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MULTILINEAR  FUNCTIONS 
OF  DIRECTION 


641 


MULTILINEAR  FUNCTIONS 
OF  DIRECTION 


CAMBRIDGE  UNIVERSITY  PRESS 

C.  F.  CLAY,  MANAGER 
LONDON   :  FETTER  LANE,  E.G.  4 


NEW  YORK  :  THE  MACMILLAN  CO. 

BOMBAY       \ 

CALCUTTA  I  MACMILLAN  AND  CO.,  LTD. 

MADRAS       j 

TORONTO    :   THE  MACMILLAN  CO.   OF 

CANADA,  LTD. 
TOKYO :  MARUZEN-KABUSHIKI-KAISHA 


ALL  RIGHTS  RESERVED 


MULT     ^INEAR  FUNGI  IONS 


OF    DIRECT  ION 


AND  THEIR  USES  IN  DIFFERENTIAL  GEOMETRY 


BY 


ERIC  HAROLD  NEVILLE 


LATE  FELLOW  OF  TRINITY  COLKHfE,  CAMBRIDGE 
PROFESSOR  OF  MATHEMATICS  IN  UNIVERSITY  COLLEGE,  READING 


CAMBRIDGE 

AT  THE  UNIVERSITY  PRESS 
1921 


PREFACE 

rjlHE  distinctive  feature  of  this  work  is  that  the  functions  dis- 
J-  cussed  are  primarily  not  functions  of  a  single  variable  direction 
but  functions  of  several  independent  directions.  Functions  of  a 
single  direction  emerge  when  the  directions  originally  independent 
become  related,  and  a  large  number  of  elementary  theorems  of 
differential  geometry  express  in  different  terms  a  few  properties 
of  a  few  simple  functions ;  since  one  of  the  objects  of  the  essay  is 
to  emphasise  the  coordinating  power  of  the  theory,  the  presence  of 
many  results  with  which  every  reader  will  be  thoroughly  familiar 
calls  for  no  apology. 

In  the  applications  to  the  geometry  of  a  single  surface  two 
functions  thought  to  be  new  are  described.  The  first,  studied  in 
Section  4,  depends  on  two  tangential  directions,  reduces  to  normal 
curvature  when  these  directions  coincide,  and  is  called  here  bilinear 
curvature.  I  became  acquainted  with  this  function  in  1911  and  used 
it  in  lectures  early  in  1914.  The  second,  the  subject  of  Section  6, 
depends  on  three  directions,  and  reduces  to  the  cubic  function  as- 
sociated with  the  name  of  Laguerre ;  the  function  is  symmetrical, 
and  because  the  equations  of  Codazzi  can  be  read  as  asserting  its 
symmetry  I  have  called  the  general  function  the  Codazzi  function. 

The  theory  of  multilinear  functions  does  not  merely  coordinate. 
It  affords  simple  proofs  of  the  relations  between  the  cubic  functions 
of  Laguerre  and  Darboux  (6'231,  6'234)  and  of  formulae  (7'242, 
7*351,  7*352)  for  the  twist  of  a  family  of  surfaces,  and  it  leads 
naturally  to  expressions  (7 '241)  for  the  rates  of  change  of  the  two 
principal  curvatures  of  a  variable  member  of  a  family  of  surfaces  at 
the  current  point  of  an  orthogonal  trajectory  of  the  family,  expres- 
sions that  are  interesting  because  their  existence  was  deduced  by 
Forsyth  in  1903  from  an  enumeration  of  invariants. 

E.  H.  N. 

June,  1920. 


NOTE 

For  the  sake  of  brevity,  the  space  considered  is  real,  but  the 
restriction  operates  only  to  the  same  extent  as  in  other  branches 
of  differential  geometry.  If  it  is  removed,  the  intrinsic  distinction 
between  the  positive  square  root  and  the  negative  square  root  of 
a  given  uniform  function  has  to  be  replaced  by  a  more  artificial 
distinction  based  on  a  dissection  that  is  to  some  extent  arbitrary. 
And  there  is  always  a  possibility  that  results  need  modification 
if  isotropic  lines  or  planes  are  involved ;  as  a  rule,  nul  vectors  are 
admissible  as  arguments  but  nul  directions  are  not. 


CONTENTS 

PAGE 

PREFACE .  5 

NOTE 6 

TABLE  OF  CONTENTS 7 

PRELIMINARY  PARAGRAPHS 9 

O'l  Vectors ;  radials. 

0'2  The  projected  product  of  two  vectors. 

0'3  Vector  frames. 

0'4  Cartesian  axes. 

0'5  Directions  in  a  plane. 

0*6  Angular  differentiation. 

1.  LINEAR  AND  MULTILINEAR  FUNCTIONS     ....       13 

1*1    Definitions  of  linear  and  multilinear  functions. 

1'2   Notation  for  multilinear  functions. 

1'3   The  core  of  a  multilinear  function. 

14   The  use  of  reference  frames. 

1*5   The  source  of  a  linear  function  ;  the  projected  product  of  two  cores. 

1'6  The  derivative  of  a  variable  core  ;  the  rate  of  change  of  a  multi- 
linear function. 

1'7  The  gradient  of  a  multilinear  function  dependent  on  position  in 
space ;  the  rate  of  change  of  such  a  function  along  a  curve. 

1/8   The  angular  derivatives  of  a  multilinear  function. 

2.  FUNDAMENTAL  NOTIONS  IN  THE  KINEMATICAL  GEO- 
METRY OF  SURFACES  AND  FAMILIES  OF  SURFACES      .      22 
2'0   The  vectors  to  be  examined. 

2-l    Normal  curvature  and  geodesic  torsion. 

2 '2   Geodesic  curvature. 

2 '3  Bilinear  curvature  ;  the  relations  of  bilinear  curvature  to  normal 
curvature  and  geodesic  torsion. 

2'4   Swerve ;  geodesic  curvature  as  a  swerve. 

2 '5   The  curvature  and  torsion  of  a  curve  on  a  surface. 

2  6   The  vectors  connected  with  a  family  of  surfaces. 

2'7  The  swing  of  a  tangential  direction  about  the  orthogonal  trajec- 
tory of  a  family ;  the  twist  of  a  family ;  the  spread  of  a  family  in 
a  tangential  direction. 

2 '8   The  swing  and  the  spread  as  spins  of  a  frame. 

3.  SURFACES  AND  MULTILINEAR  FUNCTIONS  ASSOCIATED 
WITH  A  FUNCTION  OF  POSITION  IN  SPACE       ...      31 
31    The  surfaces  denned  by  a  scalar  function  of  position. 

3*2   Definition  of  the  linear  rate  of  change  of  a  function  <£ ;  the  gradient 

and  the  slope  of  4>. 

3'3   Definition  of  the  bilinear  rate  of  change  of  the  function  <£. 
3*4   Definition  of  the  multilinear  rates  of  change  of  $  ;  the  symmetry 

of  these  functions. 
3*5   Evaluation  of  the  linear  function  <£Tr  of  an  arbitrary  vector  r 


8 

PAGE 

4.  THE  BILINEAR  CURVATURE  OF  A  SURFACE     ...      35 

4'1  Deductions  from  the  bilinearity  of  the  bilinear  curvature ;  Dupin's 
theorem  ;  the  mean  curvature  of  a  surface  at  a  point. 

4 -2  The  bilinear  curvature  of  a  4>-surface ;  the  symmetry  of  the  bi- 
linear curvature ;  particular  theorems  implying  this  symmetry. 

4 '3   Geodesic  torsion  and  bilinear  torsion  ;  angular  derivatives. 

4'4  The  principal  curvatures  and  directions  of  a  surface  at  a  point, 
the  amplitude  of  curvature ;  lines  of  curvature. 

4-5  Asymptotic  directions  and  torsions  ;  Enneper's  theorem  ;  asymp- 
totic lines. 

5.  THE  BILINEAR  RATE  OF  CHANGE  OF  A  FUNCTION  OF 
POSITION 50 

5*1   The  relation  between  the  spread  of  the  ^-family  and  the  bilinear 

rate  of  change  of  <f>. 
5*2   Relations  between  the  bilinear  rate  of  change  of  <l>,  the  linear  rate 

of  change  of  the  slope  of  <£,  and  the  spread  of  the  ^-family. 
5*3   The  symmetrical  bilinear  function  ^2p(dlA-/dSq}. 
5*4   Concluding  remarks  on  the  formulae  of  this  section. 

6.  THE  CODAZZI  FUNCTION 54 

6*1    Definition  of  the  Codazzi  function ;  its  trilinearity ;  the  relation 

of  this  function  to  the  cubic  functions  of  direction  of  Laguerre 

and  Darboux  ;  the  form  of  the  function  in  special  cases. 
6*2   The  symmetry  of  the  Codazzi  function ;  the  Codazzi  equations ; 

relations  between  the  function  of  Laguerre  and  the  function  of 

Darboux. 
6'3   The  use  of  the  Codazzi  equations  for  the  calculation  of  geodesic 

curvatures. 

7.  THE  TRILINEAR  RATE  OF  CHANGE  OF  A  FUNCTION  OF 
POSITION 60 

7'1   The  relation  between  the  trilinear  rate  of  change  of  3>  and  the 

function  <£2/>  (dl^/dsq}. 
7 '2   The  rate  of  change  of  a  bilinear  curvature  and  of  the  principal 

curvatures  along  the  orthogonal  trajectory  of  a  family ;  the  twist 

of  the  <E>-family. 
7 '3   Calculation  of  bilinear  curvature  and  of  twist  by  means  of  a 

Cartesian  frame. 

8.  FUNCTIONS  OF  DIRECTION  ON  A  SURFACE       ...       71 
8'1    The  fundamental  difficulty  ;  the  Darboux  gradient. 

8*2   The  multilinear  rates  of  change  of  a  function  <J>  on  a  surface. 
8*3   Relations  between  the  bilinear  rate  of  change  of  <£  and  the  geo- 
desic curvatures  of  ^-curves  and  <$>-orthogonals. 
8'4   The  gradient  of  the  Codazzi  function. 

INDEX  OF  DEFINITIONS 79 

INDEX  OF  SYMBOLS  .  80 


MULTILINEAR  FUNCTIONS  OF  DIRECTION 

Preliminary  Paragraphs 

O'l.  The  association  of  a  direction  OR  with  a  real  number  r, 
which  may  be  positive,  zero,  or  negative,  determines  a  vector 
which  will  be  denoted  by  rB\  of  this  vector  r  will  be  called  the 
amount  in  the  direction  OR.  The  vector  rR  possesses  in  addition  to 
the  direction  OR  the  reverse  direction,  which  we  shall  denote  con- 
sistently by  OR',  and  the  amount  of  rR  in  the  direction  OR'  is  —  r. 
The  zero  vector  has  all  directions,  and  its  amount  in  every  direction 
is  zero  ;  a  proper  vector  has  only  two  directions  and  two  amounts. 

A  vector  of  amount  unity  is  called  a  unit  vector  or  radial.  The 
vector  1^  has  the  direction  OR'  as  well  as  the  direction  OR,  but 
there  is  no  confusion  in  describing  the  direction  0  R  as  the  direction 
of  the  radial. 

02.  There  is  an  infinity  of  angles  between  two  directions  in 
space,  but  these  angles  all  have  the  same  cosine.  If  €ES  is  an  angle 
between  directions  OR,  OS  of  two  vectors  r,  s  whose  amounts  in 
these  directions  are  r,  s,  the  product  rs  cos  €RS  depends  only  on  r 
and  s,  not  on  any  choice  which  is  arbitrary  when  the  vectors  are 
given;  this  product  will  be  called  the  projected  product*  of  r  and 
s  arid  denoted  by  /rs.  The  projected  product  of  a  vector  s  and  a 
radial  1^  is  the  projection  of  s  in  the  direction  OR,  and  the  pro- 
jected product  of  two  radials  is  the  cosine  of  the  angles  between 
their  directions. 

0'3.  Any  three  vectors  p1,  p2,  p3  which  are  not  coplanar  form  a 
vector  frame,  in  which  the  arbitrary  vector  r  is  determined  by  the 
three  scalars  f,  ?;,  f  such  that 


*  Many  writers  have  not  hesitated  to  call  this  the  scalar  product,  although  the 
function  is  the  negative  of  that  for  which  Hamilton  designed  the  name.  There 
is  no  universal  notation  ;  to  transfer  the  letter  as  well  as  the  name  rendered  familiar 
by  Hamilton  and  to  appropriate  brackets  of  some  special  kind  are  courses  equally 
open  to  criticism,  and  if  there  is  here  a  vacant  role  in  the  symbolism  of  vector 
analysis  it  is  one  for  which  the  initial  of  Gibbs  and  Grassmann  may  be  cast  with 
peculiar  fitness.  Neither  r  .  s  nor  r  x  s  is  quite  secure  from  misunderstanding, 
since  Heaviside  uses  the  one  for  a  dyad  and  Gibbs  the  other  for  a  vector  product;  I 
am  conservative  enough  to  regard  rs  as  denoting  a  quaternion. 


10 

The  polar  of  the  frame  p1pap8  is  the  frame  p^p3  such  that 
^  is  unity  or  zero  according  as  h  and  k  are  the  same  or 
different,  that  is  to  say,  such  that  p1  is  at  right  angles  to  both  p2 
and  p3  and  £plpl  is  unity,  p2  is  at  right  angles  to  both  p3  and  p1 
and  c^p2p2  is  unity,  and  p3  is  at  right  angles  to  both  p1  and  p2 
and  c^p3p3  is  unity.  If 


r  = 

then  Jrpl  =  \, 

and  since  the  relation  between  the  two  vector  frames  is  reciprocal, 


considered  as  derived  from  the  frame  pxp2p3,  the  projected  products 
X,  //,,  v  are  naturally  called  the  polar  coefficients  of  r. 

0'4.  When  we  have  occasion  to  use  a  Cartesian  frame  of  refer- 
ence, we  shall  not  assume  it  to  be  trirectangular.  We  shall  use 
a,  /3,  7  for  angles  between  the  axes  of  reference  and  A,  B,  T  for 
angles  between  the  planes,  A  being  an  angle  from  the  second  plane 
to  the  third  round  the  first  axis  just  as  a  is  an  angle  from  the 
second  axis  to  the  third  in  the  first  plane ;  A,  B,  F  are  external 
angles  of  the  spherical  triangle  of  which  or,  j3,  7  are  sides.  Also  we 
shall  denote  by  T  the  sine  of  this  triangle,  that  is,  we  shall  write 

T  =  sin  /3  sin  7  sin  A  =  sin  7  sin  a  sin  B  =  sin  a  sin  0  sin  F. 

Then  if  x,  y,  z  are  the  components  and  I,  'in,  n  the  projections 
of  any  vector, 

0'41  f  I  =  x  +  y  cos  7  4-  z  cos  /9, 

m  =  x  cos  7  4-  y  4-  z  cos  a, 
n  =  x  cos  (3  4-  y  cos  a  +  z, 
and  on  the  other  hand 

0'42  [x  =  ftp-2  sin2  a  +  mT'1  cot  F  -f  nT~l  cot  B, 

y  =  IT~1  cot  F  +  mT~2  sin2  /3  4-  riT"1  cot  A, 
_z  =  ZT-1  cot  B  4-  mT~!  cot  A  4-  wT~2  sin2  7. 

The  projected  square  of  the  vector,  having  the  value  Ix  4-  my  4-  nz, 
can  be  expressed  as  a  quadratic  function  of  components  alone  by 
means  of  0'41  or  of  projections  alone  by  means  of  0*42  ;  thus 

0'43     r2  =  a?  4-  y*'  4-  z1 4-  Zyz  cos  a  4-  ^zx  cos  /3  4-  2#?/  cos  7, 


11 


but  in  terms  of  projections  alone  r2  is  most  readily  given  by  means 
of  a  determinant ;  eliminating  x,  y,  z  between  0'41  and 

r2  ==  lac  +  my  +  nz 

we  have 

=  0, 


1    cos  7  cos/3   I 
cos  7   1    cos  a  m 

cos  /3  cos  a   1    n 

I    m 

n    r2 

T-2 

1 

cos  7  cos  /3 

cos  7 

1    cos  a 

cos/3 

cos  a    1 

Z 

m     ?i 

that  is 

0'44  ?-2  =  -T-2        1        cos  7     cos/3      I 

m 

0 

If  OP  is  a  direction  perpendicular  to  each  of  two  directions 
OR,  OS  and  if  eRS  is  an  angle  from  OR  to  OS  round  OP,  the  cosines 
of  OP  are  given  in  terms  of  the  ratios  of  OR  and  0$  by 

0'45  (7P,  mP,  ??P)  sin  e™  =  T 


X 


yR 


'72 


and  the  ratios  of  OP  in  terms  of  the  cosines  of  OR  and  0$  by 


046 


OP, 


sn  €     = 


The  components  x,  y,  z,  and  the  projections  I,  m,  w,  of  a  vector 
r  in  the  Cartesian  frame  OABC  are  the  coefficients  and  the  polar 
coefficients  of  r  in  the  vector  frame  composed  of  the  radials 
1^,  1£,  lc.  But  it  must  be  observed  that  the  polar  of  this  vector 
frame  is  not  as  a  rule  the  Cartesian  frame  polar  to  OABG  but 
consists  of  vectors  of  amounts  T~J  sin  a,  T"1  sin  /3,  T"1  sin  7. 

0'5.  For  the  comparison  of  directions  in  one  plane  actual  angles 
can  be  used,  a  definite  direction  of  angular  measurement  being 
adopted.  An  angle  from  OS  to  OT  will  be  denoted  by  eST;  this 
angle  is  not  free  from  ambiguity,  for  any  restriction  on  the  magni- 
tude or  sign  of  angles  is  not  merely  superfluous  but  irksome,  but 
cos  eST  and  sin  €ST  are  determinate  functions  of  the  two  directions 
0$,  OT,  and  so  also  is  the  rate  of  change  of  eST  with  respect  to  any 
variable  on  which  the  directions  depend  in  a  regular  manner. 


12 

When  axes  of  reference  A'OA,  B'OB  are  being  used  in  the 
plane,  an  angle  eAB  will  be  denoted  by  &>.  To  deal  simply  and 
symmetrically  with  a  variable  direction  OT,  angles  eAT,  eTB  are 
both  required  ;  the  sum  eAT  4-  eTB  must  differ  from  o>  by  an  integral 
multiple  of  2?r,  and  a,  fi,  or  if  necessary  aT,  /3r,  will  be  used  for  a 
pair  of  angles  eAT,  eTB  subject  to  the  convention  a-ir/3  =  w. 

The  theory  of  multilinear  functions  of  direction  in  a  plane  per- 
sistently associates  with  each  direction  one  of  the  perpendicular 
directions,  and  the  direction  which  makes  a  positive  right  angle 
with  OT  will  be  denoted  by  OE  or  by  OET;  for  OES  will  be  sub- 
stituted OD. 

0'6.  A  function  F(T)  of  the  direction  OT  in  a  plane  regarded 
as  a  function  F(eWT)  of  an  angle  to  OT  from  a  fixed  direction  OTF, 
requires  for  its  study  its  derivative  dF  (eWT)ldeWT.  This  derivative 
is  itself  a  function  of  eWT,  that  is,  of  the  direction  OT,  but  since  it 
does  not  really  depend  on  0  W  it  may  be  called  simply  the  angular 
derivative  of  F(T)  and  will  be  denoted  by  daF(T): 

0  61  daF(T)  =  lira  [{F(8)  -  F(T)}/eTS]. 

S+T 

A  function  of  a  number  of  independent  directions  in  a  plane  has 
an  angular  derivative  with  respect  to  each  of  them,  and  the  various 
angular  derivatives  of  F(Q,  R,  ...)  will  be  written  daQF(Q,  R,  ...), 
daRF(Q,  R,  ...),  and  so  on. 

If  the  directions  OQ,  OR,  ...  in  a  plane  are  made  dependent  on 
a  direction  OT  in  that  plane,  the  function  F(Q,  R,  ...)  becomes  a 
function  of  OT,  having  an  angular  derivative  with  respect  to  OT 

given  by  dF_de,Ea+dF_  rfej™  + 

d€Wg  deWT      v€WR  deWT 

The  dependence  of  OQ,  OR,  ...  on  OT  is  a  dependence  of  angles 
€TQ,  eTR,  ...  on  OT,  and  since 

€WQ  =  €WT  +  €TQ  »  €WR  =  eWT  +  €TR  >   •••  J 

the  derivatives  deWqjdeWT,  deWRjde]VT,  ...  have  the  values 


and 

0'62.    The  angular  derivative  with  respect  to  OT  of  a  function 
F(Q,  R,  ...)  of  directions  themselves  dependent  on  OT  is 
(1  +  daeTQ)  daQF+  (1  +  da  €TR)  daRF+  .... 


13 

In  particular 

0'63.  If  the  directions  OQ,  OR,  ...  make  constant  angles  with  OT, 
the  angular  derivative  of  a  function  F  (Q,  R,  ...)  with  respect  to  OT 
is  the  sum  of  the  several  angular  derivatives  daqF,  daRF,  — 

An  angular  derivative  in  space  is  a  function  of  two  directions  at 
right  angles.  If  ON  is  a  direction  at  right  angles  to  OT,  the  di- 
rection of  angular  measurement  in  the  plane  to  which  ON  is  normal 
is  related  to  ON  by  the  spatial  convention  ;  a  function  of  direction 
in  space  becomes  by  the  restriction  of  its  argument  to  the  plane 
normal  to  ON  a  function  of  direction  in  that  plane,  with  an  angular 
derivative  whose  value  at  OT  depends  no  less  on  ON  than  on  OT. 


1.   Linear  and  Multilinear  Functions 

I'll.  Intrinsically,  a  linear  function  of  a  variable  vector  is  a 
function  whose  value  for  the  sum  of  two  vectors,  and  therefore  also 
for  the  sum  of  any  finite  number  of  vectors,  is  the  sum  of  its  values 
for  the  several  components  ;  a  multilinear  function  is  a  function  of 
a  number  of  independent  vectors  that  is  linear  in  each  of  them. 

1'12.  The  value  of  any  linear  function  for  the  argument  rR  is 
r  times  the  value  of  the  same  function  for  the  argument  1^.  If  a 
frame  of  reference  OABC  is  used  and  the  components  of  the  variable 
vector  r  are  x,  y,  z,  then  since  r  is  x\A  +  y\B  +•  z\c,  a  function  F  (r) 
which  is  linear  is  necessarily  expressible  as 


and  conversely  a  function  of  r  which  is  of  the  form  scL  +  yM  +  zN 
where  L,  M,  N  do  not  depend  on  r  must  be  linear  : 

1*121.  A  linear  function  of  the  vector  r  is  a  function  which  is  a 
homogeneous  linear  function  of  the  components  of  r  in  any  frame. 

T13.  A  function  whose  arguments  are  radials  may  be  regarded 
as  a  function  simply  of  direction,  and  a  function  of  direction  is  said 
to  be  linear  if  the  function  of  r  and  OR  obtained  by  multiplying 
its  value  for  the  direction  OR  by  the  number  r  is  a  linear  function 
of  the  vector  r^.  We  can  if  we  wish  avoid  the  explicit  mention  of 
vectors  in  the  definition  of  a  linear  function  of  direction,  either  by 
introducing  implicitly  the  definition  of  the  sum  of  two  vectors  or 


14 

by  using  a  frame  of  reference.  A  function  of  direction  is  linear  if 
given  any  two  successive  steps  OQ,  QR,  of  lengths  p,  q,  whose 
resultant  OR  has  length  r,  the  sum  of  p  times  the  value  of  the 
function  for  the  direction  OQ  and  q  times  the  value  of  the  function 
for  the  direction  QR  is  r  times  the  value  of  the  function  for  the 
direction  OR.  And  a  function  of  direction  is  linear  if  it  is  expressible 
as  a  homogeneous  linear  function  of  the  ratios  of  the  direction  with 
reference  to  any  frame ;  with  this  last  definition  we  have  to  notice 
that  a  function  of  the  direction  ratios  which  is  not  given  as  a  homo- 
geneous linear  function  may  in  fact  be  expressible  in*  this  form  in 
virtue  of  the  quadratic  identity  to  which  the  ratios  are  necessarily 
subject. 

1'14.  The  definitions  of  linear  and  multilinear  functions  of 
vectors  and  directions  are  designed  to  restrict  as  little  as  possible 
the  nature  of  the  function.  In  the  present  work  the  ultimate 
equations  are  scalar,  but  vectors  and  other  functions  are  essential 
to  the  processes. 

1'21.  For  an  arbitrary  function  of  the  k  vectors  r1}  r2,  ...  r^,  the 
natural  notation  is  of  the  form  ^(r^  ra,  ...  rk),  but  for  a  function 
that  is  multilinear  there  is  more  even  than  brevity  to  be  gained 
by  substituting  the  form  Pr^ ...  rk,  or  Pkrlr2 ...  rfc  if  the  degree 
of  the  function  has  to  be  made  prominent,  for  this  form  emphasises 
the  identities  such  as 

P  (s  + 1)  r.2 . . .  rk  =  P  sr2 . . .  rk  +  P  tr.2 . . .  rk 

involved  in  the  definitions.  It  must  be  remembered  that  the  order 
in  which  the  vectors  are  written  is  not  irrelevant  unless  the  function 
is  symmetrical  in  its  definition:  a  function  defined  unsymmetrically 
may  be  in  fact  symmetrical,  in  which  event  the  order  of  writing  the 
variables  does  not  affect  the  truth  of  any  formulae  but  the  assertion 
of  the  symmetry  is  in  itself  significant. 

1'22.  The  function  of  direction  P1A1B  ...  1^  is  often  denoted  by 
PAB...K-  Were  an  attempt  made  to  deal  with  functions  of  direction 
without  mention  of  vectors  this  compact  alternative  would  be  used 
throughout,  but  since  as  a  rule  the  sum  of  two  radials  and  the  rate 
of  change  of  a  variable  radial  are  vectors  that  are  not  radials,  the 
operations  that  are  most  natural  commonly  involve  functions  of 
directions  and  functions  of  vectors  in  one  equation,  and  the  effect 


15 

of  too  persistent  a  substitution  of  PAB...K  f°r  P^A^B  ...  IJT  is  un- 
sightly. 

1*31.  The  advantages  of  detaching  the  symbol  P  from  the  group 
PrjFa ...  rk  are  secured  by  the  method  of  Russell :  P  denotes  the 
relation  of  a  value  of  the  function  to  the  set  of  vectors  on  which 
the  value  depends,  and  is  called  a  multilinear  relation.  The  relation 
P  will  be  described  as  the  core  of  the  function  Pr^ ...  rfc  and  of 
the  corresponding  function  of  direction  PAB...K- 

1'32.  To  prove  that 

1*321.    The  sum  of  any  finite  number  of  functions  multilinear  in 
the  same  set  of  vectors  is  itself  a  multilinear  function  of  the  set 
and  that 

1*322.  The  product  of  a  multilinear  function  by  any  scalar  is  a 
multilinear  function 

is  easy.  These  propositions  give  further  justification  of  the  notation 
we  are  using,  and  provide  a  basis  for  definitions  of  the  addition  of 
cores  and  of  the  multiplication  of  a  core  by  a  scalar  : 

1*323  (2P)  rira . . .  r*  =  2  (P  r,r2 . . .  r*), 

1*324  (rP)  rlr,...rk  =  r(Prlr2...  rk). 

1*33.  In  a  multilinear  function  of  degree  k  any  h  of  the  variable 
vectors  or  directions  may  play  a  parametric  part.  The  function  is 
then  regarded  as  multilinear  in  the  remaining  k  —  h  variables,  with 
a  core  which  is  a  function  of  the  h  parameters,  and  we  have  only  to 
compare  1*323  with  the  original  definition  of  a  multilinear  function 
to  see  that  this  core  is  multilinear  in  the  parameters ;  it  is  a  multi- 
linear function  which  is  neither  scalar  nor  vector.  Thus  the  bilinear 
function  Prs  or  PRS  yields  two  linear  functions  which  are  written 
as  (P#s)  r  and  (Pr#)  s  or  (P*S)R  and  (P_R*)S;  if  the  degrees  of  the 
different  functions  are  to  be  exhibited,  the  two  linear  functions  of 
direction  subsidiary  to  P*ES  are  shewn  as  (P1^s)lR  and  (PlR*)ls- 

1*41.  If  ^O1,  %h2,  %ft3  are  the  coefficients  of  rh  in  a  vector  frame 
Pap2p3,  the  linearity  of  a  function  Pr^ ...  iv^r^  in  rk  implies  the 
equality 

1-411     Prlr9...rk-r  = 


16 

and  the  expansion  of  each  of  the  variable  vectors  in  turn  in  th( 
same  way  gives  the  result 

T412     Pr1r2...rfc_1rfc  = 

S^imi  X*"*  •  •  •  Xk-ink~lXX:™k  P  P™1?™2  .  .  .  pmk-lpmk} 

where  each  of  the  affixes  mlt  m2,  ...  mje-i,  tnk  stands  for  one  of  the 
three  symbols  1,  2,  3,  and  the  summation  extends  to  the  3fc  possible 
terms.  To  obtain  a  formula  in  terms  of  the  projected  products 
</rhpl,  c^r^p2,  #Tfip9,  all  that  is  necessary  is  to  remember  that  these 
projected  products  are  the  coefficients  %^,  %h2,  %V  of  r^  in  the  frame 
pip^p3  polar  to  pap2p3,  whence 

1413     Pr1r,...iv.1rfc  = 


Particular  cases  of  1*412  and  1*413  are  expressions  for  the  multi- 
linear function  referred  to  a  Cartesian  frame,  namely 

1-421          P  rar2  .  .  .  rk  =  Sc^ic^  .  .  .  ckm*PMM  ...  Mt, 

where  c^1,  erf,  ch3  are  the  components  of  rh  and  Mh  stands  for  A,  B, 
or  C  according  as  mh  stands  for  1,  2,  or  3,  and 

1-422    P  1-^2  .  .  .  rk  =  Zpnip™*  .  .  .  pkm*P  kmikwa  .  .  .  k?»3, 

where  p^,  ph*,  pr?  are  the  projections  of  r^  and  k1,  k2,  k3  are  those 
vectors  normal  to  the  planes  OBC,  OCA,  GAB  whose  projections 
on  (L4,  OB,  OC  are  unity. 

1'43.    From  1'412  follow  two  fundamental  theorems: 

1*431.  The  value  of  a  multilinear  function  is  known  for  every  set 
of  vectors  in  space  if  it  is  given  for  every  selection  from  any  three 
vectors  that  are  not  coplanar  ; 

1*432.  A  function  that  is  multilinear  is  wholly  symmetrical  if  it 
is  symmetrical  with  respect  to  any  three  vectors  or  any  three  direc- 
tions that  are  not  coplanar. 

Because  of  the  second  of  these  results,  any  two  groups  of  theorems 
which  express  the  complete  symmetry  of  the  same  multilinear 
function  with  respect  to  different  sets  of  vectors  may  be  regarded 
as  equivalent  :  this  is  one  of  the  ways  in  which  results  diverse  in 
form  are  coordinated  by  the  theory  developed  here. 

The  two  theorems  of  the  last  paragraph  assume  the  functions 
involved  to  be  defined  for  all  sets  of  vectors  or  directions  in  space. 


17 

If  only  a  single  plane  is  in  question,  it  is  sufficient  in  T431  for  the 
selection  to  be  made  from  two  vectors  in  that  plane  but  not  collinear 
and  in  1/432  for  the  symmetry  to  be  established  for  two  such 
vectors. 

1-51.    That 

1*511.    The  projected  product  of  two  vectors  is  a  bilinear  function 
of  these  vectors, 
and  that 

1*512.  The  projection  of  a  constant  vector  on  a  variable  direction 
is  a  linear  function  of  the  direction, 

follow  from  the  elementary  distributive  property  of  the  projected 
product.  The  converse  of  these  theorems  is  also  true,  for  if  a,  b,  c 
are  scalars,  ax+by  +  cz  is  the  projected  product  of  the  vector  of 
components  x,  y,  z  and  the  vector  of  projections  a,  b,  c,  and  if  the 
former  vector  is  the  radial  lr,  the  same  sum  represents  the  pro- 
jection of  the  latter  vector  on  OT: 

T513.  Every  linear  scalar  function  of  the  variable  vector  r  can 
be  exhibited  in  one  way  only  as  the  projected  product  of  r  and  a 
vector  independent  of  r,  and  every  linear  scalar  function  of  the 
variable  direction  OT  in  one  way  only  as  the  projection  on  OT  of 
a  vector  independent  of  OT. 

It  is  convenient  in  both  cases  to  call  the  vector  the  source  of  the 
linear  function. 

1*52.  The  projected  product  of  the  sources  of  two  linear  functions 
affords  the  simplest  example  of  a  scalar  which  depends  only  on 
two  cores,  and  if  the  cores  are  Q  and  R  this  projected  product  will 
be  denoted  simply  by  QR.  If  Q  and  R  themselves  involve  variables 
QR  is  of  course  a  function  of  these  variables.  Thus  if  from  two 
bilinear  functions  QAB,  RCD  are  formed  two  linear  functions 
(QA*)B  (R*D)C>  the  projected  product  QA%  R%D  is  a  function  of  the 
directions  OA,  OD',  it  is  in  fact  a  bilinear  function,  and  so  can  be 
used  to  form  on  the  same  principle  an  infinity  of  other  functions, 
such  for  example  as  Qt£  Qt#  R#D. 

1'53.  Any  two  cores  of  the  same  degree  give  rise  to  a  function 
corresponding  to  the  projected  product  of  the  sources  of  two 
linear  functions,  but  in  the  absence  of  a  direct  definition  of  this 
function  in  general,  we  must  describe  the  function  defined  in  the 

N.  2 


18 

last  paragraph  in  such  a  way  as  to  indicate  the  line  of  extension. 
Referred  to  a  frame  OABC,  the  linear  function  P  r  can  be  expressed 
in  the  two  forms 

lpa'r  4-  nt<pyr  -4-  npzr,     xplr  +  ypmr  +  zpnr, 

where  lp,  mp,  np  are  the  projections  and  a^*,  yp,  zp  the  components 
of  the  source,  and  since  the  value  of  the  projected  product  of  two 
linear  cores  Q,  R  is  given  by  the  two  sums 


not  only  are  these  sums  equal  but  their  value  is  independent  of 
the  particular  frame  OABC.  Similarly  the  multilinear  function 
Pr^Fa  ...  rk  whatever  its  degree  can  be  expanded  with  reference  to 
the  frame  OA  EG  in  the  two  forms 


and  if  Q,  R  are  any  two  cores  of  the  same  degree  k  the  sums 


are  equal  and  have  a  value  independent  of  the  frame  OABC  ;  this 
common  value  defines  the  projected  product  of  the  cores  Q,  R,  and 
is  denoted  by  QR. 

1'54.  When  once  the  projected  product  QR  is  defined  for  cores 
of  arbitrary  degree,  a  whole  group  of  functions  is  seen  to  be 
derivable  from  any  two  or  more  cores,  or  indeed  from  any  one  core 
of  degree  not  less  than  two.  For  example,  from  a  trilinear  core  P 
by  regarding  one  direction  OB  as  parametric  we  derive  a  bilinear 
core  jP#jBt>  and  if  Q  is  a  bilinear  core,  the  projected  product  P#B+Q, 
better  denoted  by  P#s\Q*-t>  ig  itself  a  linear  function  of  OB  and 
gives  rise  by  combination  with  any  linear  scalar  core  R  to  a  pro- 
jected product  (P*§t  Q*t)  ^§  5  without  attempting  to  classify  func- 
tions of  this  kind  we  must  recognise  their  nature  when  they 
present  themselves. 

Symmetry  reduces  the  number  of  distinct  functions  to  which 
a  given  multilinear  function  is  related.  For  example,  if  QAB,  ROD 
are  unsymmetrical  bilinear  functions,  the  four  bilinear  functions 
Q*s^*r>  Qs*^*r>  Q*s^r*>  Qs*^r*  are  distinct,  but  if  the  original 
functions  are  both  symmetrical,  the  four  derived  functions  coincide. 

1'55.  If  two  multilinear  functions  Qr1r2...rA;,  Rr^...^  of  the 
same  degree  are  denned  only  for  vectors  in  a  particular  plane,  the 


19 

projected  product  QR  can  be  defined  as  in  T53,  with  the  sole 
difference  that  the  frame  of  reference  is  two-dimensional.  More- 
over, if  one  multilinear  function  Qrlr2...rk  is  defined  only  for 
vectors  in  a  particular  plane  and  another  .Rr1r2...rjb  of  the  same 
degree  is  defined  without  restriction  on  r1?  ra, ...  rk,  a  projected  pro- 
duct is  definable  by  the  restriction  of  the  arguments  of  Ur1ra...rfc 
to  the  plane  in  which  they  can  serve  as  arguments  to  (2r1r2...rj; 
also,  and  no  confusion  can  be  caused  by  denoting  this  projected 
product  by  QR ;  the  only  point  to  be  remembered  is  that  if  by  a 
change  in  the  definitions  the  restriction  on  the  arguments  of 
QrIr2...rfc  is  subsequently  removed,  QR  will  be  in  danger  of 
acquiring  a  second  meaning  inconsistent  with  the  first. 

1*61.  Should  the  function  P  r^ . . .  r^  involve  any  variables  other 
than  the  vectors  rlf  r2,  ...  r^,  then  if  a  change  in  these  additional 
variables  is  not  necessarily  accompanied  by  a  change  in  the  vectors 
it  is  the  core  that  is  to  be  regarded  as  a  function,  and  a  limit  of 
Pi^ra...!**  for  variations  in  which  r^  r2,  ...  r^  are  constant  is  a 
function  of  rlf  ra,  ...  r^  which  if  multilinear  can  be  used  to  define 
a  limit  of  P.  It  is  difficult  to  be  more  precise  in  this  assertion 
without  placing  undue  restriction  on  its  scope ;  the  case  which  is 
for  us  important  affords  the  best  commentary;  if  Pr^a...^  is  a 
scalar  or  a  vector  depending  on  a  scalar  variable  t  in  such  a  way 
that  for  each  particular  set  of  values  of  rlf  r2,  ...  Tk  there  is  a 
derivative  d(Prlr.2...rk)/dt,  it  follows  from  1*321  and  1*322  that 
this  derivative  is  multilinear  in  rl}  ra>  ...  r^,  and  dP/dt  is  defined 
as  the  core  of  d  (P  r^ . . .  rk)/dt. 

1*62.  It  is  oh  the  assumption  that  the  vectors  rl5  ra,  ...  rk  not 
only  can  be  but  are  independent  of  t  that  d(Prlr2...rk)/dt  is 
multilinear  and  introduces  dP/dt.  But  this  derived  core  is  of  no 
less  service  in  the  evaluation  of  d(Prlr2...rk)/dt  when  the  vectors 
vary  with  t,  the  symbols,  in  consequence  of  T323  and  the  defini- 
tions, grouping  themselves  in  the  familiar  mariner 

1-621     d  (P  r,  r2 . . .  rk)/dt  =  (dP/dt)  rx  r2 . . .  rk  +  P  (drjdt)  rz...rk 
+  Prl(drz/dt) ...  rfc+  ...  +Pr1r2...  (drk/dt). 

This  identity  is  sometimes  of  service  for  the  calculation  of 
(dP/dt)rlr9...rk,  but  there  is  nothing  in  the  formula  so  used  to 
shew  why  the  function  obtained  is  multilinear. 

2—2 


20 

1*71.  The  multilinear  functions  of  differential  geometry  are  not 
so  much  functions  of  directions  in  space  as  functions  of  directions 
at  a  point;  in  other  words,  they  are  functions  of  direction  with 
cores  depending  on  a  variable  point. 

Let  Pk  rl  r2  .  .  .  rk  be  such  a  function,  dependent  on  the  position 
of  a  point  Q,  and  suppose  Q  to  be  confined  to  a  curve  through  a 
particular  point  0.  On  this  curve  Pk  can  be  regarded  as  a  function 
of  the  arc  s  measured  to  Q  from  some  fixed  point,  and  to  calculate 
the  rate  of  change  dPk/ds  a  frame  of  reference  may  be  used  ;  then 

dPk  dz 


= 

ds        dx  ds       dy  ds       dz   ds  ' 
that  is, 

1-712  dP*lds  =  PfacT  +  PfyT  +  PfzT, 

where  Pf,  P2k,  Pf  are  functions  of  position  having  no  relation  to 
the  curve  described  by  Q  and  XT,  yT,  ZT  are  the  direction  ratios  of 
the  tangent  to  this  curve.  Hence 

1'713.  The  rate  at  which  the  core  of  a  multilinear  function  depen- 
dent on  position  changes  at  a  point  0  ivith  respect  to  the  arc  of  a  curve 
through  0  is  the  same  for  all  curves  whose  direction  at  0  is  the  same, 

and  can  be  called  simply  the  rate  of  change  in  the  common 
direction,  and  further 

1*714.  The  rate  of  change  of  the  core  of  a  multilinear  function  in 
a  variable  direction  is  a  linear  function  of  that  direction. 

If  the  rate  of  change  of  the  core  Pk  in  the  direction  OR  is 
dPk/dsR,  the  function  r  (dPk/dsR}  rx  r2  .  .  .  r^  is  linear  in  the  vector 
rB  as  well  as  in  the  k  vectors  r1}  r2,  ...  r^  and  is  therefore  a  multi- 
linear function  of  degree  k  +  1  ;  its  core,  which  depends  only  on 
the  variation  of  Pk  in  space,  is  called  the  gradient  of  Pk  and  de- 
noted by  P*+1.  Sometimes  the  function  Pk+l  rx  r2  .  .  .  r^  rk+l  is  called 
the  gradient  of  the  function  P*rj  r2  ...  r%. 

That  linear  and  bilinear  functions  have  a  part  to  play  follows 
from  1*511  and  1*512,  and  on  account  of  1*714  the  appearance  of 
functions  of  higher  degrees  is  inevitable,  but  it  is  not  every  useful 
multilinear  function  that  is  derivable  from  some  linear  or  bilinear 
function  by  the  formation  of  successive  gradients. 

1*72.  If  r1;  r2,  ...  r&  instead  of  being  independent  variables  are 
definite  functions  of  the  position  of  the  current  point  0  on  a  curve, 


21 

the  rate  of  change  of  the  multilinear  function  P*  i^  r2  .  .  .  TJ.  with 
respect  to  a  parameter  t  on  the  curve  is  given  by 

1-721   d  (Pk  r,  r2  .  .  .  rk)/dt  =  Pk+l  rt  r2  .  .  .  rk  w 
+  Pk  (drjdt)  r.2  .  .  .  rk  +  Pk  r,  (dr,/dt)  .  .  .  rk  +  .  .  .  +  Pk  r,  r.2  .  .  .  (drkldt)t 
where  w  is  the  velocity  of  0  with  respect  to  t.    In  particular,  the 
rate  of  change  of  a  function  of  direction  PkAB...K  along  a  curve  in 
the  direction  OL  is  given  by 

1-722  dPkAB  KldsL  =  ^^KL  +  P"^  K(d\AldsL) 


the  vector  dlH/dsL  is  not  as  a  rule  a  unit  vector,  nor  is  this  vector 
a  linear  function  of  OL  unless  the  direction  OH  is  independent  of 
the  direction  OL,  so  that  in  the  majority  of  applications  it  is  only 
the  first  of  the  terms  on  the  right  of  T722  that  is  itself  a  function  of 
direction,  but  if  dlH/dsL  can  be  put  into  the  form  pp  +  qg  +  rR, 
where  OP,  OQ,  OR  are  known  directions,  then 
1-723 


and  the  multilinear  function  of  direction  whose  core  is  Pk  reappears 
with  different  sets  of  directions  for  arguments  and  with  scalar 
multipliers  that  do  not  depend  on  P*. 

T81.  If  the  source  of  the  linear  function  QT  of  direction  in  a 
plane  is  the  vector  rR,  then 

1*811  QT  =  r  cos  €RT 

and  therefore 

da  QT  =  r  cos  (eRT  4-  \  TT)  =  r  cos  eRE, 
that  is, 

1-812  daQT=QE: 

The  value  of  the  angular  derivative  of  a  linear  function  in  the 
direction  OT  is  the  same  as  the  value  of  the  function  itself  in  the 
direction  luhich  makes  a  positive  right  angle  with  OT. 

In  other  words 

1*813.  The  angular  derivative  of  a  linear  function  QT  of  direction 
in  a  plane  is  the  linear  function  whose  source  is  obtained  by  rotating 
the  source  of  QT  through  a  positive  right  angle. 

T82.  The  partial  angular  derivatives  of  a  multilinear  function 
of  independent  directions  in  a  plane  are  given  at  once  by  1'812,  and 


22 

extension  to  functions  multilinear  in  interdependent  directions  is 
made  by  the  use  of  O62  and  0'63.  For  example,  if  PST  is  bilinear, 

1*821  dasPgy  =  1  DT,     daTPST  =  P$E> 

1*822  daPff  =  -L  ET  ~t~  -*   TE  ==  — 

1*823  da  L  fE  =  Jr EE  —  -LTT  ~ 

from  1-822, 

1'824.  If  PST  is  any  bilinear  function  of  directions  in  a  plane, 
the  sum  of  the  values  of  the  quadratic  function  PTT  for  two  directions 
at  right  angles  is  constant; 

1'823  shews  that  PTE  -  PET  also  is  constant,  but  this  is  merely  a 
second  version  of  the  same  theorem,  obtained  by  regarding  PSE  as 
a  function  of  OS  and  OT. 

1'83.  To  look  for  the  angular  derivative  in  an  arbitrary  plane 
of  a  scalar  linear  function  of  direction  in  space  is  to  reach  familiar 
ground.  Let  RT  be  the  linear  function  whose  source  is  r,  let  ON 
be  any  direction  in  space,  and  let  8  be  the  component  of  r  at  right 
angles  to  ON',  if  OT  is  a  direction  at  right  angles  to  O^V,  the  pro- 
jection of  r  on  OT  is  the  projection  of  s  on  OT,  and  therefore  the 
source  of  RT  in  the  plane  at  right  angles  to  ON  is  s ;  it  follows 
from  1*813  that  the  angular  derivative  of  RT  in  this  plane  has  for 
its  source  the  vector  obtained  by  rotating  s  through  a  positive 
right  angle  round  ON,  and  this  we  recognise  as  the  vector  product 
of  r  and  ~\.N. 

2.    Fundamental  Notions  in  the  Kinematical  Geometry 
of  Surfaces  and  Families  of  Surfaces 

2'0.  To  prepare  for  geometrical  applications  of  the  theory  of 
multilinear  functions  it  is  necessary  to  examine  the  different  vectors 
of  the  form  dlH/dsK,  where  each  of  the  directions  OH,  OK  is  either 
constantly  normal  or  constantly  tangential  to  a  definite  surface 
through  0,  and  the  rate  of  change  is  with  respect  to  the  arc  of 
some  curve  whose  direction  at  0  is  OK.  It  is  assumed  that  by  a 
satisfactory  convention  one  of  the  directions  at  right  angles  to  the 
surface  is  chosen  to  be  called  the  normal  direction,  and  that  there 
is  a  spatial  convention  by  which  the  choice  of  the  normal  direction 
determines  the  direction  of  angular  measurement  in  the  tangent 
plane  at  0.  The  normal  direction  is  denoted  by  ON,  and  OR,  OS> 


23 

0 T  will  be  used  for  arbitrary  tangential  directions ;  for  the  rest, 
the  notation  is  that  described  in  0'5. 

2*11.  The  vector  d\NjdsT  is  the  velocity  of  the  Gaussian  image 
of  0  as  0  moves  along  the  surface  in  the  direction  OT\  it  is  at 
right  angles  to  ON,  and  may  be  described  either  directly  as  due  to 
the  spin  of  the  tangent  plane  about  the  conjugate  tangent  or  by 
components  or  projections  with  respect  to  given  tangential  directions. 
The  latter  course  has  the  advantages  of  involving  no  difficulties  of 
sign  and  of  introducing  two  functions  of  prime  importance :  if  the 
velocity  of  the  Gaussian  image  is  resolved  into  a  component  along 
the  tangent  and  a  perpendicular  component,  the  amount  of  the 
first  of  these  in  the  direction  OT'  reverse  to  0 T  is  the  normal  cur- 
vature of  the  surface  in  the  direction  OT,  and  will  be  denoted  by 
Kn,  and  the  amount  of  the  second  in  the  direction  OE'  with  which 
OT  makes  a  positive  right  angle  is  the  geodesic  torsion  along  OT, 
for  which  s(J  will  be  used.  Symbolically 

2111  d\NjdsT  —  —  Kn\T  —  s^l^, 
and  since  the  directions  OT,  OE  are  perpendicular 

2112  Kn  = 

2113  sg  = 

212.  Because  the  direction  ON  depends  only  on  the  position  of 
0,  not  on  the  direction  OT,  the  vector  dlN/dsT  is  a  linear  function 
of  the  direction  OT,  and  the  projection  of  this  vector  in  a  direction 
OS  independent  of  OT  is  linear  in  both  OS  and  OT.  It  follows  that 

2121.  The  normal  curvature  and  the  geodesic  torsion  of  a  surface 
are  quadratic  functions  of  direction, 

from  which  it  is  a  corollary  that 

2122.  Neither  KH  nor  sg  can  vanish  along  more  than  two  tangents 
at  0  without  vanishing  in  every  direction  through  0. 

2'21.  Analysis  of  the  vector  dls/dsT  for  an  arbitrary  relation  of 
the  tangential  direction  OS  to  the  curve  described  by  0  is  illuminated 
by  the  corresponding  analysis  of  the  particular  vector  dlT/dsT.  This 
latter  is  the  vector  of  curvature  of  the  curve,  and  being  necessarily 
at  right  angles  to  OT  is  determined  by  its  projections  in  any  two 
directions  normal  to  the  curve.  When  the  curve  is  being  considered 
in  relation  to  a  surface  on  which  it  lies,  the  directions  on  which  the 


24 

vector  of  curvature  is  projected  are  ON,  the  normal  to  the  surface, 
and  OE,  the  tangential  normal  to  the  curve  :  the  amount  of  the 
normal  projection  is  the  normal  curvature  tcn,  and  the  formula 

2-211  Kn  =  ^(dlT/dsT)  1N 

is  reconciled  with  2'112  by  the  consideration  that  since  £\T\N  is 
constant  the  sum  £(dlT/dt)  1N  +  </  (dlN/dt)  1T  is  zero  whatever  the 
variable  t  ;  the  amount  of  the  tangential  projection  is  the  geodesic 
curvature  of  the  curve,  and  this  will  be  denoted  by  /cg  : 

2-212  Kg  =  £(dlT/dsT)  1E. 

Because  ON  and  OE  are  at  right  angles,  and  coplanar  with  the 
vector  of  curvature, 

2'213  dlT/dsT  =  KnlN  4-  KO\E. 

2*22.  The  change  in  a  tangential  radial  ls  as  0  moves  on  the 
surface  is  partly  a  motion  with  the  current  tangent  plane,  and 
partly  a  motion  in  this  plane  ;  the  two  components,  of  which  the 
first  is  wholly  normal  and  the  second  wholly  tangential,  play  equally 
useful  but  dissimilar  parts,  and  have  no  analytical  resemblance. 

2'31.  The  component  of  dls/dsT  normal  to  the  surface  to  which 
OS  and  OT  are  tangential  I  propose  to  call,  for  reasons  that  will 
become  apparent,  the  bilinear  curvature  of  the  surface  in  the  direc- 
tions OS,  OT,  and  to  denote  by  KST  : 

2-311  KST  =  £(dls/dsT)  1N. 

This  function  must  be  recognised  in  a  variety  of  different  forms 
which  are  readily  found. 

The  motion  of  15  with  the  tangent  plane  is  determined  by  the 
spin  of  this  plane,  which  if  0(7  is  a  direction  conjugate  to  OT  is  a 
spin  of  a  definite  amount  p  about  OC  : 

2'312.  If  OC  is  a  direction  conjugate  to  OT  and  the  spin  of  the 
surface  along  OT  is  of  amount  p  round  OC,  then 


To  avoid  the  use  of  p,  which  cannot  be  made  a  single-  valued  function 
of  position  and  direction  by  any  satisfactory  convention,  all  that  is 
necessary  is  to  resolve  the  vector  pc  along  determinate  directions. 
If  pc  is  resolved  into  a  vector  along  OS  and  a  perpendicular  vector, 
only  the  second  of  these  components  affects  Is,  and  the  rate  of 
change  of  ls  as  far  as  it  is  due  to  this  component  has  the  same 


25 

amount  in  the  direction  ON  as  the  component  itself  has  in  the 
direction  OD'  with  which  OS  makes  a  positive  right  angle  round  ON: 

2*313.  The  bilinear  curvature  KST  is  the  projection  in  the  direction 
with  which  OS  makes  a  positive  right  angle  of  the  spin  of  the  current 
tangent  plane  as  0  moves  in  the  direction  OT. 

Another  aspect  is  presented  if  the  spin  of  the  tangent  plane  is 
related  to  the  velocity  of  the  Gaussian  image ;  the  latter  of  these 
vectors  is  obtained  by  rotating  the  former  through  a  negative  right 
angle  in  the  tangent  plane  and  therefore 

2'314.    The  bilinear  curvature  KST  is  the  projection  in  the  direction 
reverse  to  OS  of  the  velocity  of  the  Gaussian  image  of  0  with  respect 
to  the  arc  of  any  curve  in  the  direction  OT. 
This  result  can  be  expressed  in  symbols  in  the  form 

2-315  KST  =  ~  c?(dlN/dsT)  ls, 

and  is  deducible  algebraically  from  the  definition  2*311,  for  since 
</lsliN  is  always  zero, 

2-316.  J(dls/dt)  1N  +  c?(dlN/dt)  ls  =  0, 

whatever  the  variable  t. 

2*32.  The  relation  of  bilinear  curvature  to  normal  curvature  is 
seen  immediately  from  2*211  and  2'311 : 

2*321.  The  bilinear  curvature  of  a  surface  reduces  to  the  normal 
curvature  when  the  directions  on  which  it  depends  coincide. 

But  the  part  to  be  played  by  the  bilinear  curvature  in  coordinating 
properties  of  different  functions  of  a  single  direction  is  better  ap- 
preciated after  a  comparison  of  2'315  with  2*112  and  2'113;  the 
identity  of  /cn  with  KTT  appears  again,  and  9^  is  seen  to  be  KET  : 

2*322.  If  OE  is  the  tangential  direction  making  a  positive  right 
angle  with  OT,  the  bilinear  curvature  KET  is  the  geodesic  torsion  of 
the  surface  along  OT. 

In  virtue  of  2'321  and  2*322,  2*111  may  be  written 

2*323  d].NfdsT  =  —  KTT\T  —  KET^-E> 

and  it  follows  that  if  P  r  is  any  linear  function  of  a  vector, 

2*324       P  (dlN/dsT)  =  —  KTTPT  —  xETPE  =  —  K^TP^ , 
because  OT  and  OE  are  at  right  angles. 

2*33.  The  apparent  duplicity  of  2'312  has  been  removed  in  2'313 
by  means  of  the  definite  directions  OS  and  OD;  it  may  be  removed 


26 

otherwise  by  the  use  of  OT  and  OE:  since  the  spin  along  OTis  the 
sum  of  Kn  about  OE'  and  9^  about  0 T, 

2*331  KST  —  KU  cos  eST  —  $g  sin  €ST, 

a  formula  which  in  the  form 

2*332  KST  =  KTT  sin  eSE  +  KET  sin  eTS 

merely  expresses  the  linearity  of  the  function  in  the  direction  OS. 

2*41.  The  tangential  component  of  dls/dsT  being  necessarily  at 
right  angles  to  OS,  its  direction  of  measurement  can  be  chosen  and 
an  unambiguous  scalar  obtained;  the  amount  of  the  tangential 
component  in  the  direction  which  makes  a  positive  right  angle  with 
OS  I  call  the  swerve  of  OS  along  OT  and  denote  by  o-Ts,  or  by  (7s  only 
if  the  manner  of  the  dependence  on  OT  can  be  assumed: 

2*411  o-Ts  =  c?(dIs/dsT)lD. 

The  swerve  of  OS  along  OT  is  the  rate  at  which  OS  rotates  about 
ON  as  0  moves  in  the  direction  of  OT;  hence  if  OR,  OS  are  any 
two  tangential  directions  dependent  on  the  position  of  0, 

2  412  or/  —  <TTR  =  deES/dsT: 

The  swerve  of  OS  in  any  direction  exceeds  the  swerve  of  OR  in  the 
same  direction  by  the  rate  of  change  of  an  angle  from  OR  to  OS. 

From  this  theorem  comes  a  method  of  evaluating  crs  by  means 
of  a  curve  in  the  direction  of  OT,  for  from  2'212  and  2-411  it  follows 
that  <TTT  is  Kgt  that  is,  that 

2'413.  If  OT  is  the  current  tangent  to  a  curve  on  a  surface  the 
swerve  of  OT  along  OT  is  the  geodesic  curvature  of  the  curve, 

and  therefore 

2-414  as  =  KO  +  (d€TS/ds). 

The  swerve  as  is  equal  to  /cg  if  €TS  has  any  constant  value,  and 
in  particular 

2-415  <rTE=Kg. 

2'42.  If  the  direction  OS  depends  only  on  the  position  of  0,  the 
vector  dls/dsT  is  a  linear  function  of  OT,  arid  therefore  since  the 
swerve  is  the  projection  of  this  vector  in  a  direction  independent 
ofOT, 

2*421.  The  swerve  along  OT  of  a  tangential  direction  which  depends 
only  on  tlie  position  of  0  is  a  linear  function  of  OT. 


27 

Hence 

2'422  <TTS  sin  o>  =  crAs  sin  /3  4-  <TBS  sin  or, 

and  so  in  particular 

2'423  <7-rr  sin  o>  =  o-^T  sin  @  4-  crBr  sin  a, 


2-424 


r  jf  sin  ft)  =  <TAA  sin  /3  +  aBA  sin  a, 
JTTB  sin  ft)  =  O-AB  sin  /3  4-  crBB  sin  a, 


formulae  which  by  2'414  are  equivalent  to 

2425       Kg  sin  &>  =  {kg  +  (cfo/c?s)}  sin  /3  +  {^  —  (d/3/ds)}  sin  a, 
2'426    ["{#0  —  (da/ds)}  sin  &>  =  ^  sin  /3  4-  }^  —  (dco/ds)}  sin  a, 
_{A:?  +  (dff/ds)}  sin  a>  =  {^  -f  (dai/dl)}  sin  j3  +  Kg  sin  a, 
where  ^ ,  ^  are  the  geodesic  curvatures  of  the  curves  of  reference 
and  s,  s  are  arcs  of  these  curves.   The  last  two  formulae  can  be  used 
for  isolated  curves,  but  2*425  supposes  OT  to  be  known  not  merely 
along  a  particular  curve  but  along  the  reference  curves  also,  and  is 
therefore  available  only  in  the  discussion  of  the  typical  member  of 
a  family  of  curves;  in  otherwords,  2'425  assumes  a  definite  tangential 
direction  to  be  associated  with  every  point  on  the  surface  and  gives 
the  geodesic  curvature  at  0  of  the  particular  curve  which  passes 
through  0  and  has  at  every  one  of  its  points  the  direction  corre- 
sponding to  that  point. 

2'51.   The  definitions  2*311,  2'411  are  combined  in  the  equation 

2'511  dls/dsT=  KST\N  +  <TTS\D, 

which  has  for  particular  cases  2 '2 13  and 

2'512  dlE/dsT  =  sglN— KglT. 

The  three  formulae  2-213,  2'512,  2111  express  that 

2'513.    The  frame  OTEN  has  the  spins  9^,  —  /cn,  tcg; 
the  calculation  of  the  vector  dls/dsT  by  means  of  this  moving  frame 
reproduces  2'511,  if  KST  and  aTs  are  regarded  as  defined  by  2'331 
and  2-414. 

2'52.  To  the  first  writers  on  differential  geometry,  to  associate 
the  curvatures  and  torsions  of  curves  on  a  surface  with  the  form  of 
the  surface  itself  was  the  fundamental  problem,  and  if  the  problem 
has  lost  its  interest  with  its  difficulties,  the  solution  is  not  the  less 
valuable.  Supposing  a  curve  and  its  tangential  indicatrix  both  to  be 
free  from  stationary  points,  a  choice  of  direction  along  the  principal 


28 

normal  at  a  single  point  fixes  the  standard  direction  OP  along 
the  current  principal  normal  everywhere,  and  renders  determinate 
the  binomial  direction  OB  and  the  sign*  of  the  curvature.  The 
fundamental  trirectal  OTPR  has  no  spin  about  OP,  and  its  spins 
about  OB  and  OTare  the  curvature  K  and  the  torsion  ?  of  the  curve. 
If  a  curve  is  on  a  given  surface,  a  continuously  varying  angle, 
determined  by  choice  at  a  single  point,  from  OP,  the  principal 
normal  of  the  curve,  to  ON,  the  normal  to  the  surface,  is  called 
the  normal  angle  of  the  curve  on  the  surface  and  denoted  by  OT. 
The  spin  of  the  trirectal  OTEN  differs  from  that  of  the  trirectal 
OTPB  only  by  the  addition  of  a  component  of  amount  dtsjds  about 
OT;  hence  the  spin  of  OTEN  is  compounded  of  9  4-  (d-&/ds)  about 
OT  and  K  about  OB,  and  since  the  latter  of  these  components  is  the 
sum  of  K  cos  OT  about  OE'  and  K  sin  OT  about  ON,  2513  shews  that 

2'521.  The  normal  curvature,  the  geodesic  curvature,  and  the 
geodesic  torsion,  of  a  curve  on  a  surface  are  related  to  the  curvature 
and  torsion  of  the  curve  in  space  by  the  formulae 

Kn  =  K  cos  OT,     Kg  —  K  sin  OT,     s^  =  9  +  (div/ds), 
where  OT  is  the  normal  angle. 

2'61.  In  dealing  with  a  family  of  surfaces  it  is  necessary  to  con- 
template the  variation  of  normal  and  tangential  radials  when  the 
current  point  is  no  longer  confined  to  a  single  surface.  Since  a  rate 
of  change  in  any  oblique  direction  can  be  calculated  by  means  of 
normal  and  tangential  rates  of  change,  the  rates  of  change  that  have 
now  to  be  discussed  are  normal,  that  is,  are  rates  of  change  as  the 
current  point  describes  an  orthogonal  trajectory  of  the  family,  and 
the  arc  of  this  curve  will  be  denoted  by  n.  The  vectors  to  be 
examined  have  the  forms  dlsjdn  and  dlN/dn. 

2*62.  To  suggest  the  evaluation  oi'dls/dn  presupposes  that  along 
the  particular  orthogonal  trajectory  under  consideration  there  is 
associated  with  each  position  of  0  a  definite  direction  OS  tangential 
to  the  surface  through  0;  the  vector  dls/dn  is  then  a  vector  in  the 
plane  ODN  and  is  naturally  described  by  its  projections  on  OD  and 
ON.  The  vector  dIN/dn  is  the  vector  of  curvature  of  the  trajectory 

'  The  common  convention  that  in  solid  geometry  this  sign  must  be  positive  is 
mischievous  beyond  words.  The  curvature  of  a  curve  is  in  fact  the  amount  of  a 
vector,  positive  if  measured  in  one  direction  and  negative  if  measured  in  the  reverse. 


29 

and  is  not  itself  dependent  on  particular  tangential  directions,  but 
to  describe  it  by  means  of  scalars  reference  to  specific  directions 
must  be  made;  by  a  choice  of  tangential  directions  having  intrinsic 
relations  to  the  surface  a  purely  intrinsic  account  of  dlN/dn  can  be 
given,  but  not  only  do  applications  involve  the  projection  of  dlN/dn 
on  an  arbitrary  tangential  direction  OS,  but  since  the  directions 
OS,  ON  are  at  right  angles,  this  projection  is  the  negative  of  the 
projection  </(dls/dn)  1N  which  is  in  any  case  required  in  connection 
with  dls/dn. 

2'71.  The  tangential  component  ofdls/dn,  which  I  call  the  swing 
of  OS  round  ON,  is  related  to  ON  just  as  the  swerve  of  OS  along 
OT  is  related  to  0  T,  and  the  notation  of  2*41  can  be  adopted: 

2-711  <rN8  =  J(dlsldn)lD. 

In  fact  if  OS  and  OD  are  directions  depending  only  on  the 
position  of  0,  the  projection  <£(dls/dsp)  1D  has  the  same  value  for 
all  curves  in  the  direction  OP,  whether  this  direction  is  tangential, 
oblique,  or  normal,  and  the  function  aps  defined  by 

2712  <rPs  =  J(dls/d8p)lD 

is  a  linear  function  of  OP. 

The  result  expressed  by  2*412  is  true  whatever  the  direction  of 
the  curve  involved,  and  in  particular 

2'713  a-Ns  -  aNR  =  deES/dn, 

so  that 

2'714.  If  the  angle  bettveen  two  tangential  directions  is  constant 
along  a  trajectory  the  directions  have  the  same  swing  about  the  normal. 

2'72.  To  use  2'713  for  the  calculation  of  swings,  the  swing  of 
some  one  direction  must  be  known.  Anticipating  acquaintance  with 
the  principal  tangents  of  a  surface,  we  observe  that  because  these 
tangents  are  at  right  angles  on  every  surface,  the  four  principal 
directions  have  the  same  swing;  this  swing  I  call  the  twist  of  the 
family  and  denote  by  TV.  From  2'713, 

2-721  cr/  =  nr 


where  f  is  an  angle  to  OS  from  a  principal  direction  of  the  surface; 
this  formula  breaks  down  at  an  umbilic,  and  is  quite  useless  if  the 
family  is  composed  of  planes  or  spheres,  when  the  principal  directions 


30 

are  everywhere  indeterminate,  but  in  general  the  twist  is  the  first 
swing  to  be  calculated. 

Referring  for  a  moment  to  a  topic  less  elementary  than  will  occupy 
us  in  these  pages,  it  may  be  mentioned  that  the  vanishing  of  the 
twist  is  the  necessary  and  sufficient  condition  for  a  family  not  com- 
posed of  planes  or  spheres  to  be  a  Lame  family,  that  is,  to  be  one 
of  three  families  forming  a  triply  orthogonal  system. 

2'73.    We  shall  write 

2-731  TS  =  J(dls/dn)ly, 

and  call  the  function  TS  the  spread  of  the  family  along  OS.  Being  a 
linear  function  of  OS,  the  spread  is  given  with  reference  to  any  two 
tangential  directions  OA,  OB  by  a  formula  of  the  usual  type: 

2732  rssinft)  =  TA  sin /3S  +  rBsmas. 

274.  Combining  2731  with  2711,  and  noting  that  dls/dn  is 
necessarily  at  right  angles  to  1>S,  we  have 

2741  dls/dn  =  o-Ns!D  +  TS  1N. 

2*81.   As  has  been  perceived  in  2'62, 
2-811  TS  =  -J(dl2f/dn)ls. 

The  tangential  vector  d\Njdn  can  be  expressed  by  its  projections 
on  any  two  tangential  directions: 

(dlN/dn)  sin  eST  =  {£(dIN/dn)  1D]  1T  -  {£(dlN/dn)  1E]  ls, 
that  is, 

2'812  (dlN/dn)  sin  eST  =  TE  ls  —  rD\T. 

In  particular 

2-813  dlN/dn  =  -  rsls  -rDlD, 

which  combines  with  2741  to  express  that 

2'814.  With  respect  to  the  arc  of  the  orthogonal  trajectory,  the 
frame  OSDN  has  spins  TD,  —  rs,  &NS. 

With  2*741  and  2*813  can  therefore  be  associated 
2-815  dlD/dn  =  -  <TNS  ls  +  TD  1N, 

but  this  is  only  another  version  of  2741,  for  &ND  has  the  same  value 
as  <rNs,  and  OS  makes  a  negative  right  angle  with  OD. 

2'82.    That  dlN/dn  is  the  vector  of  curvature  of  the  trajectory 


31 

must  not  be  overlooked.    Formulae  giving  the  curvature  in  terms 
of  spreads  are 

2*821  Ac2  sin2  €ST  =  T/  —  2rs TT  cos  €ST  +  rr2, 

which  is  general,  and 

2-822  *2  =  rs2  +  V, 

where  OD  and  OS  are  as  usual  perpendicular. 

2'83.  Comparison  of  2'814  with  2*513  suggests  a  valuable  out- 
look on  the  functions  <TNS,  rs.  Suppose  a  surface  drawn  to  contain 
the  trajectory  under  consideration  and  to  have  OS  for  a  tangential 
direction  at  every  point  of  this  curve;  ONS  is  the  tangent  plane 
to  this  surface  at  0,  and  if  OD  is  taken  for  the  positive  normal 
direction,  the  relation  of  the  frame  ONSD  to  the  trajectory  regarded 
as  a  curve  on  this  surface  shews  that 

2*831.  On  any  surface  containing  the  orthogonal  trajectory  and 
having  OD  for  current  normal  along  the  trajectory,  this  curve  has 
geodesic  torsion  aNs,  normal  curvature  —  TD,  and  geodesic  curvature 


3.    Surfaces  and  Multilinear  Functions  associated  with 
a  Function  of  Position  in  Space 

3'11.  Referred  to  a  frame  OABC,  a  function  <l>  of  position  in 
space  becomes  a  function  of  the  coordinates  x,  y,  z  of  the  variable 
point,  and  in  all  that  follows  it  is  assumed  that  the  functions  con- 
cerned are  not  merely  absolute  constants,  and  are  regular. 

If  OQ  denotes  the  value  of  <l>  at  the  point  Q,  the  aggregate  of 
points  for  which  O  has  the  particular  value  OQ  is  the  class  of  points 
satisfying  the  equation 

3111  3>  O,  y,  z)  =  cDa, 

and  is  therefore  in  general  a  surface,  the  <X>-surface  through  Q. 
Singular  points  are  omitted,  and  the  region  considered  is  one 
throughout  which  the  O-surfaces  compose  a  family  of  which  one 
and  only  one  member  passes  through  any  point. 

Conversely,  any  one  surface  is  given  by  a  set  of  equations  of  the 
form 

3112  x=f(u,v\    y=g(u,v),    z  =  h(u,v), 


32 

and  any  family  by  a  set  of  the  same  form  in  which  the  functions  in- 
volve in  addition  to  u  and  v  a  parametric  variable  w.  The  eliminant 
of  u  and  v  from  the  set  of  equations  3112  is  a  relation  between 
x,  y,  z,  and  w  which  within  a  sufficiently  restricted  domain  can  be 
put  into  the  form 

3113  ®(x,y,  z)  =  u). 

Hence  geometrical  properties  of  a  <f>-surface  and  a  <I>-family,  in 
so  far  as  they  do  not  involve  the  function  <£  itself,  are  properties  of 
all  regular  surfaces  and  families  of  surfaces. 

3  '21.  Along  a  curve,  defined  by  the  expression  of  x,  y,  z  as 
functions  of  the  arc  s,  the  function  <I>  has  a  rate  of  change  given  by 


3-211  _ 

ds      dx  ds      dy  ds       dz  ds' 

that  is,  by 

3-212  d^fds  =  <&XXT  +  &yyT  +  ®zZTt 

where  <&x,  <3>y,  <&z,  the  partial  derivatives  of  <1>,  are  themselves 
functions  of  position  having  no  relation  to  the  curve,  while  %T,  yT> 
ZT  are  the  ratios  of  the  direction  OT  of  the  curve.  Thus 

3*213.  The  rate  of  change  of  a  regular  scalar  function  of  position 
in  space  along  any  curve  depends  only  on  the  direction  of  the  curve 
and  is  a  linear  function  of  that  direction. 

The  linear  function  whose  value  in  the  direction  OP  is  the  rate 
of  change  of  <E>  along  any  curve  in  that  direction  will  be  denoted 
by  &lPt  the  corresponding  function  of  the  vector  p  being  written 
4>*p;  as  with  any  other  linear  function, 

3'214  &pp=p&p 

and  ^Ip  is  identical  with  <&1P. 

3'22.  The  source  of  the  linear  function  GPp  is  called  the  gradient* 
of  <E>  at  0,  and  will  be  denoted  by  G  : 

3-221  JQIP  =  ®lp. 

If  G-  is  everywhere  the  zero  vector,  then  <l>  is  an  absolute  constant  ; 
this  case  excepted,  the  region  under  consideration,  though  in  special 
cases  it  may  be  broken  into  a  number  of  separated  parts,  is  not 

*  It  is  not  necessary  to  distinguish  in  practice  between  the  source  and  the  core 
of  a  linear  function. 


33 

sensibly  contracted  by  the  omission  of  the  points  where  G  is  zero. 
The  assumption  is  therefore  made  that  Gr  is  nowhere  zero,  it  being 
understood  that  the  restriction  implied  is  not  on  <E>  but  on  the 
domain  throughout  which  results  are  asserted  to  hold.  Within  a 
united  region  where  G  is  nowhere  zero,  the  two  amounts  of  G  are 
separate  single-signed  functions  of  position,  nowhere  zero ;  one  of 
these  functions,  not  necessarily  the  one  that  is  positive,  is  chosen 
and  called  the  slope  of  <3> ;  the  slope  will  be  denoted  by  G. 

3'23.  At  a  point  0  where  G  is  not  zero,  the  directions  in  which 
the  rate  of  change  of  <E>  is  zero  are  the  directions  at  right  angles 
to  G.  Hence 

3*231.  The  tangent  plane  at  0  to  the  ^-surface  through  0  is  the 
plane  through  0  at  right  angles  to  the  gradient  of  O  at  0, 
and  the  directions  of  the  normal  to  the  <f>-surface  are  the  directions 
of  G;  of  these  directions  the  one  in  which  G  has  the  amount  G  is 
determinate,  and  is  called  briefly  the  normal  direction  at  0.  The 
normal  direction,  denoted  always  by  ON,  varies  regularly  with  the 
position  of  0 ;  hence 

3*232.    Every  ^-surface  is  bifacial  within  a  united  region  where 
<I>  is  regular  and  the  gradient  of  <J>  is  nowhere  the  zero  vector, 
and  the  choice  of  sign  for  the  slope  G  determines  implicitly  the 
direction  of  angular  measurement  in  every  tangent  plane. 

3  31.  The  gradient  of  the  core  <&l  of  the  linear  function  O^  is 
denoted  by  <E>2,  and  the  bilinear  function  <b2P<3  is  called  the  bilinear 
rate  of  change  of  <1>  in  the  directions  OP,  OQ.  Differentiation  of 
the  sum  3>xocP+ <&yyP  +  <&zzP  with  respect  to  a  variable  which  is 
not  involved  in  the  ratios  XP,  yP)  zp  gives 

3-311  <£>2Pa  =  2<&uvuPvQ,     u,  v  =  x,y,  z, 

where  the  summation  covers  the  nine  possible  terms;  since  the 
second  derivatives  <£>uv,  <&vu  are  equal, 

3'312.  The  bilinear  rate  of  change  of  any  regular  function  is 
symmetrical  in  the  two  directions  on  which  it  depends. 

3'32.  If  the  direction  OQ  coincides  with  the  direction  OP,  the 
bilinear  function  4>2pg  becomes  a  function  <£Vp  which  may  be  called 
the  quadratic  rate  of  change  of  <£  in  the  direction  OP.  This  function 
must  not  be  confused  with  the  second  order  rate  of  change 

N. 


34 

which  is  not  the  same  for  all  curves  in  the  direction  OP :  applica- 
tion of  1-722  to 

3-321  d^jdsp  =  <blP 

gives 

3  322    d*<$>ldsp>  =  <$>*pp  +  &  (dIP/dsp)  =  <f>2Pp  +  c?G  (dlP/dsP)} 
and  since  d\pjdsP  is  the  vector  of  curvature  of  the  particular  curve 
along  which  the  rate  of  change  is  being  found,  it  is  only  when  either 
the  curvature  is  zero  or  the  principal  normal  is  tangential  to  the 
^-surface  that  the  last  term  disappears  from  3*322. 

3'41.  The  conception  of  the  bilinear  rate  of  change,  and  the 
fundamental  theorem  3"312,  are  immediately  extended.  The  core 
4>2  has  a  gradient  <£3,  and  so  on,  and  the  multilinear  rate  of 
change  of  <l>  of  degree  k  is  the  function  <&kPQ  r,  where  for  each 
value  of  h  in  succession  <&h+1  is  the  gradient  of  <&h.  With  a  frame 
of  reference, 

3-411     3>*p<2...r  =  2<IV..«,MQ  •  •  •  wr>     *,  t,  . . .  w  =  a,  y,  z, 
the  coefficients  being  the  partial  derivatives  when  <£>  is  expressed  as 
a  function  of  x,  y,  z ;  hence 

3'412.  Every  multilinear  rate  of  change  of  a  regular  function  of 
position  is  symmetrical  in  the  variable  directions. 

3*51.  The  rate  of  change  of  3>  along  any  curve  on  a  <X>-surface 
being  zero, 

3-511  &s  =  0 

if  08  is  restricted  as  usual  to  denote  a  direction  tangential  to  the 
<£- surface  at  0 ;  on  the  other  hand  by  the  definition  of  the  slope 

3-512  &N  =  G. 

From  3-511  and  3'512  together  comes  the  expression  for  Oxr  when 
r  is  arbitrary :  if  r  is  expressed  as  ps  +  qN  where  OS  is  tangential, 
then  because  the  function  <t>xr  is  linear 

3-513  ®1r=p&8  +  q&Nt 

and  substitution  from  3*511  and  3'512  gives 

3-514  &r=Gq, 

that  is, 

3-515  &r  =  G£r\N\ 

this  formula  is  of  course  obvious  from  the  definition  of  G. 


35 


4.    The  Bilinear  Curvature  of  a  Surface 

411.   That 

4111.    The  bilinear  curvature  of  a  surface  is  a  bilinear  function 
of  the  two  tangential  directions  on  which  it  depends 
is  obvious  equally  in  every  expression  given  for  KST  in  2*3,  and  this 
property  alone  implies  such  formulae  as 

4112     KST  sin2  co  =  KAA  sin  @s  sin  /3r  +  KAB  sin  fis  sin  aT 

+  KBA  sm  as  SU1  PT  +  KBB  sni  as  sm  «r> 


where  05,  OT  are  independent  of  each  other, 

4114  daRKST  =  (1  +  daReRS)  KDT  +  (1  -f  daReRT)  KSE, 

if  05,  OT  depend  on  a  tangential  direction  0-B,  and  in  particular 

4115  daKTT  =  KET  +  KTE  =  —  da/cEE, 

4116  da/cTE  =  KEE  —  KTT  =  da/cET, 
special  cases  of  1/822  and  T823. 

412.    Dupin's  theorem,  that 

4121.   At  any  ordinary  point  of  a  surface  the  sum  of  the  normal 
curvatures  in  two  directions  at  right  angles  is  a  constant, 

is  shewn  by  2*321  to  be  a  case  of  1*824,  that  is,  to  follow  from  the 
simple  fact  that  the  normal  curvature  is  a  quadratic  function. 

The  half  of  the  constant  sum  KTT  +  KEE  is  the  mean  curvature  of 
the  surface  at  0,  and  will  be  denoted  by  B  ; 

4122  KTT  +  KEE  =  2B. 

The  differences  /cn  —  B  and  B  —  KH  are  the  excess  and  the  defect 
of  curvature  along  OT.    To  write 

4123  KEE  =  2B-tcn 

is  to  express  KEE  directly  as  a  function  of  OT,  and  the  function 
KEE  —  KTT,  which  appears  in  4116  and  in  a  number  of  other  formulae, 
is  given  by 

4124  KEE  ~  KTT  =  2  (B  -  xn\ 
that  is  to  say,  is  twice  the  defect  of  curvature. 

3—2 


36 

An  actual  formula  giving  the  mean  curvature  is  easy  to  find, 
for  4*112  gives 

4*125    KTT  sin2  o>  =  KAA  sin2  /3  -f  (KAB  +  KBA)  sin  /3  sin  a  +  KBB  sin2  a, 
and  substitution  of  a  +  JTT,  /3  —  J  TT  for  a,  ft  gives 

4*126   KEE  sin2  «  =  /c^  cos2  ft  —  (KAB  4-  KBA)  cos  /3  cos  a  +  KBB  cos2  a, 

whence  by  addition  we  have  not  only  a  trigonometrical  proof  of 
Dupin's  theorem  but  the  explicit  result 

4*127          25  sin2  CD  =  KAA  —  (KAB  +  KBA)  cos  &>  +  KBB. 


4*21.  But  bilinearity  alone  does  not  account  for  the  importance 
of  the  function  KST.  Differentiation  of  3*511  along  a  curve  on  a 
O-surface  gives 

4-211  &8T  +  0>-  (dl8/dsT)  =  0, 

and  substituting  from  3*515  we  see  from  2*311  that 

4*212.  The  bilinear  rate  of  change  of  a  function  <3>  along  two 
directions  OS,  OT  tangential  to  the  ^-surface  is  connected  with  the 
bilinear  curvature  KST  of  the  surface  in  those  directions  by  the  equation 

4-Vr+ftte-O, 

where  G  is  the  slope  of  <E>. 

And  this  result  not  only  enables  the  bilinear  curvature  to  be  calcu- 

lated in  specific  cases,  but  taken  with  3*312  shews  that 

4*213.  At  any  ordinary  point  of  any  surface,  the  bilinear  curva- 
ture in  two  directions  is  a  symmetric  function  of  those  directions. 

From  the  combination  of  this  result  with  4*1  1  1  springs  the  whole 
elementary  theory  of  the  curvature  of  a  surface. 

4*22.    Since  identically 

4*221          sin  /3S  sin  aT  —  sin  as  sin  j3T  =  sin  w  sin  eST, 
the  necessary  and  sufficient  condition  for  4*213  to  follow  from  the 
explicit  formula  4'112  is  the  equality  of  the  coefficients  KAB)  KBA  : 

4  222.  The  symmetry  of  the  bilinear  curvature  for  any  one  pair 
of  distinct  directions  at  a  point  implies  algebraically  the  symmetry 
of  this  function  for  any  other  pair  of  directions  at  the  same  point. 

With  the  substitution  of  KAB  for  KBA,  4*112  takes  the  form 

4*223     KST  sin2  o>  =  KAA  sin  @s  sin  /3r 

+  KAB  (sin  /3S  sin  aT  +  sin  as  sin  /3T)  +  KBB  sin  as  sin  aT> 


37 

giving 

4*224*  /cn  sin2  o>  =  KAA  sin2  ft  +  2/cAS  sin  /3  sin  a  +  tfBJ5  sin2  a, 
4*225    90  sin2  a>  =  —  #^  sin  /3  cos  /3  —  A;^  sin  (a  —  j3) 

+  KBB  sin  a  cos  a, 
and  4127  becomes 

4*226  2B  sin2  &>  =  /e^  —  2tcAB  cos  &>  +  /CB^. 

It  need  hardly  be  said  that  all  relations  between  bilinear  curvatures 
of  one  surface  in  different  pairs  of  directions  at  one  point  are  de- 
ducible  from  4*223  by  pure  trigonometry,  or  that  this  method  of 
deduction  has  nothing  to  recommend  it. 

4'23.  A  simple  case  of  4'213  is  the  assertion  that  if  /e8T,  as  de- 
scribed in  2*3,  is  zero  for  a  particular  pair  of  directions,  then  so  also 
is  KTS.  To  say  that  KST  is  zero  is  to  assert  that  as  0  moves  in  the 
direction  OT  the  tangent  plane  at  0  rotates  about  0$;  in  other 
words 

4'231.  A  pair  of  directions  for  which  the  bilinear  curvature  is 
zero  is  a  pair  of  conjugate  directions. 

Hence  4*213  includes  the  familiar  theorem  that 

4*232.   If  OS  is  conjugate  to  OT  then  OT  is  conjugate  to  OS, 
and  the  application  of  4*222  to  this  result  takes  the  form  that 

4*233.  If  a  surface  is  known  to  have  a  single  pair  of  mutually 
conjugate  distinct  tangents  at  a  point,  the  symmetry  of  the  bilinear 
curvature  at  that  point  can  be  inferred. 

4*24.  By  means  of  2*331  the  symmetry  of  the  bilinear  curvature 
can  be  expressed  as  a  relation  between  the  normal  curvatures  and 
geodesic  torsions  in  two  directions  without  explicit  mention  of  the 
bilinear  function;  comparing  the  two  formulae 

4'241  KST  =  /CTT  cos  €ST  —  KET  sin  eST, 

^TS  ~~  ^ss  cos  €$T  \  &DS  ^1^1  GST 
we  have 

4*242  (  KTT  —  KSS  )  cos  eST  —  (KET  +  KDS)  sin  €ST> 


*  This  formula  shews  that  a  geometrical  theory  without  the  bilinear  curvature  is 
as  incomplete  as  an  analytical  theory  without  the  function  for  which  M  is  used  by 
Scheffers,  Forsyth,  writers  in  the  Encyk.  d.  Math.  Wiss.,  and  others,  D'  by  Bianchi, 
and  D'M(EG  -  F2)  by  Gauss  and  Darboux. 


38 

or  to  use  a  notation  convenient  with  reference  curves 

4*243  (Kn  -  Kn)  cos  w  =  (93  +  90)  sin  &>, 

a  result  given  in  other  symbols  and  used  again  and  again  by  Darboux. 

4*31.  The  relation  between  geodesic  torsions  in  perpendicular 
directions  is  simpler  in  form  than  the  relation  between  normal 
curvatures  asserted  in  Dupin's  theorem,  but  belongs  in  fact  to  a 
more  advanced  stage,  depending  as  it  does  not  on  the  bilinearity 
alone  but  on  the  symmetry  of  the  bilinear  curvature.  To  write 
down  this  relation  from  4'225  or  4' 243  is  of  course  simple  enough, 
but  an  appeal  to  first  principles  shews  more  clearly  on  what  the 
result  depends.  The  linearity  of  KST  in  the  direction  OT  implies 

4'oJ.J.  KST'  ==  —  ^ST' 

and  in  virtue  of  the  symmetry  of  the  function  this  equation  gives 

4'312  KST  +  KT'S  ~  0  J 

hence  in  particular 

4'313  KET  +  KT'E  =  0, 

and  since  OT'  is  the  direction  making  a  positive  right  angle  with 
OE  the  function  KT>E  is  the  geodesic  torsion  along  OE : 

4*314.  The  sum  of  the  geodesic  torsions  in  two  directions  at  right 
angles  is  zero. 

This  result,  like  4*232,  is  a  special  case  of  4*213  and  implies  the 
more  general  theorem  in  which  it  is  included;  thus  4*314  and 
4'232  in  spite  of  their  diversity  of  form  are  theorems  implying 
each  other,  that  is,  are  equivalent  theorems,  on  account  of  the 
bilinearity  of  the  bilinear  curvature. 

4*32.  Brevity  is  often  achieved  by  the  use  of  the  function 
2  (KDT  +  KSE)>  which  is  the  symmetrical  bilinear  function  of  OS  and 
OT  that  reduces  to  the  geodesic  torsion  KET  when  OS  coincides 
with  OT',  it  is  natural  to  write 

4*321  ?sr  =  |  (KDT  +  KSE) 

and  to  call  this  function  the  bilinear  torsion,  but  it  must  be 
recognised  that  the  function  has  none  of  the  fundamental  impor- 
tance of  the  bilinear  curvature.  Identically, 

4*322  9TT  =  KET  =  <>g , 

4*323  9^  =  |  (  KEE  —  KTT)  —  B  —  Kn, 


39 
and  4"314  can  be  expressed  in  the  form 

4-324  *EE  =  -*g- 

Being  bilinear  and  symmetrical,  the  function  <$ST  has  its  value 
given  in  terms  of  directions  of  reference  OA,  OB  by 
4-325    9sr  sin2  w  =  SAA  sin  /3S  sin  jBT 

+  ?AB  (sin  fis  sin  a.T  +  sin  as  sin  /3T)  +  SBB  sin  as  sin  aT. 

But  unlike  the  coefficients  KAA,  KAB,  KBB,  the  coefficients  SAA,  SAB, 
<f£B  are  not  numerically  independent,  for  the  sum  9rr  +  <$EE  is  not 
merely  constant  but  is  zero  : 

4'326  SAA  —  ^AB  cos  a)  +  ?£B  =  0. 

4'33.  The  angular  derivatives  of  the  normal  curvature  and 
geodesic  torsion  are  given  in  4']  15  and  4*116.  Since  KTE  as  well 
as  KET  is  9^  the  first  of  these  formulae  becomes 

4-331  daKn  =  ^g, 

a  familiar  result;  4*116  is  equivalent  to 

4-332  da  90  =  2  (£-*„), 

which  is  therefore  more  elementary  than  4*331  since  it  is  proved 
without  reference  to  the  symmetry  of  KST.  There  is  a  temptation 
to  replace  4'331  by 

4-333  da(icn-B)  =  2sg 

and  to  treat  as  correlative  the  geodesic  torsion  and  the  excess  of 
curvature,  but  the  suggested  analogy  must  not  be  pressed  too  far. 
Written  in  the  forms 


4*331,  4-332  are  seen  to  be  corollaries  of  the  more  general  theorem 
that 

4*334.   //"  OS  is  inclined  to  OT  at  a  constant  angle,  then 


an  immediate  deduction  from  4*1  14. 

4'41.  A  function  of  direction  that  is  not  a  mere  constant  must 
have  at  least  one  direction  of  maximum  value  and  one  of  minimum. 
If  OT  is  a  direction  along  which  the  value  of  /cn  is  a  minimum, 
then  the  value  along  OT'  is  the  same  minimum,  while  it  follows 
from  Dupin's  theorem  that  along  OE  and  OE'  the  value  is  a 
maximum.  Hence  unless  /cn  has  the  same  value  in  every  direction 


40 

from  0,  there  certainly  are  two  distinct  tangents  along  which  the 
value  of  /cn  is  stationary.  On  the  other  hand,  4'331  implies  that  a 
tangent  along  which  /cn  is  stationary  is  a  tangent  along  which  9^  is 
zero,  and  since  sg  is  a  quadratic  function  there  cannot  be  more 
than  two  of  these  tangents  unless  sg  is  zero  in  every  direction. 

4*411.  At  an  ordinary  point  of  a  surface,  either  the  normal 
curvature  is  the  same  in  all  directions  and  the  geodesic  torsion  is 
zero  in  every  direction,  or  there  is  one  tangent  along  which  the 
normal  curvature  has  its  least  value  and  one  along  which  the  normal 
curvature  has  its  greatest  value,  these  tangents  are  at  right  angles 
and  are  the  only  tangents  along  which  the  geodesic  torsion  is  zero, 
and  the  normal  curvature  in  a  variable  direction  increases  or  de- 
creases steadily  as  the  direction  rotates  from  one  of  these  tangents 
to  the  other. 

A  point  at  which  the  normal  curvature  has  the  same  value  in  all 
directions  is  an  umbilic ;  the  constant  value  is  of  course  equal  to 
the  mean  curvature  B  at  the  point. 

4-42.  From  4'332  and  4'333  it  follows  that  the  sum  (KU  -  B)~  +  9/ 
does  not  vary  with  OT  but  is  a  function  only  of  the  position  of  0 
on  the  surface,  in  general  positive  but  zero  if  and  only  if  0  is 
umbilical.  Spheres  and  planes  are  composed  wholly  of  umbilics, 
but  from  a  surface  that  is  neither  plane  nor  spherical  the  umbilics 
can  be  removed,  for  it  can  be  proved  that  they  are  isolated  points 
or  compose  isolated  curves.  Throughout  a  region  which  is  nowhere 
umbilical,  the  two  square  roots  of  (/rn  —  B)z  +  sy*  are  separate  single- 
valued  functions  of  position ;  one  of  these,  selected  and  called  the 
amplitude -of  curvature,  will  be  denoted  by  A  : 

4-421  (*n-fl)'  +  9/  =  4a. 

From  4  421  the  extreme  values  of  Kn  at  a  point  0,  corresponding 
to  the  directions  along  which  9^  is  zero,  are  B  —  A  and  B  +  A  ; 
these  are  the  principal  curvatures  of  the  surface  at  0,  and  I  write 

4-422  ^  =  B-A,    *t  =  JB  +  A. 

The  principal  tangents,  that  is,  the  tangents  along  which  the 
normal  curvatures  are  »T,  xz,  are  individually  determinate  when 
the  sign  of  A  has  been  chosen.  To  secure  complete  freedom  from 
ambiguity,  definite  directions  along  these  tangents  must  be  chosen 
also;  the  choice  along  one  principal  tangent  at  one  point  is  arbi- 


41 

trary,and  determines  the  standard  direction  along  the  corresponding 
tangent  at  all  neighbouring  points ;  the  standard  direction  along 
the  other  principal  tangent  is  then  fixed  by  the  convention  that 

4"423.    One  of  the  angles  from  the  first  principal  direction  to  the 
second  is  a  positive  right  angle. 

The  principal  directions  at  0  will  be  denoted  by  0(7t,  OCZ,  but 
as  affixes  t,  z  will  be  substituted  for  (7T,  Cz. 

4'43.    The  equation 

4-431  KET  =  Q 

which  characterises  the  directions  of  curvature  implies  of  course 

4-432  KE'T=Q, 

and  is  therefore  equivalent  to  the  combination  of 

4-433  KST  =  0 

with  the  condition  that  OS  and  OT  are  at  right  angles : 

4'434.   At  any  ordinary  point  that  is  not  an  umbilic,  the  principal 
tangents  are  the  only  two  conjugate  tangents  at  right  angles. 

4'44.    From  the  definitions  and  the  convention  of  4*423, 

4  4:41  KU  =  Xl)        KIZ  =  U,        Kzz  =  HZ) 

4-442  6l5  =  i7r. 

Substitution  in  4'223  gives  for  any  two  directions 

4*443  KST  =  #t  cos  fs  cos  fy  +  #s  sin  £s  sin  fy , 

where  f  denotes  an  angle  to  the  variable  direction  from  the  first 
principal  direction;  the  forms  corresponding  to  4*224  and  4'225 
which  are  special  cases  of  4*443  are 

4*444  Kn  =  #T  cos2  f  +  *5  sin2  f, 

4-445  93  =  (#g  —  ^T)  cos  f  sin  f , 

the  formulae  of  Euler  and  Bonnet,  of  which  the  first  was  transformed 
by  Euler  himself  into  the  shape 

4-446  Kn  =  B-A  cos  2f 

and  the  second  is 

4-447  93  =  A  sin  2?, 

A,  B  having  the  meanings  assigned  in  4*11  and  4*42.  Corollaries 
of  4*444  are 

4-448      •     Kn-»  =  24sin8,     •v-*n  =  24  cos*  , 


42 

which  with  4 '447  give 

4--44.Q  c  2  _  (v       u-  \( u-       v\ 

•x  Tf±«/  S^    --  \-"z       Kn)\Kn       *t/» 

a  relation  which  is  otherwise  evident  from  4'421. 

4'45.  To  relate  4'443  to  the  fundamental  property  of  a  direction 
of  curvature  is  a  most  instructive  exercise,  if  OC  is  a  direction  of 
curvature  and  #  is  the  corresponding  principal  curvature  tccc,  the 
spin  along  OC  is  a  vector  of  amount  »  in  the  direction  with  which 
OC  makes  a  positive  right  angle,  and  therefore  the  projection  of 
this  vector  on  the  direction  OE'  with  which  OT  makes  a  positive 
right  angle  is  #  cos  6CT: 

4'451.  If  OC  is  a  direction  of  curvature  and  *  is  the  correspond- 
ing principal  curvature,  the  bilinear  curvature  KCT  has  the  value 
y*  cos  ^cj1' 

Thus 

*  iO^j  K\T  ^~     i  COS  Cy,       f£~-T  =~     5  Sin  CT") 

because  KST  is  linear  in  OS  and  the  principal  directions  are  at  right 
angles, 

4'453  KST  =  KIT  cos  fs  +  KZT  sin  %s, 

and  substitution  from  4 '452  reproduces  4'443. 

4'46.  Nor  is  the  proof  of  4'443  just  given  the  only  use,  or  the 
chief  use,  of  4'451 ;  it  is  from  4'451  that  come  formulae  for  deter- 
mining the  principal  curvatures  and  tangents  in  terms  of  magni- 
tudes related  to  arbitrary  tangential  directions  of  reference. 

Because  KAT  and  KTB  are  linear  in  OT, 

4'461  \~KAT  sm  w  ~  KAA  gin  P  +  KAB  sm  a> 

_KTB  sin  co  =  KAB  sin  0  +  KBB  sin  a, 
for  any  tangential  direction,  while  from  4'451 

4'462  KAC  =  *  cos  ac,     K(]B  =  #  cos  /3C, 

for  a  principal  direction  OC.    Hence 

4'463.  A  direction  of  curvature  in  which  the  normal  curvature 
is  x  is  characterised  by  the  pair  of  equations 

~KAA  sin  ft  +  KAB  sin  a  =  *  sin  co  cos  a, 

_KAB  sin  ft  +  KBB  sin  a  =  ^  sin  co  cos  ft. 

Elimination  of  »  reproduces  the  equation  obtained  more  simply  by 


43 

equating  to  zero  the  geodesic  torsion  as  given  by  4*225.  On  the 
other  hand,  since  identically 

sin  co  cos  a  =  sin  ft  +  cos  co  sin  a,     sin  co  cos  ft  =  sin  a  +  cos  co  sin  ft, 
the  equations  of  4*463  can  be  written  as 

4'464          \~(KAA  ~  x)  sin  0  +  (KAB  ~  *  cos  co)  sin  a  =  0, 

(./•  _  -v  /TkO  /-.i  i  eiTi   /Q    i    ^  «/•          •!/  j  em  n  —  (\ 

>*-AB        **  wVQ      /  ""-1  r-'    i^  V     BB  /  "•*•*•*•  M,  —  w. 

Elimination  of  the  ratio  sin  /9  :  sin  a  yields  an  equation  which  x 
must  satisfy,  and  since  this  equation  is  quadratic,  it  has  no  roots 
except  #T  and  *z\ 

4*465.  The  principal  curvatures  of  a  surface  are  the  roots  of  the 
equation 

(*  -  KAA)  (»  ~  *BB)  =  0  cos  co  -  KAB}\ 

The  equation  of  4*465  expands  to 

4*466   #2  sin2  co  —  *  (KAA  —  2tcAB  cos  co  +  KBB) 

-I-  (if          if  -if        2^  —  0 

»    \KAA  KBB         KAB  )  —  V, 

and  therefore  2B,  which  is  the  sum  of  the  principal  curvatures, 
and  the  product  of  these  curvatures,  which  is  the  specific  or 
absolute  curvature  of  the  surface  at  0,  and  is  denoted  always  by 
K,  are  given  by 

4*467  2B  sin2  co  =  KAA  —  %KAB  cos  co  +  KBB) 

which  has  been  obtained  already  in  4*226,  and 
4*468  K  sin2  co  =  KAA  KBB  —  KAB*  ; 

the  amplitude  of  curvature  is  determined  numerically  from  the 
identity 

4*469  &-A*=K. 

4*47.  The  fluctuations  of  the  geodesic  torsion  9^  are  seen  most 
readily  from  Bonnet's  formula  4*447 ; 

4*471.  The  extreme  values  of  9^  are  —A  and  A,  and  these  are 
assumed  in  the  directions  midway  between  consecutive  principal 
directions. 

The  discussion  of  STT  as  the  function  denned  by  identifying  OS 
with  OT  in  4*325  is  parallel  to  the  discussion  of  *:rras  the  function 
given  by  identifying  OS  with  OT  in  4*223,  and  therefore  the  extreme 
values  of  <$TT  have  for  their  sum  (?AA  —  2s\4B  cos  co  +  9BB)  cosec2  co  and 


44 

for  their  product  (9^  SBB  —  SAB}  cosec2  a>.    Thus  4'326  is  reproduced, 

and  the  amplitude  of  curvature  is  seen  to  be  given  by  the  equation 

4-472 


4'48.  If  sin  a  and  sin  /9  are  both  known,  the  direction  OT  is 
determinate,  but  the  ratio  of  the  sines  alone  does  not  distinguish 
OT  from  OT'.  Thus  in  general  when  n  has  a  definite  one  of  its 
possible  values,  either  equation  in  4P464  defines  the  corresponding 
principal  tangent  but  not  the  corresponding  principal  direction. 
These  formulae  however  render  precise  a  detail  left  vague  in  4'42. 
If 

4*481  sin  a/p  =  sin  (3/q  =  sin  co/r, 

where  p,  q,  r  are  functions  of  position  on  the  surface,  then 

4'482  r-  =  p2  +  2pq  cos  w  +  cf, 

and  throughout  a  region  where  p  and  q  do  not  vanish  simultaneously, 
r  is  a  single-signed  function  determined  everywhere  by  4  482  if  its 
sign  is  known.  Hence  the  choice  of  sign  of  a  single  radical  deter- 
mines the  principal  direction  corresponding  to  the  principal  curva- 
ture *  throughout  the  whole  of  a  region  provided  that  no  points 
are  included  where  simultaneously 

4'483  KAA—M>      KAB  =  xcosa>,      Kr,K  —  y' 

But 

KAB  =  KAA  COS  o> 
implies  that  OA  is  a  direction  of  curvature, 

KAB  =  *BB  cos  o> 

implies  that  OB  is  a  direction  of  curvature,  and  since  by  hypothesis 
OA,  OB  lie  along  distinct  tangents,  KAA  and  KBB  are  the  extreme 
values  of  the  normal  curvature,  and  the  additional  equality 

KAA   —  KBB 

implies  that  0  is  umbilical:  having  excluded  umbilical  points  for 
the  purpose  of  separating  the  principal  curvatures,  we  have  actually 
obtained  a  region  in  which  the  various  principal  directions  also  are 
separated. 

4'49.  On  any  surface,  a  curve  whose  tangent  at  every  point  is  a 
principal  tangent  of  the  surface  there,  or  in  other  words  whose 
geodesic  torsion  is  everywhere  zero,  is  called  a  line  of  curvature  of 
the  surface.  Throughout  a  united  region  containing  no  singular  or 


45 

umbilical  points,  the  two  principal  directions  at  0  are  definite 
directions  depending  regularly  on  the  position  of  0.  It  follows  from 
the  theory  of  differential  equations  that  over  such  a  region  there 
are  two  distinct  families  of  lines  of  curvature  and  that  through  each 
point  passes  one  and  only  one  member  of  each  family. 

If  F  is  a  regular  function  of  position  of  any  kind  on  the  surface, 
the  values  at  0  of  the  rates  of  change  of  F  in  the  two  positive 
directions  along  the  two  lines  of  curvature  through  0  depend  only 
on  the  position  of  0  and  define  by  their  relations  to  0  two  functions 
of  position  which  will  be  denoted  by  dF/dsl,  dF/dsz.  These  functions 
are  not  partial  derivatives;  if  in  order  to  use  sl  and  sz  as  actual 
coordinates  we  go  so  far  as  to  define  the  position  of  0  by  its  distances 
from  two  selected  trajectories  measured  along  lines  of  curvature,  it 
is  still  impossible  to  secure  that  every  curve  along  which  s^  has  a 
constant  value  is  itself  a  line  of  curvature  or  has  sl  for  its  arc;  thus 
even  in  this  case  the  partial  derivative  dF/dsl  is  not  the  rate  of 
change  in  the  direction  to  which  it  does  correspond  and  bears  no 
intrinsic  relation  to  dF/ds^  It  follows  that  although  there  are  rates 
of  change  cPF/dsf,  d'2F/dszdsl  derivable  from  dF/dsl  and  rates  of 
change  dPF/dsidSs,  d2Fjds£  derivable  from  dF/dsz,  there  is  no  reason 
to  anticipate  equality  ofd?F/d8idst  to  d^F/ds^ds^,  in  point  of  fact  it 
is  easy  when  Fis  scalar  to  evaluate  the  difference  between  d?Fjdsldst 
and  d2F/dszdsl  and  to  recognise  the  rare  cases  in  which  this  difference 
vanishes. 

4'51.  A  direction  of  curvature  is  a  direction  in  which  the  geodesic 
torsion  is  zero.  If  there  are  directions  in  which  the  normal  curvature 
is  zero,  these  directions,  which  are  called  asymptotic,  have  properties 
not  less  interesting  than  have  the  directions  of  curvature. 

Since  the  normal  curvature  at  0  varies  continuously  between  its 
extreme  values  #r,  #r.,  the  existence  of  asymptotic  directions  depends 
on  the  relation  between  the  signs  of  these  two  curvatures,  that  is, 
depends  on  the  sign  of  the  product  K.  If  K  is  strictly  positive,  there 
are  no  asymptotic  directions  and  0  is  said  to  be  an  elliptic  point  on 
tjje  surface.  If  K  is  zero,  one  if  not  both  of  the  principal  curvatures 
vanishes,  and  0  is  said  to  be  parabolic.  For  both  of  the  principal 
curvatures  to  vanish,  that  is,  for  a  point  to  be  umbilical  as  well  as 
parabolic,  is  altogether  exceptional  on  any  surface  but  a  plane.  At 
an  ordinary  parabolic  point,  one  only  of  the  principal  curvatures 


46 

vanishes,  and  the  asymptotic  directions  are  the  corresponding  direc- 
tions of  curvature.  A  developable  is  a  surface  composed  wholly  of 
parabolic  points,  but  on  a  surface  that  is  not  developable  the  para- 
bolic points  in  general,  if  there  are  any,  compose  a  curve  or  a  number 
of  distinct  curves  separating  regions  throughout  which  K  is  positive 
from  regions  throughout  which  K  is  negative.  In  discussing 
asymptotic  directions  attention  is  confined  in  the  first  place  to  a 
united  region  composed  wholly  of  hyperbolic  points,  that  is,  of  points 
where  K  is  strictly  negative. 

4*52.  Between  consecutive  directions  of  curvature  at  a  hyperbolic 
point,  there  is  one  and  only  one  direction  in  which  KH,  changing  in 
sign  from  the  sign  of  #t  to  the  sign  of  #5,  is  zero;  thus  there  are 
four  distinct  asymptotic  directions,  and  since  the  reverse  of  an 
asymptotic  direction  is  itself  asymptotic  these  are  the  four  directions 
along  two  asymptotic  tangents. 

With  a  direction  of  curvature  is  associated  the  corresponding 
normal  curvature,  which  is  a  principal  curvature  of  the  surface.  In 
the  case  of  an  asymptotic  direction  it  is  the  geodesic  torsion  that 
survives,  and  this  magnitude  is  called  the  asymptotic  torsion 
associated  with  the  direction. 

The  fundamental  relation  of  an  asymptotic  direction  01  to  an 
arbitrary  direction  OT  corresponds  to  4'451.  The  spin  of  the  surface 
as  0  moves  in  the  asymptotic  direction  01  has  no  component  at 
right  angles  to  01  but  is  simply  a  spin  of  amount  ?/7  about  01,  if 
?/7  is  the  asymptotic  torsion  along  07;  the  projection  of  this  spin 
in  the  direction  OE'  is  therefore  <?7/  sin  e/r: 

4'521.  //  01  is  an  asymptotic  direction  and  ?7/  is  the  correspond- 
ing asymptotic  torsion,  the  bilinear  curvature  KIT  has  the  value 
9/j  sin  eIT. 

If  OJ,  OK  are  two  asymptotic  directions  at  0,  the  bilinear 
curvature  KJK  is  shewn  by  4'521  to  be  expressible  both  as  <tjj  sin  eJK 
and  as  9^  sin  eKJ\  it  follows  without  reference  to  the  principal 
directions  that 

4*522.    The  two  asymptotic  torsions  at  a  hyperbolic  point  of  a 
surface  are  equal  in  magnitude  and  of  opposite  sign, 
and  it  follows  also  that  if  the  existence  of  two  distinct  asymptotic 
tangents  is  known  4'522  implies  the  complete  symmetry  of  the 


47 

bilinear  curvature.  To  find  the  actual  values  of  the  asymptotic 
torsions  we  have  only  to  compare  4*521  with  4*451 :  if  0  is  an  angle 
from  01  to  the  first  principal  direction,  then 

4*523  <?//  sin  0  =  Kn  =  »t  cos  0, 

and  since  0  +  \TT  is  an  angle  from  01  to  the  second  principal 
direction, 

4*524  ?//  cos  0  =  KK  =  —  xr,  sin  #; 

the  combination  of  4*523  with  4*524  gives 

4-525  *// =  -*i*«, 

that  is, 

4*526.    The  square  of  the  asymptotic  torsions  is  the  negative  of 
the  specific  curvature, 

a  theorem  usually  ascribed  to  Enneper  but  in  fact  announced  by 
Beltrami  four  years  earlier  than  by  Enneper. 

4*53.    For  the  determination  of  asymptotic  directions  from  arbi- 
trary directions  of  reference  4*521  is  again  useful.    Comparing 

4*531  tcAI  =  —  ?7/  sin  or/,     KIB  —  ?7/  sin  /37, 

which  are  implied  by  4*521,  with  the  general  formulae  4*461,  namely, 


4-532 


KAT  sin  w  =  KAA  sin  j3  +  KAB  sin  a, 


KTR  sin  ft>  =  KAB  sin  ft  -f  KBB  sin  a, 
we  find  that 

4*533.  An  asymptotic  direction  with  asymptotic  torsion  ?/7  is 
characterised  by  the  pair  of  equations 

~KAA  sin  ft  +  (KAB  +  ?/7  sin  &>)  sin  a  =  0, 
~(KAB  ~  Sn  sin  &))  sin  ft  +  KBB  sin  a  =  0. 

To  eliminate  ?7/  is  to  obtain  the  equation  expressing  that  the 
normal  curvature  is  zero;  the  elimination  of  sin  ft  :  sin  a  gives 

4-534  ?//2  sin2  a>  =  KAB*  -  KAA  KBB, 

a  formula  which  4*468  shews  to  be  equivalent  to  4'525. 

4*54.  Throughout  a  region  where  K  is  strictly  negative,  the 
asymptotic  tangents  are  distinguished  by  the  asymptotic  torsions, 
which  are  separate  functions  of  position.  One  of  these  square  roots 
of  —  K  is  chosen  and  called  the  first  asymptotic  torsion:  it  will  be 
denoted  by  —  ?a;  the  second  asymptotic  torsion  is  ?a.  Since  the 
four  quadrants  into  which  the  tangent  plane  at  0  is  divided  by 


48 

the  principal  tangents  Cl'OCl)  CZ'OCZ  are  distinct,  and  the  four 
asymptotic  directions  lie  one  in  each  of  these  quadrants,  the 
asymptotic  directions  also  are  distinct.  One  of  the  directions  of 
the  first  asymptotic  tangent,  chosen  arbitrarily  at  one  point  and 
in  consequence  determinate  elsewhere,  is  called  the  first  asymptotic 
direction  and  denoted  by  OJ,  and  an  angle  from  this  direction  to 
the  first  principal  direction  will  be  denoted  by  Ju.  Thus 

4'541        9a  sin  J  v  =  —  xl  cos  J  v ,     9a  cos  \v  =  yz  sin  \  v, 
implying 

4-542  #,  cos2 1  v  +  »z  sin2  \  v  =  0, 

an  equation  which  is  of  course  deducible  immediately  from  Euler's 
formula  4'444.  The  direction  making  an  angle  \v  with  the  first 
principal  direction  is  one  of  the  directions  of  the  second  asymptotic 
tangent,  and  is  denoted  by  OK  and  called  the  second  asymptotic 
direction.  The  angle  v  is  an  angle  from  one  asymptotic  tangent 
to  the  other,  and  is  given  with  as  little  ambiguity  as  possible  by 
the  equation 

4-543  B  -  A  cos  v  =  0, 

a  corollary  of  4*446. 

4'55.  In  the  use  of  the  asymptotic  directions  OJ,  OK  as  direc- 
tions of  reference,  there  is  an  embarrassing  choice,  for  the  bilinear 
curvature  KJK  and  the  asymptotic  torsion  ?rt  are  connected  by  the 
relation 

4-551  K  JK  =  -  9rt  sin  v. 

For  any  pair  of  tangential  directions, 

4'552        KST  sin2  v  =  rcJK  (sin  eSK  sin  eJT  -f  sin  ejs  sin  €TK), 
and  for  a  single  direction 

4'553  Kn  sin2  v  =  2/cjx  sin  eTK  sin  eJT , 

4-554  93  sin2  v  =  KJK  sin  (eTK  -  €JT)', 

the  last  formula  can  be  replaced  by 

4-555  90  sin  f  =  -  9«  sin  (e^  —  eJT). 

The  principal  curvatures  are  given  by 

4*556  *i  =  —  5a  tan  |  v,     #c  =  9a  cot  J  v, 

and  therefore 

4*557          B  =  9^  cot  v,     A=<sa  cosec  v,    K  =  -  9a2. 


49 

4*56.  From  asymptotic  tangents  are  defined  asymptotic  lines; 
these  on  a  united  anticlastic  region  without  singular  or  parabolic 
points  compose  two  families,  every  point  lying  on  one  member  of  each 
family.  The  relation  of  an  asymptotic  line  to  a  surface  is  in  a  sense 
more  intimate  than  that  of  a  line  of  curvature.  If  an  asymptotic  line 
has  curvature  tc  and  normal  angle  OT,  the  normal  curvature,  which 
is  zero,  is  K  cos  w,  and  three  cases  are  distinguishable :  if  tc  is  not 
zero,  then  cos  -GT  must  be  zero;  if  a  point  where  K  is  zero  is  a  limit 
of  points  where  K  is  not  zero,  continuity  requires  cos  i&  to  be  zero 
there  also;  if  fc  is  zero  everywhere  on  the  line,  the  line  is  straight, 
and  while  as  a  curve  in  space  it  has  no  determinate  principal  normal 
at  any  point,  to  assign  it  in  its  capacity  as  asymptotic  line  a  definite 
normal  by  the  convention*  that  cos  •cr  is  zero  leads  inevitably  to 
consistent  interpretations  of  general  theorems.  Thus  cos  iz  is  zero 
at  every  point  of  any  asymptotic  line,  and  continuous  variation  of 
-TO-  being  on  this  account  out  of  the  question,  there  is  far  more  gain 
than  loss  in  a  further  convention  to  fix  absolutely  the  value  of  OT, 
which  is  taken  to  be  \TT\ 

4'561.  The  normal  angle  of  an  asymptotic  line  on  a  surface  is 
everywhere  a  right  angle. 

In  other  words, 

4'562.    At  every  point  of  an  asymptotic  line  on  a  surface  the 
principal  normal  to  the  line  is  its  tangential  normal  and  the  bi- 
normal  is  the  normal  to  the  surface; 
further,  because  &  is  constant, 

4'563.    The  torsion  of  an  asymptotic  line  is  its  geodesic  torsion, 
that  is,  is  the  asymptotic  torsion  of  the  surface  in  the  direction  of 
the  line,  and  because  -sr  is  a  positive  right  angle, 

4'564"|*-  The  curvature  of  an  asymptotic  line  is  its  geodesic  curva- 
ture, 

in  sign  as  well  as  in  amount.    In  consequence  of  4*563,  theorems 
concerning  asymptotic  torsions  may  be  read  narrowly  as  theorems 

*  A  straight  line  on  a  surface  is  geodesic  as  well  as  asymptotic,  and  as  a  geodesic 
has  for  principal  normal  the  normal  to  the  surface. 

t  This  is  one  of  the  theorems  to  whose  simplicity  the  convention  that  curvature 
itself  must  be  positive  is  fatal.  The  vanishing  of  cos  •&  is  consistent  with  a  value 
-  \ir  for  w,  and  if  the  direction  OP  is  predetermined  by  the  sign  of  /c,  two  cases  have 
to  be  admitted;  either  w  itself,  or  a  symbol  for  sin  -or,  must  then  be  retained  if  the 
cases  are  to  be  treated  together. 

N.  4 


50 

concerning  the  torsions  of  asymptotic  lines,  and  in  particular  4*522 
and  4'526  imply  that 

4*565.  The  torsions  at  a  hyperbolic  point  0  of  the  two  asymptotic 
lines  through  0  are  equal  in  magnitude  and  opposite  in  sign  and 
their  product  is  the  specific  curvature  of  the  surface  at  0. 
It  is  to  be  remarked  that  for  an  asymptotic  line  to  be  straight  the 
specific  curvature  of  the  surface  need  not  be  zero:  as  an  asymptotic 
line  on  a  given  surface  containing  it,  a  straight  line  has  a  definite 
torsion  which  is  the  rate  at  which  the  tangent  plane,  which  in 
general  varies  from  point  to  point,  rotates  about  the  line;  on  a 
ruled  surface  the  rotation  disappears  if  the  same  plane  is  the  tangent 
plane  at  every  point  of  the  line,  and  this  is  precisely  the  degenerate 
case  in  which  K  is  zero  along  the  whole  line. 


5.   The  Bilinear  Rate  of  Change  of  a  Function  of  Position 

5*11.    The  equation 

5111  &s  =  0 

is  of  course  true  only  if  OS  is  tangential  to  the  <l>-surface,  but  the 
derived  equation 

5112  3>*SP  +  <£!  (dl8/d8p)  =  0 

involves  no  restriction  on  the  direction  OP,  and  leads  not  only  to 

5113  <£V  +  GKST  =  0, 

the  relation  used  to  establish  4*213,  but  also  in  virtue  of  3*515  and 
2-731  to 

5114  & 


where  rs  is  the  spread  of  the  <J>-family  along  OS,  or  the  negative 
of  the  geodesic  curvature  of  the  "^-orthogonal  regarded  as  a  curve 
on  a  surface  to  which  OS  is  tangential. 

5'21.  By  means  of  5*113  and  5'114  the  bilinear  rate  of  change 
<I>2P(3  can  be  transformed  whenever  the  direction  OP  is  tangential 
to  the  <l>-surface  :  if  the  vector  1$  is  the  sum  qT  +  SN  where  UT  is 
tangential,  then  <&*SQ  is  q&*ST  +  s<&'2SN  and  therefore 

5-211  3>*     +  G 


51 

If  OP  is  the  normal  direction  ON  the  change  is  of  another  kind  ; 
from  the  definition  of  the  slope, 

5-212  3>V  =  #, 

and  therefore  along  any  curve  in  a  direction  OQ 

5-213  d&N/dsQ=GlQ; 

but  by  1-722  and  3'515 

5-214  d&N/dsQ  =  &NQ  +  O1  (dlN/d8Q)  =  <&NQ  +  G£(dlN/dsQ)  1N, 
and  since  a  rate  of  change  of  a  radial  is  necessarily  at  right  angles 
to  the  radial  itself,  the  last  term  vanishes  and  there  remains  the 
formula 

5-215  d&N/dsQ  =  3>*NQ, 

which  taken  with  5!213  shews  that 
5"216.    Whatever  the  direction  OQ, 

*•>«=•  GV 

5"22.  The  general  relation  of  5'216  is  a  synthesis  of  the  par- 
ticular relations 

5-221  <Dv^=GV, 

5-222  &NS=Gls. 

The  first  of  these  can  be  written  in  the  form 
5-223  O2^  =  d^jdn^ 

and  suggests  a  reference  to  3'32.  The  second  can  be  compared 
with  5-114,  and  since  the  bilinear  rate  of  change  is  symmetrical 
gives 

5-224  G1 

whence* 

5-225  T  = 


5*226.  The  spread  of  the  ^-family  in  any  tangential  direction  is 
the  negative  of  the  rate  of  change  of  the  logarithmic  slope  of  <X>  in 
that  direction. 

5'23.  If  application  is  to  be  made  of  5'113,  5*114  and  5*216  to 
<£>2PQ  when  the  directions  OP,  OQ  are  both  oblique,  the  radials  1P, 

*  Allowance  must  be  made  for  the  possibility  that  G  is  negative,  and  for  this 
reason  the  logarithmic  slope  is  defined  as  ^  log  G2. 

4—2 


52 

\Q  must  both  be  resolved  into  normal  and  tangential  components. 
Assuming 

5-231  lp  =  l>s  +  rjv»     IQ  =  qT+sN) 

the  bilinearity  of  the  function  implies 
5-232        & 


and  according  to  the  purpose  in  view  the  useful  transformation 
will  be 


5'233  <£2pQ  -  rsG\  =  -G  (psrs  4-  <?rrr  +  pqtcST) 

or 

5-234          4>2P  -psGls  -  qr@lT  -  r«G  V  = 


5-31.    From  3-515 

5-311  <£>  (dlg/dsp]  =  G£(dIs/dsP)  1N, 

and  since  c^l^l^  is  zero, 

5-312  £(dls/dsp) 

hence  5'112  is  equivalent  to 

5-313  3>*    = 


for  an  arbitrary  direction  OP  and  a  tangential  direction  OS.  In 
contrast  to  this  result,  G</(dlN/dsP)  1N  is  necessarily  zero,  but  4>2^P 
is  zero  only  in  special  cases  :  the  tangency  of  OS  is  essential  to  the 
truth  of  5'313.  Multiplication  of  5'313  by  a  scalar  shews  that  as 
a  linear  function  of  a  tangential  vector  s  the  bilinear  function 
<f>2Ps  is  obtained  by  multiplying  by  G  the  projected  product  of 
d\NjdsP  and  s.  In  particular,  since  a  rate  of  change  of  the  radial 
IN  is  necessarily  tangential, 

5-314  02P  (dlN/dsQ)  =  G£(d\N/dsP)  (dlN/dsQ) 

whatever  the  directions  OP,  OQ. 

5  32.  The  function  3>2P(dIN/dsQ)  will  reappear  at  a  later  stage  ; 
5'314  shews  that  the  function  is  in  fact  symmetrical  in  OP  and 
OQ  and  indicates  the  geometrical  magnitudes  with  which  it  is 
connected,  which  depend  on  the  relations  of  OP  and  OQ  to  the 
^-surface.  If  OS,  OT  are  tangential  directions,  d\Nldss,  dl^/dsf 
are  the  corresponding  Gaussian  velocities;  dlN/dn.  is  the  vector  of 
curvature  of  the  orthogonal  trajectory.  Since  neither  KST  nor  TT 


53 

is  defined  except  for  tangential  directions,  the  notation  described 
in  1"55  is  applicable  and  it  is  possible  to  write 

5-321  t£(dlff/d8$)  (d1N/dsT)  = 

5-322  £(dlN/dss)  (dlN/dn)  = 

5-323  J'(dlN/dn)2  =  T^; 

the  last  of  these  functions  is  the  square  of  the  numerical  curvature 
of  the  trajectory.  To  discover  analytical  expressions  in  which  the 
same  projected  products  are  involved,  let  q(p)  denote  temporarily 
the  vector,  dependent  upon  OP,  which  is  such  that  for  an  arbi- 
trary direction  of  OR  the  value  of  ^Vs  ig  the  projection  of  q(p)  on 
OR,  and  let  this  vector  be  resolved  into  a  normal  and  a  tangential 
component.  The  projection  of  q(p)  on  ON,  which  by  the  definition 
of  q(p)  is  <&ZPN,  is  the  projection  of  the  normal  component  of  q(p) 
on  ON,  and  therefore  the  normal  component  of  q(p)  is  ^p^l^. 
And  from  5'313  the  projection  of  the  tangential  component  of  q(p) 
in  any  tangential  direction  is  the  same  as  the  projection  of 
Gdly/dsp  in  that  direction,  whence  since  GdlN/dsP  is  itself  tan- 
gential the  tangential  component  of  q(p)  is  nothing  but  Gd\NjdsP. 
Thus, 

5-324  q(p>  =  0  (dlN/dsP)  +  &P2fIN. 

But  if  OP,  OQ  are  any  two  directions  the  projected  product 
c^q(p)q(Q)  is  the  bilinear  scalar  function  of  OP  and  OQ  denoted  by 
^P*  02Q* ,  and  this  is  calculable  with  the  greatest  ease  by  means 
of  any  frame  of  reference.  Hence  from  5 '3 24  and  the  corresponding 
formula  giving  q(Q) 

5-325     <n*<*V  =  G*J(dlyld8P)  (dlN/dsQ)  +  &PN&QN. 
The  three  distinct  theorems  comprehended  in  5'325  can  be  ex- 
pressed in  a  variety  of  forms ;  among  the  results  are 

5-326  &s*  3>2r*  =  G*  (KS*  KT*  4-  rs TT), 

5-327  <n*  <S>V»  =  G*,cs*  r*  +  &8  &N, 

5-328  ^V  =  (02^y-(^)2. 

5-41.  In  5'226  and  4'213  we  have  two  distinct  and  independent 
deductions  from  the  symmetry  of  the  bilinear  rate  of  change  of  a 
scalar  function  of  position.  It  is  important  to  observe  that  there 
can  be  no  deductions  independent  of  these  two,  a  result  implied  by 
1*432  :  if  OS,  OT  are  distinct  tangential  directions  and  O^V  is 


54 

normal,  the  complete  symmetry  of  ^2PQ  is  deducible  from  and 
therefore  involves  no  consequences  independent  of  the  set  of 
equalities 

5-411         &ST  =  <D2rs,     &NS  =  &SN,  '  <&NT  =  &Tjr, 
of  which  the  first  is  equivalent  to  4'213,  and  the  second  and  third 
express  for  different  directions  the  single  theorem  5'226. 

5'42.  To  suppose  that  such  formulae  as  5'113,  5*114  and  5'216 
assist  in  the  calculation  of  multilinear  rates  of  change  is  completely 
to  misvalue  these  formulae.  Whatever  the  system  of  coordinates, 
the  multilinear  rates  of  change  are  among  the  functions  most 
easily  found,  and  in  application  to  particular  surfaces  and  functions 
it  is  rather  for  the  sake  of  the  other  magnitudes  involved  that 
results  of  this  kind  are  desirable. 


6.   The  Codazzi  Function 

6*11.  The  bilinear  curvature  KRS  is  not  a  function  from  which  a 
gradient  can  be  formed,  for  as  a  rule  if  the  position  of  0  is  changed 
the  directions  OR,  OS  cannot  remain  unaltered.  But  there  is  an 
elegant  function  which  plays  as  far  as  possible  the  part  of  a 
gradient,  and  it  is  with  this  function  that  the  present  chapter  is 
concerned. 

From  the  equation 

6111  &ES+G,cES  =  0 

it  follows  that  if  OR,  OS  are  specified  functions  of  the  position  of 
0  on  a  curve  with  direction  OT  on  a  ^-surface,  then 

6112  (d&xs/ds,,)  +  GITKES  +  G  (dKRSjdsT)  =  0  ; 
also  by  1'722  and  2'511 

6113 

<t>2^  (dls/dsT) 


where   OC,  OD  make   positive  right  angles  with   OR,   OS,  and 
therefore 
6114 


-  &  (°'TR>CCS 


55 

on  substitution  from  5  '2  16  and  4'212.    Thus  6112  gives 

6115  &]&.,,  +  G*RK8T  +  018KRT  +  GITKRS  +  G\RST  =  0, 
where 

6116  \RST  =  (d/cRS/dsT)  -  O-TRKCS  —  <rTs  KRD. 

The  function  \RST  denned  by  6116,  which  I  propose  to  call  the 
Codazzi  function,  belongs  like  the  bilinear  curvature  to  the  geo- 
metry of  a  single  surface,  for  this  definition  contains  no  reference 
to  the  function  <1>.  But  6115  is  of  value  as  shewing  at  once  that 
the  value  of  \RST  depends  only  on  the  three  directions  OR,  08,  OT, 
not  on  the  variation  of  OR,  OS  along  any  particular  curve  in  the 
direction  OT,  and  moreover  that 

6117.  The  Codazzi  function  is  linear  in  each  of  the  three  direc- 
tions on  which  it  depends. 

As  a  formula  for  the  calculation  of  the  Codazzi  function  6115 
may  be  modified  to 

6118 

*>RST  =  ~  (&N&RST  ~  &VM&ST  ~  &N8&XT  ~  ^NT^ES^K^N^ 

612.  The  Codazzi  function  \R$T  takes  special  forms  if  two  of 
the  directions  on  which  it  depends  coincide  or  are  perpendicular. 
Whatever  the  angle  between  OS  and  OT, 

6121  \SST  =  (dtcss/dsT)  —  2<rTs/cDS 

=  (dKss/dsT)-2o-Ts<;ss, 

6122  \STS  =  (dfCsT/dss)  ~  &S  KDT  ~  °~s  KSE 

=  (dtcST/dss)  -  2<r/9sr  -  (d€8T/d88)  KSE) 

6123 


6124  \DTS  =  (dfcDT/dss)  +  O-SDKST  -  O-STKDE 


613.  More  familiar  functions  are  among  those  of  a  single  direc- 
tion OT  which  appear  as  degenerate  forms  of  the  Codazzi  function 
and  can  be  regarded  as  defined  by  means  of  a  single  curve  in  the 
direction  OT\  that  the  function  depends  only  on  the  direction  and 
not  on  any  particular  curve  is  in  no  case  self-evident.  In  the  most 
elementary  notation, 

6131  \TTT  =  (dtcn/ds)  —  2^?^, 

6132  \TET  =  (d?g/ds)  +  2fcg  («n  -  B). 


56 

Thus  Xrrr>  the  simplest  of  cubic  functions,  is  the  function  associ- 
ated with  the  name  of  Laguerre  who  first  shewed  it  to  depend  on 
direction  alone,  and  Xr^r  is  the  cubic  function  of  Darboux.  As 
actually  given  by  6*116, 

6133  ^EET  —  (d/cEE/ds)  —  2fcgKET>, 
but  on  substitution  from  4*123,  this  becomes 

6134  \EET  =  2  (dB/ds)  -  {(dH:n/ds)  -  2*^}, 
that  is 

O  -LOO  h'EET  ~~  *•*•*-*  T  ~~  ^TTT' 

On  account  of  the  multilinearity  of  the  Codazzi  function,  \TTE, 
\ETE  bear  to  the  direction  OE  the  relations  of  \EET,  —  \TET  to  OT\ 
hence 


while  \ETE  is  the  negative  of  the  Darboux  function  of  the  direction 
OE;  \EEE  is  of  course  the  Laguerre  function  of  this  last  direction. 
6'14.  Naturally  it  is  when  the  three  directions  involved  are  all 
principal  or  all  asymptotic  that  the  Codazzi  function  is  most  simply 
expressed.  If  Kgl,  K^  are  the  geodesic  curvatures  of  the  lines  of 
curvature, 

6141  <7TT  =  a?  =  Kgl,     azl  =  azz  =  K^, 
and  therefore 

6142  Xnt  =  d^ljdsl  ,     XI8l  =  —  2  A  tcgl  ,     \x.l  =  d 


6-1 4.3        "\      —  rlv  //7<?        "X      — 
-L^rO  A'HZ  —  U""i/Gtoj5,        ^IZZ 

where  A  denotes  as  before  \  (#5  —  3/t),  the  amplitude  of  curvature. 
The  corresponding  functions  for  the  asymptotic  directions  OJ,  OK 
are  simplified  by  the  relation 

6144  KJK  =  ?a  sin  v ; 

if  KgJ,  KgK  are  the  geodesic  curvatures,  which  are  the  actual  curva- 
tures, of  the  asymptotic  lines, 

6145 

^jjj  =  -  ZsaKgj>     ^JKJ  =  (dsa/dsj)  sin  v ,     X^^  =  2?a  \KgJ  +  (dv/dsj)}, 
6*146 

:  -  2?a  {KgK  -  (dv/dsx)},  \JKK  =  (dsa/dsK)  sin  u,  \KKK  =  2?a«^. 


6'21.    We  are  now  in  a  position  to  appreciate  the  fundamental 
property  of  the  Codazzi  function,  which  is  apparent  from  6*115  : 


57 

6*211.    The  Codazzi  function  is  a  symmetrical  trilinear  function 
of  the  tangential  directions  on  which  it  depends. 

That  the  function  XBST  denned  by  6'1  16  is  linear  in  each  of  the 
directions  OR,  OS,  OT  can  be  proved  without  difficulty  from  the 
most  elementary  considerations*;  indeed,  it  is  by  its  linearity  in 
OT  that  \RST  ni>st  attracts  attention  in  the  geometry  of  a  single 
surface.    The  symmetry  of  \B8T  in  the  two  directions  OR,  08  is 
manifest  from  the  symmetry  of  KRS  in  the  same  directions,  but  the 
discovery  that  ^RST  depends  on  OT  in  the  same  way  as  on  OR  and 
OS  is  both  unexpected  and  fertile. 
6*22.    Because  \RST  is  trilinear, 
6*221    A,       sin3  w 

sin  j3B  sin  /38  sin  j3T  +  \BAA  sin  aR  sin  0S  sin  $T 
sin  (3R  sin  cts  sin  @T  +  \AAB  sin  f*R  sin  f}8  sin  aT 
sm  PR  sin  as  sin  a.T  +  \BAB  sin  OLR  sin  f$8  sin  aT 
4-  \BBA  sin  OR  sin  ofe  sin  (BT  4-  X^^^  sin  OR  sin  a^  sin  aT> 
and  the  complete  symmetry  of  the  function  is  implied  by  the  tri- 
linearity  if  the  equalities 


are  known  for  any  one  pair  of  distinct  directions.  On  account  of 
the  symmetry  of  KAB,  there  is  no  distinction  between  \BAA  and  \ABA 
or  between  \ABB  and  \BAB,  and  therefore  the  equations  necessary 
to  imply  6*211  are  two  only,  namely 

"'223  ^AAB  =  ^ABA)       ^ABB  =  ^BBAi 

which  on  reference  to  6*121  and  6*122  are  readily  identified  with 
the  equations  associated  with  the  name  of  Codazzi  : 

6*224.  The  Codazzi  equations  for  any  pair  of  families  of  curves 
of  reference  express  the  symmetry  of  the  Codazzi  function  for  the 
directions  of  reference  and  imply  the  complete  symmetry  of  this 
function, 

and  it  is  for  this  reason  that  I  have  proposed  to  attach  Codazzi's 
name  to  the  function  itself. 

From  1*43, 

6*225.    Any  two  pairs  of  Codazzi  equations  are  equivalent, 
and  this  result  adds  interest  to  a  comparison  of  different  forms 
which  the  equations  assume. 

*  See  8-1  below. 


58 

6*23.  An  important  interpretation  of  the  Codazzi  equations  comes 
from  6  '136,  which  can  now  be  read  as  a  relation  between  \TET,  the 
Darboux  function  of  OT,  and  \EEE,  the  Laguerre  function  of  OE  : 

6*231.    The  sum  of  the  Darboux  function  of  any  direction  OT  and 
the  Laguerre  function  of  the  perpendicular  direction  OE  is  a  linear 
function,  equal  to  twice  the  rate  of  change  in  the  latter  direction  of 
the  mean  curvature  of  the  surface. 
Since  the  two  equations 

D  AOA  >^TTE  =  ^TET>        "*TEE  ==  "'EET 

differ  only  in  the  direction  which  is  denoted  by  OT,  6*231  implies 
them  both*,  and  is  equivalent  to  any  pair  of  Codazzi  equations. 

Angular  differentiation  gives  relations  of  another  kind  between 
the  functions  of  Laguerre  and  Darboux.  If  the  variable  directions 
are  independent, 

u  Zoo  da  j<  \.ftgji  =  A-^S-JJ. 

Hence  because  the  Codazzi-  function  is  symmetrical, 


O  ^jOiJ  aa  A.  fTE  ~~          TEE  ~~  ^"fTT  ^~  T  ~~~  *J 

it  is  easy  to  express  these  results  in  words. 

6  31.  The  Codazzi  equations  derived  from  6*142,  6143,  and  6*145, 
6*146  are 

6*311  ZA/cp  =  -  dxjdsz,     '2AfcffZ  =  -  dxz/dsl} 

and 

6*312  r    2?a  {/Cgj  +  (dv/dsj)}  =  (d^ajdsK}  sin  v, 

[_  2?0  {tcgK  -  (dv/dsK)}  =  -  (dia/dsj)  sin  v, 

and  these  are  inevitably  regarded  as  formulae  for  the  calculation 
of  the  geodesic  curvatures  which  they  involve.  The  same  view  may 
be  taken  of  the  Codazzi  equations  in  general,  for  although  as  a  rule 
each  equation  involves  two  geodesic  curvatures,  the  pair  of  equations 

"'313  ^AAB  ~  ^ABA  >        ^ABB  ~  ^BBA 

is  linear  in  the  pair  of  geodesic  curvatures  /cg,  /cg,  and  has  for  its 
discriminant  SAB*—  SAA*>BB>  which  has  been  seen  in  4*472  to  be 
equal  to  A2  sin2  co  and  therefore  vanishes  only  at  an  umbilic. 

*-  Formulae  equivalent  to  6-232  were  discovered  in  1911  and  announced  to  the 
Fifth  International  Congress  of  Mathematics  (Cambridge,  1912;  Proceedings,  vol.  2, 
p.  34)  ;  I  have  not  hitherto  published  a  proof. 


59 

6"32.  Since  any  two  pairs  of  Codazzi  equations  are  equivalent, 
the  geodesic  curvatures  in  any  one  pair  of  families  of  reference 
curves  can  be  calculated  from  those  in  any  other  pair  ;  this  is  in 
accordance  with  2'425  and  2'426,  but  if  in  illustration  we  deduce 
Kgj  from  6'311  we  shall  see  the  economy  effected  by  the  enlarging 
of  our  ideas.  Because  the  swerve  aTs  is  linear  in  the  direction  OT, 

6'321     KgJ  +  (dv/dsj)  =  arjK  =  o-^K  cos  J  v  -  azK  sin  \  v 

=  {xgi  +  2  (dv/dsj]  cos  Ju  -  {xgz  -  %  (dv/dsz)}  sin  Ju, 
and  therefore  from  6'311 

/»  orirt        c*  A  (d*z   .    .          A  dv         .    1 

6-322       ZA   K+     -    =         sm    u  +^       cos 


t  .  dv    . 

—  -^-7—  cos  *t>  —  A  -r-  sm 
dsz 


dv 


as  anticipated.  It  would  be  rash  to  assume  that  every  useful  formula 
for  a  geodesic  curvature  is  given  by  some  Codazzi  equation  ;  in  fact 
an  example  can  be  given  to  the  contrary.  Identically, 


C.QOQ  «     o  a 

6  323         -y  —  2?a  ,    cosec  v  =  —  -  —  5—       -  tan2  1  v, 
dsl  dsl  ds\ 


a.ooA         dsa     0     dv  a  ol 

6  324         -^  —  h  2?rt  -y-  cosec  v  =  -  -*—L  cot2  \  v  ; 

dsz  dsz  dsz 

utilising  the  relations 

6-325          9a2  cot4  Ju  =  ?a3  cot3  Ju/?a  tan  \  v  =  -  ^53/^t, 
6-326         ?a2  tan4  J  u  =  9a3  tana  J  u/9a  cot  J  u  =  -  »T3/^  , 

it  is  easy  to  deduce  from  6'312  the  expression 
6'327     KgJ={d  log  (-  V/tfO/^i)  sin  |  v  cos2  J  v 

+  (<i  log  (-  »T3/:y5)/cfo5}  cos  Ju  sin2  |f, 

of  which  Bonnet  has  made  application,  but  6  '32  7  is  not  as  it  stands 

a  Codazzi  equation. 


60 


7.   The  Trilinear  Rate  of  Change  of  a  Function  of  Position 

7'11.  In  the  last  section  the  trilinear  rate  of  change  played  only 
the  subsidiary  part  of  introducing  to  our  notice  the  Codazzi  function 
and  establishing  its  symmetry,  and  for  this  purpose  the  variable 
directions  were  restricted  to  be  tangential  to  the  ^-surface.  The 
next  task  is  to  investigate  formulae  involving  the  ,same  trilinear 
rate  of  change  with  one  or  more  of  the  directions  normal. 

712.  From  the  elementary  formula 

7121  &NP  =  G1P, 

since  this  implies  for  any  variable  t  on  which  OP  may  depend 

7122  O^  (dlpldt)  =  Gl  (dlp/dt), 
it  follows  that  whatever  the  direction  OQ, 

7123  &ypQ  +  &p  (dlN/dsQ)  =  GV 

Here  is  a  simple  proof  that  the  function  <E>2P  (dlN/dso)  is  sym- 
metrical in  the  directions  OP,  OQ,  a  conclusion  reached  in  5'3,  and 
substitution  from  any  of  the  formulae  of  5'32  gives  a  corresponding 
deduction  from  7123.  Thus  5'325  gives 

7124  &N  &NPQ  +  <&%  ^  =  GG*PQ  +  &P  &Q 

in  which  no  restriction  is  implied  on  OP  or  OQ,  and  5*321,  5'322, 
5-323  imply 

7125 

7126 

7127  &NNN  +  G  KP*  = 

KP  in  7127  denoting  either  value  of  the  curvature  of  the  orthogonal 
trajectory. 

713.  The  function  ^S^PQ  is  involved  not  only  in  the  rate  of 
change  d<&2Np/dsQ  but  also  in  the  rate  of  change  d&pq/dn,  and 
deductions  from  the  symmetry  of  the  trilinear  function  are  to  be 
expected.    If  however  OQ  is  normal,  nothing  is  to  be  anticipated 
that  is  not  deducible  from  the  symmetry  of  the  bilinear  function 
GPyp',  in  fact  we  have  from  first  principles 

7131  d&xpldn  =  <&NNP  +  &N  (dlP/dn)  +  $>2P  (dlN/dn), 
and  since 

7132  ^2^  (dlp/dn)  =  Gl  (dlf/dn), 


61 

the  comparison  of  7*131  with  7*123  yields  only  the  identity 

7133  d&p/dn  =  G2NP  +  G1  (dlp/dn). 

But  d^sT/dn  repays  examination. 


7*21.    Expanding  d<&2ST/dn  in  the  usual  way  and  substituting 
from  2*741  we  have 
7-211     d&ST/dn 

+  rgly)  +  3>2S  (<TNT1E 


on  the  other  hand,  from  4*212, 

7'212       d^STjdn  =  —  d  (GicST)/dn  =  -  G  (dKST/dn)  -  GINKST. 

Hence  from  4*212  and  5*114 

7*213 

&NST  +  GPffiKsT  +  #  {(die8T/dn)  -  <rNsKDT  -  O-NTKSE  -  2r5rr}  =  0, 
or  in  a  form  analogous  to  that  of  6*118, 

7'214     (dtc8T/dn)  — 


7*22.  When  7*213  is  compared  with  7*125  the  function  <i>  itself 
disappears,  surviving  only  in  the  slope  : 

7*221     G2ST  +  G1NKST 

+  G  \(dKST/dn)  —  O-NSKDT  —  O-NTKSE  —  2rsrT  —  KS*KT*\  =  0. 

An  algebraical  transformation  reduces  the  number  of  terms  in 
this  equation.  Let  T  denote  l/6r,  which  is  the  arc  function  of  the 
trajectory  with  respect  to  the  variable  O,  and  has  been  called  the 
spaciousness  of  the  family;  then  identically,  for  any  directions  OP, 
Oft 

7-222  T1P  =  -^-2^p, 

7-223 
so  that 

7*224 
But  for  tangential  directions  OS,  OT, 

7-225  GlsG1T 

Hence 

7'226     (d/cST/dn)  —  <rNs  KDT  — 


62 

or  in  another  form,  involving  <l>  but  separating  completely  the 
geometrical  from  the  analytical  terms, 

7-227     (dx8T/dn)  -  (y 


7'23.    Particular  cases  of  7  '2  14  are 
7"231     (dfcTT/dn)  —  %CTNT<>TT 

=  ~  {&X&1TTT  ~  &NN&TT  ~  2 

7-232     (dfcET/dn)  -  2cr 


2TT 


and  the  corresponding  cases  of  7  '226  are 
7-233       (d/cTT/dn)  -  2<rNT<>TT  -  KT^  =  (T2 
7-234       (dKST/dn)-  ^NT^ET-KE^KT^  =  (T*ET 

to  appreciate  the  last  two  formulae,  we  must  recognise  tcT#2  as 
KTI?  +  KET*y  the  square  of  the  amount  of  the  spin  of  the  tangent 
plane  along  OT,  and  KE^KT^  as  KETKTT  4-  KEEKTE,  that  is,  as  2B/cET. 

7'24.  Two  symmetrical  bilinear  functions  in  a  plane  GAB  are 
identical  if  they  are  equal  for  the  pair  of  directions  OA,  OA,  for 
the  pair  of  directions  OA,  OS,  and  for  the  pair  of  directions  OB,  OB. 
Hence  any  one  group  of  three  independent  particular  cases  of  7*214 
or  7*226  is  equivalent  to  any  other  group. 

If  OT  is  a  principal  direction,  /cr#2  is  the  square  of  the  corre- 
sponding principal  curvature  and  ?rr  ig  zero;  hence* 

7'241.  If  OC  is  a  principal  direction  on  a  ^-surface  and  x  is  the 
corresponding  curvature,  then 


where  T  is  the  reciprocal  of  the  slope  of  <I>,  and  the  rate  of  change 
of  *  along  the  orthogonal  trajectory  of  the  3>-family  is  given  directly 


*  Since  the  truth  of  this  theorem  for  one  of  the  principal  directions  is  not  de- 
ducible  from  its  truth  for  the  other,  there  are  two  independent  formulae  involved  in 
7*241.  These  are  the  formulae  whose  existence  was  inferred  by  Forsyth  in  1903 
(Phil.  Trans.  Roy.  Soc.  Lond.,  Ser.  A,  vol.  202,  p.  333)  from  an  enumeration  of 
invariants  ;  discovered  by  the  methods  described  here  and  translated  into  a  form  to 
require  no  explanation  they  were  announced  to  the  London  Mathematical  Society 
(Proc.  L.M.S.,  vol.  16,  p.  xxvii)  in  1918. 


63 

The  form  taken  by  7*232  and  7  '234  for  a  principal  direction,  that 
is,  by  7'214  and  7'226  when  OS,  OT  are  principal  directions  at  right 
angles,  is  quite  different  ;  KIZ  being  zero  on  every  surface,  dK\TJdn  is 
zero,  and  K^K^  ,  a  multiple  of  KIZ>  is  zero  also.  Thus  only  two  terms 
of  7'234  and  three  of  7'232  survive,  and  since  ?I5  is  A,  the  amplitude 
of  curvature,  and  in  the  swings  aNl  an(l  ?jv8  is  to  be  recognised  the 
magnitude  described  as  the  twist  of  the  family, 

7'242.  The  twist  CT  of  the  family  of  surfaces  associated  with  a 
function  <1>  is  given  in  terms  of  <I>  itself  by 


and  in  terms  of  the  reciprocal  of  the  slope  of  <E>  by 


Of  the  results  of  applying  7 '2 14  and  7 '2 2 6  to  the  asymptotic 
directions  OJ,  OK  the  most  elegant  is 

7  243  (dsa/dn)  sin  v  -  ?a2  cos  v  =  -  T*JK/T, 

which  can  easily  be  verified  from  7'241  and  7'242. 

7'31.  To  deduce  from  7*242  formulae  for  evaluating  the  twist 
when  <J>  is  given  as  a  function  of  Cartesian  coordinates  x,  y,  z  is  a 
simple  matter,  but  requires  some  preliminary  investigations  to  which 
the  theory  of  multilinear  functions  is  not  essential. 

By  its  definition,  the  gradient  G  of  the  function  <I>  is  the  vector 
whose  projections  are  <&x,  <&y,  <&z.  The  slope  G  therefore  satisfies 
the  equation 

7-311         (?  =  -T-a        1        cos  7     cos/9     $>x 

cos  7         1         cos  a.     <&y 
cos  ft     cos  a         1         <&z 

®x  ®y  <$>z  0 

and  since  points  where  &xy  4>y,  O^  are  simultaneously  zero  are 
excluded,  G  is  determined  throughout  the  region  under  considera- 
tion by  combining  this  formula  with  a  choice  made  at  a  single  point. 
The  direction  normal  bo  the  <f>-surface  is  the  direction  in  which  the 
vector  G  has  the  amount  G,  and  therefore 

7'312.    The  direction  cosines  of  the  normal  to  the  ^-surface  are 


The  ratios  of  the  normal  direction  are  &'0/6r,  y^G,  ^G/^>  where 
XG>  2/o>  ZQ  are  the  components  of  G  and  are  therefore  given  by 
formulae  of  which  the  first  is 


7313 


G 


>a;       COS  7       COS  @ 

>y        1         cos  a 
>z     cos  a        1 


The  direction  whose  ratios  are  XT,  yT,  ZT  is  tangential  to  the 
<E>-surface  if 


7'314  $>XXT  +  ^yr  4-  <£z^r  =  0> 

and  from  0'45  it  follows  that  if  the  directions  OS,  OTare  tangential 
and  eST  is  an  angle  from  the  first  to  the  second,  then 

7-315        TG 


Also  if  OE  makes  a  positive  right  angle  with  OT  round  ON, 
then  OT  makes  a  positive  right  angle  with  ON  round  OE  and 
therefore  by  0"45 

7-316  G(1E,  mE,  nE)  =  f 


x. 


yT 


where  %G,  yG,  ZQ  have  the  values  typified  in  7'313,  and  by  0'46 


7-317 


E,  yE, 


3>, 


7"32.  The  bilinear  curvature  of  the  ^-surface  in  the  pair  of 
directions  OS,  OT  is  shewn  by  the  comparison  of  4'212  with  3'311 
to  be  given  by 

7-321 

so  that  in  particular  for  the  normal  curvature  in  the  direction  OT, 
7 '322    GKU  =  —  (<&xx,  <&yy,  <\>zz,  <&yz,  <&zx,  ^xy^Xf,  yT, 
Combining  7 '321  with  7 -3 17  we  have 
7-323 


nT 


65 


hence  in  terms  of  ratios  alone 
7-QO4      onr/^2 

I  O<a^r       &  1  Cr  9cT> 

^r  +  VT  cos  7  +  ZT  cos  £ 
#r  cos  7  +  ^/r  +  ^r  cos  a 
#r  cos  ft  +  yr  cos  a  +  £r 
^s  +  y^  cos  7  +  £5  cos  ft 
xs  cos  7  +  i/£  +  Zs  cos  a 
#s  cos  fi  +  ys  cos  a  +  % 
and  the  geodesic  torsion  in  the  direction  0 T  is  given  by 
7-325 

•  XT  +  yT  cos  7  -\-  ZT  cos  ft 
XT  cos  7  +  yT  +  -%  cos  a 
#r  cos  ft  +  yT  cos  a  -f  £y 


It  is  convenient  to  write 

7-QOA  T2C7a;a; 

I  OZO  J    B       = 


cos  7 
cos/3 


cos  {3 

cos  a 

1 


® 


cos  7 

1 
cos  a 


and  so  on,  and  to  use  H2y,  E-1'2,  E^  as  equivalent  to  S^2,  Sza;,  EJ 
with  this  notation,  7*324  becomes 

7-327 


and  7  325  takes  the  form 

7-328     G%  -  T(Hxa;,  Ey",  a22,  5"*, 

7'33.  There  is  no  need  of  the  theory  of  multilinear  functions 
in  establishing  the  theorem  that  the  principal  curvatures  of  the 
4>-surface  are  the  roots  of  the  equation 

7-331 


cos  7  + 
cos  3  + 


cos 


COS  O  + 


cos  /  + 
cos  a  4- 
G»  -f  «> 


0 


=0. 


N. 


66 


Applying  to  7*321  the  determinantal  identity 


7332 


R 


ss 


TS 


R 


T}yx  flzx 

-L  v  -Li 

Ryy  Rzy  ZSXT  —  XSZT 

J_\/  JL\J  vU  Q  t/'7T    ^"""     t/OtX/'/"' 

*v  C  tXj  nn  """"""  tv  C  &  T*  ds  Q  ti  rfl    "          Li  Q  VUT*  \J 

•  OJ.  O        A  Ot/-*-  t/  *^         -*• 

where  on  the  left-hand  side  .Rp^  denotes 

2RuvuPvQ,     u,  v  =  x,y,  z, 

and  the  nine  coefficients  of  the  form  Ruv  are  arbitrary,  we  have  in 
virtue  of  7*315 

lid  j.     \ji    j.\.   —  —        -*-a;rr        ~^ur.        ~^zx         ~*^x 

V 


zz 


0 


which  is  also  a  corollary  of  7 '331,  and  applying  the  same  identity 
to  7*327,  we  have  similarly 

7-334  (7M2  =    KXX    Eyx    E,ZX    <& 


in  making  these  deductions  we  may  take  an  arbitrary  pair  of  tan- 
gential directions  and  appeal  to  4*468  and  4*472,  or  we  may  take  a 
pair  of  principal  directions  and  remember  that  KIZ,  9n,  Szz  all  vanish. 

7*34.  For  the  calculation  of  the  twist,  or  indeed  of  the  value 
of  any  symmetrical  bilinear  function  when  its  arguments  are  the 
principal  directions  of  a  ^-surface,  it  is  not  necessary  to  calculate 
the  individual  ratios  of  the  principal  directions ;  it  is  sufficient  to 
discover  the  values  of  the  six  combinations  x^z,  y^yZ)  z^zz,  y^zz  +  z^yz, 
z^xz-\- x^,  x^yz  +  yiXz,  and  this  we  proceed  to  do. 

It  is  easy  to  find  five  linear  functions  of  these  six  combinations 
which  necessarily  vanish :  since  KIZ  is  zero,  7*321  gives  one  such, 
and  because  the  principal  directions  are  perpendicular, 


cos  a 


cos 


67 


and  similarly 


also  multiplying  the  conditions  of  tangency 

<^xxl  +  ®yyl  +  <Mt  =  0,     3>xxz  +  <&yyi  +  ®zzz  =  0 
by  xz  ,  XT  and  adding  we  have 

;8  +  <£z  (stff8  +  #ttf8)  +  <&y  (a?Ty8  +  yza;8)  =  0, 

s  +  $*  (yi*B  +  *i3fc)  +  <£*  Oi2/s  +  yTa?8)  =  o, 

+  3>y  (yizz  +  Zlyz)  +  $>x  (z^  +  a?t2r8)  =  0. 
Hence 

7  '341.    With  any  Cartesian  frame,  the  six  expressions 
z\%z,  y\Zz  +  z\yz,  Zi®z  +  %\Zz,  %\.yz  +  y\®z  are  proportional  to  the  five- 
rowed  determinants  of  the  matrix 


yy 


^zz        ^yz 

1  cos  a 
0         0 
0        $>, 


cos  7 


0 


0 

0         0       2<£z      <£>y         <&x          0 

To  find  the  factor  which  enables  us  to  replace  the  proportionality 
by  equality,  we  remark  that  7 '341  implies  that 

7*342.   For  arbitrary  values  off,  g,  h,  the  determinant 
f2        92        h*        gh         hf        fg 


1       cos  a.  cos  /3  cos  7 

00  <&Z  <&y 

0  <J>z  0  <&x 

<£„         <l>~         0 


1 

0 

0       24>, 
0          0 

is  a  multiple  of  the  product  (fxl  +  gyl  +  hz^)  (fxz+gyz  + 
and  we  evaluate  this  product  in  another  way. 

If  we  write  temporarily  m,  n  for  fxl  -f  gyl  +  A,^,  fx 
then  identically 

I  UtAS'T  1 1 1/tA/Y     "^~~      (,/    \  t/XT    L/C'     "'""      L/T  1/^7    /     "™^     At-     \   t&T  vU^     ~~~"     1//T  ^"*    I. 

tyxl-j/O  (/*•"/  \L        O  L       6/  J 

and  therefore  by  7 '3 15 

T(r  (?2^r  —  7/l^'5)  =  gtf>z  — 
similarly 

TG  (nyl  -  myz)  =  h<&x-  f®z ,     TG  (nzl  - 


-f      5  + 


5—2 


68 

But  because  $ST  is  symmetrical  and  bilinear,  to  replace  &T,  yT, 
ZT  by  nxl  —  ra#5,  ny^  —  myz,  nzT  —  mzz  on  the  right  of  7*325  is  to  re- 
place 90  by  ?i25n  —  2nmslz  +  ra29S5  on  the  left  of  the  same  equation  ; 
recalling  that  ?TI,  9TS,  9sg  have  the  values  0,  A,  0  and  replacing  the 
product  nm  by  its  value  we  have  the  equation 

7-343     -  2T3  G*A  (fa,  +  gy^  +  hz^  (faz  +  gyz  +  hzz) 


cos  7 
(f&y  ~  9®*)  &**  +  (f®v  ~  9®*)  cos 


-    <y  cos  7 


v  ~  9®*)  ®*y  +  <f®v  ~  9®x)  cos  a 

cos  /3 


It  follows  that  the  determinant  in  7*342  is  a  multiple  of  the 
determinant  in  7*343,  and  once  attention  is  drawn  to  the  existence 
of  a  connection  between  them  it  is  a  simple  matter  to  reduce  the 
former  to  the  product  of  the  latter  by  —  2.  We  conclude  that 

7'344.    The  value  of  the  determinant  in  7*342  is 

4T3  G4A  (fa,  +  gyl  +  hzj  (faz  +  gyz  +  hzt\ 
and  further  that 

7'345.    The  value  of  the  symmetrical  bilinear  function  RPQ  of 
which  the  expression  in  terms  of  Cartesian  coordinates  is 

>      i-fWD  i/      01  11      /ji  —   /v>     ti      *y 

z*  £i    UpVQ,    u,  v  —  x,  y,  z, 

when  the  arguments  of  the  function  are  the  first  and  second  principal 
directions  of  the  <&-surface,  is  given  by 

R**    Ryy    Ezz     R«z      Rzx 


1         1  cos  a  cos/3  cos 7 

00         0         <l>z  <E>y 

0      2^y      0        4>0         0  <&x 

0         0      2<l>?  OM  <l>a;          0 


69 

Determinants  of  the  form  occurring  here  were  first  used  by 
Darboux,  who  discovered  them  in  his  re3earches  on  triply- orthogonal 
systems,  and  we  shall  call  them  Darboux  determinants.  We  may 
express  7 '345  briefly  by  saying  that  the  value  of  the  Darboux  de- 
terminant which  has  Ruv  for  the  typical  element  of  its  first  row  is 


In  passing  we  may  mention  another  expression  involving  the 
product  (fx^  4-  gyl  4-  hz^  (fxz  4-  gyz  4-  hzz),  interesting  in  itself  but 
as  ill  adapted  as  that  in  7'343  to  giving  the  value  of  a  bilinear 
function  that  is  not  a  product.  From  the  identity 

7-346 

7?  7?  f         \      '         \    1 ' 

-ftco  -ft/TCi  /     XQ  4"  Cf  lie  "r"  fl  Zo 

-to  J          Oc/t/O1  o 

RST  RTT  f'xT  +  g'yT  4-  h'zT 

ZgHOf  """  ^S^T       ff 

U/Tpy  ~T)tiy  I yyy  7  / 

Ai"*"^  rf"6  rs^Z  /yi     /i/      .__  /i/    /y»  f»' 

JLv  JL  v  JL  v  vu  C  W  T1  ' /  Cfv  'T*  *  ^ 

ZSXT  —  XSZT    ®syT~ysxT  o          o 

/"  g"  h"  0  0 

since  HTI  =  0,     TETS=GU,     HS5  =  0, 

we  have 

7-347     2G*A  (fx,  +  gy,  +  htj  (fxz  +  ^5  +  hz<) 

=  —  T3 

E8*    Hy2/    Hzy    4>y    gr 

<&X  <&y  4>Z  00 

/        ^      •  A       0     0 

7-35.    The  application  of  7'345  to  7'242  is  immediate  : 

7'351.  At  a  point  which  is  not  an  umbilic  of  the  3? -surf ace  through 
it,  the  twist  -or  of  the  ^-family  is  connected  with  the  derivatives  of  <I> 
by  the  formula* 

'  The  formula  was  first  given,  in  terms  of  curvilinear  coordinates  and  without 
proof,  to  the  Fifth  International  Congress  of  Mathematicians  (Cambridge,  1912; 
see  Proceedings,  vol.  2,  p.  31).  Eesults  equivalent  to  7'351  and  7g352  in  terms  of 
rectangular  Cartesian  coordinates  were  proved  subsequently  by  Herman  (Quarterly 
Journal  of  Mathematics,  vol.46,  pp.  284  et  seq.).  Algebraical  transformations  of  the 
determinant  involved  are  to  be  found  in  Darboux's  treatise  on  triply-orthogonal  systems. 


70 


T        T 

J-  -*- 


xx 


yy 


T 

•*- 


T 

-*- 


zx 


T 

J- 


0 
0 


1 

0 
0 


cos  a     cos  /3     cos  7 


0 


o 


0 


* 


0 


where 


cos  7     cos  /3 


cos  7 

cos  /3     cos  a 


cos  a 


0 


-4  ?s  ^Ae  amplitude  of  curvature  of  the  ^-surface. 

The  value  of  A"  in  terms  of  derivatives  of  <E>  is  given  in  7'334 
above. 

The  alternative  expression  for  the  twist  given  by  7 '242  is  more 
complicated,  but  gives  the  result  explicitly  in  terms  of  third 
derivatives  of  3>.  If  #Q,  yQ,  ZQ  have  the  meanings  assigned  in  7*31, 
then  G<&*yp  is  a  linear  function  of  OP  in  which  the  coefficient  of 
xp  is 


and  G<&3NPQ  is  a  bilinear  function  of  OP  and  OQ  in  which  the 
coefficient  of  xPXq  is 

7*352.   -(/"  the  typical  element  in  the  first  row  of  a  Darboux 
determinant  is 

1 

cos  7 
cos  8 


_  2 


cos  7     cos  /3     <&x 

1        cos  7     cos  /3     <&xuv 

1        cos  a     3>y 

cos  7        1        cos  a     ^^p 

cos  a       1         '5>z 

COS  y8       COS  «          1            <l>ZMy 

3>y           $>z            0 

^^        ^^        ®z          0 

1       cos  7    cos  /3    O^ 

1       cos  7    cos/3    <&xv 

cos  7        1       cos  a     <&yu 

cos  7       1        cos  a     O^ 

cos/3    cos  a      1        <&zu 

cos  ft    cos  a       1        <&zv 

<bx      <&„      $>z        0 

<&x          $>y          <&z           0 

the  value  of  the  determinant  is  8T7GSA2'&. 


71 

It  is  to  be  remarked  that  the  expression  given  in  this  enuncia- 
tion is  not  in  general  simply  the  product  of  the  second  derivative 
TUV  by  —  T4(r5;  the  difference  between  the  two  is  a  function  which 
is  such  that  its  use  as  a  typical  element  of  the  first  row  produces 
a  Darboux  determinant  that  vanishes. 


8.   Functions  of  Direction  on  a  Surface 

8'11.  The  fundamental  difficulty  in  applying  the  theory  of 
multilinear  functions  to  problems  connected  with  any  single  surface 
other  than  a  plane  is  due  to  the  absence  of  genuine  gradients. 
The  directions  forming  the  arguments  of  such  functions  as  the 
bilinear  curvature  and  the  Codazzi  function  are  essentially  tan- 
gential, and  if  the  current  point  varies  these  tangential  directions 
are  necessarily  affected. 

Suppose  the  surface  to  be  referred  to  curvilinear  coordinates 
u,  v  and  let  a  standard  tangential  direction  0  W  be  associated  with 
each  position  of  0.  Then  a  function  F(Q,  R,  ...)  of  the  tangential 
directions  OQ,  OR,  ...  may  be  described  explicitly  as  a  function 
F(u,  v,  eWQ,  6WR,  ...),  and  if  the  directions  OQ,  OR,  ...  vary  in  a 
given  manner  with  the  position  of  0  on  a  curve  in  the  direction 
OT,  the  rate  of  change  of  F  '  (Q,  R,  ...)  along  the  curve  is  given  by 


dF     dF  du      dF  dv  vdeWQ       ,      p,deWR 

-j  —  =  3—  -j  —  i-  —  j—  +  aaQJf  —j—  -  +  aasJf  —j 

dsT      ou  dsT      dv  dsT  dsT  dsT 


that  is,  by 

.  n    dF      (dF  du      dF  dv 
8112  -j-=]      3—  +3r;j  --  (d 

dsT      [du  dsT      dv  dsT 

+  (crTQdaQF+a-TRdaRF+  ...). 

Since  u,  v  are  merely  particular  functions  of  position  on  the  surface, 
the  rates  of  change  du/dsT)  dv/dsT  are  the  linear  functions  ulT,  v1T 
of  OT,  and  since  OW  is  assumed  to  depend  only  on  the  position 
of  0,  the  swerve  aTw  also  is  a  linear  function  of  OT.  On  the  other 
hand,  neither  the  rates  of  change  dF/dsT,  ddqF,  daRF,  ...  nor  the 
swerves  <rr^,  q-TR,  ...  depend  in  any  way  on  the  actual  choice  of 
coordinates  u,  v  and  initial  direction  0  W.  Thus 

8  '113.    Associated  with  any  function  of  direction  F  (Q,  R,  ...)  on 
a  surface  there  is  a  function  gdbTF  which  is  linear  in  the  direction 


72 

OT  and  is  such  that  the  rate  of  change  of  F  along  any  curve  in  the 
direction  OT  is 

gdbTF  +  o-TQdaQF+o-TRdaRF  +  .... 

The  function  gdbTF  will  be  called  the  Darboux  gradient  of  F. 
From  8112, 

8114.  In  terms  of  coordinates  u,  v  and  an  initial  direction  0  W, 
the  value  of  the  Darboux  gradient  gdbTF  is  given  by 

gdbTF  =  (dF/du)  ulT  +  (dF/dv)  vlT  -  (daQ  F  +  daRF  +  .  .  .  )  <JTW. 

8*12.  For  a  multilinear  function  PQRS...>  the  angular  derivatives 
daQP,  daRP,  ...  have  the  values  PBRS...>  PQCS...>  •••  where  OB, 
OG,  ...  make  positive  right  angles  with  OQ,  OR,  .  .  .  ;  hence 

8121    dPQRSJdsT  =  gdbTPQRS...  +  PBRS.°TQ  +  PQCS...VTR  +  •••• 
There  is  another  route,  open  only  in  the  case  of  multilinear  func- 
tions, which  leads   to  a  similar  formula  and  therefore  shews  a 
different  aspect  of  the  Darboux  gradient.    If  the  function  PFGH 
was  defined  for  all  sets  of  directions,  there  would  be  a  gradient 
PFGH...K  also  defined  for  all  sets  of  directions,  and  for  tangential 
directions  OQ,  OR,  OS,  ...  OT  we  should  have 


8122   dPQES  JdsT  =  PQBS...T  + 

+  PNRS...  KQT  +  PQNS...  KRT  +  — 

If  the  functions  P^Rs...,  PQNS...I  •-•  which  might,  of  course,  be 
different  functions,  were  known,  the  function  PQRS  T  could  be 
determined  for  tangential  arguments  by  this  formula;  if  PQRS...  was 
given  in  the  first  place  for  tangential  arguments  only,  the  functions 
PNRS...>  PQNS...>  •••  could  be  assigned  arbitrarily,  and  by  comparing 
8122  with  8121  we  see  that  the  Darboux  gradient  is  the  gradient 
found  by  supposing  the  functions  PXRS...,  PQNS...>  •••  a^  to  be 
identically  zero. 

Nevertheless,  the  Darboux  gradient  is  a  disappointing  function. 
The  Codazzi  function  is  the  Darboux  gradient  of  the  bilinear 
curvature,  and  if  <t>  is  a  function  of  position  on  the  surface  and  <&1T 
is  the  linear  function  d<&/dsT,  the  Darboux  gradient  of  <&1T  is  the 
function  (d$>ls/dsT)  —  <&IDO-TS,  which  is  in  fact  symmetrical  and  is 
valuable  on  account  of  its  symmetry.  But  the  Darboux  gradients 
of  the  Codazzi  function  and  of  the  function  (d^>ls/dsT)  —  <&IDCTTS 
prove  both  to  be  unsymmetrical  ;  gradients  with  the  symmetry 


73 

that  is  desirable  are  not  yielded  by  any  simple  general  method, 
and  all  that  is  possible  is  to  discover  special  devices  effective  in 
particular  cases. 

8  21.  To  define  multilinear  rates  of  change  of  a  regular  scalar 
function  of  position  4>  on  the  surface,  we  extend  the  function  to 
the  whole  of  space  in  the  neighbourhood  of  the  surface  by  associating 
with  every  point  on  the  normal  at  0  the  value  of  <3>  at  0  itself.  If 
two  or  more  normals  meet  at  a  point  Q,  the  function  so  defined  may 
be  many-  valued  at  Q;  if  however  the  surface  has  only  ordinary 
points  there  is  a  region  of  space  within  which  no  two  normals  inter- 
sect, and  within  this  region  <I>  is  not  only  single-valued  but  regular. 

To  assign  the  values  of  4>  outside  the  surface  in  the  way  suggested 
seems  at  first  no  less  arbitrary  a  proceeding  than  to  construct  the 
successive  Darboux  gradients  by  defining  the  functions  <&lx,  ^Vr. 
^3NST)  -••  to  be  zero.  But  a  number  of  considerations  combine  to 
modify  this  impression  :  the  multilinear  rates  of  change  formed  by 
extending  the  function  in  any  regular  way  are  necessarily  sym- 
metrical; throughout  the  whole  of  differential  geometry  the  straight 
line  is  much  more  than  merely  the  simplest  of  curves;  and  the  hypo- 
thesis made  is  in  fact  equivalent  only  to  the  assumption  that  the 
functions  <&1N,  &XN,  ^SNNN>  •••>  functions  in  which  no  arbitrary 
directions  are  involved,  are  all  zero. 

8'22.  If  attention  is  concentrated  upon  the  distribution  of  <£  on 
the  surface,  <&1N,  ^2^N,  ^V-zw*  •  •  •  figure  as  functions  of  position  only, 
^T)  3>2NT>  ^NNT*  -  •  •  as  linear  functions  of  the  one  variable  direction 
OT,  ^ST*  3>*NST>  ^NNST'--  as  bilinear  functions  of  the  pair  of 
variable  directions  OS,  OT,  and  so  on.  The  rate  of  change  of  any 
one  of  these  functions  along  a  curve  on  the  surface  is  expressible 
by  means  of  other  functions  in  the  set.  the  typical  relation  being 

8-221 


., 

—   CD  _  rr, 

N..NNPQ...RST  T*      N...N*PQ...RS 


p., 

°*    ®N...NNAQ...RS 


h+k  ,  h+k 

N..NNNP...RS 


h+k 


74 

where  OP,  OQ,  ...  OR,  OS,  OT  are  k  +  1  tangential  directions  and 
0^.,  05,  ...  OD  make  positive  right  angles  with  OP,  OQ,  .  .  .  0$.  Com- 

7,    l    I-  -4-1 

parison  of  8'221  with  8*121   shews  the  relation  of  <I>     N 

7i+& 

to  the  Darboux  gradient  of  ®N_NNPQ  ES  : 

N,..NNPQ...RST 

k  ,h+k 

NNpQ  RS  +  hKT*® 


none  of  the  functions  <&ZNT,  ^NNT>  ^>4NNNT>  •••  vanish  identically, 
and  therefore  unless  the  surface  is  a  plane,  h  must  be  zero  for 

h+k 

h*T*3>N  N  PQ  RS  to  vanish,  and  k  must  be  unity  for  the  remaining 
terms  in  the  difference  between  the  two  functions  to  vanish.  That 
is  to  say,  <&2ST  is  the  Darboux  gradient  of  <&1T,  but  there  is  no  similar 
relation  between  others  of  the  multilinear  functions  with  which  we 
are  dealing  unless  either  the  surface  is  plane  or  the  function  <5>  has 
some  special  relation  to  the  surface. 

8'23.    It  is  easy,  accepting  the  assumptions 
8-231  <£    =  0, 


with  the  implications 

8-232      d®lN/dsT  =  0,     d&NN/dsT  =  0,     d®sNNN/dsT  =  0,  .  .  .  , 

to  arrange  the  formulae  included  under  8'221  in  such  an  order  that 
each  of  the  multilinear  functions  is  introduced  without  further 
reference  to  space  outside  the  surface  than  is  implied  in  the  occur- 
rence of  bilinear  curvatures  as  factors.  The  first  equation  is 

8-233  &T  =  d®ldsTt 

from  which  <&1T  may  be  calculated  from  a  curve  lying  wholly  in  the 
surface.  Then  since 

8-234  d^NjdsT  =  &NT  -  KT*  4>V 

identically,  and  the  rate  of  change  is  zero, 

8-235  ®-NT  -  KT*  <&\  =  0  ; 

also  because  3>1N  is  zero, 

8-236  3>2ST  -I-  <TTS®ID  =  d<bls/dsT. 


75 

Next  come 
8-237 
8-238 
8239 


in  which  the  only  fresh  functions  are 

the  process  can  be  continued  to  any  desired  extent. 

8'24.  Emphatically  the  formulae  of  the  last  paragraph  and  their 
successors  are  neither  definitions  of  the  multilinear  functions  nor 
aids  to  their  calculation.  For  the  former  part  they  are  unsuitable 
because  neither  the  symmetry  nor  the  multilinearity  of  the  functions 
is  in  evidence  in  the  formulae,  for  the  latter  because  the  rates  of 
change  and  the  swerves  contain  parts  that  are  not  multilinear  which 
it  is  superfluous  to  evaluate.  To  discuss  the  expression  of  these 
multilinear  functions  by  means  of  curvilinear  coordinates  on  the 
surface  requires  an  analytical  foundation  which  is  beyond  the  range 
of  this  pamphlet,  and  we  must  content  ourselves  with  the  observa- 
tion that  rather  than  calculate  the  functions  directly  from  8"221 
we  should  combine  8"222  with  8*114  and  use  the  formula, 


8-241 

N...NNPQ...RST 


w      h+k 


N...NNPB...RS 


but  this  is  not  the  method  actually  to  be  recommended. 

The  very  lack  of  symmetry  which  renders  the  formulae  covered 
by  8*221  unfit  to  serve  as  definitions  implies  that  significant  rela- 
tions which  do  not  themselves  involve  multilinear  rates  of  change 
are  deducible  from  these  formulae.  To  work  out  details  is  interest- 
ing —  it  will  be  found  for  example  that  8'235  and  8'238  together 
imply  the  symmetry  of  the  Coclazzi  function  —  but  here  we  will 


76 

confine  our  attention  to  the  simplest  problem  of  the  kind,  and 
examine  only  8'236. 

831.    The  bilinear  function  <£2sr  being  symmetrical,  we  have 
from  8-236, 

8-311          (d&s/d8T)  -  aTs^D  =  (d&Tldss)  -  a/4^; 

involved  in  8'311  are  really  two  families  of  curves  and  their 
orthogonal  trajectories,  and  the  equality  may  be  written  in  the 
form 

d*<5>  sd<$>        d*3>  Td3> 

O  6IZ  -j  -  =  --   0>*  -  —  =  -^  -  =  --  <7</  -=—  , 

asTass  asD      dssdsT  dsE 

or  in  a  different  notation  as 


d*$>       /.       dco\d<Z> 
8616        -jTry-.  —     ««  —  -jr.  I  -j-r  =  TT^T  —  (  KQ  +  -p  ]  TTT  , 

dsds      \  -      as)  dm     dsds      \  "      ds/dm 

where  d/dm,  d/dm  indicate  rates  of  change  along  the  orthogonal 
trajectories  of  the  families.  If  the  families  of  curves  are  everywhere 
orthogonal,  8'313  becomes 

d*3>  d<S> 

dmds     Kgm  dm 

where  tcgs,  /tgm  denote  the  geodesic  curvatures  of  a  typical  member 
of  a  family  and  of  an  orthogonal  trajectory  of  the  same  family. 

8'32.  We  must  not  fail  to  observe  that  if  what  is  being  discussed 
is  the  variation  on  a  particular  surface  of  a  function  already  defined 
throughout  space,  the  formulae  of  8'23  and  the  transformations  of 
8'31  are  not  usually  valid.  For  example,  in  general  when  the  function 
and  the  surface  are  defined  independently  of  each  other, 

8-321  d$>ls/dsT  =  <E>26T  +  o-Ts$>lD  +  ^r^1^, 

and  for  the  last  term  to  disappear  either  <&1N  must  be  zero  or  OS, 
OZ'must  be  conjugate  directions.  Of  the  cases  in  which  the  latter 
condition  is  satisfied  the  most  important  is  that  in  which  the  two 
principal  directions  occur:  without  any  hypothesis  as  to  a  relation 
between  <&  and  the  surface, 

d*3>  d<t>_    d23>  d<$> 

O  o2t2t  <P  [5  —  -j  -  j  --  KqZ  -^       —    7    —j~   T  Kqi  ~T       , 

ds^dsl       '  dsz      dS[dsz       '  dsl 

and  so  in  particular  the  function  Tlz  which  was  shewn  in  7'242 
to  be  connected  with  the  twist  of  the  <&-family  is  expressible 


77 

as  (d^T/dszds,)  -  Kgz  (dT/dsz)  or  as  (d^T/d^ds^)  +  Kgl  (dT/ds,) 
although  in  general  T*N  is  not  zero  and  T2ST  differs  from 
(&T/d8Td8a)-(rTs(dTld8D)  by  KST(dT/dn). 

8"33.  The  cases  of  8'311  which  are  most  easily  appreciated  are 
found  in  the  application  to  two  special  families  of  curves  on  the 
surface,  the  <E>-curves  and  the  <E>-orthogonals.  The  gradient  of  O 
is  a  tangential  vector  G  which  is  at  right  angles  to  the  ^>-curve. 
Points  where  the  gradient  is  the  zero  vector  being  excluded,  the 
amounts  of  the  gradient  are  separate  single-valued  functions  of 
position  on  the  surface,  and  one  of  these  is  chosen  to  be  called  the 
slope  of  <3>;  the  slope  will  be  denoted  by  G.  The  direction  in  which 
the  gradient  has  the  slope  G  is  defined  to  be  the  standard  direction 
of  the  3>-orthogonal  and  of  the  tangential  normal  to  the  4>-curve,  and 
will  be  denoted  by  OM.  The  direction  OL  with  which  ON  makes 
a  positive  right  angle  is  the  standard  direction  of  the  3>-curve. 

By  definition 

8-331  3^  =  0,     &M=G, 

whence 

8-332  <£  *MT  =  dG/dsT  =  G1T, 

8-333  <b*LT  =  -  GvTL  =  -G  {tcgT  +  (deTL/dsT)}. 

Thus 

8*334.    The  geodesic  curvature  of  the  <&-curve  is  —  ^LL/^M* 
and 

8'335.  The  geodesic  curvature  of  the  <&-  orthogonal  can  be  expressed 
both  as  —  ^LM!^M  and  as-^d  (log  G*)/dsL. 

It  may  be  added  that  8'335  is  deducible  from  2'831  and  5'224, 
for  with  the  convention  by  which  <J>  is  extended  into  space  a 
<3>-surface  is  the  ruled  surface  composed  of  the  normals  to  the 
original  surface  along  a  <E>-curve. 

841.  I  have  not  succeeded  in  continuing  satisfactorily  the 
sequence  of  geometrical  functions  of  which  the  first  two  members 
are  the  bilinear  curvature  and  the  Codazzi  function.  Differentiation 
of  6115  gives 

8-411   4>VsT  +  G*QTKKS  +  G'2BTKQS  +  G*STKQR  +  G2RSKQT 


UN  (KQTKRS  +  KRTKQS 


78 

where 
8*412 


and  while  8*412  shews  that  ^QRST  depends  only  on  the  form  of  the 
•^-surface,  8'411  shews  that  the  function  is  a  symmetrical  quadri- 
linear  function  of  tangential  directions.  Thus  there  is  no  difficulty 
in  the  construction  of  the  third  member  of  the  sequence  of  functions, 
and  none  is  to  be  anticipated  in  repeating  the  process  again  and 
again,  but  no  general  rule  is  apparent  under  which  the  constructions 
fall,  and  it  is  evident  that  the  formulae  rapidly  become  too  com- 
plicated to  be  intelligible  without  some  clue  to  their  composition. 


79 


INDEX  OF  DEFINITIONS 


Amount  of  a  vector     ...         ...     Ol 

Amplitude  of  curvature,  A     ...     4'42 
Angular  derivative,  da  ...     O6 

Asymptotic  angle,  v    4*54 

Asymptotic  torsion,  su,  sa    4 '52,  4*54 
Bilinear  curvature,  KST  ...     2*31 

Bilinear  rate  of  change,  <&2PQ  ...     3'31 
Bilinear  torsion,  SST    ...         ...     4*32 

Codazzi  function,  \RST  ...     6'11 

Core        1-31 

Darljpux  determinant ...         ...     7 '34 

Darboux  function  of 

direction,  \TET  ...  6*13 
Darboux  gradient,  gdbT  ...  8'11 
Defect  of  curvature, 

B-Kn>  SET  4-12,  4'32 
Geodesic  curvature,  <ff,  crTT  2  -21,  2-41 
Geodesic  torsion,  sg,  KET  2*11,  2*32 
Gradient  of  a  core  1-71 


Gradient  of  a  scalar  function,  Gr  3*22 
Laguerre  function  of 

direction,  \TTT  ...  6*13 

Linear  function  ...         ...  I'll 

Mean  curvature,  B      ...         ...  4'12 

Multilinear  function    ...         ...  I'll 

Multilinear  rate  of  change,  ^PQ...^  3'41 

Normal  angle,  w          2 '52 

Normal  curvature,  <n,  <TT    2 '11,  2-32 

Projected  product  of  two  cores  T53 
Projected  product  of  two 

vectors,  C£TS     ...  0'2 

Radial,  1^         O'l 

Slope,  G  3-22 

Source 1-51 

Spaciousness,  T  7-22 

Spread,  rs         2*73 

Swerve,  <TTS       2-41 

Swing,  <TNS        2-71 


80 


INDEX  OF  SYMBOLS 

1R      0-1  <TNS  2-71  B      4-12 

a,/3 0-5  <r/ 2-41  6'T,  Cz   4-42 

a,  fry  0-4  <rrr  2'41  D       0'5 

A,  B,  T 0-4  s  2-52  da,  daQ 0'6 

€ST     0-5  Sa  4-54  E      0-5 

£        4-44  Sg  2-11  G       3-22 

K        2-52  SET  4'32  G      3'22 

Kg      2-21  Sn  4'52  £      0-2 

Kn      2-11  SST  4-32  gdbT 8-11 

KET    2-32  trr  4-32  /       4^52 

KSI 2-31  TS  2-73  J,K 4-54 

KTT    2-32  v  4-54  K      4'46 

»t,  »g 4-42  Y  0-4  I,  w,  n  0'4 

6-11  *1P  3-21  PAB...K I'22 

7-32  *2pw  3.31  (Pj»)s  1-33 

OT       2-52  **  v  3-41  ra      01 

or       2-72  w     '" 0-5  T 

<TTE    2-41  A  4-42  x,y,z    0'4 


PRINTED  IN  ENGLAND  BY  J.  B.  PEACE,  3M.A. 
AT    THE     CAMBRIDGE     UNIVERSITY    PRESS 


Neville,  Eric  Harold 

Multilinear  functions  of 
direction  and  their  uses  in 
differential  geometry 


Physical  & 
Applied  Sci. 


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