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Mean curvature flow with multiplicity 22 convergence in closed manifolds

Jingwen Chen, Ao Sun Department of Mathematics, University of Pennsylvania, David Rittenhouse Lab, 209 South 33rd Street, Philadelphia, PA 19104 jingwch@sas.upenn.edu Department of Mathematics, Lehigh University, Chandler-Ullmann Hall, Bethlehem, PA 18015 aos223@lehigh.edu
Abstract.

We construct new examples of immortal mean curvature flow of smooth embedded connected hypersurfaces in closed manifolds, which converge to minimal hypersurfaces with multiplicity 22 as time approaches infinity.

1. Introduction

The mean curvature flow is the gradient flow of the area functional. This feature makes it one of the most natural extrinsic geometric flows. Mean curvature flow is widely used to study geometry and topology, and we refer the readers to some of the applications in [Gra89, Wan02, HK19, BHH21, BHH19, GLP21]. A central topic in the study of mean curvature flow is to understand the singular behavior and long-time behavior, and it is particularly important to the potential applications.

Among the possible exotic phenomena that may show up, higher multiplicity convergence is one of the most significant phenomena and has attracted much attention. Roughly speaking, higher multiplicity convergence means that the hypersurfaces can be decomposed into several connected components outside a small set, and each one of the connected components converges to the limit hypersurface smoothly. Recently, the Multiplicity One Conjecture proposed by Ilmanen was resolved by Bamler-Kleiner [BK23], showing that higher multiplicity can not show up as the blow-up of a singularity of a mean curvature flow of closed embedded surfaces in 3\mathbb{R}^{3}. In contrast, the authors [CS23] constructed an immortal mean curvature flow in 3\mathbb{R}^{3}, showing that higher multiplicity convergence can show up as the long-time behavior of mean curvature flow of connected surfaces in 3\mathbb{R}^{3}.

In this paper, we construct new examples of mean curvature flow in closed manifolds that converge to higher multiplicity minimal hypersurfaces as time goes to infinity. Recall that an immortal mean curvature flow is a smooth mean curvature flow that exists for all positive time. In the following, suppose SnS^{n} equips the round metric and Sn×[1,1]S^{n}\times[-1,1] equips the standard product metric. It is not too hard to see that Sn×{0}S^{n}\times\{0\} is a minimal hypersurface.

Theorem 1.1.

For all n2n\geq 2, there exists a smooth embedded connected immortal mean curvature flow (M(t))t>0(M(t))_{t>0} in Sn×[1,1]S^{n}\times[-1,1] such that M(t)M(t) converges to Sn×{0}S^{n}\times\{0\} with multiplicity 22 as tt\to\infty.

Of course, one can close up Sn×[1,1]S^{n}\times[-1,1] to get a compact manifold, or extend it to a complete noncompact manifold.

This new family of examples shows that the higher multiplicity convergence of mean curvature flow can occur for compact mean curvature flow in a closed manifold. In particular, there exists an infinite time singularity. This contrasts with a result of Jingyi Chen and Weiyong He [CH10], which proved that in manifold with certain curvature and growth conditions, the mean curvature flow can only have finite time singularities. We note that their growth condition does not hold for Sn×S^{n}\times\mathbb{R}.

Our new examples enhance our understanding of using mean curvature flow to construct minimal hypersurfaces. When higher multiplicity convergence shows up, the geometry and topology of the limit hypersurface may be different from the flow. This phenomenon has been discovered in other fields of geometric analysis, such as the Min-max theory. In [WZ22], Zhichao Wang and Xin Zhou constructed an example to show higher multiplicity minimal surfaces can show up in the Almgren-Pitts min-max theory. In [WZ23], Zhichao Wang and Xin Zhou observed that the possible obstruction to the existence of 44 minimal spheres in S3S^{3} with an arbitrary metric is the higher multiplicity convergence in the min-max theory.

Motivated by the generic multiplicity 11 property in the min-max theory proved by Xin Zhou [Zho20], we expect that higher multiplicity convergence is a non-generic property.

Conjecture 1.2.

Starting from a generic closed hypersurface in a Riemannian manifold, either the long-time limit has multiplicity 11, or the hypersurface breaks into different connected components, and each one of the connected components converges to a multiplicity 11 limit.

We remark that the limit minimal surfaces in our examples are stable. Also motivated by the min-max theory and the resolution of the Multiplicity One Conjecture by Bamler and Kleiner [BK23], we expect that higher multiplicity convergence can not occur if the limit minimal hypersurface is unstable.

Conjecture 1.3.

Suppose NN is a Riemannian manifold, (M(t))t>0(M(t))_{t>0} is a mean curvature flow of closed embedded hypersurfaces. if the limit of M(t)M(t) as tt\to\infty is a minimal hypersurface Σ\Sigma with multiplicity kk, and Σ\Sigma is unstable, then k=1k=1.

Now we discuss the strategy of the proof. The main idea is similar to [CS23] in which the authors used an interpolation argument. Here we also constructed a family of initial data (Mδ)(M^{\delta}), which are rotationally symmetry under the SO(n)SO(n) action on the sphere factor, and reflective symmetry along Sn×{0}S^{n}\times\{0\} and the equators of SnS^{n}s. Moreover, when δ\delta is small, the mean curvature flow starting from MδM^{\delta} would generate a neck singularity at the north pole of Sn×{0}S^{n}\times\{0\}, and when δ\delta is large, the mean curvature flow starting from MδM^{\delta} would shrink to a point on the equator of Sn×{0}S^{n}\times\{0\}. Then there exists an η\eta in between such that the mean curvature flow starting from MηM^{\eta} exists for all future time, namely it is an immortal flow.

It remains to show this immortal flow converges to Sn×{0}S^{n}\times\{0\} with multiplicity 22. To do so, we need to use some barriers to control the immortal flow. In [CS23], we used the planes, the catenoids, and the Angenent torus as barriers. In this paper, we find analogous barriers: the spherical minimal hypersurfaces, the spherical catenoids, and λ\lambda-Angenent torus. We will discuss these special solutions in the preliminary section.

2. Preliminary

2.1. Metric on Sn×[1,1]S^{n}\times[-1,1] and rotationally symmetric mean curvature flows

We equip SnS^{n} with the standard metric, namely the induced metric on Sn:={(x1,,xn+1)|x12+x22++xn+12=1}S^{n}:=\{(x_{1},\cdots,x_{n+1})|x_{1}^{2}+x_{2}^{2}+\cdots+x_{n+1}^{2}=1\} as a hypersurface in n+1\mathbb{R}^{n+1}. Then we equip Sn×[1,1]S^{n}\times[-1,1] with the product metric, denoted by gg. We can also view Sn×[1,1]S^{n}\times[-1,1] as the hypersurface in n+1×\mathbb{R}^{n+1}\times\mathbb{R}, equipped with the induced metric.

We consider the SO(n)SO(n) action rotating the hyperplane generated by the first nn coordinates of n+1×\mathbb{R}^{n+1}\times\mathbb{R}. This action can be induced to Sn×[1,1]S^{n}\times[-1,1] naturally. Any hypersurface in Sn×[1,1]S^{n}\times[-1,1] is called rotationally symmetric if it is invariant under this SO(n)SO(n) action. After taking the quotient, Sn×[1,1]S^{n}\times[-1,1] becomes [0,π]×[1,1][0,\pi]\times[-1,1], and we use xx and yy to denote the coordinates on [0,π][0,\pi] and [1,1][-1,1] respectively.

Given a rotationally symmetric hypersurface Γ\Gamma in Sn×[1,1]S^{n}\times[-1,1], there is an associated curve called profile curve γ:I[0,π]×[1,1]\gamma:I\to[0,\pi]\times[-1,1], while II can be an interval or S1S^{1}, such that Γ\Gamma is generated by rotating γ\gamma. That says, if we write γ(s)=(x(s),y(s))\gamma(s)=(x(s),y(s)), then we can parameterize Γ\Gamma as follows:

Γ={(cos(x(s)),sin(x(s))cos(φ2),,sin(x(s))sin(φ2)sin(φn),y(s))n+1×},\displaystyle\Gamma=\{(\cos(x(s)),\sin(x(s))\cos(\varphi_{2}),\cdots,\sin(x(s))\sin(\varphi_{2})\cdots\sin(\varphi_{n}),y(s))\in\mathbb{R}^{n+1}\times\mathbb{R}\},
while (s,φ2,,φn)I×[0,π]××[0,π]×[0,2π].\displaystyle\text{while }(s,\varphi_{2},\cdots,\varphi_{n})\in I\times[0,\pi]\times\cdots\times[0,\pi]\times[0,2\pi].

The area form of this parametrization is given by

(x)2+(y)2sinn1(x(s))sinn2(φ2)sin(φn)dsdφ2dφ3dφn.\sqrt{(x^{\prime})^{2}+(y^{\prime})^{2}}\sin^{n-1}(x(s))\sin^{n-2}(\varphi_{2})\cdots\sin(\varphi_{n})dsd\varphi_{2}d\varphi_{3}\cdots d\varphi_{n}.

After taking integration and using Fubini’s theorem, we see that the area of Γ\Gamma, up to a constant, equals the length of the curve γ[0,π]×[1,1]\gamma\subset[0,\pi]\times[-1,1] under the metric

(2.1) grot=(sin(x))2(n1)(dx2+dy2).g_{\text{rot}}=(\sin(x))^{2(n-1)}(dx^{2}+dy^{2}).

We will be interested in mean curvature flows with initial data that are rotationally symmetric, reflexive symmetric with respect to the middle sphere Sn×{0}S^{n}\times\{0\}, and reflexive symmetric with respect to the hypersurface {s=π2}×[1,1]\{s=\frac{\pi}{2}\}\times[-1,1]. We call a smooth hypersurface in Sn×[1,1]S^{n}\times[-1,1] with all above symmetry conditions as a desired hypersurface. By the short-time existence and uniqueness of the mean curvature flow, we know the rotational symmetry and reflexive symmetry are preserved under the mean curvature flow. Consider a mean curvature flow of desired hypersurfaces (M(t))t[0,T)(M(t))_{t\in[0,T)} on Sn×[1,1]S^{n}\times[-1,1]. For each hypersurface M(t)M(t), after taking the quotient of the SO(n)SO(n) action and the two reflections, we get a curve γt\gamma_{t} in the region D:=[0,π2]×[0,1]D:=[0,\frac{\pi}{2}]\times[0,1], and we name γt\gamma_{t} as the section curve of M(t)M(t) (note this is the top left part of the profile curve). We say γt\gamma_{t} is an ascending section curve if it is the graph of an increasing function, and let 𝒮\mathcal{S} denote the set of function ff such that the graph of ff is an ascending section curve of a desired hypersurface in Sn×[1,1]S^{n}\times[-1,1].

The reflexive symmetry implies that the curve γt\gamma_{t} intersects the two sides {x=0}\{x=0\}, {y=0}\{y=0\} orthogonally. We name the intersection point of γt\gamma_{t} with {y=0}\{y=0\} as the head point. This curve γt\gamma_{t} can be expressed as the union of two graphs of smooth functions uu and vv, and we call uu the vertical graph function and call its graph as the vertical graph; we call vv as the horizontal graph function and call its graph as the horizontal graph. See the picture below for an example.

(π2,0)(\frac{\pi}{2},0)(0,1)(0,1)xxyy(0,0)(0,0)(π2,1)(\frac{\pi}{2},1)region DDverticalgraphx=u(y)x=u(y)horizontal graph y=v(x)y=v(x)section curve γt\gamma_{t}head point\tkzMarkRightAngle\tkzMarkRightAngle
Figure 1. Example of a section curve that we study.

Let u0u_{0} and v0v_{0} be the vertical graph function and the horizontal graph function of the initial curve γ0\gamma_{0}. Suppose after reflecting and rotating γ0\gamma_{0} we get a hypersurface M(0)M(0) in Sn×[1,1]S^{n}\times[-1,1]. Then a family of hypersurfaces {M(t)}t[0,T)\{M(t)\}_{t\in[0,T)} is said to be a mean curvature flow with initial condition M(0)M(0) if the corresponding vertical graph function, horizontal graph function u(,t)u(\cdot,t), v(,t)v(\cdot,t) of γt\gamma_{t} satisfy the following equations (see Appendix A):

(2.2) {ut=uyy1+(uy)2(n1)cos(u)sin(u),vt=vxx1+(vx)2+(n1)cosxsinxvx,u(,0)=u0,v(,0)=v0,uy(0,)=0,vx(π2,)=0.\left\{\begin{aligned} &\frac{\partial u}{\partial t}=\frac{u_{yy}}{1+(u_{y})^{2}}-(n-1)\frac{\cos(u)}{\sin(u)},\\ &\frac{\partial v}{\partial t}=\frac{v_{xx}}{1+(v_{x})^{2}}+(n-1)\frac{\cos x}{\sin x}v_{x},\\ &u(\cdot,0)=u_{0},\ v(\cdot,0)=v_{0},\\ &u_{y}(0,\cdot)=0,\ v_{x}(\frac{\pi}{2},\cdot)=0.\end{aligned}\right.

For simplicity, we will say f(,t)f(\cdot,t) is a solution to equation (2.2) if its corresponding vertical graph function and horizontal graph function solve this equation. We will call the first equation in (2.2) the vertical graph equation, and call the second equation in (2.2) the horizontal graph equation.

2.2. Minimal hypersurfaces as barriers

Suppose γ1\gamma^{1} and γ2\gamma^{2} are two curves in DD. We say that γ1\gamma^{1} is on top of γ2\gamma^{2}, if for all pairs (c,y1,y2)(c,y_{1},y_{2}) such that (c,y1)γ1,(c,y2)γ2(c,y_{1})\in\gamma^{1},(c,y_{2})\in\gamma^{2}, it holds that y1y2y_{1}\geq y_{2}. Recall the comparison principle for mean curvature flow:

Proposition 2.1 (Comparison principle).

Suppose NN is a closed manifold, (M1(t))t[0,T](M^{1}(t))_{t\in[0,T]} and (M2(t))t[0,T](M^{2}(t))_{t\in[0,T]} are two mean curvature flows of smooth embedded hypersurfaces in NN. If M1(0)M^{1}(0) does not intersect M2(0)M^{2}(0), then M1(t)M^{1}(t) does not intersect M2(t)M^{2}(t) for all t[0,T]t\in[0,T].

Therefore, we can use barriers that are either on top of the flow or under the flow at the initial time to control the behavior of the flow at a later time. We will frequently use the following special solutions as barriers in this paper.

Firstly, we consider the static solutions known as the minimal hypersurfaces. The simplest possible examples are the horizontal graphs (x,v(x,t))(x,v(x,t)) given by v(x,t)Cv(x,t)\equiv C for a constant C[1,1]C\in[-1,1]. Such a minimal hypersurface is just a section of Sn×[1,1]S^{n}\times[-1,1], and we call it a minimal sphere. There is only one constant vertical graph (u(y,t),y)(u(y,t),y) given by u(y,t)π/2u(y,t)\equiv\pi/2. It is the Cartesian product of the geodesic hypersphere in SnS^{n} with [1,1][-1,1], and we still call it a geodesic hypersphere.

Another class of minimal hypersurfaces is the analog of the catenoids, and we call them spherical catenoids. Given a parameter C(0,π/2)C\in(0,\pi/2), we can solve the ODE

(2.3) uyy1+(uy)2(n1)cos(u)sin(u)=0,\frac{u_{yy}}{1+(u_{y})^{2}}-(n-1)\frac{\cos(u)}{\sin(u)}=0,

with initial condition u(0)=Cu(0)=C and uy(0)=0u_{y}(0)=0. First, (2.3) is invariant under yyy\leftrightarrow-y, so the solution must be an even function, and hence we only need to study the part of the solution where y0y\geq 0. It is straightforward to see that uyy(0)>0u_{yy}(0)>0, and hence uy>0u_{y}>0 in a neighborhood of 0. Multiplying both sides of (2.3) by uyu_{y} yields the identity

12(log(1+(uy)2))y(n1)(log(sinu))y=0,\frac{1}{2}(\log(1+(u_{y})^{2}))_{y}-(n-1)(\log(\sin u))_{y}=0,

and then we can conclude that there exists a constant λC\lambda_{C} such that

uy2=λC2(sinu)2(n1)1.u_{y}^{2}=\lambda_{C}^{2}(\sin u)^{2(n-1)}-1.

By plugging in u(0)=Cu(0)=C we obtain

λC=(sinC)(n1).\lambda_{C}=(\sin C)^{-(n-1)}.

Then we obtain that uy(y)>0u_{y}(y)>0 for all y(0,YC)y\in(0,Y_{C}), where u(YC)=πCu(Y_{C})=\pi-C. We may write the expression of uyu_{y} as

uy=(sinu)2(n1)(sinC)2(n1)1.u_{y}=\sqrt{\frac{(\sin u)^{2(n-1)}}{(\sin C)^{2(n-1)}}-1}.

We can also obtain the information of uu by looking at the inverse function vv, which satisfies the equation

(2.4) vxx1+(vx)2+(n1)cos(x)sin(x)vx=0,\frac{v_{xx}}{1+(v_{x})^{2}}+(n-1)\frac{\cos(x)}{\sin(x)}v_{x}=0,

where v(C)=0v(C)=0 and v(πC)=YCv(\pi-C)=Y_{C}, and vxv_{x}\to\infty as xCx\searrow C or x(πC)x\nearrow(\pi-C). dividing both sides of (2.4) by vxv_{x} yields the identity

[log(vx)12log(1+(vx)2)+(n1)logsinx]x=0.\left[\log(v_{x})-\frac{1}{2}\log(1+(v_{x})^{2})+(n-1)\log\sin x\right]_{x}=0.

Therefore, there exists λ¯C>0\bar{\lambda}_{C}>0 such that

vx1+(vx)2=λ¯C(sinx)(n1).\frac{v_{x}}{\sqrt{1+(v_{x})^{2}}}=\bar{\lambda}_{C}(\sin x)^{-(n-1)}.

Let xCx\searrow C, we have λ¯C=(sinC)(n1)\bar{\lambda}_{C}=(\sin C)^{-(n-1)}. Then we obtain

(2.5) vx=((sinxsinC)2(n1)1)1/2v_{x}=\left(\left(\frac{\sin x}{\sin C}\right)^{2({n-1})}-1\right)^{-1/2}

This implies that vx>0v_{x}>0 for all x(C,πC)x\in(C,\pi-C), and vx(x)+(v(πx))x=0v_{x}(x)+(v(\pi-x))_{x}=0. Then we can show that v(x)=2v(π/2)v(πx)v(x)=2v(\pi/2)-v(\pi-x). It is also clear that v(π/2)=YC/2v(\pi/2)=Y_{C}/2.

Lemma 2.2.

We have the following asymptotic of YCY_{C}:

(2.6) limC0YC=0,lim supCπ/2YC22n1.\lim_{C\to 0}Y_{C}=0,\quad\limsup_{C\to\pi/2}Y_{C}\geq 2\sqrt{\frac{2}{n-1}}.
Proof.

By (2.5) and v(C)=0v(C)=0, we have

YC=v(πC)v(C)=CπCvx(z)𝑑z=CπC((sinzsinC)2(n1)1)1/2𝑑z=2Cπ2((sinzsinC)2(n1)1)1/2𝑑z.\begin{split}Y_{C}=&v(\pi-C)-v(C)=\int_{C}^{\pi-C}v_{x}(z)dz\\ =&\int_{C}^{\pi-C}\left(\left(\frac{\sin z}{\sin C}\right)^{2(n-1)}-1\right)^{-1/2}dz=2\int_{C}^{\frac{\pi}{2}}\left(\left(\frac{\sin z}{\sin C}\right)^{2(n-1)}-1\right)^{-1/2}dz.\end{split}

Using the fact sin2zsin2C=sin(z+C)sin(zC)\sin^{2}z-\sin^{2}C=\sin(z+C)\sin(z-C), for C(0,π6)C\in(0,\frac{\pi}{6}), we have

Cπ2((sinzsinC)2(n1)1)1/2𝑑zCπ2((sinzsinC)21)1/2𝑑z\displaystyle\int_{C}^{\frac{\pi}{2}}\left(\left(\frac{\sin z}{\sin C}\right)^{2(n-1)}-1\right)^{-1/2}dz\leq\int_{C}^{\frac{\pi}{2}}\left(\left(\frac{\sin z}{\sin C}\right)^{2}-1\right)^{-1/2}dz
=\displaystyle= sinCCπ21sin2zsin2C𝑑z=sinCCπ21sin(z+C)sin(zC)𝑑z\displaystyle\sin C\int_{C}^{\frac{\pi}{2}}\frac{1}{\sqrt{\sin^{2}z-\sin^{2}C}}dz=\sin C\int_{C}^{\frac{\pi}{2}}\frac{1}{\sqrt{\sin(z+C)\sin(z-C)}}dz
\displaystyle\leq sinCsin(2C)Cπ21sin(zC)𝑑zsinCsin(2C)Cπ22zC𝑑z=2sinCπ2Csin(2C).\displaystyle\frac{\sin C}{\sqrt{\sin(2C)}}\int_{C}^{\frac{\pi}{2}}\frac{1}{\sqrt{\sin(z-C)}}dz\leq\frac{\sin C}{\sqrt{\sin(2C)}}\int_{C}^{\frac{\pi}{2}}\sqrt{\frac{2}{z-C}}dz=\frac{2\sin C\sqrt{\pi-2C}}{\sqrt{\sin(2C)}}.

By letting C0C\to 0, we see that limC0YC=0\lim\limits_{C\to 0}Y_{C}=0. On the other hand,

(sinz)2(n1)(sinC)2(n1)=(sinzsinC)(sinz+sinC)[(sinz)2(n2)+(sinC)2(n2)]\displaystyle(\sin z)^{2(n-1)}-(\sin C)^{2(n-1)}=(\sin z-\sin C)(\sin z+\sin C)[(\sin z)^{2(n-2)}+\cdots(\sin C)^{2(n-2)}]
2(n1)(sinzsinC)(sinz)2n32(n1)(sinzsinC).\displaystyle\leq 2(n-1)(\sin z-\sin C)(\sin z)^{2n-3}\leq 2(n-1)(\sin z-\sin C).

Thus

Cπ2((sinzsinC)2(n1)1)1/2𝑑z=Cπ2(sinC)2(n1)(sinz)2(n1)(sinC)2(n1)𝑑z\displaystyle\int_{C}^{\frac{\pi}{2}}\left(\left(\frac{\sin z}{\sin C}\right)^{2(n-1)}-1\right)^{-1/2}dz=\int_{C}^{\frac{\pi}{2}}\sqrt{\frac{(\sin C)^{2(n-1)}}{(\sin z)^{2(n-1)}-(\sin C)^{2(n-1)}}}dz
Cπ2(sinC)n12(n1)(sinzsinC)𝑑z=(sinC)n12(n1)Cπ21sinzsinC𝑑z.\displaystyle\geq\int_{C}^{\frac{\pi}{2}}\frac{(\sin C)^{n-1}}{\sqrt{2(n-1)(\sin z-\sin C)}}dz=\frac{(\sin C)^{n-1}}{\sqrt{2(n-1)}}\int_{C}^{\frac{\pi}{2}}\frac{1}{\sqrt{\sin z-\sin C}}dz.

Since sinzsinC=sinCcos(zC)+cosCsin(zC)sinCcosCsin(zC)\sin z-\sin C=\sin C\cos(z-C)+\cos C\sin(z-C)-\sin C\leq\cos C\sin(z-C), thus

lim supCπ2YC\displaystyle\limsup\limits_{C\to\frac{\pi}{2}}Y_{C} 2n1limCπ2Cπ21sinzsinC𝑑z2n1limCπ2Cπ21cosCsin(zC)𝑑z\displaystyle\geq\sqrt{\frac{2}{n-1}}\lim\limits_{C\to\frac{\pi}{2}}\int_{C}^{\frac{\pi}{2}}\frac{1}{\sqrt{\sin z-\sin C}}dz\geq\sqrt{\frac{2}{n-1}}\lim\limits_{C\to\frac{\pi}{2}}\int_{C}^{\frac{\pi}{2}}\frac{1}{\sqrt{\cos C\sin(z-C)}}dz
2n1limCπ20π2C1sinz𝑑zcosC=2n1limCπ21/sin(π2C)sinC/2cosC=22n1.\displaystyle\geq\sqrt{\frac{2}{n-1}}\lim\limits_{C\to\frac{\pi}{2}}\frac{\int_{0}^{\frac{\pi}{2}-C}\frac{1}{\sqrt{\sin z}}dz}{\sqrt{\cos C}}=\sqrt{\frac{2}{n-1}}\lim\limits_{C\to\frac{\pi}{2}}\frac{1/\sqrt{\sin(\frac{\pi}{2}-C)}}{\sin C/2\sqrt{\cos C}}=2\sqrt{\frac{2}{n-1}}.

Remark 2.3.

Using the fact that sinzsinC=2sin(zC2)cos(z+C2)2sin(zC2)cos(π+2C4)\sin z-\sin C=2\sin(\frac{z-C}{2})\cos(\frac{z+C}{2})\geq 2\sin(\frac{z-C}{2})\cos(\frac{\pi+2C}{4}), by a similar estimate, we can show that lim supCπ2YC42n1\limsup\limits_{C\to\frac{\pi}{2}}Y_{C}\leq 4\sqrt{\frac{2}{n-1}}.

In fact, the spherical catenoids are periodic in the \mathbb{R} factor, and YCY_{C} is half of the period. See Figure 3 for a picture.

2.3. λ\lambda-Angenent curves

In his pioneer work [Ang92], Angenent constructed a rotationally symmetric self-shrinking mean curvature flow in n+1\mathbb{R}^{n+1} that is topological S1×Sn1S^{1}\times S^{n-1} before it becomes singular. More precisely, Angenent constructed a closed embedded hypersurface Σnn+1\Sigma_{n}\subset\mathbb{R}^{n+1} that is rotationally symmetric, such that {tΣn}t<0\{\sqrt{-t}\Sigma_{n}\}_{t<0} is a mean curvature flow.

It was observed by Huisken [Hui84] that if {tΣ}t<0\{\sqrt{-t}\Sigma\}_{t<0} is a mean curvature flow, then Σ\Sigma satisfies the equation H+x/2=0\vec{H}+x^{\perp}/2=0, and such Σ\Sigma is called a shrinker. Moreover, Huisken observed that a shrinker in n+1\mathbb{R}^{n+1} is the critical point of the Gaussian area functional (Σ)=Σe|x|2/4𝑑n(x)\mathcal{F}(\Sigma)=\int_{\Sigma}e^{-|x|^{2}/4}d\mathcal{H}^{n}(x). Therefore, Angenent reduced the existence of a rotationally symmetric shrinker to the existence of a closed embedded geodesic in the half-plane {(x,y)|x0}\{(x,y)|x\geq 0\} equipped with the metric x2(n1)e(x2+y2)/2(dx2+dy2)x^{2(n-1)}e^{-(x^{2}+y^{2})/2}(dx^{2}+dy^{2}).

Angenent used a shooting method to construct such a closed embedded geodesic. The idea is to examine the trajectory of the geodesics starting from (r,0)(r,0) with unit tangent vector (0,1)(0,1) as rr varies. Then an interpolation argument asserts the existence of a geodesic trajectory that will get back to some (s,0)(s,0) again with tangent vector (0,1)(0,-1). Reflecting this geodesic trajectory along the xx-axis gives a desired closed embedded geodesic.

We would like to point out that if we replace (n1)(n-1) by some λ>0\lambda>0, all the proofs in [Ang92] still work (See Appendix B for an explanation). We call a closed embedded geodesic in the half-plane {(x,y)|x0}\{(x,y)|x\geq 0\} equipped with the metric x2λe(x2+y2)/2(dx2+dy2)x^{2\lambda}e^{-(x^{2}+y^{2})/2}(dx^{2}+dy^{2}) a λ\lambda-Angenent curve. Such curves will be the barriers. In fact, when n3n\geq 3, we can just use the (n1)(n-1)-dimensional Angenent torus as the barrier. Only in the case n=2n=2 we need a λ\lambda-Angenent curve as the barrier for λ(0,1)\lambda\in(0,1).

3. Main result

Throughout this paper, to simplify the notation, we will use the names of the hypersurfaces (minimal spheres, geodesic hyperspheres, spherical catenoids, etc.) to denote their profile curves and section curves as well.

3.1. Rotationally symmetric mean curvature flow

In this section, we study the solutions to the equation (2.2).

We will introduce the following notations throughout this section. (M(t))t[0,T)(M(t))_{t\in[0,T)} is a rotationally symmetric mean curvature flow in Sn×[1,1]S^{n}\times[-1,1]. The section curve of M(t)M(t) is γt\gamma_{t}, and can be expressed as the graph of f(,t)f(\cdot,t). Therefore f(,t)f(\cdot,t) is a solution to the equation (2.2). u(,t)u(\cdot,t), v(,t)v(\cdot,t) will denote the vertical graph function and the horizontal graph function of f(,t)f(\cdot,t).

Proposition 3.1.

If the initial section curve γ0\gamma_{0} is an ascending section curve and T>0T>0 is the first singular time, then γt\gamma_{t} is an ascending section curve for all t(0,T)t\in(0,T).

Proof.

γ0\gamma_{0} is an ascending section curve means u(y)>0u^{\prime}(y)>0, and v(x)>0v^{\prime}(x)>0 besides the boundary. Since u(,t)u(\cdot,t), v(,t)v(\cdot,t) are solutions to the equation (2.2), we know that uyu_{y} and vxv_{x} satisfies the following equation

(3.1) uyt=(uy)yy1+(uy)22uy[(uy)y]2(1+(uy)2)2+(n1)uysin2u,\displaystyle\frac{\partial u_{y}}{\partial t}=\frac{(u_{y})_{yy}}{1+(u_{y})^{2}}-2\frac{u_{y}[(u_{y})_{y}]^{2}}{(1+(u_{y})^{2})^{2}}+(n-1)\frac{u_{y}}{\sin^{2}u},
vxt=(vx)xx1+(vx)22vx[(vx)x]2(1+(vx)2)2(n1)vxsin2x+(n1)cosxsinx(vx)x.\displaystyle\frac{\partial v_{x}}{\partial t}=\frac{(v_{x})_{xx}}{1+(v_{x})^{2}}-2\frac{v_{x}[(v_{x})_{x}]^{2}}{(1+(v_{x})^{2})^{2}}-(n-1)\frac{v_{x}}{\sin^{2}x}+(n-1)\frac{\cos x}{\sin x}(v_{x})_{x}.

By the strict maximum principle of the quasilinear equation, we claim that for t>0t>0,

(3.2) uy(y,t)>0,vx(x,t)>0.\displaystyle u_{y}(y,t)>0,\ v_{x}(x,t)>0.

From now on we will assume that the initial section curve γ0\gamma_{0} is ascending. It follows from Proposition 3.1 that γt\gamma_{t} is an ascending section curve, thus the height of γt\gamma_{t} (i.e. the maximum of f(,t)f(\cdot,t)) is given by f(π2,t)f(\frac{\pi}{2},t). We prove in the next lemma that it is monotone.

Lemma 3.2.

If γ0\gamma_{0} is an ascending section curve, then the height of γt\gamma_{t} is strictly decreasing in tt.

Proof.

The horizontal line y=f(π2,t)y=f(\frac{\pi}{2},t) is on top of the curve γt\gamma_{t}, and remains static under the mean curvature flow. By Proposition 2.1, for any t<tt<t^{\prime}, y=f(π2,t)y=f(\frac{\pi}{2},t) is on top of the curve γt\gamma_{t^{\prime}}, thus f(π2,t)f(π2,t)f(\frac{\pi}{2},t^{\prime})\leq f(\frac{\pi}{2},t). Moreover, if f(,0)f(\cdot,0) is not a constant function, then the strong maximum principle yields the result.

Although Lemma 3.2 shows that the height of the section curve of the flow strictly decreases, we do not have a quantitative estimate of the decreasing rate. To obtain such a bound, we need to construct a new family of barriers.

Given a(0,π2)a\in(0,\frac{\pi}{2}), Consider a smooth function laC([0,π2])l_{a}\in C^{\infty}([0,\frac{\pi}{2}]) such that

la(x)={0for0xa2,1foraxπ2,l_{a}(x)=\left\{\begin{aligned} &0\qquad\text{for}\qquad 0\leq x\leq\frac{a}{2},\\ &1\qquad\text{for}\qquad a\leq x\leq\frac{\pi}{2},\end{aligned}\right.

and la(x)>0l_{a}^{\prime}(x)>0 for x(a2,a)x\in(\frac{a}{2},a).

By similar arguments as in authors’ previous paper [CS23], there exists a smooth solution La(x,t)L_{a}(x,t) to the horizontal graph equation with initial data La(x,0)=la(x)L_{a}(x,0)=l_{a}(x), and boundary condition xLa(0,t)=xLa(π2,t)=0\frac{\partial}{\partial x}L_{a}(0,t)=\frac{\partial}{\partial x}L_{a}(\frac{\pi}{2},t)=0. We have the following lemmas which are based on the maximum principle and Sturmian theorem (see [CS23, Lemma 3.4, 3.5]).

Lemma 3.3.

There exist a constant βa>0\beta_{a}>0 and a time Ta>0T_{a}>0 such that La(π2,t)<1βaL_{a}(\frac{\pi}{2},t)<1-\beta_{a} for all t>Tat>T_{a}.

Lemma 3.4.

Given T>0T>0, there exists a continuous nonincreasing function σ:(0,π4]+\sigma:(0,\frac{\pi}{4}]\to\mathbb{R}_{+} that only depends on the head point of the initial condition (i.e. u(0,0)u(0,0)) and TT, such that

0<uy(y,t)eσ(δ)/t,δ=min{u(y,t),π2u(y,t)},\displaystyle 0<u_{y}(y,t)\leq e^{\sigma(\delta)/t},\quad\delta=\min\{u(y,t),\frac{\pi}{2}-u(y,t)\},

holds for all 0<t<T0<t<T, 0<y<f(π2,t)0<y<f(\frac{\pi}{2},t).

Next, we examine the behavior of the head point when the singularity appears during the mean curvature flow. By Lemma 3.2, we know the limit of the height h:=limtTf(π2,t)h:=\lim\limits_{t\to T}f(\frac{\pi}{2},t) exists. The gradient estimate in Lemma 3.4 implies that if the height of the function f(,t)f(\cdot,t) tends to 0, then the head point must tend to the boundary x=π2x=\frac{\pi}{2}.

Corollary 3.5.

If h=0h=0, then limtTu(0,t)=π2\lim\limits_{t\to T}u(0,t)=\frac{\pi}{2}.

Proof.

We prove this by contradiction. Suppose not, then there exists 0<ϵ<120<\epsilon<\frac{1}{2} and an increasing sequence {ti}\{t_{i}\} such that limiti=T\lim\limits_{i\to\infty}t_{i}=T, limiu(0,ti)<π2ϵ\lim\limits_{i\to\infty}u(0,t_{i})<\frac{\pi}{2}-\epsilon.

Then f(x,ti)f(x,t_{i}) is well-defined on [π2ϵ,π2ϵ2][\frac{\pi}{2}-\epsilon,\frac{\pi}{2}-\frac{\epsilon}{2}]. Let a(ti)=f(π2ϵ,ti)a(t_{i})=f(\frac{\pi}{2}-\epsilon,t_{i}), b(ti)=f(π2ϵ2,ti)b(t_{i})=f(\frac{\pi}{2}-\frac{\epsilon}{2},t_{i}), then by Lemma 3.4,

ϵ2=u(b(ti),ti)u(a(ti),ti)=a(ti)b(ti)uy(y,ti)𝑑y(b(ti)a(ti))eσ(ϵ2)/ti.\displaystyle\frac{\epsilon}{2}=u(b(t_{i}),t_{i})-u(a(t_{i}),t_{i})=\int_{a(t_{i})}^{b(t_{i})}u_{y}(y,t_{i})dy\leq(b(t_{i})-a(t_{i}))e^{\sigma(\frac{\epsilon}{2})/t_{i}}.

Hence f(π2,ti)b(ti)ϵ2eσ(ϵ2)/tiϵ2eσ(ϵ2)/Tf(\frac{\pi}{2},t_{i})\geq b(t_{i})\geq\frac{\epsilon}{2}e^{-\sigma(\frac{\epsilon}{2})/t_{i}}\geq\frac{\epsilon}{2}e^{-\sigma(\frac{\epsilon}{2})/T} for all ii. Moreover limtiTf(π2,ti)ϵ2eσ(ϵ2)/T>0\lim\limits_{t_{i}\to T}f(\frac{\pi}{2},t_{i})\geq\frac{\epsilon}{2}e^{-\sigma(\frac{\epsilon}{2})/T}>0, which contradicts to limtTf(π2,t)=0\lim\limits_{t\to T}f(\frac{\pi}{2},t)=0.

On the other hand, if the limit of the height hh is not zero, we obtain an improved gradient estimate.

Lemma 3.6.

If the height h>0h>0, then for any 0<a<h0<a<h, let λ=πha\lambda=\frac{\pi}{h-a}, there exists a constant ε>0\varepsilon>0 such that uy(y,t)εeλ2tsin(λ(ya))u_{y}(y,t)\geq\varepsilon e^{-\lambda^{2}t}\sin(\lambda(y-a)) for all y[a,h]y\in[a,h], 0t<T0\leq t<T. In addition, u(a,t)π22ελeλ2Tu(a,t)\leq\frac{\pi}{2}-\frac{2\varepsilon}{\lambda}e^{-\lambda^{2}T}.

Proof.

For 0t<T0\leq t<T, u(y,t)u(y,t) is well-defined on [0,h][0,h] and uy(y,t)>0u_{y}(y,t)>0 for y(0,h]y\in(0,h]. We know uu satisfies the vertical graph equation

ut=uyy1+(uy)2cosusinu.\displaystyle u_{t}=\frac{u_{yy}}{1+(u_{y})^{2}}-\frac{\cos u}{\sin u}.

Define θ(y,t)=arctanuy(y,t)\theta(y,t)=\arctan u_{y}(y,t), then θ(y,t)(0,π2)\theta(y,t)\in(0,\frac{\pi}{2}) for y[a,h]y\in[a,h], and

ut=θycosusinu,θt=11+(uy)2(uy)t=11+(uy)2(ut)y=11+(uy)2(θyy+uysin2u).\displaystyle u_{t}=\theta_{y}-\frac{\cos u}{\sin u},\qquad\theta_{t}=\frac{1}{1+(u_{y})^{2}}(u_{y})_{t}=\frac{1}{1+(u_{y})^{2}}(u_{t})_{y}=\frac{1}{1+(u_{y})^{2}}\left(\theta_{yy}+\frac{u_{y}}{\sin^{2}u}\right).

Hence θtθyy1+(uy)2>0\theta_{t}-\frac{\theta_{yy}}{1+(u_{y})^{2}}>0 for y[a,h]y\in[a,h]. Since θ(y,0)>0\theta(y,0)>0 for all y[a,h]y\in[a,h], let ε=miny[a,h]θ(y,0)>0\varepsilon=\min_{y\in[a,h]}\theta(y,0)>0, φ(y,t)=εeλ2tsin(λ(ya))\varphi(y,t)=\varepsilon e^{-\lambda^{2}t}\sin(\lambda(y-a)). Then φt=φyy0\varphi_{t}=\varphi_{yy}\leq 0 on [a,h][a,h], thus

φtφyy1+(uy)2=φyy(uy)21+(uy)20<θtθyy1+(uy)2.\displaystyle\varphi_{t}-\frac{\varphi_{yy}}{1+(u_{y})^{2}}=\varphi_{yy}\frac{(u_{y})^{2}}{1+(u_{y})^{2}}\leq 0<\theta_{t}-\frac{\theta_{yy}}{1+(u_{y})^{2}}.

Therefore ϕ\phi is a subsolution, and θ\theta is a supersolution of the PDE ftfyy1+(uy2)=0f_{t}-\frac{f_{yy}}{1+(u_{y}^{2})}=0 on the interval [a,h][a,h]. Initially we have φ(y,0)εθ(y,0)\varphi(y,0)\leq\varepsilon\leq\theta(y,0), and at the two endpoints of the interval [a,h][a,h], φ(a,t)=0<θ(a,t)\varphi(a,t)=0<\theta(a,t), φ(h,t)=0<θ(h,t)\varphi(h,t)=0<\theta(h,t). By the classical maximum principle, we conclude θ(y,t)φ(y,t)\theta(y,t)\geq\varphi(y,t) for all ayh,0t<Ta\leq y\leq h,0\leq t<T. Therefore

uy(y,t)=tanθ(y,t)θ(y,t)φ(y,t)=εeλ2tsin(λ(ya)),\displaystyle u_{y}(y,t)=\tan\theta(y,t)\geq\theta(y,t)\geq\varphi(y,t)=\varepsilon e^{-\lambda^{2}t}\sin(\lambda(y-a)),
u(h,t)u(a,t)=ahuy(y,t)𝑑yahεeλ2tsin(λ(ya))𝑑y=2λeλ2t.\displaystyle u(h,t)-u(a,t)=\int_{a}^{h}u_{y}(y,t)dy\geq\int_{a}^{h}\varepsilon e^{-\lambda^{2}t}\sin(\lambda(y-a))dy=\frac{2}{\lambda}e^{-\lambda^{2}t}.

This implies u(a,t)π22ελeλ2Tu(a,t)\leq\frac{\pi}{2}-\frac{2\varepsilon}{\lambda}e^{-\lambda^{2}T}.

Now we are ready to describe the possible singular behaviors of the mean curvature flow with a desired hypersurface as the initial condition. Recall that we assume the initial section curve γ0\gamma_{0} is ascending. In [CS23], we used the Evans-Spruck estimates ([ES92, Corollary 5.3], also see [AAG95, Page 303]) of the gradient of the graph function of mean curvature flow in n+1\mathbb{R}^{n+1}. We need a generalization of this graph estimate to Sn×S^{n}\times\mathbb{R} in [BM12].

In the following, for r(0,π/2)r\in(0,\pi/2), we use BrB_{r} to denote a given ball of radius rr in SnS^{n}.

Lemma 3.7.

Given r>0r>0, there exists τ=τ(r)\tau=\tau(r) with the following significance: Suppose f:Br(p)×[0,τ]f:B_{r}(p)\times[0,\tau]\to\mathbb{R} is a function such that the graph of f(,t)f(\cdot,t) is a mean curvature flow in Br×B_{r}\times\mathbb{R}, then for t[0,τ]t\in[0,\tau],

(3.3) |f(p,t)|C(τ)+C(τ)|f(p,0)|.|\nabla f(p,t)|\leq C(\tau)+C(\tau)|\nabla f(p,0)|.
Proof.

The proof can be found in [BM12]. In the following, distp\operatorname{dist}_{p} is the distance function on SnS^{n} from the point pSnp\in S^{n}, and for μ<0\mu<0, cμ(ρ)=cosh(μρ)c_{\mu}(\rho)=\cosh(\sqrt{-\mu}\rho). Using the proof of [BM12, Theorem 7], we can obtain that for any μ<0\mu<0,

(3.4) (cμ(r)μcμ(distp(x))μeμt)21+|f(x,t)|2\displaystyle\left(\frac{c_{\mu}(r)}{-\mu}-\frac{c_{\mu}(\operatorname{dist}_{p}(x))}{-\mu}e^{-\mu t}\right)^{2}\sqrt{1+|\nabla f(x,t)|^{2}}
\displaystyle\leq (cμ(r)μ)2e(n1)μtsupdistp(y)r1+|f(y,0)|2.\displaystyle\left(\frac{c_{\mu}(r)}{-\mu}\right)^{2}e^{-(n-1)\mu t}\sup_{\operatorname{dist}_{p}(y)\leq r}\sqrt{1+|\nabla f(y,0)|^{2}}.

Then when τ\tau is sufficiently small, we can choose appropriate μ<0\mu<0 such that cμ(r)>eμτc_{\mu}(r)>e^{-\mu\tau} to derive a desired bound for |f(p,τ)||\nabla f(p,\tau)|.

Proposition 3.8.

The flow first becomes singular at time TT if and only if limtTu(0,t)=0\lim\limits_{t\to T}u(0,t)=0 or limtTu(0,t)=π2\lim\limits_{t\to T}u(0,t)=\frac{\pi}{2}. In addition, if such TT doesn’t exist, then the mean curvature flow exists for all future time.

Proof.

As shown in equation (2.2), the mean curvature of the hypersurfaces near the head point is given by uyy1+(uy)2(n1)cos(u)sin(u)\frac{u_{yy}}{1+(u_{y})^{2}}-(n-1)\frac{\cos(u)}{\sin(u)}, thus a singularity appears when limtTu(0,t)=0\lim\limits_{t\to T}u(0,t)=0. If limtTu(0,t)=π2\lim\limits_{t\to T}u(0,t)=\frac{\pi}{2}, then the section curve collapses, and singularity appears at the geodesic hypersphere. Now we assume neither of the above happens, and we want to show that TT is not a singular time.

We prove by contradiction and assume that a singularity appears at time TT. By Corollary 3.5, h>0h>0. We claim that there exists ϵ1>0\epsilon_{1}>0 such that u(0,t)>ϵ1u(0,t)>\epsilon_{1} for all 0t<T0\leq t<T. Otherwise there exists a sequence {ti}\{t_{i}\} in [0,T)[0,T) such that limiu(0,ti)=0\lim\limits_{i\to\infty}u(0,t_{i})=0. Up to extracting from a subsequence, we can assume tit_{i} converges to T[0,T]T^{\prime}\in[0,T]. Since u(0,T)0u(0,T)\neq 0, T<TT^{\prime}<T, and a singularity appears at the origin at time TT^{\prime}, which is a contradiction.

By a similar argument, we can also assume that u(0,t)<π2ϵ1u(0,t)<\frac{\pi}{2}-\epsilon_{1} for all 0t<T0\leq t<T.

For any 0<a<h0<a<h, by Lemma 3.6, we know u(a,t)<π22ελeλ2Tu(a,t)<\frac{\pi}{2}-\frac{2\varepsilon}{\lambda}e^{-\lambda^{2}T}. Let ϵ=min{ϵ1,2ελeλ2T}\epsilon=\min\{\epsilon_{1},\frac{2\varepsilon}{\lambda}e^{-\lambda^{2}T}\}, we know ϵ<u(0,t)<u(a,t)<π2ϵ\epsilon<u(0,t)<u(a,t)<\frac{\pi}{2}-\epsilon.

We claim that u(y,t)u(y,t) is smooth at (y,t)[0,a]×[0,T](y,t)\in[0,a]\times[0,T]. This follows from uy(0,t)=0u_{y}(0,t)=0, a priori estimate for uyu_{y} in Lemma 3.4, and hence (see [LSU68]) for all higher derivatives of uu in the interior. Therefore the singularity can only appear on the boundary, i.e. at (π2,h)(\frac{\pi}{2},h).

Now consider the horizontal graph function v(x,t)v(x,t), which is defined for π2ϵ1xπ2\frac{\pi}{2}-\epsilon_{1}\leq x\leq\frac{\pi}{2}, 0<t<T0<t<T, and we can extend this function smoothly on xx to [π2,π2+ϵ1][\frac{\pi}{2},\frac{\pi}{2}+\epsilon_{1}] by the symmetry. This function is uniformly bounded by the height of the initial condition, and it is a solution of the horizontal graph equation. Let τ=τ(ϵ12)\tau=\tau(\frac{\epsilon_{1}}{2}), for any p(πϵ12,π+ϵ12)p\in(\frac{\pi-\epsilon_{1}}{2},\frac{\pi+\epsilon_{1}}{2}), consider the flow of vx,tv_{x,t} on Bϵ12(p)×[Tτ,T)B_{\frac{\epsilon_{1}}{2}}(p)\times[T-\tau,T). By Lemma 3.7, v\nabla v, as well as all higher space derivatives of vv, are uniformly bounded on the region {(x,t):πϵ12xπ+ϵ12,Tτ<t<T}\{(x,t):\frac{\pi-\epsilon_{1}}{2}\leq x\leq\frac{\pi+\epsilon_{1}}{2},\ T-\tau<t<T\}. Hence v(x,t)v(x,T)v(x,t)\to v(x,T) uniformly in πϵ12xπ+ϵ12\frac{\pi-\epsilon_{1}}{2}\leq x\leq\frac{\pi+\epsilon_{1}}{2} as tTt\nearrow T. We have also shown that vt(r,t)v_{t}(r,t) is uniformly bounded for πϵ12xπ+ϵ12\frac{\pi-\epsilon_{1}}{2}\leq x\leq\frac{\pi+\epsilon_{1}}{2}, Tτ<t<TT-\tau<t<T, hence (π2,h)=(π2,v(π2,T))(\frac{\pi}{2},h)=(\frac{\pi}{2},v(\frac{\pi}{2},T)) cannot be a singular point.

In the following proposition, we show that the appearance of the singularity on the boundary {x=0}\{x=0\} (i.e. the rotation axis {North pole}×[1,1]\{\text{North pole}\}\times[-1,1] in the manifold) is an open condition.

Proposition 3.9.

Let \mathscr{L} denote the set of function f0𝒮f_{0}\in\mathcal{S} such that the solution f(,t)f(\cdot,t) to the equation (2.2) with initial condition f(,0)=f0f(\cdot,0)=f_{0} becomes singular in finite time, and limtTu(0,t)=0\lim\limits_{t\to T}u(0,t)=0 for some T>0T>0, then \mathscr{L} is an open set in 𝒮\mathcal{S} with respect to the C1C^{1} norm.

Proof.

The idea is similar to the proof of [CS23, Proposition 3.10]. We can isometrically embed Sn×[1,1]S^{n}\times[-1,1] into n+2\mathbb{R}^{n+2}. Then the mean curvature flow (M0(t))t[0,T)(M^{0}(t))_{t\in[0,T)} corresponds to f0𝒮f_{0}\in\mathcal{S} in Sn×[1,1]S^{n}\times[-1,1] can be interpreted as a mean curvature flow with additional force in n+2\mathbb{R}^{n+2}. We refer the readers to [HZ23] for some properties of mean curvature flow with additional force. In particular, by the classification of rotationally symmetric self-shrinkers, the tangent flow at the singular point of M0(t)M^{0}(t) is modeled by a cylinder Sn1(2(n1))×S^{n-1}(\sqrt{2(n-1)})\times\mathbb{R}. That says, if we dilate the half-space by Tt\sqrt{T-t}, then for any R>0R>0, the profile curve of M0(t)M^{0}(t) will converge to the straight line {x=2(n1)}\{x=\sqrt{2(n-1)}\} as tTt\to T in BRB_{R}.

By the smooth dependence of the initial data, for any t0(0,T)t_{0}\in(0,T), if f1𝒮f_{1}\in\mathcal{S} is sufficiently close to f0f_{0} in C1C^{1}, then the mean curvature flow M1(t)M^{1}(t) will be very close to M0(t)M^{0}(t) on [0,t0][0,t_{0}], in particular, also very close to the straight line {x=2(n1)}\{x=\sqrt{2(n-1)}\} in BRB_{R}. Then using the appropriate dilation of the λ\lambda-Angenent curve as a barrier, we see that M1(t)M^{1}(t) can only have singularity on the rotation axis. This shows the openness of \mathscr{L}. ∎

3.2. Interpolation family of hypersurfaces

In this section, we construct an immortal flow using the interpolation argument. By Lemma 2.2, there exists C1(0,π2)C_{1}\in(0,\frac{\pi}{2}) such that YC1=2nY_{C_{1}}=\frac{2}{n}. Then for the spherical catenoid constructed in Section 2.2 with parameter C1C_{1}, the restriction of its profile curve onto the region DD has a connected segment that joins the head point (C1,0)(C_{1},0) and (π2,1n)(\frac{\pi}{2},\frac{1}{n}). We denote this segment of the profile curve by 𝒞\mathcal{C}.

Next, we introduce two constants α,β\alpha,\beta. The λ\lambda-Angenent curve is constructed in Appendix B, we will let λ=(n1)2\lambda=\frac{(n-1)}{2} in the following. We can choose a constant α(0,C14)\alpha\in(0,\frac{C_{1}}{4}) and dilate the λ\lambda-Angenent curve such that the upper half of the dilated λ\lambda-Angenent curve is contained in the region (2α,π4)×[0,12n](2\alpha,\frac{\pi}{4})\times[0,\frac{1}{2n}], and we denote this segment of curve as 𝒜\mathcal{A}, and let T0T_{0} be the time at which 𝒜\mathcal{A} collapses to a point under mean curvature flow. We choose a constant β(C1,π2)\beta\in(C_{1},\frac{\pi}{2}) such that 𝒞\mathcal{C} is on top of the curve {(β,y)|y[0,12n]}{(x,12n)|x[β,π2]}\{(\beta,y)|y\in[0,\frac{1}{2n}]\}\cup\{(x,\frac{1}{2n})|x\in[\beta,\frac{\pi}{2}]\}.

We consider a family of initial data {ρδ}δ(0,π2)\{\rho_{\delta}\}_{\delta\in(0,\frac{\pi}{2})} that forms a smooth foliation of a subset of the region DD. ρδ\rho_{\delta} is the graph of an increasing smooth function fδ(x)f_{\delta}(x) with vertical graph function uδ(y)u_{\delta}(y) and horizontal graph function vδ(x)v_{\delta}(x). After reflecting ρδ\rho_{\delta} with respect to the lines {x=π2}\{x=\frac{\pi}{2}\} and {y=0}\{y=0\}, we get a smooth curve in [0,π]×[1,1][0,\pi]\times[-1,1], in other word, all odd order derivatives of uδu_{\delta} at 0 and vδv_{\delta} at π2\frac{\pi}{2} vanish. ρδ\rho_{\delta} also has the following properties:

(3.5) fδ is defined on the interval [δ,π2], and fδ(δ)=0.f_{\delta}\text{ is defined on the interval }[\delta,\frac{\pi}{2}],\text{ and }f_{\delta}(\delta)=0.
(3.6) ρα ends at (π2,12n), and ρα is on top of 𝒜.\rho_{\alpha}\text{ ends at }(\frac{\pi}{2},\frac{1}{2n}),\text{ and }\rho_{\alpha}\text{ is on top of }\mathcal{A}.
(π2,0)(\frac{\pi}{2},0)(0,1)(0,1)(0,0)(0,0)(π2,1)(\frac{\pi}{2},1)(α,0)(\alpha,0)(π2,12n)(\frac{\pi}{2},\frac{1}{2n})(δ,0)(\delta,0)(β,0)(\beta,0)ρα\rho_{\alpha}ρδ\rho_{\delta}ρβ\rho_{\beta}
Figure 2. The family of interpolation curves.

By property (3.5) and the fact that {ρδ}δ(0,π2)\{\rho_{\delta}\}_{\delta\in(0,\frac{\pi}{2})} forms a foliation, we know for δ>α\delta>\alpha, the curve ρα\rho_{\alpha} is on top of ρδ\rho_{\delta}. By property (3.6), the height of ρα\rho_{\alpha} is 12n\frac{1}{2n}, since β>α\beta>\alpha, thus the height of ρβ\rho_{\beta} is at most 12n\frac{1}{2n}. Therefore by property (3.5) and the choice of β\beta, 𝒞\mathcal{C} is on top of ρβ\rho_{\beta}.

Let fδ(,t)f_{\delta}(\cdot,t) be the family of solutions to the equation (2.2) with initial data fδ(x)f_{\delta}(x). Denote the vertical graph function and the horizontal graph function of fδ(,t)f_{\delta}(\cdot,t) by uδ(,t),vδ(,t)u_{\delta}(\cdot,t),v_{\delta}(\cdot,t).

Lemma 3.10.

Given δ>α\delta>\alpha, if limtTuδ(0,t)=0\lim\limits_{t\to T}u_{\delta}(0,t)=0, then uδ(0,t)βu_{\delta}(0,t)\leq\beta for all time before the singularity occurs.

Proof.

Since δ>α\delta>\alpha, we know the height of ρδ\rho_{\delta} is less than 12n\frac{1}{2n}. By Lemma 3.2, we know fδ(,t)12nf_{\delta}(\cdot,t)\leq\frac{1}{2n} for all time tt.

If uδ(0,t1)>βu_{\delta}(0,t_{1})>\beta at some time t1t_{1} before the singularity occurs, then by the choice of β\beta, 𝒞\mathcal{C} is on top of the graph of fδ(,t1)f_{\delta}(\cdot,t_{1}). Then by Theorem 2.1, 𝒞\mathcal{C} is on top of the graph of fδ(,t)f_{\delta}(\cdot,t) for all time t>t1t>t_{1}, which implies that uδ(0,t)>C1u_{\delta}(0,t)>C_{1} for all t>t1t>t_{1}. We get a contradiction with the assumption limtTuδ(0,t)=0\lim\limits_{t\to T}u_{\delta}(0,t)=0.

We are now ready to prove the existence of an immortal flow on Sn×[1,1]S^{n}\times[-1,1]. We first sketch the picture of the two main comparison results that are used to apply the interpolation argument, See Figure 3. We compare the family of initial data ρδ\rho_{\delta} to the curves 𝒜\mathcal{A} and 𝒞\mathcal{C}. The head point of the initial curve in the first picture will tend to 0 in finite time, meanwhile, the initial curve in the second picture will remain C1C_{1} away from 0 before the singular time.

Refer to caption
Figure 3. The blue curves are the flows that we want to study. The red curve on the left represents one λ\lambda-Angenent curve; the purple curve on the right represents one spherical catenoid.
Theorem 3.11.

There exists an immortal nonstatic rotationally symmetric mean curvature flow of hypersurfaces in Sn×[1,1]S^{n}\times[-1,1].

Proof.

For δα\delta\leq\alpha, we know that the curve ρδ\rho_{\delta} is on top of 𝒜\mathcal{A}. We restricted the curve ρδ\rho_{\delta} and 𝒜\mathcal{A} onto the region [0,π4]×[0,1][0,\frac{\pi}{4}]\times[0,1], and view these two segments as the graph of a function of yy. In this region, the function value is bounded above by π4\frac{\pi}{4}, thus

uyy1+(uy)2(n1)cos(u)sin(u)uyy1+(uy)2(n1)21u.\frac{u_{yy}}{1+(u_{y})^{2}}-(n-1)\frac{\cos(u)}{\sin(u)}\leq\frac{u_{yy}}{1+(u_{y})^{2}}-\frac{(n-1)}{2}\frac{1}{u}.

Hence T0t𝒜\sqrt{T_{0}-t}\mathcal{A} (i.e., the solution to (B.2) with initial condition 𝒜\mathcal{A}) is a supersolution to the vertical graph equation, and initially 𝒜\mathcal{A} is on top of the curve ρδ\rho_{\delta}. By maximum principle, T0t𝒜\sqrt{T_{0}-t}\mathcal{A} remains on top of the graph of uδ(,t)u_{\delta}(\cdot,t) for all time t>0t>0. The head point of the λ\lambda-Angenent curve T0t𝒜\sqrt{T_{0}-t}\mathcal{A} tends to 0 in finite time T0T_{0}, which forces uδ(0,t)0u_{\delta}(0,t)\to 0 at some time t<T0t<T_{0}. By Proposition 2.1, if uδ(0,t)0u_{\delta}(0,t)\to 0 in finite time, then uδ(0,t)0u_{\delta^{\prime}}(0,t)\to 0 in finite time for all 0<δ<δ0<\delta^{\prime}<\delta.

For βδ<π2\beta\leq\delta<\frac{\pi}{2}, 𝒞\mathcal{C} is on top of the curve ρδ\rho_{\delta}. By Proposition 2.1, 𝒞\mathcal{C} is on top of the graph of fδ(,t)f_{\delta}(\cdot,t) for all time tt, which implies uδ(0,t)βu_{\delta}(0,t)\geq\beta for all tt.

Hence, by continuous dependence of the initial data (see e.g. [Ama88]) and Proposition 3.9, there exists a maximal interval (0,η)(0,\eta) such that for any δ\delta within this interval, uδ(0,t)u_{\delta}(0,t) converges to 0 in finite time. As indicated in the preceding argument, α<ηβ\alpha<\eta\leq\beta. By Proposition 2.1 and Proposition 3.8, the singular time T(ρδ)T(\rho_{\delta}) is strictly increasing in δ(0,η)\delta\in(0,\eta), and its limit as δη\delta\to\eta has to be \infty, otherwise uη(0,t)u_{\eta}(0,t) will converge to 0 in finite time by the continuous dependence. By the selection of η\eta, uη(0,t)u_{\eta}(0,t) never reaches 0 in finite time. Combining this with Lemma 3.10, we conclude that for δ(α,η)\delta\in(\alpha,\eta) and t[0,T(ρδ))t\in[0,T(\rho_{\delta})), we have uδ(0,t)βu_{\delta}(0,t)\leq\beta. By continuous dependence and the fact that limδηT(ρδ)=\lim\limits_{\delta\to\eta}T(\rho_{\delta})=\infty, we can deduce that uη(0,t)βu_{\eta}(0,t)\leq\beta for all tt.

As a result, uη(0,t)u_{\eta}(0,t) does not converge to either 0 or π2\frac{\pi}{2} within any finite time, by Proposition 3.8, the solutions uη(,t)u_{\eta}(\cdot,t) and vη(,t)v_{\eta}(\cdot,t) exist for all time t[0,)t\in[0,\infty).

3.3. Multiplicity 22 convergence

From the construction above, we know that the solution fη(,t)f_{\eta}(\cdot,t) to the equation (2.2) exists for all time t[0,)t\in[0,\infty). In the following, we will show the mean curvature flow induced from fη(,t)f_{\eta}(\cdot,t) will converge to the minimal sphere Sn×{0}S^{n}\times\{0\} with multiplicity 22. In fact, outside a neighborhood of the north pole and south pole of Sn×{0}S^{n}\times\{0\}, we can show the mean curvature flow has two connected components, and each component converges to Sn×{0}S^{n}\times\{0\} outside a neighborhood of the north pole and south pole smoothly.

By a similar height decreasing argument as in [CS23, Lemma 3.15], we show that the head point of the function fηf_{\eta} converges to 0 as tt\to\infty, i.e. limtuη(0,t)=0\lim\limits_{t\to\infty}u_{\eta}(0,t)=0. We can also use c𝒜c\mathcal{A} as a barrier to obtain a linear upper bound of the function fηf_{\eta}.

Lemma 3.12.

fη(x,t)<14nαxf_{\eta}(x,t)<\frac{1}{4n\alpha}x for all t[0,)t\in[0,\infty) and x(uη(0,t),4α]x\in(u_{\eta}(0,t),4\alpha].

Proof.

We prove this by contradiction. Suppose not, then fη(x0,t)14nαx0f_{\eta}(x_{0},t)\geq\frac{1}{4n\alpha}x_{0} for some t[0,)t\in[0,\infty), x0(uη(0,t),4α]x_{0}\in(u_{\eta}(0,t),4\alpha], then the graph of fη(,t)f_{\eta}(\cdot,t) is on top of the dilated λ\lambda-Angenent curve x02α𝒜\frac{x_{0}}{2\alpha}\mathcal{A}, which implies that fηf_{\eta} has a finite time singularities. This is a contradiction. ∎

We are ready to prove the key long-time gradient estimate of fηf_{\eta}.

Proposition 3.13.

Given 0<a<b<π40<a<b<\frac{\pi}{4}, for any 0<ϵ1<1ln(tanb2)ln(tana2)0<\epsilon_{1}<1-\frac{\ln(\tan\frac{b}{2})}{\ln(\tan\frac{a}{2})}, there exist a constant ω\omega depending on a,ϵ1a,\epsilon_{1}, and a time T1T_{1} depending on a,b,ϵ1a,b,\epsilon_{1}, such that

xfη(x,t)tan(πln(tanb2)2ln(tan(a2))+ωcosblnt+ϵ1),\frac{\partial}{\partial x}f_{\eta}(x,t)\leq\tan\left(\frac{\pi\ln(\tan\frac{b}{2})}{2\ln(\tan(\frac{a}{2}))}+\frac{\omega\cos b}{\ln t}+\epsilon_{1}\right),

for all x[b,π2]x\in[b,\frac{\pi}{2}], tT1t\geq T_{1}. In addition, limtfη(π2,t)fη(b,t)=0\lim\limits_{t\to\infty}f_{\eta}(\frac{\pi}{2},t)-f_{\eta}(b,t)=0.

Proof.

Given any 0<a<b<π40<a<b<\frac{\pi}{4}. Since limtuη(0,t)=0\lim\limits_{t\to\infty}u_{\eta}(0,t)=0, we know that there exists T>10T>10 such that for any tTt\geq T, uη(0,t)<a2u_{\eta}(0,t)<\frac{a}{2}. Then fη(x,t)f_{\eta}(x,t) is a smooth function over [a,π2][a,\frac{\pi}{2}] for all tTt\geq T. For simplicity, we will use f(x,t)f(x,t) to express the function fη(x,t)f_{\eta}(x,t) restricted on the interval [a,R][a,R], which is smooth for all time tTt\geq T. We know

ft=fxx1+fx2+(n1)cosxsinxfx,fx>0 for all x[a,π2).\displaystyle f_{t}=\frac{f_{xx}}{1+f_{x}^{2}}+(n-1)\frac{\cos x}{\sin x}f_{x},\qquad f_{x}>0\text{ for all }x\in[a,\frac{\pi}{2}).

Let ϕ(x,t)=arctan(fx(x,t))\phi(x,t)=\arctan(f_{x}(x,t)), x[a,π2]x\in[a,\frac{\pi}{2}], t[T,)t\in[T,\infty). Then 0ϕ(x,t)<π20\leq\phi(x,t)<\frac{\pi}{2}, and fx(x,t)=tan(ϕ(x,t))f_{x}(x,t)=\tan(\phi(x,t)). Then

ϕx(x,t)=fxx(x,t)1+fx2(x,t),ft=ϕx+(n1)cosxsinxfx.\displaystyle\phi_{x}(x,t)=\frac{f_{xx}(x,t)}{1+f_{x}^{2}(x,t)},\qquad f_{t}=\phi_{x}+(n-1)\frac{\cos x}{\sin x}f_{x}.

Moreover,

ϕt=11+fx2(fx)t=11+fx2(ft)x=11+fx2(ϕxx+(n1)cosxsinxfxx(n1)fxsin2x).\phi_{t}=\frac{1}{1+f_{x}^{2}}(f_{x})_{t}=\frac{1}{1+f_{x}^{2}}(f_{t})_{x}=\frac{1}{1+f_{x}^{2}}(\phi_{xx}+(n-1)\frac{\cos x}{\sin x}f_{xx}-(n-1)\frac{f_{x}}{\sin^{2}x}).

Therefore,

(3.7) ϕt(n1)cosxsinxϕx11+fx2ϕxx=(n1)fxsin2x(1+fx2)<0.\phi_{t}-(n-1)\frac{\cos x}{\sin x}\phi_{x}-\frac{1}{1+f_{x}^{2}}\phi_{xx}=-(n-1)\frac{f_{x}}{\sin^{2}x(1+f_{x}^{2})}<0.

Let μ=π2ln(tan(a2))\mu=-\frac{\pi}{2\ln(\tan(\frac{a}{2}))} and ω\omega be a positive constant to be determined later. Define φ(x,t)=μln(tanx2)+ωcosxlnt+ϵ1\varphi(x,t)=-\mu\ln(\tan\frac{x}{2})+\frac{\omega\cos x}{\ln t}+\epsilon_{1}. Then for x[a,π2]x\in[a,\frac{\pi}{2}], tTt\geq T, we have

φx=μsinxωsinxlnt<0,φxx=μcosxsin2xωcosxlnt.\varphi_{x}=-\frac{\mu}{\sin x}-\frac{\omega\sin x}{\ln t}<0,\quad\varphi_{xx}=\frac{\mu\cos x}{\sin^{2}x}-\frac{\omega\cos x}{\ln t}.

Then

If φxx0,\displaystyle\text{If }\varphi_{xx}\geq 0, φt(n1)cosxsinxφxφxx1+fx2φt(n1)cosxsinxφxφxx\displaystyle\varphi_{t}-(n-1)\frac{\cos x}{\sin x}\varphi_{x}-\frac{\varphi_{xx}}{1+f_{x}^{2}}\geq\varphi_{t}-(n-1)\frac{\cos x}{\sin x}\varphi_{x}-\varphi_{xx}
ωcosxt(lnt)2+(n1)μcosxsin2x+(n1)ωcosxlntμcosxsin2x+ωcosxlnt\displaystyle\geq\frac{-\omega\cos x}{t(\ln t)^{2}}+\frac{(n-1)\mu\cos x}{\sin^{2}x}+\frac{(n-1)\omega\cos x}{\ln t}-\frac{\mu\cos x}{\sin^{2}x}+\frac{\omega\cos x}{\ln t}
=(n2)μcosxsin2x+ωcosxlnt(n1tlnt)0.\displaystyle=(n-2)\frac{\mu\cos x}{\sin^{2}x}+\frac{\omega\cos x}{\ln t}(n-\frac{1}{t\ln t})\geq 0.
If φxx<0,\displaystyle\text{If }\varphi_{xx}<0, φt(n1)cosxsinxφxφxx1+fx2φt(n1)cosxsinxφx\displaystyle\varphi_{t}-(n-1)\frac{\cos x}{\sin x}\varphi_{x}-\frac{\varphi_{xx}}{1+f_{x}^{2}}\geq\varphi_{t}-(n-1)\frac{\cos x}{\sin x}\varphi_{x}
ωcosxt(lnt)2+(n1)μcosxsin2x+(n1)ωcosxlnt\displaystyle\geq\frac{-\omega\cos x}{t(\ln t)^{2}}+\frac{(n-1)\mu\cos x}{\sin^{2}x}+\frac{(n-1)\omega\cos x}{\ln t}
=(n1)μcosxsin2x+ωcosxlnt(n11tlnt)0.\displaystyle=(n-1)\frac{\mu\cos x}{\sin^{2}x}+\frac{\omega\cos x}{\ln t}(n-1-\frac{1}{t\ln t})\geq 0.

Since fx(π2,T)=0f_{x}(\frac{\pi}{2},T)=0, we have ϕ(π2,T)=0\phi(\frac{\pi}{2},T)=0, and there exists 0<δ<π40<\delta<\frac{\pi}{4} such that ϕ(x,T)<ϵ1\phi(x,T)<\epsilon_{1} for all x[π2δ,π2]x\in[\frac{\pi}{2}-\delta,\frac{\pi}{2}]. Let ω=πlnT2sinδ\omega=\frac{\pi\ln T}{2\sin\delta}, then for x[π2δ,π2]x\in[\frac{\pi}{2}-\delta,\frac{\pi}{2}], φ(x,T)ϵ1>ϕ(x,T)\varphi(x,T)\geq\epsilon_{1}>\phi(x,T); for x[a,π2δ)x\in[a,\frac{\pi}{2}-\delta), φ(x,T)ωcosxlnTπ2ϕ(x,T)\varphi(x,T)\geq\frac{\omega\cos x}{\ln T}\geq\frac{\pi}{2}\geq\phi(x,T).

Thus

φ(x,T)ϕ(x,T),φt(n1)cosxsinxφxφxx1+fx20>ϕt(n1)cosxsinxϕxϕxx1+fx2,φ(a,t)μln(tana2)π2ϕ(a,t),φ(π2,t)>0=ϕ(π2,t).\displaystyle\begin{aligned} &\varphi(x,T)\geq\phi(x,T),\\ &\varphi_{t}-(n-1)\frac{\cos x}{\sin x}\varphi_{x}-\frac{\varphi_{xx}}{1+f_{x}^{2}}\geq 0>\phi_{t}-(n-1)\frac{\cos x}{\sin x}\phi_{x}-\frac{\phi_{xx}}{1+f_{x}^{2}},\\ &\varphi(a,t)\geq-\mu\ln(\tan\frac{a}{2})\geq\frac{\pi}{2}\geq\phi(a,t),\\ &\varphi(\frac{\pi}{2},t)>0=\phi(\frac{\pi}{2},t).\end{aligned}

Now we can apply the parabolic maximum principle to conclude that φ(x,t)ϕ(x,t)\varphi(x,t)\geq\phi(x,t) for all x[a,π2]x\in[a,\frac{\pi}{2}] and tT1t\geq T_{1}. On the other hand, for any x[b,π2]x\in[b,\frac{\pi}{2}],

φ(x,t)φ(b,t)=πln(tanb2)2ln(tana2)+ωcosblnt+ϵ1.\varphi(x,t)\leq\varphi(b,t)=\frac{\pi\ln(\tan\frac{b}{2})}{2\ln(\tan\frac{a}{2})}+\frac{\omega\cos b}{\ln t}+\epsilon_{1}.

Thus there exists T1>TT_{1}>T such that for all x[b,π2]x\in[b,\frac{\pi}{2}] and tT1t\geq T_{1}, φ(x,t)<π2\varphi(x,t)<\frac{\pi}{2}. In summary, for x[b,π2]x\in[b,\frac{\pi}{2}], tT1t\geq T_{1}, we have the gradient estimate

(3.8) fx(x,t)=tan(ϕ(x,t))tan(φ(x,t))tan(πln(tanb2)2ln(tan(a2))+ωcosblnt+ϵ1).f_{x}(x,t)=\tan(\phi(x,t))\leq\tan(\varphi(x,t))\leq\tan\left(\frac{\pi\ln(\tan\frac{b}{2})}{2\ln(\tan(\frac{a}{2}))}+\frac{\omega\cos b}{\ln t}+\epsilon_{1}\right).

Next, integrating this gradient bound yields

f(π2,t)f(b,t)=bπ2fx(x,t)𝑑x(π2b)tan(πln(tanb2)2ln(tan(a2))+ωcosblnt+ϵ1).f(\frac{\pi}{2},t)-f(b,t)=\int_{b}^{\frac{\pi}{2}}f_{x}(x,t)dx\leq(\frac{\pi}{2}-b)\tan\left(\frac{\pi\ln(\tan\frac{b}{2})}{2\ln(\tan(\frac{a}{2}))}+\frac{\omega\cos b}{\ln t}+\epsilon_{1}\right).

Let tt\to\infty,

0lim supt[f(π2,t)f(b,t)](π2b)tan(πln(tanb2)2ln(tan(a2))+ϵ1).\displaystyle 0\leq\limsup\limits_{t\to\infty}[f(\frac{\pi}{2},t)-f(b,t)]\leq(\frac{\pi}{2}-b)\tan\left(\frac{\pi\ln(\tan\frac{b}{2})}{2\ln(\tan(\frac{a}{2}))}+\epsilon_{1}\right).

Let a0a\to 0,

0lim supt[f(π2,t)f(b,t)](π2b)tanϵ1.\displaystyle 0\leq\limsup\limits_{t\to\infty}[f(\frac{\pi}{2},t)-f(b,t)]\leq(\frac{\pi}{2}-b)\tan\epsilon_{1}.

Since ϵ1\epsilon_{1} can be chosen arbitrarily small, we have limt[f(π2,t)f(b,t)]=0\lim\limits_{t\to\infty}[f(\frac{\pi}{2},t)-f(b,t)]=0.

The gradient estimate yields the following two corollaries, which can be combined to show that fη(x,t)f_{\eta}(x,t) will C1C^{1} converge to 0.

Corollary 3.14.

fη(x,t)f_{\eta}(x,t) converges to 0 uniformly as tt\to\infty, for all x(0,π2]x\in(0,\frac{\pi}{2}].

Proof.

By Lemma 3.2, we know limtfη(π2,t)\lim\limits_{t\to\infty}f_{\eta}(\frac{\pi}{2},t) exists. By Lemma 3.12, Proposition 3.13, for any 0<b4α0<b\leq 4\alpha,

0limtfη(π2,t)=limtfη(b,t)b4nα.\displaystyle 0\leq\lim\limits_{t\to\infty}f_{\eta}(\frac{\pi}{2},t)=\lim\limits_{t\to\infty}f_{\eta}(b,t)\leq\frac{b}{4n\alpha}.

Let b0b\to 0, we get limtfη(π2,t)=0\lim\limits_{t\to\infty}f_{\eta}(\frac{\pi}{2},t)=0. Since fη(,t)f_{\eta}(\cdot,t) is a strictly increasing function, thus fη(x,t)f_{\eta}(x,t) converges to 0 as tt\to\infty and this convergence is uniform in xx.

Corollary 3.15.

Given 0<b<π20<b<\frac{\pi}{2}, xfη(x,t)\frac{\partial}{\partial x}f_{\eta}(x,t) converges to 0 uniformly as tt\to\infty, for all x[b,π2]x\in[b,\frac{\pi}{2}].

Proof.

For any ϵ>0\epsilon>0, there exists 0<a<b,0<a<b, and 0<ϵ1<1ln(tanb2)ln(tana2)0<\epsilon_{1}<1-\frac{\ln(\tan\frac{b}{2})}{\ln(\tan\frac{a}{2})} such that πln(tanb2)2ln(tan(a2))<ϵ3\frac{\pi\ln(\tan\frac{b}{2})}{2\ln(\tan(\frac{a}{2}))}<\frac{\epsilon}{3}, and ϵ1<ϵ3\epsilon_{1}<\frac{\epsilon}{3}. Let ω\omega, T1T_{1} be as determined in Proposition 3.13. Then there exists TT1T^{\prime}\geq T_{1} such that for tTt\geq T^{\prime}, ωcosblnt<ϵ3\frac{\omega\cos b}{\ln t}<\frac{\epsilon}{3}. By Proposition 3.13, for x[b,π2]x\in[b,\frac{\pi}{2}], tTt\geq T^{\prime},

xfη(x,t)tan(πln(tanb2)2ln(tan(a2))+ωcosblnt+ϵ1)<tanϵ.\displaystyle\frac{\partial}{\partial x}f_{\eta}(x,t)\leq\tan\left(\frac{\pi\ln(\tan\frac{b}{2})}{2\ln(\tan(\frac{a}{2}))}+\frac{\omega\cos b}{\ln t}+\epsilon_{1}\right)<\tan\epsilon.

Let M(t)M(t) denote the desired hypersurface with the graph of fη(x,t)f_{\eta}(x,t) as its section curve.

Theorem 3.16.

(M(t))t[0,)(M(t))_{t\in[0,\infty)} is an immortal mean curvature flow on Sn×[1,1]S^{n}\times[-1,1], and the forward limit of this flow is the minimal sphere Sn×{0}S^{n}\times\{0\} with multiplicity 22.

Proof.

Following from the proof of Theorem 3.11, we only need to prove that for any ϵ>0\epsilon>0, fη(x,t)|x[ϵ,π2]f_{\eta}(x,t)|_{x\in[\epsilon,\frac{\pi}{2}]} converges to 0 in C1C^{1}. Given ϵ>0\epsilon>0, we know that there exists T>0T>0 such that uη(0,t)<ϵu_{\eta}(0,t)<\epsilon for tTt\geq T. So fη(x,t)|[ϵ,R]f_{\eta}(x,t)|_{[\epsilon,R]} is well defined for all tTt\geq T. By Lemma 3.12, fη(,t)|[0,ϵ]f_{\eta}(\cdot,t)|_{[0,\epsilon]} is contained in the rectangle [0,ϵ]×[0,ϵ4nα][0,\epsilon]\times[0,\frac{\epsilon}{4n\alpha}] for tTt\geq T. By Corollary 3.14 and 3.15, we know fη(,t)|[ϵ,π2]f_{\eta}(\cdot,t)|_{[\epsilon,\frac{\pi}{2}]} C1C^{1} converges to 0 as tt\to\infty. This completes the proof.

Appendix A Curves in the plane with conformal metrics

Given a C2C^{2} function ϕ(x,y)\phi(x,y) defined on an open subset UU of the plane, let us consider the metric gϕ=e2ϕ(dx2+dy2)g_{\phi}=e^{2\phi}(dx^{2}+dy^{2}), and the corresponding Levi-Civita connection \nabla. We present some computations related to curves in (U,gϕ)(U,g_{\phi}) in this section.

By standard calculations, we can write down the Christoffel symbols:

Γxxx=xϕ,Γxxy=yϕ,Γxyx=yϕ,Γxyy=xϕ,Γyyx=xϕ,Γyyy=yϕ.\displaystyle\Gamma_{xx}^{x}=\partial_{x}\phi,\quad\Gamma_{xx}^{y}=-\partial_{y}\phi,\quad\Gamma_{xy}^{x}=\partial_{y}\phi,\quad\Gamma_{xy}^{y}=\partial_{x}\phi,\quad\Gamma_{yy}^{x}=-\partial_{x}\phi,\quad\Gamma_{yy}^{y}=\partial_{y}\phi.

Suppose γ:IU\gamma:I\to U is a C2C^{2}-curve, where II can be an interval or S1S^{1}. We consider the coordinate expression γ(s)=(x(s),y(s))\gamma(s)=(x(s),y(s)). Then γ(s)=xx+yy\gamma^{\prime}(s)=x^{\prime}\partial_{x}+y^{\prime}\partial_{y} and the length \ell of γ\gamma^{\prime} is eϕ(x)2+(y)2e^{\phi}\sqrt{(x^{\prime})^{2}+(y^{\prime})^{2}}. Let Es=1γE_{s}=\ell^{-1}\gamma^{\prime}. Then the geodesic curvature vector of γ\gamma is given by

(A.1) (EsEs)=2(x′′x+y′′y)+2(s)(γ)+2((x)2xx+xyxy+xyyx+(y)2yy)=(2x′′+2((x)2(y)2)xϕ+22xyyϕ)x+(2y′′+2((y)2(x)2)yϕ+22xyxϕ)y.\begin{split}(\nabla_{E_{s}}E_{s})^{\perp}=&\ell^{-2}(x^{\prime\prime}\partial_{x}+y^{\prime\prime}\partial_{y})^{\perp}+\ell^{-2}(\partial_{s}\ell)(\gamma^{\prime})^{\perp}\\ &+\ell^{-2}((x^{\prime})^{2}\nabla_{\partial_{x}}\partial_{x}+x^{\prime}y^{\prime}\nabla_{\partial_{x}}\partial_{y}+x^{\prime}y^{\prime}\nabla_{\partial_{y}}\partial_{x}+(y^{\prime})^{2}\nabla_{\partial_{y}}\partial_{y})^{\perp}\\ =&(\ell^{-2}x^{\prime\prime}+\ell^{-2}((x^{\prime})^{2}-(y^{\prime})^{2})\partial_{x}\phi+2\ell^{-2}x^{\prime}y^{\prime}\partial_{y}\phi)\partial_{x}^{\perp}\\ &+(\ell^{-2}y^{\prime\prime}+\ell^{-2}((y^{\prime})^{2}-(x^{\prime})^{2})\partial_{y}\phi+2\ell^{-2}x^{\prime}y^{\prime}\partial_{x}\phi)\partial_{y}^{\perp}.\end{split}

Choose the unit normal vector field 𝐧ϕ=1(yx+xy)=eϕ𝐧\mathbf{n}_{\phi}=\ell^{-1}(-y^{\prime}\partial_{x}+x^{\prime}\partial_{y})=e^{-\phi}\mathbf{n}, where 𝐧\mathbf{n} is the normal vector of the curve in the Euclidean metric. This implies that

x=1ye2ϕ𝐧ϕ,y=1xe2ϕ𝐧ϕ.\partial_{x}^{\perp}=-\ell^{-1}y^{\prime}e^{2\phi}\mathbf{n}_{\phi},\quad\partial_{y}^{\perp}=\ell^{-1}x^{\prime}e^{2\phi}\mathbf{n}_{\phi}.

Therefore, the curvature vector κϕ\vec{\kappa}_{\phi} is given by

(A.2) κϕ=((2x′′+2((x)2(y)2)xϕ+22xyyϕ)1ye2ϕ+(2y′′+2((y)2(x)2)yϕ+22xyxϕ)1xe2ϕ)𝐧ϕ=(3(xy′′x′′y)+e2ϕ1(yxϕxyϕ))e2ϕ𝐧ϕ.\begin{split}\vec{\kappa}_{\phi}=&(-(\ell^{-2}x^{\prime\prime}+\ell^{-2}((x^{\prime})^{2}-(y^{\prime})^{2})\partial_{x}\phi+2\ell^{-2}x^{\prime}y^{\prime}\partial_{y}\phi)\ell^{-1}y^{\prime}e^{2\phi}\\ &+(\ell^{-2}y^{\prime\prime}+\ell^{-2}((y^{\prime})^{2}-(x^{\prime})^{2})\partial_{y}\phi+2\ell^{-2}x^{\prime}y^{\prime}\partial_{x}\phi)\ell^{-1}x^{\prime}e^{2\phi})\mathbf{n}_{\phi}\\ =&(\ell^{-3}(x^{\prime}y^{\prime\prime}-x^{\prime\prime}y^{\prime})+e^{-2\phi}\ell^{-1}(y^{\prime}\partial_{x}\phi-x^{\prime}\partial_{y}\phi))e^{2\phi}\mathbf{n}_{\phi}.\end{split}

Note that we can interpret this as

(A.3) κϕ=eϕ(κ+ϕ),\kappa_{\phi}=e^{-\phi}(\vec{\kappa}+\nabla^{\perp}\phi),

where κ\vec{\kappa} and \nabla^{\perp} are the curvature and normal projection of the gradient of the curve under the Euclidean metric respectively.

Example A.1.

Consider ϕ=f(x)\phi=f(x) only depending on xx. Suppose f(x)f(x) is chosen such that the curves in (U,gf)(U,g_{f}) give the area of the hypersurface that is rotating the curve in some Riemannian manifold, for example, f(x)=(n1)logxf(x)=(n-1)\log x (gives the area of rotationally symmetric hypersurfaces in n+1\mathbb{R}^{n+1}) or f(x)=(n1)logsinxf(x)=(n-1)\log\sin x (gives the area of rotationally symmetric hypersurfaces in Sn×S^{n}\times\mathbb{R}). Suppose the curve is γ\gamma.

After taking the quotient of SO(n1)SO(n-1) action, we identify the mean curvature vector as h\vec{h}, and the unit normal vector as 𝐧\mathbf{n}. Then from the first variational formula, we have 𝐡=e2fκf\vec{\mathbf{h}}=e^{-2f}\vec{\kappa}_{f}, and 𝐧f=ef𝐧\mathbf{n}_{f}=e^{-f}\mathbf{n}. After taking the quotient of the mean curvature flow of the hypersurfaces, the profile curves satisfy the equation

(A.4) tγ,𝐧Euc=𝐡.\langle\partial_{t}\gamma,\mathbf{n}\rangle_{\text{Euc}}=\vec{\mathbf{h}}.

Under the conformal metric, this can be expressed as

(A.5) tγ,𝐧fg𝐧f=e2fκf\langle\partial_{t}\gamma,\mathbf{n}_{f}\rangle_{g}\mathbf{n}_{f}=e^{-2f}\vec{\kappa}_{f}

Notice that this curvature flow is different from the curve shortening flow under the metric gg up to the conformal factor.

Now we derive the equation of the graphs under this flow. Suppose γ(x,t)=(x,v(x,t))\gamma(x,t)=(x,v(x,t)), we obtain that

(A.6) vt1x𝐧f=(3(xy′′x′′y)+e2f1yxf)e2f𝐧f\begin{split}v_{t}\ell^{-1}x^{\prime}\mathbf{n}_{f}=(\ell^{-3}(x^{\prime}y^{\prime\prime}-x^{\prime\prime}y^{\prime})+e^{-2f}\ell^{-1}y^{\prime}\partial_{x}f)e^{2f}\mathbf{n}_{f}\end{split}

Plugging in x=1x^{\prime}=1, x′′=0x^{\prime\prime}=0, y=vxy^{\prime}=v_{x}, y′′=vxxy^{\prime\prime}=v_{xx} gives

(A.7) vt=vxx1+(vx)2+fxvx.v_{t}=\frac{v_{xx}}{1+(v_{x})^{2}}+f_{x}v_{x}.

Similarly, suppose γ(y,t)=(u(y,t),y)\gamma(y,t)=(u(y,t),y), we have

(A.8) ut=uyy1+(uy)2fx(u).u_{t}=\frac{u_{yy}}{1+(u_{y})^{2}}-f_{x}(u).

Appendix B λ\lambda-Angenent curves

Let λ>0\lambda>0. Consider the metric gϕ=e2ϕ(dx2+dy2)g_{\phi}=e^{2\phi}(dx^{2}+dy^{2}) with ϕ(x,y)=λlogx(x2+y2)/4\phi(x,y)=\lambda\log x-(x^{2}+y^{2})/4, defined on the right half plane {(x,y):x>0}\{(x,y):x>0\}. We call a closed embedded geodesic under the metric e2ϕ(dx2+dy2)e^{2\phi}(dx^{2}+dy^{2}) a λ\lambda-Angenent curve. When λ=(n1)\lambda=(n-1), rotating the curves by SO(n1)SO(n-1) action gives the Angenent doughnut in n+1\mathbb{R}^{n+1}.

Suppose γ¯(s)=(x(s),y(s))\bar{\gamma}(s)=(x(s),y(s)) is a λ\lambda-Angenent curve. Let

γ(s,t)=tγ¯(s)=(tx(s),ty(s))\gamma(s,t)=\sqrt{-t}\bar{\gamma}(s)=(\sqrt{-t}x(s),\sqrt{-t}y(s))

for t<0t<0. Because γ¯\bar{\gamma} is a geodesic under the metric e2ϕ(dx2+dy2)e^{2\phi}(dx^{2}+dy^{2}), following the computations in Section A, we have 3(xy′′x′′y)+e2ϕ1(yxϕxyϕ)=0\ell^{-3}(x^{\prime}y^{\prime\prime}-x^{\prime\prime}y^{\prime})+e^{-2\phi}\ell^{-1}(y^{\prime}\partial_{x}\phi-x^{\prime}\partial_{y}\phi)=0.

From now on we will use the Euclidean coordinates on 2\mathbb{R}^{2}. Suppose (u(y,t),y)(u(y,t),y) is a parametrization of a part of γ(,t)\gamma(\cdot,t), then u(ty(s),t)=tx(s)u(\sqrt{-t}y(s),t)=\sqrt{-t}x(s). Therefore we can conclude that

tuy2tyu=x2t,yuy=x,tyyu(y)2+yuy′′=x′′.\partial_{t}u-\frac{y}{2\sqrt{-t}}\partial_{y}u=-\frac{x}{2\sqrt{-t}},\quad\partial_{y}uy^{\prime}=x^{\prime},\quad\sqrt{-t}\partial_{yy}u(y^{\prime})^{2}+\partial_{y}uy^{\prime\prime}=x^{\prime\prime}.

γ¯\bar{\gamma} being a geodesic implies that

3(yuyy′′tyyu(y)3yuyy′′)+e2ϕ1y(xϕyuyϕ)=0,\ell^{-3}(\partial_{y}uy^{\prime}y^{\prime\prime}-\sqrt{-t}\partial_{yy}u(y^{\prime})^{3}-\partial_{y}uy^{\prime}y^{\prime\prime})+e^{-2\phi}\ell^{-1}y^{\prime}(\partial_{x}\phi-\partial_{y}u\partial_{y}\phi)=0,

namely

(B.1) tyyu1+(yu)2=xϕyuyϕ=(λxx2)+yuy2.\frac{\sqrt{-t}\partial_{yy}u}{1+(\partial_{y}u)^{2}}=\partial_{x}\phi-\partial_{y}u\partial_{y}\phi=(\frac{\lambda}{x}-\frac{x}{2})+\partial_{y}u\frac{y}{2}.

In summary, we obtain the equation

(B.2) tu=yyu1+(yu)2λu.\partial_{t}u=\frac{\partial_{yy}u}{1+(\partial_{y}u)^{2}}-\frac{\lambda}{u}.

Angenent proved the existence of a simple closed λ\lambda-Angenent curve in [Ang92]. To have the same notation as [Ang92], let us temporarily change the domain of the right-half plane to the upper-half plane by a rotation, and we use the (x,r)(x,r) as the coordinate in the upper-half plane. Namely, we want to construct a simple closed geodesic in the upper-half plane {(x,r):r>0}\{(x,r):r>0\} equipped with the metric r2λex2+r24(dx2+dr2)r^{2\lambda}e^{-\frac{x^{2}+r^{2}}{4}}(dx^{2}+dr^{2}). Although in [Ang92], Angenent only discussed the cases that λ=n1\lambda=n-1 for positive integers n2n\geq 2, the proof indeed works for general λ>0\lambda>0 verbatim, by replacing nn in [Ang92, Page 9-16] by λ+1\lambda+1. We refer the readers to [Ang92] for the proof.

It is worth noting that Drugan-Nguyen [DN18] also constructed shrinking doughnuts using a variational method. It is still an open question that whether their construction coincides with Angenent’s construction. It seems that their method can also be applied to construct λ\lambda-Angenent curves.

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