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arXiv:2406.05635v2 [math.DG] 10 Jul 2024

Gauss curvature flow to the LpL_{p}-Gaussian chord Minkowski problemThanks:Β 2020 Mathematics Subject Classification: 52A20 35K96 58J35.

Xia Zhao and Peibiao Zhao
Abstract.

Recently, Huang and Qin [15] introduced the Gaussian chord measure and LpL_{p}-Gaussian chord measure by variational methods. Meanwhile, they posed Gaussian chord Minkowski problem for p=1p=1 and used variational methods to obtain an origin-symmetric normalized measure solution for the Gaussian chord Minkowski problem. The smooth solution, up to now, to the LpL_{p}-Gaussian chord Minkowski problem is still open.

Motivated by the forgoing works by Huang and Qin in [15], we propose in the present paper the Lp​(p>0)L_{p}(p>0)-Gaussian chord Minkowski problem and log-Gaussian chord Minkowski problem, and obtain the smooth even solutions to these two types of problems by the method of a Gauss curvature flow.

Key words and phrases:Β 
Gauss curvature flow; LpL_{p}-Gaussian chord Minkowski problem; Monge-Ampère equation

1. Introduction and main results

In the past 30 years, the Minkowski problem has played an important role in the study of convex geometry, and the research of Minkowski problem has promoted the development of fully nonlinear partial differential equations. The classical Minkowski problem argues the existence, uniqueness and regularity of a convex body whose surface area measure is equal to a pre-given Borel measure on the sphere. If the given measure has a positive continuous density, the Minkowski problem can be seen as the problem of prescribing the Gauss curvature in differential geometry. With the emergence of LpL_{p} surface measure, the LpL_{p} Minkowski problem has also been proposed. In particularly, the LpL_{p}(pβˆˆβ„p\in\mathbb{R})-Minkowski problem is extremely important, because it contains some special versions, such as when p=1p=1, it is the classical Minkowski problem; when p=0p=0, the critical L0L_{0} case which is called cone volume measure, the Minkowski problem for cone volume measure is the log-Minkowski problem [3]; when p=βˆ’np=-n, it corresponds to the centro-affine Minkowski problem [34]; the LpL_{p}-Minkowski problem with p>1p>1 was first proposed and studied by Lutwak [23], whose solution plays a key role in establishing the LpL_{p}-affine Sobolev inequality [12, 24].

With the development of Minkowski problems, scholars have proposed some types of Minkowski problems. We know that the different geometric measures are corresponding to different Minkowski type problems. For instance, Xiao [32] prescribed capacitary curvature measures on planar convex domains: If a given finite, nonnegative Borel measure μ∈S1\mu\in S^{1} has centroid at the origin and its supp(ΞΌ\mu) does not comprise any pair of antipodal points, then, there is a unique (up to translation) convex, nonempty, open set Ξ©βŠ‚β„2\Omega\subset\mathbb{R}^{2} such that d​μq​(Ξ©,β‹…)=d​μ​(β‹…)d\mu_{q}(\Omega,\cdot)=d\mu(\cdot), where ΞΌq​(Ξ©,β‹…)\mu_{q}(\Omega,\cdot) is qq-capacitary curvature measure of Ξ©\Omega with q∈(1,2]q\in(1,2].

Recently, a theory analogous to the one for the Minkowski problem was introduced by Lutwak, Xi, Yang, and Zhang [25], the volume is replaced by (qq) chord integrals and surface area measure is replaced by the differential of (qβ‰₯0q\geq 0) chord integrals which is defined chord measure. Based on chord measure, they posed and solved chord Minkowski problem and chord log-Minkowski problem (partly solved). Interestingly, when q=1q=1, the chord measure recovers surface area measure, and when (q=0)(q=0), it is the area measure Snβˆ’2S_{n-2}. For the LpL_{p} chord Minkowski problem, Xi, Yang, Zhang and Zhao [31] used variational methods gave a measure solution when p>1p>1 and 0<p<10<p<1 in the symmetric case. Guo, Xi and Zhao [11] also obtained a measure solution for 0≀p<10\leq p<1 by similar methods without the symmetric assumption. In addition, authors [33] posed the Orlicz chord Minkowski problem and obtained smooth solutions by a Gauss curvature flow. When q=1q=1, the LpL_{p} chord Minkowski problem is the LpL_{p} Minkowski problem. For other references with respect to the LpL_{p} chord Minkowski problem, please refer to [13, 14, 19, 26].

Huang, Xi and Zhao [16] extended the classical Minkowski problem in ℝn\mathbb{R}^{n} to the Gaussian probability space, where the volume and surface area measure in Euclidean space were replaced by Gaussian volume and Gaussian surface measure, respectively. Then the Gaussian Minkowski problem was posed and provided a sufficient condition for the existence of solution. Later, Liu [20] extended the Gaussian Minkowski problem to LpL_{p} form, when pβ‰₯1p\geq 1, a sufficient condition for the existence and uniqueness of origin-symmetric weak solution was given. Moreover, Feng, Hu and Xu [9] provided the existence of symmetric (resp. asymmetric) solutions to the problem for p≀0p\leq 0 (resp. pβ‰₯1p\geq 1). Furthermore, Sheng and Xue [30] obtained smooth solutions by method of Gauss curvature flow for p>0p>0 and βˆ’nβˆ’1<p≀0-n-1<p\leq 0 to normalized LpL_{p} Gaussian Minkowski problem and pβ‰₯n+1p\geq n+1 and 0<p<n+10<p<n+1 to LpL_{p} Gaussian Minkowski problem. Contrary to classical surface area measure, the Gaussian surface measure is neither translationally invariant nor homogeneous. These special properties make the Gaussian Minkowski problem quite differ from the classical Minkowski problem, which has an interest on its own.

Very recently, based on chord integral and Gaussian probability space, Huang and Qin [15] generalized the chord integrals to Gaussian probability space for q>1q>1. In the case of q>1q>1, the Gaussian chord integral is defined by

IΞ³,q​(K)\displaystyle I_{\gamma,q}(K) =∫K∫K1|zβˆ’y|nβˆ’q+1​d​ℋγn​(z)​d​ℋγn​(y)\displaystyle=\int_{K}\int_{K}\frac{1}{|z-y|^{n-q+1}}d\mathcal{H}^{n}_{\gamma}(z)d\mathcal{H}^{n}_{\gamma}(y)
(1.1) =∫K∫Keβˆ’(|z|2+|y|2)/2|zβˆ’y|nβˆ’q+1​𝑑z​𝑑y.\displaystyle=\int_{K}\int_{K}\frac{e^{-(|z|^{2}+|y|^{2})/2}}{|z-y|^{n-q+1}}dzdy.

Furthermore, they established (LpL_{p}) the variational formula of Gaussian chord integral with (LpL_{p}) Minkowski sum. Here, we first state the variational formula for p=1p=1.

Theorem 1.1.

[15, Theorem 4.3]Β Β Β Β Let Kβˆˆπ’¦onK\in\mathcal{K}_{o}^{n} and q>1q>1. Suppose that g:Snβˆ’1→ℝg:S^{n-1}\rightarrow\mathbb{R} is a continuous function and ht:Snβˆ’1→ℝh_{t}:S^{n-1}\rightarrow\mathbb{R} is given by

ht(u)=hK(u)+tg(u)+o(t,u),t∈(βˆ’Ξ΄,+Ξ΄)andu∈Snβˆ’1,\displaystyle h_{t}(u)=h_{K}(u)+tg(u)+o(t,u),\quad t\in(-\delta,+\delta)\quad\text{and}\quad u\in S^{n-1},

where o⁑(t,u)/tβ†’0o(t,u)/t\rightarrow 0 uniformly on Snβˆ’1S^{n-1}, as tβ†’0t\rightarrow 0. If

Kt={xβˆˆβ„n:xβ‹…u≀ht​(u)​for all​u∈Snβˆ’1},t∈(βˆ’Ξ΄,+Ξ΄),\displaystyle K_{t}=\{x\in\mathbb{R}^{n}:x\cdot u\leq h_{t}(u)~~\text{for all}~~u\in S^{n-1}\},\quad t\in(-\delta,+\delta),

is the Wulff shape of hth_{t}, it holds

limtβ†’0ρKt​(u)βˆ’ΟK​(u)t=g⁑(Ξ½K​(ρK​(u)​u))uβ‹…Ξ½K​(ρK​(u)​u).\displaystyle\lim_{t\rightarrow 0}\frac{\rho_{K_{t}}(u)-\rho_{K}(u)}{t}=\frac{g(\nu_{K}(\rho_{K}(u)u))}{u\cdot\nu_{K}(\rho_{K}(u)u)}.

Then

dd​t|IΞ³,q​(Kt)=\displaystyle\frac{d}{dt}\bigg|I_{\gamma,q}(K_{t})= limtβ†’0IΞ³,q⁑(Kt)βˆ’IΞ³,q⁑(K)t\displaystyle\lim_{t\rightarrow 0}\frac{I_{\gamma,q(K_{t})}-I_{\gamma,q(K)}}{t}
=\displaystyle= limtβ†’01t​{∫K∫K1|zβˆ’y|nβˆ’q+1​d​γ​(z)​d​γ​(y)βˆ’βˆ«Kt∫Kt1|zβˆ’y|nβˆ’q+1​d​γ​(z)​d​γ​(y)}\displaystyle\lim_{t\rightarrow 0}\frac{1}{t}\bigg\{\int_{K}\int_{K}\frac{1}{|z-y|^{n-q+1}d\gamma(z)d\gamma(y)}-\int_{K_{t}}\int_{K_{t}}\frac{1}{|z-y|^{n-q+1}d\gamma(z)d\gamma(y)}\bigg\}
=\displaystyle= ∫Snβˆ’1∫Snβˆ’1limtβ†’0{∫0ρKt​(u)∫0ρKt​(v)βˆ’βˆ«0ρK​(u)∫0ρK​(v)}r1nβˆ’1r2nβˆ’1eβˆ’(r12+r22)/2|r1​uβˆ’r2​v|nβˆ’q+1dr1dr2dudv\displaystyle\int_{S^{n-1}}\int_{S^{n-1}}\lim_{t\rightarrow 0}\bigg\{\int_{0}^{\rho_{K_{t}}(u)}\int_{0}^{\rho_{K_{t}}(v)}-\int_{0}^{\rho_{K}(u)}\int_{0}^{\rho_{K}(v)}\bigg\}\frac{r_{1}^{n-1}r_{2}^{n-1}e^{-(r_{1}^{2}+r_{2}^{2})/2}}{|r_{1}u-r_{2}v|^{n-q+1}}dr_{1}dr_{2}dudv
=\displaystyle= 2β€‹βˆ«Snβˆ’1∫Snβˆ’1∫0ρK​(v)ρK(u)nβˆ’1r2nβˆ’1eβˆ’(ρK(u)2+r22)/2|ρK​(u)​uβˆ’r2​v|nβˆ’q+1​limtβ†’0ρKt​(u)βˆ’ΟK​(u)t​d​r2​𝑑u​𝑑v\displaystyle 2\int_{S^{n-1}}\int_{S^{n-1}}\int_{0}^{\rho_{K}(v)}\frac{\rho_{K}(u)^{n-1}r_{2}^{n-1}e^{-(\rho_{K}(u)^{2}+r_{2}^{2})/2}}{|\rho_{K}(u)u-r_{2}v|^{n-q+1}}\lim_{t\rightarrow 0}\frac{\rho_{K_{t}}(u)-\rho_{K}(u)}{t}dr_{2}dudv
=\displaystyle= 2β€‹βˆ«Snβˆ’1∫Snβˆ’1∫0ρK​(v)ρK(u)nβˆ’1r2nβˆ’1eβˆ’(ρK(u)2+r22)/2|ρK​(u)​uβˆ’r2​v|nβˆ’q+1​g⁑(Ξ½K​(ρK​(u)​u))uβ‹…Ξ½K​(ρK​(u)​u)​d​r2​𝑑u​𝑑v\displaystyle 2\int_{S^{n-1}}\int_{S^{n-1}}\int_{0}^{\rho_{K}(v)}\frac{\rho_{K}(u)^{n-1}r_{2}^{n-1}e^{-(\rho_{K}(u)^{2}+r_{2}^{2})/2}}{|\rho_{K}(u)u-r_{2}v|^{n-q+1}}\frac{g(\nu_{K}(\rho_{K}(u)u))}{u\cdot\nu_{K}(\rho_{K}(u)u)}dr_{2}dudv
=\displaystyle= 2βˆ«βˆ‚K∫Keβˆ’z2/2|yβˆ’z|nβˆ’q+1dzβ‹…g(Ξ½K(y))eβˆ’y2/2dβ„‹nβˆ’1(y)\displaystyle 2\int_{\partial K}\int_{K}\frac{e^{-z^{2}/2}}{|y-z|^{n-q+1}}dz\cdot g(\nu_{K}(y))e^{-y^{2}/2}d\mathcal{H}^{n-1}(y)
=\displaystyle= βˆ«βˆ‚Kg⁑(Ξ½K​(y))​V~Ξ³,q​(K,y)​d​ℋnβˆ’1​(y)=∫Snβˆ’1g⁑(u)​d​FΞ³,q​(K,u),\displaystyle\int_{\partial K}g(\nu_{K}(y))\widetilde{V}_{\gamma,q}(K,y)d\mathcal{H}^{n-1}(y)=\int_{S^{n-1}}g(u)dF_{\gamma,q}(K,u),

where

(1.2) V~Ξ³,q(K,y)=2eβˆ’|y|2/2{∫Keβˆ’|z|2/2|zβˆ’y|nβˆ’q+1dz},\displaystyle\widetilde{V}_{\gamma,q}(K,y)=2e^{-|y|^{2}/2}\bigg\{\int_{K}\frac{e^{-|z|^{2}/2}}{|z-y|^{n-q+1}}dz\bigg\},

and

FΞ³,q​(K,Ξ·)=∫νKβˆ’1​(Ξ·)V~Ξ³,q​(K,y)​d​ℋnβˆ’1​(y),Borel setβ€‹Ξ·βŠ†Snβˆ’1.\displaystyle{F}_{\gamma,q}(K,\eta)=\int_{\nu_{K}^{-1}(\eta)}\widetilde{V}_{\gamma,q}(K,y)d\mathcal{H}^{n-1}(y),\quad\text{Borel set}~~\eta\subseteq S^{n-1}.

Next, a similar result holds for the LpL_{p}-combination perturbation of the supporting function, which is stated in the following theorem.

Theorem 1.2.

[15, Theorem 4.4]Β Β Β Β Let pβ‰ 0p\neq 0, q>1q>1 and Kβˆˆπ’¦onK\in\mathcal{K}^{n}_{o}. Suppose that g:Snβˆ’1→ℝg:S^{n-1}\rightarrow\mathbb{R} is a continuous function and ht:Snβˆ’1→ℝh_{t}:S^{n-1}\rightarrow\mathbb{R} is given by

ht​(u)=(hK​(u)p+t​g​(u)p)1p,u∈Snβˆ’1\displaystyle h_{t}(u)=(h_{K}(u)^{p}+tg(u)^{p})^{\frac{1}{p}},\quad u\in S^{n-1}

and KtK_{t} is the Wulff shape of hth_{t}, it holds

limtβ†’0ρKt​(u)βˆ’ΟK​(u)t=1p​g​(Ξ½K​(ρK​(u)​u))p​hK​(Ξ½K​(ρK​(u)​u))1βˆ’puβ‹…Ξ½K​(ρK​(u)​u).\displaystyle\lim_{t\rightarrow 0}\frac{\rho_{K_{t}}(u)-\rho_{K}(u)}{t}=\frac{1}{p}\frac{g(\nu_{K}(\rho_{K}(u)u))^{p}h_{K}(\nu_{K}(\rho_{K}(u)u))^{1-p}}{u\cdot\nu_{K}(\rho_{K}(u)u)}.

Then

dd​t|t=0​IΞ³,q​(Kt)=\displaystyle\frac{d}{dt}\bigg|_{t=0}I_{\gamma,q}(K_{t})= βˆ«βˆ‚Kg​(Ξ½K​(y))p​V~Ξ³,q​(K,y)​hK​(Ξ½K​(y))1βˆ’p​d​ℋnβˆ’1​(y)\displaystyle\int_{\partial K}g(\nu_{K}(y))^{p}\widetilde{V}_{\gamma,q}(K,y)h_{K}(\nu_{K}(y))^{1-p}d\mathcal{H}^{n-1}(y)
(1.3) =\displaystyle= ∫Snβˆ’1g​(u)p​d​GΞ³,p,q​(K,u),\displaystyle\int_{S^{n-1}}g(u)^{p}dG_{\gamma,p,q}(K,u),

where

(1.4) GΞ³p,q=GΞ³,p,q​(K,Ξ·)=2pβ€‹βˆ«Ξ½Kβˆ’1​(Ξ·)V~Ξ³,q​(K,y)​hK​(Ξ½K​(y))1βˆ’p​d​ℋnβˆ’1​(y),Borel setβ€‹Ξ·βŠ†Snβˆ’1.\displaystyle G_{\gamma}^{p,q}=G_{\gamma,p,q}(K,\eta)=\frac{2}{p}\int_{\nu_{K}^{-1}(\eta)}\widetilde{V}_{\gamma,q}(K,y)h_{K}(\nu_{K}(y))^{1-p}d\mathcal{H}^{n-1}(y),\text{Borel set}~~\eta\subseteq S^{n-1}.

In fact, we can directly obtain Theorem 1.2 by replacing limtβ†’0ρKt​(u)βˆ’ΟK​(u)t\lim_{t\rightarrow 0}\frac{\rho_{K_{t}}(u)-\rho_{K}(u)}{t} with 1p​g​(Ξ½K​(ρK​(u)​u))p​hK​(Ξ½K​(ρK​(u)​u))1βˆ’puβ‹…Ξ½K​(ρK​(u)​u)\frac{1}{p}\frac{g(\nu_{K}(\rho_{K}(u)u))^{p}h_{K}(\nu_{K}(\rho_{K}(u)u))^{1-p}}{u\cdot\nu_{K}(\rho_{K}(u)u)} in Theorem 1.1. When p=1p=1, (1.3) correspondings to the Gaussian chord measure in Theorem 1.1.

As for the log\log-Minkowski perturbation, the variational formula of nonlocal function in Gaussian probability space is obtained in the following Theorem.

Theorem 1.3.

[15, Theorem 4.5]Β Β Β Β Let q>1q>1 and Kβˆˆπ’¦onK\in\mathcal{K}^{n}_{o}. Suppose that g:Snβˆ’1→ℝg:S^{n-1}\rightarrow\mathbb{R} is a continuous function and ht:Snβˆ’1→ℝh_{t}:S^{n-1}\rightarrow\mathbb{R} is given by

log⁑ht​(u)=\displaystyle\log h_{t}(u)= log⁑hK​(u)+t​g​(u)+o⁑(t,u)t∈(βˆ’Ξ΄,+Ξ΄)andu∈Snβˆ’1,\displaystyle\log h_{K}(u)+tg(u)+o(t,u)\quad t\in(-\delta,+\delta)\quad\text{and}\quad u\in S^{n-1},

where, o⁑(t,β‹…)/tβ†’0o(t,\cdot)/t\rightarrow 0 uniformly on Snβˆ’1S^{n-1}, as tβ†’0t\rightarrow 0. If KtK_{t} is the Wulff shape of hth_{t}, it holds

limtβ†’0ρKt​(u)βˆ’ΟK​(u)t=\displaystyle\lim_{t\rightarrow 0}\frac{\rho_{K_{t}}(u)-\rho_{K}(u)}{t}= ρKt′​(u)|t=0=ρK​(u)​log⁑ρKt′​(u)|t=0\displaystyle\rho_{K_{t}}^{\prime}(u)|_{t=0}=\rho_{K}(u)\log\rho_{K_{t}}^{\prime}(u)|_{t=0}
=\displaystyle= ρK​(u)​limtβ†’0log⁑ρKt​(u)βˆ’log⁑ρK​(u)t=hK​(Ξ½K​(ρK​(u)​u))​g⁑(Ξ½K​(ρK​(u)​u))uβ‹…Ξ½K​(ρK​(u)​u).\displaystyle\rho_{K}(u)\lim_{t\rightarrow 0}\frac{\log\rho_{K_{t}}(u)-\log\rho_{K}(u)}{t}=h_{K}(\nu_{K}(\rho_{K}(u)u))\frac{g(\nu_{K}(\rho_{K}(u)u))}{u\cdot\nu_{K}(\rho_{K}(u)u)}.

Then

dd​t|t=0​IΞ³,q​(Kt)=\displaystyle\frac{d}{dt}\bigg|_{t=0}I_{\gamma,q}(K_{t})= βˆ«βˆ‚Kg⁑(Ξ½K​(y))​V~Ξ³,q​(K,y)​hK​(Ξ½K​(y))​d​ℋnβˆ’1​(y)\displaystyle\int_{\partial K}g(\nu_{K}(y))\widetilde{V}_{\gamma,q}(K,y)h_{K}(\nu_{K}(y))d\mathcal{H}^{n-1}(y)
(1.5) =\displaystyle= ∫Snβˆ’1g⁑(u)​d​GΞ³,0,q​(K,u),\displaystyle\int_{S^{n-1}}g(u)dG_{\gamma,0,q}(K,u),

where

(1.6) GΞ³log,q=GΞ³,0,q​(K,Ξ·)=∫νKβˆ’1​(Ξ·)V~Ξ³,q​(K,y)​hK​(Ξ½K​(y))​d​ℋnβˆ’1​(y),Borel setβ€‹Ξ·βŠ†Snβˆ’1.\displaystyle G_{\gamma}^{\log,q}=G_{\gamma,0,q}(K,\eta)=\int_{\nu_{K}^{-1}(\eta)}\widetilde{V}_{\gamma,q}(K,y)h_{K}(\nu_{K}(y))d\mathcal{H}^{n-1}(y),\text{Borel set}~~\eta\subseteq S^{n-1}.

In the same way, we immediately get Theorem 1.3 by replacing limtβ†’0ρKt​(u)βˆ’ΟK​(u)t\lim_{t\rightarrow 0}\frac{\rho_{K_{t}}(u)-\rho_{K}(u)}{t} with hK​(Ξ½K​(ρK​(u)​u))​g⁑(Ξ½K​(ρK​(u)​u))uβ‹…Ξ½K​(ρK​(u)​u)h_{K}(\nu_{K}(\rho_{K}(u)u))\frac{g(\nu_{K}(\rho_{K}(u)u))}{u\cdot\nu_{K}(\rho_{K}(u)u)} in Theorem 1.1.

With the help of variational formula (1.3), we can propose the normalized LpL_{p}-Gaussian chord Minkowski problem for p≠0p\neq 0.

The LpL_{p}-Gaussian chord Minkowski problem. Let q>1q>1, pβ‰ 0p\neq 0 and ΞΌ\mu be a finite Borel measure on Snβˆ’1S^{n-1}, under what necessary and sufficient conditions, does there exist a unique convex body Ξ©βˆˆπ’¦on\Omega\in\mathcal{K}_{o}^{n} and positive constant Ο„1\tau_{1} so that

(1.7) ΞΌ=Ο„1​GΞ³p,q​(Ξ©,β‹…)​?\displaystyle\mu=\tau_{1}G_{\gamma}^{p,q}(\Omega,\cdot)?

From [15, Proposition 3.7], we know that GΞ³p,q​(Ξ©,β‹…)G_{\gamma}^{p,q}(\Omega,\cdot) is absolutely continuous with respect to the surface measure S⁑(K,β‹…)S(K,\cdot). If the given measure ΞΌ\mu is absolutely continuous with respect to the spherical Lebesgue measure, that is, Β΅\textmu has a density function f:Snβˆ’1β†’(0,∞)f:S^{n-1}\rightarrow(0,\infty) is smooth, then, solving problem (1.7) can be equivalently viewed as solving the following normalized Monge-AmpΓ¨re equation from the (1.4) for pβ‰ 0p\neq 0 on Snβˆ’1S^{n-1}.

(1.8) Ο„1​V~Ξ³,q​(Ξ©,β‹…)​hΞ©1βˆ’p​det(hi​j+h​δi​j)=f.\displaystyle\tau_{1}\widetilde{V}_{\gamma,q}(\Omega,\cdot)h_{\Omega}^{1-p}\det(h_{ij}+h\delta_{ij})=f.

When p=1p=1, the LpL_{p}-Gaussian chord Minkowski problem is the Gaussian chord Minkowski problem which was first studied by Huang and Qin [15], they obtained an origin-symmetric normalized measure solution by variational method.

Similar to cone volume measure, we call GΞ³log,qG_{\gamma}^{\log,q} cone-Gaussian chord measure. The Minkowski problem prescribing cone-Gaussian chord measures is:

The log-Gaussian chord Minkowski problem. Let q>1q>1 and ΞΌ\mu be a finite Borel measure on Snβˆ’1S^{n-1}, under what necessary and sufficient conditions, does there exist a unique convex body Ξ©βˆˆπ’¦on\Omega\in\mathcal{K}_{o}^{n} and positive constant Ο„2\tau_{2} so that

(1.9) ΞΌ=Ο„2​GΞ³log,q​(Ξ©,β‹…)​?\displaystyle\mu=\tau_{2}G_{\gamma}^{\log,q}(\Omega,\cdot)?

The partial differential equation associated with (1.9) is a new type of Monge-AmpΓ¨re equation from (1.6) on Snβˆ’1S^{n-1},

(1.10) Ο„2​V~Ξ³,q​(Ξ©,β‹…)​hΩ​det(hi​j+h​δi​j)=f.\displaystyle\tau_{2}\widetilde{V}_{\gamma,q}(\Omega,\cdot)h_{\Omega}\det(h_{ij}+h\delta_{ij})=f.

In this paper, we will study the LpL_{p}-Gaussian chord Minkowski problem and give the existence of smooth even solutions for (1.8) with q>2q>2 and p>0p>0 by the method of a Gauss curvature flow. In addition, we also provide a smooth even solution to log-Gaussian chord Minkowski problem to (1.10). The Gauss curvature flow was first introduced and studied by Firey [10] to model the shape change of worn stones. It can mainly be used to study the existence of smooth solutions to the famous Minkowski (type) problems. For instances, Chen, Huang and Zhao [6] obtained smooth even solutions to the LpL_{p} dual Minkowski problem by the method of Gauss curvature flow. Liu and Lu [21] used a Gauss curvature flow to solve dual Orlicz-Minkowski problem and obtained its smooth solutions. Since then, various problems of Gauss curvature flows have been extensively studied, see examples [2, 4, 5, 8, 18, 22] and the references therein.

Remark 1.4.

From the definitions of the Lp​(pβ‰ 0)L_{p}(p\neq 0)-combination perturbation and log-Minkowski perturbation of the support function, we konw that the log-Minkowski perturbation is the limit form of the LpL_{p} combination perturbation when pp tends to 00. In this sense, the variational formula (1.3) and (1.5) belong to different categories, then, the corresponding Lp​(pβ‰ 0)L_{p}(p\neq 0)-Gaussian chord Minkowski problem (1.7) is different from log-Gaussian chord Minkowski problem (1.9). However, when we transform (1.7) to equivalent form equation (1.8) and (1.9) to (1.10), from the perspective of the equation, these two problems can be considered unifiedly. To this end, we can unifiedly construct the following curvature flow to solve the LpL_{p}-Gaussian chord Minkowski problem for p>0p>0 and log-Gaussian chord Minkowski problem for the critical L0L_{0} case.

Let βˆ‚Ξ©0\partial\Omega_{0} be a smooth, closed and origin-symmetric strictly convex hypersurface in ℝn\mathbb{R}^{n}. We consider the long-time existence and convergence of the following Gauss curvature flow which is a family of convex hypersurfaces βˆ‚Ξ©t\partial\Omega_{t} parameterized by smooth maps X⁑(β‹…,t):Snβˆ’1Γ—(0,∞)→ℝnX(\cdot,t):S^{n-1}\times(0,\infty)\rightarrow\mathbb{R}^{n} satisfying the initial value problem

{βˆ‚X⁑(x,t)βˆ‚t=βˆ’ΞΈβ‘(t)β€‹βŸ¨X,v⟩p​𝒦​(x,t)​f​(v)V~Ξ³,q​(Ξ©t,β‹…)​v+X⁑(x,t),X⁑(x,0)=X0​(x),\displaystyle\left\{\begin{array}[]{lc}\frac{\partial X(x,t)}{\partial t}=-\theta(t)\frac{\langle X,v\rangle^{p}\mathcal{K}(x,t)f(v)}{\widetilde{V}_{\gamma,q}(\Omega_{t},\cdot)}v+X(x,t),\\ X(x,0)=X_{0}(x),\\ \end{array}\right.

where 𝒦⁑(x,t)\mathcal{K}(x,t) is the Gauss curvature of hypersurface βˆ‚Ξ©t\partial\Omega_{t}, v=xv=x is the outer unit normal at X⁑(x,t)X(x,t), ⟨X,v⟩\langle X,v\rangle represents standard inner product of XX and vv, and θ⁑(t)\theta(t) is given by

θ⁑(t)=∫Snβˆ’1V~Ξ³,q​(Ξ©t,β‹…)​ρn​(ΞΎ,t)β€‹π‘‘ΞΎβˆ«Snβˆ’1hp​(x,t)​f​(x)​𝑑x,\displaystyle\theta(t)=\frac{\int_{S^{n-1}}\widetilde{V}_{\gamma,q}(\Omega_{t},\cdot)\rho^{n}(\xi,t)d\xi}{\int_{S^{n-1}}h^{p}(x,t)f(x)dx},

where ρ\rho and hh are the radial function and support function of the convex hypersurface βˆ‚Ξ©t\partial\Omega_{t}, respectively.

Remark 1.5.

When p=0p=0, the flow (1) and θ⁑(t)\theta(t) be meaningful. Thus, the flow (1) can also be used to study the log-Gaussian chord Minkowski problem.

Combining problem (1.8), (1.10) with flow (1), we establish the following result in this article.

Theorem 1.6.

Suppose q>2q>2, pβ‰₯0p\geq 0, βˆ‚Ξ©0\partial\Omega_{0} be a smooth, closed and origin-symmetric strictly convex hypersurface in ℝn\mathbb{R}^{n} and ff be a positive smooth even function on Snβˆ’1S^{n-1}. Then, the flow (1) has a unique smooth solution to the βˆ‚Ξ©t=X⁑(Snβˆ’1,t)\partial\Omega_{t}=X(S^{n-1},t) for t∈(0,∞)t\in(0,\infty). When tβ†’βˆžt\rightarrow\infty, there is a subsequence of βˆ‚Ξ©t\partial\Omega_{t} converges in C∞C^{\infty}to a smooth, closed, origin-symmetric and strictly convex hypersurface Ω∞\Omega_{\infty}, whose support function satisfies (1.8) for p>0p>0 and (1.10) for p=0p=0.

This paper is organized as follows. We collect background materials in Section 2. In Section 3, we give the parameterized form of flow (1) by support function and discuss properties of two important functionals along the flow (1). In Section 4, we give the priori estimates for the solution to the flow (1). We obtain the convergence of the flow and complete the proof of Theorem 1.6 in Section 5.

2. Preliminaries

In this section, we give a brief review of some relevant notions about convex bodies and recall some basic properties of convex hypersurfaces that readers may refer to [29] and a book of Schneider [27].

2.1. Convex bodies

Let ℝn\mathbb{R}^{n} be the nn-dimensional Euclidean space, let |z|=zβ‹…z|z|=\sqrt{z\cdot z} be the Euclidean norm of zz. The unit sphere in ℝn\mathbb{R}^{n} is denoted by Snβˆ’1S^{n-1}, Ο‰n\omega_{n} is the volume of the unit ball. For k∈[0,n]k\in[0,n], β„‹k\mathcal{H}^{k} denotes the kk-dimensional Hausdorff measure in ℝn\mathbb{R}^{n}. In integrals with respect to β„‹n\mathcal{H}^{n}, we often abbreviate d​ℋn​(z)d\mathcal{H}^{n}(z) by d​zdz. Similarly, in integrals over the unite sphere Snβˆ’1S^{n-1}, instead of d​ℋnβˆ’1d\mathcal{H}^{n-1} we write d​udu. β„‹Ξ³k\mathcal{H}^{k}_{\gamma} is the kk-dimensional Hausdorff measure with respect to Gaussian density function f(z)=eβˆ’|z2|/2f(z)=e^{-|z^{2}|/2}, zβˆˆβ„nz\in\mathbb{R}^{n}.

Assume that βˆ‚Ξ©\partial\Omega be a smooth, closed and strictly convex hypersurface containing the origin in its interior. The support function of convex body Ξ©\Omega is defined by

hΩ​(ΞΎ)=h⁑(Ξ©,ΞΎ)=max⁑{ΞΎβ‹…y:y∈Ω},βˆ€ΞΎβˆˆSnβˆ’1,\displaystyle h_{\Omega}(\xi)=h(\Omega,\xi)=\max\{\xi\cdot y:y\in\Omega\},\quad\forall\xi\in S^{n-1},

and the radial function of Ξ©\Omega with respect to zβˆˆβ„z\in\mathbb{R} is defined by

ρΩ,z​(v)=ρ⁑((Ξ©,z),v)=max⁑{c>0:c​v+z∈Ω},v∈Snβˆ’1.\displaystyle\rho_{\Omega,z}(v)=\rho((\Omega,z),v)=\max\{c>0:cv+z\in\Omega\},\quad v\in S^{n-1}.

For a compact convex subset Ξ©βˆˆπ’¦n\Omega\in\mathcal{K}^{n} and v∈Snβˆ’1v\in S^{n-1}, the intersection of a supporting hyperplane with Ξ©\Omega, H⁑(Ξ©,v)H(\Omega,v) at vv is given by

H⁑(Ξ©,v)={y∈Ω:yβ‹…v=hΩ​(v)}.\displaystyle H(\Omega,v)=\{y\in\Omega:y\cdot v=h_{\Omega}(v)\}.

A boundary point of Ξ©\Omega which only has one supporting hyperplane is called a regular point, otherwise, it is a singular point. The set of singular points is denoted as σ​Ω\sigma\Omega, it is well known that σ​Ω\sigma\Omega has spherical Lebesgue measure 0.

For yβˆˆβˆ‚Ξ©βˆ–Οƒβ€‹Ξ©y\in\partial\Omega\setminus\sigma\Omega, its Gauss map Ξ½Ξ©:yβˆˆβˆ‚Ξ©βˆ–Οƒβ€‹Ξ©β†’Snβˆ’1\nu_{\Omega}:y\in\partial\Omega\setminus\sigma\Omega\rightarrow S^{n-1} is represented by

νΩ​(y)={v∈Snβˆ’1:yβ‹…v=hΩ​(v)}.\displaystyle\nu_{\Omega}(y)=\{v\in S^{n-1}:y\cdot v=h_{\Omega}(v)\}.

Correspondingly, for a Borel set Ξ·βŠ‚Snβˆ’1\eta\subset S^{n-1}, its inverse Gauss map is denoted by Ξ½Ξ©βˆ’1\nu_{\Omega}^{-1},

Ξ½Ξ©βˆ’1​(Ξ·)={yβˆˆβˆ‚Ξ©:νΩ​(y)∈η}.\displaystyle\nu_{\Omega}^{-1}(\eta)=\{y\in\partial\Omega:\nu_{\Omega}(y)\in\eta\}.

Specially, for a convex hypersurface βˆ‚Ξ©\partial\Omega of class C2C^{2}, then, the support function of Ω can be stated as

h⁑(Ξ©,x)=xβ‹…Ξ½βˆ’1​(x)=ν⁑(X⁑(x))β‹…X⁑(x),X⁑(x)βˆˆβˆ‚Ξ©.\displaystyle h(\Omega,x)=x\cdot\nu^{-1}(x)=\nu(X(x))\cdot X(x),\quad X(x)\in\partial\Omega.

Moreover, the gradient of h⁑(Ξ©,β‹…)h(\Omega,\cdot) satisfies

βˆ‡h​(Ξ©,x)=Ξ½βˆ’1​(x)=X⁑(x).\displaystyle\nabla h(\Omega,x)=\nu^{-1}(x)=X(x).

For the Borel set Ξ·βŠ‚Snβˆ’1\eta\subset S^{n-1}, its surface area measure is defined as

SΩ​(Ξ·)=β„‹nβˆ’1​(Ξ½Ξ©βˆ’1​(Ξ·)).\displaystyle S_{\Omega}(\eta)=\mathcal{H}^{n-1}(\nu_{\Omega}^{-1}(\eta)).

2.2. Convex hypersurface

Suppose that Ξ©\Omega is parameterized by the inverse Gauss map X:Snβˆ’1β†’Ξ©X:S^{n-1}\rightarrow\Omega, that is X⁑(x)=Ξ½Ξ©βˆ’1​(x)X(x)=\nu_{\Omega}^{-1}(x). Then, the support function hh of Ξ©\Omega can be computed by

(2.1) h⁑(x)=xβ‹…X⁑(x),x∈Snβˆ’1,\displaystyle h(x)=x\cdot X(x),\ \ x\in S^{n-1},

where xx is the outer normal of Ξ©\Omega at X⁑(x)X(x). Let {e1,e2,β‹―,enβˆ’1}\{e_{1},e_{2},\cdots,e_{n-1}\} be an orthonormal frame on Snβˆ’1S^{n-1}, denote ei​je_{ij} by the standard metric on the sphere Snβˆ’1S^{n-1}. Differentiating (2.1), there has

βˆ‡ih=βˆ‡ixβ‹…X⁑(x)+xβ‹…βˆ‡iX​(x),\displaystyle\nabla_{i}h=\nabla_{i}x\cdot X(x)+x\cdot\nabla_{i}X(x),

since βˆ‡iX​(x)\nabla_{i}X(x) is tangent to Ξ©\Omega at X⁑(x)X(x), thus,

βˆ‡ih=βˆ‡ixβ‹…X⁑(x).\displaystyle\nabla_{i}h=\nabla_{i}x\cdot X(x).

By differentiating (2.1) twice, the second fundamental form Ai​jA_{ij} of Ξ©\Omega can be computed in terms of the support function,

(2.2) Ai​j=βˆ‡i​jh+h​ei​j,\displaystyle A_{ij}=\nabla_{ij}h+he_{ij},

where βˆ‡i​j=βˆ‡iβˆ‡j\nabla_{ij}=\nabla_{i}\nabla_{j} denotes the second order covariant derivative with respect to ei​je_{ij}. The induced metric matrix gi​jg_{ij} of Ξ©\Omega can be derived by Weingarten’s formula,

(2.3) ei​j=βˆ‡ixβ‹…βˆ‡jx=Ai​k​Al​j​gk​l.\displaystyle e_{ij}=\nabla_{i}x\cdot\nabla_{j}x=A_{ik}A_{lj}g^{kl}.

The principal radii of curvature are the eigenvalues of the matrix bi​j=Ai​k​gj​kb_{ij}=A^{ik}g_{jk}. When considering a smooth local orthonormal frame on Snβˆ’1S^{n-1}, by virtue of (2.2) and (2.3), there has

(2.4) bi​j=Ai​j=βˆ‡i​jh+h​δi​j.\displaystyle b_{ij}=A_{ij}=\nabla_{ij}h+h\delta_{ij}.

Then, the Gauss curvature of X⁑(x)∈ΩX(x)\in\Omega is given by

(2.5) 𝒦⁑(x)=(det(βˆ‡i​jh+h​δi​j))βˆ’1.\displaystyle\mathcal{K}(x)=(\det(\nabla_{ij}h+h\delta_{ij}))^{-1}.

3. Geometric flow and its associated functionals

In this section, we shall introduce the geometric flow and its associated functionals for solving the LpL_{p}-Gaussian chord Minkowski problem. For convenience, the Gauss curvature flow is restated here. Let βˆ‚Ξ©0\partial\Omega_{0} be a smooth, closed and origin symmetric strictly convex hypersurface in ℝn\mathbb{R}^{n} and ff be a positive smooth even function on Snβˆ’1S^{n-1}. We consider the following Gauss curvature flow

{βˆ‚X⁑(x,t)βˆ‚t=βˆ’ΞΈβ‘(t)β€‹βŸ¨X,v⟩p​𝒦​(x,t)​f​(v)V~Ξ³,q​(Ξ©t,β‹…)​v+X⁑(x,t),X⁑(x,0)=X0​(x),\displaystyle\left\{\begin{array}[]{lc}\frac{\partial X(x,t)}{\partial t}=-\theta(t)\frac{\langle X,v\rangle^{p}\mathcal{K}(x,t)f(v)}{\widetilde{V}_{\gamma,q}(\Omega_{t},\cdot)}v+X(x,t),\\ X(x,0)=X_{0}(x),\\ \end{array}\right.

where 𝒦⁑(x,t)\mathcal{K}(x,t) is the Gauss curvature of the hypersurface βˆ‚Ξ©t\partial\Omega_{t} at X⁑(β‹…,t)X(\cdot,t), v=xv=x is the unit outer normal vector of βˆ‚Ξ©t\partial\Omega_{t} at X⁑(β‹…,t)X(\cdot,t), ⟨X,v⟩\langle X,v\rangle represents standard inner product of XX and vv, and θ⁑(t)\theta(t) is given by

(3.3) θ⁑(t)=∫Snβˆ’1V~Ξ³,q​(Ξ©t,β‹…)​ρn​(ΞΎ,t)β€‹π‘‘ΞΎβˆ«Snβˆ’1hp​(x,t)​f​(x)​𝑑x.\displaystyle\theta(t)=\frac{\int_{S^{n-1}}\widetilde{V}_{\gamma,q}(\Omega_{t},\cdot)\rho^{n}(\xi,t)d\xi}{\int_{S^{n-1}}h^{p}(x,t)f(x)dx}.

Taking the scalar product of both sides of the equation and of the initial condition in (3) by vv, by means of the definition of support function (2.1), we describe the flow equation associated with the support function as follows

{βˆ‚h⁑(x,t)βˆ‚t=βˆ’ΞΈβ‘(t)​hp​𝒦​(x,t)​f​(x)V~Ξ³,q​([h],β‹…)+h⁑(x,t),h⁑(x,0)=h0​(x).\displaystyle\left\{\begin{array}[]{lc}\frac{\partial h(x,t)}{\partial t}=-\theta(t)\frac{h^{p}\mathcal{K}(x,t)f(x)}{\widetilde{V}_{\gamma,q}([h],\cdot)}+h(x,t),\\ h(x,0)=h_{0}(x).\\ \end{array}\right.

Next, we investigate the characteristic of Guassian chord integral IΞ³,q​(Ξ©t)I_{\gamma,q}(\Omega_{t}) along the flow (3). Let’s list a fact firstly (see e.g. [21]).

(3.6) 1ρ⁑(ΞΎ,t)β€‹βˆ‚Οβ‘(ΞΎ,t)βˆ‚t=1h⁑(x,t)β€‹βˆ‚h⁑(x,t)βˆ‚t.\displaystyle\frac{1}{\rho(\xi,t)}\frac{\partial\rho(\xi,t)}{\partial t}=\frac{1}{h(x,t)}\frac{\partial h(x,t)}{\partial t}.
Lemma 3.1.

For q>1q>1, pβˆˆβ„p\in\mathbb{R}, the IΞ³,q​(Ξ©t)I_{\gamma,q}(\Omega_{t}) is unchanged with regard to Eq. (3), namely,

βˆ‚βˆ‚t​IΞ³,q​(Ξ©t)=0.\displaystyle\frac{\partial}{\partial t}I_{\gamma,q}(\Omega_{t})=0.
Proof.

Let h⁑(β‹…,t)h(\cdot,t) and ρ⁑(β‹…,t)\rho(\cdot,t) be the support function and radial function of Ξ©t\Omega_{t}, respectively. From (1.1) and (1.2), we can derive

IΞ³,q​(K)=\displaystyle I_{\gamma,q}(K)= ∫K∫Keβˆ’(|z|2+|y|2)/2|zβˆ’y|nβˆ’q+1​𝑑z​𝑑y\displaystyle\int_{K}\int_{K}\frac{e^{-(|z|^{2}+|y|^{2})/2}}{|z-y|^{n-q+1}}dzdy
=\displaystyle= ∫Keβˆ’|y|2/2∫Keβˆ’|z|2/2|zβˆ’y|nβˆ’q+1dzdy\displaystyle\int_{K}e^{-|y|^{2}/2}\int_{K}\frac{e^{-|z|^{2}/2}}{|z-y|^{n-q+1}}dzdy
(3.7) =\displaystyle= 12β€‹βˆ«KV~Ξ³,q​(K,y)​𝑑y.\displaystyle\frac{1}{2}\int_{K}\widetilde{V}_{\gamma,q}(K,y)dy.

Therefore, applying polar coordinates to (3.7), by (3.3), (3), (3.6) and ρn​𝒦​d​ξ=h​d​x\rho^{n}\mathcal{K}d\xi=hdx, we have

βˆ‚βˆ‚t​IΞ³,q​(Ξ©t)=\displaystyle\frac{\partial}{\partial t}I_{\gamma,q}(\Omega_{t})= βˆ‚βˆ‚t​(12β€‹βˆ«Ξ©tV~Ξ³,q​(Ξ©t,y)​𝑑y)\displaystyle\frac{\partial}{\partial t}\bigg(\frac{1}{2}\int_{\Omega_{t}}\widetilde{V}_{\gamma,q}(\Omega_{t},y)dy\bigg)
=\displaystyle= 12β€‹βˆ‚βˆ‚t​(∫Snβˆ’1∫0ρ⁑(ΞΎ,t)V~Ξ³,q​(Ξ©t,ρ⁑(ΞΎ,t))​ρnβˆ’1​𝑑ρ​𝑑ξ)\displaystyle\frac{1}{2}\frac{\partial}{\partial t}\bigg(\int_{S^{n-1}}\int_{0}^{\rho(\xi,t)}\widetilde{V}_{\gamma,q}(\Omega_{t},\rho(\xi,t))\rho^{n-1}d\rho d\xi\bigg)
=\displaystyle= 12β€‹βˆ«Snβˆ’1V~Ξ³,q​(Ξ©t,ρ⁑(ΞΎ,t))​ρnβˆ’1β€‹βˆ‚Οβˆ‚t​𝑑ξ\displaystyle\frac{1}{2}\int_{S^{n-1}}\widetilde{V}_{\gamma,q}(\Omega_{t},\rho(\xi,t))\rho^{n-1}\frac{\partial\rho}{\partial t}d\xi
=\displaystyle= 12β€‹βˆ«Snβˆ’1V~Ξ³,q​(Ξ©t,ρ⁑(ΞΎ,t))​ρnβ€‹π’¦π’¦β€‹Οβ€‹βˆ‚Οβˆ‚t​𝑑ξ\displaystyle\frac{1}{2}\int_{S^{n-1}}\widetilde{V}_{\gamma,q}(\Omega_{t},\rho(\xi,t))\frac{\rho^{n}\mathcal{K}}{\mathcal{K}\rho}\frac{\partial\rho}{\partial t}d\xi
=\displaystyle= 12β€‹βˆ«Snβˆ’1V~Ξ³,q​(Ξ©t,ρ⁑(ΞΎ,t))​h𝒦​hβ€‹βˆ‚hβˆ‚t​𝑑x\displaystyle\frac{1}{2}\int_{S^{n-1}}\widetilde{V}_{\gamma,q}(\Omega_{t},\rho(\xi,t))\frac{h}{\mathcal{K}h}\frac{\partial h}{\partial t}dx
=\displaystyle= 12β€‹βˆ«Snβˆ’1V~Ξ³,q​(βˆ’ΞΈβ‘(t)​𝒦​hp​f​(x)V~Ξ³,q+h)​1𝒦​𝑑x\displaystyle\frac{1}{2}\int_{S^{n-1}}\widetilde{V}_{\gamma,q}\bigg(-\theta(t)\frac{\mathcal{K}h^{p}f(x)}{\widetilde{V}_{\gamma,q}}+h\bigg)\frac{1}{\mathcal{K}}dx
=\displaystyle= 12(βˆ’βˆ«Snβˆ’1V~Ξ³,q​h𝒦​𝑑x∫Snβˆ’1hp​f​𝑑x∫Snβˆ’1hpf(x)dx+∫Snβˆ’1V~Ξ³,q​h𝒦dx)\displaystyle\frac{1}{2}\bigg(-\frac{\int_{S^{n-1}}\frac{\widetilde{V}_{\gamma,q}h}{\mathcal{K}}dx}{\int_{S^{n-1}}h^{p}fdx}\int_{S^{n-1}}h^{p}f(x)dx+\int_{S^{n-1}}\frac{\widetilde{V}_{\gamma,q}h}{\mathcal{K}}dx\bigg)
=\displaystyle= 12(βˆ’βˆ«Snβˆ’1V~Ξ³,q​h𝒦+∫Snβˆ’1V~Ξ³,q​h𝒦dx)\displaystyle\frac{1}{2}\bigg(-\int_{S^{n-1}}\frac{\widetilde{V}_{\gamma,q}h}{\mathcal{K}}+\int_{S^{n-1}}\frac{\widetilde{V}_{\gamma,q}h}{\mathcal{K}}dx\bigg)
=\displaystyle= 0.\displaystyle 0.

∎

For the convenience of discussing Gauss curvature flow (3), we introduce a following functional for any tβ‰₯0t\geq 0,

(3.8) Φ⁑(Ξ©t)=1pβ€‹βˆ«Snβˆ’1f⁑(x)​hp​(x,t)​𝑑x,\displaystyle\Phi(\Omega_{t})=\frac{1}{p}\int_{S^{n-1}}f(x)h^{p}(x,t)dx,

where h⁑(β‹…,t)h(\cdot,t) is the support function of Ξ©t\Omega_{t} and pβ‰ 0p\neq 0. When p=0p=0, we write

(3.9) Φ⁑(Ξ©t)=∫Snβˆ’1log⁑h⁑(x,t)​f​(x)​𝑑x.\displaystyle\Phi(\Omega_{t})=\int_{S^{n-1}}\log h(x,t)f(x)dx.
Lemma 3.2.

The functional (3.8) and (3.9) are non-increasing along the flow (3) for any tβ‰₯0t\geq 0. That is, βˆ‚βˆ‚t​Φ​(Ξ©t)≀0\frac{\partial}{\partial t}\Phi(\Omega_{t})\leq 0.

Proof.

Firstly, we prove pβ‰ 0p\neq 0, by (3.8), (3.3), (3), (3.6) and ρn​𝒦​d​ξ=h​d​x\rho^{n}\mathcal{K}d\xi=hdx, we obtain the following result,

βˆ‚βˆ‚t​Φp​(Ξ©t)=\displaystyle\frac{\partial}{\partial t}\Phi_{p}(\Omega_{t})= ∫Snβˆ’1hpβˆ’1​f​(x)β€‹βˆ‚hβˆ‚t​𝑑x\displaystyle\int_{S^{n-1}}h^{p-1}f(x)\frac{\partial h}{\partial t}dx
=\displaystyle= ∫Snβˆ’1hpβˆ’1​f​(x)​(βˆ’ΞΈβ‘(t)​𝒦​hp​f​(x)V~Ξ³,q+h)​𝑑x\displaystyle\int_{S^{n-1}}h^{p-1}f(x)\bigg(-\theta(t)\frac{\mathcal{K}h^{p}f(x)}{\widetilde{V}_{\gamma,q}}+h\bigg)dx
=\displaystyle= βˆ’βˆ«Snβˆ’1V~Ξ³,q​h𝒦​𝑑x∫Snβˆ’1hp​f​(x)​𝑑x∫Snβˆ’1h2​pβˆ’1f2(x)𝒦(V~Ξ³,q)βˆ’1dx+∫Snβˆ’1hpf(x)dx\displaystyle-\frac{\int_{S^{n-1}}\widetilde{V}_{\gamma,q}\frac{h}{\mathcal{K}}dx}{\int_{S^{n-1}}h^{p}f(x)dx}\int_{S^{n-1}}h^{2p-1}f^{2}(x)\mathcal{K}(\widetilde{V}_{\gamma,q})^{-1}dx+\int_{S^{n-1}}h^{p}f(x)dx
=\displaystyle= (∫Snβˆ’1hpf(x)dx)βˆ’1{βˆ’βˆ«Snβˆ’1V~Ξ³,qh𝒦dx∫Snβˆ’1f2h2​pβˆ’1𝒦(V~Ξ³,q)βˆ’1dx\displaystyle\bigg(\int_{S^{n-1}}h^{p}f(x)dx\bigg)^{-1}\bigg\{-\int_{S^{n-1}}\widetilde{V}_{\gamma,q}\frac{h}{\mathcal{K}}dx\int_{S^{n-1}}f^{2}h^{2p-1}\mathcal{K}(\widetilde{V}_{\gamma,q})^{-1}dx
+(∫Snβˆ’1f(x)hpdx)2}\displaystyle+\bigg(\int_{S^{n-1}}f(x)h^{p}dx\bigg)^{2}\bigg\}
=\displaystyle= (∫Snβˆ’1hpf(x)dx)βˆ’1{βˆ’[(∫Snβˆ’1V~Ξ³,qh𝒦dx)12(∫Snβˆ’1f2h2​pβˆ’1𝒦(V~Ξ³,q)βˆ’1dx)12]2\displaystyle\bigg(\int_{S^{n-1}}h^{p}f(x)dx\bigg)^{-1}\bigg\{-\bigg[\bigg(\int_{S^{n-1}}\widetilde{V}_{\gamma,q}\frac{h}{\mathcal{K}}dx\bigg)^{\frac{1}{2}}\bigg(\int_{S^{n-1}}f^{2}h^{2p-1}\mathcal{K}(\widetilde{V}_{\gamma,q})^{-1}dx\bigg)^{\frac{1}{2}}\bigg]^{2}
+(∫Snβˆ’1f(x)hpdx)2}\displaystyle+\bigg(\int_{S^{n-1}}f(x)h^{p}dx\bigg)^{2}\bigg\}
=\displaystyle= (∫Snβˆ’1hpf(x)dx)βˆ’1{βˆ’[(∫Snβˆ’1((V~Ξ³,qh𝒦)12)2dx)12\displaystyle\bigg(\int_{S^{n-1}}h^{p}f(x)dx\bigg)^{-1}\bigg\{-\bigg[\bigg(\int_{S^{n-1}}\bigg(\bigg(\widetilde{V}_{\gamma,q}\frac{h}{\mathcal{K}}\bigg)^{\frac{1}{2}}\bigg)^{2}dx\bigg)^{\frac{1}{2}}
(∫Snβˆ’1((f2h2​pβˆ’1𝒦(V~Ξ³,q)βˆ’1)12)2dx)12]2+(∫Snβˆ’1f(x)hpdx)2}\displaystyle\bigg(\int_{S^{n-1}}\bigg(\bigg(f^{2}h^{2p-1}\mathcal{K}(\widetilde{V}_{\gamma,q})^{-1}\bigg)^{\frac{1}{2}}\bigg)^{2}dx\bigg)^{\frac{1}{2}}\bigg]^{2}+\bigg(\int_{S^{n-1}}f(x)h^{p}dx\bigg)^{2}\bigg\}
≀\displaystyle\leq (∫Snβˆ’1hpf(x)dx)βˆ’1{βˆ’[∫Snβˆ’1(V~Ξ³,qh𝒦)12(f2h2​pβˆ’1𝒦(V~Ξ³,q)βˆ’1)12dx]2\displaystyle\bigg(\int_{S^{n-1}}h^{p}f(x)dx\bigg)^{-1}\bigg\{-\bigg[\int_{S^{n-1}}\bigg(\widetilde{V}_{\gamma,q}\frac{h}{\mathcal{K}}\bigg)^{\frac{1}{2}}\bigg(f^{2}h^{2p-1}\mathcal{K}(\widetilde{V}_{\gamma,q})^{-1}\bigg)^{\frac{1}{2}}dx\bigg]^{2}
+(∫Snβˆ’1f(x)hpdx)2}\displaystyle+\bigg(\int_{S^{n-1}}f(x)h^{p}dx\bigg)^{2}\bigg\}
=\displaystyle= 0.\displaystyle 0.

By the equality condition of HΓΆlder inequality, we know that the above equality holds if and only if Ο„1​(V~Ξ³,q​h𝒦)12=(f2​h2​pβˆ’1​𝒦​(V~Ξ³,q)βˆ’1)12\tau_{1}\bigg(\widetilde{V}_{\gamma,q}\frac{h}{\mathcal{K}}\bigg)^{\frac{1}{2}}=\bigg(f^{2}h^{2p-1}\mathcal{K}(\widetilde{V}_{\gamma,q})^{-1}\bigg)^{\frac{1}{2}}, i.e.,

Ο„1​V~Ξ³,q​h1βˆ’p​det(hi​j+h​δi​j)=f.\displaystyle\tau_{1}\widetilde{V}_{\gamma,q}h^{1-p}\det(h_{ij}+h\delta_{ij})=f.

Next, we give proof of p=0p=0. Taking p=0p=0 in (3.3) and (3), from (3.9), (3.6) and ρn​𝒦​d​ξ=h​d​x\rho^{n}\mathcal{K}d\xi=hdx, we deduce that

βˆ‚βˆ‚t​Φ​(Ξ©t)=\displaystyle\frac{\partial}{\partial t}\Phi(\Omega_{t})= ∫Snβˆ’1f⁑(x)hβ€‹βˆ‚hβˆ‚t​𝑑x\displaystyle\int_{S^{n-1}}\frac{f(x)}{h}\frac{\partial h}{\partial t}dx
=\displaystyle= ∫Snβˆ’1f⁑(x)h​(βˆ’ΞΈβ‘(t)​𝒦​f​(x)V~Ξ³,q+h)​𝑑x\displaystyle\int_{S^{n-1}}\frac{f(x)}{h}\bigg(-\theta(t)\frac{\mathcal{K}f(x)}{\widetilde{V}_{\gamma,q}}+h\bigg)dx
=\displaystyle= βˆ’βˆ«Snβˆ’1V~Ξ³,q​h𝒦​𝑑x∫Snβˆ’1f⁑(x)​𝑑x∫Snβˆ’1f2​(x)h​V~Ξ³,q𝒦dx+∫Snβˆ’1f(x)dx\displaystyle-\frac{\int_{S^{n-1}}\widetilde{V}_{\gamma,q}\frac{h}{\mathcal{K}}dx}{\int_{S^{n-1}}f(x)dx}\int_{S^{n-1}}\frac{f^{2}(x)}{h\widetilde{V}_{\gamma,q}}\mathcal{K}dx+\int_{S^{n-1}}f(x)dx
=\displaystyle= (∫Snβˆ’1f(x)dx)βˆ’1{βˆ’βˆ«Snβˆ’1V~Ξ³,qh𝒦dx∫Snβˆ’1f2h​V~Ξ³,q𝒦dx+(∫Snβˆ’1f(x)dx)2}\displaystyle\bigg(\int_{S^{n-1}}f(x)dx\bigg)^{-1}\bigg\{-\int_{S^{n-1}}\widetilde{V}_{\gamma,q}\frac{h}{\mathcal{K}}dx\int_{S^{n-1}}\frac{f^{2}}{h\widetilde{V}_{\gamma,q}}\mathcal{K}dx+\bigg(\int_{S^{n-1}}f(x)dx\bigg)^{2}\bigg\}
=\displaystyle= (∫Snβˆ’1f(x)dx)βˆ’1{βˆ’[(∫Snβˆ’1V~Ξ³,qh𝒦dx)12(∫Snβˆ’1f2h​V~Ξ³,q𝒦dx)12]2\displaystyle\bigg(\int_{S^{n-1}}f(x)dx\bigg)^{-1}\bigg\{-\bigg[\bigg(\int_{S^{n-1}}\widetilde{V}_{\gamma,q}\frac{h}{\mathcal{K}}dx\bigg)^{\frac{1}{2}}\bigg(\int_{S^{n-1}}\frac{f^{2}}{h\widetilde{V}_{\gamma,q}}\mathcal{K}dx\bigg)^{\frac{1}{2}}\bigg]^{2}
+(∫Snβˆ’1f(x)dx)2}\displaystyle+\bigg(\int_{S^{n-1}}f(x)dx\bigg)^{2}\bigg\}
=\displaystyle= (∫Snβˆ’1f(x)dx)βˆ’1{βˆ’[(∫Snβˆ’1((V~Ξ³,qh𝒦)12)2dx)12(∫Snβˆ’1((f2h​V~Ξ³,q𝒦)12)2dx)12]2\displaystyle\bigg(\int_{S^{n-1}}f(x)dx\bigg)^{-1}\bigg\{-\bigg[\bigg(\int_{S^{n-1}}\bigg(\bigg(\widetilde{V}_{\gamma,q}\frac{h}{\mathcal{K}}\bigg)^{\frac{1}{2}}\bigg)^{2}dx\bigg)^{\frac{1}{2}}\bigg(\int_{S^{n-1}}\bigg(\bigg(\frac{f^{2}}{h\widetilde{V}_{\gamma,q}}\mathcal{K}\bigg)^{\frac{1}{2}}\bigg)^{2}dx\bigg)^{\frac{1}{2}}\bigg]^{2}
+(∫Snβˆ’1f(x)dx)2}\displaystyle+\bigg(\int_{S^{n-1}}f(x)dx\bigg)^{2}\bigg\}
≀\displaystyle\leq (∫Snβˆ’1f⁑(x)​𝑑x)βˆ’1​{βˆ’[∫Snβˆ’1(V~Ξ³,q​h𝒦)12​(f2h​V~Ξ³,q​𝒦)12​𝑑x]2+(∫Snβˆ’1f⁑(x)​𝑑x)2}\displaystyle\bigg(\int_{S^{n-1}}f(x)dx\bigg)^{-1}\bigg\{-\bigg[\int_{S^{n-1}}\bigg(\widetilde{V}_{\gamma,q}\frac{h}{\mathcal{K}}\bigg)^{\frac{1}{2}}\bigg(\frac{f^{2}}{h\widetilde{V}_{\gamma,q}}\mathcal{K}\bigg)^{\frac{1}{2}}dx\bigg]^{2}+\bigg(\int_{S^{n-1}}f(x)dx\bigg)^{2}\bigg\}
=\displaystyle= 0.\displaystyle 0.

We know that the above equality holds if and only if Ο„2​(V~Ξ³,q​h𝒦)12=(f2h​V~Ξ³,q​𝒦)12\tau_{2}\bigg(\widetilde{V}_{\gamma,q}\frac{h}{\mathcal{K}}\bigg)^{\frac{1}{2}}=\bigg(\frac{f^{2}}{h\widetilde{V}_{\gamma,q}}\mathcal{K}\bigg)^{\frac{1}{2}} by the equality condition of HΓΆlder inequality, i.e.,

Ο„2​V~Ξ³,q​h​det(hi​j+h​δi​j)=f.\displaystyle\tau_{2}\widetilde{V}_{\gamma,q}h\det(h_{ij}+h\delta_{ij})=f.

Combining the above two situations, Ξ©t\Omega_{t} satisfies (1.8) and (1.10) with 1Ο„1=θ​(t)​(pβ‰ 0)\frac{1}{\tau_{1}}=\theta(t)(p\neq 0) and 1Ο„2=θ​(t)​(p=0)\frac{1}{\tau_{2}}=\theta(t)(p=0). This completes proof of Lemma 3.2. ∎

4. Priori estimates

In this section, we establish the C0,C1C^{0},C^{1} and C2C^{2} estimates for the solutions to Eq. (3). In the following of this paper, we always assume that βˆ‚Ξ©0\partial\Omega_{0} is a smooth, closed and origin-symmetric strictly convex hypersurface in ℝn\mathbb{R}^{n}, h:Snβˆ’1Γ—[0,T)→ℝh:S^{n-1}\times[0,T)\rightarrow\mathbb{R} is a smooth even solution to Eq. (3) with the initial h⁑(β‹…,0)h(\cdot,0) the support function of Ξ©0\Omega_{0}. Here, TT is the maximal time for which the smooth solution exists to Eq. (3).

4.1. C0,C1C^{0},C^{1} estimates

In order to complete the C0C^{0} estimate, we firstly need to introduce the following Lemma which was proven by Chen and Li [7] for convex bodies.

Lemma 4.1.

[7, Lemma 2.6] Let Ξ©βˆˆπ’¦on\Omega\in\mathcal{K}^{n}_{o}, hh and ρ\rho be respectively support function and radial function of Ξ©\Omega, and xmaxx_{\max} and ΞΎmin\xi_{\min} be two points such that h⁑(xmax)=maxSnβˆ’1⁑hh(x_{\max})=\max_{S^{n-1}}h and ρ⁑(ΞΎmin)=minSnβˆ’1⁑ρ\rho(\xi_{\min})=\min_{S^{n-1}}\rho. Then,

maxSnβˆ’1⁑h=\displaystyle\max_{S^{n-1}}h= maxSnβˆ’1⁑ρandminSnβˆ’1⁑h=minSnβˆ’1⁑ρ,\displaystyle\max_{S^{n-1}}\rho\quad\text{and}\quad\min_{S^{n-1}}h=\min_{S^{n-1}}\rho,
h⁑(x)β‰₯\displaystyle h(x)\geq xβ‹…xmax​h​(xmax),βˆ€x∈Snβˆ’1,\displaystyle x\cdot x_{\max}h(x_{\max}),\quad\forall x\in S^{n-1},
ρ⁑(ΞΎ)​ξ⋅ξminβ‰₯\displaystyle\rho(\xi)\xi\cdot\xi_{\min}\geq ρ⁑(ΞΎmin),βˆ€ΞΎβˆˆSnβˆ’1.\displaystyle\rho(\xi_{\min}),\quad\forall\xi\in S^{n-1}.
Remark 4.2.

The results in Lemma 4.1 be true for any tβ‰₯0t\geq 0, for example, we can write

h⁑(x,t)β‰₯\displaystyle h(x,t)\geq xβ‹…xmaxt​h​(xmax,t),βˆ€x∈Snβˆ’1.\displaystyle x\cdot x^{t}_{\max}h(x_{\max},t),\quad\forall x\in S^{n-1}.
Lemma 4.3.

Assume pβ‰₯0p\geq 0, βˆ‚Ξ©t\partial\Omega_{t} be a smooth solution to the flow (3) in ℝn\mathbb{R}^{n} and ff is a positive smooth even function on Snβˆ’1S^{n-1}. Then, there is a positive constant CC independents of tt such that

(4.1) 1C≀h⁑(x,t)≀C,βˆ€(x,t)∈Snβˆ’1Γ—[0,T),\displaystyle\frac{1}{C}\leq h(x,t)\leq C,\ \ \forall(x,t)\in S^{n-1}\times[0,T),
(4.2) 1C≀ρ⁑(ΞΎ,t)≀C,βˆ€(ΞΎ,t)∈Snβˆ’1Γ—[0,T).\displaystyle\frac{1}{C}\leq\rho(\xi,t)\leq C,\ \ \forall(\xi,t)\in S^{n-1}\times[0,T).

Here, h⁑(x,t)h(x,t) and ρ⁑(ξ,t)\rho(\xi,t) are the support function and radial function of Ωt\Omega_{t}, respectively.

Proof.

We only give proof of (4.1), and (4.2) can be obtained by the first conclusion of Lemma 4.1 and (4.1).

Firstly, we prove the upper bound of (4.1). From monotonicity of Φ⁑(Ωt)\Phi(\Omega_{t}) in Lemma 3.2 and the second result of Lemma 4.1, there is following result for p>0p>0,

Φ⁑(Ξ©0)β‰₯\displaystyle\Phi(\Omega_{0})\geq Φ⁑(Ξ©t)=1pβ€‹βˆ«Snβˆ’1f⁑(x)​h​(x,t)p​𝑑x\displaystyle\Phi(\Omega_{t})=\frac{1}{p}\int_{S^{n-1}}f(x)h(x,t)^{p}dx
β‰₯\displaystyle\geq 1pβ€‹βˆ«Snβˆ’1f⁑(x)​[h⁑(xmax,t)​xβ‹…xmaxt]p​𝑑x\displaystyle\frac{1}{p}\int_{S^{n-1}}f(x)[h(x_{\max},t)x\cdot x^{t}_{\max}]^{p}dx
β‰₯\displaystyle\geq 1p∫{x∈Snβˆ’1:xβ‹…xmaxtβ‰₯12}f(x)[h(xmax,t)xβ‹…xmaxt]pdx\displaystyle\frac{1}{p}\int_{\{x\in S^{n-1}:x\cdot x^{t}_{\max}\geq\frac{1}{2}\}}f(x)[h(x_{\max},t)x\cdot x^{t}_{\max}]^{p}dx
β‰₯\displaystyle\geq 1p∫{x∈Snβˆ’1:xβ‹…xmaxtβ‰₯12}f(x)[12h(xmax,t)]pdx\displaystyle\frac{1}{p}\int_{\{x\in S^{n-1}:x\cdot x^{t}_{\max}\geq\frac{1}{2}\}}f(x)[\frac{1}{2}h(x_{\max},t)]^{p}dx
=\displaystyle= 1ph​(xmax,t)p2p∫{x∈Snβˆ’1:xβ‹…xmaxtβ‰₯12}f(x)dx\displaystyle\frac{1}{p}\frac{h(x_{\max},t)^{p}}{2^{p}}\int_{\{x\in S^{n-1}:x\cdot x^{t}_{\max}\geq\frac{1}{2}\}}f(x)dx
β‰₯\displaystyle\geq C​h​(xmax,t)p,\displaystyle Ch(x_{\max},t)^{p},

then,

suph⁑(xmax,t)≀(Φ⁑(Ξ©0)C)1p,\displaystyle\sup h(x_{\max},t)\leq\bigg(\frac{\Phi(\Omega_{0})}{C}\bigg)^{\frac{1}{p}},

where, h⁑(xmax,t)=maxSnβˆ’1⁑h⁑(x,t)h(x_{\max},t)=\max_{S^{n-1}}h(x,t) for any tt. Here, CC is a positive constant independents from tt.

Similarly, when p=0p=0, we have

Φ⁑(Ξ©0)β‰₯\displaystyle\Phi(\Omega_{0})\geq Φ⁑(Ξ©t)=∫Snβˆ’1f⁑(x)​log⁑h⁑(x,t)​𝑑x\displaystyle\Phi(\Omega_{t})=\int_{S^{n-1}}f(x)\log h(x,t)dx
β‰₯\displaystyle\geq ∫Snβˆ’1f⁑(x)​log⁑[h⁑(xmax,t)​xβ‹…xmaxt]​𝑑x\displaystyle\int_{S^{n-1}}f(x)\log[h(x_{\max},t)x\cdot x^{t}_{\max}]dx
β‰₯\displaystyle\geq logh(xmax,t)∫Snβˆ’1f(x)dx+∫{x∈Snβˆ’1:xβ‹…xmaxtβ‰₯12}f(x)log(xβ‹…xmaxt)\displaystyle\log h(x_{\max},t)\int_{S^{n-1}}f(x)dx+\int_{\{x\in S^{n-1}:x\cdot x^{t}_{\max}\geq\frac{1}{2}\}}f(x)\log(x\cdot x^{t}_{\max})
β‰₯\displaystyle\geq Clogh(xmax,t)βˆ’c∫{x∈Snβˆ’1:xβ‹…xmaxtβ‰₯12}f(x)dx\displaystyle C\log h(x_{\max},t)-c\int_{\{x\in S^{n-1}:x\cdot x^{t}_{\max}\geq\frac{1}{2}\}}f(x)dx
β‰₯\displaystyle\geq C​log⁑h⁑(xmax,t)βˆ’c1,\displaystyle C\log h(x_{\max},t)-c_{1},

then,

suph⁑(xmax,t)≀eΦ⁑(Ξ©0)+c1C.\displaystyle\sup h(x_{\max},t)\leq e^{\frac{\Phi(\Omega_{0})+c_{1}}{C}}.

Here, CC and c1c_{1} be positive constants independent on tt.

To prove the lower bound of h⁑(x,t)h(x,t), we use the contradiction. Let us assume that {tk}βŠ‚[0,T)\{t_{k}\}\subset[0,T) be a sequence such that h⁑(x,tk)h(x,t_{k}) is not uniformly bounded away from 00, i.e., minSnβˆ’1⁑h⁑(x,tk)β†’0\min_{S^{n-1}}h(x,t_{k})\rightarrow 0 as kβ†’βˆžk\rightarrow\infty. On the other hand, making use of the upper bound, by Blaschke-Selection theorem, there is a subsequence in {Ξ©tk}\{\Omega_{t_{k}}\}, for convenience, which is still denoted by {Ξ©tk}\{\Omega_{t_{k}}\}, such that {Ξ©tk}β†’Ξ©~\{\Omega_{t_{k}}\}\rightarrow\widetilde{\Omega} as kβ†’βˆžk\rightarrow\infty, where Ξ©~\widetilde{\Omega} is a origin-symmetric convex body. Then, we obtain minSnβˆ’1⁑h⁑(Ξ©~,β‹…)=limkβ†’βˆžminSnβˆ’1⁑h⁑(Ξ©tk,β‹…)=0\min_{S^{n-1}}h(\widetilde{\Omega},\cdot)=\lim_{k\rightarrow\infty}\min_{S^{n-1}}h(\Omega_{t_{k}},\cdot)=0. This implies that Ξ©~\widetilde{\Omega} is contained in a lower-dimensional subspace in ℝn\mathbb{R}^{n}. This can lead to ρ⁑(ΞΎ,tk)β†’0\rho(\xi,t_{k})\rightarrow 0 as kβ†’βˆžk\rightarrow\infty almost everywhere with respect to the spherical Lebesgue measure. According to bounded convergence theorem and formula (3.7), we can derive

IΞ³,q​(Ξ©~)=\displaystyle I_{\gamma,q}(\widetilde{\Omega})= 12β€‹βˆ«Ξ©~V~Ξ³,q​(Ξ©~,y)​𝑑y\displaystyle\frac{1}{2}\int_{\widetilde{\Omega}}\widetilde{V}_{\gamma,q}(\widetilde{\Omega},y)dy
=\displaystyle= limkβ†’βˆž12β€‹βˆ«Snβˆ’1∫0ρ⁑(ΞΎ,tk)V~Ξ³,q​(Ξ©~,ρ⁑(ΞΎ,tk))​ρ​(ΞΎ,tk)nβˆ’1​𝑑ρ​𝑑ξ→0.\displaystyle\lim_{k\rightarrow\infty}\frac{1}{2}\int_{S^{n-1}}\int_{0}^{\rho(\xi,t_{k})}\widetilde{V}_{\gamma,q}(\widetilde{\Omega},\rho(\xi,t_{k}))\rho(\xi,t_{k})^{n-1}d\rho d\xi\rightarrow 0.

However, Lemma 3.1 shows that

IΞ³,q​(Ξ©~)=IΞ³,q​(Ξ©0)=c​(positive constant)β‰ 0,\displaystyle I_{\gamma,q}(\widetilde{\Omega})=I_{\gamma,q}(\Omega_{0})=c~~\text{(positive constant)}\neq 0,

which is a contradiction. It follows that h⁑(x,t)h(x,t) has a uniform lower bound. Therefore, we complete estimate of Lemma 4.3. ∎

Lemma 4.4.

Let pβ‰₯0p\geq 0, βˆ‚Ξ©t\partial\Omega_{t} be a smooth solution to the flow (3) in ℝn\mathbb{R}^{n} and ff is a positive smooth even function on Snβˆ’1S^{n-1}. Then, there is a positive constant CC independents of tt such that

(4.3) |βˆ‡h​(x,t)|≀C,βˆ€(x,t)∈Snβˆ’1Γ—[0,T),\displaystyle|\nabla h(x,t)|\leq C,\quad\forall(x,t)\in S^{n-1}\times[0,T),

and

(4.4) |βˆ‡Οβ€‹(ΞΎ,t)|≀C,βˆ€(ΞΎ,t)∈Snβˆ’1Γ—[0,T).\displaystyle|\nabla\rho(\xi,t)|\leq C,\quad\forall(\xi,t)\in S^{n-1}\times[0,T).
Proof.

The desired results immediately follows from Lemma 4.3 and the identities (see e.g. [18]) as follows

h=ρ2ρ2+|βˆ‡Ο|2,ρ2=h2+|βˆ‡h|2.\displaystyle h=\frac{\rho^{2}}{\sqrt{\rho^{2}+|\nabla\rho|^{2}}},\qquad\rho^{2}=h^{2}+|\nabla h|^{2}.

∎

Lemma 4.5.

Suppose pβ‰₯0p\geq 0, βˆ‚Ξ©t\partial\Omega_{t} be a smooth solution to the flow (3) in ℝn\mathbb{R}^{n} and ff is a positive smooth even function on Snβˆ’1S^{n-1}. There always exists a positive constant CC independents of tt, such that

1C≀θ⁑(t)≀C,t∈[0,T).\displaystyle\frac{1}{C}\leq\theta(t)\leq C,\quad t\in[0,T).
Proof.

By the definition of θ⁑(t)\theta(t),

θ⁑(t)=∫Snβˆ’1V~Ξ³,q​(Ξ©t,β‹…)​ρn​(ΞΎ,t)β€‹π‘‘ΞΎβˆ«Snβˆ’1hp​(x,t)​f​(x)​𝑑x.\displaystyle\theta(t)=\frac{\int_{S^{n-1}}\widetilde{V}_{\gamma,q}(\Omega_{t},\cdot)\rho^{n}(\xi,t)d\xi}{\int_{S^{n-1}}h^{p}(x,t)f(x)dx}.

Let Ξ©tβˆˆπ’¦on\Omega_{t}\in\mathcal{K}^{n}_{o}, z∈Ωtz\in\Omega_{t}, yβˆˆβˆ‚Ξ©ty\in\partial\Omega_{t}, u∈Snβˆ’1u\in S^{n-1}, yβˆ’z=s​uy-z=su, then, d​z=βˆ’snβˆ’1​d​s​d​udz=-s^{n-1}dsdu, y=ρΩt​(u)​uy=\rho_{\Omega_{t}}(u)u, z=ρΩt​(u)​uβˆ’s​uz=\rho_{\Omega_{t}}(u)u-su and s∈[0,ρΩt,z​(u)]s\in[0,\rho_{\Omega_{t},z}(u)]. Thus,

V~Ξ³,q​(Ξ©t,y)=\displaystyle\widetilde{V}_{\gamma,q}(\Omega_{t},y)= 2eβˆ’|y|2/2∫Ωteβˆ’|z|2/2|zβˆ’y|nβˆ’q+1dz\displaystyle 2e^{-|y|^{2}/2}\int_{\Omega_{t}}\frac{e^{-|z|^{2}/2}}{|z-y|^{n-q+1}}dz
=\displaystyle= 2eβˆ’|ρΩt(u)u|2/2∫Snβˆ’1∫0ρΩt,z​(u)eβˆ’|ρΩt(u)uβˆ’su|2/2snβˆ’1snβˆ’q+1dsdu\displaystyle 2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}\int_{S^{n-1}}\int_{0}^{\rho_{\Omega_{t},z}(u)}\frac{e^{-|\rho_{\Omega_{t}}(u)u-su|^{2}/2}s^{n-1}}{s^{n-q+1}}dsdu
(4.5) =\displaystyle= 2eβˆ’|ρΩt(u)u|2/2∫Snβˆ’1∫0ρΩt,z​(u)eβˆ’|ρΩt(u)uβˆ’su|2/2sqβˆ’2dsdu,\displaystyle 2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}\int_{S^{n-1}}\int_{0}^{\rho_{\Omega_{t},z}(u)}e^{-|\rho_{\Omega_{t}}(u)u-su|^{2}/2}s^{q-2}dsdu,

from the C0C^{0} estimate, it suffices to have

(4.6) 1C≀V~Ξ³,q​(Ξ©t,y)≀C.\displaystyle\frac{1}{C}\leq\widetilde{V}_{\gamma,q}(\Omega_{t},y)\leq C.

Therefore, the upper and lower bound of θ⁑(t)\theta(t) can be directly obtained from the Lemma 4.3 and (4.6). ∎

4.2. C2C^{2} estimate

In this subsection, we establish the upper and lower bounds of principal curvature. This will shows that Eq. (3) is uniformly parabolic. The technique used in this proof was first introduced by Tso [28] to derive the upper bound of the Gauss curvature.

By Lemma 4.3 and Lemma 4.4, if hh is a smooth even solution of Eq. (3) on Snβˆ’1Γ—[0,T)S^{n-1}\times[0,T) and ff is positive smooth even function on Snβˆ’1S^{n-1}, then along the flow (3) for [0,T),βˆ‡h+h​x[0,T),\nabla h+hx, and hh are smooth functions whose ranges are within some bounded domain Ξ©[0,T)\Omega_{[0,T)} and bounded interval I[0,T)I_{[0,T)}, respectively. Here Ξ©[0,T)\Omega_{[0,T)} and I[0,T)I_{[0,T)} depend only on the upper and lower bounds of hh on [0,T)[0,T).

Lemma 4.6.

For q>2q>2 and pβ‰₯0p\geq 0, assume βˆ‚Ξ©t\partial\Omega_{t} be a smooth solution to the flow (3) in ℝn\mathbb{R}^{n} and ff is a positive smooth even function on Snβˆ’1S^{n-1}. There is a positive constant CC depending on β€–fβ€–C0​(Snβˆ’1),β€–fβ€–C1​(Snβˆ’1),β€–fβ€–C2​(Snβˆ’1)\|f\|_{C^{0}(S^{n-1})},\|f\|_{C^{1}(S^{n-1})},\|f\|_{C^{2}(S^{n-1})}, β€–hβ€–C0​(Snβˆ’1Γ—[0,T)𝐢𝐿𝑂𝑆𝐸\|h\|_{C^{0}(S^{n-1}\times[0,T)}, β€–hβ€–C1​(Snβˆ’1Γ—[0,T)𝐢𝐿𝑂𝑆𝐸\|h\|_{C^{1}(S^{n-1}\times[0,T)} and β€–ΞΈβ€–C0​(Snβˆ’1Γ—[0,T)𝐢𝐿𝑂𝑆𝐸\|\theta\|_{C^{0}(S^{n-1}\times[0,T)}, such that the principal curvatures ΞΊi\kappa_{i} of Ξ©t\Omega_{t}, i=1,β‹―,nβˆ’1i=1,\cdots,n-1, are bounded from above and below, satisfying

1C≀κi​(x,t)≀C,βˆ€(x,t)∈Snβˆ’1Γ—[0,T).\displaystyle\frac{1}{C}\leq\kappa_{i}(x,t)\leq C,\quad\forall(x,t)\in S^{n-1}\times[0,T).
Proof.

The proof is divided into two parts: in the first part, we derive an upper bound for the Gauss curvature 𝒦⁑(x,t)\mathcal{K}(x,t); in the second part, we give an estimate of bound above for the principal radii bi​j=hi​j+h​δi​jb_{ij}=h_{ij}+h\delta_{ij}.

Step 1: Prove 𝒦≀C\mathcal{K}\leq C.

Firstly, we construct the following auxiliary function,

W⁑(x,t)=θ⁑(t)​V~Ξ³,qβˆ’1​hp​fβ€‹π’¦βˆ’hhβˆ’Ξ΅0β‰‘βˆ’hthβˆ’Ξ΅0,\displaystyle W(x,t)=\frac{\theta(t)\widetilde{V}_{\gamma,q}^{-1}h^{p}f\mathcal{K}-h}{h-\varepsilon_{0}}\equiv\frac{-h_{t}}{h-\varepsilon_{0}},

where

Ξ΅0=12​minSnβˆ’1Γ—[0,T)⁑h⁑(x,t)>0,ht=βˆ‚hβˆ‚t.\displaystyle\varepsilon_{0}=\frac{1}{2}\min_{S^{n-1}\times[0,T)}h(x,t)>0,\quad h_{t}=\frac{\partial h}{\partial t}.

For any fixed t∈[0,T)t\in[0,T), we assume that W⁑(x0,t)=maxSnβˆ’1⁑W⁑(x,t)W(x_{0},t)=\max_{S^{n-1}}W(x,t) is the spatial maximum of WW. Then at (x0,t)(x_{0},t), we have

(4.7) 0=βˆ‡iW=βˆ’ht​ihβˆ’Ξ΅0+ht​hi(hβˆ’Ξ΅0)2,\displaystyle 0=\nabla_{i}W=\frac{-h_{ti}}{h-\varepsilon_{0}}+\frac{h_{t}h_{i}}{(h-\varepsilon_{0})^{2}},

and from (4.7), at (x0,t)(x_{0},t), we also get

0β‰₯βˆ‡i​iW=\displaystyle 0\geq\nabla_{ii}W= βˆ’ht​i​ihβˆ’Ξ΅0+ht​i​hi(hβˆ’Ξ΅0)2+ht​i​hi+ht​hi​i(hβˆ’Ξ΅0)2βˆ’ht​hi​(2​(hβˆ’Ξ΅0)​hi)(hβˆ’Ξ΅0)4\displaystyle\frac{-h_{tii}}{h-\varepsilon_{0}}+\frac{h_{ti}h_{i}}{(h-\varepsilon_{0})^{2}}+\frac{h_{ti}h_{i}+h_{t}h_{ii}}{(h-\varepsilon_{0})^{2}}-\frac{h_{t}h_{i}(2(h-\varepsilon_{0})h_{i})}{(h-\varepsilon_{0})^{4}}
=\displaystyle= βˆ’ht​i​ihβˆ’Ξ΅0+2​ht​i​hi+ht​hi​i(hβˆ’Ξ΅0)2βˆ’2​ht​hi​hi(hβˆ’Ξ΅0)3\displaystyle\frac{-h_{tii}}{h-\varepsilon_{0}}+\frac{2h_{ti}h_{i}+h_{t}h_{ii}}{(h-\varepsilon_{0})^{2}}-\frac{2h_{t}h_{i}h_{i}}{(h-\varepsilon_{0})^{3}}
=\displaystyle= βˆ’ht​i​ihβˆ’Ξ΅0+2​ht​i​hi+ht​hi​i(hβˆ’Ξ΅0)2+2​ht​i​hi(hβˆ’Ξ΅0)2\displaystyle\frac{-h_{tii}}{h-\varepsilon_{0}}+\frac{2h_{ti}h_{i}+h_{t}h_{ii}}{(h-\varepsilon_{0})^{2}}+\frac{2h_{ti}h_{i}}{(h-\varepsilon_{0})^{2}}
(4.8) =\displaystyle= βˆ’ht​i​ihβˆ’Ξ΅0+ht​hi​i(hβˆ’Ξ΅0)2.\displaystyle\frac{-h_{tii}}{h-\varepsilon_{0}}+\frac{h_{t}h_{ii}}{(h-\varepsilon_{0})^{2}}.

From (4.8), we obtain

βˆ’ht​i​iβ‰€βˆ’ht​hi​ihβˆ’Ξ΅0,-h_{tii}\leq\frac{-h_{t}h_{ii}}{h-\varepsilon_{0}},

hence,

βˆ’ht​i​iβˆ’ht​δi​i≀\displaystyle-h_{tii}-h_{t}\delta_{ii}\leq βˆ’ht​hi​ihβˆ’Ξ΅0βˆ’ht​δi​i=βˆ’hthβˆ’Ξ΅0​(hi​i+(hβˆ’Ξ΅0)​δi​i)\displaystyle\frac{-h_{t}h_{ii}}{h-\varepsilon_{0}}-h_{t}\delta_{ii}=\frac{-h_{t}}{h-\varepsilon_{0}}(h_{ii}+(h-\varepsilon_{0})\delta_{ii})
(4.9) =\displaystyle= W⁑(hi​i+h​δi​iβˆ’Ο΅0​δi​i)=W⁑(bi​iβˆ’Ξ΅0​δi​i).\displaystyle W(h_{ii}+h\delta_{ii}-\epsilon_{0}\delta_{ii})=W(b_{ii}-\varepsilon_{0}\delta_{ii}).

At (x0,t)(x_{0},t), we also have

(4.10) βˆ‚βˆ‚t​W=\displaystyle\frac{\partial}{\partial t}W= βˆ’ht​thβˆ’Ο΅0+ht2(hβˆ’Ο΅0)2\displaystyle\frac{-h_{tt}}{h-\epsilon_{0}}+\frac{h_{t}^{2}}{(h-\epsilon_{0})^{2}}
=\displaystyle= f(hβˆ’Ο΅0)​[βˆ‚(θ⁑(t)​V~Ξ³,qβˆ’1​hp)βˆ‚t​𝒦+θ⁑(t)​V~Ξ³,qβˆ’1​hpβ€‹βˆ‚(det(βˆ‡2h+h​I))βˆ’1βˆ‚t]+W+W2\displaystyle\frac{f}{(h-\epsilon_{0})}\bigg[\frac{\partial(\theta(t)\widetilde{V}_{\gamma,q}^{-1}h^{p})}{\partial t}\mathcal{K}+\theta(t)\widetilde{V}_{\gamma,q}^{-1}h^{p}\frac{\partial(\det(\nabla^{2}h+hI))^{-1}}{\partial t}\bigg]+W+W^{2}
=\displaystyle= f(hβˆ’Ο΅0)​[(βˆ‚ΞΈβ‘(t)βˆ‚t​V~Ξ³,qβˆ’1​hp+θ⁑(t)β€‹βˆ‚(V~Ξ³,qβˆ’1​hp)βˆ‚t)​𝒦+θ⁑(t)​V~Ξ³,qβˆ’1​hpβ€‹βˆ‚(det(βˆ‡2h+h​I))βˆ’1βˆ‚t]\displaystyle\frac{f}{(h-\epsilon_{0})}\bigg[\bigg(\frac{\partial\theta(t)}{\partial t}\widetilde{V}_{\gamma,q}^{-1}h^{p}+\theta(t)\frac{\partial(\widetilde{V}_{\gamma,q}^{-1}h^{p})}{\partial t}\bigg)\mathcal{K}+\theta(t)\widetilde{V}_{\gamma,q}^{-1}h^{p}\frac{\partial(\det(\nabla^{2}h+hI))^{-1}}{\partial t}\bigg]
+W+W2.\displaystyle+W+W^{2}.

Here, we firstly compute βˆ‚V~Ξ³,qβˆ‚t\frac{\partial\widetilde{V}_{\gamma,q}}{\partial t}. Recall (4.5), we know that for u∈Snβˆ’1u\in S^{n-1},

V~Ξ³,q(Ξ©t,y)=2eβˆ’|ρΩt(u)u|2/2∫Snβˆ’1∫0ρΩt,z​(u)eβˆ’|ρΩt(u)uβˆ’su|2/2sqβˆ’2dsdu.\displaystyle\widetilde{V}_{\gamma,q}(\Omega_{t},y)=2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}\int_{S^{n-1}}\int_{0}^{\rho_{\Omega_{t},z}(u)}e^{-|\rho_{\Omega_{t}}(u)u-su|^{2}/2}s^{q-2}dsdu.

Then,

βˆ‚V~Ξ³,qβˆ‚t=\displaystyle\frac{\partial\widetilde{V}_{\gamma,q}}{\partial t}= βˆ’2eβˆ’|ρΩt(u)u|2/2|ρΩt(u)u|βˆ‚ΟΞ©t​(u)βˆ‚tu∫Snβˆ’1∫0ρΩt,z​(u)eβˆ’|ρΩt(u)uβˆ’su|2/2sqβˆ’2dsdu\displaystyle-2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}|\rho_{\Omega_{t}}(u)u|\frac{\partial\rho_{\Omega_{t}}(u)}{\partial t}u\int_{S^{n-1}}\int_{0}^{\rho_{\Omega_{t},z}(u)}e^{-|\rho_{\Omega_{t}}(u)u-su|^{2}/2}s^{q-2}dsdu
(4.11) +2eβˆ’|ρΩt(u)u|2/2∫Snβˆ’1ρΩt,z(u)qβˆ’2eβˆ’|ρΩt(u)uβˆ’ΟΞ©t,z(u)u|2/2βˆ‚ΟΞ©t,z​(u)βˆ‚tdu,\displaystyle+2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}\int_{S^{n-1}}\rho_{\Omega_{t},z}(u)^{q-2}e^{-|\rho_{\Omega_{t}}(u)u-\rho_{\Omega_{t},z}(u)u|^{2}/2}\frac{\partial\rho_{\Omega_{t},z}(u)}{\partial t}du,

where ρΩt,z​(u)=h⁑(Ξ©t,x)βˆ’zβ‹…xuβ‹…x\rho_{\Omega_{t},z}(u)=\frac{h(\Omega_{t},x)-z\cdot x}{u\cdot x}, z=βˆ‡hz=\nabla h, at x0x_{0}, there is

βˆ‚ΟΞ©t,z​(u)βˆ‚t=\displaystyle\frac{\partial\rho_{\Omega_{t},z}(u)}{\partial t}= βˆ‚hβˆ‚tβˆ’βˆ‚zβˆ‚tβ‹…xuβ‹…x=βˆ‚hβˆ‚tβˆ’(βˆ‡h)tβ‹…xuβ‹…x\displaystyle\frac{\frac{\partial h}{\partial t}-\frac{\partial z}{\partial t}\cdot x}{u\cdot x}=\frac{\frac{\partial h}{\partial t}-(\nabla h)_{t}\cdot x}{u\cdot x}
=\displaystyle= βˆ‚hβˆ‚tuβ‹…xβˆ’xuβ‹…x​(βˆ‘ihi​t​ei+ht​x)\displaystyle\frac{\frac{\partial h}{\partial t}}{u\cdot x}-\frac{x}{u\cdot x}\bigg(\sum_{i}h_{it}e_{i}+h_{t}x\bigg)
=\displaystyle= βˆ‚hβˆ‚tuβ‹…xβˆ’xuβ‹…x​(βˆ‘iht​hihβˆ’Ξ΅0​ei+ht​x).\displaystyle\frac{\frac{\partial h}{\partial t}}{u\cdot x}-\frac{x}{u\cdot x}\bigg(\sum_{i}\frac{h_{t}h_{i}}{h-\varepsilon_{0}}e_{i}+h_{t}x\bigg).

Therefore, from Lemma 4.3 and (4.11), we can obtain

βˆ‚V~Ξ³,qβˆ‚t≀\displaystyle\frac{\partial\widetilde{V}_{\gamma,q}}{\partial t}\leq 2eβˆ’|ρΩt(u)u|2/2∫Snβˆ’1ρΩt,z(u)qβˆ’2eβˆ’|ρΩt(u)uβˆ’ΟΞ©t,z(u)u|2/2[βˆ‚hβˆ‚tuβ‹…x\displaystyle 2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}\int_{S^{n-1}}\rho_{\Omega_{t},z}(u)^{q-2}e^{-|\rho_{\Omega_{t}}(u)u-\rho_{\Omega_{t},z}(u)u|^{2}/2}\bigg[\frac{\frac{\partial h}{\partial t}}{u\cdot x}
βˆ’xuβ‹…x(βˆ‘iht​hihβˆ’Ξ΅0+htx)]du\displaystyle-\frac{x}{u\cdot x}\bigg(\sum_{i}\frac{h_{t}h_{i}}{h-\varepsilon_{0}}+h_{t}x\bigg)\bigg]du
=\displaystyle= 2eβˆ’|ρΩt(u)u|2/2∫Snβˆ’1ρΩt,z(u)qβˆ’2eβˆ’|ρΩt(u)uβˆ’ΟΞ©t,z(u)u|2/2[βˆ’W⁑(hβˆ’Ο΅0)uβ‹…x\displaystyle 2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}\int_{S^{n-1}}\rho_{\Omega_{t},z}(u)^{q-2}e^{-|\rho_{\Omega_{t}}(u)u-\rho_{\Omega_{t},z}(u)u|^{2}/2}\bigg[\frac{-W(h-\epsilon_{0})}{u\cdot x}
βˆ’xuβ‹…x(βˆ‘iβˆ’W⁑(hβˆ’Ο΅0)​hihβˆ’Ξ΅0βˆ’W(hβˆ’Ο΅0)x)]du\displaystyle-\frac{x}{u\cdot x}\bigg(\sum_{i}\frac{-W(h-\epsilon_{0})h_{i}}{h-\varepsilon_{0}}-W(h-\epsilon_{0})x\bigg)\bigg]du
≀\displaystyle\leq 2eβˆ’|ρΩt(u)u|2/2∫Snβˆ’1ρΩt,z(u)qβˆ’2eβˆ’|ρΩt(u)uβˆ’ΟΞ©t,z(u)u|2/2xuβ‹…x(βˆ‘iW⁑(hβˆ’Ο΅0)​hihβˆ’Ξ΅0\displaystyle 2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}\int_{S^{n-1}}\rho_{\Omega_{t},z}(u)^{q-2}e^{-|\rho_{\Omega_{t}}(u)u-\rho_{\Omega_{t},z}(u)u|^{2}/2}\frac{x}{u\cdot x}\bigg(\sum_{i}\frac{W(h-\epsilon_{0})h_{i}}{h-\varepsilon_{0}}
OPEN+W⁑(hβˆ’Ο΅0)​x)​d​u\displaystyle+W(h-\epsilon_{0})x\bigg)du
(4.12) ≀\displaystyle\leq C1​W​(x0,t).\displaystyle C_{1}W(x_{0},t).
βˆ‚ΞΈβ‘(t)βˆ‚t=\displaystyle\frac{\partial\theta(t)}{\partial t}= βˆ‚βˆ‚t​(∫Snβˆ’1V~Ξ³,q​ρnβ€‹π‘‘ΞΎβˆ«Snβˆ’1hp​f​(x)​𝑑x)\displaystyle\frac{\partial}{\partial t}\bigg(\frac{\int_{S^{n-1}}\widetilde{V}_{\gamma,q}\rho^{n}d\xi}{\int_{S^{n-1}}h^{p}f(x)dx}\bigg)
=\displaystyle= ∫Snβˆ’1βˆ‚V~Ξ³,qβˆ‚t​ρn​𝑑ξ+nβ€‹βˆ«Snβˆ’1V~Ξ³,q​ρnβˆ’1β€‹βˆ‚Οβˆ‚tβ€‹π‘‘ΞΎβˆ«Snβˆ’1hp​f​(x)​𝑑xβˆ’pβ€‹βˆ«Snβˆ’1V~Ξ³,q​ρnβ€‹π‘‘ΞΎβ€‹βˆ«Snβˆ’1hpβˆ’1​f​(x)β€‹βˆ‚hβˆ‚t​𝑑x(∫Snβˆ’1hp​f​(x)​𝑑x)2.\displaystyle\frac{\int_{S^{n-1}}\frac{\partial\widetilde{V}_{\gamma,q}}{\partial t}\rho^{n}d\xi+n\int_{S^{n-1}}\widetilde{V}_{\gamma,q}\rho^{n-1}\frac{\partial\rho}{\partial t}d\xi}{\int_{S^{n-1}}h^{p}f(x)dx}-\frac{p\int_{S^{n-1}}\widetilde{V}_{\gamma,q}\rho^{n}d\xi\int_{S^{n-1}}h^{p-1}f(x)\frac{\partial h}{\partial t}dx}{\bigg(\int_{S^{n-1}}h^{p}f(x)dx\bigg)^{2}}.

By ρ2=h2+|βˆ‡h|2\rho^{2}=h^{2}+|\nabla h|^{2} and (x0,t)(x_{0},t) is a maximum point of WW, we obtain

(4.13) βˆ‚Οβˆ‚t=Οβˆ’1​(h​ht+βˆ‘hk​hk​t)=Οβˆ’1​W​(Ο΅0​hβˆ’Ο2)β‰€Οβˆ’1​W​(x0,t)​(Ο΅0​hβˆ’Ο2).\displaystyle\frac{\partial\rho}{\partial t}=\rho^{-1}(hh_{t}+\sum h_{k}h_{kt})=\rho^{-1}W(\epsilon_{0}h-\rho^{2})\leq\rho^{-1}W(x_{0},t)(\epsilon_{0}h-\rho^{2}).

From (4.1), (4.2), (4.6), (4.12) and (4.13), we can get

(4.14) βˆ‚ΞΈβ‘(t)βˆ‚t≀C2​W​(x0,t).\displaystyle\frac{\partial\theta(t)}{\partial t}\leq C_{2}W(x_{0},t).

For pβ‰₯0p\geq 0, (4.1), (4.6) and (4.12) tell us that

βˆ‚(V~Ξ³,qβˆ’1​hp)βˆ‚t=\displaystyle\frac{\partial(\widetilde{V}_{\gamma,q}^{-1}h^{p})}{\partial t}= βˆ’(V~Ξ³,q)βˆ’2​V~Ξ³,qβˆ‚t​hp+(V~Ξ³,q)βˆ’1β€‹βˆ‚(hp)βˆ‚t\displaystyle-(\widetilde{V}_{\gamma,q})^{-2}\frac{\widetilde{V}_{\gamma,q}}{\partial t}h^{p}+(\widetilde{V}_{\gamma,q})^{-1}\frac{\partial(h^{p})}{\partial t}
=\displaystyle= βˆ’(V~Ξ³,q)βˆ’2​V~Ξ³,qβˆ‚t​hp+(V~Ξ³,q)βˆ’1​p​hpβˆ’1β€‹βˆ‚hβˆ‚t\displaystyle-(\widetilde{V}_{\gamma,q})^{-2}\frac{\widetilde{V}_{\gamma,q}}{\partial t}h^{p}+(\widetilde{V}_{\gamma,q})^{-1}ph^{p-1}\frac{\partial h}{\partial t}
(4.15) =\displaystyle= βˆ’(V~Ξ³,q)βˆ’2​V~Ξ³,qβˆ‚t​hpβˆ’p​(V~Ξ³,q)βˆ’1​hpβˆ’1​W​(hβˆ’Ο΅0)<0.\displaystyle-(\widetilde{V}_{\gamma,q})^{-2}\frac{\widetilde{V}_{\gamma,q}}{\partial t}h^{p}-p(\widetilde{V}_{\gamma,q})^{-1}h^{p-1}W(h-\epsilon_{0})<0.

We use (2.5), (4.9) and recall bi​j=βˆ‡i​jh+h​δi​jb_{ij}=\nabla_{ij}h+h\delta_{ij} may give

βˆ‚(det(βˆ‡2h+h​I))βˆ’1βˆ‚t=\displaystyle\frac{\partial(\det(\nabla^{2}h+hI))^{-1}}{\partial t}= βˆ’(det(βˆ‡2h+h​I))βˆ’2β€‹βˆ‚(det(βˆ‡2h+h​I))βˆ‚bi​jβ€‹βˆ‚(βˆ‡2h+h​I)βˆ‚t\displaystyle-(\det(\nabla^{2}h+hI))^{-2}\frac{\partial(\det(\nabla^{2}h+hI))}{\partial b_{ij}}\frac{\partial(\nabla^{2}h+hI)}{\partial t}
=\displaystyle= βˆ’(det(βˆ‡2h+h​I))βˆ’2β€‹βˆ‚(det(βˆ‡2h+h​I))βˆ‚bi​j​(ht​i​j+ht​δi​j)\displaystyle-(\det(\nabla^{2}h+hI))^{-2}\frac{\partial(\det(\nabla^{2}h+hI))}{\partial b_{ij}}(h_{tij}+h_{t}\delta_{ij})
≀\displaystyle\leq (det(βˆ‡2h+h​I))βˆ’2β€‹βˆ‚(det(βˆ‡2h+h​I))βˆ‚bi​j​W​(bi​jβˆ’Ξ΅0​δi​j)\displaystyle(\det(\nabla^{2}h+hI))^{-2}\frac{\partial(\det(\nabla^{2}h+hI))}{\partial b_{ij}}W(b_{ij}-\varepsilon_{0}\delta_{ij})
(4.16) ≀\displaystyle\leq 𝒦​W​((nβˆ’1)βˆ’Ξ΅0​(nβˆ’1)​𝒦1nβˆ’1).\displaystyle\mathcal{K}W((n-1)-\varepsilon_{0}(n-1)\mathcal{K}^{\frac{1}{n-1}}).

where the last inequality uses

βˆ‘ibi​iβ‰₯(nβˆ’1)​𝒦1nβˆ’1.\displaystyle\sum_{i}b^{ii}\geq(n-1)\mathcal{K}^{\frac{1}{n-1}}.

Therefore, from (4.6), (4.14), (4.15) and (4.16), we have following conclusion at (x0,t)(x_{0},t) in (4.10),

βˆ‚βˆ‚t​W≀\displaystyle\frac{\partial}{\partial t}W\leq f(hβˆ’Ο΅0)​[(βˆ‚ΞΈβ‘(t)βˆ‚t​V~Ξ³,qβˆ’1​hp)​𝒦+θ⁑(t)​V~Ξ³,qβˆ’1​hpβ€‹βˆ‚(det(βˆ‡2h+h​I))βˆ’1βˆ‚t]+W+W2\displaystyle\frac{f}{(h-\epsilon_{0})}\bigg[\bigg(\frac{\partial\theta(t)}{\partial t}\widetilde{V}_{\gamma,q}^{-1}h^{p}\bigg)\mathcal{K}+\theta(t)\widetilde{V}_{\gamma,q}^{-1}h^{p}\frac{\partial(\det(\nabla^{2}h+hI))^{-1}}{\partial t}\bigg]+W+W^{2}
(4.17) ≀\displaystyle\leq 1hβˆ’Ξ΅0​(C3​W2+f​θ​hp​V~Ξ³,qβˆ’1​𝒦​W​((nβˆ’1)βˆ’Ξ΅0​(nβˆ’1)​𝒦1nβˆ’1))+W+W2.\displaystyle\frac{1}{h-\varepsilon_{0}}\bigg(C_{3}W^{2}+f\theta h^{p}\widetilde{V}_{\gamma,q}^{-1}\mathcal{K}W((n-1)-\varepsilon_{0}(n-1)\mathcal{K}^{\frac{1}{n-1}})\bigg)+W+W^{2}.

If W⁑(x,t)>>1W(x,t)>>1(>⁣>>>: far greater than), according to construction of WW and the previous estimate, we easily obtain

1C4​𝒦≀W≀C4​𝒦,\displaystyle\frac{1}{C_{4}}\mathcal{K}\leq W\leq C_{4}\mathcal{K},

then, (4.17) implies that

βˆ‚βˆ‚t​W≀\displaystyle\frac{\partial}{\partial t}W\leq 1hβˆ’Ξ΅0​(C3​W2+f​θ​hp​V~Ξ³,qβˆ’1​C4​W2​[(nβˆ’1)βˆ’Ξ΅0​(nβˆ’1)​(C4​W)1nβˆ’1])+W+W2\displaystyle\frac{1}{h-\varepsilon_{0}}\bigg(C_{3}W^{2}+f\theta h^{p}\widetilde{V}_{\gamma,q}^{-1}C_{4}W^{2}[(n-1)-\varepsilon_{0}(n-1)(C_{4}W)^{\frac{1}{n-1}}]\bigg)+W+W^{2}
=\displaystyle= 1hβˆ’Ξ΅0​W2​(C3+f​θ​hp​V~Ξ³,qβˆ’1​C4​(nβˆ’1)βˆ’f​θ​hp​V~Ξ³,qβˆ’1​C4nnβˆ’1​(nβˆ’1)​Ρ0​W1nβˆ’1+2)\displaystyle\frac{1}{h-\varepsilon_{0}}W^{2}\bigg(C_{3}+f\theta h^{p}\widetilde{V}_{\gamma,q}^{-1}C_{4}(n-1)-f\theta h^{p}\widetilde{V}_{\gamma,q}^{-1}C_{4}^{\frac{n}{n-1}}(n-1)\varepsilon_{0}W^{\frac{1}{n-1}}+2\bigg)
=\displaystyle= f​θ​hp​V~Ξ³,qβˆ’1​C4nnβˆ’1​(nβˆ’1)hβˆ’Ξ΅0​W2​(C3+f​θ​hp​V~Ξ³,qβˆ’1​C4​(nβˆ’1)+2f​θ​hp​V~Ξ³,qβˆ’1​C4nnβˆ’1​(nβˆ’1)βˆ’Ξ΅0​W1nβˆ’1)\displaystyle\frac{f\theta h^{p}\widetilde{V}_{\gamma,q}^{-1}C_{4}^{\frac{n}{n-1}}(n-1)}{h-\varepsilon_{0}}W^{2}\bigg(\frac{C_{3}+f\theta h^{p}\widetilde{V}_{\gamma,q}^{-1}C_{4}(n-1)+2}{f\theta h^{p}\widetilde{V}_{\gamma,q}^{-1}C_{4}^{\frac{n}{n-1}}(n-1)}-\varepsilon_{0}W^{\frac{1}{n-1}}\bigg)
≀\displaystyle\leq C5​W2​(C6βˆ’Ξ΅0​W1nβˆ’1)<0,\displaystyle C_{5}W^{2}(C_{6}-\varepsilon_{0}W^{\frac{1}{n-1}})<0,

since C5C_{5} and C6C_{6} depend on β€–fβ€–C0​(Snβˆ’1)\|f\|_{C^{0}(S^{n-1})}, β€–hβ€–C0​(Snβˆ’1Γ—[0,T)CLOSE\|h\|_{C^{0}(S^{n-1}\times[0,T)}, β€–hβ€–C1​(Snβˆ’1Γ—[0,T)CLOSE\|h\|_{C^{1}(S^{n-1}\times[0,T)}, β€–ΞΈβ€–C0​(Snβˆ’1Γ—[0,T)CLOSE\|\theta\|_{C^{0}(S^{n-1}\times[0,T)}. Consequently, we get

W⁑(x0,t)≀C,\displaystyle W(x_{0},t)\leq C,

and for any (x,t)(x,t),

𝒦⁑(x,t)=(hβˆ’Ξ΅0)​W​(x,t)+hθ⁑(t)​(V~Ξ³,q)βˆ’1​hp​f≀(hβˆ’Ξ΅0)​W​(x0,t)+hθ⁑(t)​(V~Ξ³,q)βˆ’1​hp​f≀C.\displaystyle\mathcal{K}(x,t)=\frac{(h-\varepsilon_{0})W(x,t)+h}{\theta(t)(\widetilde{V}_{\gamma,q})^{-1}h^{p}f}\leq\frac{(h-\varepsilon_{0})W(x_{0},t)+h}{\theta(t)(\widetilde{V}_{\gamma,q})^{-1}h^{p}f}\leq C.

Step 2: Prove ΞΊiβ‰₯1C\kappa_{i}\geq\frac{1}{C}.

We consider the auxiliary function as follows

E⁑(x,t)=log⁑βmax​({bi​j})βˆ’A​log⁑h+B​|βˆ‡h|2,\displaystyle E(x,t)=\log\beta_{\max}(\{b_{ij}\})-A\log h+B|\nabla h|^{2},

where A,BA,B are positive constants which will be chosen later, and Ξ²max​({bi​j})\beta_{\max}(\{b_{ij}\}) denotes the maximal eigenvalue of {bi​j}\{b_{ij}\}; for convenience, we write {bi​j}\{b^{ij}\} for {bi​j}βˆ’1\{b_{ij}\}^{-1}.

For every fixed t∈[0,T)t\in[0,T), suppose maxSnβˆ’1⁑E⁑(x,t)\max_{S^{n-1}}E(x,t) is attained at point x0∈Snβˆ’1x_{0}\in S^{n-1}. By a rotation of coordinates, we may assume

{bi​j​(x0,t)}​ is diagonal,andΞ²max​({bi​j}​(x0,t))=b11​(x0,t).\displaystyle\{b_{ij}(x_{0},t)\}\text{ is diagonal,}\quad\text{and}\quad\beta_{\max}(\{b_{ij}\}(x_{0},t))=b_{11}(x_{0},t).

Hence, in order to show ΞΊiβ‰₯1C\kappa_{i}\geq\frac{1}{C}, that is to prove b11≀C.b_{11}\leq C. By means of the above assumption, we transform E⁑(x,t)E(x,t) into the following form,

E~​(x,t)=log⁑b11βˆ’A​log⁑h+B​|βˆ‡h|2.\displaystyle\widetilde{E}(x,t)=\log b_{11}-A\log h+B|\nabla h|^{2}.

Utilizing again the above assumption, for any fixed t∈[0,T)t\in[0,T), E~​(x,t)\widetilde{E}(x,t) has a local maximum at x0x_{0}, thus, we have at x0x_{0},

(4.18) 0=βˆ‡iE~=\displaystyle 0=\nabla_{i}\widetilde{E}= b11β€‹βˆ‡ib11βˆ’A​hih+2​Bβ€‹βˆ‘hk​hk​i\displaystyle b^{11}\nabla_{i}b_{11}-A\frac{h_{i}}{h}+2B\sum h_{k}h_{ki}
=\displaystyle= b11​(hi​11+h1​δi​1)βˆ’A​hih+2​B​hi​hi​i,\displaystyle b^{11}(h_{i11}+h_{1}\delta_{i1})-A\frac{h_{i}}{h}+2Bh_{i}h_{ii},

and

0β‰₯\displaystyle 0\geq βˆ‡i​iE~\displaystyle\nabla_{ii}\widetilde{E}
=\displaystyle= βˆ‡ib11​(hi​11+h1​δi​1)+b11​[βˆ‡i(hi​11+h1​δi​1)]βˆ’A⁑(hi​ihβˆ’hi2h2)+2​B​(βˆ‘hk​hk​i​i+hi​i2)\displaystyle\nabla_{i}b^{11}(h_{i11}+h_{1}\delta_{i1})+b^{11}[\nabla_{i}(h_{i11}+h_{1}\delta_{i1})]-A\bigg(\frac{h_{ii}}{h}-\frac{h_{i}^{2}}{h^{2}}\bigg)+2B(\sum h_{k}h_{kii}+h^{2}_{ii})
=\displaystyle= βˆ’(b11)βˆ’2β€‹βˆ‡ib11​(hi​11+h1​δi​1)+b11​(βˆ‡i​ib11)βˆ’A⁑(hi​ihβˆ’hi2h2)+2​B​(βˆ‘hk​hk​i​i+hi​i2)\displaystyle-(b_{11})^{-2}\nabla_{i}b_{11}(h_{i11}+h_{1}\delta_{i1})+b^{11}(\nabla_{ii}b_{11})-A\bigg(\frac{h_{ii}}{h}-\frac{h_{i}^{2}}{h^{2}}\bigg)+2B(\sum h_{k}h_{kii}+h^{2}_{ii})
=\displaystyle= b11β€‹βˆ‡i​ib11βˆ’(b11)2​(βˆ‡ib11)2βˆ’A⁑(hi​ihβˆ’hi2h2)+2​B​(βˆ‘hk​hk​i​i+hi​i2).\displaystyle b^{11}\nabla_{ii}b_{11}-(b^{11})^{2}(\nabla_{i}b_{11})^{2}-A\bigg(\frac{h_{ii}}{h}-\frac{h_{i}^{2}}{h^{2}}\bigg)+2B(\sum h_{k}h_{kii}+h^{2}_{ii}).

At x0x_{0}, we also have

βˆ‚βˆ‚t​E~=\displaystyle\frac{\partial}{\partial t}\widetilde{E}= 1b11β€‹βˆ‚b11βˆ‚tβˆ’A​hth+2​Bβ€‹βˆ‘hk​hk​t\displaystyle\frac{1}{b_{11}}\frac{\partial b_{11}}{\partial t}-A\frac{h_{t}}{h}+2B\sum h_{k}h_{kt}
=\displaystyle= b11β€‹βˆ‚βˆ‚t​(h11+h​δ11)βˆ’A​hth+2​Bβ€‹βˆ‘hk​hk​t\displaystyle b^{11}\frac{\partial}{\partial t}(h_{11}+h\delta_{11})-A\frac{h_{t}}{h}+2B\sum h_{k}h_{kt}
=\displaystyle= b11​(h11​t+ht)βˆ’A​hth+2​Bβ€‹βˆ‘hk​hk​t.\displaystyle b^{11}(h_{11t}+h_{t})-A\frac{h_{t}}{h}+2B\sum h_{k}h_{kt}.

From Eq. (3) and (2.5), we know that

log⁑(hβˆ’ht)=\displaystyle\log(h-h_{t})= log⁑(h+θ​hp​f​V~Ξ³,qβˆ’1β€‹π’¦βˆ’h)\displaystyle\log\bigg(h+\theta h^{p}f\widetilde{V}_{\gamma,q}^{-1}\mathcal{K}-h\bigg)
=\displaystyle= log⁑𝒦+log⁑(θ​hp​f​V~Ξ³,qβˆ’1)\displaystyle\log\mathcal{K}+\log\bigg(\theta h^{p}f\widetilde{V}_{\gamma,q}^{-1}\bigg)
(4.19) =\displaystyle= βˆ’log⁑[det(βˆ‡2h+h​I)]+log⁑(θ​hp​f​V~Ξ³,qβˆ’1).\displaystyle-\log[\det(\nabla^{2}h+hI)]+\log\bigg(\theta h^{p}f\widetilde{V}_{\gamma,q}^{-1}\bigg).

Let

ψ⁑(x,t)=log⁑(θ​hp​f​V~Ξ³,qβˆ’1).\displaystyle\psi(x,t)=\log\bigg(\theta h^{p}f\widetilde{V}_{\gamma,q}^{-1}\bigg).

Differentiating (4.19) once and twice, we respectively get

hkβˆ’hk​thβˆ’ht=\displaystyle\frac{h_{k}-h_{kt}}{h-h_{t}}= βˆ’βˆ‘bi​jβˆ‡kbi​j+βˆ‡kψ\displaystyle-\sum b^{ij}\nabla_{k}b_{ij}+\nabla_{k}\psi
=\displaystyle= βˆ’βˆ‘bi​i(hk​i​i+hiΞ΄i​k)+βˆ‡kψ,\displaystyle-\sum b^{ii}(h_{kii}+h_{i}\delta_{ik})+\nabla_{k}\psi,

and

h11βˆ’h11​thβˆ’htβˆ’(h1βˆ’h1​t)2(hβˆ’ht)2=\displaystyle\frac{h_{11}-h_{11t}}{h-h_{t}}-\frac{(h_{1}-h_{1t})^{2}}{(h-h_{t})^{2}}= βˆ’(βˆ’βˆ‘(bi​i)2(βˆ‡ibi​i)2+bi​iβˆ‡i​ibi​i)+βˆ‡11ψ\displaystyle-\bigg(-\sum(b^{ii})^{2}(\nabla_{i}b_{ii})^{2}+b^{ii}\nabla_{ii}b_{ii}\bigg)+\nabla_{11}\psi
=\displaystyle= βˆ’βˆ‘bi​iβˆ‡11bi​i+βˆ‘bi​ibj​j(βˆ‡1bi​j)2+βˆ‡11ψ.\displaystyle-\sum b^{ii}\nabla_{11}b_{ii}+\sum b^{ii}b^{jj}(\nabla_{1}b_{ij})^{2}+\nabla_{11}\psi.

By the Ricci identity, we have

βˆ‡11bi​i=βˆ‡i​ib11βˆ’b11+bi​i.\displaystyle\nabla_{11}b_{ii}=\nabla_{ii}b_{11}-b_{11}+b_{ii}.

Thus, we can derive

βˆ‚βˆ‚t​E~hβˆ’ht=\displaystyle\frac{\frac{\partial}{\partial t}\widetilde{E}}{h-h_{t}}= b11​(h11​t+hthβˆ’ht)βˆ’A​hth⁑(hβˆ’ht)+2​Bβ€‹βˆ‘hk​hk​thβˆ’ht\displaystyle b^{11}\bigg(\frac{h_{11t}+h_{t}}{h-h_{t}}\bigg)-A\frac{h_{t}}{h(h-h_{t})}+\frac{2B\sum h_{k}h_{kt}}{h-h_{t}}
=\displaystyle= b11​(h11​tβˆ’h11hβˆ’ht+h11+hβˆ’h+hthβˆ’ht)βˆ’A​1h​htβˆ’h+hhβˆ’ht+2​Bβ€‹βˆ‘hk​hk​thβˆ’ht\displaystyle b^{11}\bigg(\frac{h_{11t}-h_{11}}{h-h_{t}}+\frac{h_{11}+h-h+h_{t}}{h-h_{t}}\bigg)-A\frac{1}{h}\frac{h_{t}-h+h}{h-h_{t}}+\frac{2B\sum h_{k}h_{kt}}{h-h_{t}}
=\displaystyle= b11​(βˆ’(h1βˆ’h1​t)2(hβˆ’ht)2+βˆ‘bi​iβ€‹βˆ‡11bi​iβˆ’βˆ‘bi​i​bj​j​(βˆ‡1bi​j)2βˆ’βˆ‡11ψCLOSE\displaystyle b^{11}\bigg(-\frac{(h_{1}-h_{1t})^{2}}{(h-h_{t})^{2}}+\sum b^{ii}\nabla_{11}b_{ii}-\sum b^{ii}b^{jj}(\nabla_{1}b_{ij})^{2}-\nabla_{11}\psi\bigg.
OPEN+h11+hβˆ’(hβˆ’ht)hβˆ’ht)βˆ’Ah​(βˆ’(hβˆ’ht)+hhβˆ’ht)+2​Bβ€‹βˆ‘hk​hk​thβˆ’ht\displaystyle\bigg.+\frac{h_{11}+h-{(h-h_{t})}}{h-h_{t}}\bigg)-\frac{A}{h}\bigg(\frac{-(h-h_{t})+h}{h-h_{t}}\bigg)+\frac{2B\sum h_{k}h_{kt}}{h-h_{t}}
=\displaystyle= b11​(βˆ’(h1βˆ’h1​t)2(hβˆ’ht)2+βˆ‘bi​iβ€‹βˆ‡11bi​iβˆ’βˆ‘bi​i​bj​j​(βˆ‡1bi​j)2βˆ’βˆ‡11ψ)\displaystyle b^{11}\bigg(-\frac{(h_{1}-h_{1t})^{2}}{(h-h_{t})^{2}}+\sum b^{ii}\nabla_{11}b_{ii}-\sum b^{ii}b^{jj}(\nabla_{1}b_{ij})^{2}-\nabla_{11}\psi\bigg)
+b11​(h11+hhβˆ’htβˆ’1)+Ahβˆ’Ahβˆ’ht+2​Bβ€‹βˆ‘hk​hk​thβˆ’ht\displaystyle+b^{11}\bigg(\frac{h_{11}+h}{h-h_{t}}-1\bigg)+\frac{A}{h}-\frac{A}{h-h_{t}}+\frac{2B\sum h_{k}h_{kt}}{h-h_{t}}
=\displaystyle= b11​(βˆ’(h1βˆ’h1​t)2(hβˆ’ht)2+βˆ‘bi​iβ€‹βˆ‡11bi​iβˆ’βˆ‘bi​i​bj​j​(βˆ‡1bi​j)2βˆ’βˆ‡11ψ)+1βˆ’Ahβˆ’ht\displaystyle b^{11}\bigg(-\frac{(h_{1}-h_{1t})^{2}}{(h-h_{t})^{2}}+\sum b^{ii}\nabla_{11}b_{ii}-\sum b^{ii}b^{jj}(\nabla_{1}b_{ij})^{2}-\nabla_{11}\psi\bigg)+\frac{1-A}{h-h_{t}}
βˆ’b11+Ah+2​Bβ€‹βˆ‘hk​hk​thβˆ’ht\displaystyle-b^{11}+\frac{A}{h}+\frac{2B\sum h_{k}h_{kt}}{h-h_{t}}
≀\displaystyle\leq b11​(βˆ‘bi​i​(βˆ‡i​ib11βˆ’b11+bi​i)βˆ’βˆ‘bi​i​bj​j​(βˆ‡1bi​j)2)βˆ’b11β€‹βˆ‡11ψ+1βˆ’Ahβˆ’ht\displaystyle b^{11}\bigg(\sum b^{ii}(\nabla_{ii}b_{11}-b_{11}+b_{ii})-\sum b^{ii}b^{jj}(\nabla_{1}b_{ij})^{2}\bigg)-b^{11}\nabla_{11}\psi+\frac{1-A}{h-h_{t}}
+Ah+2​Bβ€‹βˆ‘hk​hk​thβˆ’ht\displaystyle+\frac{A}{h}+\frac{2B\sum h_{k}h_{kt}}{h-h_{t}}
≀\displaystyle\leq βˆ‘bi​i​[(b11)2​(βˆ‡ib11)2+A⁑(hi​ihβˆ’hi2h2)βˆ’2​B​(βˆ‘hk​hk​i​i+hi​i2)]\displaystyle\sum b^{ii}\bigg[(b^{11})^{2}(\nabla_{i}b_{11})^{2}+A\bigg(\frac{h_{ii}}{h}-\frac{h_{i}^{2}}{h^{2}}\bigg)-2B(\sum h_{k}h_{kii}+h_{ii}^{2})\bigg]
βˆ’b11βˆ‘bi​ibj​j(βˆ‡1bi​j)2βˆ’b11βˆ‡11ψ+1βˆ’Ahβˆ’ht+Ah+2​Bβ€‹βˆ‘hk​hk​thβˆ’ht\displaystyle-b^{11}\sum b^{ii}b^{jj}(\nabla_{1}b_{ij})^{2}-b^{11}\nabla_{11}\psi+\frac{1-A}{h-h_{t}}+\frac{A}{h}+\frac{2B\sum h_{k}h_{kt}}{h-h_{t}}
≀\displaystyle\leq βˆ‘bi​i[A(hi​i+hβˆ’hhβˆ’hi2h2)]+2Bβˆ‘hk(βˆ’βˆ‘bi​ihk​i​i+hk​thβˆ’ht)\displaystyle\sum b^{ii}\bigg[A\bigg(\frac{h_{ii}+h-h}{h}-\frac{h_{i}^{2}}{h^{2}}\bigg)\bigg]+2B\sum h_{k}\bigg(-\sum b^{ii}h_{kii}+\frac{h_{kt}}{h-h_{t}}\bigg)
βˆ’2Bβˆ‘bi​i(bi​iβˆ’h)2βˆ’b11βˆ‡11ψ+1βˆ’Ahβˆ’ht+Ah\displaystyle-2B\sum b^{ii}(b_{ii}-h)^{2}-b^{11}\nabla_{11}\psi+\frac{1-A}{h-h_{t}}+\frac{A}{h}
≀\displaystyle\leq βˆ‘bi​i​[A⁑(bi​ihβˆ’1)]+2​Bβ€‹βˆ‘hk​(hkhβˆ’ht+bk​k​hkβˆ’βˆ‡kψ)\displaystyle\sum b^{ii}\bigg[A\bigg(\frac{b_{ii}}{h}-1\bigg)\bigg]+2B\sum h_{k}\bigg(\frac{h_{k}}{h-h_{t}}+b^{kk}h_{k}-\nabla_{k}\psi\bigg)
βˆ’2Bβˆ‘bi​i(bi​i2βˆ’2bi​ih)βˆ’b11βˆ‡11ψ+1βˆ’Ahβˆ’ht+Ah\displaystyle-2B\sum b^{ii}(b_{ii}^{2}-2b_{ii}h)-b^{11}\nabla_{11}\psi+\frac{1-A}{h-h_{t}}+\frac{A}{h}
≀\displaystyle\leq βˆ’2Bβˆ‘hkβˆ‡kΟˆβˆ’b11βˆ‡11ψ+(2B|βˆ‡h|βˆ’A)βˆ‘bi​iβˆ’2Bβˆ‘bi​i\displaystyle-2B\sum h_{k}\nabla_{k}\psi-b^{11}\nabla_{11}\psi+(2B|\nabla h|-A)\sum b^{ii}-2B\sum b_{ii}
+4​B​(nβˆ’1)​h+2​B​|βˆ‡h|2+1βˆ’Ahβˆ’ht+n​Ah.\displaystyle+4B(n-1)h+\frac{2B|\nabla h|^{2}+1-A}{h-h_{t}}+\frac{nA}{h}.

Recall

ψ⁑(x,t)=log⁑(θ​hp​f​(V~Ξ³,q)βˆ’1)=log⁑θ+p​log​h+log⁑fβˆ’log⁑V~Ξ³,q,\displaystyle\psi(x,t)=\log\bigg(\theta h^{p}f(\widetilde{V}_{\gamma,q})^{-1}\bigg)=\log\theta+p\log h+\log f-\log\widetilde{V}_{\gamma,q},

since θ\theta is a constant factor, we have θk=0\theta_{k}=0. Consequently, we may obtain following form by ψ⁑(x,t)\psi(x,t) and (4.18),

βˆ’2Bβˆ‘hkβˆ‡kΟˆβˆ’b11βˆ‡11ψ\displaystyle-2B\sum h_{k}\nabla_{k}\psi-b^{11}\nabla_{11}\psi
=\displaystyle= βˆ’2Bβˆ‘hk(phkh+fkfβˆ’(V~Ξ³,q)kV~Ξ³,q)βˆ’b11βˆ‡11ψ\displaystyle-2B\sum h_{k}\bigg(p\frac{h_{k}}{h}+\frac{f_{k}}{f}-\frac{(\widetilde{V}_{\gamma,q})_{k}}{\widetilde{V}_{\gamma,q}}\bigg)-b^{11}\nabla_{11}\psi
=\displaystyle= βˆ’2Bβˆ‘hk(phkh+fkfβˆ’(V~Ξ³,q)kV~Ξ³,q)\displaystyle-2B\sum h_{k}\bigg(p\frac{h_{k}}{h}+\frac{f_{k}}{f}-\frac{(\widetilde{V}_{\gamma,q})_{k}}{\widetilde{V}_{\gamma,q}}\bigg)
βˆ’b11​(p​h11​hβˆ’h12h2+f​f11βˆ’f12f2βˆ’(V~Ξ³,q)11​V~Ξ³,qβˆ’(V~Ξ³,q)12(V~Ξ³,q)2)\displaystyle-b^{11}\bigg(p\frac{h_{11}h-h_{1}^{2}}{h^{2}}+\frac{ff_{11}-f_{1}^{2}}{f^{2}}-\frac{(\widetilde{V}_{\gamma,q})_{11}\widetilde{V}_{\gamma,q}-(\widetilde{V}_{\gamma,q})_{1}^{2}}{(\widetilde{V}_{\gamma,q})^{2}}\bigg)
≀\displaystyle\leq C7​B+C8​b11+2​Bβ€‹βˆ‘hk​(V~Ξ³,q)kV~Ξ³,qβˆ’|p|​b11​h⁑(b11βˆ’h)h2+b11​((V~Ξ³,q)11​V~Ξ³,qβˆ’(V~Ξ³,q)12(V~Ξ³,q)2)\displaystyle C_{7}B+C_{8}b^{11}+2B\sum h_{k}\frac{(\widetilde{V}_{\gamma,q})_{k}}{\widetilde{V}_{\gamma,q}}-|p|b^{11}\frac{h(b_{11}-h)}{h^{2}}+b^{11}\bigg(\frac{(\widetilde{V}_{\gamma,q})_{11}\widetilde{V}_{\gamma,q}-(\widetilde{V}_{\gamma,q})_{1}^{2}}{(\widetilde{V}_{\gamma,q})^{2}}\bigg)
=\displaystyle= C7​B+C8​b11+2​Bβ€‹βˆ‘hk​(V~Ξ³,q)kV~Ξ³,qβˆ’|p|h+|p|​b11h+b11​((V~Ξ³,q)11​V~Ξ³,qβˆ’(V~Ξ³,q)12(V~Ξ³,q)2)\displaystyle C_{7}B+C_{8}b^{11}+2B\sum h_{k}\frac{(\widetilde{V}_{\gamma,q})_{k}}{\widetilde{V}_{\gamma,q}}-\frac{|p|}{h}+\frac{|p|b^{11}}{h}+b^{11}\bigg(\frac{(\widetilde{V}_{\gamma,q})_{11}\widetilde{V}_{\gamma,q}-(\widetilde{V}_{\gamma,q})_{1}^{2}}{(\widetilde{V}_{\gamma,q})^{2}}\bigg)
≀\displaystyle\leq C7​B+C9​b11+2​Bβ€‹βˆ‘hk​(V~Ξ³,q)kV~Ξ³,q+b11​(V~Ξ³,q)11V~Ξ³,q.\displaystyle C_{7}B+C_{9}b^{11}+2B\sum h_{k}\frac{(\widetilde{V}_{\gamma,q})_{k}}{\widetilde{V}_{\gamma,q}}+b^{11}\frac{(\widetilde{V}_{\gamma,q})_{11}}{\widetilde{V}_{\gamma,q}}.

Recall (4.5)

V~Ξ³,q(Ξ©t,y)=2eβˆ’|ρΩt(u)u|2/2∫Snβˆ’1∫0ρΩt,z​(u)eβˆ’|ρΩt(u)uβˆ’su|2/2sqβˆ’2dsdu,\displaystyle\widetilde{V}_{\gamma,q}(\Omega_{t},y)=2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}\int_{S^{n-1}}\int_{0}^{\rho_{\Omega_{t},z}(u)}e^{-|\rho_{\Omega_{t}}(u)u-su|^{2}/2}s^{q-2}dsdu,

then,

(V~Ξ³,q)k=\displaystyle(\widetilde{V}_{\gamma,q})_{k}= βˆ’2eβˆ’|ρΩt(u)u|2/2|ρΩt(u)u|(ρku+ρ⋅ek)∫Snβˆ’1∫0ρΩt,z​(u)eβˆ’|ρΩt(u)uβˆ’su|2/2sqβˆ’2dsdu\displaystyle-2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}|\rho_{\Omega_{t}}(u)u|(\rho_{k}u+\rho\cdot e_{k})\int_{S^{n-1}}\int_{0}^{\rho_{\Omega_{t},z}(u)}e^{-|\rho_{\Omega_{t}}(u)u-su|^{2}/2}s^{q-2}dsdu
(4.20) +2eβˆ’|ρΩt(u)u|2/2∫Snβˆ’1ρΩt,z(u)qβˆ’2eβˆ’|ρΩt(u)uβˆ’ΟΞ©t,z(u)u|2/2(ρΩt,z)kdu,\displaystyle+2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}\int_{S^{n-1}}\rho_{\Omega_{t},z}(u)^{q-2}e^{-|\rho_{\Omega_{t}}(u)u-\rho_{\Omega_{t},z}(u)u|^{2}/2}(\rho_{\Omega_{t},z})_{k}du,

where ρΩt,z​(u)=h⁑(Ξ©t,x)βˆ’zβ‹…xuβ‹…x\rho_{\Omega_{t},z}(u)=\frac{h(\Omega_{t},x)-z\cdot x}{u\cdot x}, z=βˆ‡hz=\nabla h,

(4.21) (ρΩt,z)k=(h⁑(Ξ©t,x)βˆ’βˆ‘ihiβ‹…xuβ‹…x)k=hkβˆ’(βˆ‘ihi​k​x+βˆ‡h)uβ‹…xβˆ’(hβˆ’βˆ‡hβ‹…x)(ekβ‹…x+u)(uβ‹…x)2,\displaystyle(\rho_{\Omega_{t},z})_{k}=\bigg(\frac{h(\Omega_{t},x)-\sum_{i}h_{i}\cdot x}{u\cdot x}\bigg)_{k}=\frac{h_{k}-(\sum_{i}h_{ik}x+\nabla h)}{u\cdot x}-\frac{(h-\nabla h\cdot x)(e_{k}\cdot x+u)}{(u\cdot x)^{2}},

from ρ=(h2+|βˆ‡h|2)12\rho=(h^{2}+|\nabla h|^{2})^{\frac{1}{2}}, we get

(4.22) ρk=Οβˆ’1​(h​hk+Σ​hk​hk​k)=Οβˆ’1​(h​hk+Σ​hk​(bk​kβˆ’h​δk​k)).\displaystyle\rho_{k}=\rho^{-1}(hh_{k}+\Sigma h_{k}h_{kk})=\rho^{-1}(hh_{k}+\Sigma h_{k}(b_{kk}-h\delta_{kk})).

Thus, from Lemma 4.3, (4.6), (4.20), (4.21) and (4.22), we get

2​Bβ€‹βˆ‘hk​(V~Ξ³,q)kV~Ξ³,q≀C10​B​b11.\displaystyle 2B\sum h_{k}\frac{(\widetilde{V}_{\gamma,q})_{k}}{\widetilde{V}_{\gamma,q}}\leq C_{10}Bb_{11}.
(V~Ξ³,q)11=\displaystyle(\widetilde{V}_{\gamma,q})_{11}= βˆ’2eβˆ’|ρΩt(u)u|2/2|ρΩt(u)u|(ρ11u+ρ1β‹…e1+ρ1β‹…e1+Ξ΄11)Γ—\displaystyle-2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}|\rho_{\Omega_{t}}(u)u|(\rho_{11}u+\rho_{1}\cdot e_{1}+\rho_{1}\cdot e_{1}+\delta_{11})\times
∫Snβˆ’1∫0ρΩt,z​(u)eβˆ’|ρΩt(u)uβˆ’su|2/2sqβˆ’2dsdu\displaystyle\int_{S^{n-1}}\int_{0}^{\rho_{\Omega_{t},z}(u)}e^{-|\rho_{\Omega_{t}}(u)u-su|^{2}/2}s^{q-2}dsdu
βˆ’2eβˆ’|ρΩt(u)u|2/2|ρΩt(u)u|(ρ1u+ρ⋅e1)∫Snβˆ’1ρΩt,z(u)qβˆ’2eβˆ’|ρΩt(u)uβˆ’ΟΞ©t,z(u)u|2/2(ρΩt,z)kdu\displaystyle-2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}|\rho_{\Omega_{t}}(u)u|(\rho_{1}u+\rho\cdot e_{1})\int_{S^{n-1}}\rho_{\Omega_{t},z}(u)^{q-2}e^{-|\rho_{\Omega_{t}}(u)u-\rho_{\Omega_{t},z}(u)u|^{2}/2}(\rho_{\Omega_{t},z})_{k}du
βˆ’\displaystyle- 2eβˆ’|ρΩt(u)u|2/2|ρΩt(u)u|(ρ1u+ρ⋅e1)∫Snβˆ’1ρΩt,z(u)qβˆ’2eβˆ’|ρΩt(u)uβˆ’ΟΞ©t,z(u)u|2/2(ρΩt,z)kdu\displaystyle 2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}|\rho_{\Omega_{t}}(u)u|(\rho_{1}u+\rho\cdot e_{1})\int_{S^{n-1}}\rho_{\Omega_{t},z}(u)^{q-2}e^{-|\rho_{\Omega_{t}}(u)u-\rho_{\Omega_{t},z}(u)u|^{2}/2}(\rho_{\Omega_{t},z})_{k}du
+\displaystyle+ 2eβˆ’|ρΩt(u)u|2/2[(qβˆ’2)∫Snβˆ’1ρΩt,z(u)qβˆ’3eβˆ’|ρΩt(u)uβˆ’ΟΞ©t,z(u)u|2/2(ρΩt,z)12du\displaystyle 2e^{-|\rho_{\Omega_{t}}(u)u|^{2}/2}\bigg[(q-2)\int_{S^{n-1}}\rho_{\Omega_{t},z}(u)^{q-3}e^{-|\rho_{\Omega_{t}}(u)u-\rho_{\Omega_{t},z}(u)u|^{2}/2}(\rho_{\Omega_{t},z})_{1}^{2}du
+∫Snβˆ’1ρΩt,z(u)qβˆ’2eβˆ’|ρΩt(u)uβˆ’ΟΞ©t,z(u)u|2/2(βˆ’|ρΩt(u)uβˆ’ΟΞ©t,z(u)u|(ρ1u+ρe1\displaystyle+\int_{S^{n-1}}\rho_{\Omega_{t},z}(u)^{q-2}e^{-|\rho_{\Omega_{t}}(u)u-\rho_{\Omega_{t},z}(u)u|^{2}/2}\bigg(-|\rho_{\Omega_{t}}(u)u-\rho_{\Omega_{t},z}(u)u|(\rho_{1}u+\rho e_{1}
(4.23) βˆ’(ρΩt,z)1uβˆ’ΟΞ©t,ze1))(ρΩt,z)1du+∫Snβˆ’1ρΩt,z(u)qβˆ’2eβˆ’|ρΩt(u)uβˆ’ΟΞ©t,z(u)u|2/2(ρΩt,z)11du],\displaystyle-(\rho_{\Omega_{t},z})_{1}u-\rho_{\Omega_{t},z}e_{1})\bigg)(\rho_{\Omega_{t},z})_{1}du+\int_{S^{n-1}}\rho_{\Omega_{t},z}(u)^{q-2}e^{-|\rho_{\Omega_{t}}(u)u-\rho_{\Omega_{t},z}(u)u|^{2}/2}(\rho_{\Omega_{t},z})_{11}du\bigg],

where

(ρΩt,z)11=\displaystyle(\rho_{\Omega_{t},z})_{11}= (h11βˆ’(βˆ‘ihi​11​x+βˆ‘ihi​1+βˆ‘ihi​1)CLOSEuβ‹…xβˆ’(h1βˆ’(βˆ‘ihi​1β‹…x+βˆ‡h)​(e1​x+u)CLOSE(uβ‹…x)2\displaystyle\frac{(h_{11}-(\sum_{i}h_{i11}x+\sum_{i}h_{i1}+\sum_{i}h_{i1})}{u\cdot x}-\frac{(h_{1}-(\sum_{i}h_{i1}\cdot x+\nabla h)(e_{1}x+u)}{(u\cdot x)^{2}}
βˆ’(h1βˆ’βˆ‘ihi​1xβˆ’βˆ‡h)(e1β‹…x+u)+(h+(βˆ‡hβ‹…x))(Ξ΄11β‹…x+2e1)(uβ‹…x)2\displaystyle-\frac{(h_{1}-\sum_{i}h_{i1}x-\nabla h)(e_{1}\cdot x+u)+(h+(\nabla h\cdot x))(\delta_{11}\cdot x+2e_{1})}{(u\cdot x)^{2}}
(4.24) +2(e1β‹…x+u)(hβˆ’βˆ‡hβ‹…x)(e1β‹…x+u)(uβ‹…x)3.\displaystyle+\frac{2(e_{1}\cdot x+u)(h-\nabla h\cdot x)(e_{1}\cdot x+u)}{(u\cdot x)^{3}}.

From (4.22), we get

ρ11=h​h11+h12+Σ​h1​h111+Σ​h112Οβˆ’h12​b112ρ3.\displaystyle\rho_{11}=\frac{hh_{11}+h_{1}^{2}+\Sigma h_{1}h_{111}+\Sigma h_{11}^{2}}{\rho}-\frac{h_{1}^{2}b_{11}^{2}}{\rho^{3}}.

This combined with (4.18) implies

(4.25) ρ11=h⁑(b11βˆ’h)+h12+Σ​h1​(A​h1hβˆ’2​B​h​(b11βˆ’h)βˆ’b11​(h1​δ11))​b11Οβˆ’h12​b112ρ3.\displaystyle\rho_{11}=\frac{h(b_{11}-h)+h_{1}^{2}+\Sigma h_{1}\bigg(A\frac{h_{1}}{h}-2Bh(b_{11}-h)-b^{11}(h_{1}\delta_{11})\bigg)b_{11}}{\rho}-\frac{h_{1}^{2}b_{11}^{2}}{\rho^{3}}.

By Lemma 4.3, Lemma 4.4, (4.6), (4.23), (4.18), (4.24) and (4.25), we conclude for q>2q>2,

b11​(V~Ξ³,q)11V~Ξ³,q≀C11​b11.\displaystyle b^{11}\frac{(\widetilde{V}_{\gamma,q})_{11}}{\widetilde{V}_{\gamma,q}}\leq C_{11}b_{11}.

It follows that

βˆ‚βˆ‚t​E~hβˆ’ht≀C12​B​b11+C13​b11+(2​B​|βˆ‡h|βˆ’A)β€‹βˆ‘bi​iβˆ’2​Bβ€‹βˆ‘bi​i+4​B​(nβˆ’1)​h+n​Ah<0,\displaystyle\frac{\frac{\partial}{\partial t}\widetilde{E}}{h-h_{t}}\leq C_{12}Bb_{11}+C_{13}b^{11}+(2B|\nabla h|-A)\sum b^{ii}-2B\sum b_{ii}+4B(n-1)h+\frac{nA}{h}<0,

provided b11>>1b_{11}>>1 and if we choose A>>BA>>B. We obtain

E~​(x0,t)≀C,\displaystyle\widetilde{E}(x_{0},t)\leq C,

hence,

E⁑(x0,t)=E~​(x0,t)≀C.\displaystyle E(x_{0},t)=\widetilde{E}(x_{0},t)\leq C.

This tells us the principal radii are bounded from above, or equivalently ΞΊiβ‰₯1C\kappa_{i}\geq\frac{1}{C}. ∎

5. The convergence of the flow

With the help of priori estimates in the section 4, the long-time existence and asymptotic behaviour of the flow (1) (or (3)) are obtained, we also can complete proof of Theorem 1.6.

Proof of the Theorem 1.6.

Since Eq. (3) is parabolic, we can get its short time existence. Let TT be the maximal time such that h⁑(β‹…,t)h(\cdot,t) is a smooth even solution to Eq. (3) for t∈[0,T)t\in[0,T). Lemma 4.3-4.5 enable us to apply Lemma 4.6 to Eq. (3), thus, we can deduce a uniformly upper and lower bounds for the biggest eigenvalue of {(hi​j+h​δi​j)​(x,t)}\{(h_{ij}+h\delta_{ij})(x,t)\}. This implies

Cβˆ’1​I≀(hi​j+h​δi​j)​(x,t)≀C​I,βˆ€(x,t)∈Snβˆ’1Γ—[0,T),\displaystyle C^{-1}I\leq(h_{ij}+h\delta_{ij})(x,t)\leq CI,\quad\forall(x,t)\in S^{n-1}\times[0,T),

where C>0C>0 independents on tt. This shows that Eq. (3) is uniformly parabolic. Estimates for higher derivatives follows from the standard regularity theory of uniformly parabolic equations Krylov [17]. Hence, we obtain the long time existence and regularity of solutions for the flow (1) (or (3)). Moreover, we obtain

(5.1) β€–hβ€–Cx,tl,m​(Snβˆ’1Γ—[0,T))≀Cl,m,\displaystyle\|h\|_{C^{l,m}_{x,t}(S^{n-1}\times[0,T))}\leq C_{l,m},

for some Cl,mC_{l,m} (l,ml,m are nonnegative integers pairs) independent of tt, then T=∞T=\infty. Using parabolic comparison principle, we can attain the uniqueness of the smooth even solution h⁑(β‹…,t)h(\cdot,t) of Eq. (3).

Now, recall the non-increasing property of Φ⁑(Ξ©t)\Phi(\Omega_{t}) in Lemma 3.2, we know that for pβ‰₯0p\geq 0,

(5.2) βˆ‚Ξ¦β‘(Ξ©t)βˆ‚t≀0.\displaystyle\frac{\partial\Phi(\Omega_{t})}{\partial t}\leq 0.

Based on (5.2), there exists a t0t_{0} such that

βˆ‚Ξ¦β‘(Ξ©t)βˆ‚t|t=t0=0,\displaystyle\frac{\partial\Phi(\Omega_{t})}{\partial t}\bigg|_{t=t_{0}}=0,

this yields

Ο„1​V~Ξ³,q​(Ξ©t0,β‹…)​hΞ©t01βˆ’p​det(hi​j+h​δi​j)=f,p>0.\displaystyle\tau_{1}\widetilde{V}_{\gamma,q}(\Omega_{t_{0}},\cdot)h_{\Omega_{t_{0}}}^{1-p}\det(h_{ij}+h\delta_{ij})=f,\quad p>0.

and

Ο„2​V~Ξ³,q​(Ξ©t0,β‹…)​hΞ©t0​det(hi​j+h​δi​j)=f,p=0.\displaystyle\tau_{2}\widetilde{V}_{\gamma,q}(\Omega_{t_{0}},\cdot)h_{\Omega_{t_{0}}}\det(h_{ij}+h\delta_{ij})=f,\quad p=0.

Let Ξ©=Ξ©t0\Omega=\Omega_{t_{0}}, thus, Ξ©\Omega satisfies (1.8) for p>0p>0 and (1.10) for p=0p=0.

In view of (5.1), applying the Arzela`\grave{a}-Ascoli theorem and a diagonal argument, we can extract a subsequence of tt, denoted by {tj}jβˆˆβ„•βŠ‚(0,+∞)\{t_{j}\}_{j\in\mathbb{N}}\subset(0,+\infty), and there exists a smooth even function h⁑(x)h(x) such that

(5.3) β€–h⁑(x,tj)βˆ’h⁑(x)β€–Ci​(Snβˆ’1)β†’0,\displaystyle\|h(x,t_{j})-h(x)\|_{C^{i}(S^{n-1})}\rightarrow 0,

uniformly for each nonnegative integer ii as tjβ†’βˆžt_{j}\rightarrow\infty. This reveals that h⁑(x)h(x) is a support function. Let us denote by Ξ©\Omega the convex body determined by h⁑(x)h(x). Thus, Ξ©\Omega is smooth, origin-symmetric and strictly convex.

Moreover, by (5.1) and the uniform estimates in section 4, we conclude that Φ⁑(Ξ©t)\Phi(\Omega_{t}) is a bounded function in tt and βˆ‚Ξ¦β‘(Ξ©t)βˆ‚t\frac{\partial\Phi(\Omega_{t})}{\partial t} is uniformly continuous. Thus, for any t>0t>0, by monotonicity of the Φ⁑(Ξ©t)\Phi(\Omega_{t}) in Lemma 3.2, there is a constant C>0C>0 independents of tt, such that

∫0t(βˆ’βˆ‚Ξ¦β‘(Ξ©t)βˆ‚t)​𝑑t=Φ⁑(Ξ©0)βˆ’Ξ¦β‘(Ξ©t)≀C,\displaystyle\int_{0}^{t}\bigg(-\frac{\partial\Phi(\Omega_{t})}{\partial t}\bigg)dt=\Phi(\Omega_{0})-\Phi(\Omega_{t})\leq C,

this gives

(5.4) limtβ†’βˆžΞ¦(Ξ©t)βˆ’Ξ¦(Ξ©0)=βˆ’βˆ«0∞|βˆ‚βˆ‚tΞ¦(Ξ©t)|dt≀C.\displaystyle\lim_{t\rightarrow\infty}\Phi(\Omega_{t})-\Phi(\Omega_{0})=-\int_{0}^{\infty}\bigg|\frac{\partial}{\partial t}\Phi(\Omega_{t})\bigg|dt\leq C.

The left hand side of (5.4) is bounded below by βˆ’2​C-2C, therefore, there is a subsequence tjβ†’βˆžt_{j}\rightarrow\infty such that

βˆ‚βˆ‚t​Φ​(Ξ©tj)β†’0astjβ†’βˆž.\displaystyle\frac{\partial}{\partial t}\Phi(\Omega_{t_{j}})\rightarrow 0\quad\text{as}\quad t_{j}\rightarrow\infty.

The proof of Lemma 3.2 shows that when p>0p>0,

(5.5) (∫Snβˆ’1f⁑(x)​(h∞)p​𝑑x)2=∫Snβˆ’1V~Ξ³,q​hβˆžπ’¦β€‹π‘‘xβ€‹βˆ«Snβˆ’1f2​(h∞)2​pβˆ’1​𝒦​V~Ξ³,qβˆ’1​𝑑x,\displaystyle\bigg(\int_{S^{n-1}}f(x)(h^{\infty})^{p}dx\bigg)^{2}=\int_{S^{n-1}}\widetilde{V}_{\gamma,q}\frac{h^{\infty}}{{\mathcal{K}}}dx\int_{S^{n-1}}f^{2}(h^{\infty})^{2p-1}{\mathcal{K}}\widetilde{V}_{\gamma,q}^{-1}dx,

and p=0p=0,

(5.6) (∫Snβˆ’1f⁑(x)​𝑑x)2=∫Snβˆ’1V~Ξ³,q​hβˆžπ’¦β€‹π‘‘xβ€‹βˆ«Snβˆ’1f2​𝒦(h∞)​V~Ξ³,q​𝑑x,\displaystyle\bigg(\int_{S^{n-1}}f(x)dx\bigg)^{2}=\int_{S^{n-1}}\widetilde{V}_{\gamma,q}\frac{h^{\infty}}{{\mathcal{K}}}dx\int_{S^{n-1}}\frac{f^{2}{\mathcal{K}}}{(h^{\infty})\widetilde{V}_{\gamma,q}}dx,

where h∞h^{\infty} is the support function of Ω∞\Omega^{\infty}. By equality condition of Hâlder inequality, (5.5) and (5.6) means that for p>0p>0,

(5.7) Ο„1​V~Ξ³,q​(Ξ©,β‹…)​(hΩ∞)1βˆ’p​det(hi​j∞+hβˆžβ€‹Ξ΄i​j)=f⁑(x),\displaystyle\tau_{1}\widetilde{V}_{\gamma,q}(\Omega,\cdot)(h^{\infty}_{\Omega})^{1-p}\det(h^{\infty}_{ij}+h^{\infty}\delta_{ij})=f(x),

and p=0p=0,

(5.8) Ο„2​V~Ξ³,q​(Ξ©,β‹…)​hΞ©βˆžβ€‹det(hi​j∞+hβˆžβ€‹Ξ΄i​j)=f⁑(x),\displaystyle\tau_{2}\widetilde{V}_{\gamma,q}(\Omega,\cdot)h^{\infty}_{\Omega}\det(h^{\infty}_{ij}+h^{\infty}\delta_{ij})=f(x),

(5.7) satisfies (1.8) and (5.8) satisfies (1.10) with Ο„1\tau_{1} and Ο„2\tau_{2} given by

1Ο„1=limtjβ†’βˆžΞΈβ‘(tj),p>0,\displaystyle\frac{1}{\tau_{1}}=\lim_{t_{j}\rightarrow\infty}\theta(t_{j}),\quad p>0,

and

1Ο„2=limtjβ†’βˆžΞΈβ‘(tj),p=0,\displaystyle\frac{1}{\tau_{2}}=\lim_{t_{j}\rightarrow\infty}\theta(t_{j}),\quad p=0,

This completes the proof of Theorem 1.6. ∎

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