to  Ox ;  P^HK  and 
PL  parallel  to  O.i',  meeting  PJNI  and  P^M^  in  H,  K,  and  L. 


Since 


Similarly 


M, 


y 

Fig.  1. 


P,H  _  P^P 
PL  ~PP, 


m 


I 


tK'  tC-i 


x^-  X     m 


x(l  -t-  m)  =  lx.2  +  mx^, 
lx„  +  nix. 


x  = 


I  +  m 
I  +  m 


M  Mj 


These  are  the  co-ordinates  of  the  internal  point  of  section. 
Those  of  the  external  point  may  he  found  in  the  same  way  to  be 


IXn 


X=^ 


■mx-, 


l-m 


OF  THE  STRAIGHT  LINE 


and 


y  = 


^2  -  m/i 


I  -  m 

Ex.  1.   Prove  that  the  co-ordinates  of  the  middle  point  of  the  line  whicii 
cuts  off  unit  length  from  Oa;  and  0//  are  h  and  |. 

2.  Find  the  co-ordinates  of  the  jioints  of  trisection  of  this  line,  and  also  of 
the  points  which  divide  it  externally  in  the  ratio  1  : 2. 

3.  Prove  that  the  C.G.  of  the  triangle  whose  angular  ]ioints  are  (2,  1), 

(4,  3),  (2,  5)  is  the  point  (-,  3);  and  give  the  general  the 


leorem. 


§  3.  The  Equation  of  the  First  Degree  represents  a  Straight 
Line. 

If  the  point  P  move  along  a  curve  the  co-ordinates  of  the 
point  are  not  independent  of  each  other.  In  mathematical 
language  "  y  is  a  function  of  z,"  and  we  speak  of  y  =/(■''■)  as  the 
equation  of  the  curve,  meaning  that  this  equation  is  satisfied  by 
the  co-ordinates  (x,  y)  of  any  point  upon  the  curve.  For  example, 
the  equation  of  the  circle  whose  centre  is  at  the  origin  and 
whose  radius  is  a  is  *-  +  y^  =  a-.  The  properties  of  curves  may 
often  be  obtained  by  discussing  their  equations. 

The  simplest  equation  is  that  of  the  first  degree,  ax  +  hy  +  r  -0, 
It,  b,  and  c  being  constants. 

For  example,  take  the  equation 

X  +2y=4:. 

By  assigning  any  value  to  x  and  solving 
the  equation  for  y  we  obtain,  as  in  the 
accompanying  table,  the  co-ordinates  of  any 
number  of  points  upon  the  locus.  Plotting 
these  points  on  the  diagram  we  see  that 
all  lie  upon  a  straight  line. 

AVe  proceed  to  prove  that  this  is  true 
in  general ;  in  other  words,  that  all  the 
points  whose  co-ordinates  satisfy  the  equation 

ax  +  by  +  c  =  0 

lie  upon  a  straight  line. 

Let  P^  (Xp  y^  and  P.^  {x.^,  y.,)  be  two  points  upon  the  locus. 

Then  we  have  ax^  +  by^  +  c  =  0         .         .         .         ( 1 ) 

aXo  +  by^  +  c^O         ...  (2) 


X 

V 

-3 

3-5 

_  2 

3 

-  1 

2 -.5 

0 

0 

1 

1-5 

2 

1 

3 

•5 

4  THE  ANALYTICAL  GEOMETRY 

Multiplying  (1)  by  in  and  (2)  by  I,  and  adding,  we  obtain 
a{b:,  +  m,i\)  +  h{ly.^  +  mii^)  +  (■(/  +  m)  =  0, 

\    I  +  7n    /        \    I  +  m    / 

-^  ^    Ix^'rmx^     ly„  +  my,  .  ..  .     , 

i5ut    — ^ -,     ~ —   are  the  co-ordinates   of   the  point 

/  +  III  I  +  m 

dividing  P-^P^  in  the  ratio  I :  in,  and  /,  ///  may  be  chosen  at 
random.  It  follows  that  if  Pp  P.^  are  two  fixed  points  on  the 
locus  given  by 

a:c  +  by  +  c  ==  0, 

any  other  point  on  the  unlimited  straight  line  P^P.,  is  also  upon 
the  locus ;  and  it  can  easily  be  shown  that  no  point  off  this  line 
lies  upon  the  curve. 

Therefore  the  equation 

a.r  +  by  +  c  =  0 
represents  a  straight  line. 

Ex.  Prove  this  theorem  by  showing  that  if  PQR  are  any  three  points 
whose  co-ordinates  satisfy  the  given  equation,  the  triangle  PQR  has  zero  area. 

^  4.  In  the  last  article  we  have  shown  that  the  equation  of 
the  first  degree  represents  a  straight  line.  It  is  not  then 
necessary  in  plotting  the  locus  given  by  such  an  equation  to 
proceed  as  we  did  above  in  the  example  x  +  2y  -  4.  Two  points 
fix  a  straight  line.  Therefore  we  have  only  to  find  two  points 
whose  co-ordinates  satisfy  the  equation.  The  most  convenient 
points  are  those  where  the  line  cuts  the  axes,  and  these  are 
found  by  putting  x  =  0  and  y  =  0,  respectively,  in  the  equation. 

Ex.  1.  Draw  tlie  lines    (i.)  ^'  =  0,     x  =  l,     ;r=  -  1 
(ii.)  7/  =  0,     y  =  2,     y=-2 
(iii.)  r  +  y=0,      x  +  y^l 
(iv.)  y  =  2x,       //=2,r-r3 

2.  Determine  whether  the  point  (2,  3)  is  on  tlie  line 

4x  +  3y=l5. 

3.  What  is  the  condition  that  the  point  («,  h)  should  lie  upon  the  line 

ax  +  by  =  2ab '{ 


OF  THE  STRAIGHT  LINE 


§  5.   The  Gradient  of  a  Line. 

When  we  speak  of  "the  gradient"  of  a  road  being  1  in  200 
we  usually  mean  that  the  ascent  is  1  foot  vertical  for  200  feet 
horizontal.  This  might  also  be  called  the  slope  of  the  road. 
The  same  expression  is  used  with  regard  to  the  straight  line. 
The  "gradient"  or  the  "slope"  of  a  straight  line  is  its  rise  per 
unit  horizontal  distance ;  or  the  ratio  of  the  increase  in  y  to  the 
increase  in  x  as  we  move  along  the  line.  This  is  evidently  the 
same  at  all  points  of  the 
straight  line,  and  is  equal 
to  the  tangent  of  the  angle 
the  line  makes  with  the 
axis  of  ;';  measured  in  the 
positive  direction. 

To  save  ambiguity  it 
is  well  to  fix  upon  the 
angle  to  be  chosen,  and 
in  these  pages  it  will  be 
convenient  to  consider 
the  line  as  always  drawn 
upward  in  the  direction 
of  the  arrow  (Fig.  2),  and  thus  to  restrict  the  angle  (/>  to  lie 
between  0°  and  180^ 

Wiien  0<(^<^  the  gradient  is  positive. 
When  ^  <(/)<- the  gradient  is  negative. 

Ex.   1.   Write  down  the  values  of  <p  for  the  lines  in  §  4  (i.). 
2.   Prove  that  tlie  gradient  of  the  line  y  =  m.v  +  c  is  m,  and  interpret  the 
constant  c. 

§  6.  Different  forms  of  the  Equation  of  the  Straight  Line. 
In  the  preceding  articles  we  have  shown  that  the  equation 

ax  +  1)1/  +  c  =  0 

represents  a  straight  line,  and  we  have  seen  how  the  line  may 
be  drawn  when  its  equation  is  given.     We  have  now  to  show 
how  to  obfain  the  equation  of  the  line  when  its  position  is  given. 
(A)   The  equation  of  the  line  fhrouf/h  two  given  points. 


Fig.  2. 


6  THE  ANALYTICAL  GEOMETEY 

Let  (a-p  //^),  (.7;.,,  y.^  be  the  two  given  points.  Let  (.';,  y)  be 
the  co-ordinates  of  any  jjoint  upon  the  line.  Then  it  is  clear 
(cf.  Fig.  1)  that 

•^ — ^1  =  the  gradient  of  the  line, 
and  that  Vilih  = 

.Xg  —  X-^ 

Thus  we  have  the  equation 

yjlllJ-hZll 

«//  ^~  tC-i  •^o  t'j-* 

between  the  co-ordinates  (a-,  y)  of  the  representative  point  and 
the  co-ordinates  (.r^  y^  (.r.,,  y,^  of  the  fixed  points.  This  is  the 
equation  of  the  straight  line  through  these  points.  It  is  more 
conveniently  written 

X  -  x^_  y  -  y^ 

^1  -  ^2  ~  Vi-  y-2 

It  folloAvs  that 

(B)  The  equation  of  the  line  through  [u-^,  y^),  making  an  angle  ^ 
with  the  axis  of  x,  is 

qc    /yi  '      ^ 

and  that 

(C)  The  equation  of  the  line  which  cuts  off  a  length  c  from  the  axis 
of  y,  and  is  inclined  at  an  angle  whose  tangent  is  in  to  the  axis  ofx,  is 

y  =  mx  +  c, 
and  that 

(D)  The  equation  of  the  line  which  cuts  off'  intercepts  a  and  h  from 
the  axis  of  x  and  y  is 

%f=l. 
a     b 

Ex.  1.  Write  down  the  equations  of  the  lines  through  the  following  pairs 
of  points  :  (1,  1)  (1,  -  1)  ;  (1,  2)  (  -  1,  -  2) ;  (3,  4)  {5,  6) ;  {a,  b)  {a,  -  h).  ' 

2.  Find  the  equations  of  the  lines  tlirough  the  point  (3,  4)  with  gradient 
±5,  and  draw  the  lines. 

3.  The  lines  y  =  x  and  y  =  2x  form  two  adjacent  sides  of  a  parallelogram, 
the  <)2)posite  angular  point  liciiig  (4,  5).  Find  the  equations  of  the  other  two 
sides  ;  and  of  the  diagonals. 


OF  THE  STRAIGHT  LINE  7 

4.  Write  down  the  equations  of  the  lines  making  angles  30°,  45°,  60°, 
120°,  135°,  and  150°  with  the  axis  of  x,  which  cut  this  axis  at  unit  distance 
from  the  origin  in  the  negative  direction. 

§7.  The  "Perpendicular"  Form  of  the  Equation  of  the 
Straight  Line. 

A  straight  line  is  determined  when  the  length  of  the  perpen- 
dicular upon  it  from  the 
origin,   and  the  direction 
of  this  perpendicular  are 
given. 

Let  ON  be  the  perpen- 
dicular, ]),  upon  the  line. 

Let  the  angle  between 
ON  and  Ox  be  a,  this 
angle  lying  between  0 
and  27r  (cf.  Fig.  3). 

Then  N  is   the    point 

,  •         X  Fig.  3. 

(|>  cos  a,  p  Sin  a). 

Using  the  form  (B)  of  §  6  the  equation  of  the  line  becomes 


y  -  V  sm  a 

- — =  tan  d)  =  tan    a  +  „ 

x-p  cos  a  \       2 


cos  a 
sin  a 


This  reduces  to 

(E)  X  cos  a  +  y  sin  a  =7/. 

N.B. — The  quantity  p  is  to  be  taken  always  positive,  and  the 
angle  a  is  the  angle  between  0.^  and  ON. 

§  8.   The  Point  of  Intersection  of  Two  Straight  Lines. 
Since  the  point  of  intersection  of  the  two  lines 

ax  +  by  +  (■  -  0 
ax  +  b'y  +  c  -  0 

lies  on  both  lines,  its  co-ordinates  x,  y  satisfy  both  equations. 
Solving  the  equations  we  have 


X 


V 


1 


ic'  -  h'r     m  —  c'a     ah'  —  a'l 


8  THE  ANALYTICAL  GEOMETRY 

It  is  clear  that  if 

ah'  -  ah  =  0, 

and  neither  of  the  other  two  denominators  vanish,  the  co-ordinates 
.T,  y  are  infinite,  and  the  lines  are  parallel. 
If  in  addition 

ca'  -  c'a  =  0 

,  a      h      c 

we  have  -  =  -  =  - 

a      b      c 

and  the  third  denominator  he  -  h'c  also  vanishes. 

In  this  case  the  two  equations  are  not  independent,  and  they 
really  represent  the  same  straight  line. 

Ex.  1.  Find  the  co-ordinates  of  the  point  of  intersection  of  the  line.s 

.c  +  2y=&. 

Illustrate  your  result  by  a  diagram. 

2.  Find  the  equations  of  the  lines  through  (2,  3)  parallel  to 

3.  Find  the  co-ordinates  of  the  angular  points  of  the  triangle  whose  sides 
are  given  by 

^+  y  =  2        .         .         .         .         .         (1), 

Sx-2y=l (2), 

ix+Bi/=2-l (3). 

Also  find  the  equations  of  the  medians  of  this  triangle  and  the  co-ordinates 
of  its  C.G. 

§  9.  The  Angle  between  Two  Straight  Lines  whose  Equations 
are  given. 

The  equations  of  the  lines  may  always  be  reduced  to  the  forms 

( 1 )  If  =  inx  +  c, 

(2)  y=m'.r  +  c', 

and  in  this  case  the  angles  they  make  with  the  axis  of  x  are  f/j 
and  (^'  where 

tan  (^  =  m,  (cf.  Fig.  4) 

tan  </)'  =  m'. 
Hence 

tan  ((^  -  (/,    =  r  =  tan  d, 

1  -f-  mm 

and  the  angle  6  between  the  lines  is  tan      ( , 


OF  THE  STRAIGHT  LINE 


9 


Unless  care  is  shown  in  taking  for  the  line  (1)  that  with  the 
greatei^  slope,  Ave  would  obtain  a  negative  value  for  the  tangent 
of  the  an  trie  between  the  lines.     The  reason  for  this  is  obvious. 


Fig.  4. 

It  follows  that 

(i.)  The  lines  are  parallel  if  m  =  m  ; 

(ii.)  The  lines  are  perpendicular  if  mm  +1  =  0. 

When  the  equations  are 

ax  +  hij  +  c  —  0 
a'x  +  h'!J  +  r,'  =  0 

(i.)   The  lines  are  parallel  if  —  =  p  .;  -y 

(ii.)  The  lines  are  perpendicular  if  aa  +  hh'  =  0. 

Ex.  1.  Write   down    the    equation    of    the   straight    liue    through    (1,  2) 
perpendicular  to  x-y  =  0. 

2.   Find  the  angles  between  the  lines 

..•-2y+l=0} 
x  +  By  +  2  =  0) 
and  4a;  +  3j/=12) 

3,'+ 4?/ =12/' 
and  draw  the  lines. 


10 


THE  ANALYTICAL  GP:OMETRY 


3.  Write  down  the  equation  of  the  straight  line  through  (a,  b)  perpen- 
dicular to  bx-ay= a^  +  IP'. 

4.  Write  down  the  equation  of  the  line  bisecting  the  line  joining  (1,  2) 
(3,  4)  at  right  angles,  and  the  equations  of  the  perpendiculars  upon  both  lines 
from  the  origin. 

5.  Prove  that  l{x-a)-^m{y-h)  =  ()  is  a  line  through  (a,  &)  parallel  to 
lc  +  viij  =  0  ;  and  write  down  the  equation  of  the  line  through  (a,  h)  perpen- 
dicular to  lx  +  my  =  0. 

6.  AVrite  down  the  equations  of  the  lines  through  the  C.G.  of  the  triangle 
whose  angular  points  are  at  (4,  -5)  (5,  -6)  (3,  1)  parallel  and  perpendicular 
to  the  sides. 

§  10.  The  Length  of  the  Perpendicular  from  a  Point  (.i^,  v/^,) 
upon  a  Straight  Line  whose  Equation  is  given. 

(i.)  If  the  equation  of 
the  straight  line  is  given 
in  the  "  perpendicular " 
form 

X  cos  a  +  y  sill  u  =J)        (1), 

the  line  through  P  (.Tq,  y^) 
parallel    to    it    is    given 
Fio.5.  (^^   (2)    by 

{x  -  .Tq)  cos  a-T  (y  -  y^  sin  a  =  0 

or  X  cos  a  +  y  sin  a  =  Xq  cos  a  +  yQ  sin  a. 


(2), 


But  if  Pq  is  the  perpendicular  ONq  from  0  upon  the  line  (2), 
and  if  N,  Nq  are  on  the  same  side  of  0,  the  equation  of  PN^  may 
be  written 

X  cos  a  +  //  sin  a  =2\r 

Therefore 

X(^  cos  a  +  v/p  sin  a  =2\y 

Also  the  perpendicular  from  P  upon  the  line  (1)  is 

ONp  -  ON,  (cf.  Fig.  5) 

ie.  i>^-p, 

i.e.  Xq  cos  a  +  ^0  sin  a  -p. 

In  the  case  when  N^  lies  between  0  and  N  we  have  to  take 


P-Po 


OF  THE  STRAIGHT  LINE  11 

and  when  N,  Nq  lie  on  opposite  sides  of  0,  ON^^  makes  angle 
(a  +  tt)  with  O'',  and  we  have  to  take 

In  both  these  cases  the  length  of  the  perpendicular  is  given  by 

-  Xq  cos  a  -  y^  sin  a  +  p. 
(ii. )  If  the  equation  of  the  line  is  given  as 

ax  +  bj/^c     (r>0)     .  .  .  (1), 

we  have  first  to  throw  this  into  the  "  perpendicular  "  form. 
►Suppose  it  becomes 

X  cos  a  +  //  sin  a  =  'p      .  .  .        (2). 

Then,  by  equating  the  values  we  find  from  these  two  equa- 
tions for  the  intercepts  upon  the  axes,  we  obtain 

cos  a     sin  a     p 
a  be 

Therefore  c  cos  a  =  ap, 

c  sin  a  =  bp, 
and  c-  =  (a-  +  b^)p- ; 

,-.     c=  \/(T-  +  b^^  p, 

where  there  is  no  ambiguity  in  the  square  root,  as  both  j'  ^md  c 
are  positive. 

Hence  cos  a  = 


sin  a  = 


b 
c 


and  p  —  —r         ., 

^      'J  a?  +  b^ 

and  the  "  perpendicular  "  form  of  the  line 

ax  +  by  =  c     (O  0) 

.     ■  ax  by  c 

vPTP  "^  s/wTp  ~  'slWTW 

Hence  the  length  of  the  perpendicular  from  {x^,  i/q)  upon 

ax  +  bi/  -  c  =  0 

s/a^  +  b'- 


12  THE  ANALYTICAL  GEOMETEY 

And  the  positive  sign  is  taken  when  {x^,  y^)  is  upon  the  opposite 
side  of  the  h'ne  from  the  origin,  the  negative  sign  when  it  is  on 
the  same  side  of  the  line  as  the  origin.-' 

This  result  holds  for  the  equation  of  the  straight  line, 
in  Avhatever  form  it  is  given.  The  reason  for  the  change  of 
sign  in  the  expression  for  the  length  of  the  perpendicular  is 
that  the  equation  of  the  first  degree  Ix  +  my  +  n  =  0  divides  the 
plane  of  xy  into  two  parts,  in  one  of  which  Ix  +  my  +  n  is  positive  : 
and  in  the  other  it  is  negative.  Upon  the  line  the  expression 
vanishes. 

Ex.  1.   Tiausforni  the  equations 

(i. )  3.r  ±  4?/  =  5  (ii, )  3./;  +  4?/  =  -  5 

into  the  perpendicular  form,  and  from  your  tables  write  down  tlie  value  of 
a  for  each. 

2.  "Write  down  the  length  (if  the  iperpendicular  from  the  origin  upon  the 
line  joining  (2,  3)  (6,  7). 

3.  Write  down  the  length  of  the  perpendicular  from  the  point  (2.  3)  upon 
the  lines 

\jc  +  iy^l,     5x+\2y  =  2Q,     3.r  +  4(/  =  S. 

4.  P'ind  the  inscrilied  and  escribed  centres  of  the  triangle  whose  sides  are 

Zx  +  4?/  =  0,     5x-12y  =  0,     y=\5, 
and  the  equations  of  the  internal  and  external   bisectors  of  the  angles  of 
this  triangle,  distinguishing  the  different  lines. 

[The  student  is  referred  for  a  fuller  discussion  of  the  subject  matter  of  this 
chapter  to  (i.)  Briggs  and  Bryan's  Elements  of  Co-ordinate  Geometry,  Part  I. 
chapters  i.-x.  ;  (ii. )  Louey's  Co-ordinate  Geometry,  chapters  i.-vi.  ;  and  (iii.) 
to  C.  Smith's  Elementary  Treatise  on  Conic  Sections,  chapters  i.  and  ii. 

In  all  these  hoolcs  a  large  number  of  examjiles  will  be  found  illustrating 
the  points  we  have  discussed.] 

EXAMPLES   ON   CHAPTER    I 
1.   Find  the  equation  of  the  locus  of  the  point  P  which  moves  so  that 

(i.)  AP2+PB-^  =  c2 
(ii.)  AP2-PB2  =  c-^ 
(iii.)      AP.PB  =  c-, 
A  and  B  being  the  points  (-«,  0),  {a,  0). 

Ride. — To  find  the  length  of  the  perpendicular  from  a  given  point  (o:„,  y^) 
upon  a  given  straight  line 

lx-\-my-\-n  =  Q, 
insert  tlie  values  (,r„,  ?/„)  in  place  of  {x,  y)  in  the  linear  exjiression  and  divide  by 
the   square  root  of  the  sum  of  the  squares  of  the  coefficients  of  x  and  y  in  this 
expression. 


OF  THE  STRAIGHT  LINE  13 

2.  Find  the  equation  of  the  straight  line  through  (  - 1,  3),  (3,  2),   ami 
show  that  it  passes  through  (11,  0). 

3.  Show  that  the  lines 

3.>'-    2?/H-7--=0 
ix+     2/  +  3  =  0 
19./;+ 13?/       =0 
all  pass  through  one  point,  and  lind  its  co-ordinates. 

4.  Find  the  equations  of  the  lines  through  the  origin  parallel  and  perpen- 
dicular to  the  lines  of  Ex.  3  ;    also  those  through  the  point  (2,  2). 

.5.   Find  the  equation  of  the  line  joining  the  feet  of  the  perpendiculars 
from  the  origin  u]ion  tlie  lines 

4x+   il=\1 
x  +  2y  =  o. 

6.  Draw  the  lines 

4?/  +  3a-  =  12 
Sy  +  ix=2i. 
Find  the  equations  of  the  bisectors  of  the  angles  between  them,  distinguish- 
in£c  the  two  lines. 

7.  The  sides  of  a  triangle  are 

,,:-    ?/+    1=0 
X-ilf+    7  =  0 
x  +  2ij-U=0. 
Find  (i. )  the  co-ordinates  of  its  angular  points, 

(ii.)  the  tangents  of  its  angles, 

(iii. )  the  e(|uations  of  the  internal  and  external  bisectors  of  these 
angles. 
8.   The  angular  points  of  a  triangle  are  at  (0,  0)  (2,  4)  (  -  6,  8).     Find 
(i.)  the  equations  of  the  sides, 
(ii.)  the  tangents  of  the  angles, 
(iii. )  the  equations  of  the  medians, 
(iv.)  the  equations  and  lengths  of  the  perpendiculars  from  the  angular 

points  on  the  opposite  sides, 
(v.)  the  equations  of  the  lines  through  the  angular  points  parallel  to 

the  opposite  sides, 
(vi.)  the  co-ordinates  of  the  C.G., 

(vii.)  the  co-ordinates  of  the  centres  of  the  inscribed,  circumscribed, 
and  nine-points  circles. 


CHAPTER    II 

THE   MEANING    OF    DIFFERENTIATION 

§  11.  The  Idea  of  a  Function. 

If  two  variable  quantities  are  related  to  one  another  in  such 
a  way  that  to  each  value  of  the  one  corresponds  a  definite 
value  of  the  other,  the  one  is  said  to  be  a  function  of  the  other. 
The  variables  being  x  and  i/,  we  express  this  by  the  equation 
y  =f{x) ;  in  Avhich  case  z  and  y  are  called  the  independent  and 
dependent  variables  respectively.  Analytical  Geometry  furnishes 
us  with  a  representation  of  such  functions  of  great  use  in  the 
experimental  sciences.  The  variables  are  taken  as  the  co- 
ordinates of  a  point,  and  the  curve,  whose  equation  is 

gives  us  a  picture  of  the  way  in  which  the  variables  change. 

So  far  as  we  are  concerned  in  these  chapters  the  equation 
y  -f{x)  may  be  assumed  to  give  us  a  curve.  There  are,  how- 
ever, some  peculiar  functions  which  cannot  thus  be  represented. 

v^  12.  Examples  from  Physics  and  Dynamics. 

If  a  quantity  of  a  perfect  gas  is  contained  in  a  cylinder 
closed  by  a  piston  the  volume  of  the  gas  Avill  alter  with  the 
pressure  upon  the  piston.  Boyle's  Law  expresses  the  relation- 
.?hip  between  the  pressure  p  upon  unit  area  of  the  piston, 
and  the  volume  r  of  the  gas,  when  the  temperature  remains 
unaltered.     This  law  is  given  by  the  equation 


pv=]>^>\ 


0' 


where  p^,  l■^^  are  two  corresponding  values  of  the  pressure  and 

14 


THE  MEANING  OF  DIFFERENTIATION  15 

the  volume.  When  the  volume  v  for  unit  pressure  is  unity, 
this  equation  becomes 

2w=  1, 

and  the  rectangular  hyperbola,  Avhose  equation  is 

X1J  =  1, 

will  show  more  clearly  than  any  table  of  numerical  values  of  p 
and  V  the  way  in  which  these  quantities  change. 

When  the  pressure  is  increased  past  a  certain  point  Boyle's 
Law  ceases  to  hold,  and  the  relation  between  p  and  v  in  such  a 
case  is  given  by  van  der  Waals's  equation  : — • 

a  and  b  being  certain  positive  quantities  which  have  been 
determined  by  experiment  for  different  gases.  Inserting  the 
values  of  a  and  h  for  the  gas  under  consideration,  and  drawing 
the  curve 

with  suitable  scales  for  x  and  //,  the  Avay  in  which  ^;  and  v  vary 
is  made  evident. 

Such  illustrations  could  be  indefinitely  multiplied.  We  add 
only  two,  taken  from  the  case  of  the  motion  of  a  particle  in 
a  straight  line. 

When  the  velocity  is  constant,  the  distance  s  from  a  fixed  point 
in  the  line  to  the  position  of  the  particle  at  time  t  is  given  by 

s  =  rt  +  Sq, 

where  s^  is  the  distance  to  the  initial  position  of  the  particle, 
and  V  is  the  constant  velocity. 
The  straight  line 

y  =  vx  +  s^ 

then  represents  the  relation  between  s  and  t. 

When  the  acceleration  is  constant,  the  corresponding  equation  is 

s  =  1/^2  +  ^_j^  ^  ,^^ 
where  /  =  the  acceleration, 

Vq  =  the  initial  velocity, 

5,5  =  the  distance  to  the  initial  position. 


f 


16  THE  MEANING  OF  DIFFERENTIATION 

In  this  case  we  have  the  parabola 

y  =  h'^x-  +  r^x  +  Sy. 

Also  in  both  these  cases  we  might  obtain  an  approximate  value 
of  s  for  a  given  value  of  /,  or  the  value  of  /  for  a  given  value 
of  s,  by  simple  measurements  in  the  figures  representing  the 
respective  curves. 

i^  13.  The  Fundamental  Problem  of  the  Differential  Calculus. 

The  aim  of  the  Differential  Calculus  is  the  investigation  of 

the  rate  at  which  one  variable  quantity  changes  with  regard  to 

another,  when  the  change  in  the  one  depends  upon  the  change 

I  in  the  other,  and  the  magnitudes  vary  in  a  continuous  manner, 

y  The  element  of  time  does  not  necessarily  enter  into  the  idea  of 

a  rate,  and  we  may  be  concerned  with  the  rate  at  which  the 
pressure  of  a  gas  changes  with  the  volume,  or  the  length  of  a 
metal  rod  with  the  temperature,  or  the  temperature  of  a  con- 
ducting wire  with  the  strength  of  the  electric  current  along  it, 
or  the  boiling  point  of  a  liquid  with  the  barometric  pressure,  or 

I         the  velocity  of  a  wave  with  the  density  of  the  medium,  etc.  etc. 
The  simplest  cases  of  rates  of   change  are,    however,   those  in 

*         which  time  does  enter,  and  we  shall  liegin  our  consideration  of 
the  subject  with  such  examples. 

§  I  i.  Rectilinear  Motion. 

In  elementary  dynamics  the  velocity  of  a  point,  which  is 
moving  uniformly,  is  defined  as  its  rate  of  change  of  position, 
and  this  is  equal  to  the  quotient  obtained  by  dividing  the 
distance  traversed  in  any  period  by  the  duration  of  the  period, 
the  distance  being  expressed  in  terms  of  a  unit  of  length,  and 
the  period  in  terms  of  some  unit  of  time. 

When  equal  distances  are  covered  in  equal  times  this  fraction 
is  a  perfectly  definite  one  and  does  not  depend  upon  the  time, 
1)ut  when  the  rate  of  change  of  position  is  gradually  altering, 
as,  for  instance,  in  the  case  of  a  body  falling  under  gravity,  the 
value  of  such  a  fraction  alters  with  the  length  of  the  time  con- 
sidei-ed.  If,  however,  we  note  the  distance  travelled  in  difterent 
intervals  measured  from  the  time  t,  such  intervals  beinir  taken 
smaller  and  smaller,  we  find  that  the  values  we  obtain  for  what  we 


/ 


THE  MP:ANING  of  DIFFEKENTIATION  17 

might   call    the   average   velocity   in    these  intervals    are   getting 
nearer  and  nearer  to  a  definite  quantity. 

For  example,  in  the  case  of  the  body  falling  from  rest  we  have 

s=^hgf. 

Let  (s  +  &)  be  the  distance  which  corresponds  to  the  time 
{f  +  8f). 

These  quantities  8s  and  8i  added  to  s^  and  f  ave  called  the 
"  increments  "  of  these  variables. 

Then        .s  +  8s  -  hg{t  +  8t)"  =  hgt-  +  gt .  8t  +  hg(8ty', 

8s 
and  .-.  ~-  -^  qt  +  }jg8f. 

8t 

It  is  clear  that  as  8t  gets  smaller  and  smaller,  the  "  average 
velocity  "  in  the  interval  8f  approaches  nearer  and  nearer  to  the 
value  gt.  This  value  towards  which  the  average  velocity  tends 
as  the  interval  diminishes  is  called  the  velocitij  at  the  instant  t,  on 
the  understanding  that  wo  can  get  an  "average  velocity"  as 
near  this  as  we  please  by  taking  the  interval  sufficiently  small. 
The  actual  motion  with  these  average  velocities  in  the  successive 
intervals  would  be  a  closer  and  closer  approximation  to  the  con- 
tinually changing  motion  in  proportion  to  the  minuteness  of  the 
subdivisions  of  the  time.  The  advantage  of  the  method  of  the 
Dirt'erential  Calculus  is  that  it  gives  us  a  means  of  getting 
these  "instantaneous  velocities,"  or  rates  of  change,  at  the  time 
considered,  and  that,  when  the  mathematical  formula  connecting 
the  quantities  is  given,  we  can  state  what  the  rate  of  change  of 
the  one  is  with  regard  to  the  other,  without  being  dependent 
upon  an  approximation  obtained  by  a  set  of  observations  in 
gradually  diminishing  intervals. 

§  15.  Limits.     Differential  Coefficient. 

If  a  variable  which  changes  according  to  some  law  can  be 
made  to  approach  some  fixed  constant  value  as  nearly  as  we  please, 
but  can  never  become  exactly  equal  to  it,  the  constant  is  called 
the  limit  of  the  variable  under  these  circumstances.  Now  if 
this  variable  is  .'•,  and  the  limiting  value  of  x  is  a,  the  dependent 
variable  y  (where  y^f{o'))  may  become  more  and  more  nearly 
equal  to  some  fixed  constant  value  h  as  x  tends  to  its  limit  '/, 


18  THE  MEAjS^ING  OF  DIFFERENTIATION 

and  we  may  be  able  to  make  y  difter  from  h  by  as  little  as  we 
please,  by  making  x  get  nearer  and  nearer  to  a.  In  this  case 
h  is  called  the  limit  of  the  function  as  x  approaches  its  limit  a,  or 
more  shortly,  the  limit  of  the  function  for  x  =  a,  and  this  is 
written  Lt^^,,  (y)  =  h. 

„  X .  sin  a; 

E.g.  {I.)   It  y=~r^ 


(li.)  If  /y  = 


1 


or,  more  correctly,  y  has  no  limit  for  x  =  Q.  '^ 

In  this  last  example  the  function  increases  without  limit  as  x 
approaches  its  limit.  AVe  might  have  the  corresponding  case 
of  x  increasing  without  limit  and  the  function  having  a  definite 
limit :   e.g.  if 

y  =  a^  where  0 < ft<  1, 

M.=  oo(y)  =  o. 

This  idea  of  a  limit  has  already  (§  14)  been  employed,  and 
when  s  =  hgt~,  the  velocity  at  the  time  t  of  the  moving  point  is 
what  we  here  define  as 

In  the  general  case  of  motion  when  the  relation  between 
s  and  t  is  s  —f(t),  we  take  the  distance  at  the  time  (/  +  o^)  as 
(s  +  8s),  and  we  have 

s  +  8s^f{t  +  8t), 

8s  _  /(/  +  8t)  -fit) 
8f~  8t  ■ 

Hence  the  velocity  at  the  time  t  is  given  by 

''-^^''=\8t)-^^"='\'~      8t /• 

"  P^or  a  full  discussion  of  the  idi-a  of  /irnit,  see  Gibson's  Calculus,  chapter  iv. 


or 


THE  MEANING  OF  DIFFERENTIATION  19 

This  limiting  value  of  the  ratio  of  the  increment  of  .s  to  the 
increment  of  t  as  the  increment  of  t  approaches  zero  is  called  the 
differential    coefficient  of  s  with  regard   to    t.      Instead  of  tc riling 

Lt&t=J'v;],   '^'<^  use  the  symbol  —,,for  this  limiting  value.     It  must, 
\6t J  ■  at 

hoioever,   he  carefully  noticed  that  in  this  symbol  ds  and  dt  cannot, 

ds 
so  far  as  we  are  here  concerned,   be  taken  separately,   and  that  -y, 

stands  for  the  result  of  a  definite  mathematical  operation,  viz.  the 
evaluation  of  the  limiting  value  of  the  ratio  of  the  corresponding 
increments  of  s  and  t,  as  the  increment  of  t  gets  smaller  and  smcdler. 

We  shall  see  later  in  §  38  that  there  is  another  notation  in 
which  ds  and  dt  are  spoken  of  as  separate  quantities,  but  until 
that  section  is  reached,  it  will  be  Avell  always  to  think  of  the 
differential  coefficient  as  the  result  of  the  operation  we  have  just 
described.  It  is  clear  that  if  8t  is  very  small,  the  corresponding 
increment  of  s,    namely  8s,   will  be  very   approximately  given 

by  -7-  •  St.  Still  it  is  not  a  true  statement,  but  only  an  approxi- 
mation, to  say  that  in  this  ease 

This  approximation  may,  however,  be  employed  in  finding 
the  change  in  the  dependent  variable  due  to  a  small  change  in 
the  independent  variable,  or  the  error  in  the  evaluation  of  a 
function  due  to  a  small  error  in  the  determination  of  the 
variable,  provided  Ave  know  the  differential  coefficient  of  the 
function. 

We  add  some  examples  in  which  the  differential  coefficients 
are  to  be  obtained  from  the  above  definition,  viz. — 


If 


^_f,f.      ds_  ffit  +  8t)-f(t)~^ 


Ex.  1.    Us  =  at  +  b,  -rr  =  a. 
dt 

1.   If  s  =  «<2  +  2W  +  c,  ~  =  2(«<  +  h). 

3.  Ife  =  <  '5^  =  w. 

at 

4.  lia;  =  «sinwc,  -;-  =  aaj  cos  u/. 

dt 


20 


THE  iMEANING  OF  DIFFERENTIATION 


i;  IG.  Geometrical  Illustration  of  the  Meaning  of  a 
Differential  Coefficient. 

In  the  last  sections  we  have  been  led  to  the  idea  of  a  limiting 
value  by  the  consideration  of  a  moving  particle,  and  have  thus 

been  brought  to  define  the 


y 

A 

T 
H 

differential  coefficient  of  s 
with  regard  to  /. 

We  have  another  illus- 
tration of  the  meaning  of 
the  differential  coefficient 
in  the  consideration  of  the 
gradient,  or  slope,  of  the 
curve 

y 

c 

)                    K 

t5. 

4 

Let  P  be  the  point  (a:,  //) 
and    Q    the    point    (o:  +  &•, 

V  ~  %))  ^iitl  let  the  tangent  at  P  make  an  angle  </>  with  Ox. 


Then  in  Fig.  6 


OM  =  .r 

ON  =x  +  &r' 


^  and  MP  =  //  =/(.t)  -\ 


MN  =  8x 

Thus  the  slope  of  the  secant  PQ 

=  tan  HP(^) 

^Sj    - 
8:r 

_f(x  +  8x)-f(x) 

~  8x  ■         ' 


Now  if  we  keep  P  fixed  and  let  Q  approach  P,  the  secant  PQ 
gets  nearer  and  nearer  the  tangent  at  P,  and  the  limiting  value 

of  the  fi-action  ^  as  8x  gets  smaller  and  smaller  is  tan  c/j. 


Thus,  Avith  the  same  notation  as  before 


'^=U..i^\  =  U 


6a: =0 


8x 


Sx  =  0 


8x 


tan  (fy. 


THE  MEANING  OF  DIFFERENTIATION 


21 


Since  the  slope  of  the  tangent  is  known  when  -y  is  found,  we  can 
at  once  proceed  to  write  dotvn  the  equation  of  the  tangent  at  a  'point  on 
the  curve  y  ^f(x),  when  the  value  of '-  at  that  point  is  known. 

Ex.  1.   If/(a')  =  c""',  write  down /(.r  +  /i)  ;  and  show  that 


Zt 


fi.r)-f{x-hy 
h 


Interpret  this  result  geometrically. 

2.  Find  the  value  of  -p  at  the  point  (2,  1)  on  the  curve  4y  =  x^,  and  show 
tliat  the  equation  of  the  tangent  at  that  point  to  this  parahola  is 

^   17.   Approximate  Graphical  Determination   of  the  Differ- 
ential Coefficient. 

When  the  equation  connecting  x  and  //  is  such  that  the  curve 

may  be  easily  drawn,  the  slopes  of  the  various  positions  of  the 
secants  PQ,  as  Q  is  made  to  move  nearer  and  nearer  to  P,  will 
give  a  series  of  values  more  and  more  nearly  approximating  to 

the  value  of  ^r  ^t   that  point.      An  instructive  example   is  the 

case  of  the  curve 

in    which   the  following   table  of   values  of   8x,    8//  and         can 

ox 

readily  be  obtained,  and  the  way  in   which    ;    approaches   its 

ox 

limiting  value  2  at  the  point  where  x  =  1  be  made  evident. 


6a;  jl 

"J 

•s 

■7 

■6 

•5 

•4    ,   -3   i   -2   ,   -1 

•09 

•o,s 

•07 

■06 

•00 

•04 

•03 

•02 

•01 

Sy  ,3 

2-61 

2-24 

1-S9 

1-56 

1-25 

•96 

•69     -44 

•21 

•1881 

•1664 

•1449 

•1236 

•1025 

•0816 

•0609 

•0404 

•0201 

Sx 

2-9 

2-S 

2-7 

2-6 

2-5 

2-4    2-3    2-2 

2^1 

2-09 

2-08 

2-07 

2-06 

2-05 

2-04 

2^03 

2^02 

2^01 

22 


THE  MEANING  OF  DIFFERENTIATION 


§  18.  In  the  chapters  which  immediately  follow  Ave  shall 
show  how  to  obtain  the  differential  coefficients  of  the  most 
important  functions.  This  process  of  obtaining  the  differential 
coefficient  is  called  differentiating  the  function.  We  shall  see 
that  in  very  many  cases  there  is  little  difficulty  in  differentia- 
tion, and  that  the  knowledge  of  the  differential  coefficients  is 
of  great  value  not  only  in  geometry,  but  in  the  application  of 

mathematics  to  physics. 

clv 
From   Fig.    7   it  is   obvious   that   when   -f-    is   positive    the 
^  ax 

tangent  is  inclined  at  an  acute  angle  to  the  axis  of  x,  and  y 


increases    there    with    an    increase    of   x,    or   decreases    with    a 

decrease   in   .'•.      When  -f-  is  negative,  the  tangent  is  inclined 

do'  ^ 

at   an    obtuse    angle  to   the   axis   of   x,   and   ?/   decreases    as  x 

fry 

increases,   or  vice  versa.     When   -^  =  0,  the  tangent  is  parallel 

to  this  axis.  Let  us  imagine  the  curve  ABC  to  be  a  road, 
and  that  a  traveller  is  marching  along  it  in  the  positive  direction 
of  the  axis  of  ,'•,  which  is  horizontal.     When  the  traveller  ascends. 


dy 


'('/ 


j^  is  positive ;   when   he  descends,   ~   is  negative ;  and  if  the 
road  is  properly  rounded  off  and  no  sharp  corners  occur,  when 


he    passes    from   ascending   to   descending,    or    the   reverse, 
changes  sign  by  passing  through  zero. 


dy 

dx 


THE  MEANING  OF  DIFFKEENTIATION  23 

The  acceleration  of  a  moA'ing  point  is  defined  in  Dynamics 

as  the  rate  of  change  of  its  velocity.     Therefore,  if  we  write 

V  for  the  velocity  at  time  t,  the  acceleration  at  that  instant  is 

dv 

-J-.-     If  the  position  of  the  point  at  time  /  is  given  by  5;  =f{t), 

ds 


then  the  velocity  v 
and  the  acceleration 


dt 

dc      d     /ds-^ 
dt^df'  [dt 


s  = 

^hgt 

ds 
dt~ 

--of, 

dh 
df-~ 

'9- 

The  differential   coefficient   of   the   differential   coefficient    is 

called  the  second  differential  coeflticient,  and  in  the  case  of  s  =f(f), 

dh 

is  Avritten  ^-7,. 

dt- 

E.a.  If 


and 


EXAMPLES   ON   CHAPTER   II 

The  differential  coefficients  required  in  the  examples  on  this  chapter  are 
to  be  obtained  from  the  deiinition. 

1.  Plot  the  curves  (i.)  y  =  x  +  x'^ 

(ii.)  y^x», 
and  show  that  they  have  the  same  gradient  when  x  =  l. 

2.  By  considering  the  area  of  a  square  and  the  volume  of  a  cube,  show 
that  the  differential  coefficients  of  x^  and  x^  are  2x  and  ^x^  respectively. 

3.  Show  that  the  curves  y  =  x^  and  y  =  x*  intersect  at  the  origin  and 
the  points  (1,  !)(-!,  1),  and  that  at  each  of  the  two  latter  points  the  angle 

o 
between  the  tangents  is  tan  ~  '^  -  • 

4.  Show  that  the  gradient  of  the  curve  y  =  x^-'ix  at  the  point  where 
x  =  2  is  9.     Find  the  equation  of  the  tangeut  there  and  trace  the  curve. 

5.  Find  where  the  ordinate  of  the  curve  i/  =  3a;-4a:^  increases  at  the  same 
rate  as  the  alascissa,  and  where  it  decreases  five  times  as  fast  as  the  abscissa 
increases. 

6.  U  s  =  ut-lgf,  fini^l  the  values  of  the  velocity  and  acceleration  at  the 
time  t. 

7.  A  cylinder  has  a  height  h  ins.  and  a  radius  r  ins.  ;  there  is  a  possible 
small  error  5?*  ins.  in  r.  Find  an  approximate  value  of  the  possible  error 
in  the  computed  volume. 


24  THE  MEANING  OF  DIFFERENTIATION 

8.  Find  apjiroximately  the  error  made  in  tlie  volume  of  a  sphere  by 
making  a  small  error  5?-  in  the  radius  r.  Tiie  radius  is  said  to  lie  20  ins.  ; 
give  approximate  vahies  of  the  errors  made  in  the  computed  surface  and 
volume  if  there  Ije  an  error  of  -1  in.  in  the  length  assigned  to  tiie  radius. 
Also  calculate  the  ratio  of  the  errors  in  the  radius,  the  surface,  aud  the  \-olume. 

9.  The  area  of  a  circular  plate  is  expanding  by  lieat.  When  tlie  radius 
passes  tlirough  the  value  2  ins.  it  is  increasing  at  the  rate  of  -01  in.  per  sec. 
Show  that  the  area  is  increasing  at  tlie  rate  of  •047r  sq.  in.  per  sec.  at  that 
time. 

10.  The  length  of  a  bar  at  temperature  0"  is  unity.  At  temperature  t°  its 
length  I  is  given  by  the  equation 

l  =  l+at  +  bt~, 

find  the  rate  at  which  the  bar  increases  in  length  at  temperature  f,  and  give 
an  approximation  to  the  increase  in  length  due  to  a  small  rise  in  temperature. 

11.  If  the  diameter  of  a  spherical  soap-bubble  increases  uniformly  at  the 
rate  of  "1  centimetre  per  second,  show  that  the  volume  is  increasing  at  the 
rate  of  -277  cub.  cent,  per  second  when  the  diameter  becomes  2  centimetres. 

12.  A  ladder  24  feet  long  is  leaning  against  a  vertical  wall.  The  foot  of 
the  ladder  is  moved  away  from  the  wall,  along  the  liorizontal  surface  of  the 
ground  aud  in  a  direction  at  right  angles  to  the  wall,  at  a  uniform  rate  of  1 
foot  per  second.  Find  the  rate  at  which  tlie  top  of  the  ladder  is  descending 
on  the  wall,  when  the  foot  is  12  feet  from  the  wall. 


CHAPTER    III 

DIFFERENTIATION    OF    ALGEBRAIC    FUNCTIONS;    AND    SOME 
GENERAL    THEOREMS    ON    DIFFERENTIATION 

,5^  19.   The  Differential  Coefficient  of  r". 

Let  ij  =  x": 

Then  //  +  5?/  =  (a;  +  Sx)"- 

Sx\  " 


=  a;"  ( 1 

dx 


+  — 

X 


8// 


X, 


8x  8x 

But  by  the  Binomial  Theorem,  when  h<\, 


Therefore 


(1   +/;.)»  =.1   +;,//+ ^^-1 /,2  +    .     .     . 
„/,        n  ^        71.72.  -  1  (&j)"-'  \ 

hy^_      \        X  1.2      ij;2  ) 

Sx  &r  ' 

Si/  ,      n.u  -  1         ,, 

.  ■ .     /^  nx"  - 1  +  -r--~  x>'  -  -8x  +  .  .  .  ■■•- 
8x  1.2 

The  fact  that  we  have  an  iiitinite  series  on  tlie  right  hand  sometimes  causes 
difficulty  to  the  student,  as  he  imagines  tliat  what  he  calls  the  summing  of  the 
infinite  number  of  small  terms  involving  8:c,  [dx)-,  etc.  .  .  .  may  give  rise  to  a 
finite  sum.  The  answer  to  tliis  difficulty  in  general  is  to  lie  fouml  in  a  true  view 
of  the  meaning  of  a  convergent  infinite  series,  l>ut  in  the  particular  case  of  the 
Binomial  Series  we  are  able  to  say  what  the  possible  error  by  stopping  after  a 

25 


26    DIFFERENTIATION  OF  ALGEBRAIC  FUNCTIONS 
provided  that  8x  is  so  small  that 

X 

Hence  Lk,=o(^^^  =nx''-\ 

and  the  differential  coefficient  of  x"  is  «x''~^ 

This  is  true  whatever  value  n  may  have,  provided  it  is  in- 
dependent of  X. 

Thus  ^('^)-A^S 


dx 

tx. 

dx  \x<J 

i 
X' 

2 

3  \/.7: 

§  20.  General  Theorems  on  Diflferentiation. 

Before  proceeding  to  obtain  the  differential  coefficients  of 
other  functions,  it  will  be  useful  to  show  that  many  complicated 
expressions  can  be  differentiated  by  means  of  this  result,  with 
the  help  of  the  following  general  theorems  : — 

Proposition  I.  Differentiation  of  a  Constant. 

It   is   clear   that,  '\i  y  -  a,  the  slope  of  the  line  is  zero,  and 

dv 

~  =  0.     In  other  Avords,  it  is  obvious  that  if  a  magnitude  remains 

the  same  its  rate  of  change  is  zero. 

Thus  the  differential  coefficient  of  a  constant  is  zero. 

Proposition  II.  Differentiation  of  the  Prodiict  of  a  Constant  and 
a  Function  of  x. 

Let  y  =  au,  where  (/  is  a  constant,  and  u  is  a  function  of  x. 

When  X  becomes  .'■  +  ax,  let  u  become  u  +  8u,  and  y  become 
y  +  8y. 

certain  inuuber  of  terms  can  be,  and  thus  exclude  the  infinite  series  from  onr 
argument. 

It  is,  liowever,  worthy  of  note  that  the  formula  for  the  differential  coefficient  of 
X"  can  be  obtained  without  this  series,  by  taking  first  of  all  n  a  positive  integer 
and  then  using  §  20  Prop.  VT. 


GENERAL  THEOEEMS  ON  DIFFERENTIATION     27 

Then  y  +  Sy  —  a{u  +  811), 

-  8y        8u 

and  ^  =  a— • 

8x        8x 

Therefore  Ltsx=o\j-,J  =  <^Ltsx=o  ( v-,  j , 

dy        du 
or  -f-  =  a-j-- 

dx        dx 

.'.  The  differential  coefficient  of  the  ^^Toduct  of  a  constant  and  a 
function  is  equal  to  the  product  of  the  constant  and  the  differential 
coefficient  of  the  function. 

The  geometrical  meaning  of  this  theorem  is  that  if  all  the 
ordinates  of  a  curve  are  increased  in  the  same  ratio,  the  slope  of 
the  curve  is  increased  in  the  same  ratio. 

Proposition  III.  Differentiation  of  a  Sura. 

Let  y  =  ";/  +  r. 

Then,  as  before,  y  +  8y  =  {u  +  8u)  +  (r  +  8v), 

8y  8u  8v 

8x  8.r  8x 
Proceeding  to  the  limit, 

dy  du  dr 

dx     dx     dx 

The  same  argument  applies  to  the  sum  (or  difference)  of 
several  functions,  and  we  see  that  the  differenticd  coefficient  of  such 
a  sum  is  the  sum  of  the  several  differential  coefficients. 

Ex.   Differentiate  the  following  functions  : — 

(i.)  x{2  +  ,-f 
(ii.)  {a  +  b.>:  +  cx-)\'x 
,...  ,  x^     .7'3     ,->;2     X     ,      \       \        1 

2  +  2x+Zx' 


(iv.) 


\x 


Proposition  IV.  Differentiation  of  the  Product  of  Tv:o  Fvnctions. 
Let  y  —  uv, 

Then,  as  before,  y  +  8y  =  {u  +  8u)(v  +  8v). 


28    DIFFERENTIATION  OF  ALGEBRAIC  FUNCTIONS 
Thus  hy  -  vSu  +  uSr  +  8u .  8v, 

■J  St/       8u        8v     „      8v 

and  ^i  =  v      +u■^  +  8^l.^■ 

bx        8x        bx  8x 

Proceeding  to  the  limit, 

dy        d'U         dv  _ 

dx       dx         dx ' 

since  as   8x  approaches   its   limiting  value   zero,   8u  approaches 

,  ,  8u   8v  -  du       ,  dv 

zero  also,  and  ^,  ^^^ become^-  and  -5-- 

bx    8x  dx  dx 

This  result  may  l^e  written 

1     dy     1     du     1      dv 

y     dx     u     dx     V     dx 

and  when  y  —  uvw,  we  Avould  obtain  in  the  same  Avay, 

1     dy     1      du     1     dv      1     dw 

~  ■  ^  =  - •  :r  +  ~  ■  T  +  -  ■  ^-     (Cf.  ^31.) 

y     dx     u     dx      V     dx     w     dx 

In  the  case  of  two  functions  it  is  easy  to  remember  that  the  differ- 
ential coefficient  of  the  product  of  ttvo  functions  is  equal  to  the  first 
function  x  the  differential  coefficient  of  the  second  +  the  second  function  x 
the  differential  coefficient  of  the  first. 

Ex.  Differentiate  the  following  functions  : — 

(i.)  (l+ic2)(2a;'-^-l) 
(ii.)  (2a;2+l)(a;  +  2)2 
(iii.)  iax  +  bf{cx  +  df- 
(iv.)  x{x  +  l){x  +  2), 

and  show  that  the  results  are  the  same  if   the  expressions    be   multiplied 
out  and  then  differentiated. 

Proposition  V.  Differentiation  of  a  Quotient. 
Let  y  =  ujv. 

u  +  8u 


Then  y  +  8y  = 


V  +  8v 


u.  +  8u     u      vSu  -  uSv 
and  ^^^v 


V  +  bo       V         ,  / ,        bV 
L-\\  + 
V  V 


GENERAL  THEOREMS  ON  DIFFERENTIATION     29 


8ii 

8r 

Therefore 

8>/  _ 
8x 

8x 

■!) 

Proceeding 

to  the 

limit, 

it  follows  that 

dm 

dv 

dy 

'%■ 

dX    .;, 

dx 

V^ 

In  words,  to  find  the  differential  coefficient  of  a  quotient,  froiu 
the  product  of  the  denomincdor  and  the  differential  coefficient  of  the 
numerator  subtract  the  product  of  the  numerator  and  the  differential 
coefficient  of  the  denominator,  and  divide  the  result  bi/  the  squa;re  of 
the  denominator. 

Ex.   Differentiate  the  following  expressions  :  — 

(i-)l^  (ii.)  ^^'^^^'^  (iii.)  "■ 


(a; +  3)  '     ''  (a;  +  l)(a;  +  2) 

These  five  formulae,  with  the  help  of  the  result  of  §  I'J. 
enable  us  to  differentiate  a  large  number  of  expressions,  but 
they  do  not  apply  directly  to  such  cases  as  Va  +  x,    s/a,'^  x^, 

1  1  ' 

ax  +  b   {ax  +  by 

Each  of  the  above  expressions  is  a  function  of  a  function  of 
X,  and  we  proceed  to  prove  the  general  theorem  :— 

Proposition  VI.  Differentiation  of  a  Function  of  a  Function. 
Let  //  =  F(m) 

where  u  =f{x) 

f'.g.  1/  =    \  u 

where    u  =  a~  +  x- 

Then  when  x  is  changed  to  ;/:  +  8x, 
let  u  become  n  +  8u, 

and  y  become  //  +  8y ; 

*  Tlii.s  result  may  be  obtained  by  writing 
and  then  differentiating  both  sides  of  this  equation. 


30    DIFFERENTIATION  OF  ALGEBRAIC  FUNCTIONS 

the  functions  being  such  that  for  a  small  change  in  r,  Ave  have  a 
definite  and  small  change  both  in  u  and  i/. 

-n,  j_  81/     8y     Su 

But  ^  =  ^  •  ^> 

dx     6u     8x 

.-.  proceeding  to  the  limit, 

Thus  djj^dy^(lu^ 

dx     du     dx 

Ex.   1.  When  y  =  ___^,,  we  may  put 

and  u  =  x  +  a) 


1^ 
dy     "\?i-/     du 


'<.i) 


,    —     ,        -    , -,  where  w  =  a;  +  a, 
dx       du        dx 


=  -4.1 


{x  +  af 


2.  When  2/  =  (a^  +  ^)",  prove --  =  ?ia(aa;  +  &)»-i. 

3.  When         ?y  =  (1  -  x)  \/r+^2 

g=(l-.)|(^/^^w^:^^(l-.). 

•D  4.  '^     /, .,     d\lu    du      ,  ^       ., 

but  -3-  rjl+x-  —  —, —  •  -;— ,  where  u  =  l+  x^, 

dx  du     dx 


=  (~^)i2x) 
V2\/l+a;V' 


>Jl+x^ 
di/  _  (1  -  x)x        . 

_     -Ix'-x+l 


.     ^,71.  /ax+b  dy  ad -be 

4.  When  y=  ^  ^^^,  prove  ^=2V(ax4-fc)(c..  +  rff 


GENERAL  THEOREMS  ON  DIFFERENTIATION     31 


EXAMPLES   ON   CHAPTER   III 


Find  V^  in  the  followinc'  cases  :- 
(Ix 


(i 


/=(,v'x-^'-)"  (vii.)^  =  , 


Cb  +  ft.!-'" 

(ii.)  2/=  n/2^^:^^^P  (viii-)  2/=(l+.r")' 


(iii. )  ?/  =  \/(.r  + 1  )(a'  +  2)  (ix. )  y  =  N-'x-^  +  a2  +  s V^  -  a'-^ 

(iv. )  y  =  {x  +  a)H,r.  +  by  (x. )  7/  =  -,-==  +     ,- :^ 

\'  X'  +  a-     \ix-  -  a'' 

/l+x  ,   .  .  a^ 

,   .  ,         {a-x)p  ,   ..  ,  /T+x  +  a? 

2.  Find  the  gradient  at  the  point  (./„,  2/„)  in  the  following  curves : — 

(i.)  y-  =  4ax 

(ii.)  x-  +  y'  =  a- 

(iii.)j±i:^i 

(iv.)        2j'2/  =  c-. 

3.  Prove  that  the  equations  of  the  tangents  at  {Xq,  */„)  to  these  curves  are 
respectively 

(i-)  2/2/0  =  2«(.''  +  a-o). 

(ii.)  xXn  +  yijn^aA 

,iu.,?±t=>. 

(iv.)  xy^  +  y.r^^c-. 

4.  A  boy  is  running  on  a  horizontal  plane  in  a  straight  line  towards  the 
base  of  a  tower  50  yards  high.  How  fast  is  he  approacliing  the  top,  when  he 
is  500  yards  from  the  foot,  and  he  is  running  at  8  miles  per  hour  ? 

5.  A  light  is  4  yards  above  and  directly  over  a  straight  horizontal  patli  on 
which  a  man  six  feet  high  is  walking,  at  a  sjieed  of  4  miles  per  hour,  away 
from  the  light. 

Find     (i.)  The  velocity  of  the  end  of  his  shadow  ; 

(ii.)  The  rate  at  which  his  shadow  is  increasing  in  length. 

6.  A  man  standing  on  a  wharf  is  drawing  in  the  painter  of  a  boat  at  the 
rate  of  4  feet  per  second.  If  his  hands  are  6  feet  above  the  bow  of  the  boat, 
prove  that  the  boat  is  moving  at  the  rate  of  5  feet  per  second  when  it  is  8 
feet  from  the  wharf. 

7.  A  vessel  is  anchored  in  10  fathoms  of  water,  and  the  cable  passes  over  a 
sheave  in  the  bowsprit  which  is  12  feet  above  the  water.  If  the  cable  is  hauled 
in  at  the  rate  of  1  foot  per  second,  prove  that  the  vessel  is  moving  through 
the  water  at  a  rate  of  1^  feet  per  second  when  there  are  20  fathoms  of  cable 
outt 


^tra: 


UNIVERSITY   ) 

OF 


32    DIFFEEENTIATION  OF  ALGEBRAIC  FUNCTIONvS 

8.  If  a  volume  r  of  a  gas,  contained  in  a  vessel  luitler  pressure jr;,  is  com- 
pressed or  expanded  without  loss  of  heat,  the  law  connecting  the  pressure  and 
volume  is  given  by  the  formula 

y^v''^  constant, 

where  7  is  a  constant. 

Find  the  rate  at  which  the  i)ressure  changes  with  the  volume. 

7  .2 

9.  In  Boyle's  Law.  where  iiv  —  c-,  show  that  -r-= — .,.     What  does  the 

'  dp        p' 

negative  sign  in  this  exjuession  mean  ? 

10.  In  van  der  Waals's  equation 

I  ;;+„](''  -  //)  — constant. 

Prove  that 

dv  _  {v  -  h) 


dp         (        a     2ab\ 


CHAPTEE   IV 

THE    DIFFERENTIATION    OF   THE    TRIGONOMETRIC    FUNCTIONS 

{The  angles  are  supposed  to  he  measured  in  Radians) 

§  21.  The  Differential  Coefficient  of  the  Sine. 

Let  y  =  sin  x. 

Then  y  +  %  =  sin  (.'■  +  6x), 

and  S'/  =  sill  (.'■  +  ?>:<■)  -  sin  x 

8x 


=  2  cos  ( ;r  +  —  )  sin 


/       8x 

8y  (       ^4^^ 

Therefore  &7.  =  ^°H''' "  o")  1  "l|r" 

Proceeding  to  the  limit,  and  remembering  that 
/sin  d' 


Lt.A-^    )  =  1,  it  follows  that 

dil 

-f  =  cos  .'•. 

(I.r 

K.li. — When  y  =  sin  iinx  +  u) 

dii      dii     da      . 

-^  -^  •  -T-  where  u  =  mx  +  v 

dx     dii     dx 

d(sm  u)     du 

d\L         dx 

-  cos  ?« .  m 

=  m  cos  {mx  +  ii). 

Ex.   Prove  from  the  detinitiou  of  —,  that  when  7/  =  sin  {mx  +  n), 

CLdb 

(III  ,  . 

-^=vi  COS  {m.y  +  n). 
ax 

4  33 


34  THE  DIFFERENTIATION  OF  THE 

§  22.  The  Differential  Coeflacient  of  the  Cosine. 

Let  y  =  cos  X. 

Then  y  +  %  =  cos  (;*•  +  8x) 

and  8y  =  cos  (.f  +  8x)  -  cos  x 

■     (        h\     .    & 
=  -  2  sin  \x.  +  -J  sm  -. 

i 

2 
Proceeding  to  the  limit, 

di/ 


,    =  -  sin  z. 

ax 


k 


N.B. — When  y  =  cos  {mx  +  n),     -y  -  -in  sin  (i/w;  +  n) 

Ex.  Prove  from  the  definition  of  -f-,  that  wlien  y  —  cos,  {iax+  it), 

-3-=  -msm  {mx  +  n). 

§  23.  The  Differential  Coefficient  of  the  Tangent. 

_  sin  z 

Let  y  =  tan  x  = 


cos  a:; 


c/(sni  x)       .      d(cos  x) 

n.,  7       cos  x  ^—^ sin  X — 

Then  dy  _  dx  dx 

dx 


cos'^x 

cos^^  +  sin^;i; 

cos^.?: 
1 

cos-:i; 

^z 

sec^x. 

N.B. — When  y  =  tan  (mx  +  n),     j-.  ="  ""^  sec-('mrc     /()• 

Ex.   Prove  from  tlie  definition  that  when  y  —  tAii  {mx  +  n), 

-rr-  -  111  sec-  iinx  +  n). 
ax 


TRIGONOMETRIC  FUNCTIONS  35 

From  these  three  results  it  is  easy  to  deduce  the  following : — 

— -  .  cot  .*■  =  -  cosec-.r  :  -r-  ■  cot  hm:  +  n)  =  -  m  cosec-(m.r  +  n) 
ax  ax 


I  sin  z      d  ,  ,  sin  {mx  +  n) 

sec  ;';  =  — 5-  ;  —  •  sec  \inx  +  n)  =  in 


dx  '       cos'' r '  (/.'■  '  co^\mx  +  n) 

d  cosx      d  .  .  cos  (mx  +  n) 

-r    •  COSeC  X= r-TT  ',    ^^  '  COSCC  (lltX  +  '11)-    -  111     .    ., ^. 

dx  sm^x'  dx  ^  '  sm-{mx+n) 

§  24.  Geometrical  Proofs  of  these  Theorems. 
All  these  cases  of  differentiation  may  be  discussed  geometri- 
cally.     The    method    will    be    followed 
easily   from   the    case    of    the  tangent, 
which  we  now  examine. 

Let  Z.MOP  be  the  angle  0  radians, 
and  let  OM  be  1  unit  in  length. 

Let  zlPOQ  be  86,  and  let  QPM  be 
perpendicular  to  the  line  OM  from 
which  6  is  measured. 

Let  PN  be  perpendicular  to  OQ. 
Then  8(tan  0)  =  PC^ 

=  PN  sec  ZINPQ 

=  PN  sec  {$  +  86) 

=  OP  sec  (6  +  86)  sin  86 

-  sec  6  sec  (6  +  86)  sin  86. 

rvv.  8{iiin6)  /n  ,  sa\/^^^\ 

Thus  ^-^ — ^  =  sec  ^  sec  (^  +  S^)f  — r^  j, 

and  proceeding  to  the  limit, 

c/(tau  6)  ,^, 

-d6      ='"''^- 

Examples.     Find  —-  in  the  following  cases  : — 

(i.)  y  =  2a  sin  {hx  +  c)  sin  [hx  -  c). 
(ii. )  y  =  X'  cos  2x. 
(iii. )  y  =  tan  3a;  +  cot  3a,'. 

, .    ,         sin  2x  -  sin  x 

(iv. )  y= • 

'^  cos  a; 

(v.)  y  =  x"^sm'^x. 

(vi.)  y  =  x"^  sin  7ix. 

(vii.)  ?/ =  sin-^  aj  COS' a'. 

(viii. )  y  =  sec-  {ax  +b)  +  cosec-  (ex  +  d). 


36  THE  DIFFERENTIATION  OF  THE 

§  25.   The  Inverse  Trigonometrical  Functions. 

Since  the  sine  of  an  angle  varies  continuously  from  -  1  to  +1 

as  the  angle  passes  from  -  -  through  zero  to  +  ^ ,  it  is  convenient 

to  take  the  inverse  sine  as  lying  in  these  two  quadrants.     In 
other  words,  for 

^  =  sin  "  ^,' 

we  take  that  part  of  the  curve 

sin  //  =  a',  ■ 

which  lies  between  //  =  -  -^  and  y  =  -^  -■ 

In  this  case,  when 

•      1  /     ^  ^\ 

?/  =  sm   \r  V     o^.'^<2/ 

sin  y  =  a; 

and  difterentiating,  ,-(sin  //)  =  -r  (■'')■ 

ax        '         (l.r 

„,        ,  (/(sin  y)     ihf      ^ 

Iherefore  ,   •^'  .-^=1 

ciy         ax 

or 

But 

and  therefore 

XT  ^ 

Hence  ^(om    .. ,  -  , — 

do->  '        +    v'l  -,r- 

§  26.   The  DiflFerentiation  of  the  Inverse  Cosine. 

In  the  case  of  //  =  cos~\'-, 

it  is  convenient  to  take  //  as  lying  between  <»  and  tt,  and  in  this 
case  the  equation 


cos  ;//   • 

(l.r 

C0S;^  = 

+   ^'l 

-  .'■-,  since  - 

n                    TT 

dy 

1 

dx  " 

+  x/r 

-  x'^ 

,-r,A  - 

1 

on  difterentiation,  gives 


d  dy 

^{cosy)  .  ^  =  1, 

di/  d.i 


TRIGONOMETRIC  FUNCTIONS  3  7 

d;, 

(0  <//<-) 


or, 

-  sin 

d.r 

and  since 

sin  //  =  + 

s'l-x' 

di^  _ 

1 

dx 

x/1-7^' 

or 

J-(cos-V)=  - 

1 

/i         To 

This  result  may  obviously  be  derived  from  that  for  sin"^r, 

since  sin"^,*:  +  cos~^,''  = -• 

2 

^'21.  The  DiflFerentiation  of  the  Inverse  Tangent. 

In  the  case  of  the  inverse  tangent  we  get  a  complete  set  of 

values  by  taking  //  in  the  interval   -  ~  to  +  -• 

When  //  =  tan  "  ^x 

tan  //  =  ,'■, 
and  differentiating, 

(/(tan  ij)      d// 
dji  dx       ' 

or  sec-//  •    ,-  =  1. 

dx 

Hence  (tan~^.r)  = 


dx  1  +  .''- 

If  the  student  Avill  examine  the  graphs  of  the  functions 
sin-^r,  cos  "I'',  etc.,  he  will  see  that  without  the  above  restrictions 
on  the  size  of  the  angle  there  would  be  an  ambiguity  in  the 
results  for  the  sine,  cosine,  secant,  and  cosecant.  For  a  given 
value  of  .r,  Avithin  the  possible  range  of  values  for  .'■,  Ave  have  an 
infinite  number  of  values  of  //,  and  at  these  points  on  the  curve 
the  gradients  are  equal  in  magnitude,  but  may  be  opposite  in  sign. 

Ex.   Write  down  the  values  of    ■    in  the  following  cases  : — 

dx 


(i.)  2/  =  sin-M -j+cos-'(^j.  (iv.)  y=tan-i(^j— ; 

(ii.)  y  —  s,m.-'^{\-x).  (v.)  y  =  x^fim-'^{\>r). 

(iii.)  ?/  =  cos-M    — '^,\.  (vi.)  ;/  =  tan-H''''')- 


38  THE  DIFFERENTIATION  OF  THE 

EXAMPLES  ON  CHAPTER  IV 

1.  Differentiate  the  following  functions  : — 

(i.)  sin-'x  +  cos'',''. 

(ii. )  tan  ;>•  +  -  tan"  ,vj. 
o 

(iii.)  sec- a;  +  tan- :)'. 

(iv.  cosec-  X  +  cot-  o: 

1  +  sin  X 


(v.) 


VI. 


1  -  sin  X 

1  -  cos  X 
1  +  cos  X 


,    Ti-  sm  a  dii     cos^  a;  -  sm"  a; 

2.   It  */  =  :, — ,  prove  that  -r-  =  , . -„. 

1  +  tan  X  ^  ax     (cos  x  +  sm  xy 

S.   If  ?/  =  cos  (.'-■'),  prove  that  ~=  -  3x-  sin  (a/),  and  find  ^  when 

ax  ^  ax 

(i.)  2/=a;™sina-". 

(ii.)  y  =  x''"'Cosx". 

(iii.)  2/  =  a:™ tana". 

4^.   Differentiate  the  following  functions  : — 

(i.)  (a!2  +  l)  tan-la; -a;, 
(ii. )  X  .sin-i  x  +  \/T^^. 

(iii.)  tan-'(  ^''"'"^  )     .         .     (Put  \'.r=  tan  0,    v'«  =  taiia.) 
(iv. )  tan-'' 


^-X-rX' 
(V.) 


cot-i(l±yLL^)        .         .     (Put  a- =  tan  e.) 


5.  A  particle  P  is  revolving  with  constant  angular  velocity  w  in  a  circle  of 
radius  a.  The  line  PM  is  drawn  from  P  perpendicular  to  the  line  from  the 
centre  to  the  initial  position  of  the  particle.  Find  tlie  velocity  and  accelera- 
tion of  M. 

6.  If  the  position  of  a  point  is  given  at  time  t  by  the  equations 

a;  =  a(ct;^  +  sin  w<), 
y  =  a{l  -  cos  ut), 

where  a  and  w  are  constants,  find  its  component  velocities  and  accelerations, 
and  its  direction  of  motion  at  the  time  t. 

7.  Prove  that  when 

ax  3.  y/,,.^  _  I 

and  that  when 

^  1     ^  /        1    ^  1 


dx  xsix^-l' 

and  illustrate  your  results  from  tlie  graph  of  the  inverse  secant. 


TRIGONOMETRIC  FUNCTIONS  39 

8.  Prove  that  when 

^>'^r  ^^  (cosec-'  X) :- 


die  xfja^  —  l' 

and  that  when 

a;<  -  1,  -y-  (cosec"'  x)— 


dx  ■       .vsV-i' 

and  illustrate  your  results  from  the  graph  of  the  inverse  cosecant. 


CHAPTEE    V 

THE    EXPONENTIAL   AND    LOGARITHMIC    FUNCTIONS — PARTIAL 
DIFFERENTIAL    COEFFICIENTS — DIFFERENTIALS 

§  28.  In  this  chapter  we  assume  a  knowledge  of  the  properties 
of  the  following  series  : — 

e«  =  1  +  .!•  +  — -  +    ... 

A, 

a*  =  1  +  ,'■  log  «  +  1^  (log  of  +    .  .  . 

which  hold  for  all  values  of  .'■,  and 

fi     .7-3 
log(l+.0  =  :i--^  +--    .   .   . 

which  holds  Avhen   -  1<.'<  +  1,  using  "log  .':"  for  "logg.''." 

We  shall  now  show  how  to  differentiate  e^,  «^,  log  ;'',  and  other 
functions  whose  differential  coefficients  may  thus  be  obtained. 


§29. 

To  differentiate  e*. 

Let 

])  =  e""- 

Then 

y  +  8y  =  e^+^^, 

.-.     Sij  =  e''+^' -(.'■'' , 

=  e'(e^^-  1), 

J,      8x     (SxY 

5y     w,    «■>;    (&)- 


40 


EXPONENTIAL  AND  LOGARITHMIC  FUNCTIONS    41 
Proceeding  to  the  limit, 


dy 
dx 

d^. 

Thus 

i'-) 

=  e^. 

It  follows 

that  the 

equation 

dy  _ 

ilx 

■-y 

is  satisfied  by  //  =  ce^,  where  c  is  any  quantity  independent  of  x. 
p]x.   1.   If  v/  =  «e''-^,  prove  that '-^  =  />//. 
■2.   It  u-e'-,  prove  that  j-^=-2,nj. 

3.  Uy  =  .t-e*'",  prove  tliat  .'■  y-(  =  ( 1  4- 2.>-)?/. 

4.  Prove, /ro7«  the  definition  of  the  differential  coefficient,  that  if  \j  —  ae^'^, 


aa; 

I  30. 

To  differentiate  log  '. 

Let 

y  =  log  ,'■. 

Then 

y  +  8y  =  log  (x  +  dx), 

and 

Sy  =  log  (x  +  d/;)  -  log  .'■, 

=  7-2(7)  ^aU  -■  • 

•      ^K?)<^- 

6//_  1        1   /6x\        1    /6,r 


Proceeding  to  the  limit, 

dy^l 
dx     X 


Ex.  1.   If?/  =  «^,  log  v/ =  .f  log  «.     Hence  show  that 

(fa ' 


—  {a^)  =  a^Aogea. 


2.  It  2/  =  log„  .1;  prove  that  -^  =  — =^^  =  — , 

d'-        ,'•        .'■ .  log,,  a 

3.  If  2/  =  log  («.  +  &),  prove  that  1=^^. 


42    EXPONENTIAL  AND  LOGARITHMIC  FUNCTIONS 

4.  Prove  the  result  of  (3)  from  the  definition  of  the  differential  coefficient. 

5.  If  ^  =  log   -y ,  prove  that  -r  =  ^^— w,    — ^• 

\o-  X )    ^  rlx     [a  -  X)  {b  -  x) 

6.  If  7/  =  log  {x+  ^x~±a-),  prove  that  -j-  =  — = . 

^    tj.        ,  ta-b  cos  Q  , ,    ^  dy         ab  sin  6 

I.   If  w  =  lo£f  .  /  5 T  ,  prove  that --^  =   „     ,„       „„■ 

^        ^  V  a  +  b cose'  '■  dd     a^-b- cos^ 6 

v^  31.   Logarithmic  Differentiation. 

We  have  already  obtained  a  general  rule  for  the  differentia- 
tion of  a  product  or  quotient.  We  are  now  able  to  prove 
another  method  which  often  leads  more  quickly  to  the  result. 
This  method  is  called  Loi/arifhmk  Differenfidfion. 

Let  y/=  nnc. 

Then  log  y  -  log  n  +  log  r  +  log  tr, 

d  ,-        ,      dy      d   ,.        .      du      d  ,.        ,      dv 

d  dw 

d2o  dx' 

1  dy      1      du      1  dv  1  die 

y  dx     u     dx     V  dx  w  dx 
In  other  words,  before  differentiation  of  an  exjjression  involving  the 

irrodud  or  quotient  or  poioers  of  other  expressions,  take  logarithms  of 
both  sides  of  the  given  equation. 

T-       -,     1,-        {ax+bY{cx  +  dy'     1     dy        an  qr  se 

Ex.    1.    It  //  =  '  -       ■     •  -       '       '      ^ 


{ex+fY  y     dx    ax  +  b     cx  +  d     cx-\-f 

2x 


2    If,,-    ./^±^    ^-    / 

^-   112/-  V  i_^,...  ,fo.- ^/(l+:^^2)(l_^2)a- 
^      _        /(i.  +  2bx  +  cx'^    ^^y  _  b{a-cx') 
V    (I  -  'Ibx  +  ex-     dx     (a  - 


{a  -  2bx  +  ca;2)»(a  +  2bx  +  cx'')i 


S  32.  Important  Example. 

If  y  =  c-' "■'  sin  hx, 


dv       ■     ■,     d   ,     ^  .  „>.     ^  /  •     7  X 

-f-  =  sni  bx  -r  (e~'^^)  +  e~""^  ■  -y-  (sin  bo-) 
dx  dx  dx  ' 

=  e ""•'"(-  a  .sin  bx  +  b  cos  bx). 


PARTIAL  DIFFERENTIAL  COEFFICIENTS  43 

NoAv  if  a  =  tan ~^{^),  o.  and  b  being  positive, 


a 

cos  a  = 


Sin  a  = 


b 


/7y/  

and  -r-  =  -   x^ft"-^  +  b- .  e~^^  (sin  fo  cos  a  -  cos  bx  .  sin  a), 


=  -   v^'?'  +  b-  .  e'"-^  sin  (fe  -  a). 

Thus  the  tangent  to  y  =  r-""^  sin  fo' is  parallel  to  the  axis  of  x 

when  bx  =  n-n-  +  a, 

and  the  equation  defines  an  oscillating  curve  with  continually 
diminishing  amplitude  in  the  waves  as  we  proceed  along  Ox. 
It  is  easy  to  show  that  when 

y  -  gaX  gj,;^   Qjj.  _L   ,.^^ 

-1  =  v/o^T-  f"^  sin  (bx  +  c  +  a), 
ax 

and    that    here   the  waves  increase    in    amplitude ;    and   corre- 
sponding results  hold  for  the  case  of  the  cosine. 

v?  33.  Maxima  and  Minima  Values  of  a  Function  of  one 
Variable. 

The  student  is  already  familiar  with  the  graphical  and 
aloebraical  discussion  of  the  maxima  and  minima  of  certain 
simple  algebraical  expressions.  The  methods  of  the  Differential 
Calculus  are  well  adapted  to  the  solution  of  such  problems, 
since,  if  the  graph  of  the  function  is  supposed  drawn,  the 
turning -points,  or  places  where  the  ordinate  changes  from 
increasing  to  decreasing,  or  vice  versa,  can  only  occur  where 
the  tangent  is  parallel  to  the  axis  of  x,  as  in  the  points 
Ap  A2  .  .  .  of  Fig  9,  or  where  it  is  parallel  to  the  axis  of  y  as 
in  the  points  B^,  B.,  .  .  .,  except  in  such  cases  as  the  points 
Cp  C.3  .  .  .,  where,  although  the  curve  is  continuous,  the  gradient 


44    EXPONENTIAL  AND  LOGAEITHMIC  FUNCTIONS 

suddenly  changes  sign,  without  passing  through  the  value  zero 
or  becoming  infinitely  great. 

In  case  (A) :    .    is  zero  at  the  turning-point;  and  if  this  point 

is  one  at  Avhich  the  curve  ceases  to  ascend  and  begins  to  descend, 


dy 


dx 


-  changes  from  being  positive  just  before  that  point  to  being 


Fici.  9. 


negative  just  after.  At  such  a  point  the  function  is  said  to 
have  a  maximum  value.      In   the  other  case,  where    the    curve 

ceases  to  descend  and  begins  to  ascend,  y-  changes  from  nega- 
tive to  positive,  and  we  have  a  minimum.  In  Fig.  9,  at  A^ 
there  is  a  inaximnm ;  at  A.,  there  is  a  minimum. 

In  case  B  :   -r_  is,  infinitely  great  at  the  turning-point,  and 

ftJy 

at  Bj,  where  there  is  a  viaxim,um,  it  changes  from  positive  to 
negative,  while  at  Bo,  where  there  is  a  minimum,  it  changes  from 
negative  to  positive. 

The  other  turning-points  Cj,  C^  in  Fig.  9  correspond  to  dis- 


PARTIAL  DIFFERENTIAL  COEFFICIENTS  45 

continuities    in   ~,   but  it  can  be  shown  that   these   will   not 

a,r. 

occur  in  the  functions  with  which  we  are  dealing. 
.^34.  Points  of  Inflection. 

Althoue;h  the  vanishini*;  of   ^  is  a  necessari/  condition  for  a 

'^^  '^        dx 

maximum  or  minimum,  it  is  not  a  sufficient  condition,  since 
the  gradient  of  the  curve  may  become  zero  Avithout  changing 
its  sign  as  we  pass  through  that  point.  Examples  of  such 
points  are  to  be  found  in  Dj,  D.^  of  Fig.  9.  In  the  case  of  I)^ 
the  gradient  is  positive  before  and  after  the  zero  A^alue ;  in  the 
case  of  D^  it  is  negative.  At  these  points  the  curve  crosses  its 
tangent,  and  when  this  occurs,  whethei'  the  tangent  is  horizontal 
or  not,  the  point  is  called  a  point  of  inflection. 

We  cannot  here  discuss  the  analytical  conditions  for  such  a 
point  in  general ;  but  in  the  cases  of  horizontal  tangent  (case  D) 

we  see  that  -—  vanishes  and  does  not  change  sign  ;  and  in  the  case 


if, 


of  vertical  tangent  (case  E),  y^  is  infinitely  great  at  the  point, 
and  does  not  change  sign  as  we  pass  through  it. 

Ex.  1.  Show  that  ij  =  a.i'-  +  2h.i'  +  c  has  always  one  turning-point;  and 
point  out  when  it  is  a  maximum  and  when  it  is  a  uiinimuni. 

2.  Find  the  maximum  and  nunimum  ordinates  of  tlie  curve //  =  ;r^  -  6.'''-+  12, 
and  also  find  the  points  of  maximum  gradient. 

3.  Find  the  turning-points  of  the  curve  1/ =(;>• +  !)■'(,'•- 2 j'',  and  show  that 
(  -  1,  0)  is  a  point  of  inflection. 

(,v-l) 

4.  Find  the  turning-points  ot  y  =  -rr, — ^/ 

§  35.  Partial  Differentiation. 

So  far  we  have  been  considering  functions  of  only  one 
independent  variable,  y  =/(•').  Cases  occur  in  Geometry  and 
in  all  the  applications  of  the  Calculus  where  the  quantities 
which  vary  depend  upon  more  than  one  variable.  For  instance, 
in  (xeometry  the  co-ordinates  of  any  point  (.r,  ?/,  :■)  upon  the 
sphere  of  radius  a,   whose  centre  is   at   the   origin,  satisfy   the 

relation  .'■-  -f  //-  -f  :-  =  a'. 

Hence  we  have  z'  =  a-  -  .'-  -  //"-, 


46    EXPONENTIAL  AND  LOGARITHMIC  FUNCTIONS 

and  if  we  cut  the  sphere  by  a  plane  parallel  to  the  //:  plane, 
along  the  circle  where  this  plane  cuts  the  sphere  x  is  constant 
and  the  change  in  z  is  due  to  a  change  in  //  only.  In  the 
section  by  a  plane  parallel  to  the  zx  jDlane,  the  change  in  z 
would  be  due  to  a  change  in  .';  only.  Similar  results  hold  for 
other  surfaces. 

Again,  the  area  of  a  rectangle  whose  sides  are  x  in.  and  //  in. 
is  xji  sq.  in.,  and  we  may  imagine  the  sides  x  and  y  to  change  in 
length  independently  of  each  other ;  while  the  volume  of  a 
rectangular  box  whose  edges  are  x,  y,  and  ,:;  in.  is  o-yz  cub.  in., 
and  x,  y,  z  may  be  supposed  to  change  here  independently. 

The  ordinary  gas  equation 

pv 

jt;^  =  constant 

is  another  example  of  the  same  sort  of  relation,  and  it  would 
be  easy  to  multiply  these  instances  indefinitely. 

§  36.  Let  the  equation 

express  such  a  relation  between  two  independent  variables  .'•  and 
v/,  and  a  dependent  variable  „. 

Let  us  suppose  that  the  independent  variable  y  is  kept 
constant,  and  that  ./■  changes. 

Then  the  rate  at  which  z  changes  with  regard  to  ,/•,  when  // 
is  kept  constant,  will  be  given  by 


(f(x  +  8x,y)-f(x,y)] 


In  the  second  case  let  ;/;  be  kept  constant  and  let  //  change. 
Then  the  rate  at  which  z  changes  in  this  case  is 

^fh  =  Oy  ^^  }■ 

These    two    differential    coefficients    are    called    the    Partial 

Differential  Coefficients  of  ~;  with  regard  to  x  and  y  respectively, 

7)~  Pi 

and  are  written  ^  and  ^  respectively.* 

ox         dy 

'> 

cz 
*  It  is  hardly  necessary  to  point  that  this  symbol  5—  stands  for  an  operation, 

and  that  ds,  dj/  are  not  to  lie  considered  separately  ;  also  that  this  is  a  different 
notation  from  the  d.c  of  our  earlier  work. 


PARTIAL  DIFFERENTIAL  COEFFICIENTS  47 

Oz  oz 

Ex.  1.  When  z  =  .a/,  prove  from  the  definition  that  ^  =  v,  and  t^^  —  x. 
'  oa;  dy 

2.  When  2as  =  a;-  +  y-,  i)rove  from  the  definition  that  ^^  =  -,  and  7^^  = ' . 

3.  If  ii  —  jnjz,  prove  from  the  definition  that— =  ?/c. 

§  37.  Total  Differentiation. 

When  the  variables  x  and  //  in  the  above  examples  Ijoth 
depend  upon  a  third  variable  t,  say, ,::  will  vary  in  value  as  ,/•  and 
//  change  with  t. 

In  the  case  z  =  xy 

z  +  Si'  =  (,/•  +  8./:)(v/  +  8//) 
and  ^z        8x        8//     8x 

8t^^^  ¥"-■'¥  "-81  ■"' 

so  that,  proceeding  to  the  limit, 

dz        dx        dii 
dt     '  dt        dt 

But  dz         ,  dz       , 

y  =  7r   and  X  ~    ~    when  ~  =  xy, 

therefore,  in  this  case 

(h     dz     dx     dz     dy 
7t~  dj-'  dt^dji  '  Tif  ' 

In  the  second  example, 

2az  =  X-  +  ,//-, 


we  find 

2a&  =  %i'8x  +  ■2y8ij  +  {8xf  4 

and 

dz      '  dx        dy 
''dt=-'dJ'-^df- 

so  that  again 

dz     dz      dx     dz      dy 
di~di.'  dt^  dii'  dt 

It  can  be  shown  that  this  holds  in  genei^al,  but  the  proof  of  the 
theorem  cannot  be  taken  at  this  stage  of  our  work. 

The  differential  coefficient   ,^  is  called  the  Total  Differential 

dt 

Coefficient  in  such  cases,  as  compared  with  the  Partial  Differen- 
tial Coefficient  defined  above. 


48    EXPONENTIAL  AND  LOGARITHMIC  FUNCTIONS 

As  a  special  case,  when  z  =/('■,  y)  and  v/  is  a  function  of  ,'■,  we 
obtain 


dz     dz     dz  cly 
d.r     dx     dy  dx 


and  the  left-hand  side  is  called  the  Total  Differential  Coefficient 
of  z  with  regard  to  x. 

Also  the  result  that  when  z  =f(x,  y)  and  ,'-,  y  are  functions  of  t, 

dz     dz     dx     d:  dy 
df  ~  dx     df  "^  dy  dt 

may  be  used  to  obtain  an  approximation  to  the  small  change  6~ 
in  z  due  to  the  small  changes  8x  and  ?>y  in  ,'■  and  //,  when  t 
becomes  t  +  8f. 

For,  as  we  have  seen  already  (p.  19), 

dx 

di 

dy 

Jt 

dz 

dt 
and  we  thus  have,  on  multiplying  the  above  equation  by  M, 


8x  will  be  approximately 

8z 


8t, 

Si, 
8t 


8z  =  ^-  8x  +  ^^  ■  8//. 


dx 


38.  Differentials.* 


r)y 

In  the  case  of  the  curve 
y=f{x)  the  increment  8y  of  y 
which  corresponds  to  the  in- 
crement 8x  of  .'■  is  given  in 
Fig.  10  by  HQ. 

Also 

HQ  =  HT  -f  TQ  =  8x  ■  '^  +  TQ, 


(IX 


.  • .   8/1  =  8x 


dy 
dx 


TQ. 


M 
Fk;.  in 


N 


As  8x  ffets  smaller  and 
smaller,  TQ  gets  smaller  and 
smaller,  at  least  in  the  neigh- 

*  §  38  may  be  omitted  on  first  iviidiiig. 


PARTIAL  DIFFERENTIAL  COEFFICIENTS  49 

boiirhood  of  P ;  and  the  "  small  quantity "  TQ  is  a  smallei- 
"  small  quantity  "  than  S.i;  since 

Sy  _  dy     T(^) 

1  .      1     ,.    .    S'/  .  ,        (hi  ,       TU  .. 

and  ni  the  limit  —  is  equal  to   ,,  so  that    —  must  disappear  in 

&r  ^  (It  Ac  ^^ 

the  limit.  In  mathematical  language,  if  8x  is  an  infinitesimal  (or 
small  quantity)  of  the  first  order,  TQ  will  be  at  least  an  infini- 
tesimal of  the  second  order. 

It  is  convenient  to  ha^e  a  name  and  syml;»ol  for  this  quantity 
dy 

tr 

symbol  is  "  dy." 

Hence  with  this  dehnition  of  the  term  "  differential," 


Y  ■  Sx.     The  name  adopted  is  the  "differential  of  y,"  and  the 


where  we  have  enclosed  ~  in  l)rackets  on  the  right-hand  side 

d.r 

SO   that  it   may   Ite   clear   that  this   stands  for  the   differential 
coefhcient  ol)tained  by  the  processes  we  have  been  developing 
in  the  preceding  pages. 
By  the  above  definition 

'^(/(■'■))=/V)-S-',  where  ,/>)  =  ':^^ 

and  dx  =  8x. 

So  that  dy  =/'(•'■)  •  '^'''i  when  //  =/(■'■)• 

Hence  we  may  restate  our  definition  as  follows  : — 

The  differential  of  fhe  independent  variable  is  the  actual  increment 

of  th(d  variable. 

The  differenticd  of  a  function   i>>  the  differential  coefficient  of  tlic 

function  multiplied  by  the  differential  of  the  independent  variable. 

In    this   definition   it  is   not   necessary  to   assume   that   the 

differentials  are  small  quantities  or  infinitesimals,  but  in  all  the 

applications  of  this  notation  this  assumption  is  made.      In  that 

case  the  equation 

dy=f'{x)dx 

5 


50    EXPONENTIAL  AND  LOGAKITHMIC  FUNCTIONS 

will  give  the  increment  of  y,  if  small  quantities  of  the  second 
order  be  neglected. 
Such  an  equation  as 

dy  =f{x)cb; 

a  differential  equation  as  it  is  called,  may  be  used  in  this 
way  to  give  the  approximate  change  in  the  dependent  variable, 
and  from  this  point  of  view  it  saves  the  trouble  of  writing  down 
the  equation  between  the  increments,  and  then  cutting  out  the 
terms  whose  smallness  is  such  that  they  may  be  neglected. 

Ex.  1.   Write  down  a  table  of  differeutials  corresponding  to  the  standard 

differential  coefficients. 

e.g.  d{x")  =  )i:e"-''dx. 

du 
2.  If  a,'  =  a  cos  6,  y  =  a  sin  6,  prove  by  differentials  that  -^=  -  cot  0. 

.->    Tf  I   X      ■       ^s  /I  ^\  ii    i  dy       sin  ojt 

6.   It  x  =  a[M  +  sixi  ut),  t/  =  a[l  -cos  wt),  prove  that  -f-  =  ] 


dx     1  +  cos  ut 

4.   If  ~  =  xij,  prove  that  dz  —  ~dx  +  ~  dy. 

cx        cy 


EXAMPLES  ON  CHAPTER  V 

1.  Find  the  differential  coefficients  of 

(i.).™-^,    (ii. )  a;'»e»^,    (iii.)  (aa;-  +  6)c''^+'',    (iv.)  c^«"~^^. 

2.  Find  the  differential  coefficients  of 

(i.)ci+-^",    (ii.)  a-V^",    (iii.)  ./-'"C"",    (iv.)  .f'"a^". 

3.  Find  the  differential  coefficients  of 

{\.)x-nogx,   (ii.)log(^'^^),   (iii.)log(v'.^^+V-^l),   (iv.)  log  (^^^j, 

4.  Differentiate  the  following  expressions  logarithmically  : — 

(i.)  n/(2.^  +  1)(,«-2),    (ii.)  v^+^.'    (iii-)  ^2(^)3.   (iv.)^-, 

^    '  cos'^wa;'  '  \       x) 

and   point  out  why  we  cannot  apply  our  formula  for  the  differential  co- 
efficient of  a;"  to  the  case  of  ,r^. 

1  f    ax  +  b   \  .,    ,  di/  1  ,        ,„ , 

5.  I{v=    I tan~M      , ,  prove  that  ~= — 5 — --, (acyb^.) 

.    ,,        1  ,      {x  +  lf       1     ^       ,  /2,c-l\  ^,    ^dy        1 


PARTIAL  DIFFERENTIAL  COEFFICIENTS  51 

7.  If  2/  =  2  cos-i  V  ^^,  pi-ove  that  ^=  ^^ ^     _        .  (a  >  a-  >  ^.) 

8.  If  2/  =     ,1_  cos-J  ^  Z''  r_^',  prove  that  5^= ^=^  .    (cc  <  a  <  ,S.) 

^    T„        ,       /b  +  atiosx+  sjb-  -  ofi  sin  x\  ^i    ^dy       Jb'^  -  a^ 

9.  If  w  =  log  ( T ,  prove  that  ^  =  -—^ . 

\  a  +  beosx  J  ax    a  +  b  cos  x 

10.  it  /  -— — -==  tan-i{  A  /  ,  tan  -  ,-,  prove  that  -ts  =  — -, -.  • 

sja- -b-  l^    a  +  b         2 J  ^  dd     a+b  cos  d 

{a^>b-\) 

11.  Ill  the  curves  whose  equations  in  polar  co-ordinates  are  (i.)  )-  =  ae9cota, 
(ii.)  r"-a"  sin  nd,  (iii.)  r"  =  a"  cos  n6,   (iv.)  ?•"  =  ««  sec  7id,  (v.)  r"  =  «"  cosec«^, 

find  r-T-  •     Can  you  give  any  geometrical  meaning  to  this  expression  ? 

12.  If  2/  =  e-'-^sin(2.r+l),  prove  that  -^  =  2  ^''2  •  e-^-^  cos  (2./-+1 -f  ^). 

13.  Find  the  value  of  V   in  the  following  curves  ;  discuss  the  way  in  which 

dx 

it  changes  as  x  passes  along  the  axis  ;  and  find  the  turning-points,  if  there 
are  any,  of  each  curve  ; — 

{i.)y  =  x(x-lf. 

(n.)y  =  x'{x-lf. 

{m.)y  =  (x-mx-2r. 

,.     ,        x^+x+\ 
■      (IV.)  y=  — 

,    ,        x~-x  +  \ 

(vi.),  =  (--l)(--2) 
(vii.)  ?/  = 
(viii.)  y  = 

(^^■•)^=       (x-4) 
.     .         ^,?  +  \ 

[These  curves  are  discussed  algebraically  and  drawn  to  scale  in  Chrystal's 
Jntroduction  to  Algebra,  pp.  391-404.  The  student  is  recommended  to  com- 
pare his  results  with  those  to  be  deduced  from  these  figures.] 

14.  It  c  =  — , -f  ^„  prove  that x  —  +  y^=  2z. 

a-     b~  '■  ex     •"  cy 


■X- 

''  +  x  +  -i 

x- 

'  +  X+1 

{X- 

-1){X- 

2) 

{X- 

-1)(^'- 

3) 

{X- 

-2){x- 

4) 

{X- 

-l){x- 

2) 

lo.   It  i  =  tan~M  -,,—  -„  I,  prove  that  X7^+  y  ^r-  =  0, 

\x-  +  y-J   ^  ox     ''  dy 


52    EXPONENTIAL  AND  LOGARITHMIC  FUNCTIONS 

16.  The  formula  for  the  index  of  refraction  //  of  a  j^as  at  temperature  6" 

and  pressure  ?.  is  ^_i=^._^_, 

where  /Xp^^the  index  of  refraetion  at  O'^, 

a^the  coefficient  of  expansion  of  the  gas. 
Prove  tliat  the  etl'ect  of  small  variations  5^  and  bp  of  the  temperature  and 
pressure  on  the  index  of  refraction  is  to  cause  it  to  varj^  by  an  amount 


-    _  /X||  -  1  /     bp  paSe    \ 

"'^^  760^  U  +  a^     (14  ai9)-/" 


(l4a(?)- 

17.  U  pv='\id  is  the  ordinary  gas  equation,  where  d  =  l  +  al,  writedown 
the  values  of 

.  vv 

...  ,  dp 
(n.).|' 

(iii.)  The  approximate  increase  in  the  pressure  due  to  a  small  decrease  in 
the  volume,  the  temperature  being  unchanged, 

(iv.)  The  ap[)roximate  increase  in  the  volume  due  to  a  small  increase  in 
the  tem])erature,  the  pressure  remaining  the  same, 

(v.)  The  approximate  increase  in  the  pressure  due  to  a  small  increase  in 
both  temperature  and  volume. 

18.  Assuming  that  the  H.P.  required  to  pro}icI  a  steamer  of  a  given  design 
varies  as  the  square  of  the  length  and  the  cube  of  the  speed,  prove  that  a  '2% 
increase  in  length,  with  a  7%  increase  in  H.P.,  will  result  in  a  1%  increase 
in  speed. 

19.  The  area  of  a  triangle  is  calculated  from  measurements  of  two  sides  and 
their  included  angle.  Determine  the  error  in  the  area  arising  from  small 
errors  in  these  measurements. 

20.  Assuming  that  the  area  of  an  ellijise  whose  semiaxes  are  o  and  b  inches 
is  wah  sq.  in.,  and  that  an  elliptical  metal  plate  is  exj)anded  by  heat  or 
pressure,  so  that  when  tlie  semiaxes  are  4  and  6  inches,  each  is  increasing  at 
the  rate  "1  in.  per  .second,  prove  that  the  area  of  the  plate  is  increasing  at  the 
rate  of  tt  .s(|.  in.  pei'  second. 


CHAPTER    VI 


THE    CONIC    SECTIONS  "-'' 


i^  39.  Ill  this  chapter  we  shall  very  briefly  examine  the  pro- 
perties of  the  Conic  Sections,  or  the  curves  in  Avhich  a  plane 
cuts  a  Right  Circular  Cone.  It  is  shown  in  the  Geometry  of 
Conies  that  these  curves  are  the  loci  of  a  point  which  moves  in 
a  plane  so  that  its  distance  from  a  fixed  point  is  in  a  constant 
ratio  to  its  distance  from  a  fixed  straight  line.  The  fixed  point 
S  is  called  the  focus  ;  the  fixed  line,  the  directrix  ;  and  the 
constant  ratio,  c,  the  eccentricity. 

When  e<  1,  the  curve  is  called  an  Ellipse  ; 

when  e  ^  1,  the  curve  is  called  a  Parabola  ; 

when  '>],  the  curve  is  called  a  Hyperbola  ; 
and  the  circle  is  a  special  case  of  the  ellipse,   the  eccentricity 
being  zero,  and  the  directrix  at  infinity. 

I5  40.  The  Parabola  («  =  1). 
(i.)   To  Jiiid  its  equation. 

Let  the  focus  S  be  the  point  [a,  0),  and  the  directrix  the  line 
X  +  ((  =  0  (Fig.  11). 

Let  P  be  the  point  (.'•,  //). 
Then  since  SP-  =  PM^ 

(,,  _  af  +  ,/  =  (,r  +  a)\ 

if-  =  ia.r. 

*  The  stuilent  is  referred  for  a  fuller  discussion  of  the  properties  of  the  conic 
sections  to  the  books  mentioned  on  p.  12. 

5:j 


54 


THE  CONIC  SECTIONS 


This  is  the  equation  of  the  parabola  Avith  the  origin  at  the 
point  where  the  curve  cuts  the  perpendicular  from  S  on  the 
directrix.      This   point   is  called  the   vertex  of  the  curve  ;  the 


Fig.  11. 


axis  of  X  is  called  the  axis  of  the  curve  ;  and  the  ordinate  L'SL 
through  the  focus  is  called  the  Latus  Rectum. 

(ii.)  The  shape  of  the  curve. 

From  the  form  of  the  equation  of  the  curve  we  see  that  the 
curve  lies  wholly  to  the  right  of  the  axis  of  //,  and  that  it  is 
sjmmetrical  with  regard  to  the  axis  of  o: 


Also  since 


(If/     -la  a 

^  =  —  =     /  -  when  //  >  0. 


It  follows  that  the  tangent  at  the  vertex  coincides  with  the 
axis  of  y,  and  that  as  we  move  along  the  curve  in  the  direction 
of  o:  increasing,  the  curve  continually  ascends,  the  slope  getting 
less  and  less  the  greater  x  becomes. 

(iii.)  The  equations  of  the  tangent  and  normal  at  (^x^,  ?/q). 


THE  CONIC  SECTIONS  55 

fl  il  ^  ft 

Since  the  value  of   —  at  (.'■,-,,  ?/,.)  is  ~,  the  equation  of  the 

iix  11 Q 


tangent  there  is 


y  -  %  _  2a^ 


X  -  .1' 


■  0 


;'/o 


or  ;Vo(.'/  -  //o)  =  'M^'  -  ■'■o)> 

which  l:)ecomes  ////q  =  2a{x  +  x^),  since  i/^-  =  4«3q. 
Also  the  normal  is  the  line 

//o(.?;  -  ,ro)  +  -lad/  -  >/q)  =  0, 

since  this  passes  through  (.>\^,  ;//q)  and  is  perpendicular   to   the 


tangent. 


EXAMPLES  OX  THE  PARABOLA 


1.   Show  that  the  curves  x^—  +4?/  are  parabolas,  and  plot  the  curves. 
'2.   Show  that  the  equation  y  =  ax- + '2bx  +  c  always  represents  a  parabola, 
and  plot  the  curves 

(i.)     y  =  x^+'ix  +  B, 
(ii.)  4Ly  =  x^  +  Ax-  8, 
(iii.)     x  =  i/  +  7j. 
Find  also 

(i.)  The  co-ordinates  of  their  foci  ; 
(ii. )  The  co-ordinates  of  their  vertices  ; 
(iii.)  The  equations  of  their  latera  recta  ; 
(iv. )  The  lengths  of  their  latera  recta  ; 
(v.)  The  equations  of  their  axes  ; 
(vi.)  The  equations  of  the  tangents  at  their  vertices. 

3.  Find  algebraically  and  graphically  the  minimum  value  of  the  expres- 
sion X"  -  2x  -  4,  and  the  maximum  value  of  5  +  4a;  -  2x^. 

4.  The  tangent  at  P  meets  the  axis  of  the  pai'abola  of  Fig.  11  in  T,  and  the 
normal  meets  the  axis  in  G.     Prove  the  following  properties  :  — 

(i.)  AN  =  AT, 
(ii.)  SP  =ST  =  SG, 
(iii.)  NG  =  2AS, 

and  show  that  the  tangents  at  the  ends  of  a  focal  chord  meet  at  right  angles 
on  the  directrix. 

5.  Prove  that  the  line  y  =  x+l  touches  the  parabola  y~  =  ix,  and  that  the 

line  y  =  mx-{ —  touches  the  parabola  y-  =  ia.r.     Find  the  point  of  contact  in 

each  case. 

6.  Find  the  equations  of  the  tangent  and  normal  at  the  point  where  the 
line  x=2  cuts  the  parabola  x-  =  iy. 

7.  Find  the  equations  of  the  tangents  and  normals  at  the  extremities  of 
the  latus  rectum  of  the  parabola  y-—ia,r,  and  show  that  they  form  a  square. 


56 


THE  CONIC  SECTIONS 


8.  Prove  that  the  locus  of  the  middle  points  of  the  chords  of  the  parabola 
y-  =  4a,i-,  wliich  make  an  angle  6  with  the  axis  of  a',  is  the  straight  line 

y  =  2acot  0. 

9.  The  chord  PQ  meets  the  axis  of  the  parabola  of  Tig.  11  in  0.  PM  and 
QN  are  the  ordinates  of  P  and  Q.  Prove  tliat  AM  •  A]Sr  =  AO^,  by  finding  the 
equation  of  the  chord  in  its  simplest  form. 

10.  Tlie  position  of  a  moving  point  is  given  by  the  equations 

.','  =  V  cos  a  .  t, 
y—v  sin  a.  t-  hgt'-. 

Interpret  the  equations,  and  prove  that  the  point  moves  on  a  parabola 
whose  axis  is  parallel  to  the  axis  of  i/ ; 

' X-  sin  a  cos  a    c-  sin-  a ' 


9 


whose  vertex  is  at  the  point 
whose  directrix  is  the  line  7/  =  —- ; 
and  whose  latus  rectum  is  of  length 

S  41.   The  Ellipse  (^<1). 
(i.)   To  find  its  rijiiatidii. 


2^ 


2v^  cos-  a 
9 


Kin.  V2. 

Let  the  axis  of  ,'•  be  the  axis  of  the  ellipse  {i.e.  the  line  through 
the  focus  perpendicular  to  the  directrix) ; 
and  S  the  point  (d,  0)  ; 
the  axis  of  y  the  directrix. 
Let  1'  (x,  if)  be  any  point  upon  the  curve. 

Then  SP2  =  e^VMK 


(.r-iJy  +  !/'=^e^A 


THE  CONIC  SECTIONS  57 

.-.     ,f'-^(l  -  (T)  -  2xd  +  If' ^  -d\ 

d     Y  'I'  <-l'  '^^  'i'c^ 

'■  -  --       J    +      ■ 


\-<^'        l-e"      (1  -  r'f      1-^2      (1  -  e'r 

Now  change  the  origin  to  the  point  (  — ^—^,  0  j   keeping  the 

axes  parallel  to  their  original  directions. 
The  equation  of  the  ellipse  then  becomes 

[j-  d^e- 


x'  + 


(l-e2)     (1-.^)^ 


I.e. 


9  O 

il-e-  ti-c- 


a^  = 


dh^ 

and  b-  = 5, 

1  -  e^ 


Putting 


we  have 


■.,  +  'f^=  1,  where  //-  =  ((-^(l  -  e^). 


In  this  form  the  origin  C  is  called  the  centre  of  the  curve, 
since  it   bisects  every  chord  which  passes  through  it.      This  is 

clear,  since  if  (x^,  1/^)  lies  on  ^  +  —  =  1,  so  does  (  -  x^,  -  //^). 

d  de^ 

Also  we  notice  that  CS  =  ^ ;  -  d  = ,  -  ae, 

i  -  e-  \  -  e- 

and  t^at  CX  =  ;; :,  =    • 

\  -  e-     e 

From  the  symmetry  of  the  equation 

■'■-      '/-      , 
tt-      0- 

it  is  clear  that  there  is  another  focus,  namely,  the  point  {ae,  0) ; 

and  another  directrix,  the  line  .*;  =  -,  with   reg-ard  to   the  axes 

through  the  point  C. 


58  THE  CONIC  SECTIONS 

The  axis  of  x  is  in  this  case  called  the  major  axis,  and  the 
axis  of  y  the  minor  axis.  The  one  is  of  length  2a  ;  the  other  of 
length  1h.  If  h  had  l)een  greater  than  a,  the  foci  would  have 
lain  upon  the  axis  of  //,  and  this  axis  would  have  been  the  major 
axis.     When  a  and  //  are  given  the  eccentricity  e  is  given  by 

//2  =  „^(1 -,<^).     {a>h.) 

In  the  circle  a  -  b,  and  e  =  0. 
(ii.)   The  shape  of  the  nirre. 

Since  the  equation  involves  only  the  terms  ^'-  and  //-,  the 
curve  is  symmetrical  about  both  the  axes  of  ;<■  and  //. 

Also,  since  //-  =  l)-{  1  — 5  j,  we  see  that  x  must  lie  between 

-  a  and  +  a,  and  that  as  ,r  passes  from  -  a  to  +  a  the  positive 
value  of  y  gradually  increases  from  zero  to  h,  and  then  diminishes 
again  to  zero. 

The  curve  is  thus  a  closed  curve,  lying  altogether  within  the 
rectangle  x=  ±  a,  y  =  ±  h. 

This  is  also  evident  from  the  property  of  Ex.  3,  p.  59,  where  it 
is  stated  that  the  curve  may  be  drawn  by  fixing  the  two  ends  of 
a  string  of  length  2a  to  the  points  S  and  S',  and  holding  the 
string  tight  by  the  point  P  of  the  tracing  pencil. 

(iii.)  The  equations  of  the  tangent  and  normal  at  (./q,  y^,). 

Since  -^  +  Vi  =  1 

a^     0- 

^     ■'  ^1  =  0 
a-     b''  dx 

Therefore  the  equation  of  the  tangent  at  (.>„,  y^^  is 

?/^  %  ^  _  ^% 
X  -  .r^,  ((% 

which  becomes 


(^■-■'o),e+(//-//o)^^o, 


2  ^,2 

or 


^-^  =  1,  since  ^  +  §>,=  1. 
a-       b-  a-      0- 


THE  CONIC  SECTIONS  59 

It  follows  that  the  equation  of  the  normal  is 

or  ^-^l^  =  ryl'^^ 

«%     h-ij       ^ 
or  — =  «-  -  0-. 

^'o       Ho 

EXAMPLES  ON  THE  ELLIPSE 

1.  Trace  the  ellipses    (i.)  3a;2  +  4i/=12  ; 

(ii.)  3(x- 1)2  +  4(2/- ■2y-'  =  12; 

(iii. )  x^+iy^=Sjj  ; 

(iv.)  4y-^  +  3y^=12; 
and  find  the  co-ordinates  of  the  foci  and  of  the  extremities  of  the  axes,  the 
length  of  the  latiis  rectum,  and  the  eccentricity  of  each. 

2.  In  the  ellipse  — +  |s=l,  show  that  the  co-ordinates  of  any  point  may 
be  expressed  as  ,v  =  a  cos  d,y  =  b  sin  d  ;  and  interpret  the  result  geometrically. 

3.  P  is  the  point  {.'\,  y-^)  on  the  ellipse  ^+r^  =  l.     Prove  that  SP  =  «  +  f.ri, 

and  S'F  =  a-eXi,  and  deduce  that  the  curve  is  the  locus  of  the  point  which 
moves  so  that  the  sum  of  its  distances  from  two  fixed  points  is  constant. 

4.  The  tangent  at  P  meets  the  major  axis  in  T,  and  PN  is  the  ordinate  of 
P,  prove  that  CN  .  CT  =  CA2. 

5.  The  normal  at  P  meets  the  major  axis  in  G.  Prove  that  SG  :SP  =  e, 
and  deduce  that  PG  bisects  the  angle  SPS'. 

6.  Prove  that  the  middle  point  of  the  chord  y  =  x  +  l  lies  u[)on  //=  — 5  a', 

and  that  the  middle  points  of  chords  jiarallel  to  y  =  mx  lie  upon  the  chord 

,     ''"     . 
?/  —  m  X,  where  mm  +  - .,  =  0. 
a- 

7.  If  CP  bisects  chords  parallel  to  CD,  prove  that  CD  bisects  chords  parallel 
to  CP  (CP  and  CD  ai'e  then  said  to  be  conjiigaie  diameter!^)  ;  and  prove  that 
the  tangents  at  P  and  D  form  with  CP  and  CD  a  parallelogram. 

8.  If  P  is  the  point  {a  cos  0,  h  sin  6).  prove  that  CD  is  the  line  «sin  d.y 
-f  6  cos  e .  X  =  0,  and  deduce  that  CP-  +  CD-  =  a-  +  V^. 

§  42.  The  Hyperbola  (ol).      (i.)   To  find  its  equation. 
Proceeding  as  in  §  41  (i.)  we  obtain  the  equation 

9  o 

f/2g2 

where  we  have  written  a-  for     ,- r-,? 

{'"  -  1)- 


60 

;ui(l 


THE  CONIC  SECTIONS 

h-  for    .,        ,  i.e.  for  d-^n-  -  1), 


and  d  is  the  distance  from  the  focus  S  to  the  directrix. 


Fi<!.  13. 


a 


It  follows  that  CS  =  nc,  CX  =   ,  and  that  there  are  two  foci 

(', 

and  two  directrices. 

The  line  joining  the  foci  S,  S'  is  called  the  transverse  axis  of 
the  hyperbola. 

(ii.)   The  shape  of  the  curve. 

The  form  of  the  equation  shows  that  the  curve  is  symmetri- 


cal about  both  axes,  and  since  //-  =  //-'(  — ,  -  1  )  it  is  clear  that  . 


cannot  lie  Ijetween  -  ((■  and  +  a,  while  since  ,'■'-*  =  <i'{  1  +  p  ),  //  can 

have  any  value  Avhatsoever. 
If  we  write  the  ecpiations  as 

X-     a'-     X- 


we  see  that,  when  .'•  is  numerically  very  great,  '  :,  is  less  than,  but 


THE  CONIC  SECTIONS  (n 

/ - 
very  nearly  equal  to    .;  ;  and  that  for  all  points  on  the  curve 

'f  .    1         t,       ^' 
-,  IS  less  than  — ,  ■ 
.(•"-  fl- 

Also  the  value  of  //  decreases  as  .'■  passes  from  -  x  to  -  a, 
where  it  vanishes,  and  it  increases  without  limit  from  the  value 
zero  at  x  =  a  as  .'•  passes  along  the  positive  axis  of  ,'•. 

The  shape  of  the  ciu've  is  thus  as  in  the  figui'e.     The  lines 

//  =  ±  -  ./■  are  called  the  asymptotes,  and  the  curve  lies  whollv 
a 

between  those  lines;  while,  as  the  numerical  \'alue  of  x  gets  greater 

and  greater,  it  approaches  more  and  more  nearly  to  these  lines 

without  ever  actually  reaching  them. 

(iii.)   The  eqvdtioiis  of  the  tanrjent  and  normal  at  (,/;„  y^^  are  easily 

shown  to  be 

and  |(.'  -  .;,)  +  'p  -  „,)  =  0. 

(iv.)  The  product   of  the  perpendiculars  from  any  point  on   the 
curve  to  the  asymptote's  is  constant. 

The  asymptotes  are   the  lines  //  =  ±  -  .'■.     Then  if  PM,  PX 

are  the  perpendiculars  to  these  lines  from  the  point  (.r^,  //^j, 

/;  b 

PM  =  — -r——,    PN  =  — ,-—-  • 
\   1  +  -,  \^  1  +  ~> 

Therefore  PM  .  PN  =  ^^f  "J^  =  4^-,^ 

since  ^  -'^-  1 . 

a-      ir 

Hence  PM  .  PN  =  constant. 

Now  when  //-  =  a"',  the  asymptotes  are  at  right  angles,  and 
the  eccentricity  is  \/2.      In  this  case,  by  taking  the  asymptotes 


62  THE  COXIC  SECTIONS 

as  axes,  the  equation  x^  -  if-  =  a~  is  transformed  to 

2:nj  =  a-. 

This  equation  is  of  the  form  .///  =  ';-,  a  relation  which  is  of  the 
greatest  importance  in  Physics.  We  could  obtain  an  equation 
of  the  same  form  for  any  hyperbola  referred  to  its  asymptotes 
as  oblique  axes. 

EXAMPLES  ON  THE  HYPERBOLA 

1.  Trace  the  hyperbolas  : 

(i.)  •ix^-iy-=l2, 
(ii.)  3(a;- 1)2-4(2/ -2)2  =12, 
(iii. )  a;2-  4i/2=8i/, 
(iv.)  4x'-  3i/=12; 

and  tincl  tlie  co-ordinates  of  the  foci  and  of  tlie  points  where  each  curve  cuts 
its  transverse  axis,  tlie  length  of  the  latus  rectum,  and  the  eccentricity 
of  each. 

2.  Trace  the  rectangular  hyperbolas  : 

(i.)  rij=±4, 

(ii.)  u='i-±l, 

and  find  the  co-ordinates  of  the  foci  and  of  the  points  where  the  transverse 
axis  meets  each  curve. 

3.  Prove  that  the  tangent  at  (x^,  )/„)  to  the  hyperbola  .17/  =  c^  is 
a^2/o  +  2/-^o  =  2c2,  and  that  the  point  of  contact  bisects  the  part  of  the  tangent 
cut  off  by  the  asj^mptotes. 

2         ^ 

4.  Pis  the  point  (.'„  //j)  on  the  hyperbola  whose  equation  is  —,-^=1. 

Prove  that  ^?  =  cx-^-a,  and  8'V  =  ex-^  +  a,  and  deduce  that  the  curve  is  the 
locus  of  a  ]ioint  which  moves  so  that  the  difference  of  its  distances  from  two 
fixed  points  is  constant. 

5.  The  tangent  at  P  on  the  hyperbola  ^-fr,  =  l  meets  the  transverse  axis 

in  T,  and  FN  is  the  ordinate  of  P.     Prove  that  CN  .  CT  =  a2. 

6.  The  normal  at  P  meets  the  major  axis  in  G  ;  show  that  SG  =  eSP,  and 
deduce  that  PG  bisects  the  angle  SPS'. 

o  'J 

7.  Prove  that,  in  the  hyperbola  '-2-10  =  1,  the  middle  point  of  the  chord 

y  =  x+\  lies  ujion  the  line  y  =  —,x,  and  that  the  locus  of  the  middle  points  of 

chords  parallel  to  y  —  mx  is  the  line  y  =  in'x,  where   vivi'  —  —.■ 

a- 


OF 


THE  CONIC  SECTIONS  63 

o  ■> 

X"       if 

8.' If  OP  and  CD  are  two  coiijiicrate  diameters  of  the  liyperbola  —-'—  =  1 

•'  '■  a-     b^ 

[i.e.  if  each  bisects  chords  parallel  to  the  other),  prove  that  if  P  lies  upon 

this  curve,  CD  does  not  meet  the  curve,  and  that  if  D  is  the  point  wliere  CD 

meets  the  hyperbola  -o-Vo^  -  1, 


CHAPTEE  YIl 

THE  INTEGRAL  CALCULUS — INTECHATION 

§  4:3.  Ix  considering  the  motion  of  a  point  along  a  straight  line, 
we  saw  that  if 

is  the  relation  l^etween  the  distance  and  the  time,  the  velocity  v 
is  given  by  '■  =  ^^=/'(0, 

and,  in  general,  that  the  problem  of  the  DitFerential  Calcnlus  is, 
given  the  law  in  obedience  to  which  two  related  magnitudes 
vary,  to  find  the  rate  at  which  the  one  changes  with  I'egard  to 
the  other.  The  problem  of  the  Integral  Calculus  is  the  inverse 
one  :  given  the  rate  at  which  the  magnitudes  change  with  regard 
to  each  other,  to  find  the  law  connecting  them.  In  other  words, 
in  the  Differential  Calculus  we  determine  the  infinitesimal  change 
in  the  one  magnitude  which  corresponds  to  an  infinitesimal 
change  in  the  other,  when  we  know  wliat  function  the  one  is  of 
the  other.  In  the  Integral  Calculus  we  determine  Avhat  function 
the  one  is  of  the  other  when  the  corresponding  infinitesimal 
changes  are  known.  We  have  thus  to  find  the  function  of  .'•, 
denoted  by  //,  which  is  such  that 

The  A^ilue  of  //  which  satisfies  this  equation  is  written  y/(.r)</,r 
and  is  called  the  iiifnjral  ('//{■'')  witk  rcj/ard  fa  ./'. 

d 


E.I/.   {i.)/.rd.r  =  ~,  since  ^-^('0 


ax  \  •!  / 


THE  INTEGRAL  CALCULUS— INTEGRATION      65 

(ii.)  y*sec-,rf/.''  =  tan  a;,  since       (tan  a;)  =  sec-.*'. 

In  each  of  these  cases  we  might  have  added  any  constant  to 
the  right-hand  side,  since  the  differential  coefficient  of  the 
constant  is  zero,  and  the  complete  result  would  be 

Jxclx  =  '^^  +  C 

/&QC?xdx  =  tan  x  +  C, 

where  C  is  called  the  constant  of  integration. 
It  is  thus  evident  that  the  equations 

and  F(.)  =//{.)d.r 

represent   the  same  thing,  and  that  the  fuller  statement  of  the 
second  would  be 

F(,r)  +  C  =/f{x)dx. 

Owing  to  the  presence  of  the  arbitrary  constant  ff{x)dx  is 
called  the  Indefinite  Integral  of  J\x). 

The  geometrical  meaning  of  the  constant  of  integration  is 
that  there  is  a  family  of  curves  all  having  the  same  slope  as  a 
given  curve,  or  parallel  to  it ;  thus  the  curves 

//  =  FOr)  +  C 

are  all  parallel,  when  C  is  given  different  constant  values. 

§  44.  Table  of  Standard  Integrals. 

From  this  point  of  view  of  integration,  as  the  process  of  find- 
ing the  integral  is  called,  the  first  recpiisite  is  a  table  of  the  more 
important  forms.  This  table  is  obtained  from  the  corresponding 
results  in  differentiation,  and  any  result  in  integration  can  always 
be  verified  by  differentiation.  Later  we  shall  see  that  there  are 
certain  general  theorems  on  integration  which  correspond  to  the 
general  theorems  of  dift'erentiation.  These  will  help  us  to 
decide  upon  the  most  likely  ways  of  finding  an  answer  to  the 
question  which  the  symbol  of  integration  puts  to  us ;  namely, 
What  is  the  function  whose  differential  coefficient  is  the  given 
expression  l  To  answer  this  question  is  in  very  many  cases 
6 


66      THE  INTEGRAL  CALCULUS— INTEGRATION 

impossible  ;    but   practice  soon  makes   it  easy  to  recognise  the 
cases  which  can  be  treated  with  success. 

The  following  is  the  table  of  Standard  Forms  : — 

(i.)  fxMx  = -,     smce  — =  .c"       (h  4=  -  1) 

^  '  -^  %  +  1  ax  \n+\J 

(ii.)  j  ^  =  ^°g  ^''    ^^"^®  ^  (^°g  '')  =  ^ 


(iii.)  Je'^Hx 


a 
1 


(iv.)  faHx  =  . 

^     '  -^  loga 

(v.)  ycos  xdx  =  sin  x 

(vi.)  ysin  2'&'  =  -  cos  x 

(vii.)        ytan  xdx  -  log  (sec  x) 

(viii. )      ycosec  iC(?a;  =  log  ( tan-  j 

(ix.)        /sec"xdx  =  tan  x 
(x. )    /cosech:dx  —  -  cot  x 

/      .    V  f  dx  .      -1    X  /  -ly\  \ 

XI.)  ===^  =  sin      -or     -cos     -)  (a2>a;2)  L    ,. 

^     ^      .'  \/a2  -  X"  "■      V  «/  ^         ^  I  Radian 

f    dx         1        -1  .>■           1        -1  .-c  I  Measure, 

(xii.)  -i x  =  -tan      -or cot 

./  a-^  +  .^^      a  a  a  a  ) 

(xiii-)       I      =^,  =  log(.^•+  Va;-^  ±  a^) 

(Unless  otherwise  stated,  the  logarithms  are  supposed  to  be  to 
the  base  e.) 

The  student  is  recommended  to  draw  up  a  corresponding  table 
for  the  cases  ivhere  mx  +  n  takes  the  pilace  of  x  in  this  list. 

§  45.  Two  General  Theorems. 

(i.)  f{cu)dx^cfiuh; 
(ii. )  f{u  +  v)dx  =J'udx  +J-vdx, 
c  being  a  constant,  and  u,  v  functions  of  .t. 

To  prove  these  theorems  it  is  sufficient  to  show  that  the 
differential  coefficients  of  the  two  sides  of  the  equations  are  the 
same,  since  in  that  case  the  answers  to  the  questions  which  the 
sign  of  integration  puts  to  us  are  the  same  for  both  sides  of  the 
equation. 


THE  INTEGRAL  CALCULUS— INTEGRATION      67 
They  may  be  proved  directly  as  follows  : — 


(i.)  Let 

f{x)  =Judx. 

Then 

|-/w  =  »' 

•••  i  <*■»='«■ 

.•.     cf{x)=Jcudx, 

the  integral, 

r/udx  =fcudx. 

(ii.)  Let 

f{x)  =fudx, 

F(.r)  =fvdx. 

by  the  definition  of 


Then  _i(;(,,:),Fw}=|,.;W.|,F(,..) 

.•.    /(.*■)  +  F(.'-)  =/{u  +  v)dx,  by  the  definition, 
.•.  /iidx  +/vdx  -Jill  +  v)dx. 
Ex.  1 .  J{o-'3?  +  2&a:  +  c)dx  ~  a/a?dx  +  2bfxdx  +  cf\  d.r  * 

=  x  +  \og{2x-l). 

3.  [    '^^  =  []_(J: L_Vtet 

Jx--a?    J  2a\x-a     x  +  a) 

if  dx        1   /   dx 
2a J  X  -  a     2a J  x  +  a 

=  ^  loe  I '■  ] ,        where  xya. 

2a     *  \x  +  aj^ 

4-  ycos  ax  cos  hxdx  —  -j  [cos  («  +  b)x  +  cos  {a  -  b)x]dx 

=  -  /  cos  (a  +  b)xdx  +  -  /  cos  {a  -  b)xdx 

■  sin  {a  +  b)x  H-  — r,  sin  (a  —  b)x. 


2{a  +  b)        ^     '    '     '  2{a-b)' 
§  46.  Integration  by  Substitution. 

To  prove  that  /f{x)dx  =/f{x)  •  jj-dt,  where  x  =  <^(t). 

*  Jl .  dx  is  usually  written  a,sjdx. 
t  This  is  an  important  example.     Cf.  (xii.)  p.  66. 


68      THE  INTEGKAL  CALCULUS— INTEGRATION 

This  important  result,  which  allows  us  to  change  an  integral 
with  regard  to  x  into  an  integral  in  terras  of  another  variable,  may 
be  deduced  at  once  from  the  rule  for  difterentiating  a  function 
of  a  function. 

Let  y  =/jlx)dx,  and  x  =  <f)(t). 

From  the  relation  between  x  and  f,  //  is  a  function  of  t. 

dy     dy  dx 
dt     dx   dt 

dji  dx        .       dy  , 

•'•       irf^^'^dt^    «"^ce^-^.=/0.) 

11  =  f fix)  —  -df,  bv  the  definition  of  an 

integral. 

The  expressions  under  the  sign  of  integration  are  supposed 
given  in  terms  of  t. 

This  result  may  be  written 

(A.)  Jf(x)dx  ^ff{x)  .  '1^  .  dt  =/^[</>(/)]-|[<^(0]rf/. 

The  simple  rule  for  "  changing  the  variable  "  from  .'•  to  /  is  : 

Replace  dx  hi/  -^  .  dt,  and  hi/  means  of  the  equation  connectinq  x 

dt  '  ■  -L 

and  t,  exp'ess  f(x)  as  a  function  of  t. 

The  advantaares  of  this  method  will  be  evident  from  the 
following  examples  : — 

Ex.    (i.)  J{a:i-  +  h)"dx.  Vwt  n.i-  +  h  =  u. 

dx  _1 

du     a 

r                     r       I            if              ?t"+'^  1  ■"+^ 

and  J(a.r  +  byd:r=Ju"  .  -.  du=-\u"du  =  ~ ztt^-,       ^Aax  +  b) 

if.        ,  cos  n         1 


Similarly  (ii. )       y  sin  {ax  +  h)dx  =  --  I  sin  udu  = =  -  -  cos  {ax  +  h), 

f       dx 

(ill-)  /  .  o     ,o  •     Vut  ax  =  ii. 

-'  \'  a-x-  -  ir 

.       dx  _\ 

dv     a 

J  f       dx  /■       1  ]       ,       1    j"     du 

and  /     ,  -    =  /     /         -  •      •  du  =  -      -, 

J  >y«V  _  1-2     J  V?t^  -  63     a  a  j  ^'„-i  _  b-i 

1  , 


=  -  log  {ax  +  \'aV-  -  b"). 


THE  INTEGEAL  CALCULUS— INTEGRATION   69 

(iv.)  P^g'^-.,^,^,  Vnt.r  =  c". 


X 


dx 

clu 


and  /  -?  '^clx  =  /  -  •  c«  •  dii  =  fudic  =  ^  u^ 

J     X  J  e"  J  2 


=  \\o^xf. 


^^•^  \a-X^Y^  Put,.=co.s(^. 


{\-x)i 

dx 


■   ■    d0= -'''''' 

f  dx  f  1  ,  .        .^  ,, 

j(l-a')Vl-j;'2     j  (1  -  cos  ^)  sin  ^  ^ 

_  _  1  f   dd 
•'  sin-;5 

.6 
=  cot-, 

_  V  ]  -  X' 

l-x 
(vi. )  Integrate  the  following  exi^ressions  : — 

, x" 

(a)       x^'-^iax'^  +  h);  x\la\  +  x^;  ^^j-^. 

^^)       x^  +  lx  +  2  '  ..-^r2"J+ 2'  P"""'S  ^'  +  ^  =  "• 

(3)       -7^^-r -  .,  ;     z-^'^^,       ^.  putting  .,_•  +  2  =.  M. 

(^)  /     9     „^    =  ;     /-'  o    ^ ,      - '  Pitting  aa;  +  h  =  u.     {ac)h-.) 

s'ax^  +  2bx  +  c     \'ax^  +  2o.r  +  c 

1  COS  CtJ 

(f )        sin^  :<:  cos^  a;  :  , — -. —  :  cot  .'•,  putting  sin  x  =  7i. 

iv)       -2 5 ur-^^r  ;  --  o  --o  .  putting  tan  a;  =  i(. 

§  47.  Integration  l)y  Substitution — continued. 

Although  there  are  certain  general  principles  that  guide  us 
in  the  choice  of  a  suitable  substitution,  the  second  form  (B.), 
p.  70,  of  the  theorem  of  §  46  Avill  often  suggest  what  the 
transformation  should  be.     We  have  seen  that 

ffW)]  ^^^W)¥t=/f(x)dx,  where  x  =  <f.{t), 


70      THE  INTEGRAL  CALCULUS— INTEGRATION 

and  we  may  write  this  result  in  the  form 

(B.)    //L>(.r)]^[</)(.v)]rf.;  =ff{v) .  du,  where  ^t  =  ^(x),* 

as  the  particular  symbol  we  employ  is  immaterial. 

Thus  in  the  case  of  the  examples  of  last  article  Ave  obtain  our 
results  immediately — ■ 

e.g.  (i.)  /(ax  +  Hydx  =  -  I  (ax  +  i)"  •  -^  (ax  +  h)dx 


=  -   u'hh,  w 
a  J 


here  ax  +  h  —  u 


a  J 

1      u»+^  1 


71  +  1     a 


-, -.  (ax  +  /0"+'- 

a(%+  1)  ^  ^ 


(ii.)    ysin-  X  cos  xdx  =y*sin-  x  -r;(sin  x')dx 

-/ifidti,  where  sin  x  =  u 

=  -  sin"*  X. 
o 

(ill.) -.  ■  dx  =  - .  •  T-  •  (1  +  -'^0  •  d-^ 

^     ^        ;  1  +  x^  5J  I  +  x;'    dx    ^  ^ 

--]    - ,  where  m  =  1  +  x^ 
5.'  u 

=  -\ogu 

=  l\og(l+o:^). 

(iv.)  jm^^^^iogM. 

In  this  way  it  is  easy  to  see  that 

f      ax  +  h        ,       1 1      /    o     ^, 

/     9     ^j  dx  =  -  log  (ax-  +  2bx  +  c), 

J  ax^  +  2bx  +  c  2     *=  ^  ^ 

*  This  can  be  verified  ]>y  starting  with 

//{vyiu, 
ami  putting  u  —  <p(x),  as  in  (A.) 


THE  INTEGRAL  CALCULUS— INTEGRATION      71 
since  the  integral  may  be  written  as 

1     fdU  ,  o  ^7 

i.e.  - 1  — ,  where  w  =  ax-  +  2bx  +  c. 

2.1  u 

Also  /  — 2 — -. =  I ;; ^, T^  •  — (aa  +  h)  •  dx. 

J  ax^  +  2ox  +  c     .'  {ax  +  b)-  +  ac  -¥   ax  ' 

=  I  -s rz^  ■  du,  where  ii  —  ax  +  h, 

J  u^  +  ac  -  b^ 

and  this  is  one  of  the  standard  forms. 
It  follows  that  amj  expression  of  the  form 

Ix  +  m 
ax"  +  2hx  +  c 

may  he  easily  integrated,  since  we  can  rewrite  the  numerator  as 

P(aa;  +  6)  +  Q, 

,                                     ^     I      ,^     am  -  lb 
where  P  =  -  ;  Q  = . 

a  a 

If  higher  powers  of  x  occur  in  the  numerator,  we  must  first  of 
all  divide  out  by  the  denominator  till  we  ol>tain  a  remainder  of 
the  first  degree  or  a  constant.* 

The    expression       .  may   he   reduced   in   a  similar 

fJax?  +  2hx  +  c 


way. 


Ex.   Integrate  the  following  expressions — 

1  1  1  x+1  2x  +  Z 


(i.) 


(ii.) 


x^±4:  '  a?x^±b'^  '  4.r2  +  4x-  +  3  '  4a;2  +  4a;±3  '  3  +  4x-a:2  ' 

X^      _  X'-X  +  l  _        x-\       _       x^  +  x  +  \ 
a;2  +  1  '  .x-2  +  a;  + 1  '  x- -  5x  +  6  '  (.r -!)(./■- 2)" 

11  1  a;+l  2x  +  3 


v/a;2  +  4  '  sld'x"±lr  '  \/4a;^  +  4«  +  3  '  v'4.>j- +  4a;  ±  3  '  x/5  +  4.T-a;2' 


*  When  the  factors  of  the  denominator  are  real,  the  method  of  Partial  Fractions 
should  be  employed. 


72      THE  INTEGEAL  CALCULUS— INTEGRATION 

§  48.  Integration  by  Parts. 

The    second    important    method    in    integration    is    called 

integration  by  parts,  and  can  he  used  only  when  the  function 

to  be  integrated  is  the  product  of  two  functions,  one  of  which 

can  be   expressed  as  a    differential    coefficient.      This    method 

follows  at  once  from  the  rule  for  the  differentiation  of  a  product. 

^.  (/   .     ,         dv        da 

omce  -r  (uv)  =  u  ^  +  v  ^, 

ax  dx       dx 

uv  -  \(u      +  V  j-jdx,  by  the  definition  of  integration, 

r   dv    ,        r  du    ,     ,      .   , _ 

r    dv   .  f   du    , 

JU-— dx  =  uo -J  r -- -dx. 

dx  dx 

This  result  Avill  be  of  use  only  if  fv  -    dx  can  be  more  easily 

evaluated  than  fu  —-  dx. 
dx 


For  example — 

(i. )    fx  ■  log  X  ■  dx  =  ;^  I  log  «  ^  (a;2)  •  di 


dx 


=  ~{x'  log  X  -Jx^  ~  (log  x)d. 
=  - ix-  log  X  -fxdx) 
=  -(^o:'\ogx-'^) 
(2  1ogr.-l). 


_x- 
(ii.)  y.'r  •  cos  X  •  dx  =Jxr  %    (sin  x)dx 


=  x'^  sin  9:;  -  /"sin  .'•  ■       (.*•■-')  •  dx 
=  x^  sin  X  -  2ysin  x  ■  x  •  dx 
=  J?  sin  X  +  2fx  •  -7-(cos  x)dx 


=  X-  sin  ;*;  +  2 


/;  cos 


X  -fcos,  X  -^ (x) •  dx) 


THE  INTEGEAL  CALCULUS— INTEGKATION      73 

=  X-  sin  X  +  2{x  cos  x  -J'cos  xdx) 
=  .)?  sin  X  +  2;/;  cos  x  -  2  sin  x. 

In  both  of  these  examples  this  artifice  allows  us  gradually 
to  reduce  the  integral  to  one  of  a  simpler  form,  and  in  such 
cases  where  powers  of  o:  are  associated  with  a  trigonometrical, 
exponential,  or  logarithmic  term,  it  is  of  great  value.* 

An  important  expression  which  can  be  integrated  by  this 
method  is   \';';-  +  a-. 

We  have 

f  ^'^V^'  ■  dx  =  j  \/:r^Va^  •  J  (./•)  dx 

r  rl 

=  X  v^,T-  +  a-  -  I X  —  'Jx-  +  d^  •  dx. 
J     dx 

■  ■  -     I  \^x-  +  a-  ■  dx  =  .(-■  six-  +  a-  -  \  -/  „       „  •  dx 
J  J  v.T^  +  fr 

dx 


■     /■./■■^  +  a^-  a- 

X  \'x?  +  ft-  -  I  -  ,  ^       q 
i  \-  a;-^  +  ft^ 


/"    ^ c      dx 

=  ,/:  V .r-  +  a?-  -  I  s/ x?  ■\-  c?  dx  +  ft-  I     /  .,        o' 
;  ;  \'x^  +  ft- 

.  •.      21   sJo?  +  ft"^  dx  -  X  \/,i'-  +  ft"^  +  ft-  log  (.}■  +    V.;;-  +  d^) 
I  V  a;-  +  ft-  ft.v  = -_ 4-  —  log  (.>■  +  \'x"  +  cr). 

Ex.  Integrate  the  following  expressions  : — 

a'-  log  X  ;  a;^  e*^  ;  .<;  tan~^  x  ;  x-  sin  aa; ;  Va'-^  -  a"  ;  v'.-c^  -  «^. 

EXAMPLES  ON   CHAPTER    VII 
1.   Integrate  the  following  expressions — 

N/aa;  +  &      \/a;     «  +  3 

,..  ,  1  •-''■  - 1  a^  X* 

(11.) 

(iii.) 


x{\-x)''    x-~-6x  +  -z'    a;-  +  a;  +  l'    x^-x  +  \' 

1  2a; -1 x  + 1 

'Jx(\^x)'    'Jx^-Zx  +  2'    VaT^Tai  +  l" 


Cf.  p.  74  ;  Exs.  11,  12,  13,  14,  and  15. 


74      THE  INTEGRAL  CALCULUS— INTEGRATION 

2.  Integrate  the  following  expressions  by  parts — 

sin"^./-,     d?  tan~^a',     a;^  sin  4.'',     o-}  cos  3:/;,     a:'"  log  x,  x-c~^. 

3.  Prove  that 

1  1  a;-2 


ar*+l     3(.r+l)     3(.r2-a-  +  l)' 
and  hence  integrate  the  expression. 

4.   Prove  that 

1  111 

+ 


(.j-  +  l)(a;-l)2     2(a;-l)-     4(,''-l)     4(a;+l)' 
and  hence  integrate  the  expression. 

5.   Prove  that 

x-\  2  1 


(a;-2)(.Y-8)     :>-^     «-2' 
and  hence  integrate  the  expression. 

6.  Integrate  the  expressions  x  V 1  +  x  and  — ,  by  putting  ,i-  +  1  =  v.-. 

7.  Prove  that 

dx                 1^1      x\^'l 
r  =  — r=  tan~' 


/,- 


(1  +  a;-)  N^l  -  x^     \'2  """       s'l  -  x- 
(pnt  a;  =  sin  0). 

8.   Integrate  the  following  trigonometrical  expressions- 


sin  X 


sin  e'    sin  {6  +  a)'    sin  ^  +  cos  d'    cos"'*  ^  s,/a^  tan-  9  +  6'-^'    cos"^  a;(4  tan^^a:;  +  3) 

9.  Show  that,  when  a^b^, 

f       dx  2  _j/      /ci-h  ^      x\ 

J  a  +  b  cos  X-  ^/„2— 6^  *^"      ^  V  a  +  ^,  ^an  -  j. 

Put  a  +  b  cos  a;  into  the  form  {c  +  h)  cos"  '|  +  («  -  Z*)  sin- 1    • 


Also  integrate  the  expressions 

1  1 


5  ±  4  cos  a;     4  +  5  cos  a;     3  ±  2  sin  .^;     2  +  3  sin  x 
10.  Prove,  by  integration  by  parts,  that 

i;  \   Car        17       &  sin  5a;  + «  cos  &a:  „^ 
(1. )  /c"^  cos  bxdx  = 5 — rs e    , 

r  ■  \    r  OT   ■    I    7       a  sin  6a;  -  &  cos  bx 
(11. )  /c""  sin  bxdx  = 5 — ,„ ef". 


11.   Prove,  by  integration  by  parts,  that 

/■  •   «  ojo         cos  ^  sin"-^  ^     n  -if.       „  ^  , 

I  am"  Odd  = +  /sin"--6>(i? 

•^  n  n   J 


and  hence  show  that 


f  ■  i  n,a         sin^^cos^     3   .     ,        n     3^ 

7  sill-'  Bi/d  = sin  e  cos  ^  +  s  ^• 

4  o  o 


THE  INTEGRAL  CALCULUS— INTEGRATION      75 

12.   Prove,  by  integration  by  parts,  that 

r      r,  nja     sin  6  cos"-i  d     {n  -I)  f      „  ,  ^  ,^ 
/  cos"  ed0  = + ■    cos"-2  ddd, 

-'  71  11      J 

and  thus  obtain  the  value  of/ cos''  dd9  andy'cos-'  ddd. 

13.  Prove  that 

Jai^'c^dx  -  ,7;"e=^  -  nfx''-'^e''dx, 
and  explain  how  this  result  may  be  used  in  evaluating  such  integrals  as 

fu^e^dx,  Jx?e~'^dx,  etc. 

14.  Prove  that 

y^n-i(iog  xY^dx  —Jif^c^ydij, 

where  x=ey,  and  explain  how  this  result  may  be  used  in  evaluating  integrals 
such  as 

fr'^{\og  xfdx,  J'x~\\og  xfdx. 

15.  Prove  that 

x^  sin  mxdx  =  - '—  cos  mx  -\ —  /  a;""^  cos  mxdx 
m  mj 

a;"  n     ,.  ,   .  n.7i-l  f  „  <,  .  , 

= cos  7nx  -\ — s  a-""'  sin  mx 5 —  I  ^      sm  mxdx, 

m  m-  m''     J 

and  show  how  this  may  be  used  in  evaluating  such  integrals.*    Obtain  a  corre- 
sponding result  in  the  case  of 

fx"  cos  mxdx. 

*  Examples  3,  4,  5  are  cases  of  the  use  of  the  method  of  Partial  Fractions 
in  the  integration  of  algebraic  functions  ;  11-15,  of  the  method  of  Successive 
Reduction.     Cf.  Lamb's  Infinitesimal  Calculus,  §§  80,  SI. 


CHAPTEE    YIII 


THE    DEFINITE    INTEGRAL    AND    ITS    APPLICATIONS 


i^  49.  In  the  last  chapter  we  have  considered  the  process  of 
integration  as  the  means  of  answering  the  question  :  What  is 
the  function  whose  difierential  coefficient  is  a  given  function  ? 
There  is  another  and  a  more  important  way  of  regarding  the 
subject,  in  which  integration  appears  as  an  operation  of  sum- 
mation, or  of  finding  the  limit  of  the  sum  of  a  number  of  terms, 
Avhen  these  terms  increase  in  number  and  diminish  indefinitely 
ill  size.  We  shall  examine  integration  from  this  standpoint  in 
the  following  sections. 

§50.  Areas  of  Curves.    The  Definite  Integral  as  an  Expression 
for  the  Area. 

Let  //=,/(.'•)  be  the  equation  of  an  ordinary  continuous  curve, 

and  let  us  consider  the 
area  enclosed  between 
the  ordinates  at  P^C'^'o)  ^o)' 
and  P(.r,  y),  the  axis  of 
X  and  the  curve  Avhere 
PqP  is  above  that  axis. 
This  area  is  obviously  a 
function  of  .r,  since  to 
every  position  of  P  cor- 
responds a  value  of  the 
area. 

Let  A  stand    for    the 
area     PoMqIMP  ;     A  +  SA 
for    the    area    P^M^NQ ; 
and  let  Q  be  the  point  (.'•  +  h\  //  +  %).     Then   if   the  slope  is 

76 


THE  DEFINITE  INTEGRAL  AND  ITS  APPLICATIONS  77 

l)Ositive  from  P  to  the   neighbouring  point  Q,  we  see  by  con- 
sidering the  inner  and  outer  rectangles  at  P  and  the  element 

of  area  there,  that 

v/5.r<SA<(y  +  8i/)  8.r, 

and  if  the  slope  is  negative  the  signs  are  reversed. 

Hence  in  each  case,  when  we  let  8x  approach  its  limit  zero, 
we  have 

thus    A  =/f{'i)dx  +  const.  =  F(.';)  +  C,  sa}^ 
Also,  since  A  vanishes  when  x  =  x^^,  C  =  -  F(.)'(,) ; 

.-.  A  =  F(,r)  -  F(.g. 
This  expression  F(.'')  -  F(,*'p) 

is  an  important  one,  and  the  symbol 


J  Xn 


is  used  to  denote  it. 

/  f(x)dx  is  called  the  definite  integral  of  f{x)  with  regard  to  x 

J  Xq 

between  the  liviits  x^  and  x,  and  its  value  is  obtained  by  siibtracting  the 

value  of  the  indefinite  integral— ff{x)dx— for  x  ^  x^from  that  for  x  =  x. 

AVith   this   notation   the  area  of  the  curve  y  =f(x)  included 

between  the  ordinates  at  (iq,  y^)  and  {x^,  //j),  the  axis  of  .'•  and  the 

curve  is  equal  to  I   f{x)dx,  and  it  is  clear  that  if  the  curve  cuts 

J  .'ij 
the  axis  between  the  limits  x^  and  ,r^,  the  definite  integral  gives 

the  algebraical  sum  of  the  areas,  those  above  being  taken  positive, 

those  below  the  axis  negative. 

Ex.   1.   To  find  the  area  of  the  part  of  the  circle  x~+i/  =  a'-^  cut  off  Ijy  the 
lines  ,T  =  0,  and  x  =  Xi. 

The  required  area  =  2  /     Ja'^  -  x-  dx. 

J  ^n 
Now  it  is  easy  to  show  that 

j  s'^i^'  djx^'^'^'^  +  \  sin-i  (■^)  (cf.  §  48)  : 


the  area  =    x  \'a^  - .'/-  +  a-  sin-^  (  -  j       , 


78  THE  DEFINITE  IXTEGEAL 

where  we  iise  these  square  brackets  to  denote  tliat  we  subtract  the  value  for 
x  =  Xq  from  that  for  ci:  =  xi. 

If  we  take  X(j  =  0  and  Xi  =  a  we  find  the  area  of  the  semicircle  as  7  ctr. 

■1.  To  find  the  area  of  the  part  of  the  parabola  y-=\ax  cut  off  by  the 
lines  x  —  Xq  and  x=x-^. 


Here  the  required  area  =  2  /     \/4aa-  dx, 

J  ^0 

/-  /^^    n 
=  4  N  ft  /       \X  dx, 


9 


and  it  follows  that  the  area  cut  off  by  the  latus  rectum  is  ^  of  the  rectangle 

o 

upon  LL'  as  base,  with  AS  for  its  altitude. 


3.   Prove  that  the  area  of  the  ellipse  -2  +  |^  =  l  is  wab. 


«2  '  62 


4.   Prove  the  following 


O   ' 


(1.)  /     =log(\/2  +  l)=  /    -^— 

J  o^osx       °  '  ./  77  sm ; 

4 

W  IT 

(ii.)  /     sin-x.dx  =  j=  I   cos-x  dx. 

Jo  4      J  „ 

...  ,  /"'J  dx _jr^_  j'2  dx 

J  a  a"^  sivP'X  +  b"^  cos^^c  ~  'lab  ~  J  q  a-  cos'-u;  +  6^  sin'^ 

(iv. )  /    sin-^a;  fte  =    '^ecosedd  =  ^~l 

(V.)  f'P--''^' 


sm-a; 


/dx  _  TT 


.5.  Prove  that  when  ?n  and  n  are  positive  integers 

TT  TT 

(iii. )  /  '"'  sin'"  d  cos"  ^f/^  =  '^^——  i  ^  sin'"-'-  B  cos"  ^rf^. 

^0  ''(■  +  "-'0 


AND  ITS  APPLICATIONS  79 


(iv.)  I"  sin^ecos^ede  =  —  ^ 


{y■) 


/  ^  sin«  ^  cos«  ^f^^  =  ^^'    ^'    I",  /  "  cos*  edd  =  ^,  ■ 


14.  12.  10./ 0  '-^l'^ 

In  cases  where  integration  is  not  possible  there  are  various 
approximate  methods  of  finding  the  area.  The  expressions  for 
the  area  of  a  trapezium  or  a  portion  of  a  paral)ola  give  the 
trapezoidal  and  parabolic  rules,  and  we  shall  see  more  fully  in 
§§  51-52  how  the  inner  and  outer  rectangles  may  be  applied. 
The  value  of  a  definite  integral  may  also  be  obtained  by 
mechanical  means  by  the  use  of  difterent  instruments,  of  which 
the  planimeters  are  perhaps  the  best  known. 

Ex.  Evaluate  the  following  integrals  by  the  trapezoidal  method,  i.e.  find 
the  sum  of  the  inscribed  trapeziums  instead  of  the  inner  or  outer  rectangles 
as  above  : — 

,12 

(i. )    I    .i'hlx,  dividing  the  interval  into  11  ecpial  parts,  and  compare  with 
-  1 
tlie  result  of  integration. 

Answers,  577i  ;  575f . 

.32° 

(ii. )     I     cos  d.r,  by  dividing  the  interval  into  6  equal  parts,  and  compare 

■^  31° 

as  above. 

Answers,  -0148  ;   "0149. 

§  51.   The  Definite  Integral  as  the  Limit  of  a  Sum. 

We  have  in  the  last  article  shown  that  the  symbol  I  f(j:)dx 

J   ,-'0 

represents  the  area  between  the  curve  y=f{x),  the  axis  of  x,  and 
the  bounding  ordinates.  We  shall  now  obtain  an  expression  for 
this  area  as  the  limit  of  a  sum,  and  thus  see  in  Avhat  Avay  the 
process  of  integration  may  be  viewed  as  a  summation. 

Let  PqPi  be  any  portion  of  the  curve  on  which  the  slope 
remains  positive. 

Divide  the  interval  M^M^  into  n  equal  parts  S.t,  so  that 

erect  the  ordinates  m-^p-^,  ni^'p.^,  etc.,  and  construct  inner  and 
outer  rectangles  as  in  Fig.  15. 

Then  the  difference  of  the  sum  of  these  outer  rectangles  and 


80 


THE  DEFINITE  INTEGRAL 


the  sum  of  the  inner  rectangles  is  {//^  -  ^q)o'',  and  this  may  be 

made  as  small  as  we 
please  by  increasing 
the  number  of  inter- 
vals and  decreasing 
their  size. 

Also  the  area  of  the 
curve  lies  between 
these  two  sums,  and 
tlierefore  this  area  is 
the  limit  of  either  sum 
ss  8x  approaches  zero. 
Now  the  sum  of 
the  inner  set  of  rect- 
angles 


M(^m,  mj  rrij 


Fin.  15. 


=  2    f(x^  +  r8x)8x. 


-f./(.r,  +  w-1.8,r).fe] 


But  the  area  is  [F(;r^)  -  F{.'\^^)]  Avhere  F(,/')  =/f{x)dx,  and  we  agreed 

/■'I 
to  denote  this  by   /  /(.')'/■'■. 

...        r  f{.^)dx  =  Lts,=o  X  '^"     ./(.'o  +  rSx) .  &r, 

.'  ■,■()  nSx  =  Xi-Xof  )■  =  () 

=  lJs^^Q'Sf(x)8x,  written  shortly. 

It  is  easy  to  remove  the  restriction  placed  upon  /(.')  that  the 
slope  of  the  curve  should  be  positive  from  P^  to  P^ ;  and  to  show 
that  this  result  holds  for  any  ordinary  continuous  curve  whether 
it  ascends  or  descends,  and  is  above  or  below  the  axis  in  the 
interval  .'v  to  x^. 

It  is  only  necessary  to  point  out  that  in  the  case  of  such  a 
portion  of  the  curve  y=f(x)  as  is  given  in  Fig.  16,  the  area  of  the 
portion  of  the  curve  marked  11  will  appear  as  a  negative  area, 
andif//(r>/r  =  F(4 

'  f{.r)d.r,  or  [Vih)  -  F{a)l 


f 


AND  ITS  APPLICATIONS 


81 


is  equal  to 


(I)  -  (II)  +  (III). 


Fig.  10. 

Tlie  importance  of  this  result  lies  in  the  fact  that  many  geo- 
metrical and  physical  quantities  {e.g.  volumes  and  surfaces  of 
solids,  centres  of  gravity  and  pressure,  total  pressure,  radius  of 
gyration,  etc.)  may  be  expressed  in  terms  of  the  limits  of  certain 
sums.  The  problem  of  obtaining  these  quantities  is  thus  reduced 
to  a  question  of  integration.  The  symbol  of  integrationy'  really 
stands  for  the  large  S  of  summation,  and  it  was  in  the  attempts 
to  calculate  areas  bounded  by  curves  that  the  Infinitesimal 
Calcuhis  was  discovered. 

It  is  also  possible  to  start  with  the  definition  of  the  symbol 

f{x)dx 

J    Xo 

as  the  limit  of  a  sum,  and  then  obtain  its  value  in  terms  of  the 
indefinite  integral.* 

§  52.  The  Evaluation  of  a  Definite  Integral  from  its  Defini- 
tion as  the  Limit  of  a  Sum. 

It  is  instructive  to  see  how,  by  algebraical  methods,  the  values 
of  certain  definite  integrals  may  be  obtained  direct  from  this 
summation. 

*  Cf.  Lariil)'s  Calculus,  §§  90,  91. 
7 


82  THE  DEFINITE  INTEGRAL 

For  example,  in  the  case  of  the  parabola 

y  =  A 
we  can  obtain  the  area,  or  the  Definite  Integral,  as  follows  : — 

y,     Sx{Xq  +  rSxf 

r  =  0 

=  S4;<-o'  +  (^0  +  ^''-y'  +  (^0  +  25,>f  +  {X,  +  n-l.  a,>f  ] 
-  i,x\nx^^^  ^-n  .  {n-\) .  x^h:  + — r-^ y^'')") 

using  the  results  for 

1  +  2  +  3  +    .   .   .    +  {n  -  1),  and  1-  +  2^  +    .  .   .    +  («  -  1)2. 
Therefore,  since  nhx  =  (x^  -  x^), 

'' 2  '   8x(x,  +  r8^f  =  x^ix,  -  X,)  +  x,{x,  -  x^  (l  -  1) 


r  =  n-l 

Lt         2      8x{x^  +  rhf 

fix  =  0       )    ?-  =  0 


J-'^  ft  =  c» 


fix  =  0       ) 
/i6x= xi-.ro  ) 

=  x^\x^  -  x^)  +  .ro(.r,  -  .ro)2  +  ^(:r,  -  x^f 


o  J  '•'1  ■*'0 

x-dx  =  — ^    .    "  • 


Ex.   Prove  in  the  same  way  that 

fim  1 

/       COS  mxdx  =  j^^  • 
■  0 


AND  ITS  APPLICATIONS  83 

§  53.   Properties  of        f{x)d:r. 

J    -('O 

The   following  properties   of   the   Definite  Integral  may  be 
deduced  from  either  of  the  definitions  of  this  symbol : — 

I.  Mdx  =  -       f{x)dx. 

J    Xq  J    Xi 

II.  (  f{x)dx  =   {   f{r)dx  +   (   /(..>/,r. 

J   'J:o  J  .'0  -'   f 

III.  The  integral  of  an  even  function  between  the  limits  -  a  and 
+  a  =  twice  the  integral  of  the  function  between  0  and  a. 

E.g.      I      xMx=2{  x}dx='^a^ 


ain-e .  de  =  2 


sin-Ode  =  TT- 


IV.  The  integral  of  an  odd  function  between  the  limits  -  a  and 

+  a  is  zero. 

E.g.  1        xHx  =  0,       I        sin^dd  =  0. 

Similarly  1   sin"' 6  cos'^''+^  ede  =  0, 

m,  n  being  positive  integers. 


V.  In  applying  the  method  of  "  change  of  variable  "  to  the 
evaluation  of  definite  integrals,  we  need  not  express  the  result 
in  terms  of  the  original  variable.  We  need  only  give  the 
new  variable  the  values  at  its  limits  which  correspond  to  the 
change  from  x^  to  x^  in  the  variable  x,  care  being  taken  in  the 
case  of  a  many-valued  function  that  the  values  we  thus  alhjt  are 
those  which  correspond  to  the  given  change  in  x. 


84  THE  DEFINITE  INTEGRAL 

E.g.       I  ^W^^.dx 


*2 


a^      cos-OdO,  putting  x  =  a  sin  d, 

Jo 


2(2 


2  V  2        ,, 

§  54.  Application  to  Areas  in  Polar  Co-ordinates. 

AYhen  the  equation  of  the  curve  is  given  in  polar  co-ordinates, 
the  area  of  the  sector  bounded  bj'  0  =  6^  and  0-9^  may  be 
sho's\ai  to  be 

with  the  same  notation  as  before.     Hence  if  the  curve  is  r  =f(B), 
the  sectorial  area  is 

If'' 

"J  9o 

Polar  co-ordinates  offer  the  most  convenient  method  of  finding 
the  area  of  a  looji  of  a  curve. 
For  example,  the  lemniscate 

r^  =  a^  cos  20 


has  a  loop  between  0  -  -  ^  and  6  =  -. 


1  (■' 
The  area  of  this  loop  =  -         f-dd 


AND  ITS  APPLICATIONS 


85 


rt^ 


COS  26(16. 


J 


4 


the  area  of  the  loop  =  a^      cos  26cW  (Cf.  §  53,  III) 


a- 


a- 


sin2(? 


Similarly,  in  the  Folium  of  Descartes,  whose  equation  is 

a;3  +  yZ  =3  3axy, 
there  is  a  loop  in  the  first  quadrant ;  and  transferring  to  polar 
co-ordinates  we  find  that  the  area  of  the  loop 


1 


7-m 


n 


JfSa  cos  6  sin  ^V^  /^ 
I  ws¥T"sin¥/ 
0 
n 

9    2  r^     cos^^  sin^^ 

2''        (cos^^^^  +  sin=*^)2 '^^ 


9    . 
3  ... 


f- 


J  11 


l  +  f 


r,  ■  df,     putting  tan  6  =  t,       (Cf.  §  53,  V.) 


3    o 

3a2 

~         2  ■ 

3 

Ex. — Prove  that  the  area  of  the  cardioide  r  =  «(l  -  cos  6)  is  n'^a^- 

§  55.  Applications  to  Lengths  of  Curves. 
The   length   of   an   arc    PgP^  of   the  curve   //-./(«)   may   be 
regarded  as  the  limit  of  the  sum  of  the  different  chords  into 


86  THE  DEFINITE  INTEGRAL 

which  PgP^  is  divided  by  the  ordinates  at  m^,  ???.,,  .   .   .   (cf.  Fig. 
15). 
Hence 

arc  PqP,  =  L/5,=o    '^\f(8x)^'T'(8i/Y 

,   dx=   I'    ^14-  m'-dy, 

J    3/0 

since     /  1  +    rjl]  will  differ  from     /  1  +    f^j "  by  a  very  small 

quantity  when  &x  is  very  small,  and  the  sum  of  these  differences 
multiplied  by  8x  will  vanish  in  the  limit. 

If  polar  co-ordinates  are  used,  we  obtain  in  the  same  way  for 
the  curve  r  =f{0)  the  two  expressions 

since  the  chord  is  in  this  case  \^'{8r)"  +  (rSd)-. 

Owing  to  the  presence  of  the  radical  sign  under  the  sign  of 
integi^ation,  the  problem  of  finding  the  length  of  the  curve  has 
been  solved  in  only  a  limited  number  of  cases. 

Ex.  1.  Prove  that  the  length  of  the  arc  of  the  jjarabola  y-  =  4ax  from  the 
vertex  to  the  end  of  the  latus  rectum  is  equal  to  a[\^2  +  log(\^2  +  l)] 

2.   Prove  that  the  length  of  the  cardioide  r  =  a{l  -  cos  6)  is  8a. 

§  56.  Volume  of  Solid,  whose  Cross-section  is  given. 

If  the  section  of  a  solid  by  planes  perpendicular  to  the  axis 
of  X  is  given  and  denoted  by  A,  the  volume  of  the  portion  of 
this  solid  cut  off  by  two  such  planes  may  be  obtained  by 
integration,  since  this  volume  is  readily  seen  to  be  "' 

x=xn 


or 


*  With  the  notation  of  §  49  we  have 

A8x<:dy<(A+dA)dx 
and  d\' 

ax 


AND  ITS  APPLICATIONS 


87 


As  a  special  case,  the  volume  of  such  a  portion  of  the  solid 
formed  by  the  revolution  of  the  curve  ij  =f(x)  about  the  axis  of 


o:  IS 


rr[f(x)fd.r, 


or 


-       i/cb; 


J    J-O 


and  for  revolution  about  the  axis  of  //,  we  have  in  the  same  way 


>n 


77 


oMy. 


yo 


Ex.  1.  The  portion  of  the  parabola  if=^ax  from  the  vertex  to  the  point 
P(a;,  y)  revolves  aljout  Ox.  Prove  that  the  volume  of  the  cup  we  thus  obtain 
is  2aTrx'. 

2.  Obtain  the  volume  of  a  sphere  by  considering  the  rotation  of  the 
semicircle  x^  +  y-  =  a^  aliout  O.v. 

3.  Find  the  volume  (i.)  of  aright  circular  cone  and  (ii.)  of  a  cone  in 
which  the  base  is  any  plane  figure  of  area  A,  and  the  perpendicular  from  the 
vertex  upon  the  base  is  h. 

4.  Prove  that  the  volume  of  a  spherical  cap  of  height  h  is  irh\r  -  ■^),  where 
r  is  the  radius  of  the  sphere. 

§  57.  Surface  of  Solid  of  Revolution. 

It  is  easy  to  show  that  the  surface  of  a  right  circular  cone 
whose  vertical  angle  is  2  a  and  whose 
generators  are  of  length  I  is  tt/- sin  a, 
and  we  can  deduce  from  this  that 
the  surface  of  the  slice  of  a  cone 
obtained  by  revolving  a  line  PQ 
about  Ox  is  equal  to 

27r .  PQ  .  NR, 
where   NR  is   the   ordinate  from 
the  middle  point  of  PQ. 

Suppose  then  that  an  arc  P^P^  of  the  curve  y=f{^')  rotates 
about  Ox,  the  area  of  the  surface  generated  by  P^P^  is  the 
limiting  value  of  the  sum  of  the  areas  of  the  surfaces  generated 
by  the  chords  into  which  we  suppose  this  arc  divided.  That  is, 
the  area  of  the  surface  generated  by  PqPi 


0 


N 
Fig.  17. 


1    + 


.  6x 


di/\  - 
do: 


.  dx, 


where  ?/=/(■'')• 


88  THE  DEFINITE  INTEGRAL 


n 


This  may  be  written   27r       yds,  by  changing  the  variable  from 

J    So 

X  to  s,  Avhere  s  is  the  length  of  the  arc  from  a  fixed  point  to  the 
point  (./•,  y). 

When  the  axis  of  revolution  is  the  axis  of  y,  we  obtain  in 

the  same  way  the  expression  27r  I     xds. 


Ex.   1.  Obtain  the  expression  for  the  surface  of  a  sphere  of  radius  a. 
Here  we  take  the  curve  y=  va-  -  x'^, 


and  the  surface      =47r|    s'a^-x^   '\/^  +  ~o' 

■I  0  y 

■,j   dx 


dx 

0  r 

a 
iira  I 

0 


2.  Prove  that  the  area  of  the  portion  of  a  sphere  cut  off  by  two  parallel 
planes  is  equal  to  tiie  area  which  they  cut  off  from  tlie  circumscribing  cylinder 
whose  generators  are  perpendicular  to  these  planes. 

3.  Prove  that  the  area  of  the  surface  formed  by  rotating  the  circle  of  radius 
a,  whose  centre  is  distant  d  from  the  axis  of  x,  about  that  axis  is  Att-cuI. 

§  58.  The  Centre  of  Gravity  of  a  Solid  Body. 
If  a  number  of  particles  of  masses  m^,  ?«.„   .  .  .  are  situated 
at  the  points  (x-^,  ?/j,  z^)  .   .   .  their  C.G.  is  given  by 

_  2(m^^)        _  2(r/? ,.//,)     .  _  S(m^g^) 

and  as  we  may  suppose  a  continuous  solid  l)ody  broken  up  into 
small  elements  of  mass  8711  whose  centres  are  (x,  y,  z),  we  may 
write  these  results  for  a  solid  body  in  the  form 

""= — M — '  y= — j.r— '  '= — M — 

In  many  cases  we  can  transform  these  expressions  into 
integrals  which  we  can  evaluate  by  the  methods  already 
employed,  though  in  general  they  involve  integration  with 
regard  to  more  than  one  variable,  and  these  cannot  be  dis- 
cussed here. 


AND  ITS  APPLICATIONS 


89 


We  add  some  illustrative  examples  : — 

Ex.  1.  The  Centre  of  Gravity  of  a  Semi-circular  Plate. 

Take  the  boundary  of  the  plate  along  the  axis  of  y,  and  suppose  the 
semicircle  divided  bj'  a  set  of  lines  parallel 
to  that  axis  and  very  near  one  another.  The 
C.G.  of  each  of  these  strips  PQ'  lies  on  the 
axis  of  X,  and  therefore  the  C.G.  of  the  semi- 
circle lies  on  0./;. 


We  thus  have 


X—- 


2/  xydx 

J  0 


ira- 
~2" 


4  r    

=  — 9  I    X  Ja^  -  X? .  dx 

-'  0 

[-i(«-.^)'T 


_4^ 

TTff 

4a 


OTT  Fig.  is. 

and  */  =  0. 

2.  The  Centre  of  Gravity  of  a  uniform  Solid  Hemisphere. 
Let  the  axis  of  .'■  be  the  radius  to  the  pole  of  the  hemisphere,  and  suppose 

the  solid  divided  up  into  thin  slices  by  a 
set  of  planes  perpendicular  to  this  axis. 

Then  the  C.G.  of  each  of  these  slices 
lies  on  this  axis,  and  therefore  the  C.G. 
of  the  hemisphere  does  so  also. 
Then 


I    xyHx 
J  ft 


•■_•'  0 


-  7r«' 
3 


.  3 

x  =  -a 
3 


90 


THE  DEFINITE  INTEGRAL 


3.  Prove  that  the  C.G.  of  any  cone  or  pyramid  upon  a  plane  base  is  one 
fourth  of  the  way  up  the  line  from  the  vertex  to  the  C.G.  of  the  base. 

4.  Prove  that  the  C.G.  of  the  upper  portion  of  the  ellipse  —+%  =  l  is  at 


a'  '  62- 


■ib 
the  point  (  0,  -- 

'  OTT 


§  59.  Moments  of  Inertia. 

The  moment  of  inertia,  I,  of  a  set  of  particles  ?n^,  m.-,,  .... 
with  respect  to  an  axis  from  which  they  are  distant  i\,  ?•<,,  etc.,  is 
the  expression 

m-^r^"  +  m.^r.-,'  +  .   .   .  . 

and  in  the  case  of  a  continuous  solid  body  we  may  express  this  as 

I  =  Ltsm=o  ^r-8m. 

The  radius  of  gyration  k  is  defined  by  the  equation 

I  =  M/;2. 

In  many  cases  we  may  obtain  the  values  of  I  and  F  by  the 
use  of  the  methods  of  integration  we  have  been  discussing. 
We  add  some  illustrative  examples. 

Ex.  1.  To  find  the  radius  of  gyration  of  a  thin  rod  of  mass  M  and  length 
21,  about  an  axis  at  right  angles  to  the  rod  and  passing  through  its  centre. 

Here 

I  =  i/<5,„  _  0  ^^^  •  ^^' 

=  p  I      x-dx, 

-  -1 
where  2Ip  =  'M 

=  2/3  /  x'^dx 

^  2 

_M.P 
3  • 

2.  To  find  the  moment  of  inertia  of  a  solid  circular  cylinder  about  its 
axis. 

Here  I  =  Lf^y^-Q  2r^5?n, 

where        din  =  ph  {7r(?'  +  8r)-  -  wr-\ 

=  irph{2r8r+{dr)-},  where  p  is  the  vol.  density. 


A- 


0 


Fig.  20. 


AND  ITS  APPLICATIONS  91 

Therefore  I  =  ivph  I  ?•- .  2 

ra 

=  2Tr ph  I   r 

•^     it 


'2rdr 

(1 


r^dr 

0 


But  7rpA«2  =  M; 

■  ■■    i=mJ' 


3.   Prove  that  the  radius  of  gyration  of  a  thin  circular  plate  of  radius  a. 


about  a  diameter  as  axis  is  -  «-. 

4 


EXAMPLES  ON  CHAPTER  VIII 

1.  Find  the  areas  bounded  by 
(i. )  2/  =  sin  2a3,  a;  =  0,  x=  -. 

(ii. )  y  =  e~^  sin  1x,  a;  =  0,  .r  =  -. 

(iii.)  The  hyperbola  onj  =  a?,  x  =  x\,  x  =  x^. 
(iv.)  y  =  x^,  a;  =  0,  :/;  =  4. 
(v.)  2/  =  2a-^,  the  axis  of  y,  and  the  lines  7/  =  2  and  y=^i. 

2.  Find  the  area  of  the  part  of  the  parabola  ii  —  x--Zx  +  2  ci;t  off  by  the 

X  axis.     What  does  /  ydx  here  represent  ? 

•^  0 

3.  Trace  the  parabola  (?/  -  aj  -  3)-  =  a;  +  ?/,  and  find  the  area  of  the  part  of  the 
curve  cut  off  by  the  lines  x  —  0  and  cC  =  4i. 

4.  Find  the  areas  in  polar  co-ordinates  of 

(i.)  The  part  of  r  =  a^  included  between  ^  =  0  and  d  =  2Tr  ; 
(ii. )  A  loop  of  each  of  the  curves  ?-  =  a  sin  Id,  a  sin  2>d,  etc. ; 
(iii.)  A  loop  of  each  of  the  curves  r  =  a  cos  26,  a  cos  3^,  etc. ; 
(iv.)  The  part  of  the  hyperbola  r- sin  ^  cos  ^  =  a'^  included  between  9  =  di 
and  0  =  6.2  > 

(v.)  A  sector  of  the  ellipse  -^  +  ^  =  1  and  of  the  hyperbola  —2-fo  —  '^,  the 

centre  being  the  pole. 

(vi. )  Prove  that  the  area  between  the  two  parabolas  y'^  =  ^ax  and  x^=iay  is 
16ft- 
3 


92  THE  DEFINITE  INTEGRAL 

(vii.)  Prove  that  the  area  between  the  two  ellipses  ^,  +  ^  =  1  and  ^  +  '^=1 

is  4aJ  tan~^-. 
a 

5.  By  substituting  x -a  cos,  6,  7j  =  b  ain  9,  show  that  the  [lerimeter  of  the 

ellipse  of  semiaxes  a,  b  is  given  by  4a  P  ^/l  -  c-  sin-^ .  dd,  and  deduce  that  for 

-  0 

an  ellipse  of  small  eccentricity  the  perimeter  is  apjiroximately  2ira  (  1  -  - 

6.  Find  the  lengths  of  the  following  curves  : — 
(i.)    The  equiangular  spiral  r  =  ae^ '^°*  "  from  d  =  <)  to  d  =  2w  \ 
(ii.)  The  spiral  of  Archimedes  r  =  ad  from  ^  =  0  to  ^  =  27r  ; 

X  X 

(iii. )  The  catenary  y  =  '~^(e"  +  e    "j  from  a;  =  0  to  a-  =  a  ; 

(iv. )  And  show  that  the  length  of  a  complete  undulation  of  the  curve 

II  — b  sin  - 
■^  a 


is  equal  to  the  perimeter  of  an  ellipse  whose  axes  are  2n'«-  +  6^  and  la. 

7.  Find  the  volumes  of  the  following  solids  : — 

(i.)  The  solid  formed  by  revolving  the  jjart  of  the  line  rc  +  i/=l  cut  off  by 
the  axes,  about  the  axis  of  x,  and  verify  your  result  by  finding  tlie  volume  of 
the  cone  in  the  usual  way  ; 

(ii.)  The  spheroid  formed  by  rotating  the  ellipse  9a:-+16?/'^  =  144:  about  tlie 
axis  of  X  ; 

(iii.)  The  cup  formed  by  the  revolution  of  a  quadrant  of  a  circle  about  the 
tangent  at  the  end  of  one  of  its  bounding  radii ; 

(iv.)  The  cup  of  height  h  formed  by  the  revolution  of  the  curve  a^y  —  u? 
about  the  axis  of  y  ; 

(v.)  The  ring  formed  by  the  revolution  of  the  circle  {x-a)~  +  y-=b^  about 
the  axis  of  y  ; 

^2  y2  ;~2 

(vi.)  The  ellipsoid  -2+t2+-2==1. 

And  show  that  if  Sg,  Sj,  S^  are  the  areas  of  three  parallel  sections  of  a  sphere 
at  equal  distances  a,  the  volume  included  between  Sq,  S,  and  the  spherical 

boundary  is  -  (S0  +  4S1  +  S2). 

8.  The  ellipse  whose  eccentricity  is  e  rotates  about  its  major  axis.  Prove 
that  the  area  of  the  surface  of  the  prolate  spheroid  thus  formed  is 

27r6(&  +  -sin-^c). 

X        _x 

9.  The  catenary  2/  =  -  f  (;"  +  g    "  j  rotates  about  the  axis  of?/ ;  prove  that  the 


AND  ITS  APPLICATIONS  93 

area  of  the  surface  of  the  cup  formed  by  the  part  of  the  curve  from  a  =  0  to 

r 


a;  =  a  is  2Tra-     1 

\       ^ 

10.  The  cardioide  ?-  =  a(l  -  cos  0)  revolves  about  the  initial  line  ;  prove  that 

32 
the  surface  of  the  solid  thus  formed  is  -r-  tto^. 

0 

11.  Find  the  C.G.  of  the  following  :— 

(i.)  A  thin  straight  rod  of  length  I  in  which  the  density  varies  as  the 
distance  from  one  end. 

(ii.)  An  arc  of  a  circle  of  radius  a  which  subtends  an  angle  2a  at  the  centre. 

o  o 

(iii.)  A  quadrant  of  the  ellipse  —,  +  '-jT,=  1- 

(iv.)  A  circular  sector  as  in  (ii.) 

(v.)  The  segment  of  the  sector  of  (iv.)  bounded  by  the  arc  and  its  chord. 

(vi. )  A  thin  hemispherical  shell  of  radius  a. 

12.  Find  the  moments  of  inertia  of  each  of  the  following  :  — 

(i.)  A  thin  straight  rod,  about  an  axis  through  an  end,  perpendicular  to 
its  length. 

(ii. )  A  fine  circular  wire  of  radius  a,  about  a  diameter, 
(iii.)  A  circular  disc  of  radius  a,  about  an  axis  through  its  centre  perpen- 
dicular to  the  plane  of  the  disc. 

(iv.)  A  hallow  circular  cylinder  of  radii  a,  b  and  height  h,  about  its  axis, 
(v.)  A  sphere  of  radius  a,  about  a  tangent  line. 

(vi.)  (a)  A  rectangle  whose  sides  are  2«and  2b,  about  an  axis  through  its 
centre  in  its  plane  perpendicular  to  the  side  2a  ; 

(/3)  about  an  axis  through  its  centre  perpendicular  to  its  plane, 
(vii.)  An  ellipse  whose  axes  are  2a  and  2b, 
(a)  about  the  major  axis  a  ; 
{j3)  about  the  minor  axis  b  ; 

(7)  about  an  axis  perpendicular  to  its  plane  through  the  centre. 
iV.5.— The  case  of  the  circle  follows  on  putting  a  =  b. 
(viii.)  An  ellipsoid,  semiaxes  a,  b,  c,  about  the  axis  a. 
JS\  B. — For  the  sphere  a  =  b  =  c. 

(ix.)  A  right  solid  whose  sides  are  2a,  2b,  2c,  about  an  axis  through  its 
centre  perpendicular  to  the  plane  containing  the  sides  b  and  c. 

A^.^.— Routh's    Rule    for   these  last  four  important   cases   can  be   easily 
remembered  : — 

/  sum  of  squares  of  perpendicular  \ 

Moment  of  Inertia  about  an  axis\  _  \ semiaxes / 

'  of  symmetry  ^ -mass  3,  4,  or  5 

The  deno7ninator  is  to  be  3,  4,  or  5  according  as  the  body  is  rectangular, 
elliptical,  or  ellipsoidal. 

Cf.  Routh's  Eigid  Dyna.mics,  vol.  i.  p.  6. 


ANSWERS 


CHAPTER  I.   (p.  12) 

1.  (i.)     x^-\-f-='^^.  (ii.)  ..-■=!^^. 

(iii. )  ar*  +  2.«Y  +  y*  +  2a'^{y'^  -x-)  +  a*  -  c^  =  0. 

2.  x'  +  4j/-ll  =  0. 
13     19^ 


^-    •       11'    11 

4.  The  parallel  lines  through  0  are 

3a'-2?/=:z0,  ix  +  y^Q,  19;/;+13j/  =  0. 
The  perpendicular  lines  through  0  are 

2a'  +  3i/  =  0,  a;-42/  =  0,  13^'-19?/  =  0. 
The  parallels  through  (2 .  2)  are 

3.«-2!/  =  2,  4a;  +  2/  =  10,  19.i'  +  13?/  =  64. 
The  perpendiculars  through  (2 .  2)  are 

2./'  +  3?/=10,  ;(;-47/  +  6  =  0,  IS.-.-- 19y+ 12  =  0. 

5.  a;  +  3//-7  =  0. 

6.  7a; +  7?/ -36  =  0  is  the  bisector  of  the  acute  angle. 

a; -y-  12  =  0  is  the  liisector  of  the  obtuse  angle. 

7.  (i.)  (1.2),         (3,  4),         (5,  3). 

Si.)  I  -3,  I 

(iii.)  The  internal  bisectors  are 
x-y+1  _-x-\-iy-7     x-y  +  l_-x-2ij  +  \l     x-  4y  +  7_.>J  +  2y- 11 
\J2  s'l7       '        n'2  VF        '        n'17  ^5 

The  external  bisectors  are 
x-y+l  _x-iy+7     x  ~y+l  _x-{-2y -11     x  -iy  +  T  _  -  x  -  2y  +  11 
n/2     ~      \'l7     '         \/2     ~        V5       '         v^r7     ~  Jl 

8.  If  the  points  (0,  0),  (2,  4),  (-6,  8)  be  called  A,  B,  C  respectively,  the 
equation  to 

(i.)  BO  is     a' +  2?/ -10  =  0, 

to  CA  is  4a3+32/=0,  * 

to  AB  is  2x-y  =  0. 

(ii.)     tan  A  =  2,  tanB  =  oo,  tan  C  =  -- 

95 


96  INFINITESIMAL  CALCULUS 

(iii.)   Median  through  A  is  y  +  8x~0, 

Median  through  Bis  ?/  -  4  =  0, 

Median  through  C  is  6.>'  +  7y~  20  =  0. 
(iv.)  The  perpendicular  from  A  on  BC  is  the  line  AB  ;  its  length  is  2  ^'5. 
The  perpendicular  from  B  on  CA  is  the  line  3x-iy+ll  =  0;  its 

length  is  4. 
The  perpendicular  from  G  on  AB  is  the  line  CB  ;  its  length  is 


4  ^,'5. 

(V.) 

x  +  2y  =  0, 

4a; +  3?/ -20  =  0, 

2x-y  +  20-0. 

(vi.) 

4 

(vii.) 

/- 2(3-^/5)     2(4+ v5) 
^     3  +  V5            3+^5 

(-3,  4),  (  -1.4 


CHAPTER    II.   (p.  23) 

4.  y-9x+\6  =  0. 

6.  u-gt;    -(J. 

7.  2Tn-h5r. 

8.  5V  =  47rr25r,         50-27,         502-66. 

The  proportional  errors  are  1  :  1607r  :  16007r. 

9.  (a  +  2U)         8l  =  {a  +  2bt)SL 

12.  — 7=  feet  per  second. 

\^3 

CHAPTER   III.    (p.  31) 
dy^B{x-inx  +  l) 


d 


X 


s 


2?;^ 


...  ,  dy  a-x 


f'.^'     \/2ax-x^' 

,...  .  dy  2(z  +  3 

(111-)  31.= 


(^a-     2v'(a;+l)  (a;+2) 

3^=(x  +  a)i^- 
dx 

dy  1 


(iv.)  ^=(x  +  a)i^-i(a;+i)''-i(y/  +  f/).;f  +  ^a+;ji. 


(v.)    ,    - 

dx     {l-x)\/\-x^ 

(vi.)  ^~^yi.i{qa-pb  +  {p-q)x). 

,  ..  .     ^   ,  {b(n-m):rf"  +  na) 

(vn.)  .>'"-i — -. 

{Ox'"  +  uj- 

(viii.)  7/(?u"-i(H-Jc" )"'-!. 


(ix.) 


\/x*-a* 


ANSWERS  97 

(x. )    - x{(x-  +  a^) -i  +  (a;2 - a^) " ^}- 
.   .  .         3.x,'-' 
(^1-)  Ti' 

(Xll.) -3- 

{l+x  +  x^)^{l-x  +  x^)^- 

2/0 

(ii.)    --«. 
2/0 

(lU.       +-:3— • 
«"2/o 

(iv.)   -■^. 

ii'O 

4.  7 '96  miles  per  hour. 

5.  8  miles  per  hour  ;    4  miles  per  hour. 

'   dv  V 

9.  When  the  pressure  decreases,  the  volume  increases,  and  conversely. 

CHAPTER   IV.    (p.   38) 

1.   (i. )  3  sin  a;  cos  a;(sin  a;  -  cos  cc). 

(ii. )  sec  *x. 

....  .   4  sin  a; 
(in.) 

(iv.) 

(V.) 

^'^^•^  (l  +  cosxf 

3.  (i. )  x^-\m  sin  (a;")  +  «,<;"  cos  (a;»)]. 
(ii. )  x"^~\tn  cos  (a;")  -  nx'^  sin  (a;")]. 

(iii. )  af^-\m  tan  (.«")  +  ?ia;"  sec  ^(.x")]. 

4.  (i.)  2ajtan-^a'. 
(ii.)  sin  ~'a'. 

1 


cos 

^x' 

-4 

cos  a; 

sin  '^x 

•2. 

cos  a; 

(1- 

sin  x)"^ 

2 

sin  a; 

(iii.) 


2^x{\+x) 

^^^■'  i  +  Zx^  +  x'' 


2(1 +a,''^) 

5.  rtw  sin  w/,  aus' cos  oit. 

6.  x  =  2aw  cos"  —  ;  y-=aw  sin  a;<. 
Jc=  -  aoo"  sin  w^  ;   ij  —  cuxj^  cos  w^. 

The  direction  of  motion  at  time  t  makes  an  angle  -^  with  tlie  axis  of  x. 
8 


98  INFINITESIMAL  CALCULUS 

CHAPTER  V.    (p.   50) 

1.  (i.)  e'(l+,r).         (ii.)  x"'-h"^{m  +  nx).         (iii.)  {a  +  be  +  cax)e'^+<'. 

(iv.)  e''^'''~^^( sm-h'.-r—;^=^]. 
^      '  \  Vl-W 

2.  (i.)2a'ci+^.         (ii.)  2.i'e«^"(l+aa;2).         (iii.)  «'"-^e''^''(m  +  Ma«"). 
(iv. )  a-™-^a^"('»i  +  ?ia;"  log  a). 

3.  (i.)x"-(l+mlog.).     (ii.)^^^i~-      (iii-)  2;^. 

-6a;  ^/x'^+l+a-  .  1 

^^^•^l-a=2)(4-a;2)-     ^^-^    a;x/^;vr"     ^"^''^l -a;)  Vi" 
,       ...  4a;-3  ....         a^  .....    2-5a; 


2V(2a;+l)(a;-2)'  (a2  +  a;2)f'  ■V(a;-1)''' 

(iv.)  .7:^(1+ log  a;). 

(^•) '  ..»»+L^ (^1-)     log—-- -^       1+    ^ 


cos'^+^Tia;  ^    ''   \     ^     X       x  +  1 


X 


11.   (i.)  tan  a. 

(ii. )  tan  n0. 

(iii.)  -cotnd. 

(iv. )  cot  n6. 

(v.)  -tan  n9. 

r-r-  is  the  tangent  of  the  angle  between  the  radius  vector  to  the  point 
(r,  Q),  and  the  tangent  to  the  curve  at  that  point. 


13. 


(i.)  g=(3a--l)(a;-l)  .  Max.  at  Q,  ^. 

llin.  at  (1,  0). 

(ii.)  V^  =  a;(5a;-2)(a;-l)2  .  Max.  at  origin. 

Min.  at  ("4,  -03456). 

(iii.)  ^==2(a;-l)(a;-2)(2a;-3)  .   Min.  at  (1,  0)  ;  (2,  0). 

Max.  at  (I  ^ 

^^''•)£  =  ^"|2-Max.at(-L   -1). 
Min.  at  (1,  3). 

(v.)  $  =  2t-£^-^^.  Max.  at(-l,  3). 


Min.  at  (  1 


'  3y" 


Min.  at  (1-4,   --06)  nearly. 


ANSWERS  99 

dx  (.r-l)V-'-2)2 


(vii.)  J-  -/,^"!'-,^|^fj2  •  Min.  at  (  -  -9,  -16)  nearly 


Max.  at  (1-4,  18-2)  nearly. 
(""•)  7ir='jt-Wi^-i?  ^"^  *"^'°^"S  points. 

IX.)  -f-=     ,      -TTij—  .  Max.  at  (l-o,  '1)  nearly. 
dx       {x  -\y 

'\l\\\.  at  (6-45,  9-9)  nearly. 
(X.)  '^  =  ^-'1.  .  Min.  at  (1-26,  1-89)  nearly. 

,.,  4'. 
<"■)  I 

....  ,   .   R^- 

(ill.)   op  =  ^^ov. 

(iv.)  Sv^—8t. 
P 

,     ,        ^  R(H-a<)^   aK^, 

(v.)   5»=  -  5^-i — -Iv^ — U. 


EXAMPLES  ON  THE  PARABOLA  (p.  55) 


(1) 

(2) 

(3) 

2. 

Foci 

(— !> 

(-2,   -2), 

H) 

Vertices 

(-2,   -1*, 

(-2,   -3), 

i-H 

Latera  recta 

3 

2/= -2, 

x  =  0. 

Lengths  of  recta 

1, 

4, 

1. 

Axes 

if  =  -  2, 

x=  -2, 

1 

Tangents  at  vertices 

y=-h 

2/= -3, 

1 
^■=-4' 

.3. 

-5.     7. 

5. 

(1, 

2),                 (; 

a 

2fA 

6. 

x-y 

-1  =  0, 

x  +  y-3=^0. 

( . 

x-y 

+  a  =  0, 

x  +  y-3a  —  0. 

x  +  y  +  a  —  Q, 

x-y  -  3«  =  0. 

8  a 


100  INFINITESIMAL  CALCULUS 

EXAMPLES  ON  THE  ELLIPSE  (p.  59) 

1.  The  foci,  extremities  of  the  axes,  length  of  latus  rectum,   and  eccen- 
tiicity  are  for 

(i.)[±1.0],     [±2.0],     [0+N%     3,     I 

(ii.)[2.2],     [0.2],     [3.2],    [-1,2],    [1,2+^/3],    [1,2-^^3],     3,    ~. 
(ill.)  [±  ^/3,  1],     [±2,1],     [0.2],     [0.0],     ^,     ^. 
(iv.)  [0±1],     [.)±2],     [±v'3.0],     3,     1 

EXAMPLES  ON  THE  HYPERBOLA  (p.  62) 

1.  (i.)  (±v'7,  0):(±2,  0)  :3:^. 

(ii.)  (1  ±  v'7,  2)  :  (3,  2):(-l,  2):3:^. 

(iii.)  (0,    -  1  ±  V5)  :  (0,  0)  :  (0,    -  2)  :  S  :   ^'5. 

(iv.)  (±n'7,  0)  :(±V3,  0):i|^:  -^-|\ 

2.  (i.)  (±2^2,   ±2\/2)  :  (±2,   ±2). 
(ii.)  (±2^/2,   +2x/2):(  +  2,   +2). 

CHAPTER  VIL   (p.  73) 

1.  ,.  ,(a;-a)*     2sJax'-^'b     2    ,-,„       ^ 

(1-)  —i~  '-^-a =  3  V.^'(3  +  a:)  :  «-log(a;  +  3). 

,..  ,   ,         X        .      {x~2f     (x-lf      2  -i/2,7-+l\ 

(iii.)  sin-i(2a;-l);  2  Vcc'^- 3.7J  +  2  +  2  log  (.r-^+ Va;—3a.-  +  2)  ; 
V(a;2  +  .'•  +  1)  +  ^  log  ('a;  +  ^  +  \/x^  +  .r  +  l  \ 

2.  a,-.sin-b  +  v^r^'';  '^ts^n'^x-^.  x^  +  ^log{l+x')  ■  cos4c>/m^')  + 

sm  ix .  -^  ; 
o 

/9,7;--2\    .     „       2x  .^™+i  .r'«+i 


ANSWERS  101 


3-    ;t  log    , — ——2    +  ^5  tau 


'■     -2 


5.    log 


2a;-l     4     ^  \.r-l, 

(a; -3)2 


a;-2 


6.    (i.)2(l+,)»{|-A}.  (ii.)log-^| 


Va;  + 1  -  1 


Vx  + 1  + 1 


8.    log  tan  -.        log  tan      ^     .        —77:  log  tan     ~  + 


1  —  1  •,      2  sec  X  - 1 

-log(atan^+  ^Han^^  +  n  4l°g2sec^-+ l' 

f       dx  2._,fl.x 

[^^^^  =  1  tan- fa  tan:; 
j5-4cosa;3  \  2 


/cfa'        _  1 , 
4  +  5cosa;~3  °^ 

j  4  -  5  cos  a;    3     ^ 


,7' 

3  +  tan  ^ 
3  -  tan  - 


X 

1  +  3  tan  2 

1  -  3  tan  - 
2 


f_^_=   2    tan-\/ltanf'|-'^y 
j  3  +  2sina;     ^5  V  5        \2     ^j 

/"       cgx        _   2  /^).     ^\ 

J3-2sina;-V!*^''"'^^*^^i2~4J- 

i       dx       ^2^^     v/5  +  tan(|-^) 

J  2  +  3  sin  a;     ,^5     °     ,-  /a;    7r\ 

v5-tan\^2~  4 

i  2  -  3  sin  a; 


/-        /  a;     TT 

_^     ^l+v^5tan(^2"4 

v/5     *  ,-        (x     V 

1  +  v5  tan  I  9  ~  T 

10  1        2a    •    a  ,  2    .     a  cos  3^  sin  ^     3         „    •     /I     3 

12.  5  cos  2^  sin  ^  +  -  sin  ^ .  ^ +  t  cos  ^  sin  ^  +  k  ' 

o  3  4  4  8 


^"  „;.    ^^  _,_    "     .,„-!  .„„  „„^      «(?l^  Ln-2  , 


15.  —  sin  mx  -\ — r,  a'""^  cos  mx  — ^ — ^ — -  \  a;"~-  cos  mxdx. 

m  m~  m- 


102  INFINITESIMAL  CALCULUS 

CHAPTER  VIII.    (p.  91) 

1.     (i.)  1. 

(ii.)  jlye    •■^  +  1 

(iii.)  a-  log  -. 
(iv.)  64. 

(v.)  3f2§-J 


2.  -:  the  difference  between  the  area  bounded  by  the  rc-axis,  the  //-axis 

and  the  curve,  and  the  area  which  lies  on  the  negative  side  of  the  aaxis. 
o    343 
^-   l2'- 

4.      (i.)^-^^ 

....   7r«-         TTrt'-^         7ra- 

("•^  ^;    T^'     4,r 

....  .   TTtt"         TTrt'^         ira? 

o  1-  4'/6 

,.     .     o  1      tan  p-7 

(iv. )  fr  log  , -". 

^      '  '=  tan  6-^ 

(y  \  —  tan-i  ^^  ^^'^^  ^o^an^) 

ah  .  ^^  {b  +  a  tan  O^)  (b  -  a  tan  9^) 
4      °  {b  +  a  tan  ^J  (6  -  «  tan  ^2) ' 

,.         /.   ■!  /  2  TT  cot  a      , , 

0.      (1.)  a  sec  a  (c  -1). 

(ii.)  ^('(27rv'r+4^+log  (27r  + \/r+45f-)Y 
(iii.)|(€-0. 

(ii.)  487r. 

.....    57r«*     ir'^ci? 

(iv.)  '-  irh^a^. 

(v.)  -laV-Tr-. 

(vi.)  -  7ra6c. 
o 

2 
11.     (i.)  ,-.-:  from  that  end. 
•J 

(ii.)  On  the  radius  bisecting  the  arc  at  a  distance  from  the 

centre. 


ANSWERS  103 

(ni.)  x=—,     y=-^- 

TV  OTT 

,.  ^  2a  sin  a   . 

(iv.)  On  the  radius  bisecting  the  sector  at  a  distance  — trora 

o        a 

the  centre. 

O  SlU    OL 

(v.)  On    the    bisector  of  the  chord  at  a   distance  ^a -. 

^    '  3     a-  sm  a  cos  a 

from  the  centre, 
(vi.)  The  middle  point  of  the  radius  perpendicular  to  the  base. 

12.     (i.)  I  M~^  .  (rod  of  length  '2z). 

(ii.)  ~  Ma^-. 

(iii.)  ~Ma2. 

(iv.)  ^^{a^  +  b% 

(v.)  ^Ma2. 


(VI.)  (a)-g-:(/3)M(^— g— j. 
(vii.)  (a)M|':(/3)M~:(7)M(^ 
(viii.)M(^^). 
(i.)M(-±^). 


4 


THE   END 


Of 


Printed  by  R.  &  R.  Clark,  Limited,  Edinburgh. 


THIS  BOOK  IS  DUE  ON  THE  LAST  DATE 
STAMPED  BELOW 

AN  INITIAL  FINE  OP  25  CENTS 

W.UU  .NCREASE  TO  SO  CENTS  ON  THE  FOUR^;^ 

SCekoue.  '°   *'°°   ^'^  ™^  seventS^oIv 


.^^,;Nci 


-MAY^-124935-_ 


-Am-24r-493g- 


tODeo'OTir 


^^^^1-^0-753^- 


^^KTDXD^ 


J1££L_5_ 


-^ 


— EEE__2IL\93a 


TCcr:gB"7^39 


r.,oC. 


^Cl 


IMugHM 


COLD 


-48&^ 


LD  21-100to-8,'34 


^■■\: 


kr^'* 


(^ 


208 


p:o 


;■'■'■■ 

ii^i.',*  •^'?  .' 


-•r-    .■■■-■:■*-■■  ■      -■  - 


m-.