Handbook of Global Analysis 287 Demeter Krupka and David Saunders c 2007 Elsevier All rights reserved

The of operators of Dirac and Laplace type

P. Gilkey

Contents

1 Introduction 2 The geometry of operators of Laplace and Dirac type 3 Heat trace asymptotics for closed 4 Hearing the shape of a drum 5 Heat trace asymptotics of manifolds with boundary 6 Heat trace asymptotics and index theory 7 Heat content asymptotics 8 Heat content with source terms 9 Time dependent phenomena 10 Spectral boundary conditions 11 Operators which are not of Laplace type 12 The spectral geometry of Riemannian submersions

1 Introduction

The field of spectral geometry is a vibrant and active one. In these brief notes, we will sketch some of the recent developments in this area. Our choice is somewhat idiosyncratic and owing to constraints of space necessarily incomplete. It is impossible to give a com- plete bibliography for such a survey. We refer Carslaw and Jaeger [41] for a comprehensive discussion of problems associated with heat flow, to Gilkey [54] and to Melrose [91] for a discussion of methods related to the index theorem, to Gilkey [56] and to Kirsten [84] for a calculation of various heat trace and heat content asymptotic formulas, to Gordon [66] for a survey of manifolds, to Grubb [73] for a discussion of the pseudo-differential calculus relating to boundary problems, and to Seeley [116] for an introduction to the pseudo-differential calculus. Throughout we shall work with smooth manifolds and, if present, smooth boundaries. We have also given in each section a few ad- ditional references to relevant works. The constraints of space have of necessity forced us 288 Spectral geometry to omit many more important references than it was possible to include and we apologize in advance for that. We adopt the following notational conventions. Let (M, g) be a compact Riemannian of dimension m with smooth boundary ∂M. Let Greek indices µ, ν range from 1 to m and index a local system of coordinates x = (x1, ..., xm) on the of M. 2 µ ν Expand the metric in the form ds = gµν dx ◦dx were gµν := g(∂xµ , ∂xν ) and where we adopt the Einstein convention of summing over repeated indices. We let gµν be the inverse 1 m p matrix. The Riemannian measure is given by dx := g dx ...dx for g := det(gµν ). ∇ ∇ ∂ = Γ σ∂ Γ σ Let be the Levi-Civita connection. We expand ∂xν xµ νµ xσ where νµ are the Christoffel symbols. The curvature R and corresponding curvature tensor R are may then be given by R(X,Y ) := ∇X ∇Y − ∇Y ∇X − ∇[X,Y ] and given by R(X,Y,Z,W ) := g(R(X,Y )Z,W ). We shall let Latin indices i, j range from 1 to m and index a local orthonormal frame {e1, ..., em} for the tangent bundle of M. Let Rijkl be the components of the curvature tensor relative to this base; the Ricci tensor ρ and the scalar curvature τ are then given by setting ρij := Rikkj and τ := ρii = Rikki. We shall often have an auxiliary vector bundle V and an auxiliary connection given on V . We use this connection and the Levi-Civita connection to covariantly differentiate tensors of all types and we shall let ‘;’ denote the components of multiple covariant differentiation. Let dy be the measure of the induced metric on the boundary ∂M. We choose a local orthonormal frame near the boundary of M so that em is the inward unit normal. We let indices a, b range from 1 to m−1 and index the induced local frame {e1, ..., em−1} for the tangent bundle of the boundary. Let Lab := g(∇ea eb, em) denote the second fundamental form. We sum over indices with the implicit range indicated. Thus the geodesic curvature κg is given by κg := Laa. We shall let ‘:’ denote multiple tangential covariant differentia- tion with respect to the Levi-Civita connection of the boundary; the difference between ‘;’ and ‘:’ being, of course, measured by the second fundamental form.

2 The geometry of operators of Laplace and Dirac type

In this section, we shall establish basic definitions, discuss operators of Laplace and of Dirac type, introduce the DeRham complex, and discuss the Bochner Laplacian and the Weitzenboch¨ formula; [55] provides a good reference for the material of this section. Let D be a second order partial on the space of smooth sections ∞ µν σ C (V ) of a vector bundle V over M. Expand D = −{a ∂xµ ∂xν +a ∂xσ +b} where the coefficients {aµν , aµ, b} are smooth endomorphisms of V ; we suppress the fiber indices. We say that D is an operator of Laplace type if aµν = gµν id. A first order operator A on C∞(V ) is said to be an operator of Dirac type if A2 is an operator of Laplace type. ν If we expand A = γ ∂xν + γ0, then A is an operator of Dirac type if and only if the endomorphisms γν satisfy the Clifford commutation relations γν γµ + γµγν = −2gµν id. ν Let A be an operator of Dirac type and let ξ = ξν dx be a smooth 1-form on M. ν We let γ(ξ) = ξν γ define a Clifford module structure on V ; this is independent of the particular coordinate system chosen. We can always choose a fiber metric on V so that γ is skew-adjoint. We can then construct a unitary connection ∇ on V so that ∇γ = 0. Such ∇ A = γν ∇ + ψ a connection is called compatible. If is compatible, we expand ∂xν A; the P. Gilkey 289 endomorphism ψA is tensorial and does not depend on the particular coordinate system chosen; it does, of course, depend on the particular compatible connection chosen.

2.1 The DeRham complex The prototypical example is given by the exterior algebra. Let C∞(ΛpM) be the space of smooth p forms. Let d : C∞(ΛpM) → C∞(Λp+1M) be exterior differentiation and let δ = d∗ be the adjoint operator, interior differentiation. If ξ is a cotangent vector, let ext(ξ): ω → ξ ∧ ω denote exterior multiplication, and let int(ξ) be the dual, interior multiplication. Let γ(ξ) := ext(ξ)−int(ξ) define a Clifford module on the exterior algebra Λ(M) d + δ = γ(dxν )∇ d + δ . Since ∂xν , is an operator of Diract type. The associated 2 0 p m Laplacian ∆M := (d + δ) = ∆M ⊕ ... ⊕ ∆M ⊕ ... ⊕ ∆M decomposes as the direct sum p ∞ p of operators of Laplace type ∆M on the space of smooth p forms C (Λ M). One has 0 −1 µν ∆M = −g ∂xµ gg ∂xν . It is possible to write the p-form valued Laplacian in an invariant form. Extend the µν Levi-Civita connection to act on tensors of all types. Let ∆˜ M ω := −g ω;µν define the Bochner or reduced Laplacian. Let R give the associated action of the curvature tensor. The Weitzenbock¨ formula then permits us to express the ordinary Laplacian in terms of the ˜ 1 µ ν Bochner Laplacian in the form ∆M = ∆M + 2 γ(dx )γ(dx )Rµν . This formalism can be applied more generally: Lemma 2.1 Let D be an operator of Laplace type on a Riemannian manifold. There exists a unique connection ∇ on V and there exists a unique endomorphism E of V so that µν µ Dφ = −φ;ii − Eφ. If we express D locally in the form D = −{g ∂xν ∂xµ + a ∂xµ + b} then the connection 1-form ω of ∇ and the endomorphism E are given by

1 µ σε νµ σ ων = 2 (gνµa + g Γσεν id) and E = b − g (∂xν ωµ + ων ωµ − ωσΓνµ ) .

Let V be equipped with an auxiliary fiber metric. Then D is self-adjoint if and only if ∇ is unitary and E is self-adjoint. We note that if D is the Spin Laplacian, then ∇ is the spin connection on the spinor bundle and the Lichnerowicz formula [86] yields, with our 1 sign convention, that E = − 4 τ id where τ is the scalar curvature.

3 Heat trace asymptotics for closed manifolds

Throughout this section, we shall assume that D is an operator of Laplace type on a closed Riemannian manifold (M, g). We shall discuss the L2 spectral resolution if D is self- adjoint, define the heat equation, introduce the heat trace and the heat trace asymptotics, present the leading terms in the heat trace asymptotics, and discuss the form valued Lapla- cian; [41, 54, 116] are good references for the material of this section and other references will be cited as needed. We suppose that D is self-adjoint. There is then a complete spectral resolution of D on 2 2 L (V ). This means that we can find a complete orthonormal basis {φn} for L (V ) where the φn are smooth sections to V which satisfy the equation Dφn = λnφn. Let ||k denote the Ck-. 2 P∞ 2 Theorem 3.1 Let φ ∈ L (V ). Expand φ = n=1 cnφn in the L sense where one has R ∞ k cn := M (φ, φn). If φ ∈ C (V ), then this series converges in the C topology for any 290 Spectral geometry

∞ k k; φ ∈ C (V ) if and only if limn→∞ n cn < ∞ for any k. The set of eigenvalues is discrete. Each eigenvalue appears with finite multiplicity and there are only a finite number of negative eigenvalues. If we enumerate the eigenvalues so that λ1 ≤ λ2 ≤ ..., 2/m then λn ∼ n as n → ∞. There exist constants νk > 0 and Ck > 0 so that one has νk norm estimates ||φn||k ≤ Ckn for all k, n. This yields the familiar Weyl asymptotic formula [127] giving the eigenvalue growth. 2 For example, if D = −∂θ on the circle, then the eigenvalues grow quadratically since the associated spectral resolution is given by {n2, √1 einθ} . The L2 expansion of 2π n∈Z Theorem 3.1 in this setting then becomes the usual Fourier series expansion for φ and one has the familiar result that a function on the circle is smooth if and only if its Fourier coefficients are rapidly decreasing. Let the initial temperature distribution be given by φ ∈ L2(V ). Impose the classical time evolution for the subsequent temperature distribution without additional heat input:

2 (∂t + D)u = 0 for t > 0 and lim u(t, ·) = φ in L . t↓0

Then u(t, ·) = e−tDφ where e−tD is given by the . This operator is R infinitely smoothing; we have u(t, x) = M K(t, x, x˜)φ(˜x)dx˜ for a smooth kernel function K. If D is self-adjoint, let {λn, φn} be a spectral resolution of D. Then

X −tλn K(t, x, x˜) := e φn(x) ⊗ φn(˜x): Vx˜ → Vx . n

Theorem 3.1 implies this series converges uniformly in the Ck topology for t ≥ ε > 0. Let F ∈ C∞(End(V )) be an auxiliary endomorphism used for localizing; F is of-  −tD ten referred to as a smearing endomorphism. The localized heat trace TrL2 F e is analytic for t > 0. As t ↓ 0, there is a complete asymptotic expansion [117]

∞  −tD X (n−m)/2 TrL2 F e ∼ an(F,D)t . n=0

The coefficients an(F,D) are the heat trace asymptotics; an(F,D) = 0 if n is odd. In Section 5 we will consider manifolds with boundary and the corresponding invariants are non-trivial for n both even and odd. There exist locally computable endomorphisms M en (D)(x) of V which are defined for all x ∈ M so that Z M an(F,D) = Tr{F en (D)}(x)dx . (3.a) M

M The invariants en (D) are uniquely characterized by Equation (3.a). We use Lemma 2.1 to express D = D(g, ∇,E) where ∇ is a uniquely defined connec- tion on V and where E is a uniquely defined auxiliary endomorphism of V . Let Ωij be the endomorphism valued components of the curvature defined by the connection ∇. Theorem 3.2 Let F ∈ C∞(End(V )) be a smearing endomorphism.

−m/2 R (1) a0(F,D) = (4π) M Tr{F }dx. −m/2 1 R (2) a2(F,D) = (4π) 6 M Tr{F (6E + τ id)}dx. P. Gilkey 291

−m/2 1 R 2 (3) a4(F,D) = (4π) 360 M Tr{F (60E;kk + 60τE + 180E 2 2 2 +12τ ;kk id +5τ id −2|ρ| id +2|R| id +30ΩijΩij)}dx. R 18 17 2 4 (4) a6(F,D) = M Tr{F (( 7! τ ;iijj + 7! τ ;kτ ;k − 7! ρij;kρij;k − 7! ρjk;nρjn;k 9 28 8 24 12 + 7! Rijkl;nRijkl;n + 7! ττ ;nn − 7! ρjkρjk;nn + 7! ρjkρjn;kn + 7! RijklRijkl;nn 35 3 14 2 14 2 208 64 + 9·7! τ − 3·7! τ|ρ| + 3·7! τ|R| − 9·7! ρjkρjnρkn − 3·7! ρijρklRikjl 16 44 80 − 3·7! ρjkRjnliRknli − 9·7! RijknRijlpRknlp − 9·7! RijknRilkpRjlnp) id 1 1 1 1 1 + 45 Ωij;kΩij;k + 180 Ωij;jΩik;k + 60 Ωij;kkΩij + 60 ΩijΩij;kk − 30 ΩijΩjkΩki 1 1 1 1 1 − 60 RijknΩijΩkn − 90 ρjkΩjnΩkn + 72 τΩknΩkn + 60 E;iijj + 12 EE;ii 1 1 1 3 1 1 1 + 12 E;iiE + 12 E;iE;i + 6 E + 30 EΩijΩij + 60 ΩijEΩj + 30 ΩijΩijE 1 1 1 1 1 1 + 36 τE;kk + 90 ρjkE;jk + 30 τ ;kE;k − 60 E;jΩij;i + 60 Ωij;iE;j + 12 EEτ 1 1 2 1 2 1 2 + 30 Eτ ;kk + 72 Eτ − 180 E|ρ| + 180 E|R| )}dx.

There are formulas available for a8 and a10; we refer to Amsterdamski, Berkin, and O’Connor[1], to Avramidi [9], and to van de Ven [124] for further details. There is also information available about the general form of the heat trace asymptotics an for all values of n; we refer to Avramidi [10] and to Branson et al. [36] for further details. These formulas play an important role in the compactness results we shall discuss presently in Theorem 4.6. Let D be an operator of Laplace type on a closed Riemannian n n+1 manifold M. Let ∆E = −E;kk. Set n = (−1) /{2 · 1 · 3 · ... · (2n + 1)}. Theorem 3.3 Let ‘+...’ denote lower order terms.

−m/2 R n−1 (1) If n ≥ 1, then a2n(F,D) = n(4π) M Tr{F (−(8n + 4)∆ E −2n∆n−1τ id +...}dx.

−m/2 2 n−2 2 (2) If n ≥ 3, then a2n(D) = n(4π) Tr{(n − n − 1)|∇ τ| id +2|∇n−2ρ|2 id +4(2n + 1)(n − 1)∇n−2τ · ∇n−2E +2(2n + 1)∇n−2Ω · ∇n−2Ω +4(2n + 1)(2n − 1)∇n−2E · ∇n−2E + ...}dx. We note that Polterovich [109, 110] has introduced a formalism for computing in closed form the heat trace asymptotics an for all n. If one specializes these formulas for a0, a2, and a4 to the case in which D is the form valued Laplacian, one has the following result of Patodi [106]. Introduce constants:

m! c(m, p) = p!(m−p)! , c0(m, p) = c(m, p) − 6c(m − 2, p − 1), c1(m, p) = 5c(m, p) − 60c(m − 2, p − 1) + 180c(m − 4, p − 2), c2(m, p) = −2c(m, p) + 180c(m − 2, p − 1) − 720c(m − 4, p − 2), c3(m, p) = 2c(m, p) − 30c(m − 2, p − 1) + 180c(m − 4, p − 2) .

p −m/2 Theorem 3.4 (1) a0(∆M ) = (4π) c(m, p) Vol(M). p −m/2 1 R (2) a2(∆M ) = (4π) 6 c0(m, p) M τdx. p −m/2 1 R 2 2 2 (3) a4(∆M ) = (4π) 360 M {c1(m, p)τ + c2(m, p)ρ + c3(m, p)R }dx. 292 Spectral geometry

Such formulas play an important role in the study of spectral geometry. There is a long history involved in computing these invariants. Weyl [127] discovered the leading term in the asymptotic expansion, a0. Minakshisundaram and Pleijel [93, 94] examined the asymptotic expansion for the scalar Laplacian in some detail. The a2 and a4 terms in the asymptotic expansion were investigated by McKean and Singer [90] in the scalar case and by Patodi [105] for the form valued Laplacian. The a6 term for the scalar Laplacian was determined by Sakai [111] and the general expression for a2, a4 and a6 for arbitrary operators of Laplace type was worked out in [53]. As noted above, there are formulas for a8 and a10. The literature is a vast one and we refer to [54, 56] more details and additional references. We now discuss the relationship between the heat trace asyptotics and the eta and zeta functions in a quite general context. Let P be a positive, self-adjoint elliptic partial differ- ential operator on a closed Riemannian manifold M. Then e−tP is an infinitely smoothing operator which is given by a smooth kernel function. Let Q be an auxiliary partial differ- −tP ential operator. Then TrL2 {Qe } is analytic for t > 0 and as t ↓ 0, there is a complete asymptotic expansion with locally computable coefficients:

∞ −tP X (n−m−ord(Q))/ ord(P ) TrL2 {Qe ) ∼ an(P,Q)t n=0 The generalized zeta function is given by:

−s ζ(s, P, Q) := TrL2 (QP ) for <(s) >> 0 . The Mellin transform may be used to relate the zeta function to the . Let Γ be the classical Gamma function. We refer to Seeley [116, 117] for the proof of Assertions (1) and (2) and to [50] for the proof of Assertion (3) in the following result. Assertion (2) generalizes eigenvalue growth estimates of Weyl [127] given previously in Theorem 3.1. −1 R ∞ s−1 −tP Theorem 3.5 (1) If Re(s) >> 0, then ζ(s, P, Q) = Γ(s) 0 t TrL2 (Qe )dt. Γ(s)ζ(s, P, Q) has a meromorphic extension to the complex plane with isolated sim- ple poles at s = (m + ord(Q) − n)/ ord(P ) for n = 0, 1, ... and

Ress=(m+ord(Q)−n)/ ord(P ) Γ(s)ζ(s, P, Q) = an(P,Q).

(2) The leading heat trace coefficient a0(P ) is non-zero. Let λ1 ≤ ... ≤ λn ≤ ... be the −m/ ord(P ) m −1 eigenvalues of P . Then limn→∞ nλn = Γ( ord(P ) ) a0(P ). (3) Let A(t) and B(t) be polynomials of degree a ≥ 0 and b > 0 where B is monic. There are constants so an(B(P ),A(P )) = Σk≤k(n)c(k, n, m, A, B)ak(P ).

4 Hearing the shape of a drum

Let Spec(D) = {λ1 ≤ λ2 ≤ ...} denote the set of eigenvalues of a self-adjoint operator of Laplace type, repeated according to multiplicity. One is interested in what geometric and topological properties of M are reflected by the spectrum. Good references for this section are [26, 54, 66]; other references will be cited as appropriate. One says that M and M˜ are isospectral if Spec(∆0 ) = Spec(∆0 ); p-isospectral M M˜ refers to ∆p. M. Kac [81] in his seminal article raised the question of determining the P. Gilkey 293 geometry, at least in part, of the underlying manifold from the spectrum of the scalar 0 ∆M . It is not possible in general to completely determine the geome- try: Theorem 4.1 (1) Milnor [92]: There exist isospectral non isometric flat tori of dimen- sion 16. (2) Vigneras [125]: There exist isospectral non-isometric hyperbolic Riemann surfaces. Furthermore, if m ≥ 3, there exist isospectral hyperbolic manifolds with different fundamental groups. (3) Ikeda [79]: There exist isospectral non-isometric spherical space forms.

(4) Urakawa [123]: There exist regions Ωi in flat space for m ≥ 4 which are isospectral for the Laplacian with both Dirichlet and Neumann boundary conditions but which are not isometric.

These examples listed above come in finite families. We say that a family of metrics gt on M is a non-trivial family of isospectral manifolds if (M, gt) and (M, gs) are isospectral for every s, t, but (M, gt) is not isometric to (M, gs) for s 6= t. Theorem 4.2 (1) Gordon-Wilson [67]: There exists a non-trivial family of isospectral metrics on a smooth manifold M which are not conformally equivalent. (2) Brooks-Gordon [37]: There exists a non-trivial family of isospectral metrics on a smooth manifold M which are conformally equivalent. There is a vast literature in the subject. In particular, Sunada [121] gave a general method for attacking the problem which has been exploited by many authors. Despite this somewhat discouraging prospect, there are a number of positive results available. For example Berger [27] and Tanno [122] showed that a sphere or projective space is characterized by its spectral geometry, at least in low dimensions:

Theorem 4.3 Let Mi and M2 be closed Riemannian manifolds of dimension m ≤ 6 which are isospectral. If M1 has constant sectional curvature c, so does M2. Patodi [106] showed additional geometrical properties are determined by the form val- ued Laplacian. The following is an easy consequence of Theorem 3.4.

Theorem 4.4 Let M1 and M2 be closed Riemannian manifolds which are p-isospectral for p = 0, 1, 2. Then:

(1) If M1 has constant scalar curvature τ = c, then so does M2.

(2) If M1 is Einstein, so is M2.

(3) If M1 has constant sectional curvature c, then so does M2. For manifolds with boundary, suitable boundary conditions must be imposed. Formulas that will be discussed presently in Section 5 have been used by Park [104] to show:

Theorem 4.5 Let M1 and M2 be compact Einstein Riemannian manifolds with smooth boundaries with the same constant scalar curvatures τ M1 = τ M2 . Also assume that M1 and M2 are isospectral for both Neumann and Dirichlet boundary conditions. Then:

(1) If M1 has totally geodesic boundary, then so does M2. 294 Spectral geometry

(2) If M1 has minimal boundary, then so does M2.

(3) If M1 has totally umbillic boundary, then so does M2.

(4) If M1 has strongly totally umbillic boundary, then so does M2. There are also a number of compactness results. Theorem 3.3 plays a central role in the following results: Theorem 4.6 (1) Osgood, Phillips, and Sarnak [102]: Families of isospectral metrics on Riemann surfaces are compact modulo gauge equivalence.

(2) Brooks, Perry, and Yang [39] and Chang and Yang [42]: If m = 3, then families of isospectral metrics within a conformal class are compact modulo gauge equivalence.

(3) Brooks, Perry, and Petersen [38]: Isospectral negative curvature manifolds contain only a finite number of topological types.

5 Heat trace asymptotics of manifolds with boundary

In previous sections, we have concentrated on closed Riemannian manifolds. Let D be an operator of Laplace type on a compact Riemannian manifold M with smooth boundary ∂M. Good basic references for the material of this section are [56, 73, 84]. Many authors have contributed to the material discussed here; we refer in particular to the work of [40, 76, 78, 82, 83, 90, 93, 94, 96, 120, 127]. We impose suitable boundary conditions B to have a well posed problem; B must satisfy a condition called the strong Lopatenski-Shapiro condition. We shall suppress tech- nical details for the most part in the interests of simplicity. The boundary conditions we shall consider have physical underpinnings. Dirichlet boundary conditions correspond to immersing the boundary in ice water; Neumann boundary conditions correspond to an in- sulated boundary. Robin boundary conditions are a generalization of Neumann boundary conditions where the heat flow across the boundary is proportional to the temperature on the boundary. Transmission boundary conditions arise in the study of heat conduction problems between closely coupled membranes. Transfer boundary conditions arise in the study of branes. Both these conditions reflect the heat flow between two inhomogeneous mediums coupled along a common boundary or brane. Transmission boundary conditions correspond to having the two components pressed tightly together. By contrast, heat trans- fer boundary conditions correspond to a loose coupling between the two components. We refer to Carslaw and Jaeger [41] for further details. Through out the remainder of this section, we let F ∈ C∞(End(V )) define a localizing or smearing endomorphism and let B denote a suitable boundary operator; in what follows, we shall give a number of examples. Let DB be the realization of an operator D of Laplace type with respect B; the domain of DB is then the set of all functions φ in a suitable Schwarz space so that φ satisfies the appropriate boundary conditions, i.e. so that Bφ = 0. Greiner [68, 69] and Seeley [118, 119] showed that there was a full asymptotic expansion as t ↓ 0 of the form:

∞ −tDB X (n−m)/2 TrL2 {F e } ∼ an(F,D, B)t . n=0 P. Gilkey 295

There are locally computable endomorphisms en(D)(x) defined on the interior and locally ∂M computable endomorphisms en,k (D, B)(y) defined on the boundary so that Z M an(F,D, B) = Tr{F en (D)}(x)dx M n−1 X Z + Tr{(∇k F )e∂M (D, B)}(y)dy . em n,k k=0 ∂M

M ∂M The invariants en (D) and en,k (D, B) are uniquely characterized by this identity; the in- M terior invariants en (D) are not sensitive to the boundary condition and agree with those considered previously in Equation (3.a). The remainder of Section 5 is devoted to giving explicit combinatorial formulas for these invariants. A function φ satisfies Dirichlet boundary conditions if φ vanishes on ∂M. Thus the Dirichlet boundary operator is defined by:

Bφ := φ|∂M . (5.a)

Theorem 5.1 [Dirichlet boundary conditions] Let F ∈ C∞(End(V )).

−m/2 R (1) a0(F,D, B) = (4π) M Tr{F }dx.

−(m−1)/2 1 R (2) a1(F,D, B) = −(4π) 4 ∂M Tr{F }dy.

−m/2 1 R −m/2 1 R (3) a2(F,D, B) = (4π) 6 M Tr{F (6E + τ)}dx + (4π) 6 ∂M Tr{2FLaa

−3F;m}dy.

1 −(m−1)/2 R (4) a3(F,D, B) = − 384 (4π) ∂M Tr{96FE + F (16τ + 8Ramam + 7LaaLbb

−10LabLab) − 30F;mLaa + 24F;mm}dy.

−m/2 1 R 2 2 (5) a4(F,D, B) = (4π) 360 M Tr{F (60E;kk + 60τE + 180E + 30Ω + 12τ ;kk 2 2 2 −m/2 1 R +5τ − 2|ρ | + 2|R |)}dx + (4π) 360 ∂M Tr{F (−120E;m + 120ELaa

−18τ ;m + 20τLaa + 4RamamLbb − 12RambmLab + 4RabcbLac + 24Laa:bb 40 88 320 + 21 LaaLbbLcc − 7 LabLabLcc + 21 LabLbcLac) + F;m(−180E − 30τ 180 60 − 7 LaaLbb + 7 LabLab) + 24F;mmLaa − 30F;iim}dy.

Neumann boundary conditions are defined by the operator BN φ := φ;m|∂M ; the asso- ciated boundary conditions define a perfectly insulated boundary with no heat flow across the boundary. It is convenient in many applications to consider slightly more general con- ditions called Robin boundary conditions that permit the heat flow to be proportional to the temperature. Let S be an auxiliary endomorphism of V over ∂M. The Robin boundary operator is defined by:

BSφ := (φ;m + Sφ)|∂M . (5.b)

Theorem 5.2 [Robin boundary conditions] Let F ∈ C∞(End(V )).

−m/2 R (1) a0(F,D, BS) = (4π) M Tr{F }dx. 296 Spectral geometry

(1−m)/2 1 R (2) a1(F,D, BS) = (4π) 4 ∂M Tr{F }dy.

−m/2 1 R −m/2 1 R (3) a2(F,D, BS) = (4π) 6 M Tr{F (6E + τ)}dx + (4π) 6 ∂M Tr{F (2Laa

+12S) + 3F;m}dy.

(1−m)/2 1 R (4) a3(F,D, BS) = (4π) 384 ∂M Tr{F (96E + 16τ + 8Ramam + 13LaaLbb 2 +2LabLab + 96SLaa + 192S +F;m(6Laa + 96S) + 24F;mm}dy.

−m/2 1 R 2 2 (5) a4(F,D, BS) = (4π) 360 M Tr{F (60E;kk +60τE +180E +30Ω +12τ ;kk 2 2 2 −m/2 1 R +5τ − 2|ρ| + 2|R| )}dx + (4π) 360 ∂M Tr{F (240E;m + 42τ ;m

+24Laa:bb + 120ELaa + 20τLaa + 4RamamLbb − 12RambmLab + 4RabcbLac 40 32 + 3 LaaLbbLcc + 8LabLabLcc + 3 LabLbcLac + 360(SE + ES) + 120Sτ 2 3 +144SLaaLbb + 48SLabLab + 480S Laa + 480S + 120S:aa) + F;m(180E 2 +30τ + 12LaaLbb + 12LabLab + 72SLaa + 240S ) + F;mm(24Laa + 120S)

+30F;iim}dy. When discussing the Euler characteristic of a manifold with boundary in Section 6 subsequently, it will useful to consider absolute and relative boundary conditions. Let r be the geodesic distance to the boundary. Near the boundary, decompose a differential form ∞ ω ∈ C (Λ(M)) in the form ω = ω1 + dr ∧ ω2 where the ωi are tangential differential forms. We define the relative boundary operator Br and the absolute boundary operator Ba for the operator d + δ by setting:

Br(ω) = ω1|∂M and Ba(ω) = ω2|∂M . (5.c)

There are induced boundary conditions for the associated Laplacian (d + δ)2. They are ¯ defined by the operator Br/aφ := Br/aφ ⊕ Br/a(d + δ)φ. ¯ The boundary conditions defined by the operators Br/a provide examples of a more general boundary condition which are called mixed boundary conditions. We can combine Theorems 5.1 and 5.2 into a single result by using such boundary conditions. We assume given a decomposition V |∂M = V+ ⊕ V−. Extend the bundles V± to a collared neighbor- hood of ∂M by parallel translation along the inward unit geodesic rays. Set χ := Π+−Π−. Let S be an auxiliary endomorphism of V+ over ∂M. The mixed boundary operator may then be defined by setting

Bχ,Sφ := Π+(φ;m + Sφ)|∂M ⊕ Π−φ|∂M . (5.d)

One sets χ = id, Π+ = id, and Π− = 0 to obtain the Robin boundary operator of Equation (5.b); one sets χ = − id, Π+ = 0, and Π− = id to obtain the Dirichlet boundary operator of Equation (5.a). The formulas of Theorem 5.1 and Theorem 5.2 then be obtained by this specialization. Theorem 5.3 [Mixed boundary conditions] Let F = f id for f ∈ C∞(M). Then:

−m/2 R (1) a0(F,D, Bχ,S) = (4π) M Tr{F }dx.

−(m−1)/2 1 R (2) a1(F,D, Bχ,S) = (4π) 4 ∂M Tr{F χ}dy. P. Gilkey 297

−m/2 1 R (3) a2(F,D, Bχ,S) = (4π) 6 M Tr{F (6E + τ)}dx −m/2 1 R +(4π) 6 ∂M Tr{2FLaa + 3F;mχ + 12FS}dy.

−(m−1)/2 1 R (4) a3(F,D, Bχ,S) = (4π) 384 ∂M Tr{F (96χE + 16χτ + 8χRamam 2 +[13Π+ − 7Π−]LaaLbb + [2Π+ + 10Π−]LabLab + 96SLaa + 192S

−12χ:aχ:a) + F;m([6Π+ + 30Π−]Laa + 96S) + 24χF;mm}dy. −m/2 1 R 2 (5) a4(F,D, Bχ,S) = (4π) 360 M Tr{F (60E;kk + 60τE + 180E 2 2 2 2 −m/2 1 R +30Ω +12τ ;kk +5τ −2|ρ| +2|R| )}dx+(4π) 360 M Tr{F ([240Π+

−120Π−]E;m + [42Π+ − 18Π−]τ ;m + 120ELaa + 24Laa:bb + 20τLaa 280 +4RamamLbb − 12RambmLab + 4RabcbLac + 720ES + 120Sτ + [ 21 Π+ 40 168 264 224 320 + 21 Π−]LaaLbbLcc + [ 21 Π+ − 21 Π−]LabLabLcc + [ 21 Π+ + 21 Π−] 2 3 ×LabLbcLac + 144SLaaLbb + 48SLabLab + 480S Laa + 480S + 120S:aa

+60χχ:aΩam − 12χ:aχ:aLbb − 24χ:aχ:bLab − 120χ:aχ:aS) + F;m(180χE 84 180 2 84 60 +30χτ + [ 7 Π+ − 7 Π−]LaaLbb + 240S + [ 7 Π+ + 7 Π−]LabLab

+72SLaa − 18χ:aχ:a) + F;mm(24Laa + 120S) + 30F;iimχ}dy. −(m−1)/2 1 R (6) a5(F,D, Bχ,S) = (4π) 5760 ∂M Tr{F {360χE;mm + 1440E;mS 2 2 +720χE + 240χE:aa + 240χτE + 48χτ ;ii + 20χτ − 8χρijρij 2 +8χRijklRijkl − 120χρmmE − 20χρmmτ + 480τS + 12χτ ;mm 2 +24χρmm:aa + 15χρmm;mm + 270τ ;mS + 120ρmmS + 960SS:aa 2 +16χRammbρab − 17χρmmρmm − 10χRammbRammb + 2880ES 4 111 +1440S + (90Π+ + 450Π−)LaaE;m + ( 2 Π+ + 42Π−)Laaτ ;m

+30Π+LabRammb;m + 240LaaS:bb + 420LabS:ab + 390Laa:bS:b 487 413 +480Lab:aS:b + 420Laa:bbS + 60Lab:abS + ( 16 Π+ + 16 Π−)Laa:bLcc:b 49 11 +(238Π+ − 58Π−)Lab:aLcc:b + ( 4 Π+ + 4 Π−)Lab:aLbc:c 535 355 151 29 +( 8 Π+ − 8 Π−)Lab:cLab:c + ( 4 Π+ + 4 Π−)Lab:cLac:b

+(111Π+ − 6Π−)Laa:bbLcc + (−15Π+ + 30Π−)Lab:abLcc 15 75 945 285 +(− 2 Π+ + 2 Π−)Lab:acLbc + ( 4 Π+ − 4 Π−)Laa:bcLbc

+(114Π+ − 54Π−)Lbc:aaLbc + 1440LaaSE + 30LaaSρmm + 240LaaSτ

−60LabρabS + 180LabSRammb + (195Π+ − 105Π−)LaaLbbE 195 105 +(30Π+ + 150Π−)LabLabE + ( 6 Π+ − 6 Π−)LaaLbbτ 275 215 +(5Π+ + 25Π−)LabLabτ + (− 16 Π+ + 16 Π−)LaaLbbρmm 275 215 +(− 8 Π+ + 8 Π−)LabLabρmm + (−Π+ − 14Π−)LccLabρab 109 49 +( 4 Π+ − 4 Π−)LccLabRammb + 16χLabLacρbc 133 47 +( 2 Π+ + 2 Π−)LabLacRbmmc − 32χLabLcdRacbd 315 2041 65 + 2 LccLabLabS + ( 128 Π+ + 128 Π−)LaaLbbLccLdd 298 Spectral geometry

417 141 +150LabLbcLacS + ( 32 Π+ + 32 Π−)LccLddLabLab 2 2 375 777 +1080LaaLbbS + 360LabLabS + ( 32 Π+ − 32 Π−)LabLabLcdLcd 885 17 3 + 4 LaaLbbLccS + (25Π+ − 2 Π−)LddLabLbcLac + 2160LaaS 231 327 2 +( 8 Π+ + 8 Π−)LabLbcLcdLda − 180E + 180χEχE − 120S:aS:a 105 105 +720χS:aS:a − 4 ΩabΩab + 120χΩabΩab + 4 χΩabχΩab − 45ΩamΩam

+180χΩamΩam − 45χΩamχΩam + 360(ΩamχS:a − ΩamS:aχ)

+45χχ:aΩamLcc − 180χ:aχ:bΩab + 90χχ:aχ:bΩab + 90χχ:aΩam;m

+120χχ:aΩab:b +180χχ:aΩbmLab +300χ:aE:a −180χ:aχ:aE −90χχ:aχ:aE 675 +240χ:aaE −30χ:aχ:aτ −60χ:aχ:bρab +30χ:aχ:bRmabm − 32 χ:aχ:aLbbLcc 75 195 675 − 4 χ:aχ:bLacLbc − 16 χ:aχ:aLcdLcd − 8 χ:aχ:bLabLcc − 330χ:aS:aLcc 15 15 15 105 −300χ:aS:bLab + 4 χ:aχ:aχ:bχ:b + 8 χ:aχ:bχ:aχ:b − 4 χ:aaχ:bb − 2 χ:abχ:ab 135 195 −15χ:aχ:aχ:bb− 2 χ:bχ:aab}+F;m{( 2 Π+−60Π−)τ ;m+240τS−90ρmmS 3 +270S:aa + (630Π+ − 450Π−)E;m + 1440ES + 720S + (90Π+ + 450Π−) 165 255 2 ×LaaE + (− 8 Π+ − 8 Π−)Laaρmm + (15Π+ + 75Π−)Laaτ + 600LaaS 1215 315 45 165 +( 8 Π+ − 8 Π−)Laa:bb − 4 χLab:ab +(15Π+ −30Π−)Labρab +(− 4 Π+ 465 705 75 459 495 + 4 Π−)LabRammb + 4 LaaLbbS − 2 LabLabS + ( 32 Π+ + 32 Π−) 267 1485 225 ×LaaLbbLcc +( 16 Π+ − 16 Π−)LccLabLab +(−54Π+ + 2 Π−)LabLbcLac 165 405 −210χ:aS:a − 16 χ:aχ:aLcc − 8 χ:aχ:bLab +135χχ:aΩam}+F;mm{30LaaS 315 1215 645 945 +( 16 Π+ − 16 Π−)LaaLbb +(− 8 Π+ + 8 Π−)LabLab +60χτ −90χρmm 2 +360χE + 360S − 30χ:aχ:a} + F;mmm{180S + (−30Π+ + 105Π−)Laa}

+45χF;mmmm}dy.

We now consider transmission and transfer boundary conditions. Let M+ and M− be two manifolds which are coupled along a common boundary Σ := ∂M+ = ∂M−. We have metrics g± and operators D± of Laplace type on M±. We have scalar smearing functions f± over M±. Transmission boundary conditions arise in the study of heat conduction problems between closely coupled membranes. We impose the compatibility conditions

g+|Σ = g−|Σ,V+|Σ = V−|Σ = VΣ, f+|Σ = f−|Σ .

No matching condition is assumed on the normal derivatives of f or of g on the interface Σ. Assume given an impedance matching endomorphism U defined on the hypersurface Σ. The transmission boundary operator is given by:   BU φ := φ+|Σ − φ−|Σ ⊕ ∇ν+ φ+|Σ + ∇ν− φ−|Σ − Uφ+|Σ , (5.e) + − ωa := ∇a − ∇a .

Since the difference of two connections is tensorial, ωa is a well defined endomorphism of VΣ. The tensor ωa is chiral; it changes sign if the roles of + and − are reversed. On the other hand, the tensor field U is non-chiral as it is not sensitive to the roles of + and −. P. Gilkey 299

The following result is due to Gilkey, Kirsten, and Vassilevich [62]; see also related work by Bordag and Vassilevich [31] and by Moss [95]. Define:

even + − odd + − Lab := Lab + Lab, Lab := Lab − Lab, even odd F;ν := f;ν+ + f;ν− , F;ν := f;ν+ − f;ν− , even odd F;νν := f;ν+ν+ + f;ν−ν− , F;νν := f;ν+ν+ − f;ν−ν− , Eeven := E+ + E−, Eodd := E+ − E−, even + − odd + − E;ν := E;ν+ + E;ν− , E;ν := E;ν+ − E;ν− , even + − odd + − Rijkl := Rijkl + Rijkl, Rijkl := Rijkl − Rijkl even + − odd + − Ωij := Ωij + Ωij, Ωij := Ωij − Ωij .

Theorem 5.4 [Transmission boundary conditions]

−m/2 R (1) a0(f, D, BU ) = (4π) M f Tr(id)dx.

(2) a1(f, D, BU ) = 0.

−m/2 1 R (3) a2(f, D, BU ) = (4π) 6 M f Tr{τ id +6E}dx −m/2 1 R even +(4π) 6 Σ 2f Tr{Laa id −6U}dy.

(1−m)/2 1 R 3 even even even even (4) a3(f, D, BU ) = (4π) 384 Σ Tr{f[ 2 Laa Lbb + 3Lab Lab ] id even even 2 even even +9Laa F;ν id +48fU + 24fωaωa − 24fLaa U − 24F;ν U}dy.

−m/2 1 R 2 (5) a4(f, D, BU ) = (4π) 360 M f Tr{60E;kk + 60RijjiE + 180E 2 2 2 +30ΩijΩij + [12τ ;kk + 5τ − 2|ρ| + 2|R| ] id}dx −m/2 1 R odd odd odd odd +(4π) 360 Σ Tr{[−5RijjiF;ν + 2Raνaν F;ν odd even odd odd even odd 18 even even even −5Laa Lbb F;ν − Lab Lab F;ν + 7 Lab Lab F;ν 12 even even even even even odd odd even − 7 Laa Lbb F;ν + 12Laa F;νν ] id +f[−Lab Lab Lcc even odd odd odd odd even odd odd even −Lab Lab Lcc + 2Lab Lbc Lac + 2RabcbLac + 12Rijji;ν 40 even even even 4 even even even 68 even even even + 21 Laa Lbb Lcc − 7 Lab Lab Lcc + 21 Lab Lbc Lac even even even even even even even +24Laa:bb + 10Rijji Laa + 2Raνaν Laa − 6Raνbν Lab even even 2 even odd odd odd odd +2Rabcb Lac ] id +18ωaF;ν − 30E F;ν + 15ULaa F;ν even even even 2 even 2 even −30UF;νν − 9ULaa F;ν + 30U F;ν + f[12ωaLbb even even odd even even 3 +24ωaωbLab + 60E;ν − 60ωaΩaν + 60E Laa − 60U even even even even −30URijji − 180UE − 60U:aa − 18ULaa Lbb even even 2 even 2 −6ULab Lab + 60U Laa − 60Uωa]}dy. We now examine transfer boundary conditions. As previously, we take structures (M, g, V, D) = ((M+, g+,V+,D+), (M−, g−,V−,D−)). We now assume the compat- ibility conditions

∂M+ = ∂M− = Σ and g+|Σ = g−|Σ . 300 Spectral geometry

We no longer assume an identification of V+|Σ with V−|Σ. Let F± be smooth smearing endomorphisms of V±; there is no assumed relation between F+ and F−. Let Tr± denote the fiber trace on V±. We suppose given auxiliary impedance matching endomorphisms S := {S±±} from V± to V±. The transfer boundary operator is defined by setting:  +    ∇ + S++ S+− φ B φ := ν+ + . (5.f) S S ∇− + S φ −+ ν− −− − Σ

We set S+− = S−+ = 0 to introduce the associated decoupled Robin boundary conditions B φ := (∇+ + S )φ | , R(S++) + ν+ ++ + Σ and B φ := (∇− + S )φ | . R(S−−) − ν− −− − Σ

Define the correction term an(F,D,S)(y) by means of the identity Z Z

an(F,D, BS) = an(F,D)(x)dx + an(F+,D+, BR(S++))dy M Σ Z Z

+ an(F−,D−, BR(S−−))dy + an(F,D,S)(y)dy . Σ Σ

As the interior invariants an(F,D) are discussed in Theorem 3.4 and as the Robin invari- ants an(F,D, BR(S++)) and an(F,D, BR(S−−)) are discussed in Theorem 5.2, we must only determine the invariant an(F,D,S) which measures the new interactions that arise from S+− and S−+. We refer to [63] for the proof of the following result: Theorem 5.5 [Transfer boundary conditions]

(1) an(F,D, BS)(y) = 0 for n ≤ 2.

(1−m)/2 1  (2) a3(F,D, BS)(y) = (4π) 2 Tr+(F+S+−S−+) + Tr−(F−S−+S+−) . −m/2 1  (3) a4(F,D, BS)(y) = (4π) 360 Tr+{480(F+S++ + S++F+)S+−S−+ +480F+S+−S−−S−+ + − +(288F+Laa + 192F+Laa + 240F+;ν+ )S+−S−+}

+ Tr−{480(F−S−− + S−−F−)S−+S+− + 480F−S−+S++S+− − + +(288F−Laa + 192F−Laa + 240F−;ν− )S−+S+−} . We now take up . We refer to [33, 34] for the material of this section. Let M be a compact Riemannian manifold. Let A be an operator of Dirac type and 2 −tD let D = A be the associated operator of Laplace type. Instead of studying TrL2 (e ), −tD we study TrL2 (Ae ); this provides a measure of the spectral asymmetry of A. Let ∇ be a compatible connection; this means that ∇γ = 0 and that if there is a fiber V ∇ A = γν ∇ + ψ ∂M metric on that is unitary. Expand ∂xν A. If is non-empty, we shall use local boundary conditions; we postpone until a subsequent section the question of spectral boundary conditions. Let {e1, ..., em} be a local orthonormal frame for the tangent bundle near ∂M which is normalized so em is the inward unit geodesic normal vector field. Suppose there exists an endomorphism χ of V |∂M so that χ is self-adjoint and so that

2 χ = 1, χγm + γmχ = 0, and χγa = γaχ for 1 ≤ a ≤ m − 1 . P. Gilkey 301

Such a χ always exists if M is orientable and if m is even as, for example, one could take th χ = εγ1...γm−1 where ε is a suitable 4 root of unity. There are topological obstructions ± 1 to the existence of χ if m is odd; if ∂M is empty, χ plays no role. Let Πχ := 2 (id ±χ) − be orthonormal projection on the ±1 eigenspaces of χ. We let Bφ := Πχ φ|∂M . The 2 associated boundary condition for D := A is defined by the operator B1φ := Bφ ⊕ BAφ and is equivalent to a mixed boundary operator Bχ,S where

1 S = 2 Π+(γmψA − ψAγm − Laaχ)Π+ . As t ↓ 0, there is an asymptotic expansion

∞ 2 −tAB X η (n−m−1)/2 TrL2 (F Ae ) ∼ an(F, A, B)t . n=0 η η These invariants measure the spectral asymmetry of A; an(F, A, B) = −an(F, −A, B). 1 Theorem 5.6 Let Wij := Ωij − 4 Rijklγkγl where Ω is the curvature of ∇. Let F = f id for f ∈ C∞(M). η (1) a0(f, A, B) = 0. η −m/2 R (2) a1(f, A, B) = −(4π) (m − 1) M f Tr{ψA}dx. η 1 −(m−1)/2 R (3) a2(f, A, B) = 4 (4π) ∂M (2 − m)f Tr{ψAχ}dy. η 1 −m/2 R  (4) a3(f, A, B) = − 12 (4π) M f Tr{2(m − 1)∇ei ψA + 3(4 − m)ψAγiψA

+3γjψAγjγiψA};i + (m − 3) Tr{−τψA − 6γiγjWijψA + 6γiψA∇ei ψA 3 2 1 −m/2 R +(m − 4)ψA − 3ψAγjψAγj} dx − 12 (4π) ∂M Tr{6(m − 2)f;mχψA

+f[(6m − 18)χ∇em ψA + 2(m − 1)∇em ψA + 6χγmγa∇ea ψA 2 +6(2 − m)χψALaa + 2(3 − m)ψALaa + 6(3 − m)χγmψA + 3γmψAγaψAγa

+3(3 − m)χγmψAχψA + 6χγaWam]}dy.

6 Heat trace asymptotics and index theory

We refer to [54] for a more exhaustive treatment; the classical results may be found in [2, 3, 4, 7, 8]. In this section, we only present a brief introduction to the subject as it relates ∞ ∞ to heat trace asymptotics. Let P : C (V1) → C (V2) be a first order partial differential operator on a closed Riemannian manifold M. We assume V1 and V2 are equipped with fiber metrics. We say that the triple C := (P,V1,V2) is an elliptic complex of Dirac type if ∗ ∗ the associated second order operators D1 := P P and D2 := PP are of Laplace type. One may then define Index(C) := dim ker(D1) − dim ker(D2) −tD1 −tD2 Bott noted that TrL2 {e } − T rL2 {e } = Index(C) was independent of the parameter t. He then used the asymptotic expansion of the heat equation to obtain a lo- cal formula for the index in terms of heat trace asymptotics. Following the notation of Equation (3.a), one may define the heat trace asymptotics of P by setting:

M  M M an (P )(x) := Tr{en (D1)} − Tr{en (D2)}}(x) . One then has a local formula for the index: 302 Spectral geometry

Theorem 6.1 Let C be an elliptic complex of Dirac type over a closed Riemannian mani- fold M. Then: Z  M Index(C) if n = m, an (P )(x)dx = M 0 if n 6= m .

M The critical term am (P )(x)dx is often referred to as the index density. The other terms are in divergence form since they integrate to zero. They need not, however, vanish identically. The existence of a local formula for the index implies the index is constant under defor- mations. It also yields, less trivially, that the index is multiplicative under finite coverings and additive with respect to connected sums. In the next section, we shall see that the index of the DeRham complex is the Euler-Poincare characteristic χ(M) of the manifold. Thus if F → M1 → M2 is a finite covering, then χ(M1) = |F | · χ(M2). Similarly, if m M = M1#M2 is a connected sum, then χ(M) + χ(S ) = χ(M1) + χ(M2). Analogous formulas hold for the Hirzebruch signature of a manifold. We define DeRham complex as follows. Let d : C∞(ΛpM) → C∞(Λp+1M) be exterior differentiation and let δ : C∞(ΛpM) → C∞(Λp−1M) be the dual, interior mul- tiplication. We may then define a 2-term elliptic complex of Dirac type:

(d + δ): C∞(ΛeM) → C∞(ΛoM) where (6.a) e 2n o 2n+1 Λ (M) := ⊕nΛ (M) and Λ (M) := ⊕nΛ (M) .

Let Rijkl be the curvature tensor. Let m = 2m ¯ be even. Let {e1, ..., em} be a local orthonormal frame for the tangent bundle. We sum over repeated indices to define the Pfaffian

g(ei1 ∧ ... ∧ eim , ej1 ∧ ... ∧ ejm ) PF : = R ...R . m πm¯ 8m¯ m¯ ! i1i2j1j2 im−1imjm−1jm

Set PF m = 0 if m is odd. The following result of Patodi [105] recovers the classical Gauss-Bonnet theorem of Chern [43]: Theorem 6.2 Let M be a closed even dimensional Riemannian manifold. Then

M (1) an (d + δ)(x) = 0 for n < m.

M (2) am (d + δ)(x) = PF m(x). R (3) χ(M) = M PF m(x)dx. One can discuss Gauss-Bonnet theorem for manifolds with boundary similarly. On the boundary, normalize the orthonormal frame so em is the inward unit normal and let indices a, b range from 1 to m − 1 and index the induced frame for the tangent bundle of the boundary. Let Lab be the components of the second fundamental form. Define the transgression of the Pfaffian by setting:

X g(ea1 ∧ ... ∧ eam−1 , eb1 ∧ ... ∧ ebm−1 ) T PF : = m πk8kk!(m − 1 − 2k)! vol(Sm−1−2k) k

× Ra1a2b1b2 ...Ra2k−1a2kb2k−1b2k La2k+1b2k+1 ...Lam−1bm−1 . P. Gilkey 303

If we impose absolute boundary conditions as discussed in Equation (5.c) to define the el- liptic complex, we recover the Chern-Gauss-Bonnet theorem for manifolds with boundary e o [44]. Let ∆M and ∆M denote the Laplacians on the space of smooth differential forms of even and odd degrees, respectively. Let

∂M  ∂M e ∂M 0 an (d + δ)(y) = Tr{en (∆M , Ba)} − Tr{en (∆M , Ba)} (y) . Theorem 6.1 extends to this setting to become: Z Z  M ∂M 0 if n 6= m, an (d + δ)(x)dx + an (d + δ)(y)dy = M ∂M χ(M) if n = m . Theorem 6.2 then extends to this setting to yield: ∂M Theorem 6.3 (1) an (d + δ)(y) = 0 for n < m. ∂M (2) am (d + δ)(y) = T PF m. R R (3) χ(M) = M PF m(x)dx + ∂M T PF m(y)dy. M The local index invariants am+2(d + δ)(x) are in divergence form but do not vanish identically. Set m¯ Φ = {R R ...R } m πm¯ 8m¯ m¯ ! i1i2j1k;k i3i4j3j4 im−1imjm−1jm ;j2 × g(ei1 ∧ ... ∧ eim , ej1 ∧ ... ∧ ejm ) .

M 1 1 Theorem 6.4 If M is even, then am+2(d + δ) = 12 PF m;kk + 6 Φm. Spectral boundary conditions plan an important role in index theory. We suppose given ∞ ∞ an elliptic complex of Dirac type P : C (V1) → C (V2). Let γ be the leading symbol of P . Then  0 γ∗  γ 0 defines a unitary Clifford module structure on V1⊕V2. We may choose a unitary connection ∇ on V1 ⊕ V2 which is compatible with respect to this Clifford module structure and which respects the splitting and induces connections ∇1 and ∇2 on the bundles V1 and V2, respectively. Decompose P = γi∇ei + ψ. Near the boundary, the structures depend on the normal variable. We set the normal variable xm to zero to define a tangential operator of Dirac type

−1 ∞ B(y) := γm(y, 0) (γa(y, 0)∇ea + ψ(y, 0)) on C (V1|∂M ) .

∗ 2 Let B be the adjoint of B on L (V1|∂M );

∗ −1 ∗ B = γm(y, 0) γa(y, 0)∇ea + ψB

−1 where ψB := γm(y, 0) ψ(y, 0). Let Θ be an auxiliary self-adjoint endomorphism of V1. We set

1 ∗ ∞ A := 2 (B + B ) + Θ on C (V1|∂M ), # m m −1 ∞ A := −γ A(γ ) on C (V2|∂M ) . 304 Spectral geometry

T −1 The leading symbol of A is then given by γa := γm γa which is a unitary Clifford mod- ∞ ule structure on V1|∂M . Thus A is a self-adjoint operator of Dirac type on C (V1|∂M ); # ∞ similarly A is a self-adjoint operator of Dirac type on C (V2|∂M ). + + # Let ΠA (resp. ΠA# ) be spectral projection on the eigenspaces of A (resp. A ) corre- sponding to the positive (resp. non-negative) eigenvalues; there is always a bit of technical fuss concerning the harmonic eigenspaces that we will ignore as it does not affect the heat trace asymptotic coefficients that we shall be considering. Introduce the associated spectral boundary operators by

+ ∞ B1φ1 := ΠA(φ1|∂M ) for φ1 ∈ C (V1), + ∞ B2φ2 := ΠA# (φ2|∂M ) for φ2 ∈ C (V2), ∞ BΘφ1 := B1φ1 ⊕ B2(P φ1) for φ1 ∈ C (V1) . If P , P ∗ , and D are the realizations of P , of P ∗, and of D with respect to the B1 B2 1,B 1 boundary conditions B1,B2, and BΘ, respectively, then

(P )∗ = P ∗ D = P ∗ P . B1 B2 and 1,BΘ B1 B1 We will discuss these boundary conditions in further detail in Section 10. The local index density for the twisted signature and for the twisted spin complex has been identified using methods of invariance theory; see, for example, the discussion in Atiyah, Bott, and Patodi [5]. This identification of the local index density has been used to give a heat equation proof of the Atiyah-Singer index theorem in complete generality and has led to the proof of the index theorem for manifolds with boundary of Atiyah, Patodi, and Singer [6]. Unlike the DeRham complex, a salient feature of these complexes is the necessity to introduce spectral boundary conditions for the twisted signature and twisted spin complexes – there is a topological obstruction which prevents using local boundary conditions. The eta invariant plays an essential role in this development. We also refer to N. Berline, N. Getzler, and M. Vergne [28], to Bismut [30], and to Melrose [91] for other treatments of the local index theorem. The Dolbeault complex is a bit different. Patodi [106] showed the heat trace invariants agreed with the classical Riemann-Roch invariant for a Kaehler manifold; it should be noted that this is not the case for an arbitrary Hermitian manifold. The Lefschetz fixed point formulas can also be established using heat equation methods.

7 Heat content asymptotics

We refer to [41, 56] for further details concerning the material of this section; we note that the asymptotic series for the heat content function is established by van den Berg et al [24] in a very general setting. Let D be an operator of Laplace type on a smooth vector bundle V over a smooth Riemannian manifold. Let h·, ·i denote the natural pairing between V and the dual bundle V˜ . Let ρ ∈ C∞(V˜ ) be the specific heat and let φ ∈ C∞(V ) be the initial heat temperature distribution of the manifold. Impose suitable boundary conditions B; we shall denote the dual boundary conditions for the dual operator D˜ on C∞(V˜ ) by B˜. Let ∇ be the connection determined by D and E the associated endomorphism. Then the dual connection ∇˜ and the dual endomorphism E˜ are the connection and the endomorphism determined by D˜. P. Gilkey 305

The total heat energy content of the manifold is given by: Z β(φ, ρ, D, B)(t) = β(ρ, φ, D,˜ B˜)(t) := hρ, e−tDφidx . M As t ↓ 0, there is a complete asymptotic expansion of the form

∞ X n/2 β(φ, ρ, D, B)(t) ∼ βn(φ, ρ, D, B)t . n=0

M ∂M There are local interior invariants βn and boundary invariants βn so that Z Z M ∂M βn(φ, ρ, D, B) = βn (φ, ρ, D)(x)dx + βn (φ, ρ, D, B)(y)dy . M ∂M These invariants are not uniquely characterized by this formula; divergence terms in the interior can be compensated by corresponding boundary terms. We now study the heat content asymptotics of the disk Dm in Rm and the hemisphere Hm in Sm. We let D be the scalar Laplacian, φ = ρ = 1, and impose Dirichlet boundary 0 conditions to define βn(M) := βn(1, 1, ∆M , BD). One has [16, 17] that: Theorem 7.1 Let Dm be the unit disk in Rm. Then: m πm/2 (1) β0(D ) = (2+m) . Γ( 2 )

m π(m−1)/2 (2) β1(D ) = −4 m . Γ( 2 )

m πm/2 (3) β2(D ) = m (m − 1). Γ( 2 )

m π(m−1)/2 (4) β3(D ) = − m (m − 1)(m − 3). 3Γ( 2 )

m πm/2 (5) β4(D ) = − m (m − 1)(m − 3). 8Γ( 2 )

m π(m−1)/2 (6) β5(D ) = m (m − 1)(m − 3)(m + 3)(m − 7). 120Γ( 2 )

m πm/2 2 (7) β6(D ) = m (m − 1)(m − 3)(m − 4m − 9). 96Γ( 2 )

m π(m−1)/2 4 3 2 (8) β7(D ) = − m (m − 1)(m − 3)(m − 8m − 90m + 424m + 633). 3360Γ( 2 ) Theorem 7.2 Let Hm be the upper hemisphere of the unit sphere Sm. Then

m (1) β2k(H ) = 0 for any m if k > 0.

3 8π1/2 (2) β2k+1(H ) = k!(2k−1)(2k+1) .

3/2 2k+3 5 π 2 (2−k) (3) β2k+1(H ) = 3k!(2k−1)(2k+1) . 306 Spectral geometry

k 7 π5/2  (67−54k)9 Pk 3·23` (4) β2k+1(H ) = 30 k!(2k−1)(2k+1) + `=0 `!(k−`)!(2k−2`+1) . We now study the heat content asymptotics with Dirichlet boundary conditions. Let BD be the Dirichlet boundary operator of Equation (5.a). We refer to [16, 19] for the proof of: Theorem 7.3 [Dirichlet boundary conditions] R (1) β0(φ, ρ, D, BD) = M hφ, ρidx.

√2 R (2) β1(φ, ρ, D, BD) = − π ∂M hφ, ρidy.

R R 1 (3) β2(φ, ρ, D, BD) = − M hDφ, ρidx + ∂M {h 2 Laaφ, ρi − hφ, ρ;mi}dy.

√2 R 2 2 (4) β3(φ, ρ, D, BD) = − π ∂M { 3 hφ;mm, ρi + 3 hφ, ρ;mmi − hφ:a, ρ:ai + hEφ, ρi 2 1 1 1 − 3 Laahφ, ρi;m + h( 12 LaaLbb − 6 LabLab − 6 Ramma)φ, ρi}dy. 1 R ˜ R 1 1 ˜ (5) β4(φ, ρ, D, BD) = 2 M hDφ, Dρidx + ∂M { 2 h(Dφ);m, ρi + 2 hφ, (Dρ);mi 1 1 ˜ 1 1 1 − 4 hLaaDφ, ρi − 4 hLaaφ, Dρi + h( 8 E;m − 16 LabLabLcc + 8 LabLacLbc 1 1 1 1 − 16 RambmLab + 16 RabcbLac + 32 τ ;m + 16 Lab:ab)φ, ρi 1 1 1 − 4 Labhφ:a, ρ:bi − 8 hΩamφ:a, ρi + 8 hΩamφ, ρ:ai}dy.

We may compute βn(M) for n ≤ 4 by setting φ = ρ = 1 and E = Ω = 0 in Theorem 7.3. One has a formula [18] for β5(M); β5(φ, ρ, D, BD) is not known in full generality. 1√ R Theorem 7.4 β5(M) = − 240 π ∂M {8ρmm;mm − 8Laaρmm;m + 16LabRammb;m 2 −4ρmm + 16RammbRammb − 4LaaLbbρmm − 8LabLabρmm + 64LabLacRmbcm −16LaaLbcRmbcm − 8LabLacRbddc − 8LabLcdRacbd + 4RabcmRabcm +8RabbmRaccm − 16Laa:bRbccm − 8Lab:cLab:c + LaaLbbLccLdd −4LaaLbbLcdLcd +4LabLabLcdLcd −24LaaLbcLcdLdb +48LabLbcLcdLda}dy.

The invariants β0(M), β1(M), and β2(M) were computed by van den Berg and Davies [20] and by van den Berg and Le Gall [21] for domains in Rm. The invariants β0(M), β1(M), and β2(M) were computed by van den Berg [14] for the upper hemi- sphere of the unit sphere. The general case where D is an arbitrary operator of Laplace type and where φ and ρ are arbitrary was studied in [16, 19]. Savo [112, 113, 114, 115] has given a closed formula for all the heat content asymptotics βk(M) that is combinatorially quite different in nature from the formulas we have presented here. There is also impor- tant related work of McAvity [87, 88], of McDonald and Meyers [89], and of Phillips and Jansons [108]. We now study heat content asymptotics for Robin boundary conditions. Let BS be the Robin boundary operator of Equation (5.b); the dual boundary condition is then given by ˜ ˜ ˜ BSρ = BS˜ρ = (ρ;m + Sρ)|∂M where, of course, we use the dual connection on V to define ρ;m. The following result is proved in [19, 45]: Theorem 7.5 [Robin boundary conditions] R (1) β0(φ, ρ, D, BS) = M hφ, ρidx.

(2) β1(φ, ρ, D, BS) = 0. P. Gilkey 307

R R (3) β2(φ, ρ, D, BS) = − M hDφ, ρidx + ∂M hBSφ, ρidy.

2 √2 R (4) β3(φ, ρ, D, BS) = 3 · π ∂M hBSφ, BS˜ρidy. 1 R ˜ R 1 ˜ 1 (5) β4(φ, ρ, D, BS) = 2 M hDφ, Dρidx + ∂M {− 2 hBSφ, Dρi − 2 hDφ, BS˜ρi 1 1 +h( 2 S + 4 Laa)BSφ, BS˜ρi}dy.

√2 R 4 ˜ (6) β5(φ, ρ, D, BS) = π ∂M {− 15 (hBSDφ, BS˜ρi + hBSφ, BS˜Dρi) 2 2 4 2 4 1 − 15 h(BSφ):a, (BS˜ρ):ai + h( 15 E + 15 S + 15 SLaa + 30 LaaLbb 1 1 + 15 LabLab − 15 Ramam)BSφ, BS˜ρi}dy. 1 R 2 ˜ R 1 ˜ 1 2 ˜ (7) β6(φ, ρ, D, BS) = − 6 M hD φ, Dρidx + ∂M { 6 hBSDφ, Dρi + 6 hD φ, BSρi 1 ˜ 2 1 ˜ 1 ˜ ˜ 1 ˜ + 6 hBSφ, D ρi− 6 hSBSDφ, BSρi− 6 hSBSφ, BSDρi− 12 hLaaBSDφ, BSρi 1 ˜ ˜ 1 1 1 1 − 12 hLaaBSφ, BSDρi + h( 24 E;m + 12 ELaa + 48 LabLabLcc + 24 LabLacLbc 1 1 1 1 1 − 48 RambmLab + 48 RabcbLac − 24 RamamLbb + 96 τ ;m + 48 Lab:ab + 1 12 SLaaLbb 1 1 1 1 2 1 3 + 12 SLabLab − 12 SRamam + 12 (SE + ES) + 4 S Laa + 6 S 1 ˜ 1 ˜ 1 ˜ + 6 S:aa)BSφ, BSρi − 12 Laah(BSφ):b, (BSρ):bi − 12 Labh(BSφ):a, (BSρ):bi 1 ˜ 1 ˜ − 6 hS(BSφ):a, (BSρ):ai − 24 hΩam(BSφ):a, BSρi 1 ˜ + 24 hΩamBSφ, (BSρ):ai}dy. We now turn our attention to mixed boundary conditions. We use Equation (5.d) to defined the mixed boundary operator Bχ,S. The dual boundary operator on V˜ is given by ˜ ˜ ˜ ˜ Bχ,Sρ := Π+(ρ;m + Sρ)|∂M ⊕ Π−ρ|∂M . Extend χ to a collared neighborhood of M to be parallel along the inward normal geodesic rays. Then χ;m = 0. Let φ± := Π±φ and ˜ ρ± := Π±ρ. Since χ;m = 0, φ±;m = Π±(φ;m) and ρ±;m = Π±(φ;m). As χ:a need not vanish in general, we need not have equality between φ±:a and Π±(φ:a) or between ρ±:a ˜ and Π±(ρ:a). We refer to [45] for the proof of: Theorem 7.6 [Mixed boundary conditions] R (1) β0(φ, ρ, D, Bχ,S) = M hφ, ρidx.

√2 R (2) β1(φ, ρ, D, Bχ,S) = − π ∂M hφ−, ρ−idy. R R (3) β2(φ, ρ, D, Bχ,S) = − M hDφ, ρidx + ∂M {hφ+;m + Sφ+, ρ+i 1 +h 2 Laaφ−, ρ−i − hφ−, ρ−;mi}dy.

√2 R 2 2 (4) β3(φ, ρ, D, Bχ,S) = π ∂M {− 3 hφ−;mm, ρ−i − 3 hφ−, ρ−;mmi + 2 3 Laahφ−, ρ−i;m 1 1 1 2 ˜ +h(− 12 LaaLbb+ 6 LabLab+ 6 Ramma)φ−, ρ−i+ 3 hφ+;m+Sφ+, ρ+;m+Sρ+i 2 2 −hEφ−, ρ−i + hφ−:a, ρ−:ai + 3 hφ+:a, ρ−:ai + 3 hφ−:a, ρ+:ai 2 2 − 3 hEφ−, ρ+i − 3 hEφ+, ρ−i}dy. 308 Spectral geometry

We adopt the notation of Equation (5.e) to define the transmission boundary operator BU and the tensor ω. Theorem 7.7 [Transmission boundary conditions] R R (1) β (φ, ρ, D, BU ) = hφ , ρ idx+ + hφ , ρ idx−. 0 M+ + + M− − −

√1 R (2) β1(φ, ρ, D, BU ) = − π Σhφ+ − φ−, ρ+ − ρ−idy. R R (3) β (φ, ρ, D, BU ) = − hD+φ , ρ idx+ − hD−φ , ρ idx− 2 M+ + + M− − − R  1 + − + Σ 8 (Laa + Laa)(hφ+, ρ+i + hφ−, ρ−i) 1 + − 1 − 8 (Laa +Laa)(hφ+, ρ−i+hφ−, ρ+i)+ 2 (hφ+;ν , ρ+i+hφ−;ν ρ−i+hφ+;ν , ρ−i 1 1 +hφ−;ν , ρ+i) − 2 (hφ+, ρ+;ν i + hφ−, ρ−;ν i) + 2 (hφ+, ρ−;ν i + hφ−, ρ+;ν i) 1 − 4 (hUφ+, ρ+i + hUφ−, ρ−i + hUφ+, ρ−i + hUφ−, ρ+i) dy.

√1 R ˜ (4) β3(φ, ρ, D, BU ) = 6 π Σ{4(hD+φ+, ρ+i + hφ+, D+ρ+i + hD−φ−, ρ−i ˜ ˜ ˜ +hφ−, D−ρ−i)−4(hD+φ+, ρ−i+hφ+, D−ρ−i+hD−φ−, ρ+i+hφ−, D+ρ+i)

−(hωaφ+;a, ρ+i − hωaφ−;a, ρ−i − hωaφ+, ρ+;ai + hωaφ−, ρ−;ai)

−(hωaφ+;a, ρ−i − hωaφ−;a, ρ+i + hωaφ+, ρ−;ai − hωaφ−, ρ+;ai)

+4(hφ+;ν , ρ+;ν i+hφ−;ν , ρ−;ν i+hφ+;ν , ρ−;ν i+hφ−;ν , ρ+;ν i)−2(hφ+;a, ρ+;ai

+hφ−;a, ρ−;ai) +2(hφ+;a, ρ−;ai + hφ−;a, ρ+;ai) − 2(hUφ+;ν , ρ+i

+hUφ+, ρ+;ν i+hUφ−;ν , ρ−i+hUφ−, ρ−;ν i)−2(hUφ−;ν , ρ+i+hUφ−, ρ+;ν i − + +hUφ+;ν , ρ−i + hUφ+, ρ−;ν i) + (Laa − Laa)(ν+hφ+, ρ+i − ν−hφ−, ρ−i) + − +Laa(hφ+;ν , ρ−i + hφ−, ρ+;ν i) + Laa(hφ−;ν , ρ+i + hφ+, ρ−;ν i) − + −(Laa(hφ+;ν , ρ−i + hφ−, ρ+;ν i) + Laa(hφ−;ν , ρ+i + hφ+, ρ−;ν i)) 1 + − +hωaωaφ+, ρ+i + hωaωaφ−, ρ−i − 2 LaaLbb(hφ+, ρ+i + hφ−, ρ−i) 1 + − 1 + + − − + 2 LaaLbb(hφ+, ρ−i + hφ−, ρ+i) + 2 (LabLabhφ+, ρ+i + LabLabhφ−, ρ−i) 1 − − + + 1 + + − − + 2 (LabLabhφ+, ρ+i + LabLabhφ−, ρ−i) − 2 (LabLab + LabLab)(hφ+, ρ−i + − − +hφ−, ρ+i) + LaahUφ+, ρ+i + LaahUφ−, ρ−i − LaahUφ+, ρ+i + 2 2 2 2 −LaahUφ−, ρ−i + hU φ+, ρ+i + hU φ−, ρ−i + hU φ+, ρ−i + hU φ−, ρ+i

+hE+φ+, ρ+i + hE−φ−, ρ−i + hE−φ+, ρ+i + hE+φ−, ρ−i 1 + − −h(E+ +E−)φ+, ρ−i−h(E+ +E−)φ−, ρ+i+ 2 (Ramma +Ramma)(hφ+, ρ+i 1 + − +hφ−, ρ−i) − 2 (Ramma + Ramma)(hφ+, ρ−i + hφ−, ρ+i)}dy. We continue our studies by examining the heat content asymptotics for transfer bound- ary conditions Adopt the Equation (5.f) to define the transfer boundary operator BS. Let B˜S be the dual boundary operator ( + ! ) ∇˜ + S˜ S˜  ρ  ˜ ν+ ++ −+ + BSρ := − . S˜ ∇˜ + S˜ ρ− +− ν− −− Σ We refer to [57] for the proof of the following result: P. Gilkey 309

Theorem 7.8 [Transfer boundary conditions] R R (1) β (φ, ρ, D, BS) = hφ , ρ idx+ + hφ , ρ idx−. 0 M+ + + M− − −

(2) β1(φ, ρ, D, BS) = 0. R R (3) β (φ, ρ, D, BS) = − hD+φ , ρ idx+ − hD−φ , ρ idx− 2 M+ + + M− − − R + ΣhBSφ, ρidy.

√4 R ˜ (4) β3(φ, ρ, D, BS) = 3 π ΣhBSφ, BSρi)dy. Oblique boundary conditions are of particular interest. Let D be an operator of Laplace type on a bundle V over M. Let BT be a tangential first order partial differential operator on V |∂M and let B˜T be the dual operator on V˜ |∂M . The associated oblique boundary conditions on V and dual boundary conditions on V˜ are defined by: ˜ ˜ BOφ := (φ;m + BT φ)|∂M and BOρ := (ρ;m + BT ρ)|∂M .

th Note that we recover Robin boundary conditions by taking BT to be a 0 order operator. We refer to [59] for the proof of the following result: Theorem 7.9 [Oblique boundary conditions] R (1) β0(φ, ρ, D, BO) = M hφ, ρidx.

(2) β1(φ, ρ, D, BO) = 0. R R (3) β2(φ, ρ, D, BO) = − M hDφ, ρidx + ∂M hBOφ, ρidy.

√4 R ˜ (4) β3(φ, ρ, D, BO) = 3 π ∂M hBOφ, BOρidy. 1 R ˜ R 1 ˜ (5) β4(φ, ρ, D, BO) = 2 M hDφ, Dρidx + ∂M {− 2 hBOφ, Dρi 1 ˜ 1 1 ˜ − 2 hDφ, Bρi + h( 2 BT + 4 Laa)BOφ, BOρi}dy. We refer to [24] for further details concerning Zaremba boundary conditions. We as- sume given a decomposition ∂M = CR ∪ CD as the union of two closed submanifolds with common smooth boundary CR ∩ CD = Σ. Let φ;m denote the of φ with respect to the inward unit normal on ∂M. Let S be an auxiliary endomorphism of

V |CR . We take Robin boundary conditions on CR and Dirichlet boundary conditions on CD arising from the boundary operator:

BZ φ := (φ;m + Sφ)|{CR−Σ} ⊕ φ|CD . We refer to related work of Avramidi [11], of Dowker [46, 47], and of Jakobson et al. [80] concerning the heat trace asymptotics. There is some additional technical fuss concerned with choosing a boundary condition on the interface CD ∩ CR that we will suppress in the interests of brevity. Instead, we shall simply give a classical formulation of the problem. Suppose D = ∆ is the Laplacian and that S = 0. Let W 1,2(M) be the closure of C∞(M) with respect to the Sobolev norm Z 2 2 2 ||φ||1 = {|∇φ| + |φ| }dx. M 310 Spectral geometry

Let W 1,2 (M) be the closure of the set {φ ∈ W 1,2(M): supp(φ) ∩ C = ∅}. Let 0,CD D

N(M,CD, λ) = sup(dim Eλ) for λ > 0 where the supremum is taken over all subspaces E ⊂ W 1,2 (M) such that λ 0,CD

||∇φ||L2(M) < λ||φ||L2(M), ∀φ ∈ Eλ .

This is the spectral counting function for the Zaremba problem described above. On Σ, we choose an orthonormal frame so em is the inward unit normal of ∂M in M and so that em−1 is the inward unit normal of Σ in CD.

Theorem 7.10 [Zaremba boundary conditions] There exist universal constants c1 and c2 so that: R (1) β0(φ, ρ, D, B) = M hφ, ρidx. (2) β (φ, ρ, D, B) = − √2 R hφ, ρidy. 1 π CD (3) β (φ, ρ, D, B) = − R hDφ, ρidx + R {hφ + Sφ, ρi}dy 2 M CR ;m R 1 1 R + { Laahφ, ρi − hφ, ρ i}dy − hφ, ρidz. CD 2 ;m 2 Σ

(4) β (φ, ρ, D, B) = √4 R hφ + Sφ, ρ + Sρ˜ idy − √2 R { 2 hφ , ρi 3 3 π CR ;m ;m π CD 3 ;mm 2 2 1 + 3 hφ, ρ;mmi − hφ:a, ρ:ai + hEφ, ρi − 3 Laahφ, ρi;m + h( 12 LaaLbb

1 1 R 1 √2 − 6 LabLab + 6 Ramam)φ, ρi}dy + Σ{h(c1Lm−1,m−1 + ( 2 c2 + 3 π )Luu

√1 ˜ √1 √2 + 2 π Luu + c2S)φ, ρi + 2 π hφ, ρi;m−1 − 3 π hφ, ρi;m}dz. We conclude this section with a brief description of the non-smooth setting. We refer to van den Berg and Srisatkunarajah [25] for a discussion of the heat content asymptotics of polygonal regions in the plane. The fractal setting also an important one and we refer to van den Berg [15], to Fleckinger et al. [51], to Griffith and Lapidus [70], to Lapidus and Pang [85], and to Neuberger et al. [100] for a discussion of some asymptotic results for heat problems on the von Koch snowflake.

8 Heat content with source terms

We follow the discussion in [18, 22, 23, 56] throughout this section. Let D be an operator of Laplace type. Assume ∂M = CD ∪ CR decomposes as a disjoint union of two closed, possibly empty, disjoint subsets; in contrast to the Zaremba problem, we emphasize that CD∩CR is empty. Let B be the Dirichlet boundary operator on CD and the Robin boundary operator on CR. Let φ be the initial temperature of the manifold, let ρ = ρ(x; t) be a variable specific heat, let p = p(x; t) be an auxiliary smooth internal heat source and let ψ = ψ(y; t) be the temperature of the boundary. We assume, for the sake of simplicity, that the underlying geometry is fixed. Let u(x; t) = uφ,p,ψ(x; t) be the subsequent temperature distribution which is defined by the relations:

(∂t + D)u(x; t) = p(x; t) for t > 0, P. Gilkey 311

Bu(y; t) = ψ(y; t) for t > 0, y ∈ ∂M, lim u(·; t) = φ(·) in L2 . t↓0 The associated heat content function has a complete asymptotic series as t ↓ 0: Z β(φ, ρ, D, B, p, ψ)(t) : = huφ,p,ψ(x; t), ρ(x; t)idx M ∞ X n/2 ∼ βn(φ, ρ, D, B, p, ψ)t . n=0 Assertions (1)-(4) in the following result are valid for quite general boundary condi- tions. Assertion (5) refers to the particular problem under consideration. This result when combined with the results of Theorems 7.3 and 7.4 permits evaluation of this invariant for n ≤ 4. Assertion (1) reduces to the case ρ is static and Assertion (2) decouples the in- variants as a sum of 3 different invariants. Assertion (3) evaluates the invariant which is independent of {p, ψ}, Assertion (4) evaluates invariant which depends on p, and Assertion (5) evaluates the invariant which depends on ψ. P k Theorem 8.1 (1) Expand the specific heat ρ(x; t) ∼ t ρk(x) in a Taylor series. P k≥0 Then βn(φ, ρ, D, B, p, ψ) = 2k≤n βn−2k(φ, ρk,D, B, p, ψ).

(2) If the specific heat ρ is static, then βn(φ, ρ, D, B, p, ψ) = βn(φ, ρ, D, B, 0, 0) +βn(0, ρ, D, B, p, 0) + βn(0, ρ, D, B, 0, ψ).

(3) If the specific heat ρ is static, then βn(φ, ρ, D, B, 0, 0) = βn(φ, ρ, D, B). R 1 i j/2 P k (4) Let cij := 0 (1 − s) s ds. Expand p(x; t) ∼ k≥0 t pk(x) in a Taylor series. If the specific heat is static, then:

a) β0(0, ρ, D, B, p, 0) = 0. P b) If n > 0, then βn(0, ρ, D, B, p, 0) = 2i+j+2=n cijβj(pi, ρ, D, B). P k (5) Expand the boundary source term ψ(x, t) ∼ k≥0 t ψk(x) in a Taylor series. As- sume the specific heat ρ is static. Then:

a) β0(0, ρ, D, B, 0, ψ) = 0. b) β (0, ρ, D, B, 0, ψ) = √2 R hψ , ρidy. 1 π CD 0 R 1 R c) β (0, ρ, D, B, 0, ψ) = − {h Laaψ , ρi − hψ , ρ i}dy − hψ , ρidy. 2 CD 2 0 0 ;m CR 0 d) β (0, ρ, D, B, 0, ψ) = √2 R { 2 hψ , ρ i + 1 hψ , ρ i + h 1 Eψ, ρi 3 π CD 3 0 ;mm 3 0 :aa 3 2 1 1 1 − 3 Laahψ0, ρ;mi + h( 12 LaaLbb − 6 LabLab − 6 Ramma)ψ0, ρi}dy − √4 R hψ , B˜ρidy + √4 R hψ , ρidy. 3 π CR 0 3 π CD 1 R 1 1 1 e) β (0, ρ, D, B, 0, ψ) = − { hψ , (Dρ˜ );mi − hLaaψ , Dρ˜ i + h( E;m 4 CD 2 0 4 0 8 1 1 1 1 − 16 LabLabLcc + 8 LabLacLbc − 16 RambmLab + 16 RabcbLac 1 1 1 1 + 32 τ ;m + 16 Lab:ab)ψ0, ρi − 4 Labhψ0:a, ρ:bi − 8 hΩamψ0:a, ρi 1 1 1 + 8 hΩamψ0, ρ:ai + 4 Laahψ1, ρi − 2 hψ1, ρ;mi}dy R 1 1 1 1 − {− hψ , Dρ˜ i + h( S + Laa)ψ , B˜ρi + hψ , ρi}dy. CR 2 0 2 4 0 2 1 312 Spectral geometry

9 Time dependent phenomena

We refer to [56] for proofs of the assertions in this section and also for a more complete historical discussion. Let D = {Dt} be a time-dependent family of operators of Laplace type. We expand D in a Taylor series expansion ∞   X r Dtu := Du + t Gr,iju;ij + Fr,iu;i + Eru . r=1

We use the initial operator D := D0 to define a reference metric g0. Choose local frames {ei} for the tangent bundle of M and local frames {ea} for the tangent bundle of the boundary which are orthonormal with respect to the initial metric g0. Use g0 to define the measures dx on M and dy on ∂M. The metric g0 defines the curvature tensor R and the second fundamental form L. We also use D to define a background connection ∇0 that we use to multiply covariantly differentiate tensors of all types and to define the endomorphism E. As in Section 8, we again assume ∂M = CD ∪ CR decomposes as a disjoint union of two closed, possibly empty, disjoint subsets. We consider a 1 parameter family B = {Bt} of boundary operators which we expand formally in a Taylor series ( ) X r Btφ := φ ⊕ φ + Sφ + t (Γr,aφ + Srφ) . ;m ;a CD r>0 CR The reason for including a dependence on time in the boundary condition comes, for ex- ample, by considering the dynamical . Slowly moving boundaries give rise to such boundary conditions. We let u be the solution of the time-dependent heat equation

2 (∂t + Dt)u = 0, Btu = 0, lim u(·; t) = φ(·) in L . t↓0 R There is a smooth kernel function so that u(x; t) = M K(t, x, x,¯ D, B)φ(¯x)dx¯ . The analogue of the heat trace expansion in this setting and of the heat content asymptotic expansion are given, respectively, by Z   ∞ X (n−m)/2 f(x) TrVx K(t, x, x, D, B) dx ∼ an(f, D, B)t , M n=0 Z ∞ X n/2 hK(t, x, x,¯ D, B)φ(x), ρ(¯x)idxdx¯ ∼ βn(φ, ρ, D, B)t . M n=0

By assumption, the operators Gr,ij are scalar. The following theorem describes the additional terms in the heat trace asymptotics which arise from the structures described by Gr,ij, Fr,i, Er, Γr,a, and Sr given above. Theorem 9.1 [Varying geometries]

(1) a0(F, D, B) = a0(F,D, B).

(2) a1(F, D, B) = a1(F,D, B).

−m/2 1 R 3 (3) a2(F, D, B) = a2(F,D, B) + (4π) 6 M Tr{ 2 F G1,ii}dx. P. Gilkey 313

(1−m)/2 1 R (4) a3(F, D, B) = a3(F,D, B) + (4π) Tr{−24F G1,aa}dy 384 CD (1−m)/2 1 R +(4π) Tr{24F G1,aa}dy. 384 CR

−m/2 1 R 45 45 (5) a4(F, D, B) = a4(F,D, B) + (4π) 360 M Tr{F ( 4 G1,iiG1,jj + 2 G1,ijG1,ij

+60G2,ii − 180E1 + 15G1,iiτ − 30G1,ijρij + 90G1,iiE + 60F1,i;i + 15G1,ii;jj −m/2 1 R −30G1,ij;ij)}dx + (4π) Tr{f(30G1,aaLbb − 60G1,mmLbb 360 CD

+30G1,abLab + 30G1,mm;m − 30G1,aa;m − 30F1,m) + F;m(−45G1,aa −m/2 1 R +45G1,mm)}dy + (4π) Tr{F (30G1,aaLbb + 120G1,mmLbb 360 CR −150G1,abLab−60G1,mm;m+60G1,aa;m+150F1,m+180SG1,aa−180SG1,mm

+360S1) + F;m(45G1,aa − 45G1,mm)}dy. Next we study the heat content asymptotics for variable geometries. We have the fol- lowing formulas for Dirichlet and for Robin boundary conditions. Let B := B0. Theorem 9.2 [Dirichlet boundary conditions]

(1) βn(φ, ρ, D, B) = βn(φ, ρ, D0, B) for n = 0, 1, 2. 1 R (2) β (φ, ρ, D, B) = β (φ, ρ, D0, B) + √ hG1,mmφ, ρidy. 3 3 2 π CD

1 R (3) β4(φ, ρ, D, B) = β4(φ, ρ, D0, B) − 2 M hG1,ijφ;ij + F1,iφ;i + E1φ, ρidx R 7 9 5 + { hG1,mm;mφ, ρi − LaahG1,mmφ, ρi − hF1,mφ, ρi CD 16 16 16 5 5 1 + 16 LabhG1,abφ, ρi − 8 hG1,amφ:a, ρi + 2 hG1,mmφ, ρ;mi}dy R 1 1 + {− hG1,mmB0φ, ρi + h(S1 + Γa∇e )φ, ρi}dy. CR 2 2 a

10 Spectral boundary conditions

We adopt the notation used to discuss spectral boundary conditions in Section 6. Let ∞ ∞ ∗ P : C (V1) → C (V2) be an elliptic complex of Dirac type. Let D = P P and let BΘ be the spectral boundary conditions defined by the auxiliary self-adjoint endomorphism Θ of V1. Let ∇ be a compatible connection. Expand P = γi∇ei + ψ. We begin by studying the heat trace asymptotics with spectral boundary conditions. There is an asymptotic series

m−1 −tDB X (k−m)/2 −1/8 2 Θ TrL (fe ) ∼ ak(f, DBΘ , BΘ)t + O(t ) . k=0 Continuing further introduces non-local terms; we refer to Atiyah et al. [6], to Grubb T −1 [71, 72], and to Grubb and Seeley [74, 75] for further details. Define γa := γm γa, ˆ −1 m 1 −1 m+1 −1 ψ := γm ψ, and β(m) := Γ( 2 )Γ( 2 ) Γ( 2 ) . We refer to [48] for the proof of the following result: Theorem 10.1 [Spectral boundary conditions] Let f ∈ C∞(M). Then:

−m/2 R (1) a0(f, D, BΘ) = (4π) M Tr(f id)dx. 314 Spectral geometry

1 −(m−1)/2 R (2) If m ≥ 2, then a1(f, D, BΘ) = 4 [β(m) − 1](4π) ∂M Tr(f id)dy.

−m/2 R 1 (3) If m ≥ 3, then a2(f, D, BΘ) = (4π) M 6 Tr{f(τ id +6E)}dx −m/2 R 1 ˆ ˆ ∗ 1 3 +(4π) ∂M Tr{ 2 [ψ + ψ ]f + 3 [1 − 4 πβ(m)]Laaf id m−1 1 − 2(m−2) [1 − 2 πβ(m)]f;m id}dy.

−(m−1)/2 R 1 β(m) ˆ ˆ ˆ ∗ ˆ ∗ (4) If m ≥ 4, then a3(f, D, BΘ) = (4π) ∂M Tr{ 32 (1− m−2 )f(ψψ +ψ ψ ) 1 7−8m+2m2 ˆ ˆ ∗ 1 m−1 + 16 (5 − 2m + m−2 β(m))fψψ − 48 ( m−2 β(m) − 1)fτ id 1 2m2−6m+5 T ˆ T ˆ T ˆ ∗ T ˆ ∗ + 32(m−1) (2m − 3 − m−2 β(m))f(γa ψγa ψ + γa ψ γa ψ ) 1 3−2m T ˆ T ˆ ∗ 1 4m−10 + 16(m−1) (1 + m−2 β(m))fγa ψγa ψ + 48 (1 − m−2 β(m))fρmm id 1 17+5m 23−2m−4m2 + 48(m+1) ( 4 + m−2 β(m))fLabLab id 1 17+7m2 4m3−11m2+5m−1 + 48(m2−1) (− 8 + m−2 β(m))fLaaLbb id 1 1 T T m−1 + 8(m−2) β(m)f(ΘΘ + m−1 γa Θγa Θ)} + 16(m−3) (2β(m) − 1)f;mm id 1 5m−7 5m−9 + 8(m−3) ( 8 − 3 β(m))Laaf;m id}dy. We now study heat content asymptotics with spectral boundary conditions. To simplify the discussion, we suppose P is formally self-adjoint. We refer to [60, 61] for the proof of: R Theorem 10.2 (1) β0(φ, ρ, D, BΘ) = M hφ, ρidx.

√2 R + + (2) β1(φ, ρ, D, BΘ) = − π ∂M hΠAφ, ΠA# ρidy. R R + + ˜ (3) β2(φ, ρ, D, BΘ) = − M hDφ, ρidx + ∂M {−hγmΠAP φ, ρi − hγmΠAφ, P ρi 1 ˜# ˜ # + + + 2 h(Laa + A + A − γmψP + ψP γm − ψA − ψA )ΠAφ, ΠA# ρi}dy.

11 Operators which are not of Laplace type

We follow Avramidi and Branson [12], Branson et al. [32], Fulling [52], Gusynin [77], and Ørsted and Pierzchalski [101] to discuss the heat trace asymptotics of non-minimal operators. Let M be a compact Riemannian manifold with smooth boundary and let B define either absolute or relative boundary conditions. Let E ∈ C∞(End(ΛpM)) be an auxiliary endomorphism and let A and B be positive constants. Let

p ∞ p DE := Adδ + Bδd − E on C (Λ (M)), −1 X m m c (A, B) := B−m + (B−m − A−m) (−1)k+p . m,p p k k

p (n−m)/2 p Theorem 11.1 (1) If E = 0, then an(1,D , B) = B an(1, ∆M , B) (n−m)/2 (n−m)/2 P k+p p +(B − A ) k

p p a) a0(1,DE, B) = a0(1,D , B). p p b) a1(1,DE, B) = a1(1,D , B). p p −m/2 R c) a2(1,DE, B) = a2(1,D , B) + (4π) cm,p(A, B) M Tr(E)dx. We follow the discussion in [56] to study the heat content asymptotics of the non- minimal operator D := Adδ + Bδd − E on C∞(Λ1(M)). Let φ and ρ be smooth 1 forms; expand φ = φiei and ρ = ρiei where em is the inward geodesic normal. Theorem 11.2 (1) Let B define absolute boundary conditions. Then:

R a) β0(φ, ρ, D, B) = M (φ, ρ)dx. √ √2 R b) β1(φ, ρ, D, B) = − π A ∂M φmρmdy. R c) β2(φ, ρ, D, B) = − M {A(δφ, δρ) + B(dφ, dρ) − E(φ, ρ)}dx R + ∂M A{−φmρa:a − φa:aρm − φm;mρm − φmρm;m 3 + 2 Laaφmρm}dy.

(2) Let B define relative boundary conditions. Then

R a) β0(φ, ρ, D, B) = M (φ, ρ)dx. √ √2 R b) β1(φ, ρ, D, B) = − π B ∂M φaρady. R c) β2(φ, ρ, D, B) = − M {A(δφ, δρ) + B(dφ, dρ) − E(φ, ρ)}dx R + ∂M B{−φa:aρm − φmρa:a − φa;mρa − φaρa;m 1 +Labφbρa + 2 Laaφbρb}dy. We now turn our attention to fourth order operators. Let M be a closed Riemannian manifold. Let ∇ be a connection on a vector bundle V over a closed Riemannian manifold M. Set

Γ( m−n )−1Γ( m−n ) := lim {Γ( m−s )−1Γ( m−s )} . 2 4 s→n 2 4

Theorem 11.3 Let P u = u;iijj +p2,iju;ij +p1,iu;i +p0 on a closed Riemannian manifold where p2,ij = p2,ji and where {p2,ij, p1,i, p0} are endomorphism valued. . Then:

1 −m/2 m −1 m R (1) a0(1,P ) = 2 (4π) Γ( 2 ) Γ( 4 ) M Tr(id)dx.

1 −m/2 m−2 −1 m−2 1 R 3 (2) a2(1,P ) = 2 (4π) Γ( 2 ) Γ( 4 ) 6 M Tr{τ id + m p2,ii}dx.

1 −m/2 m −1 m 1 R 90 45 (3) a4(1,P ) = 2 (4π) Γ( 2 ) Γ( 4 ) 360 M Tr{ m+2 p2,ijp2,ij + m+2 p2,iip2,jj 2 2 2 +(m − 2)(5τ id −2|ρ| id +2|R| id +30ΩijΩij) + 30τp2,ii − 60ρijp2,ij

−360p0}dx. 316 Spectral geometry

12 The spectral geometry of Riemannian submersions

We refer to [64] for further details concerning the material of this section; additionally see Bergery and Bourguignon[13], Besson and Bordoni [29], Goldberg and Ishihara [65] and Watson [126]. Let π : Z → Y be a smooth map where Z and Y are connected closed Riemannian manifolds. We say that π is a submersion if π is surjective and if π∗ : TzZ → TπzY is surjective for every z ∈ Z. −1 Submersions are fiber bundles. Let F := π (y0) be the fiber over some point y0 ∈ Y . If O is a contractable open subset of Y , then π−1(O) is homeomorphic to O × F and under this homeomorphism, π is projection on the first factor. The vertical distribution V := ker(π∗) is a smooth subbundle of TZ. The horizontal distribution is defined by ⊥ H := V . One says that π is a Riemannian submersion if π∗ : Hz → TπzY is an for every point z in Z. The fundamental tensors may be introduced as follows. Let π : Z → Y be a Rie- a mannian submersion. We use indices a, b, c to index local orthonormal frames {fa}, {f }, a ∗ ∗ {Fa}, and {F } for H, H , TY , and T , respectively. We use indices i, j, k to index local i ∗ orthonormal frames {ei} and {e } for V and V , respectively. There are two fundamental tensors which arise naturally in this setting. The unnormalized mean curvature vector θ and the integrability tensor ω are defined by:

a Z a ∞ θ := −gZ ([ei, fa], ei)f = Γiiaf ∈ C (H), 1 1 Z Z ω := ωabi = 2 gZ (ei, [fa, fb]) = 2 ( Γabi − Γbai) . Lemma 12.1 Let π : Z → Y be a Riemannian submersion.

(1) The following assertions are equivalent: a) The fibers of π are minimal. b) π is a harmonic map. c) θ = 0.

(2) The following assertions are equivalent: a) The distribution H is integrable. b) ω = 0.

(3) Let Θ := π∗θ be the integration of θ along the fiber, and let V (y) be the volume of the fiber. Then Θ = −dY ln(V ). Thus in particular, if θ = 0, then the fibers have constant volume.

∗ ∗ By naturality π dY = dZ π . The intertwining formulas for the coderivatives and for i a b the Laplacians are more complicated. Let E := ωabi extZ (e ) intZ (f ) intZ (f ) and let Ξ := intZ (θ) + E. ∗ ∗ ∗ Lemma 12.2 Let π : Z → Y be a Riemannian submersion. Then δZ π − π δY = Ξπ p ∗ ∗ p ∗ and ∆Z π − π ∆Y = {ΞdZ + dZ Ξ}π . One is interested in relating the spectrum on the base to the spectrum on the total space. The situation is particularly simple if p = 0: Theorem 12.3 Let π : Z → Y be a Riemannian submersion.

0 ∗ 0 (1) If Φ ∈ E(λ, ∆Y ) is nontrivial and if π Φ ∈ E(µ, ∆Z ), then λ = µ. (2) The following conditions are equivalent: 0 ∗ ∗ 0 ∗ 0 0 a) ∆Z π = π ∆Y . b) For all λ, π E(λ, ∆Y ) ⊂ E(λ, ∆Z ). c) θ = 0. P. Gilkey 317

Muto [97, 98, 99] has given examples of Riemannian principal S1 bundles where eigen- values can change. The study of homogeneous space also provides examples. This leads to the result: Theorem 12.4 (1) Let Y be a homogeneous manifold with H2(Y ; R) 6= 0. There exists a complex line bundle L over Y with associated circle fibration πS : S(L) → Y , and there exists a unitary connection L∇ on L so that the curvature F of L∇ is ∗ 2 harmonic and has constant norm  6= 0 and so that πSF ∈ E(, ∆S). (2) Let 0 ≤ λ ≤ µ and let p ≥ 2 be given. There exists a principal circle bundle p π : P → Y over some manifold Y , and there exists 0 6= Φ ∈ E(λ, ∆Y ) so that ∗ p π Φ ∈ E(µ, ∆Z ). The case p = 1 is unsettled; it is not known if eigenvalues can change if p = 1. On the other hand, one can show that eigenvalue can never decrease. Theorem 12.5 Let π : Z → Y be a Riemannian submersion of closed smooth manifolds. p ∗ p Let 1 ≤ p ≤ dim(Y ). If 0 6= Φ ∈ E(λ, ∆Y ) and if π Φ ∈ E(µ, ∆Z ), then λ ≤ µ. The following conditions are equivalent: p ∗ ∗ p a) We have ∆Z π = π ∆Y . ∗ p p b) For all λ, we have π E(λ, ∆Y ) ⊂ E(λ, ∆Z ). ∗ p p c) For all λ, there exists µ = µ(λ) so π E(λ, ∆Y ) ⊂ E(µ, ∆Z ). d) We have θ = 0 and ω = 0. Results of Park [103] show this if Neumann boundary conditions are imposed on a manifolds with boundary, then eigenvalues can decrease. 2 p p There are results related to finite Fourier series. We have L (Λ M) = ⊕λE(λ, ∆M ). P p Thus if φ is a smooth p-form, we may decompose φ = λ φλ for φλ ∈ E(λ, ∆M ). Let ν(φ) be the number of λ so that φλ 6= 0. We say that φ has finite Fourier series if ν(φ) < ∞. For example, if M = S1, then φ has finite Fourier series if and only if φ is a trignometric polynomial. The first assertion in the following result is an immediate consequence of the Peter-Weyl theorem; the second result follows from [49]. Theorem 12.6 (1) Let π : G → G/H be a homogeneous space where G/H is equipped with a G invariant metric and where G is equipped with a left invariant metric. If φ is a smooth p-form on G/H with finite Fourier series, then π∗φ has finite Fourier series on G.

(2) Let 1 ≤ p, 0 < λ, and 2 ≤ µ0 be given. There exists π : G → G/H and there exists p ∗ φ ∈ E(λ, ∆G/H ) so that µG(π φ) = ν0. In general, there is no relation between the heat trace asymptotics on the base, fiber, and total space of a Riemannian submersion. McKean and Singer [90] have determined the heat equation asymptotics for the sphere Sn. Let

m/2 m/2 (4πt) −t∆0 X (4πt) 0 n/2 Z(M, t) := Tr 2 e M ∼ a (∆ )t Vol(M) L Vol(M) n M n≥0 be the normalized heat trace; with this normalization, Z(M, t) is regular at the origin and has leading coefficient 1. Their results (see page 63 of McKean and Singer [90]) show that

Z(S1, t) = 1 + O(tk) for any k 318 Spectral geometry

t/4 1 −x/t 2 Z(S2, t) = √e R e √ dx = 1 + t + t + ... πt 0 sin x 3 15 1 2 2 1 t t2 Z(S × S , t) = Z(S , t)Z(S , t) = 1 + 3 + 15 + ... 3 t 1 2 Z(S , t) = e = 1 + t + 2 t + .... .

The two fibrations π : S1 × S2 → S2 and π : S3 → S2 have base S2 and minimal fibers S1. However, the heat trace asymptotics are entirely different. On the other hand, the following result shows that the heat content asymptotics on Z are determined by the heat content asymptotics of the base and by the volume of the fiber if θ = 0; Lemma 12.1 shows the volume V of the fiber is independent of the point in question in this setting. Theorem 12.7 Let π : Z → Y be a Riemannian submersion of compact manifolds with ∗ ∗ smooth boundary. Let ρZ := π ρY and let φZ := π φY . If θ = 0 and if B = BD or 0 0 B = BN , then βn(ρZ , φZ , ∆Z , B) = βn(ρY , φY , ∆Y , B) · V .

Acknowledgments

Research of P. Gilkey was partially supported by the Max Planck Institute in the Mathemat- ical Sciences (Leipzig, Germany) and by Project MTM2006-01432 (Spain). It is a pleasure to acknowledge helpful conversations with E. Puffini and L. Loro concerning these matters.

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PETER B.GILKEY Mathematics Department, University of Oregon, Eugene Or 97403 USA http://www.uoregon.edu/∼gilkey E-mail: [email protected].