Book 6A

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Course 6Book 6A: The Heat Equation and Its RelativesChapter 4

Maximum Principles

Weak and strong maximum principles, comparison, and invariant regions for systems.

30 min read · Updated Oct 2, 2026

Read with Evans, Partial Differential Equations, section 2.3.3 (the maximum principle for the heat equation), section 6.4 (maximum principles for elliptic operators, including Hopf's lemma) and section 7.1.4 (maximum principles for parabolic operators). Protter and Weinberger, Maximum Principles in Differential Equations, is the classic reference.

In this chapter · 9 sections
  1. 4.1No cold spot forms by itself
  2. 4.2The core argument
  3. 4.3The weak maximum principle
  4. 4.4The strong maximum principle and Hopf's lemma
  5. 4.5Comparison principles
  6. 4.6Systems and invariant regions
  7. 4.7Invasion fronts
  8. 4.8History
  9. 4.9Exercises

The maximum principle is the most important single tool in the analysis of the Ricci flow. Hamilton's 1982 theorem, the Hamilton–Ivey pinching estimate, the preservation of positive curvature, the lower bound on scalar curvature that Perelman uses at every step: all of them are maximum principles. And every one of them rests on an argument that fits in one line, which this chapter isolates, proves in its various forms, and then extends from single equations to systems.

The line is this. At a point where a function first reaches a new maximum, its gradient vanishes, its Hessian is negative semidefinite, and its time derivative is non-negative. So ut≥0≥Δuu_t \geq 0 \geq \Delta u there. If an equation says ut−Δuu_t - \Delta u is negative at such a point, the point cannot exist. You have met each half of this argument before: the extreme value theorem (2A.9 Continuous Functions), the derivative at a maximum (2A.10 Derivatives), and the second-derivative test (2B.8 Calculus in Several Variables). This chapter combines them.

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

  • state and prove the weak maximum principle for parabolic and elliptic operators with lower-order terms;
  • state Hopf's lemma and the strong maximum principle, and prove Hopf's lemma with a barrier;
  • prove comparison principles for semilinear equations, and compare a PDE with an ODE;
  • explain why maximum principles fail for systems in general, and prove that invariant convex sets of the reaction ODE are invariant for the reaction–diffusion system;
  • recognise the invariant-region argument as the ancestor of Hamilton's tensor maximum principle.

No cold spot forms by itself

In the world Model Thermal design by the maximum principle

Heat flows from hot to cold. In a body with no internal heat sources, conduction can only smooth temperatures out, so no new hot spot or cold spot can form inside: the maximum and minimum temperatures over the whole history are reached at the start or on the surface. This is the weak maximum principle for the heat equation (6A.3 The Heat Equation on ℝⁿ, Theorem 4.1). Engineers use it in both directions. To bound the temperature of a component that conducts heat, it suffices to bound the initial temperature and the temperatures imposed on its surface; the interior can be no worse. And when there are sources, the principle becomes a comparison: if the heating rate is at most qq, the temperature is at most that of a body heated uniformly at rate qq with the same surface conditions, which can often be computed by hand (Theorem 4.4).

The core argument

The idea The one-line maximum principle

Let uu be smooth on a region of space-time, and suppose (x0,t0)(x_0, t_0) is a point where u(⋅,t0)u(\cdot, t_0) has a spatial maximum at an interior point x0x_0, and u(x0,⋅)u(x_0, \cdot) was smaller or equal just before t0t_0. Then at (x0,t0)(x_0, t_0):

∇u=0,∇2u≤0 (so Δu≤0),ut≥0.\nabla u = 0, \qquad \nabla^2u \leq 0\ \text{(so } \Delta u \leq 0\text{)}, \qquad u_t \geq 0.

Every maximum principle in this book, and every maximum principle for the Ricci flow in 11A.4 Maximum Principles under Ricci Flow, is this observation plus a way to rule out the equality cases.

The first two are the first- and second-order conditions for an interior maximum (2B.8 Calculus in Several Variables); a negative semidefinite matrix has non-positive trace. The third is the one-sided derivative at a point the function has reached from below (2A.10 Derivatives). More generally, if (aij)(a^{ij}) is positive semidefinite and ∇2u≤0\nabla^2u \leq 0, then ∑aij∂i∂ju=tr⁡(A∇2u)≤0\sum a^{ij}\partial_i\partial_ju = \operatorname{tr}(A\nabla^2u) \leq 0 (the trace of a product of a positive and a negative semidefinite matrix is non-positive, Exercise 4.6). So the argument works for any operator whose second-order part has a positive semidefinite coefficient matrix: any elliptic operator (6A.1 What a PDE Is).

Figure 4.1. The first time t0t_0 at which max⁡xu(⋅,t)\max_xu(\cdot, t) reaches a new value, at an interior point x0x_0. The spatial profile has a peak there (∇u=0\nabla u = 0, ∇2u≤0\nabla^2u \leq 0), and the value at x0x_0 has been rising (ut≥0u_t \geq 0). An equation that forces ut−Δu<0u_t - \Delta u < 0 makes this impossible.

The weak maximum principle

Let U⊂RnU \subset \mathbb{R}^n be bounded and open, UT=U×(0,T]U_T = U\times(0, T] and ΓT\Gamma_T its parabolic boundary (6A.3 The Heat Equation on ℝⁿ). Consider the operator

Lu=ut−∑i,jaij(x,t)∂i∂ju+∑ibi(x,t)∂iu+c(x,t)u,Lu = u_t - \sum_{i,j}a^{ij}(x, t)\partial_i\partial_ju + \sum_ib^i(x, t)\partial_iu + c(x, t)u,

with continuous bounded coefficients and (aij)(a^{ij}) positive semidefinite (for the strong principle we will need uniform parabolicity, ∑aijξiξj≥θ∣ξ∣2\sum a^{ij}\xi_i\xi_j \geq \theta|\xi|^2 with θ>0\theta > 0).

Theorem 4.1 The weak maximum principle

Let u∈C2,1(UT)∩C(UT‾)u \in C^{2,1}(U_T)\cap C(\overline{U_T}).

  1. If c=0c = 0 and Lu≤0Lu \leq 0 in UTU_T, then max⁡UT‾u=max⁡ΓTu\max_{\overline{U_T}}u = \max_{\Gamma_T}u.
  2. If c≥0c \geq 0 and Lu≤0Lu \leq 0 in UTU_T, then max⁡UT‾u≤max⁡ΓTu+\max_{\overline{U_T}}u \leq \max_{\Gamma_T}u^+, where u+=max⁡(u,0)u^+ = \max(u, 0).

Proof. (1) Suppose first Lu<0Lu < 0. If the maximum over UT‾\overline{U_T} were attained at (x0,t0)(x_0, t_0) with x0∈Ux_0 \in U and 0<t0≤T0 < t_0 \leq T, then by the core argument ut≥0u_t \geq 0, ∇u=0\nabla u = 0 and ∑aij∂i∂ju≤0\sum a^{ij}\partial_i\partial_ju \leq 0 there, so Lu≥0Lu \geq 0: a contradiction. In general let uε=u−εtu^\varepsilon = u - \varepsilon t; then Luε=Lu−ε<0Lu^\varepsilon = Lu - \varepsilon < 0, so max⁡uε\max u^\varepsilon is attained on ΓT\Gamma_T, and letting ε→0\varepsilon \to 0 gives the claim.

(2) If max⁡u≤0\max u \leq 0 there is nothing to prove. Otherwise, on the open set V={u>0}∩UTV = \{u > 0\}\cap U_T, the operator L′u=Lu−cuL'u = Lu - cu satisfies L′u=Lu−cu≤0L'u = Lu - cu \leq 0, since c≥0c \geq 0 and u>0u > 0 there. Apply (1) to L′L' on (the components of) VV: the positive maximum is attained on the parabolic boundary of VV, where either u=0u = 0 or the point lies on ΓT\Gamma_T.

The sign condition on cc matters: for ut=uxx+uu_t = u_{xx} + u, the function etsin⁡xe^t\sin x on (0,π)(0, \pi) is zero on the sides, positive inside, and grows. With c<0c < 0 the equation has a source proportional to uu, and the maximum can grow. That is exactly what happens in the reaction terms below, and it is handled by comparison with an ODE rather than forbidden.

The elliptic case is the time-independent version: if −∑aij∂i∂ju+∑bi∂iu≤0-\sum a^{ij}\partial_i\partial_ju + \sum b^i\partial_iu \leq 0 in a bounded UU with (aij)(a^{ij}) uniformly positive definite, then max⁡U‾u=max⁡∂Uu\max_{\overline U}u = \max_{\partial U}u (Evans, section 6.4.1). The proof perturbs by εeλx1\varepsilon e^{\lambda x_1} instead of εt\varepsilon t, using the uniform ellipticity to make the perturbation strictly subsolution (Exercise 4.7).

The strong maximum principle and Hopf's lemma

The weak principle says the maximum is attained on the boundary. The strong principle says it is attained only there, unless the function is constant. For harmonic functions this came from the mean value property (6A.2 Harmonic Functions). For general operators, which have no mean value property, it comes from a lemma about the boundary.

Lemma 4.2 Hopf's lemma

Let u∈C2(U)∩C1(U‾)u \in C^2(U)\cap C^1(\overline U) satisfy −∑aij∂i∂ju+∑bi∂iu≤0-\sum a^{ij}\partial_i\partial_ju + \sum b^i\partial_iu \leq 0 in UU, with (aij)(a^{ij}) uniformly elliptic. Suppose x0∈∂Ux_0 \in \partial U, u(x0)>u(x)u(x_0) > u(x) for all x∈Ux \in U, and UU satisfies an interior ball condition at x0x_0: there is a ball B⊂UB \subset U with x0∈∂Bx_0 \in \partial B. Then the outward normal derivative satisfies

∂u∂ν(x0)>0.\frac{\partial u}{\partial\nu}(x_0) > 0.

Proof. Translate so that B=Br(0)B = B_r(0). Consider the barrier v(x)=e−λ∣x∣2−e−λr2v(x) = e^{-\lambda|x|^2} - e^{-\lambda r^2}, which is positive in BB, zero on ∂B\partial B, and has ∂v∂ν=−2λre−λr2<0\frac{\partial v}{\partial\nu} = -2\lambda re^{-\lambda r^2} < 0 on ∂B\partial B. A computation (Exercise 4.8) shows that for λ\lambda large, vv satisfies the strict inequality −∑aij∂i∂jv+∑bi∂iv<0-\sum a^{ij}\partial_i\partial_jv + \sum b^i\partial_iv < 0 in the annulus R=Br(0)∖Br/2(0)‾R = B_r(0)\setminus\overline{B_{r/2}(0)}. On ∂Br/2\partial B_{r/2}, u<u(x0)u < u(x_0) strictly, so for small ε>0\varepsilon > 0, w=u+εv−u(x0)≤0w = u + \varepsilon v - u(x_0) \leq 0 there; on ∂Br\partial B_r, v=0v = 0 and u≤u(x0)u \leq u(x_0), so w≤0w \leq 0. By the weak maximum principle on RR, w≤0w \leq 0 in RR, with w(x0)=0w(x_0) = 0. So ww has a maximum at x0x_0 over R‾\overline R, and ∂w∂ν(x0)≥0\frac{\partial w}{\partial\nu}(x_0) \geq 0, i.e. ∂u∂ν(x0)≥−ε∂v∂ν(x0)>0\frac{\partial u}{\partial\nu}(x_0) \geq -\varepsilon\frac{\partial v}{\partial\nu}(x_0) > 0.

The barrier is the important idea: an explicit function, built to satisfy a strict inequality, that is compared with the unknown solution by the weak maximum principle. Barriers are how boundary behaviour is controlled throughout elliptic and parabolic theory.

Theorem 4.3 The strong maximum principle

Let UU be connected and u∈C2(U)u \in C^2(U) satisfy −∑aij∂i∂ju+∑bi∂iu≤0-\sum a^{ij}\partial_i\partial_ju + \sum b^i\partial_iu \leq 0, with (aij)(a^{ij}) uniformly elliptic. If uu attains its maximum over UU at an interior point, then uu is constant. The parabolic version holds too: if ut−∑aij∂i∂ju+∑bi∂iu≤0u_t - \sum a^{ij}\partial_i\partial_ju + \sum b^i\partial_iu \leq 0 in UTU_T, with UU connected, and uu attains its maximum over UT‾\overline{U_T} at (x0,t0)(x_0, t_0) with x0∈Ux_0 \in U, 0<t0≤T0 < t_0 \leq T, then uu is constant on Ut0U_{t_0}.

Proof. (Elliptic case.) Let M=max⁡uM = \max u and C={u=M}C = \{u = M\}, closed in UU and non-empty. If V={u<M}V = \{u < M\} were non-empty, choose a point of VV closer to CC than to ∂U\partial U, and the largest ball in VV around it; this ball touches CC at some x0x_0 in the interior of UU, and VV satisfies the interior ball condition there. Hopf's lemma applied on that ball gives ∂νu(x0)>0\partial_\nu u(x_0) > 0. But x0x_0 is an interior maximum of uu, so ∇u(x0)=0\nabla u(x_0) = 0. So VV is empty. (The parabolic case is due to Louis Nirenberg, 1953; Evans, section 7.1.4.)

Where this goes The strong maximum principle for curvature

Hamilton's strong maximum principle for tensors says, for instance, that under the Ricci flow a manifold whose curvature operator is non-negative either has positive curvature operator immediately, or its curvature operator has a kernel that is invariant under parallel transport, and then the manifold locally splits as a product (11A.4 Maximum Principles under Ricci Flow). That is how κ-solutions with a zero curvature direction are shown to split off a line (12B.2 The Structure of κ-Solutions). The scalar strong maximum principle here is its first case.

Comparison principles

Most equations of interest are nonlinear. The maximum principle extends to them through comparison: a solution lying below another at the start and on the boundary stays below.

Theorem 4.4 Comparison for semilinear equations

Let f:R→Rf : \mathbb{R}\to\mathbb{R} be Lipschitz with constant KK. Suppose uu, v∈C2,1(UT)∩C(UT‾)v \in C^{2,1}(U_T)\cap C(\overline{U_T}) satisfy

ut−Δu−f(u)≤0≤vt−Δv−f(v)in UT,u_t - \Delta u - f(u) \leq 0 \leq v_t - \Delta v - f(v) \quad\text{in } U_T,

(uu is a subsolution, vv a supersolution) and u≤vu \leq v on ΓT\Gamma_T. Then u≤vu \leq v in UTU_T.

Proof. Let w=u−vw = u - v. Where w>0w > 0, f(u)−f(v)=c(x,t)wf(u) - f(v) = c(x, t)w with c=f(u)−f(v)u−vc = \frac{f(u) - f(v)}{u - v}, ∣c∣≤K|c| \leq K. So wt−Δw−cw≤0w_t - \Delta w - cw \leq 0 where w>0w > 0. Let w~=e−2Ktw\tilde w = e^{-2Kt}w: then w~t−Δw~+(2K−c)w~≤0\tilde w_t - \Delta\tilde w + (2K - c)\tilde w \leq 0 there, with 2K−c≥K>02K - c \geq K > 0. By part 2 of Theorem 4.1 (applied on the set where w~>0\tilde w > 0), max⁡w~≤max⁡ΓTw~+=0\max\tilde w \leq \max_{\Gamma_T}\tilde w^+ = 0. So w≤0w \leq 0.

Two uses recur.

Comparison with an ODE. Spatially constant functions y(t)y(t) solve ut=Δu+f(u)u_t = \Delta u + f(u) exactly when y′=f(y)y' = f(y). So on a domain where boundary terms are controlled (all of Rn\mathbb{R}^n with bounded solutions, a closed manifold, or a domain with suitable boundary values), a solution that starts above y(0)y(0) stays above y(t)y(t). The PDE is at least as good as its ODE. For example, a solution of ut=Δu+u2u_t = \Delta u + u^2 on a closed manifold with min⁡u(⋅,0)=m>0\min u(\cdot, 0) = m > 0 satisfies u≥m1−mtu \geq \frac{m}{1 - mt} and must blow up by time 1/m1/m (6A.7 Nonlinear Parabolic Equations).

Sandwiching. A solution can be trapped between an explicit subsolution and an explicit supersolution. This is how front speeds are bounded (Figure 4.3), how blow-up times are estimated, and how, in geometric flows, a flowing curve or surface is compared with explicit shrinking spheres: a closed curve inside a circle under curve shortening stays inside the shrinking circle and so must become extinct before it does (6A.8 Curve Shortening and the First Geometric Flows).

Systems and invariant regions

For a system u=(u1,…,um)u = (u^1, \dots, u^m), maximum principles componentwise generally fail. If the components are coupled in their second-order terms, or in their reaction terms, one component can be pushed above its initial maximum by another. What survives is a geometric statement: a closed convex set in the space of values that the reaction terms never push solutions out of is never left by the solution of the full system.

Theorem 4.5 Invariant regions (Weinberger; Chueh, Conley and Smoller)

Let F:Rm→RmF : \mathbb{R}^m \to \mathbb{R}^m be locally Lipschitz, and let K⊂RmK \subset \mathbb{R}^m be closed and convex. Suppose KK is invariant for the ODE y′=F(y)y' = F(y): solutions that start in KK stay in KK. Let u:M×[0,T]→Rmu : M\times[0, T] \to \mathbb{R}^m be a smooth solution of the reaction–diffusion system

ut=Δu+F(u),u_t = \Delta u + F(u),

with the same diffusion operator Δ\Delta acting on every component, on a closed manifold MM (or on Rn\mathbb{R}^n with bounded solutions, or on a bounded domain with values in KK on the boundary). If u(x,0)∈Ku(x, 0) \in K for all xx, then u(x,t)∈Ku(x, t) \in K for all xx and tt.

Proof. (Sketch.) A closed convex set is the intersection of the closed half-spaces containing it, K=⋂{y:ℓ(y)≤cℓ}K = \bigcap\{y : \ell(y) \leq c_\ell\}, over linear functionals ℓ\ell supporting KK (4A.3 Hahn–Banach and Duality). For each such ℓ\ell, the scalar function ϕ=ℓ(u)\phi = \ell(u) satisfies

ϕt=Δϕ+ℓ(F(u)),\phi_t = \Delta\phi + \ell(F(u)),

because ℓ\ell is linear and the same Δ\Delta acts on every component. At a point where ϕ\phi first reaches cℓc_\ell, the value uu is on the boundary of KK with ℓ\ell supporting KK there, and ODE-invariance of KK means F(u)F(u) does not point out of KK, so ℓ(F(u))≤0\ell(F(u)) \leq 0. Then the core argument rules out ϕ\phi crossing cℓc_\ell, after an ε\varepsilon-perturbation as in Theorem 4.1; the full proof replaces this by an argument with the distance from uu to KK, which handles all the half-spaces at once (Chueh, Conley and Smoller, 1977).

The hypotheses matter. Convexity is used to write KK by linear inequalities, which commute with Δ\Delta. Equal diffusion is used so that ℓ(u)\ell(u) solves a scalar heat equation; with different diffusion rates in different components only rectangles (products of intervals) remain invariant in general (Exercise 4.11).

The idea From invariant regions to Hamilton's maximum principle

Under the Ricci flow the curvature operator Rm⁡\operatorname{Rm} evolves by a reaction–diffusion equation

∂tRm⁡=ΔRm⁡+Rm⁡2+Rm⁡#,\partial_t\operatorname{Rm} = \Delta\operatorname{Rm} + \operatorname{Rm}^2 + \operatorname{Rm}^\#,

where the reaction term is quadratic. Hamilton's tensor maximum principle (1986) is Theorem 4.5 in this setting: a closed convex set of curvature operators, invariant under parallel transport, that is preserved by the ODE ddtRm⁡=Rm⁡2+Rm⁡#\frac{d}{dt}\operatorname{Rm} = \operatorname{Rm}^2 + \operatorname{Rm}^\#, is preserved by the Ricci flow. Positive curvature operator, positive Ricci curvature in dimension 3, and the Hamilton–Ivey pinching set are all proved invariant this way, by checking an ODE (11A.4 Maximum Principles under Ricci Flow, 11A.5 Hamilton–Ivey Pinching). The figure Figure 4.2 is redrawn for curvature in 11A.4 Maximum Principles under Ricci Flow.

Figure 4.2. The reaction field F(u,v)=(u(1−u−0.5v), v(1−v−0.6u))F(u, v) = \big(u(1 - u - 0.5v),\ v(1 - v - 0.6u)\big) of a two-species competition model, and the square K=[0,1]2K = [0, 1]^2 (shaded). On every edge FF points into KK or along the edge, so KK is invariant for the ODE, and by Theorem 4.5 the reaction–diffusion system ut=Δu+F(u)u_t = \Delta u + F(u) keeps both population densities between 00 and 11.

Invasion fronts

In the world Model Fisher–KPP and the spread of the muskrat

In 1937 Ronald Fisher, and independently Andrey Kolmogorov, Ivan Petrovsky and Nikolai Piskunov, studied

ut=Duxx+ru(1−u),u_t = Du_{xx} + ru(1 - u),

a model of a population (or an advantageous gene) that diffuses with coefficient DD and grows logistically at rate rr, with uu the density as a fraction of the carrying capacity. The interval [0,1][0, 1] is invariant for the ODE y′=ry(1−y)y' = ry(1 - y), so by comparison with the constant solutions 00 and 11 every solution starting between 00 and 11 stays there (Exercise 4.9). A population introduced in a small region spreads as a travelling front, and the front moves at the speed

c=2rD,c = 2\sqrt{rD},

the slowest speed for which a front connecting 00 to 11 with u≥0u \geq 0 exists (Exercise 4.10, Figure 4.3).

The linear rate is a striking prediction: the radius of the occupied region grows proportionally to time, not to t\sqrt t as for pure diffusion, because growth at the edge keeps refilling it. John Skellam tested it in 1951 on the spread of the muskrat in central Europe, after a few animals were released on an estate southwest of Prague in 1905. Plotting the square root of the area of the occupied range, proportional to its radius, against the year, he found the points close to a straight line, as the model predicts. Similar spreading rates have since been fitted for many invasive species, with the caveats that real landscapes are not uniform and that long-distance jumps can make fronts accelerate.

Figure 4.3. The Fisher–KPP equation ut=uxx+u(1−u)u_t = u_{xx} + u(1 - u) from a step initial state, at t=0,4,8,…,24t = 0, 4, 8, \dots, 24 (computed by an explicit finite-difference scheme). The profiles stay between 00 and 11, as the invariant region requires, and the front (where u=12u = \frac12) advances at a speed approaching the predicted 2rD=22\sqrt{rD} = 2 from below.

Chemistry. Concentrations in reaction–diffusion models of chemical systems should stay non-negative. If each reaction rate Fi(u)F^i(u) is non-negative whenever ui=0u^i = 0 and the other concentrations are non-negative (a substance can't be consumed when there is none of it), then the non-negative orthant is invariant for the ODE, and by the theorem (in its version for products of intervals, which allows different diffusion rates) for the reaction–diffusion system too. Models without this property are physically wrong, and the maximum principle is how one checks.

History

The maximum principle for harmonic functions was known in the nineteenth century; for general second-order elliptic operators the strong maximum principle is due to Eberhard Hopf (1927), and the boundary lemma to Hopf (1952) and, independently, Olga Oleinik (1952), with an earlier version by Stanisław Zaremba (1910). Louis Nirenberg proved the strong maximum principle for parabolic equations in 1953. Invariant regions for reaction–diffusion systems were introduced by Hans Weinberger (1975) and developed by Kuan-Nan Chueh, Charles Conley and Joel Smoller (1977). Richard Hamilton's tensor maximum principle appeared in his 1986 paper on four-manifolds with positive curvature operator. Fisher's and Kolmogorov–Petrovsky–Piskunov's papers are from 1937, and Skellam's from 1951.

Recall Where we stand

At a first interior maximum, ∇u=0\nabla u = 0, ∇2u≤0\nabla^2u \leq 0 and ut≥0u_t \geq 0; perturbing by εt\varepsilon t turns this into the weak maximum principle for parabolic operators, and by εeλx1\varepsilon e^{\lambda x_1} for elliptic ones, with c≥0c \geq 0 allowed for non-negative maxima. Hopf's lemma, proved with a barrier, gives the strong maximum principle. Comparison principles extend all this to semilinear equations, and comparison with the ODE y′=f(y)y' = f(y) bounds solutions of ut=Δu+f(u)u_t = \Delta u + f(u). For systems with equal diffusion, closed convex sets invariant under the reaction ODE are invariant under the PDE: the ancestor of Hamilton's tensor maximum principle. 6A.5 Weak Solutions and Elliptic Regularity turns from pointwise methods to energy methods and weak solutions.

Exercises

Exercise 4.6 A trace inequality

Let AA be symmetric positive semidefinite and HH symmetric negative semidefinite. Show that tr⁡(AH)≤0\operatorname{tr}(AH) \leq 0. (Diagonalise A=∑λkekekTA = \sum\lambda_ke_ke_k^T with λk≥0\lambda_k \geq 0, 1A.6 Symmetric Matrices and the Spectral Theorem, and write tr⁡(AH)=∑λkekTHek\operatorname{tr}(AH) = \sum\lambda_ke_k^THe_k.)

Exercise 4.7 The elliptic weak maximum principle

Let Lu=−∑aij∂i∂ju+∑bi∂iuLu = -\sum a^{ij}\partial_i\partial_ju + \sum b^i\partial_iu with a11≥θ>0a^{11} \geq \theta > 0 and ∣b∣≤β|b| \leq \beta. Show that v=eλx1v = e^{\lambda x_1} satisfies Lv<0Lv < 0 if λ>β/θ\lambda > \beta/\theta, and use u+εvu + \varepsilon v to prove that Lu≤0Lu \leq 0 in a bounded UU implies max⁡U‾u=max⁡∂Uu\max_{\overline U}u = \max_{\partial U}u.

Solution

Lv=(−a11λ2+b1λ)eλx1≤λ(−θλ+β)eλx1<0Lv = (-a^{11}\lambda^2 + b^1\lambda)e^{\lambda x_1} \leq \lambda(-\theta\lambda + \beta)e^{\lambda x_1} < 0. Then L(u+εv)<0L(u + \varepsilon v) < 0, so u+εvu + \varepsilon v cannot have an interior maximum (at one, Lu+εLv≥0Lu + \varepsilon Lv \geq 0 by the core argument). Hence max⁡U‾u≤max⁡U‾(u+εv)=max⁡∂U(u+εv)≤max⁡∂Uu+εmax⁡U‾v\max_{\overline U}u \leq \max_{\overline U}(u + \varepsilon v) = \max_{\partial U}(u + \varepsilon v) \leq \max_{\partial U}u + \varepsilon\max_{\overline U}v; let ε→0\varepsilon \to 0.

Exercise 4.8 The Hopf barrier

For v=e−λ∣x∣2−e−λr2v = e^{-\lambda|x|^2} - e^{-\lambda r^2}, compute ∂iv=−2λxie−λ∣x∣2\partial_iv = -2\lambda x_ie^{-\lambda|x|^2} and ∂i∂jv=(4λ2xixj−2λδij)e−λ∣x∣2\partial_i\partial_jv = (4\lambda^2x_ix_j - 2\lambda\delta_{ij})e^{-\lambda|x|^2}. Show that on r/2≤∣x∣≤rr/2 \leq |x| \leq r,

−∑aij∂i∂jv+∑bi∂iv≤e−λ∣x∣2(−4θλ2∣x∣2+2λtr⁡A+2λ∣b∣∣x∣),-\sum a^{ij}\partial_i\partial_jv + \sum b^i\partial_iv \leq e^{-\lambda|x|^2}\big(-4\theta\lambda^2|x|^2 + 2\lambda\operatorname{tr}A + 2\lambda|b||x|\big),

which is negative once λ\lambda is large.

Exercise 4.9 Fisher–KPP stays in [0,1][0, 1]

Use Theorem 4.4 with f(u)=u(1−u)f(u) = u(1 - u) (Lipschitz on [−1,2][-1, 2], which suffices after a truncation argument) and the constant solutions 00 and 11 to show that a solution on R\mathbb{R} with 0≤u(x,0)≤10 \leq u(x, 0) \leq 1 and bounded derivatives satisfies 0≤u≤10 \leq u \leq 1 for all time. Then show u>0u > 0 for t>0t > 0 unless u≡0u \equiv 0.

Exercise 4.10 The minimal front speed

Look for travelling waves u=U(x−ct)u = U(x - ct) of ut=uxx+u(1−u)u_t = u_{xx} + u(1 - u) with U(−∞)=1U(-\infty) = 1, U(+∞)=0U(+\infty) = 0. (a) Derive U′′+cU′+U(1−U)=0U'' + cU' + U(1 - U) = 0. (b) Linearise at U=0U = 0: U′′+cU′+U=0U'' + cU' + U = 0. Show that if c<2c < 2 the solutions oscillate around 00, so UU would become negative, and conclude c≥2c \geq 2. (With DD and rr restored, c≥2rDc \geq 2\sqrt{rD}.) That c=2c = 2 is actually attained, and is the speed selected from compactly supported data, is the theorem of Kolmogorov, Petrovsky and Piskunov.

Solution

(a) ut=−cU′u_t = -cU', uxx=U′′u_{xx} = U''. (b) The characteristic equation μ2+cμ+1=0\mu^2 + c\mu + 1 = 0 has roots μ=−c±c2−42\mu = \frac{-c \pm\sqrt{c^2 - 4}}{2}, complex when c<2c < 2, giving e−cz/2cos⁡(ωz+ϕ)e^{-cz/2}\cos(\omega z + \phi), which changes sign infinitely often as z→∞z \to \infty. With ut=Duxx+ru(1−u)u_t = Du_{xx} + ru(1 - u), rescale x↦xr/Dx \mapsto x\sqrt{r/D} and t↦rtt \mapsto rt to reduce to D=r=1D = r = 1; speeds scale by rD\sqrt{rD}.

Exercise 4.11 Rectangles with different diffusions

For the system ut=d1Δu+F1(u,v)u_t = d_1\Delta u + F^1(u, v), vt=d2Δv+F2(u,v)v_t = d_2\Delta v + F^2(u, v) with d1≠d2d_1 \neq d_2, show that the rectangle [a1,b1]×[a2,b2][a_1, b_1]\times[a_2, b_2] is invariant if F1≥0F^1 \geq 0 on the edge u=a1u = a_1, F1≤0F^1 \leq 0 on u=b1u = b_1, and similarly for F2F^2. (Apply the scalar comparison principle to each component separately.) Check that the competition model of Figure 4.2 satisfies these conditions on [0,1]2[0, 1]^2.

Exercise 4.12 Rehearsal: the scalar curvature under Ricci flow

Under the Ricci flow on a closed nn-manifold the scalar curvature satisfies ∂tR=ΔR+2∣Ric⁡∣2\partial_tR = \Delta R + 2|\operatorname{Ric}|^2 (11A.2 How Curvature Evolves), and ∣Ric⁡∣2≥1nR2|\operatorname{Ric}|^2 \geq \frac1nR^2 (Cauchy–Schwarz on the eigenvalues of Ric⁡\operatorname{Ric}). (a) Show that Rmin⁡(t)=min⁡xR(x,t)R_{\min}(t) = \min_xR(x, t) is non-decreasing. (b) If Rmin⁡(0)=ρ>0R_{\min}(0) = \rho > 0, compare with the ODE y′=2ny2y' = \frac2ny^2 to show Rmin⁡(t)≥ρ1−2ρntR_{\min}(t) \geq \frac{\rho}{1 - \frac{2\rho}{n}t}, so the flow must become singular by time n2ρ\frac{n}{2\rho}. (c) Check that the round sphere of 6A.1 What a PDE Is's rehearsal becomes singular exactly at this time: for the unit nn-sphere R=n(n−1)R = n(n - 1), and n2n(n−1)=12(n−1)\frac{n}{2n(n-1)} = \frac{1}{2(n - 1)}. This is the first maximum-principle argument of 11A.4 Maximum Principles under Ricci Flow, and Perelman uses its consequence, a lower bound on RR, everywhere.

Solution

(a) ∂tR≥ΔR\partial_tR \geq \Delta R; apply the weak maximum principle (part 1) to −R-R on the closed manifold, which has no boundary. (b) ∂tR≥ΔR+2nR2\partial_tR \geq \Delta R + \frac2nR^2; the ODE solution y=ρ1−2ρt/ny = \frac{\rho}{1 - 2\rho t/n} is a subsolution, and comparison (on a closed manifold, with the Lipschitz constant of 2nR2\frac2nR^2 on the bounded range of RR up to any time before blow-up) gives R≥yR \geq y. Since y→∞y \to \infty as t→n2ρt \to \frac{n}{2\rho}, the flow cannot be smooth past that time. (c) ρ=n(n−1)\rho = n(n - 1) gives n2n(n−1)=12(n−1)\frac{n}{2n(n - 1)} = \frac{1}{2(n - 1)}, the extinction time computed directly in 6A.1 What a PDE Is.

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