Book 9B

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Course 9Book 9B: Comparison, Convergence and Heat on ManifoldsChapter 7

The Heat Equation on a Manifold

Heat kernels, the maximum principle without boundary, Li–Yau, and the conjugate heat operator.

25 min read · Updated Oct 3, 2026

There is no single companion for this seam chapter. Grigor'yan's Heat Kernel and Analysis on Manifolds and Chavel's Eigenvalues in Riemannian Geometry are the references for heat kernels; Li and Yau's paper "On the parabolic kernel of the Schrödinger operator" (Acta Mathematica, 1986) is the source of the gradient estimate; Topping's Lectures on the Ricci Flow has the conjugate heat equation in the form used later.

In this chapter · 8 sections
  1. 7.1Distances from heat
  2. 7.2The heat kernel of a closed manifold
  3. 7.3The maximum principle without boundary
  4. 7.4Short times: what heat knows about geometry
  5. 7.5Li–Yau
  6. 7.6Moving metrics and the conjugate heat equation
  7. 7.7History
  8. 7.8Exercises

Book 6A studied the heat equation in Rn\mathbb{R}^n. Book 11A studies the Ricci flow, a heat equation for a metric. This chapter is the bridge: the heat equation ∂tu=Δu\partial_tu = \Delta u on a closed Riemannian manifold, where there is no boundary and no infinity, and where curvature enters the estimates. Everything is in place. The spectral theorem gives the solution as an eigenfunction expansion (9A.6 The Laplacian and the Bochner Formula, 4A.7 Compact Operators and Spectra). The maximum principle works as in 6A.4 Maximum Principles, with nothing to check at a boundary. The Bochner formula turns a Ricci lower bound into the Li–Yau gradient estimate, the model for Hamilton's Harnack inequality. The chapter ends with time-dependent metrics, and derives the conjugate heat operator −∂t−Δ+R-\partial_t - \Delta + R that sits at the centre of Perelman's work.

By the end of this chapter you will be able to:

  • construct the heat kernel of a closed manifold from eigenfunctions, and list its basic properties;
  • prove the maximum principle and conservation of total heat on a closed manifold, and use Hamilton's trick;
  • state the short-time asymptotics (Minakshisundaram–Pleijel, Varadhan) and read geometry from them;
  • state and check the Li–Yau gradient estimate and its Harnack inequality;
  • derive the adjoint of the heat operator for a time-dependent metric, and recognise the conjugate heat equation of the Ricci flow.

Distances from heat

In the world In use Geodesics in heat

Heat spreading from a point for a very short time tt reaches a point at distance dd with an amount roughly proportional to e−d2/4te^{-d^2/4t}. So the temperature encodes distance: d2≈−4tlog⁡ud^2 \approx -4t\log u, a statement made precise by Varadhan's formula below. Keenan Crane, Clarisse Weischedel and Max Wardetzky turned this into an algorithm ("Geodesics in heat", ACM Transactions on Graphics, 2013). On a triangle mesh, run the heat equation from a source for one short time step (one sparse linear solve with the cotangent Laplacian of 9A.6 The Laplacian and the Bochner Formula). Take the direction of the gradient of the result, which points away from the source along geodesics, normalise it to unit length, and recover the distance function by solving one Poisson equation. Using only the direction of the gradient makes the method robust where Varadhan's formula applied directly would be inaccurate. The method is fast because the linear systems can be factored once and reused, and it is now standard in geometry processing.

In neuroimaging, data measured on the folded surface of the cerebral cortex (such as cortical thickness) are smoothed by running the heat equation on the surface instead of averaging over balls in space, which would mix points that are close in space but far apart along the folded cortex. Moo Chung and colleagues introduced heat-kernel smoothing for this purpose (NeuroImage, 2005).

The heat kernel of a closed manifold

Let MM be closed and connected, and let ϕ0,ϕ1,…\phi_0, \phi_1, \dots be an orthonormal basis of L2(M)L^2(M) of eigenfunctions, −Δϕk=λkϕk-\Delta\phi_k = \lambda_k\phi_k, 0=λ0<λ1≤λ2≤…0 = \lambda_0 < \lambda_1 \leq \lambda_2 \leq \dots (9A.6 The Laplacian and the Bochner Formula). The solution of ∂tu=Δu\partial_tu = \Delta u with u(⋅,0)=u0u(\cdot, 0) = u_0 is

u(x,t)=∑ke−λkt⟨u0,ϕk⟩ϕk(x)=∫Mp(x,y,t)u0(y) dV(y),u(x, t) = \sum_ke^{-\lambda_kt}\langle u_0, \phi_k\rangle\phi_k(x) = \int_Mp(x, y, t)u_0(y)\,dV(y),

with the heat kernel

p(x,y,t)=∑ke−λktϕk(x)ϕk(y).p(x, y, t) = \sum_ke^{-\lambda_kt}\phi_k(x)\phi_k(y).

The series converges smoothly for t>0t > 0, by Weyl's law for the growth of λk\lambda_k and elliptic estimates. The heat kernel has the properties of the Gaussian of 6A.3 The Heat Equation on ℝⁿ:

  • it is symmetric in x,yx, y, solves the heat equation in each variable, and tends to the delta function at yy as t→0t \to 0;
  • it is positive, and ∫Mp(x,y,t) dV(y)=1\int_Mp(x, y, t)\,dV(y) = 1, since constants are preserved;
  • it satisfies the semigroup law p(x,z,t+s)=∫p(x,y,t)p(y,z,s) dV(y)p(x, z, t + s) = \int p(x, y, t)p(y, z, s)\,dV(y);
  • as t→∞t \to \infty, p→1Vol⁡Mp \to \frac{1}{\operatorname{Vol}M}, exponentially fast at rate λ1\lambda_1: the spectral gap is the rate of equilibration (Exercise 7.3).

On the unit sphere S2S^2 the eigenfunctions are spherical harmonics, and the kernel is a Legendre series, p=∑l2l+14πe−l(l+1)tPl(cos⁡θ)p = \sum_l\frac{2l + 1}{4\pi}e^{-l(l + 1)t}P_l(\cos\theta), with θ\theta the angle between xx and yy (Figure 7.1).

Figure 7.1. The heat kernel of the unit sphere, p(θ,t)p(\theta, t), at t=0.02,0.05,0.1,0.3t = 0.02, 0.05, 0.1, 0.3 and 11, computed from its Legendre series. Heat spreads from the source and approaches the uniform value 14π\frac{1}{4\pi} (dashed), at the rate e−2te^{-2t} set by λ1=2\lambda_1 = 2.

The maximum principle without boundary

Proposition 7.1 The maximum principle on a closed manifold

If ∂tu≤Δu\partial_tu \leq \Delta u on M×[0,T]M\times[0, T], then max⁡Mu(⋅,t)\max_Mu(\cdot, t) is nonincreasing in tt. In particular solutions of the heat equation satisfy min⁡u0≤u≤max⁡u0\min u_0 \leq u \leq \max u_0, and are unique.

Proof. For ε>0\varepsilon > 0 let v=u−εtv = u - \varepsilon t, so that ∂tv<Δv\partial_tv < \Delta v. Suppose max⁡v(⋅,t)\max v(\cdot, t) exceeded max⁡v(⋅,0)\max v(\cdot, 0); then the first time and place (x0,t0)(x_0, t_0) where vv reaches a value above max⁡v(⋅,0)\max v(\cdot, 0), slightly increased, has t0>0t_0 > 0, ∂tv(x0,t0)≥0\partial_tv(x_0, t_0) \geq 0 and, because x0x_0 is a spatial maximum and there is no boundary, Δv(x0,t0)≤0\Delta v(x_0, t_0) \leq 0 (9A.6 The Laplacian and the Bochner Formula). This contradicts ∂tv<Δv\partial_tv < \Delta v. Let ε→0\varepsilon \to 0. Uniqueness: the difference of two solutions has maximum and minimum zero.

The same argument handles equations with lower-order terms, systems, and tensors: it is the template of 6A.4 Maximum Principles with the boundary case deleted. Hamilton's trick packages it. If uu is smooth on M×[0,T]M\times[0, T], the function μ(t)=max⁡Mu(⋅,t)\mu(t) = \max_Mu(\cdot, t) is Lipschitz, and at each tt its upper right derivative is at most max⁡{∂tu(x,t):u(x,t)=μ(t)}\max\{\partial_tu(x, t) : u(x, t) = \mu(t)\} (Exercise 7.5). So pointwise information at a maximum, where ∇u=0\nabla u = 0 and Δu≤0\Delta u \leq 0, becomes an ODE inequality for μ\mu. That is how the evolution of the minimum of scalar curvature was handled in the last exercise of 9B.6 Scalar Curvature and Topology.

Conservation. ddt∫Mu dV=∫MΔu dV=0\frac{d}{dt}\int_Mu\,dV = \int_M\Delta u\,dV = 0: total heat is conserved on a fixed closed manifold. The next sections ask what replaces this when the metric moves.

Short times: what heat knows about geometry

As t→0t \to 0, the heat kernel looks like the Euclidean one, corrected by curvature. Subbaramiah Minakshisundaram and Åke Pleijel (1949) proved an asymptotic expansion

p(x,x,t)∼(4πt)−n/2(1+R(x)6t+O(t2)),p(x, x, t) \sim (4\pi t)^{-n/2}\Big(1 + \frac{R(x)}{6}t + O(t^2)\Big),

with higher coefficients given by curvature invariants. Integrating over MM, the heat trace satisfies

∑ke−λkt=∫Mp(x,x,t) dV∼(4πt)−n/2(Vol⁡(M)+t6∫MR dV+O(t2)).\sum_ke^{-\lambda_kt} = \int_Mp(x, x, t)\,dV \sim (4\pi t)^{-n/2}\Big(\operatorname{Vol}(M) + \frac t6\int_MR\,dV + O(t^2)\Big).

So the eigenvalues determine the dimension, the volume and the total scalar curvature: part of the answer to Mark Kac's 1966 question "Can one hear the shape of a drum?" For a surface, ∫R=4πχ\int R = 4\pi\chi by Gauss–Bonnet, so the spectrum determines the Euler characteristic (Exercise 7.6).

Off the diagonal, Varadhan's formula (S. R. S. Varadhan, 1967) recovers the distance:

lim⁡t→0(−4tlog⁡p(x,y,t))=d(x,y)2.\lim_{t\to0}\big(-4t\log p(x, y, t)\big) = d(x, y)^2.

The normalisation matches the Euclidean kernel (4πt)−n/2e−∣x−y∣2/4t(4\pi t)^{-n/2}e^{-|x - y|^2/4t} and the analyst's Laplacian of this guide (Figure 7.2).

Figure 7.2. Varadhan's formula on the unit sphere: −4tlog⁡((4πt) p(θ,t))-4t\log\big((4\pi t)\,p(\theta, t)\big) for t=0.5,0.2,0.1,0.05t = 0.5, 0.2, 0.1, 0.05 (computed from the Legendre series), approaching d2=θ2d^2 = \theta^2 (dashed). The factor 4πt4\pi t removes the prefactor of the kernel and does not change the limit.

Li–Yau

Theorem 7.2 Li–Yau gradient estimate

Let MM be closed with Ric⁡≥0\operatorname{Ric} \geq 0, and let u>0u > 0 solve ∂tu=Δu\partial_tu = \Delta u on M×(0,∞)M\times(0, \infty). Then

∣∇u∣2u2−∂tuu≤n2t.\frac{|\nabla u|^2}{u^2} - \frac{\partial_tu}{u} \leq \frac{n}{2t}.
The idea How the proof goes

Write f=log⁡uf = \log u, so that ∂tf=Δf+∣∇f∣2\partial_tf = \Delta f + |\nabla f|^2, and consider F=t(∣∇f∣2−∂tf)=−tΔfF = t(|\nabla f|^2 - \partial_tf) = -t\Delta f. Differentiating, and using the Bochner formula (9A.6 The Laplacian and the Bochner Formula) for Δ∣∇f∣2\Delta|\nabla f|^2,

(∂t−Δ)F=Ft−2t(∣∇2f∣2+Ric⁡(∇f,∇f))+2⟨∇f,∇F⟩.(\partial_t - \Delta)F = \frac Ft - 2t\big(|\nabla^2f|^2 + \operatorname{Ric}(\nabla f, \nabla f)\big) + 2\langle\nabla f, \nabla F\rangle.

With Ric⁡≥0\operatorname{Ric} \geq 0 and ∣∇2f∣2≥1n(Δf)2=F2nt2|\nabla^2f|^2 \geq \frac1n(\Delta f)^2 = \frac{F^2}{nt^2} (Cauchy–Schwarz for the trace),

(∂t−Δ)F≤Ft−2F2nt+2⟨∇f,∇F⟩.(\partial_t - \Delta)F \leq \frac Ft - \frac{2F^2}{nt} + 2\langle\nabla f, \nabla F\rangle.

At the first time FF reaches a new maximum value, ∇F=0\nabla F = 0, ΔF≤0\Delta F \leq 0 and ∂tF≥0\partial_tF \geq 0, so 0≤Ft(1−2Fn)0 \leq \frac Ft(1 - \frac{2F}{n}), which is impossible if F>n2F > \frac n2. Hence F≤n2F \leq \frac n2, which is the estimate. The computation in Rn\mathbb{R}^n is in 6A.10 Entropy, Information and Diffusion; on the Euclidean heat kernel equality holds at every point (Exercise 7.7).

Integrating the estimate along a path from (x,t1)(x, t_1) to (y,t2)(y, t_2) gives the Harnack inequality

u(x,t1)≤u(y,t2)(t2t1)n/2exp⁡(d(x,y)24(t2−t1)),t1<t2,u(x, t_1) \leq u(y, t_2)\Big(\frac{t_2}{t_1}\Big)^{n/2}\exp\Big(\frac{d(x, y)^2}{4(t_2 - t_1)}\Big), \qquad t_1 < t_2,

which compares temperatures at different places and times: heat cannot be very concentrated now if it will be spread out later. Hamilton's Harnack inequality for the Ricci flow (11B.2 Ancient Solutions and the Harnack Inequality) is the analogue for the curvature itself, and Perelman's reduced distance (12A.5 Reduced Distance and Reduced Volume) is the length functional that this integration suggests.

Moving metrics and the conjugate heat equation

Now let the metric depend on time, ∂tg=h\partial_tg = h. The volume form changes (Exercise 7.8):

∂t dV=12tr⁡gh dV.\partial_t\,dV = \tfrac12\operatorname{tr}_gh\,dV.

For the heat operator □=∂t−Δg(t)\square = \partial_t - \Delta_{g(t)}, integrate by parts in space and time for functions u,vu, v on M×[a,b]M\times[a, b]:

∫ab ⁣ ⁣∫M(□u)v dV dt=[∫Muv dV]ab+∫ab ⁣ ⁣∫Mu(−∂tv−Δv−12(tr⁡h)v) dV dt.\int_a^b\!\!\int_M(\square u)v\,dV\,dt = \Big[\int_Muv\,dV\Big]_a^b + \int_a^b\!\!\int_Mu\big(-\partial_tv - \Delta v - \tfrac12(\operatorname{tr}h)v\big)\,dV\,dt.

So the formal adjoint of □\square is

□∗=−∂t−Δ−12tr⁡gh.\square^* = -\partial_t - \Delta - \tfrac12\operatorname{tr}_gh.

Under the Ricci flow, h=−2Ric⁡h = -2\operatorname{Ric} and 12tr⁡h=−R\frac12\operatorname{tr}h = -R, so

□∗=−∂t−Δ+R,\square^* = -\partial_t - \Delta + R,

the conjugate heat operator. If □u=0\square u = 0 and □∗v=0\square^*v = 0, then ∫Muv dV\int_Muv\,dV is constant in time; with u≡1u \equiv 1, a solution of □∗v=0\square^*v = 0 keeps ∫Mv dV\int_Mv\,dV constant. A solution of the conjugate heat equation runs backwards in time, like heat flowing from the future into the past, and conserves total mass.

Where this goes Perelman's use

Perelman's F\mathcal F- and W\mathcal W-functionals (12A.2 Ricci Flow as a Gradient Flow, 12A.3 The 𝓦-Entropy) are integrals against a density (4πτ)−n/2e−f(4\pi\tau)^{-n/2}e^{-f} that solves the conjugate heat equation along a Ricci flow, with τ\tau the time remaining before a reference time. Their monotonicity is a Li–Yau type computation for that density, and the backward heat kernel of the flow, centred at a singular point, is what his reduced volume (12A.5 Reduced Distance and Reduced Volume) and pseudolocality (12A.6 Pseudolocality) are built around.

History

Fourier's Théorie analytique de la chaleur (1822) founded the subject. Minakshisundaram and Pleijel's expansion appeared in 1949, and Kac's drum question in 1966, followed by McKean and Singer's study of the heat trace in 1967. Varadhan's formula dates from 1967. Peter Li and Shing-Tung Yau published their estimate in 1986, Hamilton his matrix Harnack inequality for the Ricci flow in 1993, and Perelman the conjugate heat equation's central role in 2002.

Recall Book 9B in one paragraph

The distance function from a point obeys a Riccati equation, and a lower Ricci bound gives Laplacian comparison, Δr≤(n−1)sn⁡k′sn⁡k\Delta r \leq (n - 1)\frac{\operatorname{sn}_k'}{\operatorname{sn}_k}, in the barrier sense everywhere (9B.1 Laplacian Comparison). Integrated, it gives Bishop–Gromov volume comparison, doubling, packing and asymptotic volume ratios (9B.2 Volume Comparison). Volume and curvature bounds together bound the injectivity radius (Cheeger–Gromov–Taylor), collapse is the only obstruction, and Perelman's κ\kappa-noncollapsing is the condition that excludes it (9B.3 Collapsing and Noncollapsing). Gromov–Hausdorff and Cheeger–Gromov convergence give limits, the compactness theorem extracts them, and the compactness–contradiction template uses them (9B.4 Convergence of Manifolds). Lines split manifolds with Ric⁡≥0\operatorname{Ric} \geq 0, and nonnegatively curved ones are bundles over souls (9B.5 Splitting and Soul Theorems). Positive scalar curvature is obstructed and survives surgery (9B.6 Scalar Curvature and Topology). On a closed manifold the heat equation has an eigenfunction kernel, a boundary-free maximum principle, Varadhan and Li–Yau estimates, and, for moving metrics, the conjugate heat operator −∂t−Δ+R-\partial_t - \Delta + R (this chapter).

Where this goes Into Book 10A

The analytic and geometric toolkit is complete. Before turning it on the Ricci flow, Book 10A asks what the answer should look like: which closed 3-manifolds exist, how they decompose along spheres and tori, and which geometries they carry. That map of destinations shows what surgery and extinction must produce (12C.1 Reading Off the Topology), and why the Poincaré conjecture is one case of Thurston's geometrization.

Exercises

Exercise 7.3 Decay to equilibrium

Let uu solve the heat equation on a closed manifold, with mean uˉ=1Vol⁡M∫u0 dV\bar u = \frac{1}{\operatorname{Vol}M}\int u_0\,dV. Show that uˉ\bar u is constant in time and that ∫(u−uˉ)2 dV≤e−2λ1t∫(u0−uˉ)2 dV\int(u - \bar u)^2\,dV \leq e^{-2\lambda_1t}\int(u_0 - \bar u)^2\,dV, both from the eigenfunction expansion and by differentiating in time and using ∫∣∇w∣2≥λ1∫w2\int|\nabla w|^2 \geq \lambda_1\int w^2 for ww of mean zero.

Solution

uˉ\bar u is the coefficient of ϕ0\phi_0, which is not damped. In the expansion, u−uˉ=∑k≥1e−λktckϕku - \bar u = \sum_{k \geq 1}e^{-\lambda_kt}c_k\phi_k, so ∥u−uˉ∥2=∑k≥1e−2λktck2≤e−2λ1t∑ck2\|u - \bar u\|^2 = \sum_{k \geq 1}e^{-2\lambda_kt}c_k^2 \leq e^{-2\lambda_1t}\sum c_k^2. Directly: ddt∫(u−uˉ)2=2∫(u−uˉ)Δu=−2∫∣∇u∣2≤−2λ1∫(u−uˉ)2\frac{d}{dt}\int(u - \bar u)^2 = 2\int(u - \bar u)\Delta u = -2\int|\nabla u|^2 \leq -2\lambda_1\int(u - \bar u)^2, and Gronwall (2B.10 Ordinary Differential Equations).

Exercise 7.4 The heat kernel of a circle

On R/2πZ\mathbb{R}/2\pi\mathbb{Z}, show p(x,y,t)=12π∑k∈Ze−k2teik(x−y)p(x, y, t) = \frac{1}{2\pi}\sum_{k \in \mathbb{Z}}e^{-k^2t}e^{ik(x - y)}, and that it also equals ∑m∈Z(4πt)−1/2e−(x−y+2πm)2/4t\sum_{m \in \mathbb{Z}}(4\pi t)^{-1/2}e^{-(x - y + 2\pi m)^2/4t} (the Euclidean kernel, wrapped around; the two expressions agree by Poisson summation). Use the second to verify Varadhan's formula for ∣x−y∣<π|x - y| < \pi.

Solution

The normalised eigenfunctions are eikx2π\frac{e^{ikx}}{\sqrt{2\pi}} with eigenvalues k2k^2. The wrapped Gaussian solves the heat equation, is periodic, and tends to the periodic delta function, so it is the same kernel. For ∣x−y∣<π|x - y| < \pi, the m=0m = 0 term dominates as t→0t \to 0, the others being smaller by factors e−c/te^{-c/t}, so −4tlog⁡p=(x−y)2+2tlog⁡(4πt)+o(1)→(x−y)2-4t\log p = (x - y)^2 + 2t\log(4\pi t) + o(1) \to (x - y)^2.

Exercise 7.5 Hamilton's trick

Let uu be smooth on M×[0,T]M\times[0, T] with MM compact, and μ(t)=max⁡Mu(⋅,t)\mu(t) = \max_Mu(\cdot, t). Show that lim sup⁡s↓0μ(t+s)−μ(t)s≤max⁡{∂tu(x,t):u(x,t)=μ(t)}\limsup_{s\downarrow0}\frac{\mu(t + s) - \mu(t)}{s} \leq \max\{\partial_tu(x, t) : u(x, t) = \mu(t)\}. (Pick xsx_s with u(xs,t+s)=μ(t+s)u(x_s, t + s) = \mu(t + s), pass to a convergent subsequence, and use u(xs,t)≤μ(t)u(x_s, t) \leq \mu(t).)

Solution

μ(t+s)−μ(t)≤u(xs,t+s)−u(xs,t)=s ∂tu(xs,t+σs)\mu(t + s) - \mu(t) \leq u(x_s, t + s) - u(x_s, t) = s\,\partial_tu(x_s, t + \sigma_s) for some σs∈(0,s)\sigma_s \in (0, s). Along a subsequence xs→x∗x_s \to x_*, and by continuity u(x∗,t)=lim⁡u(xs,t+s)=lim⁡μ(t+s)=μ(t)u(x_*, t) = \lim u(x_s, t + s) = \lim\mu(t + s) = \mu(t) (μ\mu is continuous), so x∗x_* is a maximum point at time tt and the difference quotients converge to ∂tu(x∗,t)\partial_tu(x_*, t).

Exercise 7.6 The heat trace of the sphere

For the unit S2S^2, ∑ke−λkt=∑l≥0(2l+1)e−l(l+1)t\sum_ke^{-\lambda_kt} = \sum_{l \geq 0}(2l + 1)e^{-l(l + 1)t}. Writing x=l+12x = l + \frac12, so that l(l+1)=x2−14l(l + 1) = x^2 - \frac14, and using the midpoint rule ∑l≥0f(l+12)=∫0∞f(x) dx+124f′(0)+…\sum_{l \geq 0}f(l + \frac12) = \int_0^\infty f(x)\,dx + \frac{1}{24}f'(0) + \dots for f(x)=2xe−tx2f(x) = 2xe^{-tx^2}, show that the trace is 1t+13+O(t)\frac1t + \frac13 + O(t). Compare with the Minakshisundaram–Pleijel prediction (4πt)−1(Area⁡+t6∫R)(4\pi t)^{-1}(\operatorname{Area} + \frac t6\int R) with area 4π4\pi and R=2R = 2.

Solution

∑(2l+1)e−l(l+1)t=et/4∑f(l+12)\sum(2l + 1)e^{-l(l + 1)t} = e^{t/4}\sum f(l + \frac12), and ∫0∞2xe−tx2dx=1t\int_0^\infty2xe^{-tx^2}dx = \frac1t, f′(0)=2f'(0) = 2. So the trace is (1+t4+… )(1t+112+O(t))=1t+14+112+O(t)=1t+13+O(t)(1 + \frac t4 + \dots)(\frac1t + \frac{1}{12} + O(t)) = \frac1t + \frac14 + \frac{1}{12} + O(t) = \frac1t + \frac13 + O(t). The prediction: 14πt(4π+t6⋅8π)=1t+13\frac{1}{4\pi t}(4\pi + \frac t6\cdot8\pi) = \frac1t + \frac13. (Numerically, the trace at t=0.01t = 0.01 is 100.334100.334.)

Exercise 7.7 Equality in Li–Yau

For the Euclidean heat kernel u=(4πt)−n/2e−∣x∣2/4tu = (4\pi t)^{-n/2}e^{-|x|^2/4t}, show ∣∇u∣2u2−∂tuu=n2t\frac{|\nabla u|^2}{u^2} - \frac{\partial_tu}{u} = \frac{n}{2t} at every point. Deduce the Harnack inequality's sharpness.

Solution

log⁡u=−n2log⁡(4πt)−∣x∣24t\log u = -\frac n2\log(4\pi t) - \frac{|x|^2}{4t}, so ∣∇log⁡u∣2=∣x∣24t2|\nabla\log u|^2 = \frac{|x|^2}{4t^2} and ∂tlog⁡u=−n2t+∣x∣24t2\partial_t\log u = -\frac{n}{2t} + \frac{|x|^2}{4t^2}; the difference is n2t\frac{n}{2t}. Equality in the gradient estimate along the path that realises it gives equality in the integrated Harnack inequality, so the constants cannot be improved.

Exercise 7.8 Rehearsal: the conjugate heat equation

(a) For ∂tgij=hij\partial_tg_{ij} = h_{ij}, show ∂tdet⁡g=12gijhijdet⁡g\partial_t\sqrt{\det g} = \frac12g^{ij}h_{ij}\sqrt{\det g} (use ∂tlog⁡det⁡g=gij∂tgij\partial_t\log\det g = g^{ij}\partial_tg_{ij}, 8A.7 Tensors and Index Notation). (b) Show that if −∂tv−Δv−12(tr⁡h)v=0-\partial_tv - \Delta v - \frac12(\operatorname{tr}h)v = 0, then ddt∫Mv dV=0\frac{d}{dt}\int_Mv\,dV = 0. (c) Under the Ricci flow, write the equation for vv, and check that for the shrinking round sphere a spatially constant v(t)v(t) solving it is v=cVol⁡(M,g(t))v = \frac{c}{\operatorname{Vol}(M, g(t))}. This is the equation 12A.2 Ricci Flow as a Gradient Flow starts from.

Solution

(a) As stated, since dV=det⁡g dxdV = \sqrt{\det g}\,dx. (b) ddt∫v dV=∫(∂tv+12(tr⁡h)v) dV=∫(−Δv) dV=0\frac{d}{dt}\int v\,dV = \int(\partial_tv + \frac12(\operatorname{tr}h)v)\,dV = \int(-\Delta v)\,dV = 0. (c) −∂tv−Δv+Rv=0-\partial_tv - \Delta v + Rv = 0. For constant vv: v′=Rvv' = Rv. On the shrinking sphere ddtVol⁡=−∫R dV=−RVol⁡\frac{d}{dt}\operatorname{Vol} = -\int R\,dV = -R\operatorname{Vol} (RR is constant in space), so ddtcVol⁡=cRVol⁡Vol⁡2=RcVol⁡\frac{d}{dt}\frac{c}{\operatorname{Vol}} = \frac{cR\operatorname{Vol}}{\operatorname{Vol}^2} = R\frac{c}{\operatorname{Vol}}. Its integral vVol⁡=cv\operatorname{Vol} = c is constant, as (b) predicts.

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