Book 12A

© 2026 NeckPinch · www.neckpinch.com · All rights reserved.

Course 12Book 12A: Entropy and NoncollapsingChapter 6

Pseudolocality

Almost-Euclidean regions stay controlled, and the Harnack inequality behind it.

21 min read · Updated Oct 3, 2026

Read Perelman I, §9 and §10, then the full proof of pseudolocality in Kleiner and Lott's notes. Li and Yau's 1986 paper is the ancestor of §9, and 6A.10 Entropy, Information and Diffusion and 9B.7 The Heat Equation on a Manifold set it up.

In this chapter · 5 sections
  1. 6.1Far-away events
  2. 6.2Perelman's Harnack inequality
  3. 6.3Pseudolocality
  4. 6.3.1The architecture of the proof
  5. 6.3.2Where it is used
  6. 6.4History
  7. 6.5Exercises

Book 12A ends with two results from §§9–10 of Perelman's first preprint, and the second is the deepest. The first is a differential Harnack inequality for the conjugate heat kernel on a Ricci flow background. It is a pointwise version of the monotonicity of W\mathcal W, and works locally, where integrals over the whole manifold are unavailable. The second is pseudolocality: a region that is almost Euclidean at some scale stays tame for a definite time at a smaller scale, whatever happens elsewhere. Perelman's own gloss is that regions where the curvature is huge cannot, at once, have much effect on regions that are nearly Euclidean. The flow is a heat equation, and heat equations propagate information at infinite speed; pseudolocality says that for the Ricci flow, in a precise sense, they do not propagate damage that fast.

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

  • state Perelman's Proposition 9.1 and the inequality v≤0v \leq 0 for the conjugate heat kernel, and explain how it is proved;
  • derive Perelman's Harnack inequality along curves and the comparison f≤ℓf \leq \ell;
  • state the pseudolocality theorem with every quantifier in place, and its corollaries;
  • outline the proof of pseudolocality and say where each earlier result is used;
  • say where pseudolocality is used in the rest of the proof.

Far-away events

In the world Analogy Gaussian tails

Put a hot spot on a cold metal plate. The heat equation says that the temperature everywhere rises instantly, but by an amount that is exponentially small, like e−d2/4te^{-d^2/4t} at distance dd, until tt is comparable to d2d^2. For practical purposes, a distant event does not matter yet. Pseudolocality is a statement of this kind about the curvature of the Ricci flow: if a ball looks almost Euclidean now, wild curvature outside it cannot make it wild for a time of order (its size)2^2.

Where the picture breaks

The analogy is linear and the theorem is not. Pseudolocality concerns the flow's own curvature, which is the unknown, not a passive temperature. Its hypotheses are geometric (a lower bound on scalar curvature and an almost-Euclidean isoperimetric inequality), not a distance condition, and the conclusion is a bound, not a smallness: curvature in the controlled region may still become as large as αt−1\alpha t^{-1}. And there is no exponentially small effect in the theorem. Nothing at all is claimed about the far-away region.

Perelman's Harnack inequality

Let g(t)g(t), 0≤t≤T0 \leq t \leq T, be a Ricci flow, set τ=T−t\tau = T - t, and let u=(4πτ)−n/2e−fu = (4\pi\tau)^{-n/2}e^{-f} solve the conjugate heat equation □∗u=−∂tu−Δu+Ru=0\square^*u = -\partial_tu - \Delta u + Ru = 0 (9B.7 The Heat Equation on a Manifold).

Proposition 6.1 The pointwise formula (Perelman I, Proposition 9.1)

The function v=[τ(2Δf−∣∇f∣2+R)+f−n]uv = \big[\tau(2\Delta f - |\nabla f|^2 + R) + f - n\big]u satisfies

□∗v=−2τ∣Ric⁡+∇2f−12τg∣2u.\square^*v = -2\tau\Big|\operatorname{Ric} + \nabla^2f - \frac{1}{2\tau}g\Big|^2u.

Perelman's proof is "routine computation", and it is a long one; the expositions write it out. Integrated over a closed manifold it gives the monotonicity of W\mathcal W (12A.3 The 𝓦-Entropy), since ∫v dV=W\int v\,dV = \mathcal W. Its advantage is that it holds pointwise, so it can be combined with cut-off functions.

Corollary 6.2 v≤0v \leq 0 (Perelman I, Corollary 9.3)

On a closed manifold, or whenever the maximum principle can be justified, if uu tends to a δ\delta-function as t→Tt \to T, then v≤0v \leq 0 for all t<Tt < T.

Proof. For a positive solution hh of the forward heat equation ∂th=Δh\partial_th = \Delta h along the flow, ddt∫hu dV=0\frac{d}{dt}\int hu\,dV = 0 and ddt∫hv dV=∫h⋅2τ∣⋯∣2u dV≥0\frac{d}{dt}\int hv\,dV = \int h\cdot2\tau|\cdots|^2u\,dV \geq 0 (Exercise 6.6). So ∫hv\int hv at time tt is at most its limit as t→Tt \to T, and Perelman says it is easy to see that this limit is 00. The reason is that near the δ\delta-function, uu looks like the Euclidean heat kernel, for which v=0v = 0 (Exercise 6.5). Since hh can be any positive function at time tt, v≤0v \leq 0 there.

The inequality v≤0v \leq 0 is the Ricci flow analogue of the Li–Yau inequality (6A.10 Entropy, Information and Diffusion). Both are one-sided bounds on a second-order expression in log⁡u\log u for a fundamental solution, with equality for the Gaussian. Li–Yau integrated theirs along paths to compare values of uu at different points and times, and Perelman does the same.

Corollary 6.3 Harnack along curves (Perelman I, Corollaries 9.4 and 9.5)

Under the assumptions of Corollary 6.2, for every smooth curve γ(t)\gamma(t),

−ddtf(γ(t),t)≤12(R(γ(t),t)+∣γ˙(t)∣2)−12τf(γ(t),t).-\frac{d}{dt}f(\gamma(t), t) \leq \frac12\big(R(\gamma(t), t) + |\dot\gamma(t)|^2\big) - \frac{1}{2\tau}f(\gamma(t), t).

If the δ\delta-function is at pp, then f(q,t)≤ℓ(q,T−t)f(q, t) \leq \ell(q, T - t), where ℓ\ell is the reduced distance from (p,T)(p, T) (12A.5 Reduced Distance and Reduced Volume).

The first part is an algebraic consequence of v≤0v \leq 0 (Exercise 6.7). In backward time it says ddτ(2τf)≤τ(R+∣γ˙∣2)\frac{d}{d\tau}\big(2\sqrt\tau f\big) \leq \sqrt\tau(R + |\dot\gamma|^2), so integrating along a curve gives 2τˉf≤L(γ)2\sqrt{\bar\tau}f \leq \mathcal L(\gamma), which is why the second part holds. Perelman proves it directly: (4πτ)−n/2e−ℓ(4\pi\tau)^{-n/2}e^{-\ell} is a subsolution of the conjugate heat equation (12A.5 Reduced Distance and Reduced Volume), and the conjugate heat kernel lies above it. So e−ℓe^{-\ell} is a lower barrier for the heat kernel, the precise form of the least-action picture of 12A.5 Reduced Distance and Reduced Volume. Perelman adds a striking remark (9.6): among all evolutions ∂tg=A(t)\partial_tg = A(t) of a metric, the Ricci flow is characterised by how the fundamental solutions of the conjugate heat equation behave near their starting point.

Pseudolocality

Theorem 6.4 Pseudolocality (Perelman I, Theorem 10.1)

For every α>0\alpha > 0 there exist δ>0\delta > 0 and ε>0\varepsilon > 0 with the following property. Let g(t)g(t), 0≤t≤(εr0)20 \leq t \leq (\varepsilon r_0)^2, be a smooth Ricci flow, and suppose that at t=0t = 0:

  • R(x)≥−r0−2R(x) \geq -r_0^{-2} for x∈B(x0,r0)x \in B(x_0, r_0), and
  • Vol⁡(∂Ω)n≥(1−δ)cnVol⁡(Ω)n−1\operatorname{Vol}(\partial\Omega)^n \geq (1 - \delta)c_n\operatorname{Vol}(\Omega)^{n-1} for every region Ω⊂B(x0,r0)\Omega \subset B(x_0, r_0), where cnc_n is the Euclidean isoperimetric constant.

Then

∣Rm⁡∣(x,t)≤αt+1(εr0)2whenever 0<t≤(εr0)2 and dist⁡g(t)(x,x0)<εr0.|\operatorname{Rm}|(x, t) \leq \frac{\alpha}{t} + \frac{1}{(\varepsilon r_0)^2} \qquad \text{whenever } 0 < t \leq (\varepsilon r_0)^2 \text{ and } \operatorname{dist}_{g(t)}(x, x_0) < \varepsilon r_0.

Read the quantifiers carefully. The constants δ\delta and ε\varepsilon depend only on α\alpha (and the dimension), not on the flow, the manifold or r0r_0. The hypotheses concern only the ball B(x0,r0)B(x_0, r_0) at time 00: no curvature bound is assumed there at all, only a lower bound on RR and almost-Euclidean isoperimetry. The conclusion concerns a smaller space-time region, of size εr0\varepsilon r_0 in space and (εr0)2(\varepsilon r_0)^2 in time (Figure 6.1). The statement is scale-invariant, so it is enough to prove it for r0=1r_0 = 1 (Exercise 6.8). Perelman states it for a smooth solution. In §7 he assumes that the manifold is closed or that the metrics are complete with bounded curvature, and some such standing assumption is needed for the maximum-principle arguments; the expositions make it explicit.

Figure 6.1. Pseudolocality (schematic, not to scale; ε\varepsilon is small). Almost-Euclidean data on B(x0,r0)B(x_0, r_0) at t=0t = 0 control the curvature on the shaded region of size εr0\varepsilon r_0 and duration (εr0)2(\varepsilon r_0)^2, whatever the flow does outside the ball.

Perelman draws two further statements. From the proof: under the same hypotheses, Vol⁡B(x,t)≥c(n)tn\operatorname{Vol}B(x, \sqrt t) \geq c(n)\sqrt t^n at time tt for x∈B(x0,εr0)x \in B(x_0, \varepsilon r_0) (Corollary 10.2), a noncollapsing statement at all small scales. And a variant (Theorem 10.3): if at t=0t = 0, ∣Rm⁡∣≤r0−2|\operatorname{Rm}| \leq r_0^{-2} on B(x0,r0)B(x_0, r_0) and Vol⁡B(x0,r0)≥(1−δ)ωnr0n\operatorname{Vol}B(x_0, r_0) \geq (1 - \delta)\omega_nr_0^n, then ∣Rm⁡∣≤(εr0)−2|\operatorname{Rm}| \leq (\varepsilon r_0)^{-2} for 0≤t≤(εr0)20 \leq t \leq (\varepsilon r_0)^2 and dist⁡t(x,x0)<εr0\operatorname{dist}_t(x, x_0) < \varepsilon r_0. Perelman leaves its proof, "a slight modification", to the reader, and asks whether the volume assumption can be dropped.

The architecture of the proof

The proof is by contradiction and compactness, the [CC] template in its most elaborate form so far. Figure 6.2 sets out the steps; here is what each does.

  1. Suppose it fails. Scale to r0=1r_0 = 1 and take sequences ε,δ→0\varepsilon, \delta \to 0 of flows violating the conclusion.
  2. Point picking (Claims 1–2). Starting from a bad point, move to points of larger curvature until reaching a point (xˉ,tˉ)(\bar x, \bar t) with Q=∣Rm⁡∣(xˉ,tˉ)≥αtˉ−1Q = |\operatorname{Rm}|(\bar x, \bar t) \geq \alpha\bar t^{-1} such that ∣Rm⁡∣≤4Q|\operatorname{Rm}| \leq 4Q on a backward parabolic neighbourhood of radius 110AQ−1/2\frac{1}{10}AQ^{-1/2} in space and duration 12αQ−1\frac12\alpha Q^{-1} in time, where AA is a large constant. The search must end, because curvature quadruples at each step and the flow is smooth; Lemma 8.3(b), on how distances change, keeps the neighbourhood inside the region.
  3. The conjugate heat kernel. Let uu be the conjugate heat kernel starting from a δ\delta-function at (xˉ,tˉ)(\bar x, \bar t), and v≤0v \leq 0 its function from Corollary 6.2.
  4. vv is definitely negative near (xˉ,tˉ)(\bar x, \bar t) (Claim 3). At some time t~\tilde t slightly before tˉ\bar t, ∫Bv≤−β<0\int_Bv \leq -\beta < 0 on a small ball BB about xˉ\bar x. Otherwise, rescaling by QQ and passing to a limit, (9.1) would make the limit a gradient shrinking soliton, which Perelman notes is incompatible with ∣Rm⁡∣(xˉ,tˉ)=1|\operatorname{Rm}|(\bar x, \bar t) = 1. If instead the rescaled metrics collapse, one rescales differently, towards a flat limit, and can arrange ∫Bv→−∞\int_Bv \to -\infty.
  5. Carry this back to t=0t = 0. With a cut-off function hh built from the distance to x0x_0 (Lemma 8.3(a) controls □h\square h), the formula for □∗v\square^*v gives ∫−hv≥β(1−A−2)\int -hv \geq \beta(1 - A^{-2}) at t=0t = 0, while ∫hu≥1−A−2\int hu \geq 1 - A^{-2}.
  6. Contradict log-Sobolev. At t=0t = 0, u~=hu\tilde u = hu is nearly a probability density, supported in the almost-Euclidean ball. Rescale by 12tˉ−1\frac12\bar t^{-1}, so that τ\tau becomes 12\frac12. In the limit ε,δ→0\varepsilon, \delta \to 0 the balls become large, the scalar curvature term disappears, and W\mathcal W of u~\tilde u at τ=12\tau = \frac12 stays below a negative constant. The isoperimetric constants tend to the Euclidean one, so spherical symmetrisation moves these functions to Euclidean space without spoiling the estimate. That contradicts Gross's inequality (12A.3 The 𝓦-Entropy).

Every tool of Book 12A appears: the entropy and its link to log-Sobolev (step 6), the pointwise Harnack formula (steps 3–5), compactness and the soliton equality case (step 4), and noncollapsing in the alternative of step 4.

Figure 6.2. The proof of pseudolocality (schematic), following Perelman's Claims 1–3 and the final argument of §10.1.

Where it is used

Pseudolocality controls a region from information at an earlier time, locally, which is exactly what surgery needs. In Perelman's second preprint, Theorem 10.1 is applied to show that the standard solution, the model flow glued in at surgery, exists until its natural extinction time (II, §2), and the point-picking argument of its proof reappears in the analysis of the long-time behaviour (II, §6).

Recall Book 12A in one paragraph

Perelman's preprints are short and dense; read them with the expositions, statement by statement (12A.1 How to Read Perelman). The Ricci flow, modified by diffeomorphisms, is the gradient flow of F=∫(R+∣∇f∣2)e−fdV\mathcal F = \int(R + |\nabla f|^2)e^{-f}dV, which is nondecreasing, with λ\lambda the bottom eigenvalue of −4Δ+R-4\Delta + R; there are no steady or expanding breathers (12A.2 Ricci Flow as a Gradient Flow). Adding a scale τ\tau gives the entropy W\mathcal W, scale-invariant and nondecreasing, constant only on shrinking solitons; on Rn\mathbb{R}^n, μ=0\mu = 0 is Gross's log-Sobolev inequality, and there are no shrinking breathers (12A.3 The 𝓦-Entropy). A cut-off on a collapsed ball makes μ\mu very negative, so a Ricci flow on a closed manifold over a finite time interval is κ\kappa-noncollapsed below any fixed scale: blow-up limits exist and the cigar is excluded (12A.4 κ-Noncollapsing). The L\mathcal L-length gives a reduced distance and a reduced volume, monotone for every Ricci flow, Bishop–Gromov in space-time, which proves a local noncollapsing theorem (12A.5 Reduced Distance and Reduced Volume). The conjugate heat kernel satisfies Perelman's Harnack inequality v≤0v \leq 0, and almost-Euclidean regions stay tame for a definite time: pseudolocality (this chapter).

Where this goes Into Book 12B

Book 12A gave Perelman's tools. Book 12B uses them to understand high curvature in dimension three. Blow-up limits are ancient, κ\kappa-noncollapsed solutions with nonnegative curvature: κ\kappa-solutions (12B.1 κ-Solutions). Their structure, necks, caps and compact quotients of spheres (12B.2 The Structure of κ-Solutions), gives the canonical neighbourhood theorem: every point of high curvature in any three-dimensional Ricci flow looks like one of them (12B.3 The Canonical Neighbourhood Theorem). That is what makes surgery possible (12B.4 Surgery, 12B.5 Ricci Flow with Surgery for All Time).

History

Li and Yau proved their differential Harnack inequality in 1986, and Hamilton used Harnack inequalities for the backward heat equation to prove monotonicity formulas for parabolic flows; Klaus Ecker obtained a local monotonicity formula for mean curvature flow with solutions of the backward heat equation. Perelman cites all three in §9.7*. Pseudolocality is §10 of the first preprint (2002). Perelman interpreted it in terms of his renormalisation-group picture: a region that looks trivial at a higher energy scale cannot suddenly become highly nontrivial at a slightly lower one.

Exercises

Exercise 6.5 v=0v = 0 for the Gaussian

On static flat Rn\mathbb{R}^n, let u=(4πτ)−n/2e−∣x∣2/4τu = (4\pi\tau)^{-n/2}e^{-|x|^2/4\tau} with τ=T−t\tau = T - t. Check that uu solves the conjugate heat equation, and that v=[τ(2Δf−∣∇f∣2)+f−n]u=0v = \big[\tau(2\Delta f - |\nabla f|^2) + f - n\big]u = 0.

Solution

With R=0R = 0, □∗u=−∂tu−Δu=∂τu−Δu=0\square^*u = -\partial_tu - \Delta u = \partial_\tau u - \Delta u = 0, the heat equation in τ\tau. With f=∣x∣24τf = \frac{|x|^2}{4\tau}: 2Δf=nτ2\Delta f = \frac n\tau, ∣∇f∣2=∣x∣24τ2|\nabla f|^2 = \frac{|x|^2}{4\tau^2}, so τ(2Δf−∣∇f∣2)+f−n=n−∣x∣24τ+∣x∣24τ−n=0\tau(2\Delta f - |\nabla f|^2) + f - n = n - \frac{|x|^2}{4\tau} + \frac{|x|^2}{4\tau} - n = 0.

Exercise 6.6 The duality of □\square and □∗\square^*

Let □h=∂th−Δh\square h = \partial_th - \Delta h and □∗w=−∂tw−Δw+Rw\square^*w = -\partial_tw - \Delta w + Rw along a Ricci flow on a closed manifold. Using ∂t dV=−R dV\partial_t\,dV = -R\,dV, show ddt∫hw dV=∫((□h)w−h(□∗w))dV\frac{d}{dt}\int hw\,dV = \int\big((\square h)w - h(\square^*w)\big)dV. Deduce that if □h=0\square h = 0, then ddt∫hu=0\frac{d}{dt}\int hu = 0 and ddt∫hv=∫2τh∣Ric⁡+∇2f−g2τ∣2u≥0\frac{d}{dt}\int hv = \int2\tau h|\operatorname{Ric} + \nabla^2f - \frac{g}{2\tau}|^2u \geq 0 when h>0h > 0.

Solution

ddt∫hw=∫(htw+hwt−Rhw)\frac{d}{dt}\int hw = \int(h_tw + hw_t - Rhw). And ∫(□h)w−h□∗w=∫(htw−wΔh+hwt+hΔw−Rhw)\int(\square h)w - h\square^*w = \int(h_tw - w\Delta h + hw_t + h\Delta w - Rhw), where ∫(hΔw−wΔh)=0\int(h\Delta w - w\Delta h) = 0. With w=uw = u, □∗u=0\square^*u = 0; with w=vw = v, −h□∗v=2τh∣⋯∣2u-h\square^*v = 2\tau h|\cdots|^2u.

Exercise 6.7 Harnack along a curve

Using ∂tf=−Δf+∣∇f∣2−R+n2τ\partial_tf = -\Delta f + |\nabla f|^2 - R + \frac{n}{2\tau} and v≤0v \leq 0, show that ∂tf+12R−12∣∇f∣2−f2τ≥0\partial_tf + \frac12R - \frac12|\nabla f|^2 - \frac{f}{2\tau} \geq 0. Then use −ddtf(γ(t),t)=−∂tf−⟨∇f,γ˙⟩≤−∂tf+12∣∇f∣2+12∣γ˙∣2-\frac{d}{dt}f(\gamma(t), t) = -\partial_tf - \langle\nabla f, \dot\gamma\rangle \leq -\partial_tf + \frac12|\nabla f|^2 + \frac12|\dot\gamma|^2 to derive the inequality of Corollary 6.3.

Solution

v≤0v \leq 0 gives Δf≤12(∣∇f∣2−R)+n−f2τ\Delta f \leq \frac12(|\nabla f|^2 - R) + \frac{n - f}{2\tau}. Then ∂tf≥−12(∣∇f∣2−R)−n−f2τ+∣∇f∣2−R+n2τ=12∣∇f∣2−12R+f2τ\partial_tf \geq -\frac12(|\nabla f|^2 - R) - \frac{n - f}{2\tau} + |\nabla f|^2 - R + \frac{n}{2\tau} = \frac12|\nabla f|^2 - \frac12R + \frac{f}{2\tau}. So −∂tf≤12R−12∣∇f∣2−f2τ-\partial_tf \leq \frac12R - \frac12|\nabla f|^2 - \frac{f}{2\tau}, and adding −⟨∇f,γ˙⟩≤12∣∇f∣2+12∣γ˙∣2-\langle\nabla f, \dot\gamma\rangle \leq \frac12|\nabla f|^2 + \frac12|\dot\gamma|^2 gives −ddtf≤12(R+∣γ˙∣2)−f2τ-\frac{d}{dt}f \leq \frac12(R + |\dot\gamma|^2) - \frac{f}{2\tau}.

Exercise 6.8 Quantifiers and scaling

(a) Write the statement of pseudolocality as a single sentence beginning "For every α>0\alpha > 0 there exist", and say what each constant may depend on. (b) Show that if the theorem holds for r0=1r_0 = 1, it holds for all r0r_0, by applying it to g~(t)=r0−2g(r02t)\tilde g(t) = r_0^{-2}g(r_0^2t). (c) Explain why the theorem would be useless if ε\varepsilon were allowed to depend on the flow.

Solution

(a) For every α>0\alpha > 0 there exist δ,ε>0\delta, \varepsilon > 0, depending only on α\alpha and nn, such that for every r0>0r_0 > 0 and every smooth Ricci flow on [0,(εr0)2][0, (\varepsilon r_0)^2] satisfying the two hypotheses on B(x0,r0)B(x_0, r_0) at t=0t = 0, the curvature bound holds for all (x,t)(x, t) with 0<t≤(εr0)20 < t \leq (\varepsilon r_0)^2 and dist⁡t(x,x0)<εr0\operatorname{dist}_t(x, x_0) < \varepsilon r_0. (b) g~\tilde g is a Ricci flow; R~=r02R≥−1\tilde R = r_0^2R \geq -1 on B~(x0,1)\tilde B(x_0, 1); isoperimetric ratios are scale-invariant; and ∣Rm⁡~∣(x,s)=r02∣Rm⁡∣(x,r02s)≤αs+ε−2|\widetilde{\operatorname{Rm}}|(x, s) = r_0^2|\operatorname{Rm}|(x, r_0^2s) \leq \frac\alpha s + \varepsilon^{-2} translates to the bound for gg at t=r02st = r_0^2s. (c) In applications the flow is unknown (it is the flow with surgery, near some point); the theorem gives control from local initial data alone only because ε\varepsilon and δ\delta are universal.

Exercise 6.9 Rehearsal: a sanity check on the sphere

Let g(t)g(t) be the round shrinking SnS^n with radius ρ\rho at t=0t = 0, so g(t)=(1−2(n−1)t/ρ2)g(0)g(t) = (1 - 2(n - 1)t/\rho^2)g(0), and take r0≤ρr_0 \leq \rho. (a) Check the hypothesis R≥−r0−2R \geq -r_0^{-2}. (b) Explain why, as r0/ρ→0r_0/\rho \to 0, the isoperimetric hypothesis holds on B(x0,r0)B(x_0, r_0) for any fixed δ\delta. (c) Show directly that for t≤(εr0)2t \leq (\varepsilon r_0)^2 with ε≤12n−1\varepsilon \leq \frac{1}{2\sqrt{n - 1}}, the sectional curvature is at most 2ρ2\frac{2}{\rho^2}, which is at most (εr0)−2(\varepsilon r_0)^{-2}. Which part of the conclusion is doing no work here?

Solution

(a) R=n(n−1)ρ2>0R = \frac{n(n - 1)}{\rho^2} > 0. (b) Small balls on a smooth manifold are nearly Euclidean, with isoperimetric constants tending to the Euclidean one as the radius shrinks relative to the curvature scale. (c) The sectional curvature at time tt is (ρ2−2(n−1)t)−1\big(\rho^2 - 2(n - 1)t\big)^{-1}. Since 2(n−1)t≤2(n−1)ε2r02≤r022≤ρ222(n - 1)t \leq 2(n - 1)\varepsilon^2r_0^2 \leq \frac{r_0^2}{2} \leq \frac{\rho^2}{2}, it is at most 2ρ2≤2r02\frac2{\rho^2} \leq \frac{2}{r_0^2}, and 2r02≤(εr0)−2\frac2{r_0^2} \leq (\varepsilon r_0)^{-2} because ε2≤14<12\varepsilon^2 \leq \frac14 < \frac12. The term αt\frac\alpha t does no work: it matters only when curvature can be large at small times, which a smooth flow with bounded curvature never needs.

© 2026 NeckPinch (www.neckpinch.com). All content in the guidebook (text, mathematics, figures and exercises) is protected by copyright. All rights reserved. No part may be copied, republished or redistributed without written permission.