ASF

Diffusion on Curved Spaces

March 12, 2026|
A
A

The animation above shows a sealed, rigid container whose walls curve inward and outward; inside, a swarm of particles begins concentrated near a single point and diffuses outward. The container is a closed 3-manifold (a deformed sphere), and its curvature is not decorative. It determines how the swarm spreads. Near the poles of the container, where the wall curves sharply, the particles are reflected at steeper angles than on the flatter equatorial band. The gold-to-blue colour encodes the heat kernel value Kt(x,x0)=exp(xx02/4t)K_t(\mathbf{x}, \mathbf{x}_0) = \exp(-|\mathbf{x}-\mathbf{x}_0|^2/4t) evaluated at each particle's position: gold is high concentration, deep blue is low.

That formula is the heat kernel in flat space R3\mathbb{R}^3. On a curved manifold it is only an approximation; the true kernel acquires corrections at every order in tt whose coefficients are curvature invariants. The first such correction, which appears at order tt, is the scalar curvature R(x)R(\mathbf{x}).

This post derives that result from first principles. We begin with the classical heat equation on Rn\mathbb{R}^n and its Gaussian fundamental solution (§1). We then build the Riemannian machinery (metric tensor, covariant gradient, divergence, and Laplace–Beltrami operator) from the ground up (§2). The heat equation on a Riemannian manifold (M,g)(M,g) has its own fundamental solution, derived through the parametrix construction (§3). We close with the spectral representation of the heat kernel and Weyl's law (§4).

Sign convention. The Laplace–Beltrami operator is defined as ΔM=divggradg\Delta_M = \operatorname{div}_g \circ \operatorname{grad}_g, which is negative semi-definite on functions. The heat equation is tu=ΔMu\partial_t u = \Delta_M u. The competing probabilistic convention replaces this by tu=12ΔMu\partial_t u = \tfrac{1}{2}\Delta_M u, matching the generator of Brownian motion; the two conventions differ only by the substitution t2tt \mapsto 2t throughout and produce kernels related by Ktprob(x,y)=Kt/2(x,y)K_t^{\mathrm{prob}}(\mathbf{x},\mathbf{y}) = K_{t/2}(\mathbf{x},\mathbf{y}).

1. The Heat Equation on Rn\mathbb{R}^n

1.1. Derivation from conservation

Let u ⁣:Rn×[0,)Ru \colon \mathbb{R}^n \times [0,\infty) \to \mathbb{R} be the concentration of a diffusing substance. Fick's first law [1] states that diffusive flux opposes the concentration gradient:

J(x,t)=u(x,t).\mathbf{J}(\mathbf{x},t) = -\nabla u(\mathbf{x},t).

Conservation of mass over any smooth bounded region ΩRn\Omega \subset \mathbb{R}^n requires

ddtΩudx=ΩJn^dσ,\frac{\mathrm{d}}{\mathrm{d}t} \int_\Omega u \, \mathrm{d}\mathbf{x} = -\oint_{\partial\Omega} \mathbf{J} \cdot \hat{\mathbf{n}} \, \mathrm{d}\sigma,

where n^\hat{\mathbf{n}} is the outward unit normal to Ω\partial\Omega. Applying the divergence theorem to the right side of [eq:conservation] and substituting [eq:fick]:

ddtΩudx=ΩΔudx.\frac{\mathrm{d}}{\mathrm{d}t} \int_\Omega u \, \mathrm{d}\mathbf{x} = \int_\Omega \Delta u \, \mathrm{d}\mathbf{x}.

Since Ω\Omega is arbitrary and all integrands are continuous, we conclude:

tu=Δu,(x,t)Rn×(0,).\partial_t u = \Delta u, \qquad (\mathbf{x},t) \in \mathbb{R}^n \times (0,\infty).

1.2. Solution via the Fourier transform

For fL1(Rn)f \in L^1(\mathbb{R}^n) the Fourier transform and its inverse are

f^(ξ)=Rnf(x)e2πixξdx,f(x)=Rnf^(ξ)e2πixξdξ.\hat{f}(\boldsymbol{\xi}) = \int_{\mathbb{R}^n} f(\mathbf{x})\, e^{-2\pi i \mathbf{x} \cdot \boldsymbol{\xi}}\, \mathrm{d}\mathbf{x}, \qquad f(\mathbf{x}) = \int_{\mathbb{R}^n} \hat{f}(\boldsymbol{\xi})\, e^{2\pi i \mathbf{x} \cdot \boldsymbol{\xi}}\, \mathrm{d}\boldsymbol{\xi}.

Differentiation in x\mathbf{x} becomes multiplication in ξ\boldsymbol{\xi}:

xjf^(ξ)=2πiξjf^(ξ),\widehat{\partial_{x_j} f}(\boldsymbol{\xi}) = 2\pi i \xi_j \hat{f}(\boldsymbol{\xi}),

so applying [eq:fourier-deriv] twice in each coordinate and summing:

Δf^(ξ)=4π2ξ2f^(ξ).\widehat{\Delta f}(\boldsymbol{\xi}) = -4\pi^2 |\boldsymbol{\xi}|^2 \hat{f}(\boldsymbol{\xi}).

Taking the Fourier transform of [eq:heat-flat] in x\mathbf{x} and applying [eq:fourier-laplacian]:

tu^(ξ,t)=4π2ξ2u^(ξ,t).\partial_t \hat{u}(\boldsymbol{\xi}, t) = -4\pi^2|\boldsymbol{\xi}|^2\, \hat{u}(\boldsymbol{\xi}, t).

This is a first-order linear ODE in tt for each fixed ξ\boldsymbol{\xi}, with solution

u^(ξ,t)=u^0(ξ)e4π2ξ2t.\hat{u}(\boldsymbol{\xi}, t) = \hat{u}_0(\boldsymbol{\xi})\, e^{-4\pi^2 |\boldsymbol{\xi}|^2 t}.

By the convolution theorem, this product in frequency space corresponds to convolution in physical space:

u(x,t)=(F1[e4π2ξ2t])u0(x).u(\mathbf{x}, t) = \bigl(\mathcal{F}^{-1}[e^{-4\pi^2|\boldsymbol{\xi}|^2 t}]\bigr) * u_0(\mathbf{x}).

1.3. The Gaussian heat kernel

The inverse Fourier transform of e4π2ξ2te^{-4\pi^2|\boldsymbol{\xi}|^2 t} factors over coordinates, reducing to a one-dimensional integral. Completing the square:

e4π2ξ2te2πixξdξ=ex2/4te4π2tη2dη=ex2/4t4πt,\int_{-\infty}^\infty e^{-4\pi^2 \xi^2 t}\, e^{2\pi i x\xi}\, \mathrm{d}\xi = e^{-x^2/4t} \int_{-\infty}^\infty e^{-4\pi^2 t \eta^2}\, \mathrm{d}\eta = \frac{e^{-x^2/4t}}{\sqrt{4\pi t}},

where η=ξix/(4πt)\eta = \xi - ix/(4\pi t) and the contour shift is justified by Cauchy's theorem. Multiplying over all nn coordinates gives

Kt(x):=F1 ⁣[e4π2ξ2t](x)=1(4πt)n/2ex2/4t.K_t(\mathbf{x}) := \mathcal{F}^{-1}\!\left[e^{-4\pi^2|\boldsymbol{\xi}|^2 t}\right](\mathbf{x}) = \frac{1}{(4\pi t)^{n/2}}\, e^{-|\mathbf{x}|^2/4t}.

By [eq:conv-soln], the solution to [eq:heat-flat] is u(x,t)=(Ktu0)(x)u(\mathbf{x},t) = (K_t * u_0)(\mathbf{x}), or written symmetrically:

u(x,t)=RnKt(x,y)u0(y)dy,Kt(x,y)=exy2/4t(4πt)n/2.u(\mathbf{x},t) = \int_{\mathbb{R}^n} K_t(\mathbf{x},\mathbf{y})\, u_0(\mathbf{y})\, \mathrm{d}\mathbf{y}, \qquad K_t(\mathbf{x},\mathbf{y}) = \frac{e^{-|\mathbf{x}-\mathbf{y}|^2/4t}}{(4\pi t)^{n/2}}.

The visualization below shows Kt(x)=(4πt)1/2ex2/4tK_t(x) = (4\pi t)^{-1/2} e^{-x^2/4t} in one dimension for several values of tt: the bell flattens and widens as t\sqrt{t}.

Proposition (Properties of the flat heat kernel).

The kernel [eq:flat-kernel] satisfies, for all t,s>0t, s > 0 and x,yRn\mathbf{x}, \mathbf{y} \in \mathbb{R}^n:

  1. Positivity: Kt(x,y)>0K_t(\mathbf{x},\mathbf{y}) > 0.
  2. Mass conservation: RnKt(x,y)dy=1\int_{\mathbb{R}^n} K_t(\mathbf{x},\mathbf{y})\, \mathrm{d}\mathbf{y} = 1.
  3. Symmetry: Kt(x,y)=Kt(y,x)K_t(\mathbf{x},\mathbf{y}) = K_t(\mathbf{y},\mathbf{x}).
  4. Semigroup: RnKs(x,z)Kt(z,y)dz=Ks+t(x,y)\int_{\mathbb{R}^n} K_s(\mathbf{x},\mathbf{z})\, K_t(\mathbf{z},\mathbf{y})\, \mathrm{d}\mathbf{z} = K_{s+t}(\mathbf{x},\mathbf{y}).
  5. Approximate identity: limt0+(Ktf)(x)=f(x)\lim_{t \to 0^+}(K_t * f)(\mathbf{x}) = f(\mathbf{x}) for all fCb(Rn)f \in C_b(\mathbb{R}^n), uniformly on compact sets.

Proof. (1) is immediate from the definition.

Proof of (2). Substitute z=(yx)/4t\mathbf{z} = (\mathbf{y}-\mathbf{x})/\sqrt{4t}, so dy=(4t)n/2dz\mathrm{d}\mathbf{y} = (4t)^{n/2}\,\mathrm{d}\mathbf{z}. Then

RnKt(x,y)dy=(4t)n/2(4πt)n/2Rnez2dz=1πn/2πn/2=1,\int_{\mathbb{R}^n} K_t(\mathbf{x},\mathbf{y})\,\mathrm{d}\mathbf{y} = \frac{(4t)^{n/2}}{(4\pi t)^{n/2}} \int_{\mathbb{R}^n} e^{-|\mathbf{z}|^2}\,\mathrm{d}\mathbf{z} = \frac{1}{\pi^{n/2}}\cdot\pi^{n/2} = 1,

where the last step uses the standard Gaussian integral Rnez2dz=πn/2\int_{\mathbb{R}^n} e^{-|\mathbf{z}|^2}\,\mathrm{d}\mathbf{z} = \pi^{n/2}, which factors as a product of nn one-dimensional integrals ezi2dzi=π\int_{-\infty}^\infty e^{-z_i^2}\,\mathrm{d}z_i = \sqrt{\pi} [2].

(3) is immediate from xy2=yx2|\mathbf{x}-\mathbf{y}|^2 = |\mathbf{y}-\mathbf{x}|^2.

Proof of (4). Write I=RnKs(x,z)Kt(z,y)dzI = \int_{\mathbb{R}^n} K_s(\mathbf{x},\mathbf{z})\,K_t(\mathbf{z},\mathbf{y})\,\mathrm{d}\mathbf{z}. The prefactors contribute (4πs)n/2(4πt)n/2(4\pi s)^{-n/2}(4\pi t)^{-n/2}. The combined exponent is

xz24szy24t.-\frac{|\mathbf{x}-\mathbf{z}|^2}{4s} - \frac{|\mathbf{z}-\mathbf{y}|^2}{4t}.

Expanding and collecting powers of z\mathbf{z}:

xz24szy24t=(14s+14t)z2+x2sz+y2tzx24sy24t.-\frac{|\mathbf{x}-\mathbf{z}|^2}{4s} - \frac{|\mathbf{z}-\mathbf{y}|^2}{4t} = -\left(\frac{1}{4s}+\frac{1}{4t}\right)|\mathbf{z}|^2 + \frac{\mathbf{x}}{2s}\cdot\mathbf{z} + \frac{\mathbf{y}}{2t}\cdot\mathbf{z} - \frac{|\mathbf{x}|^2}{4s} - \frac{|\mathbf{y}|^2}{4t}.

The coefficient of z2|\mathbf{z}|^2 is (s+t)/(4st)-(s+t)/(4st), and the optimal point in z\mathbf{z} is

z=tx+sys+t.\mathbf{z}^* = \frac{t\mathbf{x}+s\mathbf{y}}{s+t}.

Completing the square, the combined exponent equals

s+t4stztx+sys+t2xy24(s+t),-\frac{s+t}{4st}\left|\mathbf{z} - \frac{t\mathbf{x}+s\mathbf{y}}{s+t}\right|^2 - \frac{|\mathbf{x}-\mathbf{y}|^2}{4(s+t)},

where the residual xy2/4(s+t)-|\mathbf{x}-\mathbf{y}|^2/4(s+t) is independent of z\mathbf{z} (verified by expanding both sides and cancelling). The Gaussian integral over z\mathbf{z} now factors:

Rnexp ⁣(s+t4stzz2)dz=(4πsts+t)n/2.\int_{\mathbb{R}^n} \exp\!\left(-\frac{s+t}{4st}\left|\mathbf{z}-\mathbf{z}^*\right|^2\right)\mathrm{d}\mathbf{z} = \left(\frac{4\pi st}{s+t}\right)^{n/2}.

Combining the prefactors and residual:

I=1(4πs)n/2(4πt)n/2(4πsts+t)n/2exy2/4(s+t)=exy2/4(s+t)(4π(s+t))n/2=Ks+t(x,y).I = \frac{1}{(4\pi s)^{n/2}(4\pi t)^{n/2}}\cdot\left(\frac{4\pi st}{s+t}\right)^{n/2}\cdot e^{-|\mathbf{x}-\mathbf{y}|^2/4(s+t)} = \frac{e^{-|\mathbf{x}-\mathbf{y}|^2/4(s+t)}}{(4\pi(s+t))^{n/2}} = K_{s+t}(\mathbf{x},\mathbf{y}).

(5) follows from (2) and the standard theory of approximate identities [2, Ch. 5].

The semigroup property has a direct visual interpretation. Hold the total time T=s+tT = s + t fixed and vary the split sTss \mapsto T - s. The blue kernel KsK_s and the gold kernel Kt=KTsK_t = K_{T-s} change shape continuously, yet their convolution—the muted silver curve KTK_T—is constant throughout.

2. The Riemannian Setup

2.1. Metric tensor and volume form

Definition (Riemannian metric).

A Riemannian metric on a smooth nn-manifold MM is a smooth, symmetric, positive-definite covariant 2-tensor field gg. In local coordinates (x1,,xn)(x^1,\ldots,x^n) it reads

g=gijdxidxj,gij=g ⁣(xi,xj),g = g_{ij}\, \mathrm{d}x^i \otimes \mathrm{d}x^j, \qquad g_{ij} = g\!\left(\tfrac{\partial}{\partial x^i}, \tfrac{\partial}{\partial x^j}\right),

with Einstein summation throughout. The matrix [gij][g_{ij}] is symmetric positive definite at every point [3, Ch. 2].

Write g=det[gij]g = \det[g_{ij}] for the determinant of the metric matrix. The Riemannian volume form, the natural measure on (M,g)(M,g), is

dVg=g  dx1dxn.\mathrm{d}V_g = \sqrt{g}\; \mathrm{d}x^1 \wedge \cdots \wedge \mathrm{d}x^n.

This is independent of the chart: under a coordinate change the Jacobian determinant from the transformation of dx1dxn\mathrm{d}x^1 \wedge \cdots \wedge \mathrm{d}x^n exactly cancels the factor from g\sqrt{g}. The L2L^2 inner product on functions is

f,hL2(M,g)=Mfh  dVg.\langle f, h \rangle_{L^2(M,g)} = \int_M f\, h\; \mathrm{d}V_g.

2.2. Gradient and divergence

Definition (Riemannian gradient).

The gradient of fC(M)f \in C^\infty(M) is the unique vector field gradgf\operatorname{grad}_g f characterised by

g(gradgf,X)=df(X)=X(f)for all XX(M).g(\operatorname{grad}_g f,\, \mathbf{X}) = \mathrm{d}f(\mathbf{X}) = \mathbf{X}(f) \qquad \text{for all } \mathbf{X} \in \mathfrak{X}(M).

In local coordinates: (gradgf)i=gijjf(\operatorname{grad}_g f)^i = g^{ij}\, \partial_j f, where [gij]=[gij]1[g^{ij}] = [g_{ij}]^{-1}.

Proof of the coordinate formula. We need components XiX^i satisfying gijXiVj=(jf)Vjg_{ij} X^i V^j = (\partial_j f) V^j for all vectors V\mathbf{V}. Setting V=k\mathbf{V} = \partial_k gives gikXi=kfg_{ik} X^i = \partial_k f, whence Xi=gijjfX^i = g^{ij} \partial_j f.

Definition (Riemannian divergence).

The divergence of XX(M)\mathbf{X} \in \mathfrak{X}(M) is the smooth function divgX\operatorname{div}_g \mathbf{X} characterised by

LX(dVg)=(divgX)dVg,\mathcal{L}_{\mathbf{X}}(\mathrm{d}V_g) = (\operatorname{div}_g \mathbf{X})\, \mathrm{d}V_g,

where LX\mathcal{L}_{\mathbf{X}} is the Lie derivative. In local coordinates:

divgX=1gi ⁣(gXi).\operatorname{div}_g \mathbf{X} = \frac{1}{\sqrt{g}}\, \partial_i\!\left(\sqrt{g}\, X^i\right).

Proof of the coordinate formula. By Cartan's formula LXω=ιXdω+d(ιXω)\mathcal{L}_{\mathbf{X}} \omega = \iota_{\mathbf{X}} \mathrm{d}\omega + \mathrm{d}(\iota_{\mathbf{X}} \omega) applied to the closed top-degree form dVg\mathrm{d}V_g (for which d(dVg)=0\mathrm{d}(\mathrm{d}V_g) = 0), we get LX(dVg)=d(ιXdVg)\mathcal{L}_{\mathbf{X}}(\mathrm{d}V_g) = \mathrm{d}(\iota_{\mathbf{X}} \mathrm{d}V_g). In coordinates, expanding ιX(dVg)\iota_{\mathbf{X}}(\mathrm{d}V_g) and taking the exterior derivative yields d(ιXdVg)=1gi(gXi)dVg\mathrm{d}(\iota_{\mathbf{X}} \mathrm{d}V_g) = \tfrac{1}{\sqrt{g}}\partial_i(\sqrt{g}\, X^i)\, \mathrm{d}V_g. Comparing with [eq:div-def-eq] gives [eq:div-coords] [4, Ch. 16].

2.3. The Laplace–Beltrami operator

Definition (Laplace–Beltrami operator).

The Laplace–Beltrami operator on (M,g)(M,g) is

ΔMf=divg(gradgf).\Delta_M f = \operatorname{div}_g(\operatorname{grad}_g f).

Substituting [eq:grad-def-eq] into [eq:div-coords] gives the coordinate formula:

ΔMf=1gi ⁣(ggijjf).\Delta_M f = \frac{1}{\sqrt{g}}\, \partial_i\!\left(\sqrt{g}\, g^{ij}\, \partial_j f\right).

On Rn\mathbb{R}^n with the Euclidean metric, gij=δijg_{ij} = \delta_{ij}, g=1g = 1, and [eq:lbo-coords] reduces to the standard Laplacian Δf=ii2f\Delta f = \sum_i \partial_i^2 f.

Proposition (Variational characterisation).

ΔM\Delta_M is the negative L2(M,g)L^2(M,g)-gradient of the Dirichlet energy

E[f]=12Mgij(if)(jf)g  dnx.E[f] = \frac{1}{2}\int_M g^{ij}(\partial_i f)(\partial_j f)\, \sqrt{g}\; \mathrm{d}^n x.

Explicitly, for any φCc(M)\varphi \in C_c^\infty(M):

ddεε=0E[f+εφ]=M(ΔMf)φ  dVg.\left.\frac{\mathrm{d}}{\mathrm{d}\varepsilon}\right|_{\varepsilon=0} E[f + \varepsilon\varphi] = -\int_M (\Delta_M f)\, \varphi\; \mathrm{d}V_g.

Proof. Differentiating under the integral and using the symmetry of gijg^{ij}:

ddεε=0E[f+εφ]=122Mgij(if)(jφ)g  dnx=Mg(gradgf,gradgφ)dVg.\left.\frac{\mathrm{d}}{\mathrm{d}\varepsilon}\right|_{\varepsilon=0} E[f+\varepsilon\varphi] = \frac{1}{2}\cdot 2\int_M g^{ij}(\partial_i f)(\partial_j\varphi)\,\sqrt{g}\;\mathrm{d}^n x = \int_M g(\operatorname{grad}_g f,\, \operatorname{grad}_g\varphi)\,\mathrm{d}V_g.

It remains to show that the last integral equals M(ΔMf)φdVg-\int_M (\Delta_M f)\varphi\,\mathrm{d}V_g. Apply the Leibniz rule for the Riemannian divergence to the vector field X=φgradgf\mathbf{X} = \varphi\,\operatorname{grad}_g f:

divg(φgradgf)=g(gradgφ,gradgf)+φdivg(gradgf)=g(gradgφ,gradgf)+φΔMf.\operatorname{div}_g(\varphi\,\operatorname{grad}_g f) = g(\operatorname{grad}_g\varphi,\,\operatorname{grad}_g f) + \varphi\,\operatorname{div}_g(\operatorname{grad}_g f) = g(\operatorname{grad}_g\varphi,\,\operatorname{grad}_g f) + \varphi\,\Delta_M f.

Integrating over MM and applying the Riemannian divergence theorem (boundary term vanishes because φCc(M)\varphi \in C_c^\infty(M)):

0=Mdivg(φgradgf)dVg=Mg(gradgφ,gradgf)dVg+MφΔMf  dVg.0 = \int_M \operatorname{div}_g(\varphi\,\operatorname{grad}_g f)\,\mathrm{d}V_g = \int_M g(\operatorname{grad}_g\varphi,\,\operatorname{grad}_g f)\,\mathrm{d}V_g + \int_M \varphi\,\Delta_M f\;\mathrm{d}V_g.

Rearranging yields Mg(gradgf,gradgφ)dVg=M(ΔMf)φdVg\int_M g(\operatorname{grad}_g f,\operatorname{grad}_g\varphi)\,\mathrm{d}V_g = -\int_M (\Delta_M f)\varphi\,\mathrm{d}V_g, which is exactly [eq:first-variation] [3, Ch. 2].

2.4. Self-adjointness: Green's identity

Proposition (Green's identity).

For f,hC(M)f, h \in C^\infty(M) on a compact Riemannian manifold without boundary:

MfΔMh  dVg=MhΔMf  dVg=Mg(gradgf,gradgh)  dVg.\int_M f\, \Delta_M h\; \mathrm{d}V_g = \int_M h\, \Delta_M f\; \mathrm{d}V_g = -\int_M g(\operatorname{grad}_g f,\, \operatorname{grad}_g h)\; \mathrm{d}V_g.

Proof. Apply the Leibniz rule divg(fX)=g(gradgf,X)+fdivgX\operatorname{div}_g(f\mathbf{X}) = g(\operatorname{grad}_g f,\mathbf{X}) + f\operatorname{div}_g\mathbf{X} to X=gradgh\mathbf{X} = \operatorname{grad}_g h:

divg(fgradgh)=g(gradgf,gradgh)+fΔMh.\operatorname{div}_g(f\,\operatorname{grad}_g h) = g(\operatorname{grad}_g f,\operatorname{grad}_g h) + f\,\Delta_M h.

Integrating over MM and applying the divergence theorem (no boundary since MM is closed):

0=Mdivg(fgradgh)dVg=Mg(gradgf,gradgh)dVg+MfΔMh  dVg.0 = \int_M \operatorname{div}_g(f\,\operatorname{grad}_g h)\,\mathrm{d}V_g = \int_M g(\operatorname{grad}_g f,\operatorname{grad}_g h)\,\mathrm{d}V_g + \int_M f\,\Delta_M h\;\mathrm{d}V_g.

Rearranging:

MfΔMh  dVg=Mg(gradgf,gradgh)dVg.\int_M f\,\Delta_M h\;\mathrm{d}V_g = -\int_M g(\operatorname{grad}_g f,\operatorname{grad}_g h)\,\mathrm{d}V_g.

Applying the same argument with ff and hh exchanged (the gradient inner product is symmetric):

MhΔMf  dVg=Mg(gradgh,gradgf)dVg=Mg(gradgf,gradgh)dVg.\int_M h\,\Delta_M f\;\mathrm{d}V_g = -\int_M g(\operatorname{grad}_g h,\operatorname{grad}_g f)\,\mathrm{d}V_g = -\int_M g(\operatorname{grad}_g f,\operatorname{grad}_g h)\,\mathrm{d}V_g.

The two left-hand sides are therefore equal, giving all three expressions in [eq:green] [5, Ch. 1].

Taking f=hf = h confirms ΔM\Delta_M is negative semi-definite: ΔMf,f=Mgradgfg2dVg0\langle \Delta_M f, f\rangle = -\int_M |\operatorname{grad}_g f|_g^2 \mathrm{d}V_g \leq 0.

2.5. Examples

The round 2-sphere. In polar coordinates (θ,ϕ)(\theta, \phi) on S2S^2:

g=dθ2+sin2 ⁣θ  dϕ2,g=sinθ,ΔS2f=1sinθθ ⁣(sinθfθ)+1sin2 ⁣θ2fϕ2.g = \mathrm{d}\theta^2 + \sin^2\!\theta\; \mathrm{d}\phi^2, \quad \sqrt{g} = \sin\theta, \quad \Delta_{S^2} f = \frac{1}{\sin\theta}\frac{\partial}{\partial\theta}\!\left(\sin\theta\,\frac{\partial f}{\partial\theta}\right) + \frac{1}{\sin^2\!\theta}\frac{\partial^2 f}{\partial\phi^2}.

The eigenfunctions of ΔS2-\Delta_{S^2} are the spherical harmonics YmY_\ell^m with eigenvalues λ=(+1)\lambda_\ell = \ell(\ell+1), multiplicity 2+12\ell+1 [5, App. B].

The flat torus. On Tn=Rn/ZnT^n = \mathbb{R}^n/\mathbb{Z}^n with gij=δijg_{ij} = \delta_{ij}, the eigenfunctions are the Fourier modes e2πikxe^{2\pi i \mathbf{k} \cdot \mathbf{x}} for kZn\mathbf{k} \in \mathbb{Z}^n, eigenvalues 4π2k2-4\pi^2|\mathbf{k}|^2, and the heat kernel is

KtTn(x,y)=kZne4π2k2te2πik(xy),K_t^{T^n}(\mathbf{x},\mathbf{y}) = \sum_{\mathbf{k} \in \mathbb{Z}^n} e^{-4\pi^2|\mathbf{k}|^2 t}\, e^{2\pi i \mathbf{k} \cdot (\mathbf{x}-\mathbf{y})},

which converges to the flat Gaussian [eq:flat-kernel] as t0+t \to 0^+ (lattice images are exponentially suppressed).

3. Diffusion on a Curved Manifold

3.1. The heat equation on (M,g)(M,g)

Definition (Heat equation on a Riemannian manifold).

Let (M,g)(M,g) be a smooth Riemannian manifold. The heat equation on MM is

tu=ΔMu,u(,0)=u0L2(M,dVg).\partial_t u = \Delta_M u, \qquad u(\cdot, 0) = u_0 \in L^2(M, \mathrm{d}V_g).

For compact MM without boundary, a smooth solution for t>0t > 0 follows from the spectral theory of §4 via the heat semigroup u=etΔMu0u = e^{t\Delta_M} u_0. For complete non-compact MM, existence and uniqueness were established by Dodziuk [6] and Li–Yau [7].

3.2. The heat kernel

Definition (Heat kernel).

The heat kernel of (M,g)(M,g) is a smooth function K ⁣:(0,)×M×MRK \colon (0,\infty) \times M \times M \to \mathbb{R} such that

u(x,t)=MKt(x,y)u0(y)dVg(y)u(x,t) = \int_M K_t(x,y)\, u_0(y)\, \mathrm{d}V_g(y)

solves [eq:heat-curved] for every u0L2(M,dVg)u_0 \in L^2(M, \mathrm{d}V_g). It satisfies:

  1. (tΔMx)Kt(x,y)=0(\partial_t - \Delta_M^x)\, K_t(x,y) = 0 for all t>0t > 0, xyx \neq y.
  2. Kt(x,y)=Kt(y,x)K_t(x,y) = K_t(y,x) (symmetry from self-adjointness).
  3. MKt(x,y)dVg(y)1\int_M K_t(x,y)\, \mathrm{d}V_g(y) \leq 1 (equality for compact MM).
  4. MKs(x,z)Kt(z,y)dVg(z)=Ks+t(x,y)\int_M K_s(x,z)\, K_t(z,y)\, \mathrm{d}V_g(z) = K_{s+t}(x,y) (semigroup).
  5. Kt(x,y)>0K_t(x,y) > 0 for all t>0t > 0 [6].

3.3. Geodesic distance as the natural substitute

On (Rn,δ)(\mathbb{R}^n, \delta) the kernel [eq:flat-kernel] depends on xx and yy only through the Euclidean distance xy|\mathbf{x}-\mathbf{y}|. On a Riemannian manifold the canonical substitute is the geodesic distance dg(x,y)d_g(x,y). The heat kernel is not simply (4πt)n/2edg(x,y)2/4t(4\pi t)^{-n/2} e^{-d_g(x,y)^2/4t}, since curvature introduces corrections at every order in tt, but this is the leading term. The parametrix ansatz [8] is

Ht(x,y)=edg(x,y)2/4t(4πt)n/2k=0Nuk(x,y)tk,H_t(x,y) = \frac{e^{-d_g(x,y)^2/4t}}{(4\pi t)^{n/2}}\, \sum_{k=0}^{N} u_k(x,y)\, t^k,

where the transport coefficients uku_k are smooth functions determined by substituting [eq:parametrix] into the heat equation and matching powers of tt.

3.4. The transport equations and the short-time expansion

We derive the coefficients by inserting [eq:parametrix] into (tΔMx)Ht=0(\partial_t - \Delta_M^x)H_t = 0 and reading off each power of tt.

Setup. Fix yMy \in M and work in normal coordinates centred at yy (provided by the exponential map expy\exp_y). In these coordinates [3, Ch. 5]:

  • gij(y)=δijg_{ij}(y) = \delta_{ij} and kgij(y)=0\partial_k g_{ij}(y) = 0,
  • dg(x,y)2=x2d_g(x,y)^2 = |x|^2 to second order,
  • the volume density Θ(x,y):=g(x)\Theta(x,y) := \sqrt{g}(x) satisfies Θ(x,y)=116Rij(y)xixj+O(x3)\Theta(x,y) = 1 - \tfrac{1}{6}R_{ij}(y)x^ix^j + O(|x|^3).

Set ϕ(x,y)=dg(x,y)2/4\phi(x,y) = d_g(x,y)^2/4, so the exponential factor is eϕ/te^{-\phi/t}. Write the ansatz as Ht=(4πt)n/2eϕ/tΦH_t = (4\pi t)^{-n/2} e^{-\phi/t}\Phi where Φ=kuktk\Phi = \sum_k u_k t^k.

Applying the heat operator. Using the product formula for ΔM(eψf)\Delta_M(e^\psi f) with ψ=ϕ/t\psi = -\phi/t:

ΔM(eϕ/tΦ)=eϕ/t ⁣(ΔMΦ2tg(gradgϕ,gradgΦ)+Φ ⁣(ΔMϕt+ϕt2)).\Delta_M(e^{-\phi/t}\Phi) = e^{-\phi/t}\!\left(\Delta_M\Phi - \tfrac{2}{t}\,g(\operatorname{grad}_g\phi,\, \operatorname{grad}_g\Phi) + \Phi\!\left(-\tfrac{\Delta_M\phi}{t} + \tfrac{\phi}{t^2}\right)\right).

We evaluate two key quantities. The eikonal identity for geodesic distance:

gradgϕg2=ϕ,|\operatorname{grad}_g \phi|_g^2 = \phi,

which holds because gradgdg=r^\operatorname{grad}_g d_g = \hat{\mathbf{r}} is the unit radial vector and ϕ=dg2/4\phi = d_g^2/4 gives gradgϕ2=dg2gradgdg2/4=dg2/4=ϕ|{\rm grad}_g \phi|^2 = d_g^2|\operatorname{grad}_g d_g|^2/4 = d_g^2/4 = \phi. The Laplacian of ϕ\phi: writing gradgϕ=12dgr^\operatorname{grad}_g\phi = \tfrac{1}{2}d_g\hat{\mathbf{r}} and applying the Leibniz rule,

ΔMϕ=divg ⁣(12dgr^)=12 ⁣(g(gradgdg,r^)+dgdivgr^)=12 ⁣(1+dgdg ⁣logΘ)n1\Delta_M\phi = \operatorname{div}_g\!\left(\tfrac{1}{2}d_g\hat{\mathbf{r}}\right) = \tfrac{1}{2}\!\left(g(\operatorname{grad}_g d_g, \hat{\mathbf{r}}) + d_g\operatorname{div}_g\hat{\mathbf{r}}\right) = \tfrac{1}{2}\!\left(1 + d_g\,\partial_{d_g}\!\log\Theta\right) \cdot \frac{n}{1}

More precisely, since divgr^=dg ⁣logΘ+(n1)/dg\operatorname{div}_g\hat{\mathbf{r}} = \partial_{d_g}\!\log\Theta + (n-1)/d_g:

ΔMϕ=n2+dg2dg ⁣logΘ.\Delta_M\phi = \frac{n}{2} + \frac{d_g}{2}\,\partial_{d_g}\!\log\Theta.

Assembling [eq:product-laplacian], subtracting from tHt\partial_t H_t, and using [eq:laplacian-phi]:

(tΔMx)Ht  =  (4πt)n/2eϕ/t[kkuktk1ΔM ⁣kuktk+2tg ⁣(gradgϕ,gradgkuktk)+dg2t(dg ⁣logΘ)kuktk].\begin{aligned} (\partial_t - \Delta_M^x) H_t \;=\; (4\pi t)^{-n/2} e^{-\phi/t} \Biggl[ &\sum_k k\, u_k\, t^{k-1} - \Delta_M\!\textstyle\sum_k u_k t^k \\ &+ \tfrac{2}{t}\, g\!\left(\operatorname{grad}_g\phi,\, \operatorname{grad}_g\textstyle\sum_k u_k t^k\right) \\ &+ \tfrac{d_g}{2t}\,(\partial_{d_g}\!\log\Theta)\textstyle\sum_k u_k t^k \Biggr]. \end{aligned}

Collecting terms at order tk1t^{k-1} and using g(gradgϕ,gradg)=dg2dgg(\operatorname{grad}_g\phi, \operatorname{grad}_g\,\cdot\,) = \tfrac{d_g}{2}\partial_{d_g}:

kuk+dg2dguk+dg2(dg ⁣logΘ)uk=ΔMuk1k\, u_k + \frac{d_g}{2}\partial_{d_g} u_k + \frac{d_g}{2}(\partial_{d_g}\!\log\Theta)\, u_k = \Delta_M u_{k-1}

(with u10u_{-1} \equiv 0). Multiplying through by 2dg2k1Θ2d_g^{2k-1}\Theta shows that the left side equals dg(dg2kΘuk)/dgk1Θ1/2\partial_{d_g}(d_g^{2k}\Theta u_k)/d_g^{k-1}\Theta^{1/2}, yielding the kk-th transport ODE:

dg ⁣(dgkΘ1/2uk)=dgk1Θ1/2ΔMuk1.\partial_{d_g}\!\left(d_g^k \Theta^{1/2} u_k\right) = d_g^{k-1}\, \Theta^{1/2}\, \Delta_M u_{k-1}.

Coefficient u0u_0. Set k=0k = 0 in [eq:transport-ODE]:

dg ⁣(Θ1/2u0)=0,\partial_{d_g}\!\left(\Theta^{1/2} u_0\right) = 0,

so Θ1/2u0=c(y)\Theta^{1/2} u_0 = c(y). The normalisation condition Ht(x,y)δy(x)H_t(x,y) \to \delta_y(x) as t0+t \to 0^+ requires the leading coefficient to equal 1 at x=yx = y; since Θ(y,y)=1\Theta(y,y) = 1, we get c(y)=1c(y) = 1 and

u0(x,y)=Θ(x,y)1/2.u_0(x,y) = \Theta(x,y)^{-1/2}.

In particular, u0(y,y)=1u_0(y,y) = 1, recovering the flat-space leading term.

Coefficient u1u_1 on the diagonal. Integrate [eq:transport-ODE] for k=1k=1 from 00 to dgd_g:

dgΘ1/2(x,y)u1(x,y)=0dgΘ1/2(r,y)(ΔMu0)(r,y)dr.d_g\, \Theta^{1/2}(x,y)\, u_1(x,y) = \int_0^{d_g} \Theta^{1/2}(r,y)\,(\Delta_M u_0)(r,y)\, \mathrm{d}r.

As xyx \to y both sides vanish; applying L'Hôpital:

u1(y,y)=limdg01dg0dg(ΔMu0)(r,y)dr=(ΔMu0)(y,y).u_1(y,y) = \lim_{d_g \to 0} \frac{1}{d_g}\int_0^{d_g} (\Delta_M u_0)(r,y)\, \mathrm{d}r = (\Delta_M u_0)(y,y).

It remains to compute ΔM(Θ1/2)\Delta_M(\Theta^{-1/2}) at x=yx = y. In normal coordinates, Θ=g\Theta = \sqrt{g} has the expansion [8, Ch. 4]:

Θ1/2(x,y)=1+112Rij(y)xixj+O(x3).\Theta^{-1/2}(x,y) = 1 + \frac{1}{12} R_{ij}(y) x^i x^j + O(|x|^3).

Since ΔM(xixj)x=0=2δij\Delta_M(x^i x^j)|_{x=0} = 2\delta^{ij}, applying ΔM\Delta_M to [eq:theta-expand] at x=yx = y and using Rii=R(y)R_{ii} = R(y) (contraction of the Ricci tensor):

ΔM ⁣(Θ1/2)(y,y)=1122Rij(y)δij=R(y)6.\Delta_M\!\left(\Theta^{-1/2}\right)(y,y) = \frac{1}{12}\cdot 2\, R_{ij}(y)\delta^{ij} = \frac{R(y)}{6}.

Substituting [eq:delta-theta] into [eq:u1-lhopital]:

u1(y,y)=R(y)6.u_1(y,y) = \frac{R(y)}{6}.

The short-time diagonal expansion. Combining [eq:u0] and [eq:u1-diag] in [eq:parametrix] evaluated at x=yx = y [9]:

Kt(x,x)    1(4πt)n/2(1+R(x)6t+O(t2))as t0+.K_t(x,x) \;\sim\; \frac{1}{(4\pi t)^{n/2}} \left(1 + \frac{R(x)}{6}\, t + O(t^2)\right) \quad \text{as } t \to 0^+.
Remark (Curvature and the animation).

Return to the opening animation. Particles are coloured by exp(xx02/4t)\exp(-|\mathbf{x}-\mathbf{x}_0|^2/4t), the flat-space approximation. Equation [eq:heat-expansion] quantifies the correction: at a point xx where R(x)>0R(x) > 0 (positive curvature, near the poles of the deformed container), the diagonal kernel Kt(x,x)K_t(x,x) exceeds the flat baseline; there is less room for the particle density to spread, so it stays more concentrated. Where R(x)<0R(x) < 0 (saddle regions), the kernel is below the flat value and particles disperse faster.

The higher coefficients are universal polynomials in the curvature tensor and its covariant derivatives. The next term is [10]:

u2(x,x)=1360 ⁣(5R22Ric2+2Rm2) ⁣(x)+130ΔMR(x).u_2(x,x) = \frac{1}{360}\!\left(5R^2 - 2|\operatorname{Ric}|^2 + 2|\operatorname{Rm}|^2\right)\!(x) + \frac{1}{30}\Delta_M R(x).

3.5. Convergence of the parametrix

The parametrix [eq:parametrix] is not yet the true heat kernel; it satisfies (tΔMx)Ht=O(tNn/2)(\partial_t - \Delta_M^x)H_t = O(t^{N-n/2}) but is not exactly zero on the right. To construct the true kernel, one writes Kt=Ht+correctionK_t = H_t + \text{correction} where the correction solves a Volterra integral equation involving HtH_t. For compact MM, the correction is smooth and O(tNn/2+1)O(t^{N-n/2+1}), confirming that [eq:heat-expansion] is asymptotically exact [11, Ch. 4].

4. The Spectral Perspective

4.1. Spectral theorem for compact manifolds

Theorem (Spectral theorem for the Laplace–Beltrami operator).

Let (M,g)(M,g) be compact and connected without boundary. The operator ΔM-\Delta_M extends to a self-adjoint unbounded operator on L2(M,dVg)L^2(M, \mathrm{d}V_g) with domain H2(M)H^2(M). Its spectrum is a discrete sequence

0=λ0<λ1λ2,0 = \lambda_0 < \lambda_1 \leq \lambda_2 \leq \cdots \nearrow \infty,

and the corresponding eigenfunctions {ϕk}k0\{\phi_k\}_{k\geq 0} are smooth and form a complete orthonormal basis for L2(M,dVg)L^2(M, \mathrm{d}V_g):

ΔMϕk=λkϕk,ϕj,ϕkL2=δjk.-\Delta_M \phi_k = \lambda_k \phi_k, \qquad \langle \phi_j, \phi_k \rangle_{L^2} = \delta_{jk}.

The proof uses compactness of the Sobolev embedding H1(M)L2(M)H^1(M) \hookrightarrow L^2(M) (Rellich–Kondrachov), which forces the resolvent of ΔM-\Delta_M to be compact. The spectral theorem for compact self-adjoint operators then gives the discrete spectrum; elliptic regularity implies smoothness of eigenfunctions [12, Ch. 8].

4.2. Heat kernel as a spectral series

The heat semigroup etΔMe^{t\Delta_M} acts on L2(M)L^2(M) by

etΔMf=k=0eλktf,ϕkϕk,e^{t\Delta_M} f = \sum_{k=0}^\infty e^{-\lambda_k t} \langle f, \phi_k\rangle \phi_k,

which converges in L2L^2 for all t0t \geq 0 and in CC^\infty for t>0t > 0 (exponential decay of eλkte^{-\lambda_k t} dominates polynomial growth of λk\lambda_k). The integral kernel of etΔMe^{t\Delta_M} is

Kt(x,y)=k=0eλktϕk(x)ϕk(y),K_t(x,y) = \sum_{k=0}^\infty e^{-\lambda_k t}\, \phi_k(x)\, \phi_k(y),

confirming that [eq:kernel-rep] with this kernel reproduces [eq:semigroup-def].

On the interval [0,π][0,\pi] with Dirichlet boundary conditions, ϕn(x)=sin(nx)\phi_n(x) = \sin(nx) and λn=n2\lambda_n = n^2. The figure below animates the solution u(x,t)=n{1,3,5,7}ansin(nx)en2tu(x,t) = \sum_{n \in \{1,3,5,7\}} a_n \sin(nx)\, e^{-n^2 t}: faded traces are individual modes, bright gold is the sum. Mode n=7n = 7 (eigenvalue 4949) decays 49 times faster than mode n=1n = 1.

4.3. Weyl's law

Theorem (Weyl's law [<a href='#ref-weyl'>13</a>]).

Let N(λ)=#{k:λkλ}N(\lambda) = \#\{k : \lambda_k \leq \lambda\}. Then

N(λ)    ωn(2π)nVol(M)λn/2as λ,N(\lambda) \;\sim\; \frac{\omega_n}{(2\pi)^n}\,\mathrm{Vol}(M)\,\lambda^{n/2} \quad \text{as } \lambda \to \infty,

where ωn=πn/2/Γ(n/2+1)\omega_n = \pi^{n/2}/\Gamma(n/2+1) is the volume of the unit ball in Rn\mathbb{R}^n. Equivalently, λk(2π)2ωn2/n(k/Vol(M))2/n\lambda_k \sim (2\pi)^2 \omega_n^{-2/n}(k/\mathrm{Vol}(M))^{2/n} as kk \to \infty.

Proof via the heat trace. Define the heat trace

Z(t)=Tr(etΔM)=k=0eλkt=MKt(x,x)dVg(x).Z(t) = \operatorname{Tr}(e^{t\Delta_M}) = \sum_{k=0}^\infty e^{-\lambda_k t} = \int_M K_t(x,x)\, \mathrm{d}V_g(x).

The two expressions for Z(t)Z(t) are equal: substituting the spectral series [eq:spectral-kernel] into the integral gives keλktMϕk2dVg=keλkt\sum_k e^{-\lambda_k t}\int_M \phi_k^2\,\mathrm{d}V_g = \sum_k e^{-\lambda_k t} by orthonormality.

Step 1: heat trace asymptotics. Integrating the diagonal expansion [eq:heat-expansion] over MM:

Z(t)    Vol(M)(4πt)n/2(1+R6t+O(t2))as t0+,Z(t) \;\sim\; \frac{\mathrm{Vol}(M)}{(4\pi t)^{n/2}}\left(1 + \frac{\overline{R}}{6}\, t + O(t^2)\right) \quad \text{as } t \to 0^+,

where R=Vol(M)1MRdVg\overline{R} = \mathrm{Vol}(M)^{-1}\int_M R\, \mathrm{d}V_g is the average scalar curvature. The leading term is

Z(t)    Vol(M)(4πt)n/2as t0+.Z(t) \;\sim\; \frac{\mathrm{Vol}(M)}{(4\pi t)^{n/2}} \quad \text{as } t \to 0^+.

Step 2: rewriting as a Laplace–Stieltjes transform. Regard N(λ)=#{k:λkλ}N(\lambda) = \#\{k : \lambda_k \leq \lambda\} as a right-continuous step function on [0,)[0,\infty). Since λk\lambda_k \nearrow \infty, the Lebesgue–Stieltjes measure dN(λ)\mathrm{d}N(\lambda) is the sum of unit point masses at each λk\lambda_k, and

Z(t)=k=0eλkt=0eλtdN(λ).Z(t) = \sum_{k=0}^\infty e^{-\lambda_k t} = \int_0^\infty e^{-\lambda t}\,\mathrm{d}N(\lambda).

This is the Laplace–Stieltjes transform of NN.

Step 3: Karamata's Tauberian theorem. The general statement is: if μ\mu is a non-negative measure on [0,)[0,\infty) and its Laplace transform satisfies 0eλtdμ(λ)Ctα\int_0^\infty e^{-\lambda t}\,\mathrm{d}\mu(\lambda) \sim C\, t^{-\alpha} as t0+t \to 0^+, then μ([0,λ])Cλα/Γ(α+1)\mu([0,\lambda]) \sim C\,\lambda^\alpha / \Gamma(\alpha+1) as λ\lambda \to \infty [2, App. B].

Apply this with μ=dN\mu = \mathrm{d}N, C=Vol(M)/(4π)n/2C = \mathrm{Vol}(M)/(4\pi)^{n/2}, and α=n/2\alpha = n/2. The conclusion is

N(λ)    Vol(M)(4π)n/2λn/2Γ(n/2+1)as λ.N(\lambda) \;\sim\; \frac{\mathrm{Vol}(M)}{(4\pi)^{n/2}}\cdot\frac{\lambda^{n/2}}{\Gamma(n/2+1)} \quad \text{as } \lambda \to \infty.

Recognising ωn=πn/2/Γ(n/2+1)\omega_n = \pi^{n/2}/\Gamma(n/2+1) and (4π)n/2=2nπn/2(4\pi)^{n/2} = 2^n\pi^{n/2}:

1(4π)n/2Γ(n/2+1)=12nπn/2Γ(n/2+1)=ωn(2π)n,\frac{1}{(4\pi)^{n/2}\,\Gamma(n/2+1)} = \frac{1}{2^n\pi^{n/2}\,\Gamma(n/2+1)} = \frac{\omega_n}{(2\pi)^n},

so N(λ)ωn(2π)nVol(M)λn/2N(\lambda) \sim \frac{\omega_n}{(2\pi)^n}\mathrm{Vol}(M)\lambda^{n/2}, which is exactly [eq:weyl].

Step 4: equivalent eigenvalue asymptotics. Inverting: if N(λk)kN(\lambda_k) \approx k for large kk, then

ωn(2π)nVol(M)λkn/2k    λk((2π)nωnVol(M))2/nk2/n=(2π)2ωn2/n(kVol(M))2/n.\frac{\omega_n}{(2\pi)^n}\mathrm{Vol}(M)\,\lambda_k^{n/2} \approx k \implies \lambda_k \sim \left(\frac{(2\pi)^n}{\omega_n\,\mathrm{Vol}(M)}\right)^{2/n} k^{2/n} = (2\pi)^2\,\omega_n^{-2/n}\left(\frac{k}{\mathrm{Vol}(M)}\right)^{2/n}.

The figure below plots the exact trace Z(t)=k=160ek2tZ(t) = \sum_{k=1}^{60} e^{-k^2 t} (gold) against the Weyl leading term π/(2t)\sqrt{\pi}/(2\sqrt{t}) (blue) for the interval [0,π][0,\pi]. The animated cursor sweeps tt from large to small: agreement is excellent near t=0t = 0 but breaks down at large tt, where only the k=1k=1 mode survives.

4.4. Geometry encoded in the spectrum

The heat trace expansion [eq:trace-expansion] shows that the first two coefficients determine the volume and total scalar curvature MRdVg\int_M R\, \mathrm{d}V_g. For a compact surface (n=2n = 2), the Gauss–Bonnet theorem gives MKdVg=2πχ(M)\int_M K\, \mathrm{d}V_g = 2\pi\chi(M) where K=R/2K = R/2, so the second heat invariant encodes the Euler characteristic—a topological invariant.

The higher heat invariants are integrals of local curvature polynomials. Their computation underlies the heat-kernel proof of the Atiyah–Singer index theorem [14, 15]: for an elliptic operator DD on a compact manifold, the alternating heat trace Tr(etDD)Tr(etDD)\operatorname{Tr}(e^{-tD^*D}) - \operatorname{Tr}(e^{-tDD^*}) is constant in tt and equals the Fredholm index ind(D)\operatorname{ind}(D); expanding via the parametrix and integrating expresses the index as an integral of characteristic classes. The heat kernel is thus a bridge between the analytic data of a differential operator, the geometric data of a Riemannian metric, and the topology of the underlying manifold.

References

  1. A. Fick, "Über Diffusion," Annalen der Physik 170(1) (1855), 59–86. doi:10.1002/andp.18551700105
  2. E. M. Stein and R. Shakarchi, Fourier Analysis: An Introduction, Princeton University Press, 2003. Princeton UP
  3. J. M. Lee, Introduction to Riemannian Manifolds, 2nd ed., Springer GTM 176, 2018. doi:10.1007/978-3-319-91755-9
  4. J. M. Lee, Introduction to Smooth Manifolds, 2nd ed., Springer GTM 218, 2013. doi:10.1007/978-1-4419-9982-5
  5. I. Chavel, Eigenvalues in Riemannian Geometry, Academic Press, 1984. ScienceDirect
  6. J. Dodziuk, "Maximum principle for parabolic inequalities and the heat flow on open manifolds," Indiana Univ. Math. J. 32(5) (1983), 703–716. JSTOR
  7. P. Li and S.-T. Yau, "On the parabolic kernel of the Schrödinger operator," Acta Math. 156 (1986), 153–201. doi:10.1007/BF02399203
  8. M. Berger, P. Gauduchon, and E. Mazet, Le spectre d'une variété riemannienne, Springer LNM 194, 1971. doi:10.1007/BFb0064643
  9. S. Minakshisundaram and Å. Pleijel, "Some properties of the eigenfunctions of the Laplace operator on Riemannian manifolds," Canad. J. Math. 1 (1949), 242–256. doi:10.4153/CJM-1949-021-5
  10. P. B. Gilkey, Invariance Theory, the Heat Equation, and the Atiyah–Singer Index Theorem, 2nd ed., CRC Press, 1995. doi:10.1201/9780849378744
  11. S. Rosenberg, The Laplacian on a Riemannian Manifold, Cambridge University Press, 1997. doi:10.1017/CBO9780511623783
  12. M. E. Taylor, Partial Differential Equations II, Springer Applied Math. Sciences 116, 1996. doi:10.1007/978-1-4757-4187-2
  13. H. Weyl, "Über die asymptotische Verteilung der Eigenwerte," Nachrichten der Königlichen Gesellschaft der Wissenschaften zu Göttingen (1912), 110–117. GDZ Göttingen
  14. M. F. Atiyah, R. Bott, and V. K. Patodi, "On the heat equation and the index theorem," Inventiones Mathematicae 19 (1973), 279–330. doi:10.1007/BF01425417
  15. E. Getzler, "A short proof of the local Atiyah–Singer index theorem," Topology 25(1) (1986), 111–117. doi:10.1016/0040-9383(86)90008-X

Comments

Loading…

Leave a comment

or comment as guest

$...$ inline · $$...$$ display

0 / 2000