Book 6A

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Course 6Book 6A: The Heat Equation and Its RelativesChapter 13

Self-Similar Variables and Monotonicity

Changing variables so that self-similar solutions stand still: convergence to the Gaussian, Giga–Kohn blow-up, Gaussian-weighted monotonicity formulas, frequency functions, and the blow-up logic of Huisken, Struwe and Perelman.

57 min read · Updated Oct 23, 2026

None of the Path's books covers this chapter as a whole; it collects one idea from several sources. Giga and Kohn, "Asymptotically self-similar blow-up of semilinear heat equations" (Comm. Pure Appl. Math. 38, 1985), introduced the method for semilinear equations; Huisken, "Asymptotic behavior for singularities of the mean curvature flow" (J. Differential Geom. 31, 1990), for mean curvature flow; Struwe, "On the evolution of harmonic maps in higher dimensions" (J. Differential Geom. 28, 1988), for harmonic map flow. Mantegazza's Lecture Notes on Mean Curvature Flow (2011), chapters 3–4, and Quittner and Souplet's Superlinear Parabolic Problems (2nd edition, 2019), chapter II, are book-length references. Bakry, Gentil and Ledoux, Analysis and Geometry of Markov Diffusion Operators (2014), chapter 4, treats the Gaussian Poincaré inequality. For Perelman's version read Morgan and Tian, Ricci Flow and the Poincaré Conjecture, chapters 6–9, alongside 12A.3 The 𝓦-Entropy–12A.5 Reduced Distance and Reduced Volume and 12B.1 κ-Solutions.

In this chapter · 8 sections
  1. 13.1Self-similar solutions
  2. 13.2Forward self-similar variables: every solution becomes the Gaussian
  3. 13.3Backward self-similar variables and the Giga–Kohn functional
  4. 13.4Monotonicity formulas are weighted energy identities
  5. 13.5Frequency functions and unique continuation
  6. 13.6The blow-up argument, step by step
  7. 13.7History
  8. 13.8Exercises
  9. ↗Free resources

6A.12 Entropy, Information and Diffusion ended with a template. A monotone quantity along a flow, such as an entropy, has an equality case, and the equality case is a self-similar solution: the Gaussian for the heat equation, a self-shrinker for mean curvature flow, a shrinking soliton for the Ricci flow. So if a limit of rescalings near a singularity makes the monotone quantity constant, the limit is self-similar. That one sentence is the logical core of Perelman's analysis of singularities, and it hides three pieces of mathematics that this chapter makes explicit.

The first is a change of variables in which self-similar solutions stand still. Self-similar solutions are fixed points of the scaling symmetry; after dividing out the scaling, by measuring space in units of t\sqrt{t} or T−t\sqrt{T - t} and time logarithmically, they become stationary solutions of a new equation. The second is the discovery that in these variables many flows become gradient flows in a Gaussian-weighted space, so that their energies are automatically monotone: the monotonicity formulas of Huisken, Giga–Kohn and Struwe are nothing but the energy identity of a gradient flow, written in the original variables. The third is the blow-up argument: a bounded monotone quantity has a limit, so its derivative is integrable, so along a sequence the time derivative of the rescaled solution tends to zero, so the limit is stationary in the rescaled variables, that is, self-similar in the original ones.

We do this first for the linear heat equation, where everything is explicit and the self-similar variables turn the heat equation into the Ornstein–Uhlenbeck equation, whose spectrum is the Hermite spectrum; then for the semilinear heat equation of 6A.8 Nonlinear Parabolic Equations, following Yoshikazu Giga and Robert Kohn; then for mean curvature flow, where Huisken's formula of 6A.10 Curve Shortening and the First Geometric Flows reappears as the energy identity of a weighted area; and finally for the Ricci flow, where Perelman's W\mathcal W-entropy and reduced volume play the same role, in the form in which Morgan and Tian present them.

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

  • classify self-similar solutions of the heat equation as forward, backward and translating, and give their geometric-flow analogues;
  • transform the heat equation into forward self-similar variables, recognise the Fokker–Planck form with the Gaussian as equilibrium, and prove convergence to the Gaussian at the rate t−1/2t^{-1/2};
  • prove the Gaussian Poincaré inequality with its sharp constant from the Mehler formula, and compute the Hermite spectrum of the Ornstein–Uhlenbeck operator;
  • write the semilinear heat equation in backward self-similar variables, prove that it is a gradient flow in L2(ρ dy)L^2(\rho\,dy) with the Giga–Kohn Lyapunov functional, and explain what this says about blow-up profiles;
  • derive Struwe-type monotonicity for the heat equation and read Huisken's formula as a weighted energy identity;
  • prove monotonicity of Poon's parabolic frequency and explain its relation to unique continuation;
  • describe Colding–Minicozzi entropy and White's regularity theorem, and lay out the blow-up argument step by step;
  • match each step to its counterpart in Perelman's work and in Morgan–Tian.

Self-similar solutions

The heat equation ut=Δuu_t = \Delta u on Rn\mathbb{R}^n is invariant under the parabolic dilations uλ(x,t)=u(λx,λ2t)u_\lambda(x, t) = u(\lambda x, \lambda^2t), and, being linear, under multiplication by constants. A solution is self-similar if dilation maps it to a multiple of itself: u(λx,λ2t)=λ−au(x,t)u(\lambda x, \lambda^2t) = \lambda^{-a}u(x, t) for all λ>0\lambda > 0 and some exponent aa. Setting λ=t−1/2\lambda = t^{-1/2} shows that such a solution has the form

u(x,t)=t−a/2V(xt),u(x, t) = t^{-a/2}V\Big(\frac{x}{\sqrt t}\Big),

a fixed profile VV that spreads as t\sqrt t and changes height as t−a/2t^{-a/2}. The heat kernel is the case a=na = n, V(y)=(4π)−n/2e−∣y∣2/4V(y) = (4\pi)^{-n/2}e^{-|y|^2/4}. Self-similar solutions come in three kinds, according to how they sit in time, and each has counterparts for the geometric flows.

kind form heat equation mean curvature flow Ricci flow
forward (expanding) t−a/2V(x/t)t^{-a/2}V(x/\sqrt t), t>0t > 0 heat kernel; data homogeneous of degree −a-a expanders coming out of cones expanding solitons; the Gaussian soliton
backward (shrinking) (T−t)−a/2V(x/T−t)(T - t)^{-a/2}V(x/\sqrt{T - t}), t<Tt < T solutions blowing up at time TT self-shrinkers: spheres, cylinders shrinking solitons: spheres, cylinders
translating (steady) ectV(x−c′t)e^{ct}V(x - c't) or V(x−ct)V(x - ct) travelling waves (6A.9 Reaction–Diffusion: Fronts, Patterns and Pinching) the grim reaper (6A.10 Curve Shortening and the First Geometric Flows) steady solitons: the cigar, Bryant's soliton

Forward self-similar solutions describe how a solution forgets its initial data; backward ones describe how it approaches a singularity; translating ones are eternal and appear as limits of type II singularities (6A.8 Nonlinear Parabolic Equations, 11B.5 Singularities). The Ricci flow column is where the guide is going: shrinking solitons are the models of type I singularities, and Perelman proved that his κ\kappa-solutions look, at very large scales, like shrinking solitons (12B.1 κ-Solutions).

Homogeneous data give self-similar solutions. If u0(x)=∣x∣−au_0(x) = |x|^{-a} with 0<a<n0 < a < n, then u0(λx)=λ−au0(x)u_0(\lambda x) = \lambda^{-a}u_0(x); the solution u=Φ(⋅,t)∗u0u = \Phi(\cdot, t)*u_0 satisfies u(λx,λ2t)=λ−au(x,t)u(\lambda x, \lambda^2t) = \lambda^{-a}u(x, t) because both sides solve the heat equation with the same initial data, and the solution is unique in the class of 6A.3 The Heat Equation on ℝⁿ (Exercise 13.10). This is the simplest instance of a general principle: a scale-invariant problem has scale-invariant solutions, provided its solutions are unique. The same principle produces Ricci expanders out of Euclidean cones, and it fails exactly when uniqueness fails.

Forward self-similar variables: every solution becomes the Gaussian

To divide out the scaling, measure space in units of t\sqrt t and time by its logarithm:

y=xt,τ=log⁡t,u(x,t)=t−n/2v(y,τ).y = \frac{x}{\sqrt t}, \qquad \tau = \log t, \qquad u(x, t) = t^{-n/2}v(y, \tau).

The prefactor t−n/2t^{-n/2} preserves mass: ∫u(x,t) dx=∫v(y,τ) dy\int u(x, t)\,dx = \int v(y, \tau)\,dy. A short computation (Exercise 13.6) gives

vτ=Δv+y2⋅∇v+n2v=div⁡(∇v+y2v).v_\tau = \Delta v + \frac y2\cdot\nabla v + \frac n2v = \operatorname{div}\Big(\nabla v + \frac y2v\Big).

This is a Fokker–Planck equation (6D.3 Stochastic Differential Equations and Feynman–Kac): the heat equation with a drift that pushes mass towards the origin with velocity −y2-\frac y2, exactly compensating the spreading. Its stationary solutions with finite mass are the multiples of

G(y)=(4π)−n/2e−∣y∣2/4,G(y) = (4\pi)^{-n/2}e^{-|y|^2/4},

because ∇G+y2G=0\nabla G + \frac y2G = 0. In the new variables the heat kernel is a fixed point, and the question "does every solution look like the heat kernel for large time?" becomes "does every solution of this equation converge to its equilibrium?"

To answer it, write v=Gfv = Gf. Since ∇v+y2v=G∇f\nabla v + \frac y2v = G\nabla f, the equation becomes

fτ=1Gdiv⁡(G∇f)=Δf−y2⋅∇f=:Lf,f_\tau = \frac1G\operatorname{div}(G\nabla f) = \Delta f - \frac y2\cdot\nabla f =: Lf,

the Ornstein–Uhlenbeck equation. The operator LL is symmetric in L2(G dy)L^2(G\,dy), by the integration by parts ∫(Lf)h G=−∫∇f⋅∇h G\int(Lf)h\,G = -\int\nabla f\cdot\nabla h\,G, and nonpositive. Constants are in its kernel. Convergence to equilibrium is the decay of f−Mf - M, where M=∫fG=∫vM = \int fG = \int v is the conserved mass, and the rate is the spectral gap of −L-L. The gap is the best constant in a Poincaré inequality for the Gaussian measure.

Theorem 13.1 Gaussian Poincaré inequality

For every ff with ∫(f2+∣∇f∣2)G dy<∞\int(f^2 + |\nabla f|^2)G\,dy < \infty,

∫f2G dy−(∫fG dy)2≤2∫∣∇f∣2G dy,\int f^2G\,dy - \Big(\int fG\,dy\Big)^2 \leq 2\int|\nabla f|^2G\,dy,

with equality for f(y)=a+b⋅yf(y) = a + b\cdot y. So the spectral gap of −L-L in L2(G dy)L^2(G\,dy) is 12\frac12.

The constant 22 is the variance of each coordinate under GG, and the inequality, unlike the Poincaré inequality on a bounded domain (4A.10 Sobolev Spaces), has a constant independent of the dimension. The proof uses the explicit solution of the Ornstein–Uhlenbeck equation, the Mehler formula

(Psf)(y)=∫f(e−s/2y+1−e−s z)G(z) dz,(P_sf)(y) = \int f\big(e^{-s/2}y + \sqrt{1 - e^{-s}}\,z\big)G(z)\,dz,

which solves ∂sPsf=LPsf\partial_sP_sf = LP_sf with P0f=fP_0f = f (Exercise 13.7). It says that the Ornstein–Uhlenbeck process started at yy is, at time ss, a Gaussian centred at e−s/2ye^{-s/2}y: the drift pulls the starting point in, the noise spreads it out, and as s→∞s \to \infty the distribution becomes GG whatever the start.

Proof. Two properties of PsP_s are read off the formula. First, Psf→∫fGP_sf \to \int fG as s→∞s \to \infty and ∫(Psf)G=∫fG\int(P_sf)G = \int fG for all ss (the measure GG is invariant). Second, differentiating under the integral,

∇Psf=e−s/2Ps(∇f),so∣∇Psf∣≤e−s/2Ps∣∇f∣.\nabla P_sf = e^{-s/2}P_s(\nabla f), \qquad\text{so}\qquad |\nabla P_sf| \leq e^{-s/2}P_s|\nabla f|.

Now dds∫(Psf)2G=2∫(Psf)(LPsf)G=−2∫∣∇Psf∣2G\frac{d}{ds}\int(P_sf)^2G = 2\int(P_sf)(LP_sf)G = -2\int|\nabla P_sf|^2G. Integrating from 00 to ∞\infty,

∫f2G−(∫fG)2=2∫0∞ ⁣ ⁣∫∣∇Psf∣2G dy ds≤2∫0∞e−s∫(Ps∣∇f∣)2G dy ds.\int f^2G - \Big(\int fG\Big)^2 = 2\int_0^\infty\!\!\int|\nabla P_sf|^2G\,dy\,ds \leq 2\int_0^\infty e^{-s}\int\big(P_s|\nabla f|\big)^2G\,dy\,ds.

By Jensen's inequality, (Psh)2≤Ps(h2)(P_sh)^2 \leq P_s(h^2), since PsP_s averages against a probability measure, and by invariance ∫Ps(h2)G=∫h2G\int P_s(h^2)G = \int h^2G. So the inner integral is at most ∫∣∇f∣2G\int|\nabla f|^2G, and ∫0∞e−sds=1\int_0^\infty e^{-s}ds = 1 gives the inequality. For f=a+b⋅yf = a + b\cdot y: ∫fG=a\int fG = a, ∫f2G−a2=∫(b⋅y)2G=2∣b∣2\int f^2G - a^2 = \int(b\cdot y)^2G = 2|b|^2, and 2∫∣∇f∣2G=2∣b∣22\int|\nabla f|^2G = 2|b|^2.

Proposition 13.2 Convergence to the Gaussian

Let uu solve the heat equation on Rn\mathbb{R}^n with initial data u(⋅,1)=u1u(\cdot, 1) = u_1 at time 11 such that ∫u12e∣x∣2/4 dx<∞\int u_1^2e^{|x|^2/4}\,dx < \infty, and let M=∫u1M = \int u_1. Then for t≥1t \geq 1,

∫(u(x,t)−MΦ(x,t))2 dxΦ(x,t)≤1t∫(u1−MΦ(⋅,1))2 dxΦ(⋅,1).\int\big(u(x, t) - M\Phi(x, t)\big)^2\,\frac{dx}{\Phi(x, t)} \leq \frac1t\int\big(u_1 - M\Phi(\cdot, 1)\big)^2\,\frac{dx}{\Phi(\cdot, 1)}.

Proof. In forward variables with τ=log⁡t\tau = \log t, u(x,t)=t−n/2G(y)f(y,τ)u(x, t) = t^{-n/2}G(y)f(y, \tau) and Φ(x,t)=t−n/2G(y)\Phi(x, t) = t^{-n/2}G(y). Changing variables, the left side is ∫(f−M)2G dy\int(f - M)^2G\,dy at time τ\tau, and the hypothesis says it is finite at τ=0\tau = 0. Since f−Mf - M solves fτ=Lff_\tau = Lf and has mean zero against GG (mass is conserved),

ddτ∫(f−M)2G=−2∫∣∇f∣2G≤−∫(f−M)2G\frac{d}{d\tau}\int(f - M)^2G = -2\int|\nabla f|^2G \leq -\int(f - M)^2G

by Theorem 13.1. So ∫(f−M)2G\int(f - M)^2G decays like e−τ=1te^{-\tau} = \frac1t.

The rate is sharp: a solution whose centre of mass is not at the origin, such as the heat kernel started at a point x0≠0x_0 \neq 0, differs from MΦM\Phi at relative order ∣x0∣t\frac{|x_0|}{\sqrt t}, which is the first Hermite mode f−M∝yf - M \propto y decaying like e−τ/2e^{-\tau/2}. Subtracting the right Gaussian (centred at the centre of mass) improves the rate to t−1t^{-1}, the next eigenvalue. This is the PDE form of the central limit theorem: the heat equation is the law of Brownian motion (6A.3 The Heat Equation on ℝⁿ), and its convergence to the Gaussian, with the corrections organised by the Hermite spectrum, is the Edgeworth expansion of probability. The relative entropy version, with the log-Sobolev inequality in place of the Poincaré inequality, is the entropy production argument of 6A.12 Entropy, Information and Diffusion.

The Hermite spectrum. The eigenfunctions of −L-L are the Hermite polynomials adapted to GG: in one dimension, H0=1H_0 = 1, H1=yH_1 = y, H2=y2−2H_2 = y^2 - 2, H3=y3−6yH_3 = y^3 - 6y, ..., with −LHk=k2Hk-LH_k = \frac k2H_k (Exercise 13.8), and in nn dimensions products of these, with eigenvalue half the total degree. The eigenvalue k2\frac k2 corresponds, back in the original variables, to a correction decaying like t−k/2t^{-k/2} relative to the Gaussian. In the backward variables of the next section the same eigenfunctions are the heat polynomials in disguise: xx, x2+2tx^2 + 2t, x3+6xtx^3 + 6xt, ..., the polynomial solutions of the heat equation, written for t<0t < 0 as (−t)k/2Hk(x/−t)(-t)^{k/2}H_k(x/\sqrt{-t}) (Exercise 13.8). Their appearance there is what makes the frequency function work.

Backward self-similar variables and the Giga–Kohn functional

Now consider a solution that becomes singular at time TT at the origin, and look at it on the scale of the singularity. For the semilinear equation

ut=Δu+∣u∣p−1u,p>1,u_t = \Delta u + |u|^{p-1}u, \qquad p > 1,

of 6A.8 Nonlinear Parabolic Equations, the spatially constant solution κ(T−t)−1/(p−1)\kappa(T - t)^{-1/(p-1)}, with κ=(p−1)−1/(p−1)\kappa = (p - 1)^{-1/(p-1)}, blows up at time TT at the ODE rate, and the equation is invariant under u↦λ2/(p−1)u(λx,λ2t)u \mapsto \lambda^{2/(p-1)}u(\lambda x, \lambda^2t). Giga and Kohn (1985) introduced the backward self-similar variables

y=xT−t,s=−log⁡(T−t),w(y,s)=(T−t)1/(p−1)u(x,t).y = \frac{x}{\sqrt{T - t}}, \qquad s = -\log(T - t), \qquad w(y, s) = (T - t)^{1/(p-1)}u(x, t).

As t↑Tt \uparrow T, s→∞s \to \infty, and the singularity at the origin is spread out over all of yy-space: a point at fixed yy approaches the origin at the rate T−t\sqrt{T - t}. A computation like the forward one (Exercise 13.9) gives

ws=Δw−y2⋅∇w−wp−1+∣w∣p−1w.w_s = \Delta w - \frac y2\cdot\nabla w - \frac{w}{p - 1} + |w|^{p-1}w.

The drift now points outward, −y2⋅∇w-\frac y2\cdot\nabla w, undoing the concentration of the singularity, and the constant solution of the ODE becomes the stationary solution w≡κw \equiv \kappa. The key observation is that the linear part is 1ρdiv⁡(ρ∇w)\frac1\rho\operatorname{div}(\rho\nabla w) with the Gaussian weight

ρ(y)=(4π)−n/2e−∣y∣2/4,\rho(y) = (4\pi)^{-n/2}e^{-|y|^2/4},

because ∇ρ=−y2ρ\nabla\rho = -\frac y2\rho. So the equation is the gradient flow, in L2(ρ dy)L^2(\rho\,dy), of the weighted energy below.

Theorem 13.3 The Giga–Kohn Lyapunov functional

Let

E[w]=∫Rn(12∣∇w∣2+w22(p−1)−∣w∣p+1p+1)ρ dy.E[w] = \int_{\mathbb{R}^n}\Big(\frac12|\nabla w|^2 + \frac{w^2}{2(p - 1)} - \frac{|w|^{p+1}}{p + 1}\Big)\rho\,dy.

Then along solutions of the rescaled equation (with enough decay for the integrations by parts),

ddsE[w(s)]=−∫ws2 ρ dy≤0.\frac{d}{ds}E[w(s)] = -\int w_s^2\,\rho\,dy \leq 0.

Proof. Differentiate under the integral and integrate the gradient term by parts against the weight:

ddsE=∫(∇w⋅∇ws+wwsp−1−∣w∣p−1wws)ρ=∫(−1ρdiv⁡(ρ∇w)+wp−1−∣w∣p−1w)ws ρ.\frac{d}{ds}E = \int\Big(\nabla w\cdot\nabla w_s + \frac{ww_s}{p - 1} - |w|^{p-1}ww_s\Big)\rho = \int\Big(-\frac1\rho\operatorname{div}(\rho\nabla w) + \frac{w}{p - 1} - |w|^{p-1}w\Big)w_s\,\rho.

The bracket is −ws-w_s, by the equation, since 1ρdiv⁡(ρ∇w)=Δw−y2⋅∇w\frac1\rho\operatorname{div}(\rho\nabla w) = \Delta w - \frac y2\cdot\nabla w.

Three consequences follow, and they are the template for everything after.

  1. Integrability of the time derivative. If EE is bounded below along the flow (Giga and Kohn prove this for blowing-up solutions; it is where real work is needed), then ∫s0∞ ⁣∫ws2ρ dy ds≤E[w(s0)]−lim⁡E<∞\int_{s_0}^\infty\!\int w_s^2\rho\,dy\,ds \leq E[w(s_0)] - \lim E < \infty. So ws→0w_s \to 0 in an averaged sense, and every limit of w(⋅,sk+⋅)w(\cdot, s_k + \cdot) along a sequence sk→∞s_k \to \infty is a stationary solution of the rescaled equation.
  2. Stationary means self-similar. A stationary solution w(y)w(y) corresponds to u=(T−t)−1/(p−1)w(x/T−t)u = (T - t)^{-1/(p-1)}w(x/\sqrt{T - t}), a backward self-similar solution. So the blow-up of uu at the origin is asymptotically self-similar.
  3. A Liouville theorem finishes it. Giga and Kohn proved (1985, 1987) that for 1<p<n+2n−21 < p < \frac{n + 2}{n - 2} (any p>1p > 1 if n≤2n \leq 2) the only bounded stationary solutions are 00 and ±κ\pm\kappa, using a Pohozaev identity (6C.3 Symmetry, Noether’s Theorem and Moving Planes). For positive solutions they also proved the type I bound u≤C(T−t)−1/(p−1)u \leq C(T - t)^{-1/(p-1)} in the same range (1987), so ww is bounded. Hence w(⋅,s)→κw(\cdot, s) \to \kappa (at a blow-up point) uniformly on compact sets: in self-similar variables the solution near the singularity is flat, and the singularity looks like the ODE.

The convergence w→κw \to \kappa is the precise form of the slogan of 6A.9 Reaction–Diffusion: Fronts, Patterns and Pinching, "near a singularity reaction wins". It also hides a finer structure: the convergence is only on compact sets of yy, that is, on regions of size O(T−t)O(\sqrt{T - t}) in xx, and the shape of the singular region is decided by a slowly decaying correction. Jean Bricmont and Antti Kupiainen (1994) and Frank Merle and Hatem Zaag (1997) showed that the generic profile is

w(y,s)≈(p−1+(p−1)24p∣y∣2s)−1/(p−1),w(y, s) \approx \Big(p - 1 + \frac{(p - 1)^2}{4p}\frac{|y|^2}{s}\Big)^{-1/(p-1)},

a flat top whose width grows like s=∣log⁡(T−t)∣\sqrt{s} = \sqrt{|\log(T - t)|} in self-similar variables. The logarithm comes from the Hermite mode H2H_2, whose eigenvalue for the linearisation at κ\kappa is zero: a neutral direction, along which the approach to the self-similar solution is only logarithmic. The same mechanism, with the same kind of logarithmic correction, governs the shape of the Ricci flow neckpinch analysed by Angenent and Knopf (11B.6 Rotationally Symmetric Flows and the Standard Solution).

Monotonicity formulas are weighted energy identities

Undo the change of variables in the Giga–Kohn identity and you get a statement about uu itself, a monotonicity formula in which the Gaussian weight has become the backward heat kernel centred at the singular point,

Φ(x0,T)(x,t)=1(4π(T−t))n/2e−∣x−x0∣2/4(T−t),t<T,\Phi_{(x_0, T)}(x, t) = \frac{1}{(4\pi(T - t))^{n/2}}e^{-|x - x_0|^2/4(T - t)}, \qquad t < T,

which solves the backward heat equation ∂tΦ+ΔΦ=0\partial_t\Phi + \Delta\Phi = 0 and concentrates at x0x_0 as t↑Tt \uparrow T. The simplest example is the linear heat equation itself.

Proposition 13.4 A monotonicity formula for the heat equation

Let uu solve ut=Δuu_t = \Delta u on Rn×(0,T)\mathbb{R}^n \times (0, T), with bounded derivatives. Then

ddt[(T−t)∫∣∇u∣2Φ(x0,T) dx]=−2(T−t)∫∣ut−(x−x0)⋅∇u2(T−t)∣2Φ(x0,T) dx≤0.\frac{d}{dt}\Big[(T - t)\int|\nabla u|^2\Phi_{(x_0, T)}\,dx\Big] = -2(T - t)\int\Big|u_t - \frac{(x - x_0)\cdot\nabla u}{2(T - t)}\Big|^2\Phi_{(x_0, T)}\,dx \leq 0.

The left side is constant exactly when uu is backward self-similar about (x0,T)(x_0, T) with exponent 00, that is, u(x,t)=V((x−x0)/T−t)u(x, t) = V\big((x - x_0)/\sqrt{T - t}\big).

Proof. Take x0=0x_0 = 0. In backward variables y=x/T−ty = x/\sqrt{T - t}, s=−log⁡(T−t)s = -\log(T - t) and w(y,s)=u(x,t)w(y, s) = u(x, t), the equation becomes ws=Δw−y2⋅∇w=1ρdiv⁡(ρ∇w)w_s = \Delta w - \frac y2\cdot\nabla w = \frac1\rho\operatorname{div}(\rho\nabla w), the gradient flow of 12∫∣∇w∣2ρ\frac12\int|\nabla w|^2\rho in L2(ρ)L^2(\rho), so dds12∫∣∇w∣2ρ=−∫ws2ρ\frac{d}{ds}\frac12\int|\nabla w|^2\rho = -\int w_s^2\rho. Translate back: ∇yw=T−t ∇xu\nabla_yw = \sqrt{T - t}\,\nabla_xu and ρ(y) dy=Φ(x,t) dx\rho(y)\,dy = \Phi(x, t)\,dx, so ∫∣∇yw∣2ρ dy=(T−t)∫∣∇u∣2Φ dx\int|\nabla_yw|^2\rho\,dy = (T - t)\int|\nabla u|^2\Phi\,dx; dsdt=1T−t\frac{ds}{dt} = \frac{1}{T - t}; and ws=(T−t)ut−x2⋅∇uw_s = (T - t)u_t - \frac{x}{2}\cdot\nabla u, since x=e−s/2yx = e^{-s/2}y and t=T−e−st = T - e^{-s} give ∂x∂s∣y=−x2\frac{\partial x}{\partial s}\big|_y = -\frac{x}{2} and ∂t∂s=T−t\frac{\partial t}{\partial s} = T - t. Then ∫ws2ρ dy=(T−t)2∫∣ut−x⋅∇u2(T−t)∣2Φ dx\int w_s^2\rho\,dy = (T - t)^2\int\big|u_t - \frac{x\cdot\nabla u}{2(T - t)}\big|^2\Phi\,dx. Combining, ddt[(T−t)∫∣∇u∣2Φ]=2dsdtdds12∫∣∇w∣2ρ=−2T−t(T−t)2∫∣…∣2Φ\frac{d}{dt}[(T - t)\int|\nabla u|^2\Phi] = 2\frac{ds}{dt}\frac{d}{ds}\frac12\int|\nabla w|^2\rho = -\frac{2}{T - t}(T - t)^2\int|\ldots|^2\Phi, which is the formula. The equality case ws≡0w_s \equiv 0 means ww independent of ss.

The quantity ut−(x−x0)⋅∇u2(T−t)u_t - \frac{(x - x_0)\cdot\nabla u}{2(T - t)} is, up to the factor 1T−t\frac{1}{T - t}, the derivative of uu along the generator of the parabolic dilations centred at (x0,T)(x_0, T): it vanishes exactly for functions invariant under them, as one checks on u=V((x−x0)/T−t)u = V\big((x - x_0)/\sqrt{T - t}\big). Every monotonicity formula in this chapter has the form "a scale-invariant weighted energy decreases at the rate of the squared failure of self-similarity". Here is the list.

  • Harmonic map heat flow. Michael Struwe (1988) proved the same formula, word for word, for maps u:Rn→Nu : \mathbb{R}^n \to N into a Riemannian manifold flowing by the harmonic map heat flow (6C.7 Harmonic Maps and Their Heat Flow): (T−t)∫∣∇u∣2Φ(T - t)\int|\nabla u|^2\Phi is nonincreasing, and constant only for backward self-similar maps. Combined with an ε\varepsilon-regularity theorem, it bounds the size of the singular set of the flow.
  • Mean curvature flow. Huisken's formula (6A.10 Curve Shortening and the First Geometric Flows) is the same identity for the area of a moving hypersurface Mt⊂Rn+1M_t \subset \mathbb{R}^{n+1} against the backward heat kernel of Rn+1\mathbb{R}^{n+1} restricted to MtM_t, normalised by (4π(T−t))−n/2(4\pi(T - t))^{-n/2}:
ddt∫MtΦ dμ=−∫Mt∣H−⟨x−x0,ν⟩2(T−t)∣2Φ dμ.\frac{d}{dt}\int_{M_t}\Phi\,d\mu = -\int_{M_t}\Big|H - \frac{\langle x - x_0, \nu\rangle}{2(T - t)}\Big|^2\Phi\,d\mu.

In backward variables, the rescaled flow is the gradient flow of the Gaussian area F(Σ)=(4π)−n/2∫Σe−∣y∣2/4dμF(\Sigma) = (4\pi)^{-n/2}\int_\Sigma e^{-|y|^2/4}d\mu, and its stationary points, the hypersurfaces with H=⟨y,ν⟩2H = \frac{\langle y, \nu\rangle}{2}, are the self-shrinkers: minimal surfaces for the conformally flat metric e−∣y∣2/2nδe^{-|y|^2/2n}\delta. A sphere of radius 2n\sqrt{2n} and cylinders Sk(2k)×Rn−kS^k(\sqrt{2k})\times\mathbb{R}^{n-k} are self-shrinkers (Exercise 13.11).

  • Semilinear heat equation. The Giga–Kohn functional, written in the original variables, is a monotone combination of (T−t)(p+1)/(p−1)∫(12∣∇u∣2−∣u∣p+1p+1)Φ(T - t)^{(p+1)/(p-1)}\int\big(\frac12|\nabla u|^2 - \frac{|u|^{p+1}}{p+1}\big)\Phi and (T−t)2/(p−1)∫u2Φ(T - t)^{2/(p-1)}\int u^2\Phi.
  • Ricci flow. Perelman's reduced volume (12A.5 Reduced Distance and Reduced Volume) is a Gaussian-weighted volume ∫(4πτ)−n/2e−ℓ dV\int(4\pi\tau)^{-n/2}e^{-\ell}\,dV, with τ\tau the backward time from the base point and ℓ\ell Perelman's reduced distance playing the role of ∣x−x0∣24τ\frac{|x - x_0|^2}{4\tau}. It is nonincreasing in τ\tau, it tends to 11 as τ→0\tau \to 0 at a regular base point, and it is constant on an interval only for a gradient shrinking soliton (on flat space, the Gaussian). His W\mathcal W-entropy (12A.3 The 𝓦-Entropy) is a Gaussian-weighted log-Sobolev quantity, monotone along the flow coupled to the conjugate heat equation, constant exactly on gradient shrinking solitons.

The orientation conventions differ (Perelman's τ\tau runs backward), and the Ricci flow versions need the weight to evolve with the metric, so it is not a Euclidean Gaussian but the conjugate heat kernel or e−ℓe^{-\ell}; but the structure is identical. Morgan and Tian present the reduced volume first as an integral of a Gaussian-type density along L\mathcal L-geodesics and prove its monotonicity by a comparison argument (their chapters 6–8), rather than as a gradient flow; the equality case is analysed in the same way, and gives the asymptotic soliton of a κ\kappa-solution (12B.1 κ-Solutions).

Frequency functions and unique continuation

Monotonicity formulas measure more than energy. For harmonic functions, Frederick Almgren (1979) introduced the frequency

N(r)=r∫Br∣∇u∣2∫∂Bru2,N(r) = \frac{r\int_{B_r}|\nabla u|^2}{\int_{\partial B_r}u^2},

proved that it is nondecreasing in rr, and found that it is constant exactly for homogeneous harmonic polynomials, for which it equals the degree. Nicola Garofalo and Fang-Hua Lin (1986) used it to prove unique continuation: a solution of an elliptic equation that vanishes to infinite order at a point vanishes identically, because the frequency would have to be infinite. Chi-Cheung Poon (1996) found the parabolic version, and in backward self-similar variables it is a two-line computation.

Proposition 13.5 Monotonicity of the parabolic frequency

Let ww solve ws=Lww_s = Lw, L=Δ−y2⋅∇L = \Delta - \frac y2\cdot\nabla, with w(⋅,s)≠0w(\cdot, s) \neq 0 in L2(ρ dy)L^2(\rho\,dy). Then the frequency

N(s)=∫∣∇w∣2ρ dy∫w2ρ dyN(s) = \frac{\int|\nabla w|^2\rho\,dy}{\int w^2\rho\,dy}

is nonincreasing in ss, and constant exactly when w(⋅,s)w(\cdot, s) is an eigenfunction of LL, that is, w=e−ks/2Pk(y)w = e^{-ks/2}P_k(y) with PkP_k a Hermite polynomial of degree kk, for which N=k2N = \frac k2.

Proof. Write ⟨a,b⟩=∫ab ρ\langle a, b\rangle = \int ab\,\rho. Then ∫∣∇w∣2ρ=−⟨Lw,w⟩\int|\nabla w|^2\rho = -\langle Lw, w\rangle and dds⟨w,w⟩=2⟨Lw,w⟩\frac{d}{ds}\langle w, w\rangle = 2\langle Lw, w\rangle, dds⟨Lw,w⟩=2⟨Lw,Lw⟩\frac{d}{ds}\langle Lw, w\rangle = 2\langle Lw, Lw\rangle (using the symmetry of LL). So

dNds=−2⟨Lw,Lw⟩⟨w,w⟩+2⟨Lw,w⟩2⟨w,w⟩2≤0\frac{dN}{ds} = \frac{-2\langle Lw, Lw\rangle\langle w, w\rangle + 2\langle Lw, w\rangle^2}{\langle w, w\rangle^2} \leq 0

by the Cauchy–Schwarz inequality, with equality exactly when LwLw is a multiple of ww.

Undoing the variables, s→∞s \to \infty is t↑Tt \uparrow T: approaching the point (0,T)(0, T) of space-time, the frequency decreases to a limit, and the limit is k2\frac k2 for the lowest Hermite mode present in ww, which is half the parabolic order to which uu vanishes at (0,T)(0, T). (For u=1+(x2+2t)u = 1 + (x^2 + 2t) with T=0T = 0 the limit is 00, because u(0,0)≠0u(0, 0) \neq 0; for u=x2+2tu = x^2 + 2t it is 11.) Here is the idea of the unique continuation argument. Suppose uu vanished to infinite order at (0,T)(0, T). Then every Hermite mode would be absent in the limit, so N(s)→∞N(s) \to \infty; but NN is nonincreasing and finite at any one time, a contradiction unless w≡0w \equiv 0. This is the mechanism of unique continuation and backward uniqueness for parabolic equations, which Book 6B develops, and of which the Ricci flow has a version: Brett Kotschwar (2010) proved backward uniqueness for the Ricci flow, so a Ricci flow is determined by its metric at any one time, and isometries cannot be created or destroyed by the flow.

The blow-up argument, step by step

Here is the argument in the form in which it recurs, with its four steps named.

  1. Monotone quantity. Fix a space-time point (x0,T)(x_0, T), at or near which the solution becomes singular. A scale-invariant quantity Θ(t)\Theta(t), built with the backward heat kernel centred there, is monotone and bounded. So Θ(t)\Theta(t) has a limit Θ0\Theta_0 as t↑Tt \uparrow T, the density of the flow at (x0,T)(x_0, T), and the defect ∫∣failure of self-similarity∣2Φ\int|\text{failure of self-similarity}|^2\Phi is integrable in the logarithmic time ss.
  2. Compactness. Rescale parabolically about (x0,T)(x_0, T) by factors λk→∞\lambda_k \to \infty. The rescaled solutions satisfy uniform estimates (from the equation and from bounds on the monotone quantity), so a subsequence converges, smoothly or weakly, to a limit flow, called a tangent flow.
  3. Rigidity. By scale invariance, the monotone quantity of the kk-th rescaling at time −1-1 equals Θ(T−λk−2)\Theta(T - \lambda_k^{-2}), which tends to Θ0\Theta_0; the same holds at every negative time. So the limit has constant Θ\Theta, and the equality case of the monotonicity formula says that it is self-similar: a self-shrinker, a shrinking soliton, a self-similar harmonic map, the constant κ\kappa.
  4. Classification. Self-similar solutions satisfy an elliptic equation (stationary in self-similar variables), and under natural conditions they can be classified. The classification is a Liouville theorem.

For mean curvature flow of mean convex surfaces, step 4 is Huisken's classification (1990, 1993): the only self-shrinkers with H≥0H \geq 0 and bounded second fundamental form are the round spheres and the generalised cylinders Sk×Rn−kS^k\times\mathbb{R}^{n-k}. For the semilinear heat equation it is the Giga–Kohn Liouville theorem. For the Ricci flow in dimension three, Perelman showed that the asymptotic solitons of κ\kappa-solutions are the round sphere and its quotients, the round cylinder S2×RS^2\times\mathbb{R}, and its Z2\mathbb{Z}_2 quotient (12B.1 κ-Solutions); this is the classification that makes the canonical neighbourhood theorem possible (12B.5 The Canonical Neighbourhood Theorem).

Density and regularity. The density Θ0\Theta_0 also distinguishes regular points from singular ones. For mean curvature flow the density at a point where the flow is smooth is exactly 11 (the Gaussian area of a plane), and Brian White (2005) proved an ε\varepsilon-regularity theorem: there is ε>0\varepsilon > 0 such that if the Gaussian density ratios at all nearby points and scales are less than 1+ε1 + \varepsilon, the flow is smooth nearby with curvature bounds. Perelman's pseudolocality theorem (12A.9 Pseudolocality) is the Ricci flow counterpart: a region that is almost Euclidean at some scale, as measured by an isoperimetric inequality and a curvature lower bound, stays regular for a definite time.

Entropy. Tobias Colding and William Minicozzi (2012) took the supremum of the Gaussian area over all centres and scales,

λ(Σ)=sup⁡x0∈Rn+1, t0>0(4πt0)−n/2∫Σe−∣x−x0∣2/4t0 dμ,\lambda(\Sigma) = \sup_{x_0 \in \mathbb{R}^{n+1},\ t_0 > 0}(4\pi t_0)^{-n/2}\int_\Sigma e^{-|x - x_0|^2/4t_0}\,d\mu,

the entropy of a hypersurface. It is invariant under dilations and translations, nonincreasing under mean curvature flow by Huisken's formula, and it is 11 for a plane, 2π/e≈1.52\sqrt{2\pi/e} \approx 1.52 for a circle and 4e≈1.47\frac4e \approx 1.47 for a round two-sphere (Exercise 13.11). They proved that spheres, cylinders and planes are the only self-shrinkers that cannot be perturbed to lower entropy, so that a generic flow develops only spherical and cylindrical singularities. Perelman's ν\nu-entropy, the infimum of μ(g,τ)\mu(g, \tau) over all scales τ\tau, plays the same role for the Ricci flow, and the noncollapsing theorem of 12A.4 κ-Noncollapsing is its first consequence.

In the world In use Self-similarity in physics and engineering

Self-similar variables are a standard tool well beyond geometry. In fluid mechanics, the boundary layer along a flat plate (Blasius 1908) and the spreading of a jet are self-similar, and the change of variables y/xy/\sqrt{x} reduces their PDEs to ODEs. In explosions, Geoffrey Taylor's estimate of the energy of the first atomic test from photographs of the fireball's radius, R∝(Et2/ρ)1/5R \propto (Et^2/\rho)^{1/5}, used only the self-similar form of the blast wave. Grigory Barenblatt distinguished self-similarity "of the first kind", where the exponents follow from dimensional analysis, as for the heat kernel, from "the second kind", where they must be found by solving an eigenvalue problem, as in the porous medium equation with absorption or in the logarithmic corrections above. In image processing the scale-space of 6A.4 Fourier Methods and Scale Space is the forward self-similar picture, and in probability the convergence to the Gaussian is the central limit theorem.

History

Self-similar solutions of the heat equation are as old as the heat kernel; the change to logarithmic time and rescaled space was used for the porous medium equation by Barenblatt in the 1950s. Almgren's frequency function appeared in 1979 and Garofalo and Lin's unique continuation theorem in 1986. Giga and Kohn's paper on self-similar blow-up appeared in 1985, with sequels in 1987 and 1989. Struwe's monotonicity formula for the harmonic map flow appeared in 1988, Huisken's for mean curvature flow in 1990, and his classification of mean convex shrinkers in 1990 and 1993. Bricmont and Kupiainen's and Merle and Zaag's work on blow-up profiles dates from 1994 and 1997. Poon's parabolic frequency appeared in 1996. Perelman's entropy and reduced volume appeared in 2002, White's regularity theorem in 2005, Kotschwar's backward uniqueness for the Ricci flow in 2010, and Colding and Minicozzi's entropy in 2012.

Recall Where we stand

Self-similar solutions are fixed points of parabolic scaling, forward, backward or translating. In forward variables y=x/ty = x/\sqrt t, τ=log⁡t\tau = \log t, the heat equation becomes a Fokker–Planck equation with the Gaussian as equilibrium; with v=Gfv = Gf it is the Ornstein–Uhlenbeck equation, whose Hermite spectrum is {k2}\{\frac k2\}, and the Gaussian Poincaré inequality, proved from the Mehler formula, gives convergence to the Gaussian at the rate t−1/2t^{-1/2}. In backward variables y=x/T−ty = x/\sqrt{T - t}, s=−log⁡(T−t)s = -\log(T - t), flows become gradient flows in L2(ρ dy)L^2(\rho\,dy): the semilinear heat equation has the Giga–Kohn Lyapunov functional, and blow-up is asymptotically the constant κ\kappa, with logarithmic corrections from a neutral Hermite mode. Undoing the variables gives monotonicity formulas with the backward heat kernel as weight: for the heat equation and harmonic map flow (Struwe), mean curvature flow (Huisken) and the Ricci flow (Perelman's reduced volume and W\mathcal W), each decreasing at the rate of the squared failure of self-similarity. Poon's frequency is monotone and measures the order of vanishing, giving unique continuation. The blow-up argument runs: monotone quantity, compactness, rigidity in the equality case, classification of self-similar solutions; density and ε\varepsilon-regularity (White, pseudolocality) and entropy (Colding–Minicozzi, Perelman's ν\nu) refine it.

Recall Book 6A in one paragraph

A PDE is classified by its symbol; the heat equation is parabolic, scales like (λx,λ2t)(\lambda x, \lambda^2t), is well posed forward and ill-posed backward (6A.1 What a PDE Is). Harmonic functions are averages and obey maximum principles, Harnack and Liouville (6A.2 Harmonic Functions). The heat kernel solves the heat equation on Rn\mathbb{R}^n, smooths instantly and is the law of Brownian motion (6A.3 The Heat Equation on ℝⁿ). On the Fourier side each frequency decays by itself, smoothing is the decay of high frequencies, and blurring an image is running the heat equation (6A.4 Fourier Methods and Scale Space). At a first interior maximum ut≥0≥Δuu_t \geq 0 \geq \Delta u: maximum principles, comparison and invariant regions for systems follow (6A.5 Maximum Principles). Weak solutions exist by Lax–Milgram and are smooth by bootstrapping (6A.6 Weak Solutions and Elliptic Regularity); parabolic equations gain two space derivatives and one time derivative, and Bernstein's method bounds gradients by C/tC/\sqrt t (6A.7 Parabolic Regularity). Nonlinear equations exist for short time by linearising and a fixed point, and may blow up (6A.8 Nonlinear Parabolic Equations). Reaction against diffusion gives critical patch sizes, travelling fronts, Allen–Cahn interfaces moving by mean curvature, Turing patterns, and the curvature equations of the Ricci flow (6A.9 Reaction–Diffusion: Fronts, Patterns and Pinching). Curve shortening and mean curvature flow show solitons, ancient solutions, neckpinches and Huisken's monotonicity (6A.10 Curve Shortening and the First Geometric Flows). Energies give Euler–Lagrange equations and gradient flows (6A.11 Calculus of Variations and Gradient Flows). Entropy increases along diffusion at the rate of the Fisher information, the log-Sobolev inequality is W≥0\mathcal W \geq 0 on flat space, and the Li–Yau inequality is sharp on the heat kernel (6A.12 Entropy, Information and Diffusion). In self-similar variables flows become gradient flows in Gaussian-weighted spaces, monotonicity formulas are their energy identities, and the blow-up argument turns monotonicity into the classification of singularities (this chapter).

Where this goes Into Books 6B, 6C and 6D, and Book 7A

Book 6A is the shortest road from the heat equation to the Ricci flow. Course 6 continues for the reader who wants the whole subject: Book 6B proves the linear theory that 6A quoted (Schauder, LpL^p and De Giorgi–Nash–Moser estimates, semigroups, spectral asymptotics) and adds waves and characteristics (6B.1 First-Order Equations and Characteristics); Book 6C develops the nonlinear methods (6C.1 Regularity of Minimisers and Constraints); Book 6D builds the probabilistic and numerical side, from Brownian motion to option pricing and finite differences (6D.1 Brownian Motion). A reader on the Ricci flow route can go straight on: the analysis is now ready, but "manifold" has not been defined, and the Poincaré conjecture is about topology. Book 7A turns to topology, starting with only what differs from the metric spaces of Book 2B, and builds the fundamental group, covering spaces and the precise statement of the conjecture (7A.1 Topological Spaces and Quotients).

Exercises

Exercise 13.6 Forward self-similar variables

Let u(x,t)=t−n/2v(y,τ)u(x, t) = t^{-n/2}v(y, \tau) with y=x/ty = x/\sqrt t, τ=log⁡t\tau = \log t. Show that ut=Δuu_t = \Delta u if and only if vτ=Δv+y2⋅∇v+n2vv_\tau = \Delta v + \frac y2\cdot\nabla v + \frac n2v, and that the right side equals div⁡(∇v+y2v)\operatorname{div}(\nabla v + \frac y2v). Check that v=Gv = G is stationary, and identify the solution uu it corresponds to.

Solution

By the chain rule, ∂t[v(x/t,log⁡t)]=−x2t3/2⋅∇v+1tvτ=1t(vτ−y2⋅∇v)\partial_t[v(x/\sqrt t, \log t)] = -\frac{x}{2t^{3/2}}\cdot\nabla v + \frac1tv_\tau = \frac1t\big(v_\tau - \frac y2\cdot\nabla v\big), so ut=t−n/2−1(−n2v−y2⋅∇v+vτ)u_t = t^{-n/2 - 1}\big(-\frac n2v - \frac y2\cdot\nabla v + v_\tau\big), while Δxu=t−n/2−1Δyv\Delta_xu = t^{-n/2 - 1}\Delta_yv. Equating gives the equation. Since div⁡(y2v)=n2v+y2⋅∇v\operatorname{div}(\frac y2v) = \frac n2v + \frac y2\cdot\nabla v, it is div⁡(∇v+y2v)\operatorname{div}(\nabla v + \frac y2v). For G=(4π)−n/2e−∣y∣2/4G = (4\pi)^{-n/2}e^{-|y|^2/4}, ∇G=−y2G\nabla G = -\frac y2G, so the flux vanishes. It corresponds to u=t−n/2(4π)−n/2e−∣x∣2/4t=Φ(x,t)u = t^{-n/2}(4\pi)^{-n/2}e^{-|x|^2/4t} = \Phi(x, t), the heat kernel.

Exercise 13.7 The Mehler formula

(a) Verify that Psf(y)=∫f(e−s/2y+1−e−sz)G(z) dzP_sf(y) = \int f(e^{-s/2}y + \sqrt{1 - e^{-s}}z)G(z)\,dz satisfies P0f=fP_0f = f and ∂sPsf=LPsf\partial_sP_sf = LP_sf for, say, ff a polynomial, by checking it on f=eξ⋅yf = e^{\xi\cdot y}: show Pseξ⋅y=exp⁡(e−s/2ξ⋅y+(1−e−s)∣ξ∣2)P_se^{\xi\cdot y} = \exp\big(e^{-s/2}\xi\cdot y + (1 - e^{-s})|\xi|^2\big) and differentiate. (b) Show that ∫(Psf)G=∫fG\int(P_sf)G = \int fG.

Solution

(a) ∫eξ⋅z1−e−sG(z) dz=e(1−e−s)∣ξ∣2\int e^{\xi\cdot z\sqrt{1 - e^{-s}}}G(z)\,dz = e^{(1 - e^{-s})|\xi|^2}, because ∫eη⋅zG(z) dz=e∣η∣2\int e^{\eta\cdot z}G(z)\,dz = e^{|\eta|^2} for the Gaussian of variance 22 per coordinate. So Pseξ⋅y=exp⁡(e−s/2ξ⋅y+(1−e−s)∣ξ∣2)=:eϕP_se^{\xi\cdot y} = \exp(e^{-s/2}\xi\cdot y + (1 - e^{-s})|\xi|^2) =: e^{\phi}. Then ∂seϕ=(−12e−s/2ξ⋅y+e−s∣ξ∣2)eϕ\partial_se^\phi = \big(-\frac12e^{-s/2}\xi\cdot y + e^{-s}|\xi|^2\big)e^\phi, while ∇eϕ=e−s/2ξeϕ\nabla e^\phi = e^{-s/2}\xi e^\phi, Δeϕ=e−s∣ξ∣2eϕ\Delta e^\phi = e^{-s}|\xi|^2e^\phi, so Leϕ=(e−s∣ξ∣2−12e−s/2ξ⋅y)eϕLe^\phi = \big(e^{-s}|\xi|^2 - \frac12e^{-s/2}\xi\cdot y\big)e^\phi, the same. At s=0s = 0 it is eξ⋅ye^{\xi\cdot y}. Polynomials are obtained by differentiating in ξ\xi at ξ=0\xi = 0. (b) ∫ ⁣ ⁣∫f(e−s/2y+1−e−sz)G(y)G(z) dy dz\int\!\!\int f(e^{-s/2}y + \sqrt{1 - e^{-s}}z)G(y)G(z)\,dy\,dz: if YY, ZZ are independent with density GG, then e−s/2Y+1−e−sZe^{-s/2}Y + \sqrt{1 - e^{-s}}Z again has density GG (a Gaussian with covariance (e−s+1−e−s)⋅2I(e^{-s} + 1 - e^{-s})\cdot2I), so the integral is ∫fG\int fG.

Exercise 13.8 The Hermite spectrum

In one dimension, with L=∂y2−y2∂yL = \partial_y^2 - \frac y2\partial_y: (a) show that −L-L maps polynomials of degree kk to polynomials of degree kk, with leading coefficient multiplied by k2\frac k2; (b) find H2=y2+cH_2 = y^2 + c and H3=y3+cyH_3 = y^3 + cy with −LHk=k2Hk-LH_k = \frac k2H_k; (c) show that x2+2tx^2 + 2t and x3+6xtx^3 + 6xt solve the heat equation, and that for t<0t < 0 they equal (−t)H2(x/−t)(-t)H_2(x/\sqrt{-t}) and (−t)3/2H3(x/−t)(-t)^{3/2}H_3(x/\sqrt{-t}): Hermite polynomials in the backward variables with T=0T = 0.

Solution

(a) −L(yk)=−k(k−1)yk−2+k2yk-L(y^k) = -k(k - 1)y^{k-2} + \frac k2y^k. (b) −L(y2+c)=−2+y2-L(y^2 + c) = -2 + y^2, which equals (y2+c)(y^2 + c) times 11 when c=−2c = -2: H2=y2−2H_2 = y^2 - 2, eigenvalue 1=221 = \frac22. −L(y3+cy)=−6y+32y3+c2y-L(y^3 + cy) = -6y + \frac32y^3 + \frac c2y, and setting this equal to 32(y3+cy)\frac32(y^3 + cy) gives −6+c2=3c2-6 + \frac c2 = \frac{3c}{2}, c=−6c = -6: H3=y3−6yH_3 = y^3 - 6y. (c) ∂t(x2+2t)=2=∂x2(x2)\partial_t(x^2 + 2t) = 2 = \partial_x^2(x^2) and ∂t(x3+6xt)=6x=∂x2(x3)\partial_t(x^3 + 6xt) = 6x = \partial_x^2(x^3). With T=0T = 0 and t<0t < 0, y=x/−ty = x/\sqrt{-t}: x2+2t=(−t)(y2−2)=(−t)H2(y)x^2 + 2t = (-t)(y^2 - 2) = (-t)H_2(y) and x3+6xt=(−t)3/2(y3−6y)=(−t)3/2H3(y)x^3 + 6xt = (-t)^{3/2}(y^3 - 6y) = (-t)^{3/2}H_3(y). With s=−log⁡(−t)s = -\log(-t), w=uw = u is e−sH2e^{-s}H_2 and e−3s/2H3e^{-3s/2}H_3: eigenfunctions decaying at the rates k2\frac k2, as Proposition 13.5 says.

Exercise 13.9 Backward variables for the semilinear equation

(a) With w(y,s)=(T−t)1/(p−1)u(x,t)w(y, s) = (T - t)^{1/(p-1)}u(x, t), y=x/T−ty = x/\sqrt{T - t}, s=−log⁡(T−t)s = -\log(T - t), show that ut=Δu+∣u∣p−1uu_t = \Delta u + |u|^{p-1}u becomes ws=Δw−y2⋅∇w−wp−1+∣w∣p−1ww_s = \Delta w - \frac y2\cdot\nabla w - \frac{w}{p - 1} + |w|^{p-1}w. (b) Show that the constant stationary solutions are 00 and ±κ\pm\kappa, κ=(p−1)−1/(p−1)\kappa = (p - 1)^{-1/(p-1)}, and identify the corresponding uu. (c) Linearise at w=κw = \kappa: show that the linearised operator is L+1L + 1, and that its eigenvalues on Hermite polynomials are 1−k21 - \frac k2. Which modes are unstable, which neutral? (The unstable modes k=0,1k = 0, 1 correspond to changing the blow-up time and the blow-up point.)

Solution

(a) Write θ=T−t\theta = T - t, so dsdt=1θ\frac{ds}{dt} = \frac1\theta and ∂y∂t=y2θ\frac{\partial y}{\partial t} = \frac{y}{2\theta}. With u=θ−1/(p−1)wu = \theta^{-1/(p-1)}w: ut=θ−1/(p−1)−1(wp−1+y2⋅∇w+ws)u_t = \theta^{-1/(p-1) - 1}\big(\frac{w}{p - 1} + \frac y2\cdot\nabla w + w_s\big), Δu=θ−1/(p−1)−1Δw\Delta u = \theta^{-1/(p-1) - 1}\Delta w, and ∣u∣p−1u=θ−p/(p−1)∣w∣p−1w=θ−1/(p−1)−1∣w∣p−1w|u|^{p-1}u = \theta^{-p/(p-1)}|w|^{p-1}w = \theta^{-1/(p-1) - 1}|w|^{p-1}w. Equating gives the equation. (b) A constant ww satisfies −wp−1+∣w∣p−1w=0-\frac{w}{p - 1} + |w|^{p-1}w = 0, so w=0w = 0 or ∣w∣p−1=1p−1|w|^{p-1} = \frac{1}{p - 1}. The solution u=±κ(T−t)−1/(p−1)u = \pm\kappa(T - t)^{-1/(p-1)} is the ODE solution blowing up at TT. (c) The derivative of −wp−1+∣w∣p−1w-\frac{w}{p - 1} + |w|^{p-1}w at κ\kappa is −1p−1+pκp−1=−1p−1+pp−1=1-\frac{1}{p - 1} + p\kappa^{p-1} = -\frac{1}{p - 1} + \frac{p}{p - 1} = 1. So the linearisation is L+1L + 1, with eigenvalues 1−k21 - \frac k2 on HkH_k: positive (unstable) for k=0,1k = 0, 1, zero (neutral) for k=2k = 2, negative for k≥3k \geq 3. The neutral mode H2H_2 is responsible for the logarithmic profile of Bricmont–Kupiainen and Merle–Zaag.

Exercise 13.10 Homogeneous data

Let u0(x)=∣x∣−au_0(x) = |x|^{-a} on Rn\mathbb{R}^n, 0<a<n0 < a < n, and u=Φ(⋅,t)∗u0u = \Phi(\cdot, t)*u_0. (a) Show directly from the convolution formula that u(λx,λ2t)=λ−au(x,t)u(\lambda x, \lambda^2t) = \lambda^{-a}u(x, t). (b) Deduce that u(x,t)=t−a/2V(x/t)u(x, t) = t^{-a/2}V(x/\sqrt t) with V=u(⋅,1)V = u(\cdot, 1), and find the behaviour of V(y)V(y) as ∣y∣→∞|y| \to \infty.

Solution

(a) u(λx,λ2t)=∫Φ(λx−z,λ2t)∣z∣−adzu(\lambda x, \lambda^2t) = \int\Phi(\lambda x - z, \lambda^2t)|z|^{-a}dz; substitute z=λz′z = \lambda z': dz=λndz′dz = \lambda^ndz', Φ(λ(x−z′),λ2t)=λ−nΦ(x−z′,t)\Phi(\lambda(x - z'), \lambda^2t) = \lambda^{-n}\Phi(x - z', t) and ∣z∣−a=λ−a∣z′∣−a|z|^{-a} = \lambda^{-a}|z'|^{-a}, giving λ−au(x,t)\lambda^{-a}u(x, t). (b) Take λ=t−1/2\lambda = t^{-1/2}: u(x/t,1)=ta/2u(x,t)u(x/\sqrt t, 1) = t^{a/2}u(x, t). As ∣y∣→∞|y| \to \infty, V(y)=∫Φ(y−z,1)∣z∣−adz≈∣y∣−aV(y) = \int\Phi(y - z, 1)|z|^{-a}dz \approx |y|^{-a}, since the kernel has unit mass and concentrates within distance O(1)O(1) of yy, where ∣z∣−a≈∣y∣−a|z|^{-a} \approx |y|^{-a}. So far from the origin the solution still looks like its initial data, and the self-similar profile interpolates between a smooth cap and the cone-like tail: the same picture as a Ricci expander coming out of a cone.

Exercise 13.11 Self-shrinkers and their entropy

(a) Show that a round sphere Sn(R)⊂Rn+1S^n(R) \subset \mathbb{R}^{n+1} satisfies H=⟨y,ν⟩2H = \frac{\langle y, \nu\rangle}{2} exactly when R=2nR = \sqrt{2n}, and that the cylinder Sk(R)×Rn−kS^k(R)\times\mathbb{R}^{n-k} does exactly when R=2kR = \sqrt{2k}. (b) Show that the Gaussian area F(Σ)=(4π)−n/2∫Σe−∣y∣2/4dμF(\Sigma) = (4\pi)^{-n/2}\int_\Sigma e^{-|y|^2/4}d\mu of the shrinking circle S1(2)S^1(\sqrt2) is 2π/e\sqrt{2\pi/e}, and of S2(2)S^2(2) is 4e\frac4e. (c) For a plane through the origin, show F=1F = 1.

Solution

(a) For the sphere, H=nRH = \frac nR and ⟨y,ν⟩=R\langle y, \nu\rangle = R on it, so nR=R2\frac nR = \frac R2, R2=2nR^2 = 2n. For the cylinder, the Rn−k\mathbb{R}^{n-k} factor contributes no curvature and is orthogonal to ν\nu, so H=kRH = \frac kR and ⟨y,ν⟩=R\langle y, \nu\rangle = R, giving R2=2kR^2 = 2k. (b) n=1n = 1: (4π)−1/2⋅2π2⋅e−1/2=2π22πe=2πe≈1.520(4\pi)^{-1/2}\cdot2\pi\sqrt2\cdot e^{-1/2} = \frac{2\pi\sqrt2}{2\sqrt\pi\sqrt e} = \sqrt{\frac{2\pi}{e}} \approx 1.520. n=2n = 2: (4π)−1⋅4π⋅4⋅e−1=4e≈1.472(4\pi)^{-1}\cdot4\pi\cdot4\cdot e^{-1} = \frac4e \approx 1.472. (c) For Rn⊂Rn+1\mathbb{R}^n \subset \mathbb{R}^{n+1}, (4π)−n/2∫Rne−∣y∣2/4dy=1(4\pi)^{-n/2}\int_{\mathbb{R}^n}e^{-|y|^2/4}dy = 1. These are the entropies: for shrinkers, Colding and Minicozzi showed the supremum in λ\lambda is attained at x0=0x_0 = 0, t0=1t_0 = 1.

Exercise 13.12 Almgren's frequency for harmonic polynomials

Let uu be a homogeneous harmonic polynomial of degree kk on Rn\mathbb{R}^n. Show that N(r)=r∫Br∣∇u∣2∫∂Bru2=kN(r) = \frac{r\int_{B_r}|\nabla u|^2}{\int_{\partial B_r}u^2} = k for all rr. (Hint: ∫Br∣∇u∣2=∫∂Bru ∂ru\int_{B_r}|\nabla u|^2 = \int_{\partial B_r}u\,\partial_ru by Green's identity, and ∂ru=kru\partial_ru = \frac kru by Euler's formula for homogeneous functions.)

Solution

Since Δu=0\Delta u = 0, div⁡(u∇u)=∣∇u∣2\operatorname{div}(u\nabla u) = |\nabla u|^2, so by the divergence theorem ∫Br∣∇u∣2=∫∂Bru ∂ru\int_{B_r}|\nabla u|^2 = \int_{\partial B_r}u\,\partial_ru. By homogeneity, x⋅∇u=kux\cdot\nabla u = ku, so on ∂Br\partial B_r, ∂ru=xr⋅∇u=kru\partial_ru = \frac{x}{r}\cdot\nabla u = \frac kru. Then r∫Br∣∇u∣2=r⋅kr∫∂Bru2r\int_{B_r}|\nabla u|^2 = r\cdot\frac kr\int_{\partial B_r}u^2, and N(r)=kN(r) = k. The frequency counts the degree, the order of vanishing of uu at the origin, just as Poon's frequency counts the order of a caloric polynomial.

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