C OMPOSITIO M ATHEMATICA
R ICHARD L. I NGRAHAM The geometry of the heat equation
Compositio Mathematica, tome 12 (1954-1956), p. 147-156
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The geometry
of theheat equation
by
Richard L.
Ingraham
Institute for Advanced Study Princeton, N.J.
1. Introduction.
In this paper, the
powerful
methods of differentialgeometry
are
applied
to theequivalence problem
for n-dimensional genera- lized heatequations.
Thegeneral line
of attack is the same as that of aprevious
paper1)
in which thegeometry
of thegeneralized Laplace equation
wasinvestigated. Here, however,
the situation isslightly
morecomplicated
due to the presence of the extra varia- bletime.
Why geometry
in thesubject
ofpartial
differentialequations?
The answer
is,
that in theequivalence problem,
we are confrontedwith an array of dissimilar
looking
differentialequations
of thesame
general type,
and we ask whether there exists a transforma- tion of the group of transformationspreserving
thisgeneral type
which will transform one of two
given equations
into the other.The criterion for this expresses itself
naturally
in terms of theinvariants of the
equations,
thoseexpressions
which areformally unchanged throughout
the group of transformations of theseequations.
Andfinally,
thetheory
of the invariants of any group is theprovince
ofgeometry.
In Section 2 the
general theory
is worked out,culminating
inthe
equivalence
theorem under the restricted heatequation
trans-formation group. The theorem solves the
equivalence problem
forthis group,
i.e., gives
a finite criterion(that is,
in terms of finiteéquations)
for thisequivalence.
It is remarkable here that there isno
corresponding
theorem for the full heatequation
transforma- tion group. A usefulcorollary gives
the criterion that anequation
be reducible to an
ordinary
heatequation.
In Section 3, thetheory
is
applied
to a verysimple
heatequation arising
in thetheory
of1) "The Geometry of the Linear Partial Differential Equation of the Second
Order", Am. Journ. Math., 75, 691 (1953).
random walks with variable but
isotropic step.
The class of allsuch random walks which can be reduced to
ordinary (constant step)
random walksby
a transformation of space is characterizedby
the solutions of a certain set of non-linear second orderpartial
differential
equations
for the function ofposition defining
thelength
of the(isotropic ) step
at thatposition.
Theseequations
are
solved,
the solutionsexhibiting
asimple algebraic form,
ofdegree
atmost quadratic, for n ~
2, and a morecomplicated form,
defined
by
any harmoniefunction,
for n = 2.2. The heat
équation geometry
and theequivalence
theorem.
We write the
generalized
heatequation
in the formin which it has been normalized
by dividing
theequation through by
the(non-zero)
coefficient of the time-derivative term. The summation convention is observed.grs
and d’’ are functions of r’and t. The classical heat
equation
has the form(2.1)
in whichk a non-zero constant.
The
application
of differentialgeometric
methods to theseequations depends
on the extraction of certain invariants formed from their coefficients. To this end it is convenient to write the first two terms of(2.1)
as a covariantdivergence:
in which the covariant
divergence ~rVr
of any vector vr(here grs~s~)
is definedwith the linear connection
0393prs given
in this caseby
and
149
In these
formulas, ô-"
is the Kronecker deltaand {p rs}
theChristoffel
symbol
of the normalized cofactors grs ofgr,’:
That
(2.1’)
is identical with(2.1)
in virtue of the definition of the covariantdivergence
and the definitions(2.2)
and(2.3)
can beverified
by
direct substitution. A connection0393prs
of the form(2.2)
is called a
Weyl linear connection,
and we have shownincidentally
that a
Weyl linear
connection isalways
ageneral enough
connec-tion to write the heat
equation
in the covariant form(2.1’).
The
equation (2.1)
maintains its form under several groups of transformations.First,
under the directproduct
of the two groups of transformations of variablesNote that
although
the new space variables xm’ are allowed to be functions of the old time t, the new time t’ cannot involve the old spacevariables,
or we wouldget
second derivatives in the newtime.
Second,
as to the group of gauge transformations - multi-plication
of the wholeequation by
a non zero factor03BB(xm, t)
-this group has been eliminated
by
the normalization to the cano-nical form in which the coefficient of
~t~
isunity.
After a transformation
(2.4),
eq.(2.1’)
goes into another of thesame form in
gr’s’
andFr"
whereThe
"tensors"
grsand Fr
with the transformation rules(2.5)
under the group
(2.4)
characterizecompletely
theequation (vide (2.1)).
Defined over an n-dimensional manifoldof space
coordina-tes xm and a 1-dimensional manifold of time
values t, they
serveto define the n-dimensional heat
equation geometry.
Theequivalence problem
forequations (2.1)
is then reduced to theequivalence problem
for n-dimensional heatequation geometries.
As it now
stands,
theequivalence problem
is aproblem
in ana-lysis :
Given the two sets of functionsgr,s,, Fr,
functions of xm’ andt’ and grs,
Fr,
functions of aem and t, we ask whether there exists atransformation
(2.4)
such that their differential coefficientssatisfy (2.5). By expressing
theintegrability
conditions of(2.5),
we canreduce the
problem
to aquestion
of the existence of solutions offinite (e.g.,
oftenalgebraic) equations -
in the case that acomple-
te.set.of invariants of the heat
equation geometry
exists.By
com-plete
set of invariants is meant an array of tensors in terms of which theequivalence problem
can becompletely
stated in thisfinite form.
It turns out that no
complete
set of invariants exists for thisgeometry. However,
if we restrict attention to thesubgroup
of
(2.4),
in which space and time transformseparately,
the result-ing geometry,
the restricted heatequation geometry,
admits acomplete
set of invariants. Under(2.6)
the basic invariants trans- form :We
proceed
to solve theequivalence problem
for this group, thatis,
to express theintegrability
conditions of the set ofpartial
differential
equations (2.7).
Eq. (2.7 )a.
differentiated withrespect
to xp’ andrearranged, using
the inversesgl’8"
andgrs
to eliminateF, gives
where r is
the Christoffelsymbol
of gpqand {s’ p’ r’},
that of9,,,,,. (2.7 )a.
differentiated withrespect
to tgives
thééquivalent
set
where
and the
corresponding
definitions hold for theprimed
barred151
quantities 2).
Note theidentity Qss
= 0, so that(2.8’) comprises only 1n/2(n + 1),
notln/2 (n
+1)
+ 1,independent equations.
The
integrability
conditions of(2.7)c.
are satisfiedidentically
in virtue of
(2.8) (by
thesymmetry
of the Christoffelsymbols)
and of
(2.8’)a.
and b.(for
the latter can bere-arranged
togive dAT,/dt = 0).
Theintegrability
condition of(2.7)d.
is satisfied invirtue of
(2.8),
for thisequation implies ~p’F
= o.The
integrability
conditions of(2.8)
arewhere
Rsqpr (the
curvature tensorof {r ps})
is short for3)
and
The
integrability
condition of(2.8’)a.
isIn
addition,
all theequations
which follow from theequations (2.7)b., (2.8’)b., (2.9)a., (2.9’),
and(2.10) by differentiating
withrespect
to space and time andusing
theequations (2.7)c.
andd., (2.8),
and(2.8’)a.,
to eliminate the derivatives of theunknowns,
must be satisfied. We shall illustrate this process on
Eq. (2.7)b.;
the
procedure
istypical.
Differentiating (2.7)b.
withrespect
toxp’, rearranging,
andusing (2.7)c.
and(2.8)
weget
where
B7 p
means covariant derivative withrespect
to the Christof-fel
symbols {r pq}, and V,,, with respect
to {r’ p’q’}.
The nota-
tion
[Sl, T0]
means that we have differentiated(2.7)b.,
once with1) Hereafter usually only the définitions of the invariants of the one equation
will be given, the primed barred invariants being the corresponding expressions
in the primed barred quantities.
3) The square brackets [ ] around any set of indices indicates the alternating part: e.g.,
T[pq] ~ 1/2(Tpq - Tqp).
respect
to space and zero times withrespect
to time.Continuing
this process,
after i
space derivations weget
Differentiating (2.7)b. k
times withrespect to t’, rearranging,
and
using (2.7 )d.
and(2.8’ )a.
to eliminate derivatives of the un-knowns,
weget, similarly
where the differential
operator 17’ ... t(k-fold
covariant differentia- tion withrespect
totime) applied
to any tensor is defined re-cursively
where
Q
isgiven by (2.8’)c.
Combining
these twooperations,
weget
Of course the
operations
of covariant space and time derivation do not commute.However,
we remark that foreach
k it is suffi-cient to
impose only
oneequation
with the derivatives taken insome
arbitrary order,
for the difference between such anequation
and the
equation
with the differentiationsperformed
in any other order vanishes in virtue of aprevious equation. E.g.,
consider the difference between(2.7)b.: [Tl,5lJ
and:[Sl, Tl] (where
thesymbol 51
to theright
indicates that one space differentiation is to beperformed first, etc.).
Weget
But this is satisfied in virtue of
(2.7)b.
and(2.9’).
We can now state the
equivalence
theorem:THEOREM 1. Two
equations (2.1),
characterizedby
the in-variants grs and
Fs,
functions of aem and t, andgr,s,, Fs’,
functionsof x-’ and t’
respectively,
areequivalent
under the restricted heatequation
group(2.6)
if andonly
if the sets ofequations (2.7)a
and
b, (2.8’)b, (2.9), (2.9’), (2.10),
and the infinite sets:[S,, Tk]
(j,
k = 1, 2, ...,oo )
derived from each of these are satisfiedby
some set of functions x?,
Arr’
of xm’ and t, F of t’.153
Of course, the
equations
of this infinite set areusually
incom-patible -
the theorem asserts that in thespecial
case thatthey
are
compatible,
theequivalence
exsist. Inproof
weappeal
to thewell known theorem on
partial
differentialequations 4).
In case that the coefficients are functions
only
of spacevariables,
the theorem is
simplified by
thedropping
away in the criterion of allequations involving
timederivatives, namely (2.9’ )
and allthe
equations: [Sj, Tk]
for k > 0. From theremaining equations
it follows in
particular
that F must be a constant, or t’ =Ft,
F = const. is the
only
time transformationpossible
here.A case of
especial
interest arises when one of theequations
is anordinary
heatequation,
whose invariants areconstants;
Note that we allow any
signature
ofCrs
in the definition of anordinary
heatequation;
the classical case(cf.
p.3)
is thesignature (+,
+, ...+)
or( -,
-,... - ), depending
on thesign
ofk,
the
conductivity.
For thisequation,
all the differential invariants vanish. Weget
theCOROLLARY 1. A heat
equation (2.1)
isequivalent
to an or-dinary
heatequation
if andonly
if its intrinsicgeometry
is flat.By flat
we mean thatDEF. 1.
Then
(2.7 )a.
withCyg
substituted for grs déterminesn(n + 1)
of 2 the available constants. For anequation (2.1)
to beequivalent
tothe classical heat
equation,
it is necessary in addition that grs have definite(negative
orpositive) signature.
Make the
DEF. 2. A
(restricted)
heatequation geometry
is called Riemannian ifF,
= 0.This is of course an invariant
demand, by (2.7 )b.
The Rieman- nian(restricted
heatequation) geometries
form animportant
subclass. For
them,
theequivalence problem
reduces to a consid-eration of the metric grs and its various differential invariants.
Generalization: A trivial
generalization
of the abovetheory
con-sists in
letting
theequation (2.1)
have an extra term +dgo.
The4) See, say, Veblen, Invariants of Quadratic Differential Forms. (Cambridge University Press, 1952) p. 73.
modifications this
brings
to theequivalence
theorem are obvious.The
equations
to beadjoined
areand the set
(2.12): [Sj, Tk] (j,
k = 1, 2, ...oo )
derived from itby
successive space and time differentiation.
Remark on solutions: The above
theory
answers theequivalence question completely.
It will saysomething
about solutions insofaras this can be
phrased
as anequivalence question. E.g.,
supposewe are
looking
for asolution 99
of anequation (2.1)
in the space and time variables xmand t,
and we knowby
the abovetheory
that this
equation
isequivalent
to another(in
xm’ andt’ )
if whichwe know a solution
tp(aem’, t’ ).
Then a solution of the firstequation
is
given by
where xm’ =
1-’(x"), t’
=f(t)
is a transformationtaking
the oneequation into
the other..3.
Anapplication
of thetheory.
In the
theory
of random walks in n-dimensional number space with aposition-dependent isotropic step
one encounters theequation
where v is a function of
x1,
..., xn.Making
the substitutionand
writing
it in the canonical form(2.1),
we find the coefficients to bewhere ôjk has been defined on p. 3. The Christoffel
symbols
comeout to be
With the
hclp
ofthese,
the basic heatequation
invariants arecomputed
to be155
It is remarkable that
Fk
vanishesidentically
for thisequation.
The intrinsic
geometry
is then Riemannian in the sense of defini- tion 2 of last section.We now ask: For what v is
(3.1) equivalent
to anordinary
heatequation in 99? By Corollary
1 of last section this is so if andonly
ifthe other conditions
being
satisfiedidentically.
Thatis,
if andonly
if the curvature tensor of the metric(3.3)
is zero.Computing R fJflrt == R pQrast
from(3.2),
weget
where
(~V)2 ~ 03B4lm~lV~mV
and we have indicated the skewpart
in s and t
by
adeparture
from the standard notation with the square brackets to avoid confusion with the square bracketsaround p
and q.Eq. (3.5)
can be reduced tosimpler
form in thefollowing
way.Forming
the Ricci tensorRqr ~ Rpqrt03B4pt
from(3.5),
we inferwhere
~2V
is theLaplacian: q 2V - 03B4lm~2lmV.
Then for n ; 2 weget, rearranging
The left member is the content of the brackets in
(3.5).
Sub-stituting
in(3.5),
we infer that the coefficient ofà,
in the lastequation
mustvanish;
from the lastequation
it then follows thatBut
(3.7)
thenimplies (3.5).
Hence(3.7)
isequivalent
to(3.5).
When the substitution V =
log
ro2 is made in(3.7),
itsimplifies
to
These are
equivalent
toThese can be
integrated, giving
thegeneral
solutionIn the first solution c and
dp
arearbitrary
constants such thatc =1= 0. In the
second, d p
and e are constants,arbitrary
up to the nulllength
condition on thedp.
Thus,
for n =f= 2, the necessary andsufficient
condition that(3.1)
be reducible to the classical heat
equation
in rp ~ vn P.is that v have the
form (3.9)a.
or b. We remark that the trivial case v = const. is included in the solutions b. withdp
= 0.For n = 2, all the
non-vanishing components
ofR’JIqrt
are thesame as
R1212
up tosign.
Hence(3.5)
isequivalent
to(3.5’ )
whichfor n = 2 reduces
simply
toHence the
general
solution for v isi.e.,
v isExp {a
harmoniefunction}.
Therefore, f or
n = 2, the necessary andsufficient
condition that(3.1)
be reducible to the classical heatequation (3.10)
in ~ ~ v2P is that vequal
ew where w is some harmonicfunction.
Remark: Since the invariants here are no functions of t,
by
aremark of last section the time transformation can be at most F = const.
But since the
only equation determining
theintegration
constantsis
(2.7)a.,
F can be takenpositive,
and then absorbed into the transformation of the space variables. Hence"reducible"
in theabove two theorems about v can be taken to mean reducible
by
a transformation of space variables alone.