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arXiv:2610.20265v1 [math.DG] 14 Oct 2026

Geometric π‘ͺ𝟏\bm{C^{1}}-stability of geodesic spheres under volume-preserving mean curvature flow

Esther Cabezas-Rivas Address: Esther Cabezas-Rivas Universitat de ValΓ¨ncia Departament de MatemΓ tiques Av. Vicent AndrΓ©s EstellΓ©s 19 46100 Burjassot Spain esther.cabezas-rivas@uv.es and Carlo Sinestrari Address: Carlo Sinestrari UniversitΓ  degli Studi di Roma ”Tor Vergata” Dipartimento di Matematica Via della Ricerca Scientifica 00133, Roma Italy sinestra@mat.uniroma2.it
Date: October 14, 2026. This work has been partially supported by project PID2025-174652NB-I00, funded by MICIU/AEI /10.13039/501100011033 and by ERDF, EU. The first author has also been partially supported by project CIAICO/2023/035, funded by the Conselleria d’EducaciΓ³, Cultura, Universitats i OcupaciΓ³. The second author has been partially supported by MUR (Ministero dell’UniversitΓ  e della Ricerca) Project MatMod@TOV 2037-2027, CUP E83C23000330006 and by the MUR Prin 2022 Project CUP E53D23005750006. The second author is a member of INdAM (Istituto Nazionale di Alta Matematica).
Abstract.

We prove stability of geodesic spheres under volume-preserving mean curvature flow in the simply connected space forms under genuinely first-order geometric assumptions. The initial hypersurface is required to lie in a sufficiently thin annulus around a geodesic sphere and to have outward normal making a small angle with the radial direction. No convexity, mean convexity, initial curvature bound, or HΓΆlder control of the normal is assumed.

The main ingredient is a quantitative Alexandrov reflection argument that converts these initial assumptions into a strong reflection property preserved by the flow. The resulting radial and angular control allows us to derive estimates for the mean curvature and the full second fundamental form, and hence long-time existence, eventual convexity, and smooth exponential convergence to a geodesic sphere. In hyperbolic space, the eventual convexity can be strengthened to horospherical convexity. The reflection threshold also yields a quantitative estimate for the displacement of the limiting centre.

For Lipschitz initial hypersurfaces, we develop a separate positive-time curvature estimate that is uniform along smooth approximations. This produces an instantaneously smooth evolution with the same eventual convexity and smooth exponential convergence.

Key words and phrases:
Mean curvature flow; stability; volume-preserving; Alexandrov reflection
2020 Mathematics Subject Classification
53E10, 35B35, 53C21, 35B40

1. Introduction and main results

Volume-preserving mean curvature flow is the constrained gradient flow of area under fixed enclosed volume. Its equilibria are closed constant-mean-curvature hypersurfaces, including round spheres in Euclidean space. A fundamental problem is to identify conditions on the initial data that prevent singularity formation and force the flow to exist for all time and converge to a steady state. Classical convergence results [25, 18, 27, 3, 9] typically require convexity, pointwise or integral curvature pinching, or closeness to a sphere in a topology that quantitatively controls the variation of the normal.

In this paper, we show that the stability of geodesic spheres can be established under purely first-order geometric assumptions. The initial hypersurface is required only to lie in a sufficiently thin annulus around a geodesic sphere and to have outward unit normal making a small angle with the radial direction. No convexity or mean convexity is assumed, and no initial curvature bound or quantitative modulus of continuity of the normal is imposed. We prove that the corresponding volume-preserving mean curvature flow exists for all time, becomes strictly convex, and converges smoothly and exponentially to a geodesic sphere. We also extend the construction to Lipschitz initial hypersurfaces by deriving positive-time smoothing estimates that are uniform along smooth approximations.

To state our results precisely, let MM be a smooth, closed, nn-dimensional manifold and let X0:M→ℝn+1X_{0}:M\rightarrow\mathbb{R}^{n+1} be a smooth embedding. We denote by M0=X0​(M)M_{0}=X_{0}(M) the corresponding embedded hypersurface and assume that M0M_{0} bounds a domain Ξ©0\Omega_{0}. Let R0>0R_{0}>0 be determined by vol⁑(Ξ©0)=Ο‰n+1​R0n+1,\operatorname{vol}(\Omega_{0})=\omega_{n+1}R_{0}^{n+1}, where Ο‰n+1\omega_{n+1} denotes the volume of the unit ball in ℝn+1\mathbb{R}^{n+1}.

We assume that M0M_{0} is C1C^{1}-close to the sphere βˆ‚BR0​(0)\partial B_{R_{0}}(0) in the following sense: there exist Ξ΅0∈(0,1)\varepsilon_{0}\in(0,1) and ΞΈ0∈(0,Ο€/2)\theta_{0}\in(0,\pi/2) such that

(1.1) R0​(1βˆ’Ξ΅0)≀|x|≀R0​(1+Ξ΅0)for every ​x∈M0,R_{0}(1-\varepsilon_{0})\leq|x|\leq R_{0}(1+\varepsilon_{0})\qquad\text{for every }x\in M_{0},

and

(1.2) ⟨ν0​(x),x|x|⟩β‰₯cos⁑θ0for every ​x∈M0,\left\langle\nu_{0}(x),\frac{x}{|x|}\right\rangle\geq\cos\theta_{0}\qquad\text{for every }x\in M_{0},

where Ξ½0\nu_{0} is the outward unit normal to M0M_{0}.

We refer to (1.1) and (1.2) as the annular-closeness and the normal-oscillation assumption, respectively. They can be regarded as a geometric formulation of C1C^{1}-closeness to βˆ‚BR0​(0)\partial B_{R_{0}}(0). Indeed, (1.2) implies that M0M_{0} is star-shaped with respect to the origin, so that M0M_{0} is a radial graph over π•Šn\mathbb{S}^{n}; then (1.1) and (1.2) are equivalent to a bound on the height and gradient of its graph function.

We consider the volume-preserving mean curvature flow

(1.3) βˆ‚tX⁑(p,t)=(h⁑(t)βˆ’H⁑(p,t))​ν​(p,t),p∈M,t>0,\partial_{t}X(p,t)=\bigl(h(t)-H(p,t)\bigr)\nu(p,t),\qquad p\in M,\quad t>0,

with X⁑(β‹…,0)=X0X(\cdot,0)=X_{0}, where h⁑(t)h(t) is the averaged mean curvature, that is,

(1.4) h⁑(t)=1|Mt|β€‹βˆ«MtH​d​μt.h(t)=\frac{1}{|M_{t}|}\int_{M_{t}}H\,d\mu_{t}.

Here Mt=X⁑(M,t)M_{t}=X(M,t), while HH and Ξ½\nu denote its mean curvature and outward unit normal, respectively. Our sign convention is such that βˆ’H​ν-H\nu points inwards on a convex hypersurface (i.e. with ΞΊ1β‰₯0\kappa_{1}\geq 0, where ΞΊ1≀⋯≀κn\kappa_{1}\leq\cdots\leq\kappa_{n} denote the principal curvatures).

Our stability result in the Euclidean setting reads as follows.

Theorem 1.1.

For every nβ‰₯1n\geq 1, there exists Ξ΄βˆ—=Ξ΄βˆ—β€‹(n)>0\delta_{*}=\delta_{*}(n)>0 with the following property. Let M0βŠ‚β„n+1M_{0}\subset\mathbb{R}^{n+1} satisfy (1.1) and (1.2) with Ξ΅0+ΞΈ0<Ξ΄βˆ—.\varepsilon_{0}+\theta_{0}<\delta_{*}. Then (1.3) satisfies the following:

  1. (a)

    It has a unique smooth solution, defined for every tβ‰₯0t\geq 0.

  2. (b)

    The hypersurfaces MtM_{t} remain uniformly star-shaped and satisfy uniform curvature bounds.

  3. (c)

    There exists T<∞T<\infty such that MtM_{t} is strictly convex for every tβ‰₯Tt\geq T.

  4. (d)

    As tβ†’βˆžt\to\infty, MtM_{t} converges exponentially fast in the C∞C^{\infty} topology to a round sphere BR0​(p∞)B_{R_{0}}(p_{\infty}) for some pβˆžβˆˆβ„n+1p_{\infty}\in\mathbb{R}^{n+1}. More precisely, for every kβˆˆβ„•k\in\mathbb{N}, there exist constants Ck,Ξ»k>0C_{k},\lambda_{k}>0 such that

    distCk⁑(Mt,βˆ‚BR0​(p∞))≀Ck​eβˆ’Ξ»k​tΒ for all sufficiently largeΒ t.Β \operatorname{dist}_{C^{k}}\bigl(M_{t},\partial B_{R_{0}}(p_{\infty})\bigr)\leq C_{k}e^{-\lambda_{k}t}\qquad\text{ for all sufficiently large $t$. }
  5. (e)

    The centre of the limiting sphere satisfies

    |p∞|≀R02​Φ​(Ξ΅0,ΞΈ0),whereΦ⁑(Ξ΅,ΞΈ)=(1+Ξ΅)​sin⁑θ+(1+Ξ΅)2​sin2⁑θ+4​Ρ.|p_{\infty}|\leq\frac{R_{0}}{2}\Phi(\varepsilon_{0},\theta_{0}),\qquad\text{where}\quad\Phi(\varepsilon,\theta)=(1+\varepsilon)\sin\theta+\sqrt{(1+\varepsilon)^{2}\sin^{2}\theta+4\varepsilon}.

In particular, |p∞|≀R0​(2​θ0+Ξ΅0)|p_{\infty}|\leq R_{0}\bigl(2\theta_{0}+\sqrt{\varepsilon_{0}}\bigr) for sufficiently small initial parameters, giving a control on the displacement from the reference centre.

Our method of proof is based on the Alexandrov reflection technique, adapted to the setting of geometric flows given by Chow and Gulliver [13]. The approach is therefore direct and geometric compared with some of the techniques of the previous literature, e.g. integral estimates [25, 27] or the functional analytic techniques employed in [18].

The Euclidean result contains the core reflection mechanism, but extending it to the nonflat space forms requires additional geometric input. Alexandrov reflection remains available after replacing affine hyperplanes by totally geodesic hypersurfaces. In the spherical case, however, the reflection construction is necessarily restricted to a hemisphere, while in both nonflat settings the evolution equations contain ambient-curvature terms that must be incorporated into the curvature estimates and the late-time analysis.

Hence, with some additional work, we can extend our C1C^{1}-stability result to the non-flat setting as follows. Let NKn+1N_{K}^{n+1} denote the simply connected space form of constant sectional curvature K∈{βˆ’1,1}K\in\{-1,1\}, and fix o∈NKn+1o\in N_{K}^{n+1}. Now BRK​(p)B_{R}^{K}(p) represents the geodesic ball of radius RR centred at p∈NKn+1p\in N_{K}^{n+1}. Consider M0βŠ‚NKn+1M_{0}\subset N_{K}^{n+1} a smooth, closed and embedded hypersurface enclosing a domain Ξ©0\Omega_{0}, and let R0>0R_{0}>0 be determined by vol⁑(Ξ©0)=vol⁑(BR0K​(o)).\operatorname{vol}(\Omega_{0})=\operatorname{vol}\bigl(B_{R_{0}}^{K}(o)\bigr). Writing r⁑(x)=distNK⁑(o,x),r(x)=\operatorname{dist}_{N_{K}}(o,x), we assume that

(1.5) R0​(1βˆ’Ξ΅0)≀r⁑(x)≀R0​(1+Ξ΅0)for every ​x∈M0,R_{0}(1-\varepsilon_{0})\leq r(x)\leq R_{0}(1+\varepsilon_{0})\qquad\text{for every }x\in M_{0},
(1.6) ⟨ν0,βˆ‚r⟩β‰₯cosΞΈ0onΒ M0.\left\langle\nu_{0},\partial_{r}\right\rangle\geq\cos\theta_{0}\qquad\text{on }M_{0}.
Theorem 1.2 (Nonflat space-form extension).

Let 1≀nβˆˆβ„•1\leq n\in\mathbb{N}, K∈{βˆ’1,1}K\in\{-1,1\}, and let M0βŠ‚NKn+1M_{0}\subset N_{K}^{n+1} satisfy (1.5) and (1.6). In the spherical case, assume also that R0​(1+Ξ΅0)<Ο€2.R_{0}(1+\varepsilon_{0})<\frac{\pi}{2}. If Ξ΅0\varepsilon_{0} and ΞΈ0\theta_{0} are sufficiently small, then conclusions (a)–(d) of Theorem 1.1 hold, with round spheres replaced by geodesic spheres in NKn+1N_{K}^{n+1}. In particular, the limiting hypersurface is βˆ‚BR0K​(p∞)\partial B_{R_{0}}^{K}(p_{\infty}) for some p∞∈NKn+1p_{\infty}\in N_{K}^{n+1}. In addition, when K=βˆ’1K=-1, the evolving hypersurfaces become strictly horospherically convex for all sufficiently large times. The conclusion about the centre is now

distNK⁑(o,p∞)≀ωK​(R0,Ξ΅0,ΞΈ0),\operatorname{dist}_{N_{K}}(o,p_{\infty})\leq\omega_{K}(R_{0},\varepsilon_{0},\theta_{0}),

for a suitable positive function Ο‰K\omega_{K} satisfying Ο‰K​(R0,Ξ΅0,ΞΈ0)β†’0\omega_{K}(R_{0},\varepsilon_{0},\theta_{0})\to 0 as Ξ΅0+ΞΈ0β†’0\varepsilon_{0}+\theta_{0}\to 0.

The use of the initial assumptions in the reflection technique requires a different argument in the non-flat case, and the estimates are not as direct and explicit as in Euclidean space. This leads to the different formulation of the displacement estimate at the end of the statement.

The geometric assumptions in the above results involve only the radial position and the radial tilt of the initial hypersurface, and therefore remain meaningful for Lipschitz radial graphs. By combining smooth approximation with uniform curvature estimates, we extend the stability result to this rough-data setting as follows.

Theorem 1.3 (Lipschitz initial hypersurfaces).

Let 1≀nβˆˆβ„•1\leq n\in\mathbb{N}, K∈{βˆ’1,0,1}K\in\{-1,0,1\}, and M0βŠ‚NKn+1M_{0}\subset N_{K}^{n+1} be a closed embedded Lipschitz hypersurface that satisfies the geometric assumptions of Theorem 1.1 or Theorem 1.2, with the normal-oscillation condition understood almost everywhere. Then there exists an instantaneously smooth volume-preserving mean curvature flow (Mt)t>0,(M_{t})_{t>0}, with initial condition M0M_{0} in the following continuous sense: writing MtM_{t} and M0M_{0} as radial graphs with respect to the reference point oo, with radial functions ρ⁑(β‹…,t)\rho(\cdot,t) and ρ0\rho_{0}, respectively, one has

ρ⁑(β‹…,t)⟢ρ0uniformly as ​tβ†˜0.\rho(\cdot,t)\longrightarrow\rho_{0}\qquad\text{uniformly as }t\searrow 0.

In particular, MtM_{t} converges to M0M_{0} in the Hausdorff sense and encloses the same volume as M0M_{0}. The flow has the same eventual convexity and exponential convergence properties as in the corresponding smooth theorems.

Relation to previous work and main novelty

There is a rich literature on convergence for the flow (1.3). Huisken [25] proved global existence and convergence to a round sphere for convex hypersurfaces in ℝn+1\mathbb{R}^{n+1}, nβ‰₯2n\geq 2, while the corresponding result for curves is due to Gage [20]. A different line of research, initiated by Escher and Simonett [18], replaces convexity by perturbative closeness to a sphere in the little HΓΆlder space h1+Ξ±h^{1+\alpha}, using centre-manifold and maximal-regularity methods. Similar stability results were obtained under Sobolev smallness assumptions in [7], under integral curvature pinching in [27], and, for strictly stable critical sets in flat tori, under C1,1C^{1,1}-small perturbations in [16].

Related results in nonflat space forms rely on stronger geometric or functional hypotheses. In hyperbolic space, the first author and Miquel [9] proved convergence from horospherically convex hypersurfaces and from C1,Ξ±C^{1,\alpha}-perturbations of geodesic spheres, while subsequent works [23, 35, 28] considered L2L^{2}-almost umbilical initial hypersurfaces. Hartley [21] treated constrained curvature flows near geodesic spheres in π•Šn+1\mathbb{S}^{n+1}, under smallness assumptions in spaces h2+Ξ±h^{2+\alpha}. For curves on pinched Hadamard surfaces (i.e. allowing some variable negative ambient curvature), [1, Theorem 1.3] established stability of geodesic circles under h1+Ξ²h^{1+\beta}-small perturbations.

All the aforementioned results either impose bounds on the curvature, in a pointwise or integral sense, or consider perturbations of a sphere in a functional norm which implies at least C1,Ξ±C^{1,\alpha} smallness. Our hypotheses instead control only the radial position of the hypersurface and the pointwise angle of its normal with the radial direction. In particular, they impose no direct bound on the second fundamental form and no HΓΆlder control of the normal, whose spatial variation may be arbitrarily rapid. The first-order nature of our assumptions is essential. Mere C0C^{0}-closeness does not prevent singularities: one may attach to a sphere an arbitrarily small bubble through a sufficiently thin neck, producing a hypersurface arbitrarily close to the sphere in C0C^{0} whose flow develops a neckpinch.

Our approach is based on quantitative Alexandrov reflection, in the form developed for geometric flows by Chow and Gulliver [13, 12]. Reflection has been used mainly for expanding flows and, more recently, for constrained flows in Euclidean and hyperbolic space, in combination with convexity or related positive-curvature assumptions; see [8, 22, 6, 4, 5, 34]. Here, by contrast, quantitative reflection and geometric C1C^{1}-closeness determine each other, up to a change of parameters. The preserved reflection threshold therefore controls both the first-order geometry and the displacement of the limiting centre from the prescribed reference centre.

For more general ambient manifolds, convergence to constant-mean-curvature hypersurfaces has been established for suitably C2C^{2}-round or non-degenerate perturbations of small geodesic spheres [26, 31, 3, 30]. In this generality, reflection symmetries may be unavailable and closed constant-mean-curvature hypersurfaces may be unstable. The stability studied here is therefore tied to the geometry of the ambient space.

Strategy of the proof

The fundamental step is to establish a quantitative relation between our geometric assumptions and a strong Alexandrov reflection property. Proposition 3.1 shows that the initial annular-closeness and normal-oscillation assumptions imply reflection across hyperplanes in every direction up to a common threshold, located at a small distance from the center of the reference sphere. Conversely, Corollary 3.5 shows that, within the volume-normalized class, such a threshold controls both the radial oscillation and the tilt of the hypersurface. Thus, up to a quantitative change of parameters, strong reflection and geometric C1C^{1}-closeness determine each other.

The decisive advantage of the reflection formulation is its invariance under the flow. By the reflection principle of Chow and Gulliver [13], the initial reflection property is preserved for all positive times. Consequently, the evolving hypersurface remains in a fixed annular region and its normal remains uniformly close to the radial direction. These preserved first-order bounds provide the geometric input needed to recover the missing curvature estimates.

More precisely, the radial and angular estimates give a two-sided bound for the support function, allowing us to adapt Tso’s maximum-principle argument [33] to control the mean curvature. This step is more delicate than in the standard convex setting, since neither HH nor its spatial average hh has a prescribed sign. The full second fundamental form is then controlled in Proposition 4.4 by applying the maximum principle to a weighted quantity as in Ecker-Huisken’s interior estimates [17]. Since the tilt is measured relative to the spatially varying radial direction rather than to a fixed ambient vector, its evolution produces additional radial terms. The radial and angular bounds provided by Alexandrov reflection allow us to control these contributions.

Global existence is then obtained by parabolic regularity and a continuation argument. The area dissipation implies smooth subsequential convergence to a closed constant-mean-curvature hypersurface, which is a sphere by Alexandrov’s theorem; volume preservation determines its radius. A sufficiently late time slice is therefore uniformly convex, allowing the flow to enter the classical stability regime and giving exponential convergence to a sphere. Finally, the preserved reflection property passes to the limiting ball and yields the quantitative estimate for its centre.

The same overall strategy applies to nonflat space forms, with the Euclidean position vector replaced by the radial conformal vector field sK(r)βˆ‚r.s_{K}(r)\partial_{r}. The initial reflection threshold, however, must be estimated by a different argument. We first analyse it quantitatively for an off-centred geodesic sphere and then extend the estimate to hypersurfaces satisfying the annular and normal-oscillation assumptions by a perturbative continuity argument. This yields the radial and normal estimates needed for the curvature argument. The evolution equations now contain additional ambient-curvature terms, whose control uses the same preserved first-order geometry but requires separate estimates.

Although the reflection trick is common to the three space forms, the late-time analysis is not. In hyperbolic space, smooth subsequential convergence places the flow in the strictly horospherically convex regime, and the conclusion follows from the convergence theorem of [9]. In the spherical case, convexity alone does not provide an analogous route to convergence. We therefore develop a separate self-contained bootstrap. For nβ‰₯2n\geq 2, it is based on the evolution of the curvature pinching and the favourable sign of the relevant ambient-curvature contribution near a geodesic sphere; for curves, the corresponding conclusion is obtained by an energy argument.

The passage to Lipschitz initial data requires a separate curvature argument. Smooth volume-normalized approximations retain the same uniform first-order geometric bounds, but the mean-curvature estimate used in the smooth theory is not uniform because its constant depends on the initial curvature. We therefore bypass that estimate and apply a modified weighted maximum-principle argument directly to the full second fundamental form. The resulting positive-time curvature estimates are uniform along the approximating sequence and yield smooth compactness away from the initial time. The integrability of the radial velocity near t=0t=0 then shows that the limit flow converges to the prescribed initial hypersurface and encloses the same volume. The argument of the smooth case then gives the same exponential convergence to a sphere.

Organization of the paper

Section 2 collects the evolution equations and introduces the Alexandrov reflection framework. Section 3 establishes the quantitative correspondence between the Euclidean reflection property and the radial and normal estimates, and shows that the latter are preserved along the flow. Section 4 derives the bounds for the mean curvature and the full second fundamental form. Section 5 proves long-time existence, eventual convexity, smooth exponential convergence, and the quantitative estimate for the centre of the limiting sphere in Euclidean space. Section 6 extends the argument to hyperbolic and spherical space forms, including the ambient-curvature terms and the separate late-time analysis required in each setting. Finally, Section 7 treats Lipschitz initial hypersurfaces by smooth approximation and establishes the uniform positive-time estimates required for instantaneous regularization and the subsequent long-time behaviour.

2. Notation, conventions and preliminary results

Throughout the paper, MtM_{t} is a time-dependent closed embedded hypersurface in a space form, g=(gi​j)g=(g_{ij}) denotes the induced metric on MtM_{t}, βˆ‡\nabla its Levi-Civita connection, and Ξ”\Delta the Laplace–Beltrami operator. We denote by A=(hij)A=(h_{i}^{j}) the Weingarten operator with respect to the outward unit normal Ξ½\nu, and by H=trg⁑AH=\operatorname{tr}_{g}A the mean curvature. Our sign convention is such that the principal curvatures of the outward-oriented sphere βˆ‚BR​(p)\partial B_{R}(p) are all positive.

Indices are raised and lowered using gg, and repeated indices above and below are summed. We write

|A|2=hij​hji,tr⁑(A3)=hij​hjk​hki.|A|^{2}=h_{i}^{j}h_{j}^{i},\qquad\operatorname{tr}(A^{3})=h_{i}^{j}h_{j}^{k}h_{k}^{i}.

The notation Sβˆ—TS*T will denote a linear combination of contractions of the tensors SS and TT with respect to gg. Constants denoted by CC may change from line to line and depend only on the fixed parameters and the initial hypersurface, unless otherwise stated.

In the first part of the paper, we consider the flow in a Euclidean ambient space. We collect the evolution equations which we will later use in the curvature estimates. All geometric quantities below are computed on MtM_{t}, and the time derivative is taken in the parametrization determined by (1.3).

Lemma 2.1 (Evolution equations).

Under the vp-mcf (1.3) in ℝn+1\mathbb{R}^{n+1}, the following holds:

  1. (a)

    (βˆ‚tβˆ’Ξ”)H=(Hβˆ’h)|A|2(\partial_{t}-\Delta)H=(H-h)|A|^{2}.

  2. (b)

    The support function u=⟨X,ν⟩u=\langle X,\nu\rangle satisfies (βˆ‚tβˆ’Ξ”)u=hβˆ’2H+|A|2u(\partial_{t}-\Delta)u=h-2H+|A|^{2}u.

  3. (c)

    (βˆ‚tβˆ’Ξ”)|A|2=βˆ’2|βˆ‡A|2+2|A|4βˆ’2htr(A3).(\partial_{t}-\Delta)|A|^{2}=-2|\nabla A|^{2}+2|A|^{4}-2h\operatorname{tr}(A^{3}).

Following [13], we introduce the terminology for reflection of a closed hypersurface across a hyperplane.

Definition 2.2 (Reflection across a hyperplane).

Let MβŠ‚β„n+1M\subset\mathbb{R}^{n+1} be a smooth, closed, embedded hypersurface bounding an open domain Ξ©\Omega, and let

Ξ =Ξ Ξ»,e:={xβˆˆβ„n+1:⟨x,e⟩=Ξ»},\Pi=\Pi_{\lambda,e}:=\left\{x\in\mathbb{R}^{n+1}:\langle x,e\rangle=\lambda\right\},

for given eβˆˆπ•Šne\in\mathbb{S}^{n} and Ξ»βˆˆβ„\lambda\in\mathbb{R}. We denote the two open half-spaces determined by Ξ \Pi by

Ξ +:={xβˆˆβ„n+1:⟨x,e⟩>Ξ»},Ξ βˆ’:={xβˆˆβ„n+1:⟨x,e⟩<Ξ»}.\Pi^{+}:=\left\{x\in\mathbb{R}^{n+1}:\langle x,e\rangle>\lambda\right\},\qquad\Pi^{-}:=\left\{x\in\mathbb{R}^{n+1}:\langle x,e\rangle<\lambda\right\}.
  1. (a)

    The reflection across Ξ \Pi is the Euclidean isometry

    ℛΠ​(x)=xβˆ’2​(⟨x,eβŸ©βˆ’Ξ»)​e.\mathcal{R}_{\Pi}(x)=x-2\bigl(\langle x,e\rangle-\lambda\bigr)e.

    In particular, ℛΠ​(Ξ +)=Ξ βˆ’\mathcal{R}_{\Pi}(\Pi^{+})=\Pi^{-}, ℛΠ​(Ξ βˆ’)=Ξ +\mathcal{R}_{\Pi}(\Pi^{-})=\Pi^{+}, and β„›Ξ \mathcal{R}_{\Pi} fixes every point of Ξ \Pi.

  2. (b)

    MM reflects across Ξ \Pi in the direction ee if the reflection of the portion of Ξ©\Omega lying in Ξ +\Pi^{+} is contained in Ξ©\Omega, namely

    (2.1) ℛΠ​(Ω∩Π+)βŠ‚Ξ©βˆ©Ξ βˆ’.\mathcal{R}_{\Pi}\bigl(\Omega\cap\Pi^{+}\bigr)\subset\Omega\cap\Pi^{-}.

    Equivalently, the reflected cap ℛΠ​(M∩Π+)\mathcal{R}_{\Pi}\bigl(M\cap\Pi^{+}\bigr) does not cross MM and lies in Ξ©Β―βˆ©Ξ βˆ’\overline{\Omega}\cap\Pi^{-}.

  3. (c)

    MM reflects strictly across Ξ \Pi if

    ℛΠ​(M∩Π+)βŠ‚Ξ©βˆ©Ξ βˆ’\mathcal{R}_{\Pi}\bigl(M\cap\Pi^{+}\bigr)\subset\Omega\cap\Pi^{-}

    and if the direction ee is not tangent to MM at any point of M∩ΠM\cap\Pi.

  4. (d)

    MM reflects strictly up to Ξ Ξ»,e\Pi_{\lambda,e} if it reflects strictly across every parallel hyperplane Ξ ΞΌ,e\Pi_{\mu,e} with ΞΌβ‰₯Ξ»\mu\geq\lambda.

In the present paper, the hyperplanes Ξ Ξ»,e\Pi_{\lambda,e} are always taken with Ξ»>0\lambda>0 and therefore Ξ +\Pi^{+} is the side of the reflecting hyperplane which is farther from the origin.

Reflection across a hyperplane is an ambient isometry and therefore preserves the local geometric terms in the evolution equation. Moreover, the original and reflected hypersurfaces carry the same spatially constant term h⁑(t)h(t), which cancels when their local graph equations are compared. Hence the interior and boundary tangency arguments in [13, Theorem 2.2] apply without change, and we obtain the following result.

Theorem 2.3 (Preservation of the reflection property; cf. Chow–Gulliver).

Let MtβŠ‚β„n+1M_{t}\subset\mathbb{R}^{n+1} be a solution of the volume-preserving mean curvature flow (1.3), for t∈[0,T)t\in[0,T). If M0M_{0} reflects strictly across (resp. up to) Ξ Ξ»,e\Pi_{\lambda,e} for some eβˆˆπ•Šne\in\mathbb{S}^{n} and Ξ»βˆˆβ„\lambda\in\mathbb{R}, then MtM_{t} also reflects strictly across (resp. up to) Ξ Ξ»,e\Pi_{\lambda,e}, for all t∈[0,T)t\in[0,T).

3. C1C^{1}-control along the flow via Alexandrov reflection

3.1. Alexandrov reflection property at the initial time

We first show that our assumptions on M0M_{0} imply the reflection property up to a certain threshold, whose size can be estimated in terms of the constants appearing in (1.1) and (1.2).

Proposition 3.1.

Let c0>0c_{0}>0 satisfy

(3.1) 2​c0R0>Ξ¦(Ξ΅0,ΞΈ0):=(1+Ξ΅0)sinΞΈ0+(1+Ξ΅0)2​sin2⁑θ0+4​Ρ0.\frac{2c_{0}}{R_{0}}>\Phi(\varepsilon_{0},\theta_{0}):=(1+\varepsilon_{0})\sin\theta_{0}+\sqrt{(1+\varepsilon_{0})^{2}\sin^{2}\theta_{0}+4\varepsilon_{0}}.\textbf{}

Then M0M_{0} reflects strictly up to Ξ =Ξ c0,e\Pi=\Pi_{c_{0},e}, for every eβˆˆπ•Šne\in\mathbb{S}^{n}.

Proof.

After a rotation we may assume that

Ξ ={xβˆˆβ„n+1:⟨x,en+1⟩=c0}.\Pi=\{x\in\mathbb{R}^{n+1}:\langle x,e_{n+1}\rangle=c_{0}\}.

The goal is to show that the part of M0M_{0} lying above the hyperplane Ξ \Pi reflects into the domain enclosed by M0M_{0}.

It is convenient to write points xβˆˆβ„n+1x\in\mathbb{R}^{n+1} as x=(xΒ―,xn+1)βˆˆβ„n×ℝx=(\bar{x},x_{n+1})\in\mathbb{R}^{n}\times\mathbb{R}. So let us take any x=(xΒ―,xn+1)∈M0x=(\bar{x},x_{n+1})\in M_{0} with xn+1>c0x_{n+1}>c_{0}, and denote by

x~=(xΒ―,2​c0βˆ’xn+1)\widetilde{x}=(\bar{x},2c_{0}-x_{n+1})

its reflection across Π\Pi. Suppose, in order to get a contradiction, that x~∈M0\widetilde{x}\in M_{0}. By the Hausdorff closeness assumption (1.1), we can write

R02​(1βˆ’Ξ΅0)2≀|x~|2=|x|2βˆ’4​c0​(xn+1βˆ’c0)≀R02​(1+Ξ΅0)2βˆ’4​c0​(xn+1βˆ’c0).R_{0}^{2}(1-\varepsilon_{0})^{2}\leq|\widetilde{x}|^{2}=|x|^{2}-4c_{0}(x_{n+1}-c_{0})\leq R_{0}^{2}(1+\varepsilon_{0})^{2}-4c_{0}(x_{n+1}-c_{0}).

Hence

4​c0​(xn+1βˆ’c0)≀R02​((1+Ξ΅0)2βˆ’(1βˆ’Ξ΅0)2)=4​Ρ0​R02,4c_{0}(x_{n+1}-c_{0})\leq R_{0}^{2}\bigl((1+\varepsilon_{0})^{2}-(1-\varepsilon_{0})^{2}\bigr)=4\varepsilon_{0}R_{0}^{2},

and therefore

c0≀xn+1≀c0+Ξ΅0​R02c0.c_{0}\leq x_{n+1}\leq c_{0}+\frac{\varepsilon_{0}R_{0}^{2}}{c_{0}}.

Consequently, x~n+1=2​c0βˆ’xn+1\widetilde{x}_{n+1}=2c_{0}-x_{n+1} satisfies

c1:=c0βˆ’Ξ΅0​R02c0≀x~n+1≀c0.c_{1}:=c_{0}-\frac{\varepsilon_{0}R_{0}^{2}}{c_{0}}\leq\widetilde{x}_{n+1}\leq c_{0}.

Hence, an intersection between M0M_{0} and its reflection can only occur at points with height at least c1c_{1}. Observe that our assumption on c0c_{0} implies 2​c0>R0​4​Ρ02c_{0}>R_{0}\sqrt{4\varepsilon_{0}}, hence c1>0c_{1}>0.

We want to show that M0∩{xn+1β‰₯c1}M_{0}\cap\{x_{n+1}\geq c_{1}\} is a graph over the hyperplane {xn+1=0}\{x_{n+1}=0\}. Let z∈M0∩{xn+1β‰₯c1}z\in M_{0}\cap\{x_{n+1}\geq c_{1}\}, and denote by ΞΎ=z/|z|\xi=z/|z| the radial direction. Since assumption (1.2) ensures that

⟨ν⁑(z),ξ⟩β‰₯cos⁑θ0,\left\langle\nu(z),\xi\right\rangle\geq\cos\theta_{0},

the angle between ν⁑(z)\nu(z) and ξ\xi is at most θ0\theta_{0}. Now we can write

ν⁑(z)=cos⁑α​ξ+sin⁑α​η,\nu(z)=\cos\alpha\,\xi+\sin\alpha\,\eta,

where η\eta is a unit vector orthogonal to ξ\xi, and α∈[0,θ0]\alpha\in[0,\theta_{0}] denotes the angle between ν⁑(z)\nu(z) and ξ\xi. Decomposing en+1e_{n+1} into its components parallel and orthogonal to ξ\xi, we have

en+1=zn+1|z|​ξ+1βˆ’zn+12|z|2β€‹ΞΎβŸ‚,e_{n+1}=\frac{z_{n+1}}{|z|}\xi+\sqrt{1-\frac{z_{n+1}^{2}}{|z|^{2}}}\,\xi^{\perp},

for some unit vector ΞΎβŸ‚βŸ‚ΞΎ\xi^{\perp}\perp\xi. Using Cauchy-Schwarz, we deduce

⟨ν⁑(z),en+1⟩β‰₯zn+1|z|​cosβ‘Ξ±βˆ’1βˆ’zn+12|z|2​sin⁑α.\displaystyle\langle\nu(z),e_{n+1}\rangle\geq\frac{z_{n+1}}{|z|}\cos\alpha-\sqrt{1-\frac{z_{n+1}^{2}}{|z|^{2}}}\sin\alpha.

Since zn+1>0z_{n+1}>0, the right-hand side is decreasing as a function of α∈[0,θ0]\alpha\in[0,\theta_{0}]. Hence

(3.2) ⟨ν(z),en+1⟩β‰₯zn+1|z|cosΞΈ0βˆ’1βˆ’zn+12|z|2sinΞΈ0.\langle\nu(z),e_{n+1}\rangle\geq\frac{z_{n+1}}{|z|}\cos\theta_{0}-\sqrt{1-\frac{z_{n+1}^{2}}{|z|^{2}}}\sin\theta_{0}.

The right-hand side is positive provided

zn+1|z|>sin⁑θ0.\frac{z_{n+1}}{|z|}>\sin\theta_{0}.

Using zn+1β‰₯c1z_{n+1}\geq c_{1} and |z|≀R0​(1+Ξ΅0)|z|\leq R_{0}(1+\varepsilon_{0}), and recalling the definition of c1c_{1}, we see from (3.2) that ⟨ν⁑(z),en+1⟩>0\langle\nu(z),e_{n+1}\rangle>0 provided

(3.3) c0βˆ’Ξ΅0​R02c0>R0(1+Ξ΅0)sinΞΈ0.c_{0}-\dfrac{\varepsilon_{0}R_{0}^{2}}{c_{0}}>{R_{0}(1+\varepsilon_{0})}\sin\theta_{0}.

Setting y=c0R0y=\frac{c_{0}}{R_{0}}, we may rewrite (3.3) as y2βˆ’(1+Ξ΅0)sinΞΈ0yβˆ’Ξ΅0>0.y^{2}-(1+\varepsilon_{0})\sin\theta_{0}\,y-\varepsilon_{0}>0. The positive root of the corresponding quadratic polynomial is

(1+Ξ΅0)sinΞΈ0+(1+Ξ΅0)2​sin2⁑θ0+4​Ρ02.\frac{(1+\varepsilon_{0})\sin\theta_{0}+\sqrt{(1+\varepsilon_{0})^{2}\sin^{2}\theta_{0}+4\varepsilon_{0}}}{2}.

Therefore (3.3) follows from the assumed lower bound on c0c_{0}. We have proved that

(3.4) ⟨ν(z),en+1⟩>0onΒ M0∩{xn+1β‰₯c1}.\langle\nu(z),e_{n+1}\rangle>0\qquad\text{on }\qquad M_{0}\cap\{x_{n+1}\geq c_{1}\}.

Now we claim that (3.4) implies that M0∩{xn+1β‰₯c1}M_{0}\cap\{x_{n+1}\geq c_{1}\} is a graph over the horizontal hyperplane. Indeed, the condition ⟨ν,en+1⟩>0\langle\nu,e_{n+1}\rangle>0 shows first that the vertical projection is a local diffeomorphism. To prove global injectivity, let Ξ©0\Omega_{0} be the bounded domain enclosed by M0M_{0} and suppose that a vertical line

LzΒ―={(zΒ―,s):sβˆˆβ„}L_{\bar{z}}=\{(\bar{z},s):s\in\mathbb{R}\}

meets M0∩{xn+1β‰₯c1}M_{0}\cap\{x_{n+1}\geq c_{1}\} in two distinct points

zβˆ’=(zΒ―,sβˆ’),z+=(zΒ―,s+),c1≀sβˆ’<s+.z^{-}=(\bar{z},s_{-}),\qquad z^{+}=(\bar{z},s_{+}),\qquad c_{1}\leq s_{-}<s_{+}.

Both intersections are transverse. Moreover, ⟨ν,en+1⟩>0\langle\nu,e_{n+1}\rangle>0 means that, as the line is crossed in the direction of increasing ss, both intersections are exit points from Ω0\Omega_{0}. This is impossible, since the transverse intersections of the boundary of a bounded domain with an oriented line alternate between entry points, where ⟨ν,en+1⟩<0\langle\nu,e_{n+1}\rangle<0, and exit points, where ⟨ν,en+1⟩>0\langle\nu,e_{n+1}\rangle>0. Any intermediate entry point would also have height at least c1c_{1}, contradicting the positivity of ⟨ν,en+1⟩\langle\nu,e_{n+1}\rangle on the whole portion. Thus every vertical line meets this portion at most once, and the portion is a graph.

Since the vertical segment joining xx to x~\tilde{x} is contained in {xn+1β‰₯c1}\{x_{n+1}\geq c_{1}\}, the graph property implies that its interior does not meet M0M_{0}. Moreover, ⟨ν⁑(x),en+1⟩>0\langle\nu(x),e_{n+1}\rangle>0 shows that the segment enters Ξ©0\Omega_{0} immediately below xx. Hence its interior lies in Ξ©0\Omega_{0}, and, as x~βˆ‰M0\tilde{x}\notin M_{0}, also x~∈Ω0\tilde{x}\in\Omega_{0}. Thus

ℛΠ​(M0∩Π+)βŠ‚Ξ©0βˆ©Ξ βˆ’.\mathcal{R}_{\Pi}\bigl(M_{0}\cap\Pi^{+}\bigr)\subset\Omega_{0}\cap\Pi^{-}.

Finally, we observe that property (3.4) implies that the normal direction to Π\Pi is not tangent to M0M_{0} at the points of M0∩ΠM_{0}\cap\Pi. We conclude that M0M_{0} reflects strictly across Πc0,e\Pi_{c_{0},e}. Since the inequality required on c0c_{0} is also satisfied by the values greater than c0c_{0}, the property holds for these values too, and we have the strict reflection of M0M_{0} up to Πc0,e\Pi_{c_{0},e} as in Definition 2.2 (d). ∎

Remark 3.2.

We observe that Φ⁑(Ξ΅0,ΞΈ0)β†’0\Phi(\varepsilon_{0},\theta_{0})\to 0 as Ξ΅0+ΞΈ0β†’0\varepsilon_{0}+\theta_{0}\to 0. Therefore we can make the reflection threshold c0c_{0} as small as we wish compared to R0R_{0} by imposing that Ξ΅0+ΞΈ0\varepsilon_{0}+\theta_{0} are sufficiently small.

3.2. Reflection and first-order closeness to spheres

Before considering the evolution, we isolate the flow-independent geometric consequences of strong Alexandrov reflection. In the previous subsection, we have shown that geometric C1C^{1}-closeness to a sphere yields the reflection property across hyperplanes with distance from the origin greater than a small threshold c0c_{0}. By adapting ideas from [13], we now show that the converse is also true, and that the reflection up to a sufficiently small c0c_{0} gives a control both on the radial oscillation and on the tilt of the hypersurface. The reflection threshold c0c_{0} may therefore be regarded as a geometric measure of first-order deviation from a sphere.

Proposition 3.3 (Radial control from reflection).

Let M=βˆ‚Ξ©βŠ‚β„n+1M=\partial\Omega\subset\mathbb{R}^{n+1} be a smooth, closed, connected, embedded hypersurface, with 0∈Ω0\in\Omega, and let R0>0R_{0}>0 be such that Ξ©\Omega has the same volume as BR0​(0)B_{R_{0}}(0). Suppose that there exists c0∈(0,R0/2)c_{0}\in(0,R_{0}/2) such that MM reflects across Ξ c0,e\Pi_{c_{0},e} for every eβˆˆπ•Šne\in\mathbb{S}^{n}. Then

(3.5) R0βˆ’2​c0≀|x|≀R0+2​c0on ​M.R_{0}-2c_{0}\leq|x|\leq R_{0}+2c_{0}\qquad\text{on }M.
Proof.

Set

rβˆ’=minx∈M⁑|x|andr+=maxx∈M⁑|x|,r_{-}=\min_{x\in M}|x|\qquad\text{and}\qquad r_{+}=\max_{x\in M}|x|,

and choose xβˆ’,x+∈Mx_{-},x_{+}\in M so that |xβˆ’|=rβˆ’|x_{-}|=r_{-}, |x+|=r+|x_{+}|=r_{+}. Then the reflection property of MM across Ξ c0,e\Pi_{c_{0},e}, with ee parallel to x+βˆ’xβˆ’x_{+}-x_{-} (see the proof of [13, Corollary 2.9]) yields the inequality

(3.6) r+2βˆ’rβˆ’2≀2​c0​|x+βˆ’xβˆ’|.r_{+}^{2}-r_{-}^{2}\leq 2c_{0}\,|x_{+}-x_{-}|.

The triangle inequality gives

|x+βˆ’xβˆ’|\displaystyle|x_{+}-x_{-}| ≀|x+|+|xβˆ’|=r++rβˆ’.\displaystyle\leq|x_{+}|+|x_{-}|=r_{+}+r_{-}.

Therefore, (3.6) implies

(r+βˆ’rβˆ’)​(r++rβˆ’)≀2​c0​(r++rβˆ’).\displaystyle\bigl(r_{+}-r_{-}\bigr)\bigl(r_{+}+r_{-}\bigr)\leq 2c_{0}\bigl(r_{+}+r_{-}\bigr).

Since MM is nonempty, r+>0r_{+}>0, and hence r++rβˆ’>0.r_{+}+r_{-}>0. We may therefore divide by the latter and conclude that

(3.7) r+βˆ’rβˆ’β‰€2​c0.r_{+}-r_{-}\leq 2c_{0}.

It remains to locate this annulus relative to R0R_{0}. Notice that 0∈Ω0\in\Omega gives

Brβˆ’β€‹(0)βŠ‚Ξ©βŠ‚Br+​(0).B_{r_{-}}(0)\subset\Omega\subset B_{r_{+}}(0).

The volume normalization therefore implies rβˆ’β‰€R0≀r+.r_{-}\leq R_{0}\leq r_{+}. Combining this and (3.7), we find

(3.8) R0βˆ’2​c0≀r+βˆ’2​c0≀rβˆ’β‰€R0≀r+≀rβˆ’+2​c0≀R0+2​c0.R_{0}-2c_{0}\leq r_{+}-2c_{0}\leq r_{-}\leq R_{0}\leq r_{+}\leq r_{-}+2c_{0}\leq R_{0}+2c_{0}.

Since R0>2​c0R_{0}>2c_{0} by assumption, the lower bound above is strictly positive. Therefore MM cannot pass through the origin. Thus, for every x∈Mx\in M, rβˆ’β‰€|x|≀r+,r_{-}\leq|x|\leq r_{+}, and hence

R0βˆ’2​c0≀|x|≀R0+2​c0,R_{0}-2c_{0}\leq|x|\leq R_{0}+2c_{0},

which finishes the proof. ∎

Proposition 3.4 (Normal control from reflection).

Let MM and R0R_{0} be as in Proposition 3.3. Suppose that c0∈(0,R0/3)c_{0}\in(0,R_{0}/3) is such that MM reflects strictly up to Ξ c0,e\Pi_{c_{0},e} for every eβˆˆπ•Šne\in\mathbb{S}^{n}. Then

(3.9) ⟨ν,x|x|⟩2β‰₯1βˆ’(c0R0βˆ’2​c0)2on ​M.\left\langle\nu,\frac{x}{|x|}\right\rangle^{2}\geq 1-\left(\frac{c_{0}}{R_{0}-2c_{0}}\right)^{2}\qquad\text{on }M.

In particular, MM is star-shaped with respect to the origin.

Proof.

By definition of strict reflection, for any x∈Mx\in M and eβˆˆπ•Šne\in\mathbb{S}^{n} we have

(3.10) eβˆ‰Tx​Mwhenever⟨x,e⟩>c0.e\notin T_{x}M\qquad\text{whenever}\qquad\langle x,e\rangle>c_{0}.

For any x∈Mx\in M, we decompose the position vector into its normal and tangential components:

x=⟨x,Ξ½βŸ©β€‹Ξ½+x⊀,withx⊀=xβˆ’βŸ¨x,Ξ½βŸ©β€‹Ξ½.x=\langle x,\nu\rangle\nu+x^{\top},\qquad\text{with}\quad x^{\top}=x-\langle x,\nu\rangle\nu.

We claim that

(3.11) |x⊀|≀c0.|x^{\top}|\leq c_{0}.

If x⊀=0x^{\top}=0, there is nothing to prove. Otherwise, set e=x⊀/|x⊀|.e=x^{\top}/|x^{\top}|. Then e∈Tx​Me\in T_{x}M and ⟨x,e⟩=|x⊀|\langle x,e\rangle=|x^{\top}|. If |xT|>c0|x^{T}|>c_{0}, we would have

⟨x,e⟩>c0ande∈Tx​M,\langle x,e\rangle>c_{0}\qquad\text{and}\qquad e\in T_{x}M,

contradicting (3.10). Therefore (3.11) holds. This is also the tangential-position estimate obtained from Alexandrov reflection in [13, Corollary 2.4] and [12, Corollary 19(1)].

We now use the orthogonal decomposition of xx. Since |x|2=⟨x,ν⟩2+|x⊀|2|x|^{2}=\langle x,\nu\rangle^{2}+|x^{\top}|^{2}, we have

1βˆ’βŸ¨Ξ½,x|x|⟩2=|x|2βˆ’βŸ¨x,ν⟩2|x|2=|x⊀|2|x|2≀(c0R0βˆ’2​c0)2,\displaystyle 1-\left\langle\nu,\frac{x}{|x|}\right\rangle^{2}=\frac{|x|^{2}-\langle x,\nu\rangle^{2}}{|x|^{2}}=\frac{|x^{\top}|^{2}}{|x|^{2}}\leq\left(\frac{c_{0}}{R_{0}-2c_{0}}\right)^{2},

where we have applied (3.11) and Proposition 3.3 for the last inequality.

Notice that, since 3​c0<R03c_{0}<R_{0}, then c0R0βˆ’2​c0<1,\frac{c_{0}}{R_{0}-2c_{0}}<1, hence the right-hand side of (3.9) is strictly positive. Thus ⟨ν,x|x|⟩\left\langle\nu,\frac{x}{|x|}\right\rangle does not vanish on MM. Since MM is connected, this quantity has a constant sign. At a point where |x||x| attains its minimum, the outward unit normal points away from the origin, because 0∈Ω0\in\Omega. Therefore the sign is positive, and MM is star-shaped. ∎

Within the class of smooth, closed, connected, embedded hypersurfaces enclosing the same volume as BR0​(0)B_{R_{0}}(0) and containing the origin in the enclosed region, strong Alexandrov reflection in every direction and geometric C1C^{1}-closeness to βˆ‚BR0​(0)\partial B_{R_{0}}(0) determine each other quantitatively, up to a change of parameters. More precisely,

Corollary 3.5 (Reflection and geometric C1C^{1}-closeness).

If MM satisfies (1.1) and (1.2), then every c0>0c_{0}>0 satisfying (3.1) is a reflection threshold for MM. Conversely, a common reflection threshold c0c_{0}, with 3​c0<R03c_{0}<R_{0}, implies the radial and normal estimates of Propositions 3.3 and 3.4. In particular, both the relative annular width and the maximal angle between the normal and the radial direction tend to zero as c0/R0β†’0c_{0}/R_{0}\to 0.

Proof.

The first implication is Proposition 3.1. The converse follows from Propositions 3.3 and 3.4. ∎

The importance of the reflection formulation is that it is preserved by the evolution, by Theorem 2.3. Starting from the initial geometric assumptions, we obtain a strong reflection property, propagate it with the same threshold c0c_{0}, and then apply the converse implication of Corollary 3.5 to each time slice.

3.3. Preservation of the starting conditions under the flow

Proposition 3.6 (Annular closeness and normal oscillation for later times).

Let M0βŠ‚β„n+1M_{0}\subset\mathbb{R}^{n+1} satisfy (1.1) and (1.2) and let MtM_{t} be the solution of the flow (1.3). Let c0c_{0} be chosen as in Proposition 3.1, and assume that Ξ΅0,ΞΈ0\varepsilon_{0},\theta_{0} are sufficiently small so that R0>3​c0R_{0}>3c_{0}.

Then, for every time for which the solution is defined, we have

(3.12) R0βˆ’2​c0≀|x|≀R0+2​c0on ​MtR_{0}-2c_{0}\leq|x|\leq R_{0}+2c_{0}\qquad\text{on }M_{t}\vskip 6.0pt plus 2.0pt minus 2.0pt
(3.13) ⟨ν,x|x|⟩2β‰₯1βˆ’(c0R0βˆ’2​c0)2on ​Mt.\left\langle\nu,\frac{x}{|x|}\right\rangle^{2}\geq 1-\left(\frac{c_{0}}{R_{0}-2c_{0}}\right)^{2}\qquad\text{on }M_{t}.
Proof.

By Proposition 3.1, M0M_{0} reflects strictly up to Ξ c0,e\Pi_{c_{0},e} for every eβˆˆπ•Šne\in\mathbb{S}^{n}. Then Theorem 2.3 implies that the same threshold c0c_{0} is preserved throughout the existence interval.

We now wish to apply the static consequences of reflection from the previous subsection. Let us check that the property 0∈Ωt0\in\Omega_{t} holds throughout the flow. Since 0∈Ω00\in\Omega_{0}, let

I={tβ‰₯0:0∈Ωs​ for every ​0≀s≀t}I=\left\{t\geq 0:0\in\Omega_{s}\text{ for every }0\leq s\leq t\right\}

within the maximal existence interval. This set contains a nontrivial interval starting at t=0t=0. For every t∈It\in I, the hypersurface MtM_{t} has the same enclosed volume as M0M_{0}, namely

|Ξ©t|=|Ξ©0|=Ο‰n+1​R0n+1,|\Omega_{t}|=|\Omega_{0}|=\omega_{n+1}R_{0}^{n+1},

and reflects strictly up to Ξ c0,e\Pi_{c_{0},e} for every direction ee. Proposition 3.3 applies to MtM_{t} with the same constants R0R_{0} and c0c_{0}. In particular, the lower radial bound

|x|β‰₯R0βˆ’2​c0>0|x|\geq R_{0}-2c_{0}>0

also shows that MtM_{t} cannot pass through the origin. Since 0∈Ω00\in\Omega_{0}, the origin cannot leave the enclosed region without first belonging to its boundary. Therefore 0∈Ωt0\in\Omega_{t} for every time in the maximal existence interval. It follows that II is the entire existence interval, and the above estimates hold throughout it.

This shows that we can apply Propositions 3.3 and 3.4 for all tt for which the flow exists, for the fixed reference radius R0R_{0} and the single reflection threshold c0c_{0}. The conclusion follows. ∎

Corollary 3.7 (Control of the support function).

Under the assumptions of the previous proposition, the support function u=⟨x,ν⟩u=\langle x,\nu\rangle satisfies

(3.14) R0βˆ’3​c0≀u≀R0+2​c0R_{0}-3c_{0}\leq u\leq R_{0}+2c_{0}

throughout the existence interval. In particular, setting Ξ·0:=3​c0,\eta_{0}:=3c_{0}, we have

(3.15) |uβˆ’R0|≀η0|u-R_{0}|\leq\eta_{0}

with Ξ·0=Ξ·0​(Ξ΅0,ΞΈ0)β†’0\eta_{0}=\eta_{0}(\varepsilon_{0},\theta_{0})\to 0 as Ξ΅0+ΞΈ0β†’0\varepsilon_{0}+\theta_{0}\to 0.

Proof.

First, notice that the tangential estimate (3.11), applied to x∈Mtx\in M_{t}, gives |x⊀|≀c0.|x^{\top}|\leq c_{0}. Since x=x⊀+u​ν,x=x^{\top}+u\nu, we have u2=|x|2βˆ’|x⊀|2.u^{2}=|x|^{2}-|x^{\top}|^{2}. Estimate (3.13) gives u>0u>0, while (3.12) yields

uβ‰₯(R0βˆ’2​c0)2βˆ’c02β‰₯R0βˆ’3​c0,u\geq\sqrt{(R_{0}-2c_{0})^{2}-c_{0}^{2}}\geq R_{0}-3c_{0},

where the latter follows from 3​c0<R03c_{0}<R_{0}. Finally, the upper bound holds because u≀|x|≀R0+2​c0.u\leq|x|\leq R_{0}+2c_{0}. ∎

Remark 3.8.

From now on, we assume that the initial geometric parameters Ξ΅0,ΞΈ0\varepsilon_{0},\theta_{0} are chosen sufficiently small in order that the corresponding reflection threshold satisfies 3​c0<R0,3c_{0}<R_{0}, as required in Proposition 3.6. This is certainly possible, in view of Remark 3.2.

4. Curvature control under the flow

In this section we use the C1C^{1} control from the previous section to obtain a uniform bound of the curvature.

4.1. Control of the mean curvature and the global term

Let us first estimate the global term in the flow equation (1.3).

Lemma 4.1 (Estimate for the nonlocal term).

Let Ξ·0=3​c0\eta_{0}=3c_{0} be as in Corollary 3.7. If the initial parameters are sufficiently small that Ξ·0<R02,\eta_{0}<\frac{R_{0}}{2}, then the averaged mean curvature defined in (1.4) satisfies

|h⁑(t)βˆ’nR0|≀η0R0​maxMt​|H|,\bigg|h(t)-\frac{n}{R_{0}}\bigg|\leq\frac{\eta_{0}}{R_{0}}\max_{M_{t}}|H|,

throughout the existence interval.

Proof.

We recall that the support function uu satisfies the Minkowski identity

∫MH​u​𝑑μ=n​|M|.\int_{M}Hu\,d\mu=n|M|.

Using this and the inequality |uβˆ’R0|≀η0|u-R_{0}|\leq\eta_{0} from Corollary 3.7, we conclude

|h⁑(t)βˆ’nR0|=|1|Mt|​R0β€‹βˆ«MH⁑(R0βˆ’u)​d​μt|≀η0R0​maxMt​|H|.\bigg|h(t)-\frac{n}{R_{0}}\bigg|=\left|\frac{1}{|M_{t}|R_{0}}\int_{M}H(R_{0}-u)\,d\mu_{t}\right|\leq\frac{\eta_{0}}{R_{0}}\max_{M_{t}}|H|.

∎

Remark 4.2 (The sign of the nonlocal term).

The assumptions of the theorem do not determine the sign of either HH or hh. Indeed, for a radial graph the second-order part of the mean curvature can be written in divergence form, but its contribution to the total mean curvature does not vanish: the area element introduces a nonconstant weight, and integration by parts leaves a Hessian term with no definite sign. Since our hypotheses control only the radial position and the first derivatives of the graph, this term cannot be estimated from the initial geometric bounds. The Tso-type argument below must therefore treat the different sign configurations of HH and hh separately, making it more involved than in the usual sign-definite setting.

In the following, when considering some scalar function ff defined on MtM_{t}, we use the notation fmin:=minMt⁑ff_{\min}:=\min_{M_{t}}f and fmax:=maxMt⁑ff_{\max}:=\max_{M_{t}}f. Differential inequalities for these quantities are understood in terms of upper and lower Dini derivatives. We shall use the standard scalar maximum principle without further comment.

Proposition 4.3 (Mean curvature is bounded along the flow).

If Ξ΅0,ΞΈ0\varepsilon_{0},\theta_{0} are small enough, then we can find a positive constant C=C⁑(n,R0,Ξ΅0,ΞΈ0,β€–H⁑(β‹…,0)β€–Lβˆžβ€‹(M0))C=C\bigl(n,R_{0},\varepsilon_{0},\theta_{0},\|H(\cdot,0)\|_{L^{\infty}(M_{0})}\bigr) satisfying

(4.1) |H|≀ConMt.|H|\leq C\qquad\text{on}\quad M_{t}.
Proof.

Recall that, by Corollary 3.7, after choosing Ξ΅0,ΞΈ0\varepsilon_{0},\theta_{0} sufficiently small, the support function satisfies |uβˆ’R0|≀η0|u-R_{0}|\leq\eta_{0}, where Ξ·0=Ξ·0​(Ξ΅0,ΞΈ0)\eta_{0}=\eta_{0}(\varepsilon_{0},\theta_{0}) can be made arbitrarily small.

Setting Ξ±=R0βˆ’2​η0\alpha=R_{0}-2\eta_{0}, it holds

(4.2) Ξ·0≀uβˆ’Ξ±β‰€3​η0.\eta_{0}\leq u-\alpha\leq 3\eta_{0}.

Next we work with a Tso-type function (cf. [33]), that is, we consider

Z=Huβˆ’Ξ±.Z=\frac{H}{u-\alpha}.

We now compute the evolution of ZZ. The equations from Lemma 2.1 give by direct computation

(4.3) (βˆ‚tβˆ’Ξ”)Z=βˆ’Ξ±β€‹Z+huβˆ’Ξ±|A|2βˆ’huβˆ’Ξ±Z+2Z2+2uβˆ’Ξ±βŸ¨βˆ‡u,βˆ‡Z⟩.\displaystyle(\partial_{t}-\Delta)Z=-\frac{\alpha\,Z+h}{u-\alpha}|A|^{2}-\frac{h}{u-\alpha}Z+2Z^{2}+\frac{2}{u-\alpha}\langle\nabla u,\nabla Z\rangle.

We observe that ZmaxZ_{\max} is always positive, while ZminZ_{\min} can have any sign in general. We want to derive a two-sided bound on ZZ using the maximum principle. The role of the terms which occur in the equation for ZZ is different depending on the sign both of ZZ and of h⁑(t)h(t), therefore we need to treat different cases separately.

Let us first consider a time tt at which h⁑(t)β‰₯0h(t)\geq 0. At a point where the maximum of ZZ is attained we can write

dd​t​Zmax≀2​Zmax2βˆ’Ξ±β€‹Zmaxuβˆ’Ξ±β€‹|A|2≀2​Zmax2βˆ’Ξ±n​Zmax3​(uβˆ’Ξ±)≀Zmax2​(2βˆ’Ξ±β€‹Ξ·0n​Zmax).\frac{d}{dt}Z_{\max}\leq 2Z_{\max}^{2}-\frac{\alpha\,Z_{\max}}{u-\alpha}|A|^{2}\leq 2Z_{\max}^{2}-\frac{\alpha}{n}Z_{\max}^{3}(u-\alpha)\leq Z_{\max}^{2}\Big(2-\frac{\alpha\,\eta_{0}}{n}Z_{\max}\Big).

We deduce

(4.4) dd​t​Zmax≀0Β ifΒ h⁑(t)β‰₯0Β and ​Zmax​(t)β‰₯2​nα​η0.\frac{d}{dt}Z_{\max}\leq 0\quad\mbox{ if $h(t)\geq 0$ \quad and }Z_{\max}(t)\geq\frac{2n}{\alpha\eta_{0}}.

We now estimate the derivative of ZminZ_{\min} at a time with h⁑(t)β‰₯0h(t)\geq 0. Since we want a bound from below, we can suppose that Zmin<0Z_{\min}<0. Using (4.2), we have

(4.5) |H|max≀3​η0​|Z|max<3​η0​(Zmaxβˆ’Zmin),|H|_{\max}\leq 3\,\eta_{0}\,|Z|_{\max}<3\,\eta_{0}\,(Z_{\max}-Z_{\min}),

which by Lemma 4.1 yields

h≀1R0​(n+3​η02​(Zmaxβˆ’Zmin)).h\leq\frac{1}{R_{0}}\Big(n+3\,\eta_{0}^{2}(Z_{\max}-Z_{\min})\Big).

At a point where Z=ZminZ=Z_{\min}, we deduce from (4.3)

dd​t​Zminβ‰₯|A|2uβˆ’Ξ±β€‹(βˆ’nR0βˆ’3​η02R0​(Zmaxβˆ’Zmin)βˆ’Ξ±β€‹Zmin).\frac{d}{dt}Z_{\min}\geq\frac{|A|^{2}}{u-\alpha}\Big(-\frac{n}{R_{0}}-\frac{3\,\eta_{0}^{2}}{R_{0}}(Z_{\max}-Z_{\min})-\alpha Z_{\min}\Big).

If we choose Ξ·0\eta_{0} sufficiently small so that α​R0βˆ’3​η02>α​R02\alpha R_{0}-3\eta_{0}^{2}>\frac{\alpha R_{0}}{2}, we obtain

dd​t​Zminβ‰₯|A|2(uβˆ’Ξ±)​R0​(βˆ’nβˆ’3​η02​Zmax+α​R02​(βˆ’Zmin)).\frac{d}{dt}Z_{\min}\geq\frac{|A|^{2}}{(u-\alpha)R_{0}}\Big(-n-3\,\eta_{0}^{2}Z_{\max}+\frac{\alpha R_{0}}{2}(-Z_{\min})\Big).

Then if βˆ’Zmin>2α​R0​(n+3​η02​Zmax​(t))-Z_{\min}>\frac{2}{\alpha R_{0}}(n+3\eta_{0}^{2}Z_{\max}(t)) the right hand side above becomes positive. We conclude that

(4.6) dd​t​Zminβ‰₯0Β ifΒ h⁑(t)β‰₯0Β and ​Zmin​(t)β‰€βˆ’2α​R0​(n+3​η02​Zmax​(t)).\frac{d}{dt}Z_{\min}\geq 0\quad\mbox{ if $h(t)\geq 0$ \quad and }Z_{\min}(t)\leq-\frac{2}{\alpha R_{0}}\Big(n+3\eta_{0}^{2}Z_{\max}(t)\Big).

Next, consider a time tt at which h⁑(t)≀0h(t)\leq 0. We remark that at such a time we have Hmin​(t)<0H_{\min}(t)<0 and Zmin​(t)<0Z_{\min}(t)<0. We first estimate the derivative of ZminZ_{\min}. At a point where Z=Zmin<0Z=Z_{\min}<0, we can discard the positive terms with βˆ’Ξ±β€‹Z​|A|2-\alpha Z|A|^{2} and Z2Z^{2} in the evolution equation (4.3) and obtain

dd​t​Zminβ‰₯βˆ’huβˆ’Ξ±β€‹(|A|2+Zmin)β‰₯βˆ’huβˆ’Ξ±β€‹(H2n+Zmin)β‰₯βˆ’h​Zminuβˆ’Ξ±β€‹(Ξ·02​Zminn+1).\frac{d}{dt}Z_{\min}\geq-\frac{h}{u-\alpha}\big(|A|^{2}+Z_{\min}\big)\geq-\frac{h}{u-\alpha}\bigg(\frac{H^{2}}{n}+Z_{\min}\bigg)\geq-\frac{hZ_{\min}}{u-\alpha}\bigg(\frac{\eta_{0}^{2}Z_{\min}}{n}+1\bigg).

We deduce

(4.7) dd​t​Zminβ‰₯0Β ifΒ h⁑(t)≀0Β and ​Zmin​(t)β‰€βˆ’nΞ·02.\frac{d}{dt}Z_{\min}\geq 0\quad\mbox{ if $h(t)\leq 0$ \quad and }Z_{\min}(t)\leq-\frac{n}{\eta_{0}^{2}}.

We now consider the derivative of ZmaxZ_{\max} under the same hypothesis that h⁑(t)≀0h(t)\leq 0. Suppose further that Zmax​(t)β‰₯nΞ·02>0Z_{\max}(t)\geq\frac{n}{\eta_{0}^{2}}>0. Then, at a point where Z=ZmaxZ=Z_{\max}, we have

H=(uβˆ’Ξ±)​Zmaxβ‰₯Ξ·0​Zmaxβ‰₯nΞ·0,H=(u-\alpha)Z_{\max}\geq\eta_{0}Z_{\max}\geq\frac{n}{\eta_{0}},

as well as

|A|2β‰₯1n​H2β‰₯uβˆ’Ξ±Ξ·0​Zmaxβ‰₯Zmax.|A|^{2}\geq\frac{1}{n}H^{2}\geq\frac{u-\alpha}{\eta_{0}}Z_{\max}\geq Z_{\max}.

Accordingly, we can write

dd​t​Zmax\displaystyle\frac{d}{dt}Z_{\max} ≀|A|2uβˆ’Ξ±β€‹(βˆ’Ξ±β€‹Zmaxβˆ’h)βˆ’huβˆ’Ξ±β€‹Zmax+2​Zmax2\displaystyle\leq\frac{|A|^{2}}{u-\alpha}(-\alpha Z_{\max}-h)-\frac{h}{u-\alpha}Z_{\max}+2Z_{\max}^{2}
≀|A|2uβˆ’Ξ±β€‹(βˆ’Ξ±β€‹Zmaxβˆ’h)βˆ’huβˆ’Ξ±β€‹|A|2+2​n​|A|2(uβˆ’Ξ±)2\displaystyle\leq\frac{|A|^{2}}{u-\alpha}(-\alpha Z_{\max}-h)-\frac{h}{u-\alpha}|A|^{2}+2n\frac{|A|^{2}}{(u-\alpha)^{2}}
≀|A|2uβˆ’Ξ±β€‹(2​nΞ·0βˆ’2​hβˆ’Ξ±β€‹Zmax).\displaystyle\leq\frac{|A|^{2}}{u-\alpha}\bigg(\frac{2n}{\eta_{0}}-2h-\alpha Z_{\max}\bigg).

By substitution of (4.5) into Lemma 4.1, we obtain

βˆ’2​hβ‰€βˆ’2​nR0+6​η02R0​(Zmaxβˆ’Zmin).-2h\leq-\frac{2n}{R_{0}}+\frac{6\eta_{0}^{2}}{R_{0}}\left(Z_{\max}-Z_{\min}\right).

If we choose Ξ·0\eta_{0} sufficiently small so that α​R0βˆ’6​η02>α​R02\alpha R_{0}-6\eta_{0}^{2}>\frac{\alpha R_{0}}{2}, we obtain

dd​t​Zmax\displaystyle\frac{d}{dt}Z_{\max} ≀|A|2uβˆ’Ξ±β€‹(2​nΞ·0βˆ’2​nR0βˆ’Ξ±2​Zmaxβˆ’6​η02R0​Zmin).\displaystyle\leq\frac{|A|^{2}}{u-\alpha}\bigg(\frac{2n}{\eta_{0}}-\frac{2n}{R_{0}}-\frac{\alpha}{2}Z_{\max}-\frac{6\eta_{0}^{2}}{R_{0}}Z_{\min}\bigg).

After discarding the negative term βˆ’2n/R0-2n/R_{0} in order to simplify the constants, we get

(4.8) dd​t​Zmax≀0Β ifΒ h⁑(t)≀0Β and ​Zmax​(t)β‰₯max⁑{nΞ·02,2α​(2​nΞ·0βˆ’6​η02R0​Zmin​(t))}.\frac{d}{dt}Z_{\max}\leq 0\quad\mbox{ if $h(t)\leq 0$ \quad and }Z_{\max}(t)\geq\max\left\{\frac{n}{\eta_{0}^{2}},\frac{2}{\alpha}\left(\frac{2n}{\eta_{0}}-\frac{6\eta_{0}^{2}}{R_{0}}Z_{\min}(t)\right)\right\}.

Let us now define

Ξ³1=max⁑{2​nα​η0,nΞ·02,4​nα​η0},Ξ΄1=12​η02α​R0.\gamma_{1}=\max\bigg\{\frac{2n}{\alpha\eta_{0}},\frac{n}{\eta_{0}^{2}},\frac{4n}{\alpha\eta_{0}}\bigg\},\qquad\delta_{1}=\frac{12\eta_{0}^{2}}{\alpha R_{0}}.
Ξ³2=max⁑{2​nα​R0,nΞ·02},Ξ΄2=6​η02α​R0.\gamma_{2}=\max\bigg\{\frac{2n}{\alpha R_{0}},\frac{n}{\eta_{0}^{2}}\bigg\},\qquad\qquad\delta_{2}=\frac{6\eta_{0}^{2}}{\alpha R_{0}}.

From (4.1), (4.6), (4.7) and (4.8) we see that, regardless of the sign of h⁑(t)h(t), we have

(4.9) dd​t​Zmax≀0Β if ​Zmaxβ‰₯Ξ³1βˆ’Ξ΄1​[Zmin​(t)]βˆ’\frac{d}{dt}Z_{\max}\leq 0\quad\mbox{ if }Z_{\max}\geq\gamma_{1}-\delta_{1}[Z_{\min}(t)]_{-}
(4.10) dd​t​Zminβ‰₯0Β if ​Zminβ‰€βˆ’Ξ³2βˆ’Ξ΄2​Zmax​(t),\frac{d}{dt}Z_{\min}\geq 0\quad\mbox{ if }Z_{\min}\leq-\gamma_{2}-\delta_{2}Z_{\max}(t),

where [Zmin​(t)]βˆ’=min⁑{Zmin​(t),0}[Z_{\min}(t)]_{-}=\min\{Z_{\min}(t),0\}.

Since Ξ·0\eta_{0} can be made arbitrarily small by an appropriate choice of the initial parameters Ξ΅0,ΞΈ0\varepsilon_{0},\theta_{0}, we assume that it is chosen in such a way that Ξ΄1<1,Ξ΄2<1\delta_{1}<1,\delta_{2}<1. This allows us to take a constant Ξ›>0\Lambda>0 such that

βˆ’Ξ›<Zmin​(0)≀Zmax​(0)<Ξ›,-\Lambda<Z_{\min}(0)\leq Z_{\max}(0)<\Lambda,
Ξ›>Ξ³1+Ξ΄1​Λ,βˆ’Ξ›<βˆ’Ξ³2βˆ’Ξ΄2​Λ.\Lambda>\gamma_{1}+\delta_{1}\Lambda,\qquad-\Lambda<-\gamma_{2}-\delta_{2}\Lambda.

With this choice, we obtain

βˆ’Ξ›<Zmin​(t)≀Zmax​(t)<Ξ›-\Lambda<Z_{\min}(t)\leq Z_{\max}(t)<\Lambda

for every time for which the solution is defined. In fact, at a first time where either Zmin​(t)=βˆ’Ξ›Z_{\min}(t)=-\Lambda, or Zmax​(t)=Ξ›Z_{\max}(t)=\Lambda, a standard maximum principle argument yields a contradiction with (4.9) or (4.10).

Finally, from (4.2) we reach

|H|=|(uβˆ’Ξ±)​Z|≀3​η0​Λ,|H|=|(u-\alpha)Z|\leq 3\eta_{0}\Lambda,

which proves the uniform bound for the mean curvature. Therefore there exists a constant

C=C⁑(n,R0,Ξ΅0,ΞΈ0,β€–H⁑(β‹…,0)β€–Lβˆžβ€‹(M0))C=C\bigl(n,R_{0},\varepsilon_{0},\theta_{0},\|H(\cdot,0)\|_{L^{\infty}(M_{0})}\bigr)

such that |H|≀C|H|\leq C on MtM_{t}. ∎

Notice that by the lack of convexity assumptions, we cannot conclude that |A|2|A|^{2} is bounded from the above uniform control of the mean curvature. We need a separate extra argument inspired by [17] to reach the conclusion.

Proposition 4.4 (Shape operator is bounded along the flow).

Under the same choice of parameters as in Proposition 4.3, there exists a uniform constant bounding |A|2|A|^{2} for all times such that the solution is defined.

Proof.

For x∈Mtx\in M_{t}, set

r=|x|,Ο‰=x|x|,q=⟨ν,Ο‰βŸ©,v=qβˆ’1.r=|x|,\qquad\omega=\frac{x}{|x|},\qquad q=\langle\nu,\omega\rangle,\qquad v=q^{-1}.

By Proposition 3.6, after choosing Ξ΅0,ΞΈ0\varepsilon_{0},\theta_{0} sufficiently small, there exist constants 0<rβˆ—<rβˆ—<∞0<r_{*}<r^{*}<\infty, Οƒβˆ—>0\sigma_{*}>0, such that along the flow it holds

(4.11) rβˆ—β‰€r≀rβˆ—,q=⟨ν,Ο‰βŸ©β‰₯Οƒβˆ—.Hence1≀v≀vβˆ—:=Οƒβˆ—βˆ’1.r_{*}\leq r\leq r^{*},\qquad q=\langle\nu,\omega\rangle\geq\sigma_{*}.\qquad\text{Hence}\qquad 1\leq v\leq v_{*}:=\sigma_{*}^{-1}.

We first record the evolution of vv. Since u=r​qu=rq, the evolution from Lemma 2.1 (b) and

(βˆ‚tβˆ’Ξ”)r=hqβˆ’nβˆ’1+q2r(\partial_{t}-\Delta)r=hq-\frac{n-1+q^{2}}{r}

give

(βˆ‚tβˆ’Ξ”)q=\displaystyle(\partial_{t}-\Delta)q={} |A|2​q+hr​(1βˆ’q2)βˆ’2​Hr+q⁑(nβˆ’1+q2)r2+2rβ€‹βŸ¨βˆ‡r,βˆ‡q⟩.\displaystyle|A|^{2}q+\frac{h}{r}(1-q^{2})-\frac{2H}{r}+\frac{q(n-1+q^{2})}{r^{2}}+\frac{2}{r}\langle\nabla r,\nabla q\rangle.

Since v=qβˆ’1v=q^{-1}, it follows that

(4.12) (βˆ‚tβˆ’Ξ”)v=βˆ’|A|2vβˆ’2vβˆ’1|βˆ‡v|2+2rβŸ¨βˆ‡r,βˆ‡v⟩+β„œ,(\partial_{t}-\Delta)v=-|A|^{2}v-2v^{-1}|\nabla v|^{2}+\frac{2}{r}\langle\nabla r,\nabla v\rangle+\mathfrak{R},

where

β„œ=2​Hr​v2βˆ’hr​(v2βˆ’1)βˆ’nβˆ’1r2​vβˆ’1r2​v.\mathfrak{R}=\frac{2H}{r}v^{2}-\frac{h}{r}(v^{2}-1)-\frac{n-1}{r^{2}}v-\frac{1}{r^{2}v}.

Notice that the last two terms in the definition of β„œ\mathfrak{R} are nonpositive. By Proposition 4.3, |H|+|h|≀C|H|+|h|\leq C. Together with (4.11), this implies |β„œ|≀C|\mathfrak{R}|\leq C. Hereafter CC is a uniform constant depending on initial values, whose concrete meaning may change from line to line.

Choose k>0k>0 so that k​vβˆ—2<1,kv_{*}^{2}<1, and define

(4.13) β„±=|A|2​φ​(v2),withφ⁑(s)=s1βˆ’k​s.\mathscr{F}=|A|^{2}\varphi(v^{2}),\qquad\text{with}\qquad\varphi(s)=\frac{s}{1-ks}.

By (4.11), there are positive constants cφ,Cφc_{\varphi},C_{\varphi} such that

(4.14) cφ≀φ⁑(v2)≀CΟ†.c_{\varphi}\leq\varphi(v^{2})\leq C_{\varphi}.

Thus a uniform bound for β„±\mathscr{F} is equivalent to a uniform bound for |A|2|A|^{2}. Moreover, φ′​(v2)\varphi^{\prime}(v^{2}) and φ′′​(v2)\varphi^{\prime\prime}(v^{2}) are uniformly bounded.

Combining (4.12) and Lemma 2.1(c), and carrying out a computation similar to [17, Th. 3.1] while retaining the negative gradient term coming from the evolution of |A|2|A|^{2}, we obtain

(βˆ‚tβˆ’Ξ”)ℱ≀\displaystyle(\partial_{t}-\Delta)\mathscr{F}\leq{} βˆ’2​φ​(v2)​|βˆ‡A|2βˆ’2​k​ℱ2βˆ’2​k(1βˆ’k​v2)2​|βˆ‡v|2β€‹β„±βˆ’2​φ′​(v2)φ⁑(v2)β€‹βŸ¨βˆ‡v2,βˆ‡β„±βŸ©\displaystyle-2\varphi(v^{2})|\nabla A|^{2}-2k\mathscr{F}^{2}-\frac{2k}{(1-kv^{2})^{2}}|\nabla v|^{2}\mathscr{F}-\frac{2\varphi^{\prime}(v^{2})}{\varphi(v^{2})}\left\langle\nabla v^{2},\nabla\mathscr{F}\right\rangle
(4.15) +4r​|A|2​v​φ′​(v2)β€‹βŸ¨βˆ‡r,βˆ‡vβŸ©βˆ’2​h​tr⁑(A3)​φ​(v2)+2​|A|2​v​φ′​(v2)β€‹β„œ.\displaystyle+\frac{4}{r}|A|^{2}v\varphi^{\prime}(v^{2})\langle\nabla r,\nabla v\rangle-2h\,\operatorname{tr}(A^{3})\varphi(v^{2})+2|A|^{2}v\varphi^{\prime}(v^{2})\mathfrak{R}.

We first estimate the term containing β„œ\mathfrak{R}. By the uniform boundedness of β„œ\mathfrak{R}, vv, and φ′​(v2)\varphi^{\prime}(v^{2}), and by (4.14), we have

(4.16) 2​|A|2​v​φ′​(v2)β€‹β„œ\displaystyle 2|A|^{2}v\varphi^{\prime}(v^{2})\mathfrak{R} ≀C​|A|2≀C​ℱ.\displaystyle\leq C|A|^{2}\leq C\mathscr{F}.

We next rewrite the radial-gradient term as a drift term for β„±\mathscr{F}. Since

βˆ‡β„±=Ο†(v2)βˆ‡|A|2+2|A|2vΟ†β€²(v2)βˆ‡v,\nabla\mathscr{F}=\varphi(v^{2})\nabla|A|^{2}+2|A|^{2}v\varphi^{\prime}(v^{2})\nabla v,

we have

(4.17) 4r​|A|2​v​φ′​(v2)β€‹βŸ¨βˆ‡r,βˆ‡vβŸ©βˆ’2rβ€‹βŸ¨βˆ‡r,βˆ‡β„±βŸ©=βˆ’2r​φ​(v2)β€‹βŸ¨βˆ‡r,βˆ‡|A|2⟩.\displaystyle\frac{4}{r}|A|^{2}v\varphi^{\prime}(v^{2})\langle\nabla r,\nabla v\rangle-\frac{2}{r}\langle\nabla r,\nabla\mathscr{F}\rangle=-\frac{2}{r}\varphi(v^{2})\langle\nabla r,\nabla|A|^{2}\rangle.

Using |βˆ‡r|≀1|\nabla r|\leq 1, Kato’s inequality |βˆ‡|A|2|≀2​|A|​|βˆ‡A||\nabla|A|^{2}|\leq 2|A||\nabla A| and rβ‰₯rβˆ—>0r\geq r_{*}>0, we obtain, for every Ξ΄>0\delta>0, by Young’s inequality

(4.18) |2r​φ​(v2)β€‹βŸ¨βˆ‡r,βˆ‡|A|2⟩|\displaystyle\left|\frac{2}{r}\varphi(v^{2})\langle\nabla r,\nabla|A|^{2}\rangle\right| ≀C​φ​(v2)​|A|​|βˆ‡A|≀δ​φ​(v2)​|βˆ‡A|2+Cδ​ℱ.\displaystyle\leq C\varphi(v^{2})|A||\nabla A|\leq\delta\varphi(v^{2})|\nabla A|^{2}+C_{\delta}\mathscr{F}.

Choose, for instance, Ξ΄=1\delta=1. Combining (4.17) and (4.18) with the first term in (4.15), we obtain

βˆ’2​φ​(v2)​|βˆ‡A|2+4r​|A|2​v​φ′​(v2)β€‹βŸ¨βˆ‡r,βˆ‡vβŸ©β‰€2rβ€‹βŸ¨βˆ‡r,βˆ‡β„±βŸ©+C​ℱ,\displaystyle-2\varphi(v^{2})|\nabla A|^{2}+\frac{4}{r}|A|^{2}v\varphi^{\prime}(v^{2})\langle\nabla r,\nabla v\rangle\leq\frac{2}{r}\langle\nabla r,\nabla\mathscr{F}\rangle+C\mathscr{F},

after removing the non-positive term βˆ’Ο†β‘(v2)​|βˆ‡A|2-\varphi(v^{2})|\nabla A|^{2}. Hence (4.15) and (4.16) imply

(4.19) (βˆ‚tβˆ’Ξ”)β„±β‰€βˆ’2kβ„±2+Cβ„±βˆ’2​φ′​(v2)φ⁑(v2)βŸ¨βˆ‡v2,βˆ‡β„±βŸ©+2rβŸ¨βˆ‡r,βˆ‡β„±βŸ©βˆ’2htr(A3)Ο†(v2),\displaystyle(\partial_{t}-\Delta)\mathscr{F}\leq-2k\mathscr{F}^{2}+C\mathscr{F}-\frac{2\varphi^{\prime}(v^{2})}{\varphi(v^{2})}\left\langle\nabla v^{2},\nabla\mathscr{F}\right\rangle+\frac{2}{r}\left\langle\nabla r,\nabla\mathscr{F}\right\rangle-2h\operatorname{tr}(A^{3})\varphi(v^{2}),

where we have discarded the term involving |βˆ‡v|2​ℱ|\nabla v|^{2}\mathscr{F} because it is nonpositive. We still need to control the last cubic term. As |tr⁑(A3)|≀|A|3|\operatorname{tr}(A^{3})|\leq|A|^{3} and hh is uniformly bounded, we get

|βˆ’2​h​tr⁑(A3)​φ​(v2)|\displaystyle\left|-2h\,\operatorname{tr}(A^{3})\varphi(v^{2})\right| ≀C|A|3Ο†(v2)=Cβ„±3/2Ο†(v2)βˆ’1/2≀Cβ„±3/2≀Ρℱ2+CΞ΅,\displaystyle\leq C|A|^{3}\varphi(v^{2})=C\mathscr{F}^{3/2}\varphi(v^{2})^{-1/2}\leq C\mathscr{F}^{3/2}\leq\varepsilon\mathscr{F}^{2}+C_{\varepsilon},

which follows by Young’s inequality for every Ξ΅>0\varepsilon>0. Choosing 0<Ξ΅<k0<\varepsilon<k, this contribution is absorbed into the negative term βˆ’2​k​ℱ2-2k\mathscr{F}^{2} and we reach

(4.20) (βˆ‚tβˆ’Ξ”)ℱ≀\displaystyle(\partial_{t}-\Delta)\mathscr{F}\leq{} βˆ’c​ℱ2+C​ℱ+C~βˆ’2​φ′​(v2)φ⁑(v2)β€‹βŸ¨βˆ‡v2,βˆ‡β„±βŸ©+2rβ€‹βŸ¨βˆ‡r,βˆ‡β„±βŸ©,\displaystyle-c\mathscr{F}^{2}+C\mathscr{F}+\widetilde{C}-\frac{2\varphi^{\prime}(v^{2})}{\varphi(v^{2})}\left\langle\nabla v^{2},\nabla\mathscr{F}\right\rangle+\frac{2}{r}\left\langle\nabla r,\nabla\mathscr{F}\right\rangle,

for some uniform constants c>0c>0 and C,C~<∞C,\widetilde{C}<\infty.

At a spatial maximum point of β„±\mathscr{F}, both gradient terms in (4.20) vanish. Therefore,

(4.21) dd​t​ℱmaxβ‰€βˆ’c​ℱmax2+C​ℱmax+C~.\frac{d}{dt}\mathscr{F}_{\max}\leq-c\mathscr{F}_{\max}^{2}+C\mathscr{F}_{\max}+\widetilde{C}.

The right-hand side is negative whenever β„±max\mathscr{F}_{\max} is sufficiently large. The maximum principle therefore gives a uniform bound for β„±\mathscr{F}. Finally, by (4.14), we conclude

|A|2=ℱφ⁑(v2)≀ℱcΟ†.|A|^{2}=\frac{\mathscr{F}}{\varphi(v^{2})}\leq\frac{\mathscr{F}}{c_{\varphi}}.

It follows that supMt|A|2≀C\sup_{M_{t}}|A|^{2}\leq C for every time for which the solution is defined.∎

5. Long-time existence and exponential convergence

We complete the proof of Theorem 1.1. Throughout the section, we assume that (1.1) and (1.2) hold, with constants satisfying the same smallness assumptions as in our previous results. We first use the curvature estimate to obtain long-time existence and higher-order regularity.

Proposition 5.1.

The solution of (1.3) exists for every tβ‰₯0t\geq 0. Moreover, for every integer mβ‰₯0m\geq 0 and every Ο„>0\tau>0, there exists a constant Cm,Ο„C_{m,\tau} such that

supMt|βˆ‡mA|≀Cm,Ο„for every ​tβ‰₯Ο„.\sup_{M_{t}}|\nabla^{m}A|\leq C_{m,\tau}\qquad\text{for every }t\geq\tau.
Proof.

By Propositions 4.3 and 4.4, we have uniform bounds

|h⁑(t)|≀supMt|H|≀C,supMt|A|2≀C|h(t)|\leq\sup_{M_{t}}|H|\leq C,\qquad\sup_{M_{t}}|A|^{2}\leq C

on the maximal time interval of existence.

The evolution equations for the covariant derivatives of the second fundamental form have the usual form

(βˆ‚tβˆ’Ξ”)βˆ‡mA=βˆ‘i+j+k=mβˆ‡iAβˆ—βˆ‡jAβˆ—βˆ‡kA+hβˆ‘i+j=mβˆ‡iAβˆ—βˆ‡jA,(\partial_{t}-\Delta)\nabla^{m}A=\sum_{i+j+k=m}\nabla^{i}A*\nabla^{j}A*\nabla^{k}A+h\sum_{i+j=m}\nabla^{i}A*\nabla^{j}A,

where the symbol βˆ—* denotes a linear combination of contractions with respect to the induced metric. Since h=h⁑(t)h=h(t) is spatially constant, no spatial derivatives of hh occur. The standard Bernstein argument for mean curvature flow therefore gives, for every mβ‰₯1m\geq 1 and every Ο„>0\tau>0,

supMt|βˆ‡mA|≀Cm,Ο„,tβ‰₯Ο„;\sup_{M_{t}}|\nabla^{m}A|\leq C_{m,\tau},\qquad t\geq\tau;

see, for example, [25, 17]. The constants depend on the uniform bounds for |A||A|, hh, and on Ο„\tau.

The continuation criterion for the flow implies that a finite maximal time can occur only if

lim suptβ†—TmaxsupMt|A|=∞.\limsup_{t\nearrow T_{\max}}\sup_{M_{t}}|A|=\infty.

This is excluded by Proposition 4.4. Hence Tmax=∞.T_{\max}=\infty. ∎

Proposition 5.2 (Eventual convexity and exponential convergence).

There exist T<∞T<\infty and pβˆžβˆˆβ„n+1p_{\infty}\in\mathbb{R}^{n+1} such that MtM_{t} is strictly convex for every tβ‰₯Tt\geq T, and

MtβŸΆβˆ‚BR0​(p∞)M_{t}\longrightarrow\partial B_{R_{0}}(p_{\infty})

exponentially in the smooth topology as tβ†’βˆžt\to\infty. In addition, the limit centre point satisfies

(5.1) |p∞|≀R02​Φ​(Ξ΅0,ΞΈ0).|p_{\infty}|\leq\frac{R_{0}}{2}\Phi(\varepsilon_{0},\theta_{0}).
Proof.

The enclosed volume is preserved along the flow, while the area satisfies

(5.2) dd​t|Mt|=βˆ’βˆ«Mt(Hβˆ’h)2dΞΌt.\frac{d}{dt}|M_{t}|=-\int_{M_{t}}(H-h)^{2}\,d\mu_{t}.

Since the area is nonincreasing and bounded from below, integration of (5.2) gives

(5.3) ∫0∞∫Mt(Hβˆ’h)2​d​μt​𝑑t<∞.\int_{0}^{\infty}\int_{M_{t}}(H-h)^{2}\,d\mu_{t}\,dt<\infty.

Consequently, there exists a sequence tjβ†’βˆžt_{j}\to\infty such that

(5.4) ∫Mtj(Hβˆ’h)2​d​μtj⟢0.\int_{M_{t_{j}}}(H-h)^{2}\,d\mu_{t_{j}}\longrightarrow 0.

By Proposition 3.6, the hypersurfaces remain in a fixed compact annulus and are uniformly star-shaped. In particular, they can be written as radial graphs

Mt={r⁑(Ο‘,t)​ϑ:Ο‘βˆˆπ•Šn},M_{t}=\left\{r(\vartheta,t)\vartheta:\vartheta\in\mathbb{S}^{n}\right\},

where rr is bounded above and below by positive constants and has a uniform gradient bound. Proposition 5.1 and the relations between AA and the derivatives of a radial graph then give uniform bounds for all derivatives of r⁑(β‹…,t)r(\cdot,t), for tβ‰₯1t\geq 1.

It follows from the Arzelà–Ascoli theorem that, after passing to a subsequence,

r⁑(β‹…,tj)⟢r∞r(\cdot,t_{j})\longrightarrow r_{\infty}

smoothly. Thus MtjM_{t_{j}} converges to a smooth, closed, connected and embedded hypersurface M∞M_{\infty}.

The sequence h⁑(tj)h(t_{j}) is bounded. After passing to a further subsequence, we may assume that

h⁑(tj)⟢h∞.h(t_{j})\longrightarrow h_{\infty}.

The smooth convergence and (5.4) imply

HMβˆžβ‰‘h∞.H_{M_{\infty}}\equiv h_{\infty}.

Thus M∞M_{\infty} is a closed embedded hypersurface with constant mean curvature. By Alexandrov’s theorem when nβ‰₯2n\geq 2, and by the classification of closed planar curves with constant curvature when n=1n=1, it is a round sphere.

The C2C^{2}-convergence to a round sphere implies that MtjM_{t_{j}} is uniformly strictly convex for large enough jj. If tj0{t_{j_{0}}} is a time at which our hypersurface is convex, we conclude by Huisken’s theorem [25], that the entire flow MtM_{t} remains convex for tβ‰₯tj0t\geq{t_{j_{0}}} and converges exponentially in the smooth topology to a round sphere as tβ†’βˆžt\to\infty, which necessarily coincides with the limiting sphere M∞M_{\infty} along the subsequence. The corresponding convex convergence result for n=1n=1 is due to Gage [20], while the exponential decay follows from Gage’s estimate for the isoperimetric deficit [20], combined with the uniform parabolic estimates for the flow; see also [11].

By the preservation of the enclosed volume, the radius of the limiting sphere is R0R_{0}. Hence

M∞=βˆ‚BR0​(p∞)M_{\infty}=\partial B_{R_{0}}(p_{\infty})

for some pβˆžβˆˆβ„n+1p_{\infty}\in\mathbb{R}^{n+1}. Finally, for every sufficiently small Ξ΄>0\delta>0, Proposition 3.1 applies with cΞ΄:=R02​Φ​(Ξ΅0,ΞΈ0)+Ξ΄c_{\delta}:=\frac{R_{0}}{2}\Phi(\varepsilon_{0},\theta_{0})+\delta. Hence cΞ΄c_{\delta} is a common reflection threshold for M0M_{0}, and the corresponding radial oscillation estimate (3.7) satisfied by any MtM_{t} passes to the smooth limit:

2​|p∞|=maxM∞⁑|x|βˆ’minM∞|x|≀2​cΞ΄2|p_{\infty}|=\max_{M_{\infty}}|x|-\min_{M_{\infty}}|x|\leq 2c_{\delta}

Letting Ξ΄β†˜0\delta\searrow 0, this concludes the proof. ∎

6. The result in non-flat space forms

6.1. Geometric C1C^{1}-closeness in space forms

We now turn to the analysis of the volume preserving mean curvature flow (1.3) in space forms. Let K∈{βˆ’1,1}K\in\{-1,1\}, and let NKn+1N_{K}^{n+1} denote the simply connected space form of constant sectional curvature KK:

Nβˆ’1n+1=ℍn+1,N1n+1=π•Šn+1.N_{-1}^{n+1}=\mathbb{H}^{n+1},\qquad N_{1}^{n+1}=\mathbb{S}^{n+1}.

We fix a point o∈NKn+1o\in N_{K}^{n+1} and write

r⁑(x)=distNK⁑(o,x).r(x)=\dist_{N_{K}}(o,x).

Let R0>0R_{0}>0 be determined by

(6.1) vol⁑(Ξ©0)=vol⁑(BR0K​(o)),\operatorname{vol}(\Omega_{0})=\operatorname{vol}\bigl(B_{R_{0}}^{K}(o)\bigr),

where Ξ©0\Omega_{0}, as before, is the region enclosed by the initial data. In the spherical case, all hypersurfaces under consideration will be contained in a fixed open hemisphere centred at oo. In particular, the reference radius satisfies 0<R0<Ο€20<R_{0}<\frac{\pi}{2}.

We use the notation

(6.2) sK​(r)={sinh⁑r,K=βˆ’1,sin⁑r,K=1,cK​(r)=sK′​(r).s_{K}(r)=\begin{cases}\sinh r,&K=-1,\\ \sin r,&K=1,\end{cases}\qquad c_{K}(r)=s_{K}^{\prime}(r).

These functions satisfy cKβ€²=βˆ’K​sKc_{K}^{\prime}=-Ks_{K}, cK2+K​sK2=1c_{K}^{2}+Ks_{K}^{2}=1.

We denote by

π•Šon={v∈To​NKn+1:|v|=1}\mathbb{S}_{o}^{n}=\left\{v\in T_{o}N_{K}^{n+1}:|v|=1\right\}

the unit sphere in the tangent space at oo.

We assume that the initial hypersurface satisfies (1.5) and (1.6) for suitably small values of Ξ΅0∈(0,1)\varepsilon_{0}\in(0,1) and ΞΈ0∈(0,Ο€/2)\theta_{0}\in(0,\pi/2) which will be fixed in the following. We next record the interpretation of these assumptions in radial graph coordinates. Since ⟨ν0,βˆ‚r⟩>0,\left\langle\nu_{0},\partial_{r}\right\rangle>0, the initial hypersurface M0M_{0} is star-shaped with respect to oo, and hence can be written as

M0={expo⁑(ρ0​(Ο‘)​ϑ):Ο‘βˆˆπ•Šon}M_{0}=\left\{\exp_{o}\bigl(\rho_{0}(\vartheta)\vartheta\bigr):\vartheta\in\mathbb{S}_{o}^{n}\right\}

for a smooth function ρ0:π•Šonβ†’(0,∞).\rho_{0}:\mathbb{S}_{o}^{n}\rightarrow(0,\infty). In particular, r⁑(expo⁑(ρ0​(Ο‘)​ϑ))=ρ0​(Ο‘).r\left(\exp_{o}\bigl(\rho_{0}(\vartheta)\vartheta\bigr)\right)=\rho_{0}(\vartheta).

Let Οƒ\sigma denote the standard metric on π•Šon\mathbb{S}_{o}^{n}, and let βˆ‡Οƒ\nabla^{\sigma} denote its Levi-Civita connection. Set

v0=1+|βˆ‡ΟƒΟ0|Οƒ2sK​(ρ0)2.v_{0}=\sqrt{1+\frac{|\nabla^{\sigma}\rho_{0}|_{\sigma}^{2}}{s_{K}(\rho_{0})^{2}}}.

The outward unit normal is

Ξ½0=1v0(βˆ‚rβˆ’Οƒi​jβ€‹βˆ‚jρ0sK​(ρ0)2βˆ‚i).\nu_{0}=\frac{1}{v_{0}}\left(\partial_{r}-\frac{\sigma^{ij}\partial_{j}\rho_{0}}{s_{K}(\rho_{0})^{2}}\partial_{i}\right).

It follows that

(6.3) ⟨ν0,βˆ‚r⟩=(1+|βˆ‡ΟƒΟ0|Οƒ2sK​(ρ0)2)βˆ’1/2.\left\langle\nu_{0},\partial_{r}\right\rangle=\left(1+\frac{|\nabla^{\sigma}\rho_{0}|_{\sigma}^{2}}{s_{K}(\rho_{0})^{2}}\right)^{-1/2}.

Consequently,

(6.4) ⟨ν0,βˆ‚r⟩β‰₯cosΞΈ0⟺|βˆ‡ΟƒΟ0|σ≀sK(ρ0)tanΞΈ0.\left\langle\nu_{0},\partial_{r}\right\rangle\geq\cos\theta_{0}\quad\Longleftrightarrow\quad|\nabla^{\sigma}\rho_{0}|_{\sigma}\leq s_{K}(\rho_{0})\tan\theta_{0}.

6.2. The initial reflection property

We shall use the standard linear models to represent NKn+1N_{K}^{n+1}. We set

𝔼Kn+2={ℝn+1,1,K=βˆ’1,ℝn+2,K=1,\mathbb{E}_{K}^{n+2}=\begin{cases}\mathbb{R}^{n+1,1},&K=-1,\\ \mathbb{R}^{n+2},&K=1,\end{cases}

endowed with the Lorentzian scalar product when K=βˆ’1K=-1 and the Euclidean scalar product when K=1K=1. We denote both scalar products by βŸ¨β‹…,β‹…βŸ©K\langle\cdot,\cdot\rangle_{K}. Then

NKn+1={xβˆˆπ”ΌKn+2:⟨x,x⟩K=K},N_{K}^{n+1}=\left\{x\in\mathbb{E}_{K}^{n+2}:\langle x,x\rangle_{K}=K\right\},

where, for K=βˆ’1K=-1, we take the future component of the hyperboloid. In both cases, we choose our origin oo to be the point whose coordinates in the ambient space are (0,…,0,1)(0,\dots,0,1).

Given vβˆˆπ•Šonv\in\mathbb{S}_{o}^{n}, the unit-speed geodesic issuing from oo in the direction vv is

(6.5) Ξ³v​(s)=cK​(s)​o+sK​(s)​v.\gamma_{v}(s)=c_{K}(s)o+s_{K}(s)v.

Its unit tangent vector is

(6.6) Nv,s:=Ξ³Λ™v​(s)=βˆ’K​sK​(s)​o+cK​(s)​v.N_{v,s}:=\dot{\gamma}_{v}(s)=-Ks_{K}(s)o+c_{K}(s)v.

We observe that ⟨γv​(s),Nv,s⟩K=0\langle\gamma_{v}(s),N_{v,s}\rangle_{K}=0. We also set

(6.7) Pv,s={x∈NKn+1:⟨x,Nv,s⟩K=0}.P_{v,s}=\left\{x\in N_{K}^{n+1}:\langle x,N_{v,s}\rangle_{K}=0\right\}.

Then Pv,sP_{v,s} is the totally geodesic hypersurface passing through Ξ³v​(s)\gamma_{v}(s) and perpendicular to Ξ³v\gamma_{v}. We denote the two components of NKn+1βˆ–Pv,sN_{K}^{n+1}\setminus P_{v,s} by

β„‹v,s+={x∈NKn+1:⟨x,Nv,s⟩K>0},β„‹v,sβˆ’={x∈NKn+1:⟨x,Nv,s⟩K<0}.\mathcal{H}_{v,s}^{+}=\left\{x\in N_{K}^{n+1}:\langle x,N_{v,s}\rangle_{K}>0\right\},\qquad\mathcal{H}_{v,s}^{-}=\left\{x\in N_{K}^{n+1}:\langle x,N_{v,s}\rangle_{K}<0\right\}.

Since

⟨o,o⟩K=K,⟨v,v⟩K=1,⟨o,v⟩K=0,\langle o,o\rangle_{K}=K,\qquad\langle v,v\rangle_{K}=1,\qquad\langle o,v\rangle_{K}=0,

equation (6.6) gives

(6.8) ⟨Nv,s,Nv,s⟩K=1,⟨Nv,s,o⟩K=βˆ’sK​(s).\langle N_{v,s},N_{v,s}\rangle_{K}=1,\qquad\langle N_{v,s},o\rangle_{K}=-s_{K}(s).

In the following we will only consider s>0s>0. Then we have ⟨o,Nv,s⟩K<0\langle o,N_{v,s}\rangle_{K}<0, so oβˆˆβ„‹v,sβˆ’o\in\mathcal{H}_{v,s}^{-}.

Let us denote by β„›v,s\mathcal{R}_{v,s} the reflection of the ambient linear space across Pv,sP_{v,s}, that is

(6.9) β„›v,s​(x)=xβˆ’2β€‹βŸ¨x,Nv,s⟩K​Nv,s.\mathcal{R}_{v,s}(x)=x-2\langle x,N_{v,s}\rangle_{K}N_{v,s}.

Since Nv,sN_{v,s} is a unit spacelike vector, this map preserves βŸ¨β‹…,β‹…βŸ©K\langle\cdot,\cdot\rangle_{K}. It therefore restricts to an isometry of NKn+1N_{K}^{n+1}, fixes Pv,sP_{v,s} pointwise and exchanges β„‹v,s+\mathcal{H}_{v,s}^{+} and β„‹v,sβˆ’\mathcal{H}_{v,s}^{-}. Therefore, β„›v,s\mathcal{R}_{v,s} gives the reflection of NKn+1N_{K}^{n+1} across the totally geodesic hyperplane Pv,sP_{v,s}. This explicit representation allowed by the linear model will be convenient in our following analysis.

For fixed vv and variable ss, the hypersurfaces Pv,sP_{v,s} are the standard families used in the Alexandrov moving-plane method in space forms [2]. A detailed account of the construction in the hyperbolic case, with its application to geometric flows, has been recently given in [8, Sections 2.1 and 3.1]; for a unified treatment of moving planes in hyperbolic space and in a spherical hemisphere, see [15, Section 2].

For any closed embedded hypersurface MβŠ‚NKn+1M\subset N_{K}^{n+1}\ , we can give the definitions regarding the reflection of MM exactly as in Definition 2.2, by replacing the Euclidean hyperplanes with the totally geodesic hypersurfaces Pv,sP_{v,s}. Then Theorem 2.3 by Chow-Gulliver on the preservation of strict reflection along the flow holds unchanged in the space form setting.

We now study the relation between the C1C^{1}-closeness to a sphere of our initial data and the reflection property. We follow here a different strategy from the one of the Euclidean case: instead of analyzing M0M_{0} directly as in Proposition 3.1, we first derive estimates for the reflection of a round sphere and then extend the result to M0M_{0} by a perturbative argument.

Lemma 6.1 (Reflection of the reference sphere).

Let SR0K​(o)=βˆ‚BR0K​(o).S_{R_{0}}^{K}(o)=\partial B_{R_{0}}^{K}(o). In the spherical case, assume that R0<Ο€/2R_{0}<\pi/2. Then, for every vβˆˆπ•Šonv\in\mathbb{S}_{o}^{n} and s∈(0,R0]s\in(0,R_{0}], the sphere SR0K​(o)S_{R_{0}}^{K}(o) reflects strictly across Pv,sP_{v,s}. Along the reflection hypersurface we have the transversality relation

(6.10) βŸ¨βˆ‚r,Nv,s⟩K=sK​(s)sK​(R0)>0onSR0K(o)∩Pv,s.\left\langle\partial_{r},N_{v,s}\right\rangle_{K}=\frac{s_{K}(s)}{s_{K}(R_{0})}>0\quad\text{on}\quad S_{R_{0}}^{K}(o)\cap P_{v,s}.

In addition, the reflection is uniform for Pv,sP_{v,s} away from the origin and for xx away from Pv,sP_{v,s}, in the following sense. For any Ξ³>0\gamma>0 and ρ>0\rho>0, there exists δγ,ρ>0\delta_{\gamma,\rho}>0 such that, for every s∈[Ξ³,R0]s\in[\gamma,R_{0}] and vβˆˆπ•Šonv\in\mathbb{S}^{n}_{o}, we have

(6.11) r⁑(β„›v,s​(x))≀R0βˆ’Ξ΄Ξ³,ρr\bigl(\mathcal{R}_{v,s}(x)\bigr)\leq R_{0}-\delta_{\gamma,\rho}

for every x∈SR0K​(o)βˆ©β„‹v,s+x\in S_{R_{0}}^{K}(o)\cap\mathcal{H}_{v,s}^{+} such that dist⁑(x,Pv,s)β‰₯ρ.\dist(x,P_{v,s})\geq\rho.

Proof.

If s=R0s=R_{0}, then SR0K​(o)S_{R_{0}}^{K}(o) and Pv,sP_{v,s} touch at a single point, and the assertions of the theorem are either vacuous or trivial. We then consider s∈(0,R0)s\in(0,R_{0}) and take x∈SR0K​(o)βˆ©β„‹v,s+.x\in S_{R_{0}}^{K}(o)\cap\mathcal{H}_{v,s}^{+}. We set

a=⟨x,Nv,s⟩K,xβˆ—=β„›v,s​(x),a=\langle x,N_{v,s}\rangle_{K},\qquad x^{*}=\mathcal{R}_{v,s}(x),

where a>0a>0 since xβˆˆβ„‹v,s+x\in\mathcal{H}_{v,s}^{+}. Observe that, in our model, the distance from oo is characterized by

(6.12) cK​(r⁑(x))=Kβ€‹βŸ¨x,o⟩K.c_{K}(r(x))=K\langle x,o\rangle_{K}.

Since r⁑(x)=R0r(x)=R_{0}, equations (6.9) and (6.12) give

(6.13) cK​(r⁑(xβˆ—))=Kβ€‹βŸ¨xβˆ’2​a​Nv,s,o⟩K=cK​(R0)βˆ’2​a​Kβ€‹βŸ¨Nv,s,o⟩K=cK​(R0)+2​a​K​sK​(s),c_{K}(r(x^{*}))=K\langle x-2aN_{v,s},o\rangle_{K}=c_{K}(R_{0})-2aK\langle N_{v,s},o\rangle_{K}=c_{K}(R_{0})+2aKs_{K}(s),

which gives cK​(r⁑(xβˆ—))βˆ’cK​(R0)=2​a​K​sK​(s)c_{K}(r(x^{*}))-c_{K}(R_{0})=2aKs_{K}(s). Taking into account the different monotonicity of cK​(r)c_{K}(r) for K=1K=1 and K=βˆ’1K=-1, we conclude in both cases that r⁑(xβˆ—)<R0r(x^{*})<R_{0}, that is, xβˆ—x^{*} is contained in the open ball BR0K​(o)B_{R_{0}}^{K}(o).

To prove (6.10), let us consider any point x∈SR0K​(o)∩Pv,sx\in S_{R_{0}}^{K}(o)\cap P_{v,s}. From (6.5) and (6.6) we see that there is Ο‘βˆˆπ•Š0n\vartheta\in\mathbb{S}_{0}^{n}, such that

x=cK​(R0)​o+sK​(R0)​ϑx=c_{K}(R_{0})o+s_{K}(R_{0})\vartheta
βˆ‚r=βˆ’KsK(R0)o+cK(R0)Ο‘.\partial_{r}=-Ks_{K}(R_{0})o+c_{K}(R_{0})\vartheta.

Using cK2+K​sK2=1c_{K}^{2}+Ks_{K}^{2}=1, these two identities yield

(6.14) o=cK(R0)xβˆ’sK(R0)βˆ‚r.o=c_{K}(R_{0})x-s_{K}(R_{0})\partial_{r}.

Taking the scalar product with Nv,sN_{v,s}, and using ⟨x,Nv,s⟩K=0\langle x,N_{v,s}\rangle_{K}=0 and (6.8) we obtain

βˆ’sK(s)=βˆ’sK(R0)βŸ¨βˆ‚r,Nv,s⟩K,-s_{K}(s)=-s_{K}(R_{0})\langle\partial_{r},N_{v,s}\rangle_{K},

which proves (6.10). That identity implies in particular that Nv,sN_{v,s}, which is the normal direction to the reflecting hypersurface, is transverse to SR0K​(o)S_{R_{0}}^{K}(o) at the intersection points; this completes the verification of the strict reflection.

We now prove the uniform radial separation. By rotational symmetry, it suffices to consider a fixed vβˆˆπ•Šonv\in\mathbb{S}^{n}_{o}. For any given Ξ³,ρ>0\gamma,\rho>0, consider the set

𝒦γ,ρ={(s,x):\displaystyle\mathcal{K}_{\gamma,\rho}=\bigl\{(s,x): γ≀s≀R0,x∈SR0K(o)βˆ©β„‹v,s+,dist(x,Pv,s)β‰₯ρ}.\displaystyle\gamma\leq s\leq R_{0},\quad x\in S_{R_{0}}^{K}(o)\cap\mathcal{H}_{v,s}^{+},\quad\dist(x,P_{v,s})\geq\rho\bigr\}.

If 𝒦γ,ρ\mathcal{K}_{\gamma,\rho} is empty, the assertion is vacuous, and any positive value of δγ,ρ\delta_{\gamma,\rho} may be chosen. Otherwise, it is easy to see that 𝒦γ,ρ\mathcal{K}_{\gamma,\rho} is compact. We know from the first part of the proof that r⁑(β„›v,s​(x))<R0r(\mathcal{R}_{v,s}(x))<R_{0} for all xβˆˆπ’¦Ξ³,ρx\in\mathcal{K}_{\gamma,\rho}. Then, setting δγ,ρ:=min𝒦γ,ρ⁑R0βˆ’r⁑(β„›v,s​(x))>0\delta_{\gamma,\rho}:=\min_{\mathcal{K}_{\gamma,\rho}}R_{0}-r(\mathcal{R}_{v,s}(x))>0, we obtain the sought inequality. ∎

Proposition 6.2 (Initial reflection in space forms).

For any c0∈(0,R0)c_{0}\in(0,R_{0}) there exist Ξ΅0,ΞΈ0>0\varepsilon_{0},\theta_{0}>0, only depending on R0,c0R_{0},c_{0} such that if M0M_{0} satisfies (1.5)–(1.6) then M0M_{0} reflects strictly up to Pv,c0P_{v,c_{0}} for every vβˆˆπ•Šonv\in\mathbb{S}_{o}^{n}.

Proof.

Let us fix c0∈(0,R0)c_{0}\in(0,R_{0}) and take any sβ‰₯c0s\geq c_{0} and vβˆˆπ•Šonv\in\mathbb{S}_{o}^{n}. As before, by rotational symmetry, it is sufficient to take a fixed vv. In addition, we only need to consider s∈[s0,R0​(1+Ξ΅0)]s\in[s_{0},R_{0}(1+\varepsilon_{0})] since otherwise the outer cap of M0M_{0} is empty. We will analyze separately points of M0M_{0} which are close or far from the reflecting hypersurface.

In order to study the behaviour near Pv,sP_{v,s}, we consider signed Fermi coordinates around Pv,sP_{v,s}. We denote by zz the coordinate corresponding to the signed distance function from Pv,sP_{v,s}, chosen to be positive on β„‹v,s+\mathcal{H}_{v,s}^{+}, and by βˆ‚z\partial_{z} the corresponding unit tangent vector. Observe that the reflection β„›v,s\mathcal{R}_{v,s} corresponds to reversing the sign zβ†¦βˆ’zz\mapsto-z and leaving the other coordinates unchanged. Observe also that, at points x∈Pv,sx\in P_{v,s}, we have βˆ‚z(x)=Nv,s\partial_{z}(x)=N_{v,s}. We point out that the vector field βˆ‚z\partial_{z} depends on v,sv,s (in contrast with the Euclidean case, where it only depends on vv), although we omit writing this dependence explicitly.

We want to show that ⟨ν,βˆ‚z⟩>0\langle\nu,\partial_{z}\rangle>0 at points of M0M_{0} close to Pv,sP_{v,s}. To this purpose, we first consider points on the reference sphere. By (6.10), we have for all s∈[c0,R0]s\in[c_{0},R_{0}]

βŸ¨βˆ‚r,βˆ‚z⟩K=βŸ¨βˆ‚r,Nv,z⟩K=sK​(s)sK​(R0)β‰₯sK​(c0)sK​(R0)>0onSR0K(o)∩Pv,s.\left\langle\partial_{r},\partial_{z}\right\rangle_{K}=\left\langle\partial_{r},N_{v,z}\right\rangle_{K}=\frac{s_{K}(s)}{s_{K}(R_{0})}\geq\frac{s_{K}(c_{0})}{s_{K}(R_{0})}>0\quad\text{on}\quad S_{R_{0}}^{K}(o)\cap P_{v,s}.

By uniform continuity, there exists ρ>0\rho>0 enough small, only depending on c0,R0c_{0},R_{0}, such that, for all s∈[c0,R0]s\in[c_{0},R_{0}] and for all y∈SR0K​(o)y\in S_{R_{0}}^{K}(o) with dist⁑(y,Pv,s)≀3​ρ\dist(y,P_{v,s})\leq 3\rho, we have

(6.15) βŸ¨βˆ‚r(y),βˆ‚z(y)⟩Kβ‰₯3​sK​(c0)4​sK​(R0).\langle\partial_{r}(y),\partial_{z}(y)\rangle_{K}\geq\frac{3s_{K}(c_{0})}{4s_{K}(R_{0})}.

By the smooth dependence of βˆ‚z\partial_{z} on ss, after possibly decreasing ρ>0\rho>0 and then Ξ΅0>0\varepsilon_{0}>0, we also have

(6.16) βŸ¨βˆ‚r(x),βˆ‚z(x)⟩Kβ‰₯sK​(c0)2​sK​(R0)\left\langle\partial_{r}(x),\partial_{z}(x)\right\rangle_{K}\geq\frac{s_{K}(c_{0})}{2s_{K}(R_{0})}

for all s∈[c0,R0​(1+Ξ΅0)]s\in[c_{0},R_{0}(1+\varepsilon_{0})] and every x∈NKn+1x\in N^{n+1}_{K} for which there exists y∈SR0K​(o)y\in S_{R_{0}}^{K}(o) satisfying dist⁑(x,y)<ρ\dist(x,y)<\rho and dist⁑(y,Pv,s)≀3​ρ\dist(y,P_{v,s})\leq 3\rho. Let us additionally require that Ξ΅0>0\varepsilon_{0}>0 is small enough to have R0​Ρ0≀ρR_{0}\varepsilon_{0}\leq\rho.

With the above choice of parameters, let us now analyze the reflection of M0M_{0} across Pv,sP_{v,s}, for s∈[c0,R0​(1+Ξ΅0)]s\in[c_{0},R_{0}(1+\varepsilon_{0})]. We first consider any point x∈M0x\in M_{0} such that dist⁑(x,Pv,s)≀2​ρ\dist(x,P_{v,s})\leq 2\rho. We can write x=expo⁑(ρ0​(Ο‘)​ϑ)x=\exp_{o}\bigl(\rho_{0}(\vartheta)\vartheta\bigr) for some ΞΈβˆˆπ•Šon\theta\in\mathbb{S}_{o}^{n}. Let y=expo⁑(R0​ϑ)y=\exp_{o}(R_{0}\vartheta) be the point in SR0K​(o)S_{R_{0}}^{K}(o) on the same radial geodesic. By assumption (1.5) we have

dist⁑(x,y)=|ρ0​(Ο‘)βˆ’R0|≀R0​Ρ0≀ρ.\dist(x,y)=|\rho_{0}(\vartheta)-R_{0}|\leq R_{0}\varepsilon_{0}\leq\rho.

Then we also have

dist⁑(y,Pv,s)≀dist⁑(x,Pv,s)+dist⁑(x,y)≀3​ρ.\dist(y,P_{v,s})\leq\dist(x,P_{v,s})+\dist(x,y)\leq 3\rho.

By (6.16), we conclude that

βŸ¨βˆ‚r(x),βˆ‚z(x)⟩Kβ‰₯sK​(c0)2​sK​(R0)>0\left\langle\partial_{r}(x),\partial_{z}(x)\right\rangle_{K}\geq\frac{s_{K}(c_{0})}{2s_{K}(R_{0})}>0

for all x∈M0x\in M_{0} such that dist⁑(x,Pv,s)≀2​ρ\dist(x,P_{v,s})\leq 2\rho.

It then follows from (1.6) that for any x∈M0x\in M_{0} such that dist⁑(x,Pv,s)≀2​ρ\dist(x,P_{v,s})\leq 2\rho, we have

(6.17) ⟨ν0​(x),βˆ‚z(x)⟩Kβ‰₯βŸ¨βˆ‚r(x),βˆ‚z(x)⟩Kβˆ’|Ξ½0​(x)βˆ’βˆ‚r(x)|β‰₯sK​(c)2​sK​(R0)βˆ’2βˆ’2cosΞΈ0>0,\left\langle\nu_{0}(x),\partial_{z}(x)\right\rangle_{K}\geq\left\langle\partial_{r}(x),\partial_{z}(x)\right\rangle_{K}-|\nu_{0}(x)-\partial_{r}(x)|\geq\frac{s_{K}(c)}{2s_{K}(R_{0})}-\sqrt{2-2\cos\theta_{0}}>0,

provided ΞΈ0\theta_{0} is sufficiently small, depending only on c0c_{0}, R0R_{0}.

In particular, for points x∈M0∩Pv,sx\in M_{0}\cap P_{v,s}, (6.17) shows that ⟨ν0​(x),Nv,s⟩>0\langle\nu_{0}(x),N_{v,s}\rangle>0, i.e. Nv,sN_{v,s} is not tangent to M0M_{0} along the intersection with Pv,sP_{v,s}.

In addition, similarly to the Euclidean case, the positivity of ⟨ν0,Nv,s⟩\langle\nu_{0},N_{v,s}\rangle allows to exclude that a point x∈M0βˆ©β„‹v,s+x\in M_{0}\cap\mathcal{H}_{v,s}^{+} with dist⁑(x,Pv.s)≀2​ρ\dist(x,P_{v.s})\leq 2\rho satisfies β„›v,s​(x)∈M0\mathcal{R}_{v,s}(x)\in M_{0}. In fact, xx and β„›v,s​(x)\mathcal{R}_{v,s}(x) lie on the same geodesic perpendicular to Pv,sP_{v,s} parametrized by z∈[βˆ’2​ρ,2​ρ]z\in[-2\rho,2\rho]. Along such a geodesic, the scalar product ⟨ν0,βˆ‚z(x)⟩K\left\langle\nu_{0},\partial_{z}(x)\right\rangle_{K} must change sign on two consecutive transverse intersections with M0M_{0}, depending on whether the geodesic enters or exits the region enclosed by M0M_{0} as zz increases. On the other hand, (6.17) shows that the sign is always positive. This implies that there can be at most one intersection, and therefore β„›v,s​(M0)\mathcal{R}_{v,s}(M_{0}) cannot intersect M0M_{0} at points at distance less than 2​ρ2\rho from Pv,sP_{v,s}.

We observe that, for R0≀s≀R0​(1+Ξ΅0)R_{0}\leq s\leq R_{0}(1+\varepsilon_{0}), every point x∈M0βˆ©β„‹v,s+x\in M_{0}\cap\mathcal{H}^{+}_{v,s} satisfies

dist⁑(x,Pv,s)≀r⁑(x)βˆ’s≀R0​Ρ0≀ρ<2​ρ.\operatorname{dist}(x,P_{v,s})\leq r(x)-s\leq R_{0}\varepsilon_{0}\leq\rho<2\rho.

Thus, for such values of ss, the whole outer cap is covered by the preceding near-hyperplane argument.

It remains to consider s∈[c0,R0]s\in[c_{0},R_{0}] and points x∈M0βˆ©β„‹v,s+x\in M_{0}\cap\mathcal{H}^{+}_{v,s} such that dist⁑(x,Pv,s)>2​ρ\dist(x,P_{v,s})>2\rho. As before, we can use (1.5) to show that there is y∈SR0K​(o)y\in S_{R_{0}}^{K}(o) on the same radial geodesic, which satisfies dist⁑(x,y)≀R0​Ρ0≀ρ\dist(x,y)\leq R_{0}\varepsilon_{0}\leq\rho. Then yy satisfies

dist⁑(y,Pv,s)β‰₯dist⁑(x,Pv,s)βˆ’dist⁑(x,y)β‰₯ρ\dist(y,P_{v,s})\geq\dist(x,P_{v,s})-\dist(x,y)\geq\rho

and therefore

r⁑(β„›v,s​(y))≀R0βˆ’Ξ΄,r(\mathcal{R}_{v,s}(y))\leq R_{0}-\delta,

where Ξ΄=δ⁑(ρ,c0,R0)>0\delta=\delta(\rho,c_{0},R_{0})>0 is given from Lemma 6.1. Since β„›v,s\mathcal{R}_{v,s} is an isometry, we deduce

r⁑(β„›v,s​(x))≀r⁑(β„›v,s​(y))+dist⁑(x,y)≀R0βˆ’Ξ΄+R0​Ρ0.r(\mathcal{R}_{v,s}(x))\leq r(\mathcal{R}_{v,s}(y))+\dist(x,y)\leq R_{0}-\delta+R_{0}\varepsilon_{0}.

For Ξ΅0>0\varepsilon_{0}>0 small enough to have 2​R0​Ρ0<Ξ΄2R_{0}\varepsilon_{0}<\delta, we conclude that r⁑(β„›v,s​(x))<R0​(1βˆ’Ξ΅0)r(\mathcal{R}_{v,s}(x))<R_{0}(1-\varepsilon_{0}), so that by (1.5) β„›v,s​(x)\mathcal{R}_{v,s}(x) lies in the interior of the region bounded by M0M_{0}.

Thus, we have shown that M0M_{0} reflects strictly across every Pv,sP_{v,s} with v∈Sonv\in S_{o}^{n} and sβ‰₯c0s\geq c_{0}. ∎

We next derive the quantitative geometric consequence of the reflection property that will replace the Euclidean estimate for the tangential part of the position vector. Let

(6.18) Y=sK(r)βˆ‚rY=s_{K}(r)\partial_{r}

be the radial conformal vector field. Reflection up to distance cc in every direction controls the tangential component of YY, and hence the gradient of the radial graph function.

Lemma 6.3 (Gradient estimate from Alexandrov reflection).

Let MβŠ‚NKn+1M\subset N_{K}^{n+1} be a smooth, closed and embedded hypersurface which reflects strictly up to Pv,cP_{v,c} for every vβˆˆπ•Šonv\in\mathbb{S}_{o}^{n}. Then, wherever sK​(r)>sK​(c),s_{K}(r)>s_{K}(c), one has

(6.19) ⟨ν,βˆ‚r⟩β‰₯1βˆ’sK​(c)2sK​(r)2.\left\langle\nu,\partial_{r}\right\rangle\geq\sqrt{1-\frac{s_{K}(c)^{2}}{s_{K}(r)^{2}}}.

If MM is written as a radial graph M={expo⁑(ρ⁑(Ο‘)​ϑ):Ο‘βˆˆπ•Šon},M=\left\{\exp_{o}\bigl(\rho(\vartheta)\vartheta\bigr):\vartheta\in\mathbb{S}_{o}^{n}\right\}, then

(6.20) |βˆ‡ΟƒΟ|σ≀sK​(c)​sK​(ρ)sK​(ρ)2βˆ’sK​(c)2.|\nabla^{\sigma}\rho|_{\sigma}\leq\frac{s_{K}(c)s_{K}(\rho)}{\sqrt{s_{K}(\rho)^{2}-s_{K}(c)^{2}}}.
Proof.

Fix x∈Mx\in M. If YT​(x)=0Y^{T}(x)=0, there is nothing to prove. Assume YT​(x)β‰ 0Y^{T}(x)\neq 0, and set Ο„=YT​(x)|YT​(x)|.\tau=\frac{Y^{T}(x)}{|Y^{T}(x)|}. Then βŸ¨βˆ‚r,Ο„βŸ©K>0.\langle\partial_{r},\tau\rangle_{K}>0.

We now use the linear model of NKn+1N_{K}^{n+1} and consider the hyperplane Ο„βŸ‚βŠ‚π”ΌKn+2\tau^{\perp}\subset\mathbb{E}_{K}^{n+2} orthogonal to Ο„\tau. As Ο„βˆˆTx​MβŠ‚Tx​NKn+1\tau\in T_{x}M\subset T_{x}N_{K}^{n+1}, xx belongs to the hypersurface PΟ„=NKn+1βˆ©Ο„βŸ‚P_{\tau}=N_{K}^{n+1}\cap\tau^{\perp}, which is totally geodesic. Moreover, Ο„βˆˆTx​M\tau\in T_{x}M, showing that MM does not reflect strictly across PΟ„P_{\tau} because the transversality condition is violated.

Let sβ‰₯0s\geq 0 denote the distance from oo to PΟ„P_{\tau}. Since Ο„\tau is the unit normal to a totally geodesic hypersurface at distance ss from oo, by (6.8) it holds

sK(s)=βˆ’βŸ¨o,Ο„βŸ©K=sK(r)βŸ¨βˆ‚r,Ο„βŸ©K,s_{K}(s)=-\langle o,\tau\rangle_{K}=s_{K}(r)\langle\partial_{r},\tau\rangle_{K},

where we have written o=cK(r)xβˆ’sK(r)βˆ‚ro=c_{K}(r)x-s_{K}(r)\partial_{r} as in the final part of the proof of Lemma 6.1.

Since the reflection property does not hold, the distance of the hypersurface PΟ„P_{\tau} must satisfy s<cs<c otherwise we contradict our hypotheses. We conclude

⟨ν,βˆ‚r⟩2=1βˆ’βŸ¨Ο„,βˆ‚r⟩2=1βˆ’sK​(s)2sK​(r)2β‰₯1βˆ’sK​(c)2sK​(r)2.\langle\nu,\partial_{r}\rangle^{2}=1-\langle\tau,\partial_{r}\rangle^{2}=1-\frac{s_{K}(s)^{2}}{s_{K}(r)^{2}}\geq 1-\frac{s_{K}(c)^{2}}{s_{K}(r)^{2}}.

The orientation is chosen so that ⟨ν,βˆ‚r⟩>0\langle\nu,\partial_{r}\rangle>0, and therefore (6.19) follows. Finally, for a radial graph, combining (6.4) with (6.19) and solving for |βˆ‡ΟƒΟ|Οƒ|\nabla^{\sigma}\rho|_{\sigma} gives (6.20). ∎

We now combine the preceding gradient estimate with volume preservation to control the radial position of the evolving hypersurfaces.

Proposition 6.4 (Radial closeness for later times).

Let c0>0c_{0}>0 be suitably small (depending on R0R_{0}) and let the initial data satisfy (1.5) and (1.6) with Ξ΅0,ΞΈ0>0\varepsilon_{0},\theta_{0}>0 the values given by Proposition 6.2. Then, for every time for which the solution is defined, we have

(6.21) |r⁑(x)βˆ’R0|≀2​π​sK​(c0)for every ​x∈Mt.\big|r(x)-R_{0}\big|\leq 2\pi s_{K}(c_{0})\qquad\text{for every }x\in M_{t}.

In particular, in the case K=1K=1, if Ξ΅0,ΞΈ0\varepsilon_{0},\theta_{0} are suitably small then the solution remains inside the half-sphere of radius Ο€/2\pi/2 centred at oo.

Proof.

The strict reflection property is preserved by the flow by Theorem 2.3. Then we can apply the gradient estimate from Lemma 6.3 for every time in the existence interval.

In the case K=1K=1, let us set

Tβˆ—=sup{T>0:R02<r<Ο€2Β onΒ Mt,Β for everyΒ t∈[0,T)}.T^{*}=\sup\left\{T>0:\frac{R_{0}}{2}<r<\frac{\pi}{2}\text{ on }M_{t},\text{ for every }t\in[0,T)\right\}.

In the case K=βˆ’1K=-1, we define Tβˆ—T^{*} analogously, but requiring only the bound from below R02<r\frac{R_{0}}{2}<r. The initial annular assumption, together with the condition R0​(1+Ο΅0)<Ο€/2R_{0}(1+\epsilon_{0})<\pi/2 in the K=1K=1 case, implies by continuity that Tβˆ—>0T^{*}>0.

By requiring c0c_{0} to be sufficiently small, we may assume that sK​(c0)≀34​sK​(R0/2).s_{K}(c_{0})\leq\sqrt{\frac{3}{4}}s_{K}(R_{0}/2). Then on [0,Tβˆ—)[0,T^{*}) estimate (6.20) gives

|βˆ‡ΟƒΟ|σ≀sK​(c0)​sK​(ρ)sK​(ρ)2βˆ’sK​(c0)2≀2​sK​(c0).|\nabla^{\sigma}\rho|_{\sigma}\leq\frac{s_{K}(c_{0})s_{K}(\rho)}{\sqrt{s_{K}(\rho)^{2}-s_{K}(c_{0})^{2}}}\leq 2s_{K}(c_{0}).

Since the diameter of (π•Šon,Οƒ)(\mathbb{S}_{o}^{n},\sigma) is Ο€\pi, we conclude

(6.22) ρ+​(t)βˆ’Οβˆ’β€‹(t)≀2​π​sK​(c0),\rho_{+}(t)-\rho_{-}(t)\leq 2\pi\,s_{K}(c_{0}),

where Οβˆ’β€‹(t)=minπ•Šon⁑ρ⁑(β‹…,t),\rho_{-}(t)=\min_{\mathbb{S}_{o}^{n}}\rho(\cdot,t), ρ+​(t)=maxπ•Šon⁑ρ⁑(β‹…,t).\rho_{+}(t)=\max_{\mathbb{S}_{o}^{n}}\rho(\cdot,t).

We now use volume preservation to locate this annulus. Since vol⁑(Ξ©t)=vol⁑(BR0K​(o))\operatorname{vol}(\Omega_{t})=\operatorname{vol}\bigl(B_{R_{0}}^{K}(o)\bigr) and MtM_{t} is a radial graph, the monotonicity of the volume of geodesic balls implies

Οβˆ’β€‹(t)≀R0≀ρ+​(t).\rho_{-}(t)\leq R_{0}\leq\rho_{+}(t).

Combining this with (6.22), we obtain

(6.23) R0βˆ’2​π​sK​(c0)≀ρ⁑(Ο‘,t)≀R0+2​π​sK​(c0).R_{0}-2\pi\,s_{K}(c_{0})\leq\rho(\vartheta,t)\leq R_{0}+2\pi\,s_{K}(c_{0}).

We choose c0c_{0} so small that R0βˆ’2​π​sK​(c0)>R02R_{0}-2\pi s_{K}(c_{0})>\frac{R_{0}}{2}. In the K=1K=1 case, we also require R0+2​π​sK​(c0)<Ο€/2R_{0}+2\pi\,s_{K}(c_{0})<\pi/2. Suppose Tβˆ—<TmaxT^{*}<T_{\max}. Then the smoothness of the flow implies that (6.23) also holds at t=Tβˆ—t=T^{*}. Then we have

R02<minMTβˆ—β‘r≀maxMTβˆ—β‘r<Ο€2,\frac{R_{0}}{2}<\min_{M_{T^{*}}}r\leq\max_{M_{T^{*}}}r<\frac{\pi}{2},

where the last inequality only concerns the K=1K=1 case. By continuity, the strict inequalities also hold up to a larger time, contradicting the maximality of Tβˆ—T^{*}. This shows that Tβˆ—=TmaxT^{*}=T_{\max} and that our radial bound holds for every time for which the solution exists. ∎

Corollary 6.5 (Normal control for later times).

Let our solution satisfy the reflection property with threshold c0c_{0}. Then, for every time for which it is defined, we have ⟨ν,βˆ‚r⟩β‰₯Οƒβˆ—\langle\nu,\partial_{r}\rangle\geq\sigma_{*}, for some Οƒβˆ—=Οƒβˆ—β€‹(c0,R0)>0\sigma_{*}=\sigma_{*}(c_{0},R_{0})>0. Moreover, for any R0>0R_{0}>0, we have Οƒβˆ—β€‹(c0,R0)β†’1\sigma_{*}(c_{0},R_{0})\to 1 as c0β†’0c_{0}\to 0.

Proof.

The result follows directly from (6.19) and the lower bound on rr given by Proposition 6.4. ∎

Corollary 6.6 (Reflection and geometric C1C^{1}-closeness in space forms).

Let K∈{βˆ’1,1}K\in\{-1,1\}. Within the volume-normalized and hemispherically localized class considered above, strong Alexandrov reflection in every direction and geometric C1C^{1}-closeness to a geodesic sphere determine each other quantitatively, up to a change of parameters.

More precisely, sufficiently small annular width and normal oscillation give the common reflection threshold of Proposition 6.2. Conversely, a common threshold tending to zero implies the radial and normal estimates of Proposition 6.4 and Corollary 6.5, whose deviations from the reference geodesic sphere also tend to zero.

Proof.

The first implication is Proposition 6.2. For the converse, Lemma 6.3 gives the tangential and normal control from the reflection threshold, while the volume-normalized radial estimate follows from the argument of Proposition 6.4. ∎

The preceding corollary is the space-form counterpart of Corollary 3.5. The difference is that the initial reflection threshold is obtained perturbatively from the strict reflection property of the reference geodesic sphere, rather than from the explicit Euclidean formula (3.1). Once established, however, reflection provides the same type of first-order geometric control required in the curvature estimates.

6.3. Curvature estimates

We now extend the curvature estimates of Section 4 to the non-flat space forms. The proof is the same as in the Euclidean case, except for the presence of ambient-curvature terms. Since K∈{βˆ’1,1}K\in\{-1,1\} is constant and the hypersurfaces remain in a fixed compact annulus with a uniform lower bound for ⟨ν,βˆ‚r⟩\langle\nu,\partial_{r}\rangle, all these additional terms are of lower order and can be absorbed into the constants. We only indicate the necessary modifications.

With the notation from (6.18), the support function reads as u=⟨Y,ν⟩.u=\langle Y,\nu\rangle. By Proposition 6.4 and Corollary 6.5, there exist constants rβˆ—,rβˆ—>0r_{*},r^{*}>0 and Οƒβˆ—>0\sigma_{*}>0 such that

(6.24) rβˆ—β‰€r≀rβˆ—,⟨ν,βˆ‚r⟩β‰₯Οƒβˆ—r_{*}\leq r\leq r^{*},\qquad\langle\nu,\partial_{r}\rangle\geq\sigma_{*}

throughout the existence interval. In the spherical case, we also have rβˆ—<Ο€/2r^{*}<\pi/2. Consequently,

(6.25) 0<uβˆ—β‰€u≀uβˆ—<∞.0<u_{*}\leq u\leq u^{*}<\infty.

The evolution equations of the main geometric quantities take the following form, see, for example, [24, 9, 29].

Lemma 6.7 (Evolution equations in space forms).

Under (1.3) it holds

  1. (a)

    (βˆ‚tβˆ’Ξ”)H=(Hβˆ’h)(|A|2+nK)(\partial_{t}-\Delta)H=(H-h)(|A|^{2}+nK).

  2. (b)

    (βˆ‚tβˆ’Ξ”)|A|2=βˆ’2|βˆ‡A|2+2|A|2(|A|2βˆ’nK)+4KH2βˆ’2h(tr(A3)+KH).(\partial_{t}-\Delta)|A|^{2}=-2|\nabla A|^{2}+2|A|^{2}\big(|A|^{2}-nK\big)+4KH^{2}-2h\big(\!\operatorname{tr}(A^{3})+KH\big).

  3. (c)

    (βˆ‚tβˆ’Ξ”)u=cK(r)(hβˆ’2H)+|A|2u.(\partial_{t}-\Delta)u=c_{K}(r)(h-2H)+|A|^{2}u.

Proposition 6.8 (Uniform mean curvature bound).

There exists a constant C<∞C<\infty such that

|H|≀C|H|\leq C

for every time for which the solution is defined.

Proof.

Choose Ξ±>0\alpha>0 such that uβˆ’Ξ±β‰₯Ξ·βˆ—>0u-\alpha\geq\eta_{*}>0 along the flow, and define

Z=Huβˆ’Ξ±.Z=\frac{H}{u-\alpha}.

Using Lemma 6.7 (a) and (c), we obtain

(6.26) (βˆ‚tβˆ’Ξ”)Z=\displaystyle(\partial_{t}-\Delta)Z={} βˆ’Ξ±β€‹Z+huβˆ’Ξ±β€‹|A|2βˆ’huβˆ’Ξ±β€‹Z+2​Z2+2uβˆ’Ξ±β€‹βŸ¨βˆ‡u,βˆ‡Z⟩+EK,\displaystyle-\frac{\alpha Z+h}{u-\alpha}|A|^{2}-\frac{h}{u-\alpha}Z+2Z^{2}+\frac{2}{u-\alpha}\langle\nabla u,\nabla Z\rangle+E_{K},

where

EK=n​K​Zβˆ’n​K​huβˆ’Ξ±βˆ’(cK​(r)βˆ’1)​huβˆ’Ξ±β€‹Z+2​(cK​(r)βˆ’1)​Z2,E_{K}=nKZ-\frac{nKh}{u-\alpha}-\frac{(c_{K}(r)-1)h}{u-\alpha}Z+2(c_{K}(r)-1)Z^{2},

and the remaining terms on the right-hand side of (6.26) are the same as in the Euclidean calculation. By (6.24) and (6.25), the coefficients in EKE_{K} are uniformly bounded, hence

(6.27) |EK|≀C⁑(|Z|+Z2+|h|​(1+|Z|)).|E_{K}|\leq C\bigl(|Z|+Z^{2}+|h|(1+|Z|)\bigr).

Writing Ξ΄:=β€–uβˆ’sK​(R0)β€–Lβˆžβ€‹(Mt),\delta:=\|u-s_{K}(R_{0})\|_{L^{\infty}(M_{t})}, the space form version of the Minkowski formula gives |h|≀C⁑(1+δ​‖Hβ€–Lβˆžβ€‹(Mt))|h|\leq C\bigl(1+\delta\|H\|_{L^{\infty}(M_{t})}\bigr), as in Lemma 4.1. By Proposition 6.4 and Corollary 6.5, Ξ΄\delta can be made arbitrarily small by choosing the initial parameters sufficiently small. Hence the part of hh which grows with β€–Zβ€–L∞\|Z\|_{L^{\infty}} has an arbitrarily small coefficient, while the remaining contribution is of lower order.

Thus the leading term remains the one involving Z​|A|2Z|A|^{2}, because of the estimate

|A|2β‰₯H2n=(uβˆ’Ξ±)2​Z2n.|A|^{2}\geq\frac{H^{2}}{n}=\frac{(u-\alpha)^{2}Z^{2}}{n}.

This term provides the same cubic terms in the upper and lower maximum-principle estimates as in the Euclidean argument, while the additional KK-terms are of lower order.

The maximum-principle argument of Proposition 4.3 therefore applies, with only a change in the constants. In this way we obtain uniform bounds from above and below on ZZ, which in turn yield the desired assertion on HH. ∎

Proposition 6.9 (Uniform bound for the shape operator).

There exists a constant C<∞C<\infty such that

|A|2≀C|A|^{2}\leq C

for every time for which the solution is defined.

Proof.

Setting q=⟨ν,βˆ‚r⟩q=\langle\nu,\partial_{r}\rangle and v=qβˆ’1v=q^{-1}, (6.24) ensures that

1≀v≀vβˆ—:=Οƒβˆ—βˆ’1.1\leq v\leq v_{*}:=\sigma_{*}^{-1}.

The evolution equation for vv has the same principal terms as in the Euclidean case:

(6.28) (βˆ‚tβˆ’Ξ”)v=βˆ’|A|2vβˆ’2vβˆ’1|βˆ‡v|2+βŸ¨π’³,βˆ‡v⟩+β„›K,(\partial_{t}-\Delta)v=-|A|^{2}v-2v^{-1}|\nabla v|^{2}+\langle\mathcal{X},\nabla v\rangle+\mathcal{R}_{K},

where 𝒳\mathcal{X} is a uniformly bounded tangential vector field and β„›K\mathcal{R}_{K} contains the terms involving HH, hh, the radial coefficients sKs_{K}, cKc_{K}, and the curvature KK. Notice that no term of order higher than |A|2​v|A|^{2}v is introduced by the ambient curvature. More precisely, 𝒳\mathcal{X} and RKR_{K} depend only on the uniformly controlled quantities rr, vv, HH, and hh, and on the bounded radial coefficients sK​(r)s_{K}(r) and cK​(r)c_{K}(r). In particular, they contain no uncontrolled component of AA, and hence

|𝒳|+|β„›K|≀C.|\mathcal{X}|+|\mathcal{R}_{K}|\leq C.

Choose k>0k>0 such that k​vβˆ—2<1kv_{*}^{2}<1, and define β„±\mathscr{F} as in (4.13). As in the Euclidean case, β„±\mathscr{F} is uniformly equivalent to |A|2|A|^{2}. Combining the evolution from Lemma 6.7 (b) and (6.28), computing as in the proof of Proposition 4.4, we reach

(6.29) (βˆ‚tβˆ’Ξ”)β„±β‰€βˆ’cβ„±2+Cβ„±+C+βŸ¨π’³1,βˆ‡β„±βŸ©βˆ’c1|βˆ‡v|2β„±,(\partial_{t}-\Delta)\mathscr{F}\leq-c\mathscr{F}^{2}+C\mathscr{F}+C+\langle\mathcal{X}_{1},\nabla\mathscr{F}\rangle-c_{1}|\nabla v|^{2}\mathscr{F},

for uniform constants c,c1>0c,c_{1}>0 and C<∞C<\infty. Indeed, the additional terms in Lemma 6.7 (b) satisfy

|βˆ’2​n​K​|A|2+4​K​H2βˆ’2​K​h​H|≀C⁑(1+|A|2),\left|-2nK|A|^{2}+4KH^{2}-2KhH\right|\leq C(1+|A|^{2}),

and therefore contribute at most C⁑(β„±+1)C(\mathscr{F}+1) to (6.29). Similarly, the terms collected in β„›K\mathcal{R}_{K} contribute at most C​ℱC\mathscr{F}.

At a spatial maximum of β„±\mathscr{F}, the drift term vanishes and the term involving |βˆ‡v|2​ℱ|\nabla v|^{2}\mathscr{F} is nonpositive. Hence an equation of the form (4.21) also holds in this setting. The maximum principle therefore gives a uniform bound for β„±\mathscr{F}, and hence for |A|2|A|^{2}. ∎

Since the ambient space has constant curvature, the evolution equations for the covariant derivatives of AA differ from their Euclidean counterparts only by lower-order contractions involving KK, AA, and its derivatives. The standard Bernstein estimates therefore imply that, for every integer mβ‰₯0m\geq 0 and every Ο„>0\tau>0,

supMt|βˆ‡mA|≀Cm,Ο„for every ​tβ‰₯Ο„.\sup_{M_{t}}|\nabla^{m}A|\leq C_{m,\tau}\qquad\text{for every }t\geq\tau.

Consequently, the solution exists for every tβ‰₯0t\geq 0.

6.4. Subsequential convergence

We next use the area dissipation identity and the uniform estimates obtained above to identify the possible limiting hypersurfaces.

Proposition 6.10 (Subsequential convergence).

There exist a sequence tjβ†’βˆžt_{j}\to\infty and a point pβˆ—βˆˆNKn+1p_{*}\in N_{K}^{n+1} such that

Mtj⟢SR0K​(pβˆ—):=βˆ‚BR0K​(pβˆ—)M_{t_{j}}\longrightarrow S_{R_{0}}^{K}(p_{*}):=\partial B_{R_{0}}^{K}(p_{*})

smoothly.

Proof.

The proof is the same as in the first part of Proposition 5.2. Indeed, the area dissipation identity is unchanged, and therefore there exists a sequence tjβ†’βˆžt_{j}\to\infty such that (5.4) holds.

The radial and normal estimates, together with the higher-order curvature bounds proved above, give smooth compactness for the radial graph functions

Mt={expo⁑(ρ⁑(Ο‘,t)​ϑ):Ο‘βˆˆπ•Šon}.M_{t}=\left\{\exp_{o}\bigl(\rho(\vartheta,t)\vartheta\bigr):\vartheta\in\mathbb{S}_{o}^{n}\right\}.

Thus, after passing to a subsequence, MtjM_{t_{j}} converges smoothly to a closed embedded constant-mean-curvature hypersurface M∞M_{\infty}.

By Alexandrov’s theorem in NKn+1N_{K}^{n+1}, M∞M_{\infty} is a geodesic sphere. In the spherical case, the fixed-hemisphere assumption ensures that the corresponding version of the theorem applies. Finally, volume preservation and the strict monotonicity of the volume of geodesic balls show that its radius is R0R_{0}. Hence the statement follows. ∎

6.5. Eventual convexity and exponential convergence

The preceding proposition provides a late time slice which is arbitrarily close in the smooth topology to a geodesic sphere.

We now complete the proof of exponential convergence and at the same time show that convexity is eventually attained, although no convexity or mean-convexity is assumed initially. Smooth subsequential convergence to a geodesic sphere implies that a sufficiently late time slice is uniformly strictly convex. In Euclidean and hyperbolic space, the conclusion then follows by restarting the flow and applying the corresponding convergence theorems for convex hypersurfaces. In the spherical case, where convexity is not preserved in general by (1.3), we instead use the evolution of |A|2/H2|A|^{2}/H^{2}. The ambient-curvature term in this evolution has a favourable sign near a geodesic sphere and yields exponential decay of the traceless second fundamental form.

Proposition 6.11 (Eventual convexity and exponential convergence).

Let K∈{βˆ’1,1}K\in\{-1,1\}, and assume in the spherical case that R0<Ο€/2R_{0}<\pi/2. Then there exist T<∞T<\infty and p∞∈NKn+1p_{\infty}\in N_{K}^{n+1} such that MtM_{t} is strictly convex (hh-convex in case K=βˆ’1K=-1) for every tβ‰₯Tt\geq T and

MtβŸΆβˆ‚BR0K​(p∞)M_{t}\longrightarrow\partial B_{R_{0}}^{K}(p_{\infty})

exponentially in the smooth topology.

Proof.

By Proposition 6.10, there exist a sequence tjβ†’βˆžt_{j}\to\infty and pβˆ—βˆˆNKn+1p_{*}\in N_{K}^{n+1} such that Mtjβ†’Sβˆ—:=βˆ‚BR0K​(pβˆ—)M_{t_{j}}\to S_{*}:=\partial B_{R_{0}}^{K}(p_{*}) smoothly. Setting Ξ»0=cK​(R0)sK​(R0),\lambda_{0}=\frac{c_{K}(R_{0})}{s_{K}(R_{0})}, the Weingarten operator of Sβˆ—S_{*} is hij=Ξ»0​δij.h_{i}^{j}=\lambda_{0}\delta_{i}^{j}. Since Ξ»0>0\lambda_{0}>0, smooth convergence implies that, for all sufficiently large jj,

ΞΊi(β‹…,tj)β‰₯Ξ»02>0,i=1,…,n.\kappa_{i}(\cdot,t_{j})\geq\frac{\lambda_{0}}{2}>0,\qquad i=1,\ldots,n.

Thus MtjM_{t_{j}} is uniformly strictly convex. If K=βˆ’1K=-1, then Ξ»0=coth⁑R0>1\lambda_{0}=\coth R_{0}>1, and we may choose jj so large that

|ΞΊi​(β‹…,tj)βˆ’coth⁑R0|<coth⁑R0βˆ’12\left|\kappa_{i}(\cdot,t_{j})-\coth R_{0}\right|<\frac{\coth R_{0}-1}{2}

for every i=1,…,ni=1,\ldots,n. Consequently,

ΞΊi(β‹…,tj)>1+coth⁑R02>1,i=1,…,n,\kappa_{i}(\cdot,t_{j})>\frac{1+\coth R_{0}}{2}>1,\qquad i=1,\ldots,n,

and MtjM_{t_{j}} is strictly convex by horospheres.

Fix one such time t0=tjt_{0}=t_{j}. If K=βˆ’1K=-1, the time slice Mt0M_{t_{0}} is strictly convex by horospheres. The convergence theorem for (1.3) in hyperbolic space [9] implies that the time-shifted solution remains convex by horospheres and converges exponentially to a geodesic sphere. The enclosed volume is preserved, and therefore the limiting geodesic sphere has radius R0R_{0}. For the exponential convergence in the hyperbolic plane, one only needs κ⁑(β‹…,tj)>0\kappa(\cdot,t_{j})>0 and then invoke the corresponding convexity theorem in [34].

It remains to prove the result when K=1K=1. In this case, we could invoke the convergence theorem by Hartley [21]. However, since that result relies on deep arguments using analytic semigroups and centre manifold theory, we provide a direct independent proof, which exploits the stronger properties of the solution obtained above.

We treat separately the cases nβ‰₯2n\geq 2 and n=1n=1. If nβ‰₯2n\geq 2, we give a direct pinching argument for Q=|A|2H2Q=\frac{|A|^{2}}{H^{2}}.

Since Mt0M_{t_{0}} is arbitrarily close to Sβˆ—S_{*} in C∞C^{\infty}, after increasing t0t_{0} we may assume that

(6.30) Ξ»02≀κi≀2​λ0,n​λ02≀H,h≀2​n​λ0,hH≀32\frac{\lambda_{0}}{2}\leq\kappa_{i}\leq 2\lambda_{0},\qquad\frac{n\lambda_{0}}{2}\leq H,h\leq 2n\lambda_{0},\qquad\frac{h}{H}\leq\frac{3}{2}

on Mt0M_{t_{0}}, where λ0=cot⁑R0\lambda_{0}=\cot R_{0}.

By Lemma 6.7 (a) and (b) (see also [29, Lemma 5.1]), one has

(βˆ‚tβˆ’Ξ”)Q=\displaystyle(\partial_{t}-\Delta)Q={} 2HβŸ¨βˆ‡H,βˆ‡QβŸ©βˆ’2H4|Hβˆ‡Aβˆ’AβŠ—βˆ‡H|2\displaystyle\frac{2}{H}\langle\nabla H,\nabla Q\rangle-\frac{2}{H^{4}}|H\nabla A-A\otimes\nabla H|^{2}
(6.31) +2​hH3​(|A|4βˆ’H​tr⁑(A3))βˆ’2​n​(2βˆ’hH)​(Qβˆ’1n).\displaystyle+\frac{2h}{H^{3}}\bigl(|A|^{4}-H\operatorname{tr}(A^{3})\bigr)-2n\left(2-\frac{h}{H}\right)\left(Q-\frac{1}{n}\right).

Indeed, the KK-terms in the quotient evolution for K=1K=1 are

βˆ’2​n​|A|2H2+4βˆ’2​hHβˆ’2​n​|A|2​(Hβˆ’h)H3=2​(1βˆ’n​Q)​(2βˆ’hH).-\frac{2n|A|^{2}}{H^{2}}+4-\frac{2h}{H}-\frac{2n|A|^{2}(H-h)}{H^{3}}=2(1-nQ)\left(2-\frac{h}{H}\right).

Moreover, since Qβˆ’1n=|Å|2H2Q-\frac{1}{n}=\frac{|\mathring{A}|^{2}}{H^{2}}, if ΞΊiβ‰₯m>0\kappa_{i}\geq m>0, then

H​tr⁑(A3)βˆ’|A|4=βˆ‘i<jΞΊi​κj​(ΞΊiβˆ’ΞΊj)2β‰₯m2β€‹βˆ‘i<j(ΞΊiβˆ’ΞΊj)2=n​m2​|Å|2.H\operatorname{tr}(A^{3})-|A|^{4}=\sum_{i<j}\kappa_{i}\kappa_{j}(\kappa_{i}-\kappa_{j})^{2}\geq m^{2}\sum_{i<j}(\kappa_{i}-\kappa_{j})^{2}=n\,m^{2}|\mathring{A}|^{2}.

Consequently,

2​hH3​(|A|4βˆ’H​tr⁑(A3))β‰€βˆ’2​n​h​m2H​(Qβˆ’1n).\frac{2h}{H^{3}}\bigl(|A|^{4}-H\operatorname{tr}(A^{3})\bigr)\leq-\frac{2nhm^{2}}{H}\left(Q-\frac{1}{n}\right).

Let Tβˆ—>t0T^{*}>t_{0} be the supremum of the times for which

Ξ»04<ΞΊi<3​λ0,n​λ04<H,h<3​n​λ0,hH<74\frac{\lambda_{0}}{4}<\kappa_{i}<3\lambda_{0},\qquad\frac{n\lambda_{0}}{4}<H,h<3n\lambda_{0},\qquad\frac{h}{H}<\frac{7}{4}

holds on [t0,Tβˆ—)[t_{0},T^{*}). On this interval we may take m=Ξ»0/4m=\lambda_{0}/4, and the preceding estimates yield

(6.32) (βˆ‚tβˆ’Ξ”)Q≀2HβŸ¨βˆ‡H,βˆ‡QβŸ©βˆ’ΞΌ0(Qβˆ’1n)(\partial_{t}-\Delta)Q\leq\frac{2}{H}\langle\nabla H,\nabla Q\rangle-\mu_{0}\left(Q-\frac{1}{n}\right)

for a constant ΞΌ0=ΞΌ0​(n,R0)>0\mu_{0}=\mu_{0}(n,R_{0})>0. At a spatial maximum of QQ, the drift term vanishes. Hence the maximum principle gives

(6.33) maxMt⁑|Å|2H2≀eβˆ’ΞΌ0​(tβˆ’t0)​maxMt0​|Å|2H2for everyΒ t<Tβˆ—.\max_{M_{t}}\frac{|\mathring{A}|^{2}}{H^{2}}\leq e^{-\mu_{0}(t-t_{0})}\max_{M_{t_{0}}}\frac{|\mathring{A}|^{2}}{H^{2}}\qquad\text{for every \quad$t<T^{*}$.}

Since HH is uniformly bounded above and below on this interval, the latter implies

(6.34) β€–AΜŠβ€‹(β‹…,t)β€–Lβˆžβ‰€C​eβˆ’Ξ³β‘(tβˆ’t0)\|\mathring{A}(\cdot,t)\|_{L^{\infty}}\leq Ce^{-\gamma(t-t_{0})}

for some Ξ³>0\gamma>0. The uniform higher-order curvature estimates proved above, together with interpolation, give for every mβ‰₯0m\geq 0

(6.35) β€–βˆ‡mAΜŠβ€‹(β‹…,t)β€–Lβˆžβ‰€Cm​eβˆ’Ξ³m​(tβˆ’t0).\|\nabla^{m}\mathring{A}(\cdot,t)\|_{L^{\infty}}\leq C_{m}e^{-\gamma_{m}(t-t_{0})}.

This, by means of the Codazzi identity βˆ‡ih̊i​j=nβˆ’1nβ€‹βˆ‡jH,\nabla^{i}\mathring{h}_{ij}=\frac{n-1}{n}\nabla_{j}H, gives β€–βˆ‡H​(β‹…,t)β€–Lβˆžβ‰€C​eβˆ’Ξ³β‘(tβˆ’t0)\|\nabla H(\cdot,t)\|_{L^{\infty}}\leq Ce^{-\gamma(t-t_{0})}.

By Proposition 6.4 and Corollary 6.5, the radial graph functions satisfy

0<Οβˆ—β‰€Οβ‘(β‹…,t)β‰€Οβˆ—,|βˆ‡ΟƒΟβ€‹(β‹…,t)|Οƒ=sK​(ρ)β€‹βŸ¨Ξ½,βˆ‚rβŸ©βˆ’2βˆ’1≀C.0<\rho_{*}\leq\rho(\cdot,t)\leq\rho^{*},\qquad|\nabla^{\sigma}\rho(\cdot,t)|_{\sigma}=s_{K}(\rho)\sqrt{\left\langle\nu,\partial_{r}\right\rangle^{-2}-1}\leq C.

Since the induced metric is gt=dβ€‹ΟβŠ—d​ρ+sK​(ρ)2​σ,g_{t}=d\rho\otimes d\rho+s_{K}(\rho)^{2}\sigma, it follows that gt≀C​σg_{t}\leq C\sigma, and hence diam⁑(Mt,gt)≀C.\operatorname{diam}(M_{t},g_{t})\leq C. Consequently,

oscMt⁑H≀Cβ€‹β€–βˆ‡H​(β‹…,t)β€–Lβˆžβ‰€C​eβˆ’Ξ³β‘(tβˆ’t0).\operatorname{osc}_{M_{t}}H\leq C\|\nabla H(\cdot,t)\|_{L^{\infty}}\leq Ce^{-\gamma(t-t_{0})}.

Since Hmin≀h≀HmaxH_{\min}\leq h\leq H_{\max}, we obtain β€–Hβˆ’hβ€–Lβˆžβ€‹(Mt)≀C​eβˆ’Ξ³β‘(tβˆ’t0)\|H-h\|_{L^{\infty}(M_{t})}\leq Ce^{-\gamma(t-t_{0})}. Using (6.35), the evolution equations and parabolic interpolation once more, this improves to

(6.36) β€–Hβˆ’hβ€–Cm​(Mt)≀Cm​eβˆ’Ξ³m​(tβˆ’t0)\|H-h\|_{C^{m}(M_{t})}\leq C_{m}e^{-\gamma_{m}(t-t_{0})}

for every mβ‰₯0m\geq 0. Using the radial graph parametrization fixed above, by the flow equation (1.3), the latter implies

∫t0Tβˆ—β€–βˆ‚tX⁑(β‹…,t)β€–Cm​𝑑t≀Cm​‖AΜŠβ€‹(β‹…,t0)β€–Cm+1.\int_{t_{0}}^{T^{*}}\|\partial_{t}X(\cdot,t)\|_{C^{m}}\,dt\leq C_{m}\|\mathring{A}(\cdot,t_{0})\|_{C^{m+1}}.

Choose t0=tjt_{0}=t_{j} sufficiently large that Mt0M_{t_{0}} belongs to a smaller neighbourhood whose closure is contained in the bootstrap region defining Tβˆ—T^{*}. The estimates above, with their dependence on the initial pinching made explicit, give

β€–βˆ‚tX⁑(β‹…,t)β€–Cm≀Cmβ€‹Ξ΅βˆ—β€‹eβˆ’Ξ³m​(tβˆ’t0),\|\partial_{t}X(\cdot,t)\|_{C^{m}}\leq C_{m}\varepsilon_{*}e^{-\gamma_{m}(t-t_{0})},

where Ξ΅βˆ—=β€–AΜŠβ€‹(β‹…,t0)β€–Cm+1+β€–H⁑(β‹…,t0)βˆ’h⁑(t0)β€–Cmβ†’0\varepsilon_{*}=\|\mathring{A}(\cdot,t_{0})\|_{C^{m+1}}+\|H(\cdot,t_{0})-h(t_{0})\|_{C^{m}}\to 0 as t0=tjβ†’βˆžt_{0}=t_{j}\to\infty. Hence

β€–X⁑(β‹…,t)βˆ’X⁑(β‹…,t0)β€–Cm≀CmΞ³mβ€‹Ξ΅βˆ—for every ​t<Tβˆ—.\|X(\cdot,t)-X(\cdot,t_{0})\|_{C^{m}}\leq\frac{C_{m}}{\gamma_{m}}\varepsilon_{*}\qquad\text{for every }t<T^{*}.

Taking t0t_{0} sufficiently large, the solution remains at a uniform positive distance from the boundary of the bootstrap region. Here the bootstrap neighbourhood is understood in a fixed C2C^{2}-neighbourhood of SR01​(pβˆ—)S_{R_{0}}^{1}(p_{*}); membership in this neighbourhood controls ΞΊi\kappa_{i}, HH, hh, and h/Hh/H.

In particular, none of the inequalities defining Tβˆ—T^{*} can become an equality. If Tβˆ—<∞T^{*}<\infty, continuity would then allow the bootstrap conditions to be extended beyond Tβˆ—T^{*}, contradicting its definition. Therefore Tβˆ—=∞T^{*}=\infty. In particular, MtM_{t} remains strictly convex for every tβ‰₯t0t\geq t_{0}.

Equation (6.36) also shows that X⁑(β‹…,t)X(\cdot,t) is Cauchy in every CmC^{m}-norm. Thus it converges exponentially to a smooth limiting embedding X∞X_{\infty}. By (6.34), the limiting hypersurface satisfies Å∞=0\mathring{A}_{\infty}=0. Hence it is totally umbilical. Since it is closed, embedded and contained in an open hemisphere, it is a geodesic sphere M∞=βˆ‚BR∞1​(p∞)M_{\infty}=\partial B_{R_{\infty}}^{1}(p_{\infty}). The enclosed volume is preserved, so vol⁑(BR∞1​(p∞))=vol⁑(BR01​(o))\operatorname{vol}\bigl(B_{R_{\infty}}^{1}(p_{\infty})\bigr)=\operatorname{vol}\bigl(B_{R_{0}}^{1}(o)\bigr), and therefore R∞=R0R_{\infty}=R_{0}. This concludes the proof when nβ‰₯2n\geq 2.

Let us now consider the case of curves. As before, by Proposition 6.10 we have the smooth subsequential convergence

Mtj⟢Sβˆ—:=βˆ‚BR01​(pβˆ—).M_{t_{j}}\longrightarrow S_{*}:=\partial B_{R_{0}}^{1}(p_{*}).

We first show that the whole flow converges smoothly to Sβˆ—S_{*}. Taking pβˆ—p_{*} as the reference point, let Ξ΅j\varepsilon_{j} and ΞΈj\theta_{j} denote the annular and radial-tilt parameters of MtjM_{t_{j}}. The smooth convergence above gives Ξ΅j+ΞΈj⟢0\varepsilon_{j}+\theta_{j}\longrightarrow 0. As, by Proposition 6.2, every fixed c>0c>0 is a common reflection threshold for MtjM_{t_{j}} when jj is sufficiently large, we may choose common reflection thresholds cjβ†’0c_{j}\to 0.

By Proposition 6.4, the reflection threshold cjc_{j} is preserved for every tβ‰₯tjt\geq t_{j}. The quantitative converse in Corollary 6.6, applied uniformly on the whole time interval [tj,∞)[t_{j},\infty), therefore gives

suptβ‰₯tj‖ρpβˆ—β€‹(β‹…,t)βˆ’R0β€–C1⟢0,\sup_{t\geq t_{j}}\bigl\|\rho_{p_{*}}(\cdot,t)-R_{0}\bigr\|_{C^{1}}\longrightarrow 0,

where ρpβˆ—β€‹(β‹…,t)\rho_{p_{*}}(\cdot,t) denotes the radial graph function of MtM_{t} with respect to pβˆ—p_{*}. Since the estimate holds on the entire tail [tj,∞)[t_{j},\infty), it yields

ρpβˆ—β€‹(β‹…,t)⟢R0in ​C1​ as ​tβ†’βˆž,\rho_{p_{*}}(\cdot,t)\longrightarrow R_{0}\qquad\text{in }C^{1}\text{ as }t\to\infty,

without passing to a subsequence. The uniform higher-order estimates and interpolation then upgrade this convergence to every CmC^{m} norm. Hence Mtβ†’Sβˆ—M_{t}\to S_{*} smoothly as tβ†’βˆžt\to\infty.

It remains to prove the exponential rate. By the definition of hh,

(6.37) ∫Mtw​𝑑s=0forw:=ΞΊβˆ’h.\int_{M_{t}}w\,ds=0\qquad\text{for}\quad w:=\kappa-h.

Moreover, if YY is an ambient Killing field on π•Š2\mathbb{S}^{2}, the one-parameter group of isometries generated by YY preserves both length and enclosed area. The corresponding first-variation formulas give

(6.38) ∫Mtw⁑⟨Y,Ξ½βŸ©β€‹π‘‘s=0.\int_{M_{t}}w\langle Y,\nu\rangle\,ds=0.

On the other hand, the normal component of every Killing field YY satisfies

βˆ’βˆ‚s2⟨Y,ν⟩=(ΞΊSβˆ—2+Secπ•Š2)⟨Y,ν⟩=(cot2R0+1)⟨Y,ν⟩=1sin2⁑R0⟨Y,ν⟩;-\partial_{s}^{2}\langle Y,\nu\rangle=\bigl(\kappa^{2}_{S_{\ast}}+\operatorname{Sec}_{\mathbb{S}^{2}}\bigr)\langle Y,\nu\rangle=(\cot^{2}R_{0}+1)\langle Y,\nu\rangle=\frac{1}{\sin^{2}R_{0}}\langle Y,\nu\rangle;

see, for instance, [19, Proposition 1]. The normal components of the Killing fields obtained by moving the centre of Sβˆ—S_{*} in two independent directions are, up to a choice of origin and normalization, the sine and cosine functions on Sβˆ—S_{*}. Hence, on MtM_{t}, by (6.37) and (6.38), ww is orthogonal to the constants and to a two-dimensional space converging smoothly to this first eigenspace. Since Sβˆ—S_{*} is intrinsically a circle of radius sin⁑R0\sin R_{0}, the next eigenvalue of βˆ’βˆ‚s2-\partial_{s}^{2} is 4​sinβˆ’2⁑R04\sin^{-2}R_{0}; see [6, Chapter II.4]. The Rayleigh characterization (cf. [10, Chapter I.5]) and the smooth convergence Mtβ†’Sβˆ—M_{t}\to S_{*} therefore imply that, for every Ξ΅>0\varepsilon>0 and all sufficiently large tt,

∫Mt|βˆ‚sw|2​𝑑sβ‰₯(4​a0βˆ’Ξ΅)β€‹βˆ«Mtw2​𝑑s,witha0:=1sin2⁑R0.\int_{M_{t}}|\partial_{s}w|^{2}\,ds\geq\left(4a_{0}-\varepsilon\right)\int_{M_{t}}w^{2}\,ds,\qquad\text{with}\quad a_{0}:=\frac{1}{\sin^{2}R_{0}}.

Now set E⁑(t):=∫Mtw2​𝑑sE(t):=\int_{M_{t}}w^{2}\,ds. The evolution equations βˆ‚tΞΊ=βˆ‚s2ΞΊ+(ΞΊβˆ’h)​(ΞΊ2+1)\partial_{t}\kappa=\partial_{s}^{2}\kappa+(\kappa-h)(\kappa^{2}+1) and βˆ‚td​s=βˆ’ΞΊβ‘(ΞΊβˆ’h)​d​s\partial_{t}ds=-\kappa(\kappa-h)\,ds yield

Eβ€²(t)=βˆ’2∫Mt|βˆ‚sw|2ds+2∫Mt(ΞΊ2+1)w2dsβˆ’βˆ«MtΞΊw3ds,E^{\prime}(t)=-2\int_{M_{t}}|\partial_{s}w|^{2}\,ds+2\int_{M_{t}}(\kappa^{2}+1)w^{2}\,ds-\int_{M_{t}}\kappa w^{3}\,ds,

where the term containing h′​(t)h^{\prime}(t) vanishes because of (6.37).

Since Mtβ†’Sβˆ—M_{t}\to S_{*} smoothly, for every Ξ΅>0\varepsilon>0 and all sufficiently large tt, one can guarantee

|ΞΊ2+1βˆ’a0|≀Ρ,β€–wβ€–Lβˆžβ€‹(Mt)≀Ρ,β€–ΞΊβ€–Lβˆžβ€‹(Mt)≀C0,|\kappa^{2}+1-a_{0}|\leq\varepsilon,\qquad\|w\|_{L^{\infty}(M_{t})}\leq\varepsilon,\qquad\|\kappa\|_{L^{\infty}(M_{t})}\leq C_{0},

where C0C_{0} is independent of tt. Applying the preceding estimates, we obtain

E′​(t)β‰€βˆ’2​(4​a0βˆ’Ξ΅)​E​(t)+2​(a0+Ξ΅)​E​(t)+C0​Ρ​E​(t)β‰€βˆ’3​a0​E​(t),E^{\prime}(t)\leq-2(4a_{0}-\varepsilon)E(t)+2(a_{0}+\varepsilon)E(t)+C_{0}\varepsilon E(t)\leq-3a_{0}E(t),

after choosing Ξ΅>0\varepsilon>0 so that (4+C0)​Ρ≀3​a0.(4+C_{0})\varepsilon\leq 3a_{0}. Therefore, for all sufficiently large tt,

E⁑(t)≀C​eβˆ’3​a0​t.E(t)\leq Ce^{-3a_{0}t}.

The uniform higher-order curvature estimates and interpolation now give, for every integer mβ‰₯0m\geq 0, constants Cm,Ξ³m>0C_{m},\gamma_{m}>0 such that

‖κ⁑(β‹…,t)βˆ’h⁑(t)β€–Cm​(Mt)≀Cm​eβˆ’Ξ³m​t.\|\kappa(\cdot,t)-h(t)\|_{C^{m}(M_{t})}\leq C_{m}e^{-\gamma_{m}t}.

Finally, in radial coordinates with respect to pβˆ—p_{*}, βˆ‚tρpβˆ—=hβˆ’ΞΊβŸ¨Ξ½,βˆ‚r⟩.\partial_{t}\rho_{p_{*}}=\frac{h-\kappa}{\langle\nu,\partial_{r}\rangle}. The denominator is uniformly bounded away from zero, and its derivatives are uniformly controlled. Since ρpβˆ—β€‹(β‹…,t)β†’R0\rho_{p_{*}}(\cdot,t)\to R_{0} smoothly, integration from tt to infinity gives

‖ρpβˆ—β€‹(β‹…,t)βˆ’R0β€–Cm≀Cm​eβˆ’Ξ³m​t.\|\rho_{p_{*}}(\cdot,t)-R_{0}\|_{C^{m}}\leq C_{m}e^{-\gamma_{m}t}.

Thus MtM_{t} converges exponentially in the smooth topology to Sβˆ—S_{*}. ∎

Corollary 6.12 (Location of the limiting centre).

Let c0c_{0} be as in Proposition 6.2. Then

distNK⁑(o,p∞)≀c0.\dist_{N_{K}}(o,p_{\infty})\leq c_{0}.

In particular, distNK⁑(o,p∞)β†’0\dist_{N_{K}}(o,p_{\infty})\to 0 as Ξ΅0+ΞΈ0β†’0\varepsilon_{0}+\theta_{0}\to 0.

Proof.

As in the Euclidean case, the preserved reflection property passes to the smooth limit. Hence the limiting ball BR0K​(p∞)B_{R_{0}}^{K}(p_{\infty}) reflects inside itself across every Pv,sP_{v,s} with vβˆˆπ•Šonv\in\mathbb{S}_{o}^{n} and sβ‰₯c0s\geq c_{0}. This easily implies that the centre of the ball has distance at most c0c_{0} from oo. Since Proposition 6.2 implies the reflection property for every prescribed c0>0c_{0}>0, provided that Ξ΅0\varepsilon_{0} and ΞΈ0\theta_{0} are sufficiently small, the last assertion follows. ∎

7. Extension to Lipschitz initial data

The annular-closeness and normal-oscillation assumptions make sense for radial graphs of merely Lipschitz regularity. We prove that sufficiently small such data admit an instantaneously smooth volume preserving mean curvature flow. The construction is geometric: smooth approximations inherit a common reflection threshold, and the weighted curvature estimate gives bounds independent of their initial curvature.

In the following statement, we define sK​(β‹…)s_{K}(\cdot) as in (6.2) when K=Β±1K=\pm 1, and sK​(ρ)=ρs_{K}(\rho)=\rho for K=0K=0.

Theorem 7.1 (Lipschitz stability in space forms).

Let K∈{βˆ’1,0,1}K\in\{-1,0,1\}, and let

M0={expo⁑(ρ0​(Ο‘)​ϑ):Ο‘βˆˆπ•Šon}βŠ‚NKn+1,withρ0∈W1,βˆžβ€‹(π•Šon).M_{0}=\left\{\exp_{o}\bigl(\rho_{0}(\vartheta)\vartheta\bigr):\vartheta\in\mathbb{S}_{o}^{n}\right\}\subset N_{K}^{n+1},\qquad\text{with}\qquad\rho_{0}\in W^{1,\infty}(\mathbb{S}_{o}^{n}).

Assume that

(7.1) R0​(1βˆ’Ξ΅0)≀ρ0≀R0​(1+Ξ΅0)and|βˆ‡ΟƒΟ0|ΟƒsK​(ρ0)≀tan⁑θ0a.e. onΒ β€‹π•Šon.R_{0}(1-\varepsilon_{0})\leq\rho_{0}\leq R_{0}(1+\varepsilon_{0})\qquad\text{and}\qquad\frac{|\nabla^{\sigma}\rho_{0}|_{\sigma}}{s_{K}(\rho_{0})}\leq\tan\theta_{0}\qquad\text{a.e. on }\mathbb{S}_{o}^{n}.

When K=1K=1, require in addition that R0​(1+Ξ΅0)<Ο€2.R_{0}(1+\varepsilon_{0})<\frac{\pi}{2}. If Ξ΅0\varepsilon_{0} and ΞΈ0\theta_{0} are sufficiently small, then

  1. (a)

    There exists a family of radial graphs Mt={expo⁑(ρ⁑(Ο‘,t)​ϑ):Ο‘βˆˆπ•Šon},t>0,M_{t}=\left\{\exp_{o}\bigl(\rho(\vartheta,t)\vartheta\bigr):\vartheta\in\mathbb{S}_{o}^{n}\right\},\,t>0, which solves (1.3) classically for every t>0t>0 and is smooth for every positive time. If Ξ©t\Omega_{t} denotes the region enclosed by MtM_{t}, then vol⁑(Ξ©t)=vol⁑(Ξ©0)​for every ​t>0.\operatorname{vol}(\Omega_{t})=\operatorname{vol}(\Omega_{0})\,\text{for every }t>0. Moreover, for all sufficiently small t>0t>0,

    ‖ρ⁑(β‹…,t)βˆ’Ο0β€–Lβˆžβ€‹(π•Šon)≀C​t.\|\rho(\cdot,t)-\rho_{0}\|_{L^{\infty}(\mathbb{S}_{o}^{n})}\leq C\sqrt{t}.

    In particular, ρ⁑(β‹…,t)→ρ0\rho(\cdot,t)\rightarrow\rho_{0} uniformly as tβ†˜0t\searrow 0, and MtM_{t} converges to M0M_{0} in the Hausdorff sense.

  2. (b)

    For every T>0T>0 and every integer mβ‰₯0m\geq 0, there exists Cm,T<∞C_{m,T}<\infty such that

    sup0<t≀Tt(m+1)/2β€‹β€–βˆ‡mA​(β‹…,t)β€–Lβˆžβ€‹(Mt)≀Cm,T.\sup_{0<t\leq T}t^{(m+1)/2}\|\nabla^{m}A(\cdot,t)\|_{L^{\infty}(M_{t})}\leq C_{m,T}.
  3. (c)

    The solution exists for all times and satisfies the same conclusions as in Theorems 1.1 and 1.2 as tβ†’βˆžt\to\infty. In particular, it converges to a geodesic sphere, exponentially in the C∞C^{\infty} topology.

By Rademacher’s theorem, the gradient in (7.1) can be equivalently interpreted as the classical gradient at points of differentiability, or in the weak sense. By (6.3), we see that the requirement on βˆ‡ΟƒΟ0\nabla^{\sigma}\rho_{0} in (7.1) is equivalent to the condition ⟨ν0,βˆ‚r⟩β‰₯cosΞΈ\langle\nu_{0},\partial_{r}\rangle\geq\cos\theta in (1.2) and (1.6). Observe that one could give an equivalent formulation in terms of the smallness of the Lipschitz constant of ρ⁑(β‹…)\rho(\cdot) (depending on R0R_{0}).

Proof.

The construction proceeds by smooth approximation. We give the complete argument in Euclidean space, and in the end indicate the modifications required when K=Β±1K=\pm 1.

In order to approximate smoothly our initial datum ρ0∈W1,βˆžβ€‹(π•Šn)\rho_{0}\in W^{1,\infty}(\mathbb{S}^{n}) in a way which preserves the bounds in (7.1), it is convenient to work first with the function

(7.2) w0=log⁑ρ0R0,w_{0}=\log\frac{\rho_{0}}{R_{0}},

which satisfies

log⁑(1βˆ’Ξ΅0)≀w0≀log⁑(1+Ξ΅0)andΒ |βˆ‡Οƒw0|σ≀tan⁑θ0a.e.\log(1-\varepsilon_{0})\leq w_{0}\leq\log(1+\varepsilon_{0})\qquad\text{and }\qquad|\nabla^{\sigma}w_{0}|_{\sigma}\leq\tan\theta_{0}\qquad\text{a.e.}

Let Pt=et​ΔσP_{t}=e^{t\Delta_{\sigma}} denote the heat semigroup on π•Šn\mathbb{S}^{n}, and choose any sequence tjβ†˜0t_{j}\searrow 0. Set

w~0(j)=Ptj​w0.\widetilde{w}_{0}^{(j)}=P_{t_{j}}w_{0}.

Then the functions w~0(j)\widetilde{w}_{0}^{(j)} are in Cβˆžβ€‹(π•Šn)C^{\infty}(\mathbb{S}^{n}), satisfy log⁑(1βˆ’Ξ΅0)≀w~0(j)≀log⁑(1+Ξ΅0)\log(1-\varepsilon_{0})\leq\widetilde{w}_{0}^{(j)}\leq\log(1+\varepsilon_{0}), and converge to w0w_{0} uniformly on π•Šn,\mathbb{S}^{n}, since w0w_{0} is Lipschitz. Moreover, as RicΟƒ=(nβˆ’1)​σ\operatorname{Ric}_{\sigma}=(n-1)\sigma, well known properties of the heat kernel (cf. [32, Theorem 1.3 and Corollary 1.4]) imply that

β€–βˆ‡Οƒw~0(j)β€–Lβˆžβ‰€eβˆ’(nβˆ’1)​tjβ€‹β€–βˆ‡Οƒw0β€–Lβˆžβ‰€tan⁑θ0.\|\nabla^{\sigma}\widetilde{w}_{0}^{(j)}\|_{L^{\infty}}\leq e^{-(n-1)t_{j}}\|\nabla^{\sigma}w_{0}\|_{L^{\infty}}\leq\tan\theta_{0}.

We then define the functions ρ~0(j)=R0​ew~0(j),\widetilde{\rho}_{0}^{(j)}=R_{0}e^{\widetilde{w}_{0}^{(j)}}, which are smooth approximants of ρ0\rho_{0}. We multiply them by a factor aj>0a_{j}>0, chosen so that ρ0(j):=aj​ρ~0(j)\rho_{0}^{(j)}:=a_{j}\widetilde{\rho}_{0}^{(j)} encloses the same volume as M0M_{0}. Then it is easy to check that ajβ†’1a_{j}\to 1, and that the functions ρ0(j)\rho_{0}^{(j)} converge uniformly to ρ0\rho_{0}. In addition, they satisfy

(7.3) R0​(1βˆ’Ξ΅0βˆ’Ξ΄j)≀ρ0(j)≀R0​(1+Ξ΅0+Ξ΄j)R_{0}(1-\varepsilon_{0}-\delta_{j})\leq\rho_{0}^{(j)}\leq R_{0}(1+\varepsilon_{0}+\delta_{j})

for suitable numbers Ξ΄jβ†˜0\delta_{j}\searrow 0 and, for every sufficiently large jj,

(7.4) |βˆ‡Οƒβ€‹log​ρ0(j)|σ≀tan⁑θ0.\big|\nabla^{\sigma}\log\rho_{0}^{(j)}\big|_{\sigma}\leq\tan\theta_{0}.

For each jβ‰₯1j\geq 1, we now solve the flow (1.3) with the smooth initial data M0(j)M_{0}^{(j)} and denote by Mt(j),M_{t}^{(j)}, the corresponding smooth solutions of (1.3). Using properties (7.3) and (7.4), we can apply our previous results to obtain uniform C1C^{1}-bounds on the solutions.

In fact, let c0c_{0} be the reflection threshold fixed in Remark 3.8. As inequality (3.1) is strict, from Proposition 3.1 we obtain that c0c_{0} is a common reflection threshold for M0(j)M_{0}^{(j)} for every sufficiently large jj. Then we can apply the subsequent results of Section 3, to show that the reflection property is preserved along the flow, and the solutions satisfy, for every jj and tt,

(7.5) R0βˆ’2​c0≀|x(j)|≀R0+2​c0,R_{0}-2c_{0}\leq|x^{(j)}|\leq R_{0}+2c_{0},
(7.6) q(j):=⟨ν(j),x(j)|x(j)|⟩β‰₯qβˆ—β€‹(c0):=(1βˆ’c02(R0βˆ’2​c0)2)1/2>0.q^{(j)}:=\left\langle\nu^{(j)},\frac{x^{(j)}}{|x^{(j)}|}\right\rangle\geq q_{*}(c_{0}):=\left(1-\frac{c_{0}^{2}}{(R_{0}-2c_{0})^{2}}\right)^{1/2}>0.

By the results of Sections 4 and 5, we obtain that each Mt(j)M_{t}^{(j)} exists globally and converges to a sphere. We want to show that these solutions converge, as jβ†’βˆžj\to\infty, to a limit flow MtM_{t} which satisfies the conclusions of our theorem. To this purpose, the crucial step is to obtain uniform curvature bounds on Mt(j)M_{t}^{(j)}.

To estimate the curvature, we will adapt the strategy of Section 4 in a way that the bounds are independent of the curvature of the initial data. This time we no longer prove a separate bound on HH as in Proposition 4.3; instead, we proceed directly to estimating |A|2|A|^{2} by a suitable adaptation of the technique of Proposition 4.4.

We first observe that, by the choice of c0c_{0} in Remark 3.8, the constant in (7.6) satisfies qβˆ—β€‹(c0)β†’1q_{*}(c_{0})\to 1 as c0/R0β†’0c_{0}/R_{0}\to 0. We may therefore fix kk and choose the initial geometric parameters sufficiently small that

(7.7) n1+n<k<qβˆ—β€‹(c0)2.\frac{\sqrt{n}}{1+\sqrt{n}}<k<q_{*}(c_{0})^{2}.

Set v=(q(j))βˆ’1v=(q^{(j)})^{-1} and define β„±\mathscr{F} as in (4.13).

By (7.6), it holds 1≀v≀qβˆ—β€‹(c0)βˆ’11\leq v\leq q_{*}(c_{0})^{-1} and hence k​v2<1kv^{2}<1. Thus β„±\mathscr{F} and |A|2|A|^{2} are uniformly equivalent; in particular, β„±β‰₯φ⁑(1)​|A|2\mathscr{F}\geq\varphi(1)|A|^{2}.

Now let 𝒒j​(t):=maxMt(j)⁑F\mathscr{G}_{j}(t):=\max_{M_{t}^{(j)}}F, and compute hereafter at a point where the maximum is attained. Arguing as in the proof of Proposition 4.4, but without using any bound for |h||h| and |H||H|, we obtain

(7.8) D+​𝒒jβ‰€βˆ’2​k​𝒒j2+C⁑(1+|h|+|H|)​𝒒jβˆ’2​h​tr⁑(A3)​φ​(v2),\displaystyle D^{+}\mathscr{G}_{j}\leq-2k\mathscr{G}_{j}^{2}+C(1+|h|+|H|)\mathscr{G}_{j}-2h\operatorname{tr}(A^{3})\varphi(v^{2}),

in the upper Dini-derivative sense. Here CC depends only on nn, R0R_{0}, and the uniform first-order bounds in (7.5) and (7.6). In particular, CC is independent of jj and of the curvature of M0(j)M_{0}^{(j)}.

For every t∈(0,Tj)t\in(0,T_{j}),

(7.9) |h⁑(t)|\displaystyle|h(t)| ≀‖H⁑(β‹…,t)β€–Lβˆžβ€‹(Mt(j))≀n​‖A⁑(β‹…,t)β€–Lβˆžβ€‹(Mt(j))≀n⁑(1βˆ’k)​𝒒j​(t)1/2.\displaystyle\leq\|H(\cdot,t)\|_{L^{\infty}(M_{t}^{(j)})}\leq\sqrt{n}\,\|A(\cdot,t)\|_{L^{\infty}(M_{t}^{(j)})}\leq\sqrt{n(1-k)}\,\mathscr{G}_{j}(t)^{1/2}.

Then the last term in (7.8), which has an indefinite sign, can be estimated as follows:

(7.10) 2​|h|​|tr⁑(A3)|​φ​(v2)\displaystyle 2|h|\,|\operatorname{tr}(A^{3})|\varphi(v^{2}) ≀2​n⁑(1βˆ’k)​𝒒j1/2​𝒒j3/2φ⁑(1)=2​n​(1βˆ’k)​𝒒j2.\displaystyle\leq 2\sqrt{n(1-k)}\,\mathscr{G}_{j}^{1/2}\frac{\mathscr{G}_{j}^{3/2}}{\sqrt{\varphi(1)}}=2\sqrt{n}(1-k)\mathcal{G}_{j}^{2}.

Combining the above estimates, we reach

(7.11) D+​𝒒j≀\displaystyle D^{+}\mathscr{G}_{j}\leq{} βˆ’2​(kβˆ’n​(1βˆ’k))​𝒒j2+C​𝒒j​(1+C​𝒒j1/2).\displaystyle-2\bigl(k-\sqrt{n}(1-k)\bigr)\mathscr{G}_{j}^{2}+C\mathscr{G}_{j}(1+C\mathscr{G}_{j}^{1/2}).

By (7.7), we can choose 0<Ξ·<kβˆ’n​(1βˆ’k)0<\eta<k-\sqrt{n}(1-k) so that Young’s inequality gives C​𝒒j3/2≀2​η​𝒒j2+CΞ·.C\mathscr{G}_{j}^{3/2}\leq 2\eta\mathscr{G}_{j}^{2}+C_{\eta}. Consequently, there exist constants ΞΌ>0\mu>0 and C<∞C<\infty, independent of jj, such that

(7.12) D+​𝒒jβ‰€βˆ’ΞΌβ€‹π’’j2+C⁑(𝒒j+1).D^{+}\mathscr{G}_{j}\leq-\mu\mathscr{G}_{j}^{2}+C(\mathscr{G}_{j}+1).

Choose Mβˆ—>0M_{*}>0, independently of jj, such that C⁑(s+1)≀μ2​s2C(s+1)\leq\frac{\mu}{2}s^{2} for every sβ‰₯Mβˆ—s\geq M_{*}. Then we get D+​𝒒jβ‰€βˆ’ΞΌ2​𝒒j2D^{+}\mathscr{G}_{j}\leq-\frac{\mu}{2}\mathscr{G}_{j}^{2} whenever 𝒒jβ‰₯Mβˆ—.\mathscr{G}_{j}\geq M_{*}. A comparison argument gives 𝒒j​(t)≀max⁑{Mβˆ—,2μ​t}\mathscr{G}_{j}(t)\leq\max\left\{M_{*},\frac{2}{\mu t}\right\} for 0<t<Tj0<t<T_{j}. Consequently, we conclude that

(7.13) supMt(j)|A|2≀C⁑(1+1t),t>0\sup_{M_{t}^{(j)}}|A|^{2}\leq C\left(1+\frac{1}{t}\right),\qquad t>0

In particular,

(7.14) β€–H⁑(β‹…,t)β€–Lβˆžβ€‹(Mt(j))+|h⁑(t)|≀C⁑(1+1t),t>0.\|H(\cdot,t)\|_{L^{\infty}(M_{t}^{(j)})}+|h(t)|\leq C\left(1+\frac{1}{\sqrt{t}}\right),\qquad t>0.

The evolution equations for the covariant derivatives of AA, together with the standard interior Bernstein estimates on backward time intervals of length comparable to min⁑{t,1}\min\{t,1\}, then give

(7.15) supMt(j)β€–βˆ‡mA​(β‹…,t)β€–2≀C⁑(1+1tm+1),t>0.\sup_{M_{t}^{(j)}}\|\nabla^{m}A(\cdot,t)\|^{2}\leq C\left(1+\frac{1}{t^{m+1}}\right),\qquad t>0.

All constants are independent of the approximating sequence and of the initial curvature. Therefore the estimates give smooth compactness away from t=0t=0 and allow to pass to the limit in the smooth approximating flows.

Fix 0<Ο„<T<∞0<\tau<T<\infty. The above estimates give uniform C∞C^{\infty}-bounds for the radial functions ρ(j)\rho^{(j)} on π•ŠnΓ—[Ο„,T].\mathbb{S}^{n}\times[\tau,T]. Arzelà–Ascoli’s theorem and a diagonal argument therefore yield a subsequence which converges smoothly on every compact subset of π•ŠnΓ—(0,∞)\mathbb{S}^{n}\times(0,\infty) to a smooth positive function

ρ∈Cβˆžβ€‹(π•ŠnΓ—(0,∞)).\rho\in C^{\infty}\bigl(\mathbb{S}^{n}\times(0,\infty)\bigr).

Passing to the limit in the radial equation shows that the associated hypersurfaces MtM_{t} solve (1.3) classically for every t>0t>0.

It remains to identify the initial trace. For the radial parametrization, βˆ‚tx(j)=βˆ‚tρ(j)βˆ‚r.\partial_{t}x^{(j)}=\partial_{t}\rho^{(j)}\,\partial_{r}. Taking the scalar product with Ξ½(j)\nu^{(j)} and using (1.3), we obtain

βˆ‚tρ(j)=h(j)βˆ’H(j)⟨ν(j),βˆ‚r⟩.\partial_{t}\rho^{(j)}=\frac{h^{(j)}-H^{(j)}}{\langle\nu^{(j)},\partial_{r}\rangle}.

Estimates (7.6) and (7.14) give

|βˆ‚tρ(j)|≀C(1+tβˆ’1/2)≀Ctβˆ’1/2,0<t≀1.|\partial_{t}\rho^{(j)}|\leq C\left(1+t^{-1/2}\right)\leq Ct^{-1/2},\qquad 0<t\leq 1.

Since the right-hand side is integrable at t=0t=0, integration in time yields

(7.16) ‖ρ(j)​(β‹…,t)βˆ’Ο0(j)β€–Lβˆžβ‰€C​t,\left\|\rho^{(j)}(\cdot,t)-\rho_{0}^{(j)}\right\|_{L^{\infty}}\leq C\sqrt{t},

where CC is independent of jj. We know that ρ0(j)⟢ρ0​uniformly onΒ β€‹π•Šn,\rho_{0}^{(j)}\longrightarrow\rho_{0}\,\text{uniformly on }\mathbb{S}^{n}, therefore we can pass to the limit in (7.16) and obtain

‖ρ⁑(β‹…,t)βˆ’Ο0β€–Lβˆžβ‰€C​t,\|\rho(\cdot,t)-\rho_{0}\|_{L^{\infty}}\leq C\sqrt{t},

which proves ((a)). Since MtM_{t} and M0M_{0} are radial graphs over the same sphere, the uniform convergence of their radial functions also implies that Mtβ†’M0M_{t}\to M_{0} in the Hausdorff sense as tβ†˜0t\searrow 0.

Each approximating flow is volume-preserving, and starts from initial which, by construction, enclose the same volume as M0M_{0}. Therefore vol⁑(Ωt(j))=vol⁑(Ω0).\operatorname{vol}(\Omega_{t}^{(j)})=\operatorname{vol}(\Omega_{0}). For every fixed t>0t>0, smooth convergence of the radial functions implies convergence of the enclosed volumes. Hence vol⁑(Ωt)=vol⁑(Ω0).\operatorname{vol}(\Omega_{t})=\operatorname{vol}(\Omega_{0}). In addition, estimates (7.15) pass to the smooth limit on every compact positive-time interval and yield conclusion (b) of Theorem 7.1.

The flow MtM_{t} we have constructed starts with Lipschitz data and becomes instantaneously smooth. For any t0>0t_{0}>0 the hypersurface Mt0M_{t_{0}} satisfies the hypotheses of the convergence result Theorem 1.1 for smooth initial data, provided the original geometric parameters are chosen sufficiently small. We conclude that the limiting flow becomes strictly convex for all sufficiently large times and converges exponentially in the smooth topology to a round sphere enclosing the same volume as M0M_{0}.

The construction gives existence through a subsequential limit of smooth approximations. As in [17], no uniqueness assertion is made here for the Lipschitz initial-value problem; in particular, the limiting evolution may a priori depend on the chosen approximating sequence.

We conclude by indicating the modifications required for K∈{βˆ’1,1}K\in\{-1,1\}. The proof follows the Euclidean construction and we only record the points at which the ambient geometry changes the argument.

For the approximation, instead of the Euclidean function in (7.2), we use the conformal radial variable

(7.17) w0=Ξ¨K​(ρ0)βˆ’Ξ¨K​(R0),Ξ¨K′​(r)=1sK​(r),w_{0}=\Psi_{K}(\rho_{0})-\Psi_{K}(R_{0}),\qquad\Psi_{K}^{\prime}(r)=\frac{1}{s_{K}(r)},

for which the condition on the normal in (7.1) again becomes |βˆ‡Οƒw0|σ≀tan⁑θ0a.e.|\nabla^{\sigma}w_{0}|_{\sigma}\leq\tan\theta_{0}\qquad\text{a.e.}

The heat-semigroup approximation therefore preserves the same conformal-gradient bound. The enclosed volume is normalized by adding a spatially constant number bjb_{j} to the approximating conformal radial function. Indeed, since Ξ¨Kβ€²>0\Psi_{K}^{\prime}>0, the radial function

ρb=Ξ¨Kβˆ’1​(Ξ¨K​(R0)+w~0(j)+b)\rho_{b}=\Psi_{K}^{-1}\bigl(\Psi_{K}(R_{0})+\widetilde{w}_{0}^{(j)}+b\bigr)

is pointwise strictly increasing in bb, and hence so is its enclosed volume. There is consequently a unique bjb_{j} for which the corresponding hypersurface encloses the same volume as M0M_{0}. Uniform convergence implies bj→0b_{j}\to 0, while

βˆ‡Οƒ(w~0(j)+bj)=βˆ‡Οƒw~0(j),\nabla^{\sigma}\bigl(\widetilde{w}_{0}^{(j)}+b_{j}\bigr)=\nabla^{\sigma}\widetilde{w}_{0}^{(j)},

so the volume normalization does not affect the cone condition.

After discarding finitely many terms, Proposition 6.2 applies to all the approximations with a common reflection threshold. The preservation of reflection, Proposition 6.4, and Corollary 6.5 then give constants 0<rβˆ—β‰€rβˆ—,qβˆ—>0,0<r_{*}\leq r^{*},\,q_{*}>0, independent of the approximation, such that

(7.18) rβˆ—β‰€Ο(j)≀rβˆ—,⟨ν(j),βˆ‚r⟩β‰₯qβˆ—.r_{*}\leq\rho^{(j)}\leq r^{*},\qquad\left\langle\nu^{(j)},\partial_{r}\right\rangle\geq q_{*}.

In the spherical case, the parameters are chosen so that rβˆ—<Ο€2.r^{*}<\frac{\pi}{2}. Thus all functions of the radial variable occurring in the evolution equations, including sK​(ρ)s_{K}(\rho), cK​(ρ)c_{K}(\rho), and the required reciprocals, are uniformly bounded on the range of the approximating flows.

We can next estimate |A|2|A|^{2} by the same maximum principle of the Euclidean case, since the terms involving the ambient curvature are of lower order. The estimates on HH and on the derivatives of AA follow similarly. This allows us to apply the same compactness argument as in the Euclidean case, and to obtain a limiting smooth flow with all the desired properties. This completes the proof of the convergence result for Lipschitz initial data. ∎

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