Abstract
We investigate the large time behavior of compactly supported smooth solutions for a one-dimensional thin-film equation with linear mobility in the regime of partial wetting. We show the stability of steady state solutions. Relaxation rates are obtained for initial data which are close to a steady state in a suitable sense. The proof uses the Lagrangian coordinates. Our method is to establish and exploit differential relations between the energy and the dissipation as well as some interpolation inequalities. Our result is different from earlier results because here we consider solutions with finite mass.
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1 Introduction
Consider the following one-dimensional fourth-order nonlinear degenerate parabolic equation
where \(\lambda _{\pm } : (0,\infty )\rightarrow {\mathbb {R}}\) represent the support of u, \(u>0\) on \((\lambda _-, \lambda _+)\) and V is the velocity of the moving boundary. We supplement the problem (1.1) with the initial data \(u(0,x)=u_0(x)\) supported in \((\lambda ^0_-, \lambda ^0_+)\) and satisfying (1.1c).
Equation (1.1a) arises as the particular case of the thin-film equation in the Hele–Shaw setting [3, 25, 29]. It describes the pinching of thin necks in a Hele–Shaw cell. The function \(u = u(t,x)\ge 0\) represents the height of a two-dimensional viscous thin film on a one-dimensional flat solid as a function of time \(t > 0\) and the lateral variable x. One can rigorously derive equation (1.1) from the Hele–Shaw cell in the regime of thin films and where the dominating effects are surface tension and viscosity only [15, 20, 21].
Equation (1.1) is a particular case of the thin-film equation
where \(n>0\) is the mobility exponent. See [28] for a physical explanation of the Eq. (1.2). For \(n\in (0,3)\) and in the complete wetting regime, the existence of self-similar source-type solution for (1.2) has been established in [2] by ODE arguments. For \(n=1\), the authors of [2] prove the uniqueness in the class of self-similar solutions. See [2, Lemma 6.3, p. 231]. Recently, the uniqueness of source type solutions is proved in [23] for a larger class. For \(n=2\), well-posedness results are established in [19] for (1.2) in the case of partial wetting regime. See [12, 18] for the complete wetting regime.
The existence of weak solutions to (1.1) was investigated in [29]. See also [4, 10, 24]. More recently, the existence and uniqueness of classical solutions to (1.1) was shown in [21, Theorem 4, p. 607]. The asymptotic behavior of solutions to thin film equations with prescribed contact angle has not been considered neither in [29] nor in [21]. However, the asymptotic behavior in the complete wetting regime was investigated in many papers. See, among many, [7,8,9, 13, 14, 16, 17] and references therein. See also [31] for the multidimensional case.
In [11], the author studies the following problem for the thin-film equation in the partial wetting regime on a half-axis, with a single contact point
Using a strategy inspired by [30], the author of [11] proves the stability of the steady state given by \(h_0(x)=\max \{x,0\}\) for initial data close, in some sense, to \(h_0\). See [11, Theorem 1.2, p. 352]. We would like to point out that only the case where the free boundary is given by a single contact point was considered in [11]. As pointed out in [11], in contrast to (1.1), solutions to (1.3) do not satisfy conservation of mass or even have finite mass.
In this paper we are interested in the case where the free boundary is given by two contact points at every time t. Solutions of (1.1) preserve mass and center of mass defined respectively by
and
Note that if u has a mass \(M> 0\) and a center of mass \(\mu \in {\mathbb {R}}\), then \({\bar{u}}(t,x)=u(t,x+\frac{\mu }{M})\) has the same mass but with center of mass equal to zero. Without loss of generality, we are going to suppose that \(M> 0\) and \(\mu \in {\mathbb {R}}\) are given.
Our main goal is the study of the stability of stationary solutions to (1.1). The equation (1.1) possesses a family of stationary solutions given by
By choosing \(M=2/3\) and \(\mu =0\), we obtain \(\alpha _-=-1\) and \(\alpha _+=1\). So, we will investigate the asymptotic behavior of smooth solutions with initial data which are small perturbations of the steady state
where \(a_+=\max \{a,0\}.\) To this end, let us define the mass Lagrangian variable as follows: for given \(t\ge 0\),
such that
where \(\lambda _{\pm }(0)=\lambda ^0_{\pm }.\) The relation (1.6) together with (1.1) defines the function Z. One advantage of this transformation is that in the new coordinates the boundary is fixed to \(y=\pm 1\). Moreover, the transformation (1.6) can be seen as a perturbation of the stationary solution \(u^\infty \). In addition, the stationary solution in these coordinates is given by
which is a linear function in y.
The use of von Mises-type transformations in the analysis of thin-film equations was introduced in [12] and, besides the different steady state, the specific transformation used here was introduced in [16], and applied for \((1-x^2)^2\) instead of \((1-x^2)\) in (1.6). Changing from \((1-x^2)^2\) to \((1-x^2)\) does not yield a self-adjoint linear operator \({{\mathcal {L}}}\) for instance. See (2.8) below. This requires a new approach as explained below.
Before stating our result, we introduce the energy
where \({\tilde{u}}(t,y)=u(t, Z(t,y))\). We also define \(Z_0(y):=Z(0,y)\) and \({\tilde{u}}_0(y)=u_0(Z_0(y)).\)
Our main result can be stated as follows.
Theorem 1.1
Let u be a global smooth solution to (1.1) with initial data \(u_0\) satisfying \(M(u_0)=2/3\) and \(\mu (u_0)=0\). There exists a constant \(c_0>0\) such that, if
then there exists \(\gamma >0\) such that
Remark 1.2
Equation (1.1) is invariant under the scaling
The Lagrangian coordinate \(Z_\kappa \) verifies
and
where g is given by (2.6) below. This leads to
Then the condition (1.9) is invariant under the above scaling and hence it is relevant.
Remark 1.3
Our approach doesn’t apply for weak solutions. Indeed, we need that there is no topological change of the support \(\{\,u>0\,\}\) and that the solutions are smooth in the set \(\{\,u>0\,\}\) up to the boundary. These requirements are not guaranteed by weak solutions.
Remark 1.4
It is known from [1, 4] that (1.1) is the gradient flow with respect to the Wasserstein metric and the energy given by
Making the change of variable \(x=Z(t,y)\) in (1.11) and using Proposition 2.1 below, we obtain that
By Proposition 2.1 below, (1.8) becomes
Clearly the two energies \({\mathcal {E}}(u(t))\) and E(t) have different expressions.
The proof of Theorem 1.1 follows from taking the formal derivative of the energy (1.8), obtaining a differential inequality of the form
and proving a dissipation estimate
where \(a>0\) is a constant and D is an appropriately defined dissipation (see (2.11) below). From the previous inequalities, the result follows from considering initial data with small enough initial energy. See Corollary 3.13 below. The most laborious part of the proof is to show (1.14) which follows from a direct calculation of the time derivative and estimating several terms using Poincaré’s inequality and interpolation estimates. See Proposition 4.1 below. Note that the value of \(\gamma \) in (1.10) is given by
where \(c_0>0\) is introduced in (1.9) and satisfies \(c_0^{9}+c_0^{5/2}+c_0+ c_0^{1/3}< {1/a}.\)
From the above theorem we easily derive the following.
Corollary 1.5
Suppose (1.9) is fulfilled. Then it follows that
and
An important consequence of the decay estimate (1.10) is that it implies the desired convergence of \(\lambda _{\pm }\) to \(\pm 1\) as stated below.
Corollary 1.6
Suppose (1.9) is fulfilled. Then, for t sufficiently large, we have
and
where \(\gamma \) is as in (1.10). In particular, for t large, we have
We also obtain from Theorem 1.1 the convergence of the volumetric coordinates Z(t, y) to y with the same decay rate as in (1.10).
Corollary 1.7
Suppose (1.9) is fulfilled. Then, for t sufficiently large, we have
where \(\gamma \) is as in (1.10).
The rest of this paper is organized as follows. In the next section, we reformulate our problem and derive a first energy estimate. In Sect. 3, we recall and establish some preliminaries and useful tools. Section 4 is devoted to the energy estimate. In the last section we give the proof of the main results. We will write \(A\lesssim B\) if there exists a constant \(0<C<\infty \) such that \(A\le C B\), and \(A\approx A_1+A_2+\cdots A_N\) if there exist constants \(c_1,c_2,\ldots c_N\in {\mathbb {R}}\) such that \(A=c_1 A_1+c_2 A_2+\cdots +c_N A_N\). Finally, we denote the norm in Lebesgue space \(L^p\) by \(\Vert \cdot \Vert _p\), \(1\le p\le \infty \).
2 Reformulation of the Problem
In this section we reformulate the problem (1.1). From (1.6) we deduce the following.
Proposition 2.1
Let Z be the mass Lagrangian variable defined by (1.6). Then, we have
-
(i)
\(Z(t,\pm 1)=\lambda _{\pm }(t).\)
-
(ii)
\(Z_t(t,y)=u_{xxx}(t,Z(t,y)).\)
-
(iii)
\(Z_y(t,y)=\frac{u^\infty (y)}{u(t,Z(t,y))}.\)
Proof
Part (i) follows immediately from the definition (1.6). To prove (ii) we differentiate (1.6) with respect to variable t to obtain
Using boundary condition (1.1b) and equation (1.1a), we get
since \(u\,u_{xxx}=0\) at \(x=\lambda _{\pm }(t)\). This obviously leads to (ii).
Now we differentiate (1.6) with respect to variable y to obtain
which is exactly (iii). \(\square \)
Remark 2.2
-
(1)
By choosing \(y=1\) in (1.6) and using the fact that \(Z(t,1)=\lambda _+(t)\) we get
$$\begin{aligned} M=\int _{\lambda _-(t)}^{\lambda _+(t)}\,u(t,x)\,dx=\int _{-1}^{1}u^\infty (x)\,dx=\frac{2}{3}. \end{aligned}$$ -
(2)
Making the change of variable \(x=Z(t,y)\) and using (iii) of the previous proposition, we see that the center of mass given by (1.5) reads
$$\begin{aligned} \mu =\int _{\lambda _-(t)}^{\lambda _+(t)}\,x\,u(t,x)\,dx=\frac{1}{2}\int _{-1}^1\, \left( 1-y^2\right) \,Z(t,y)\,dy. \end{aligned}$$(2.1)
In order to derive an evolution equation in the Lagrangian coordinates, observe that by the previous proposition we have
As in [16], the relation (2.2) suggests to define
The evolution equation satisfied by G is given in the following proposition.
Proposition 2.3
The function G defined by (2.3) solves
Proof
Differentiating (2.3) with respect to t yields
Since, by Proposition 2.1 (iii), \(u^\infty (y)\,G(t,y)=u(t, Z(t,y))\), it follows that \(\partial _y(u^\infty \,G)=Z_y\,u_x=\frac{1}{G}\,u_x\). Therefore
Similarly we obtain that
Using Part (ii) in Proposition 2.1 and (2.5), we infer
This leads to (2.4a). To prove (2.4b) we use the L’Hôpital rule to deduce that
Hence \((Z_y(t,1))^2=1\). By (2.2), \(Z_y\ge 0\). Then, using (2.3) we get (2.4b). Similarly for \(y=-1.\) \(\square \)
Since we want to study perturbations of \(G^\infty =\frac{1}{Z^\infty _y}=1\), we set
Referring to (2.4), we obtain that
where
and
Using (2.2), (2.3) and (2.6), we may rewrite the energy given by (1.8) as
We also introduce the dissipation
as well as the following quantities
Our aim now is to obtain a first energy estimate. We have obtained the following.
Proposition 2.4
Let E and D be given by (2.10) and (2.11) respectively. Then
Proof
Multiplying (2.7a) by \(-\partial _y^2\,g\) and integrating in \(y\in (-1,1)\) we get, using (2.7b)
In fact, since \(g(t,\pm 1)=0\) for all \(t>0\), we have
Also,
Hence
Then
and we get (2.12). \(\square \)
3 Useful Tools
In this section, we recall some known and useful tools. Then, we use them to obtain crucial estimates needed in our proofs.
Proposition 3.1
(Poincaré’s inequality). Suppose \(I=(a,b)\subset {\mathbb {R}}\) is a bounded interval and \(1\le \,p,\,q\le \infty \). Then, for every \(u\in \,W^{1,p}_0(I)\), we have
Proof
For \(x\in I\) we have \(u(x)=\int _a^x\,u'(t)\,dt\). Hence, for all \(x\in I\)
This proves (3.1) for \(q=\infty \). Suppose now \(q<\infty \). Then, by (3.2), we obtain that
This leads to (3.1) as desired. \(\square \)
Remark 3.2
For \(u\in W^{1,p}(I)\) we introduce
This definition makes sense since \(W^{1,p}(I)\hookrightarrow C({\bar{I}})\). We also define
Clearly \(W^{1,p}_0(I)\subset {\tilde{W}}^{1,p}(I).\)
A more general statement of Poincaré’s inequality can be stated as follows.
Proposition 3.3
Suppose \(I=(a,b)\subset {\mathbb {R}}\) is a bounded interval and \(1\le \,p,\,q\le \infty \). Then, for every \(u\in \,{\tilde{W}}^{1,p}(I)\), we have
From Proposition 3.3 we deduce the following Poincaré–Wirtinger inequality.
Proposition 3.4
(Poincaré–Wirtinger’s inequality). Let \(1\le p, q\le \infty \) and \(I=(a,b)\subset {\mathbb {R}}\) a bounded interval. Then, for any \(u\in W^{1,p}(I)\), we have
where
Proof
Let \(u\in W^{1,p}(I)\) and define \(v=u-{\overline{u}}\). Since \(\int _{I}\,v=0\) and \(v\in C({\bar{I}})\), then \(v\in {\tilde{W}}^{1,p}(I)\). Applying (3.3) with v we conclude the proof since \(v'=u'\). \(\square \)
Note that, if \(u\in W^{2,p}(I)\cap W^{1,p}_0(I)\), then \(\overline{u'}=0\). Hence, by applying (3.4) with \(u'\) instead of u, we obtain the following useful inequality.
Corollary 3.5
Let \(1\le p, q\le \infty \) and \(I=(a,b)\subset {\mathbb {R}}\) a bounded interval. Then, for any \(u\in W^{2,p}(I)\cap W^{1,p}_0(I)\), we have
We also recall the following Gagliardo-Nirenberg interpolation inequalities useful for our purpose. We refer to [5, 26, 27] for more general statements.
Proposition 3.6
Suppose \(I=(a,b)\subset {\mathbb {R}}\) is a bounded interval, \(1\le \,q<\infty \) and \(1\le \,r\le \,\infty \). Then, there exists a constant \(C=C(q,r)>0\) such that for every \(u\in W^{1,r}(I)\), we have
where \(0<\,\delta \,\le \, 1\) is defined by
Proof
We start with the case \(r>1\). We first suppose \(u(a)=0\). Then
where \(G(\tau )=|\tau |^{\alpha -1}\tau \) and \(\alpha =\frac{1}{\delta }\in (1,\infty )\). It follows by Hölder’s inequality that
where we have used the fact that \(r'(\alpha -1)=q\). Therefore
We now turn to the case when \(u(a)\ne 0\). Let \(\eta \in C^1([a,b])\) defined by
Clearly \(0\le \eta \le 1\) and \(0\le \eta '\le \frac{4}{|I|}\). Applying (3.8) respectively to \(v(x):=\eta (x)u(x)\) and \(w(x)=\eta (x)u(a+b-x)\), we get
and
Combining (3.9) and (3.10) we obtain the desired inequality (3.6) when \(r>1\). This finishes the proof since the case \(r=1\) is trivial. \(\square \)
Remark 3.7
A careful inspection of the proof shows that the constant C appearing in (3.6) can be taken as
where \(C_0>0\) is an absolute constant.
Proposition 3.8
Suppose \(I=(a,b)\subset {\mathbb {R}}\) is a bounded interval, \(1\le \,q<\infty \), \(q\le \,p\,\le \infty \) and \(1\le \,r\le \,\infty \). Then, there exists a constant \(C=C(|I|, p,q,r)>0\) such that for every \(u\in \,W^{2,r}(I)\cap W^{1,r}_0(I)\), we have
where \(0\le \,\theta \le \,1\) is defined by
Proof
The case \(p=q\) is trivial. We will focus only on the case \(q<p\le \infty \). The proof will be divided into three steps.
Step 1. We claim that
for some constant \(C=C(|I|, p,q,r)>0\), where \(\theta \) is given as in (3.12). Note that for \(p=\infty \) we have \(\theta =\delta \) and (3.13) reduces to (3.6). To see (3.13) for \(p<\infty \) we write using (3.6)
Therefore
This leads to (3.13) thanks to \(\theta =\delta (1-\frac{q}{p})\) and \(1-\theta =(1-\delta )(1-\frac{q}{p})+\frac{q}{p}\).
Step 2. We claim that
for some constant \(C=C(|I|, p,q,r)>0\), where \(\theta \) is given as in (3.12).
Since \({\overline{v}}=0\), we obtain by using (3.13) and (3.4) that
Step 3. Now we are ready to conclude the proof. Let \(u\in \,W^{2,r}(I)\cap W^{1,r}_0(I)\). Then clearly \(u'\in W^{1,r}(I)\) and \(\displaystyle \int _{I}\,u'=0\). Applying (3.14) to \(v:=u'\) we get (3.11). \(\square \)
Remark 3.9
Choose \(q=r=2\) in Proposition 3.8, we see that \(\theta =\frac{1}{2}-\frac{1}{p}\). The inequality (3.11) takes the following form
for all \(2\le p\le \infty \) and \(u\in H^2(I)\cap H^1_0(I)\).
From the above inequalities we deduce the following estimates.
Lemma 3.10
Let \(g=g(y)\in H^2(-1,1)\cap \, H^1_0(-1,1)\). Then, we have
-
(i)
$$\begin{aligned} \Vert g\Vert _{\infty }\lesssim \, E^{1/2}. \end{aligned}$$(3.16)
-
(ii)
$$\begin{aligned} E\,\le \,D. \end{aligned}$$(3.17)
-
(iii)
For every \(2\le \,p\le \infty \),
$$\begin{aligned} \Vert \partial _y\,g\Vert _p\lesssim \,E^{\frac{1}{4}+\frac{1}{2p}}\,D^{\frac{1}{4}-\frac{1}{2p}}. \end{aligned}$$(3.18) -
(iv)
$$\begin{aligned} \Vert \sqrt{1-y^2}\partial _y^2\,g\Vert _2\lesssim \,E^{1/4}\,D^{1/4}. \end{aligned}$$(3.19)
-
(v)
For every \(2\le \,p\,< \infty \),
$$\begin{aligned} \Vert \partial _y^2g\Vert _p\lesssim D^{1/2}. \end{aligned}$$(3.20) -
(vi)
For every \(\epsilon >0\),
$$\begin{aligned} \Vert (1-y^2)^\epsilon \,\partial _y^2\,g\Vert _\infty \lesssim \,D^{1/2}. \end{aligned}$$(3.21)
Proof
-
(i)
Applying (3.1) with \(q=\infty \) and \(p=2\), we obtain (3.16).
-
(ii)
The inequality (3.17) follows from (3.5) with \(p=q=2\). Indeed, applying (3.5) with \(p=q=2\) yields
$$\begin{aligned} E=\frac{1}{2}\Vert \partial _y\,g\Vert _2^2\le & {} 2\Vert \partial _y^2\,g\Vert _2^2\\\le & {} 8\Vert \partial _y^2\,g\Vert _2^2+\frac{1}{2}\Vert \sqrt{1-y^2}\,\partial _y^3\,g\Vert _2^2=D. \end{aligned}$$ - (iii)
-
(iv)
We write, using integration by parts,
$$\begin{aligned} \int _{-1}^1(1-y^2)\left( \partial ^2_y g\right) ^2 dy= & {} \int _{-1}^1(1-y^2)\partial ^2_y g \partial ^2_y g dy\\ {}= & {} -\int _{-1}^1(1-y^2)\partial ^3_y g \partial _y g dy+\int _{-1}^12y\partial ^2_y g \partial _y g dy. \end{aligned}$$Then (3.19) follows by the Cauchy–Schwarz inequality.
-
(v)
To prove (3.20) we write,
$$\begin{aligned} \partial _y^2g(y)= & {} \partial _y^2g(0)+\int _0^y\partial _y^3g(z)dz\\= & {} \partial _y^2g(0)+\int _0^y \sqrt{1-z^2}\partial _y^3g(z)\frac{1}{\sqrt{1-z^2}}dz. \end{aligned}$$Since \(\sqrt{1-y^2}\ge \frac{\sqrt{3}}{2}\) for \(y\in (-{1/2}, {1/2})\), we obtain
$$\begin{aligned} |\partial _y^2g(0)|\lesssim & {} \Vert \partial _y^2g\Vert _{L^\infty (-1/2,-1/2)}\\\lesssim & {} \Vert \partial _y^2g\Vert _{H^1(-1/2,-1/2)} \\\lesssim & {} \Vert \sqrt{1-y^2}\partial _y^3g\Vert _2+\Vert \partial _y^2g\Vert _2\\\lesssim & {} D^{1/2}. \end{aligned}$$By Cauchy–Schwarz’s inequality, we get
$$\begin{aligned} |\partial _y^2g(y)|\lesssim & {} |\partial _y^2g(0)|+\left( \left| \int _0^y \left( \sqrt{1-z^2}\partial _z^3g(z)\right) ^2dz\right| \right) ^{1/2}\left( \left| \int _0^y\frac{1}{1-z^2}dz\right| \right) ^{1/2} \nonumber \\\lesssim & {} D^{1/2}+D^{1/2}\left( \frac{1}{2}\left| \log \left( \frac{1+y}{1-y}\right) \right| \right) ^{1/2} \end{aligned}$$(3.22)The desired inequality (3.20) follows thanks to the fact that \(\left( \left| \log \left( \frac{1+y}{1-y}\right) \right| \right) ^{1/2}\in L^p(-1,1)\) for any \(2\le p<\infty .\)
-
(vi)
Inequality (3.21) can be deduced easily from (3.22) making use of \(x^\alpha \,\log (x)\in L^\infty (0,a)\) for any positive constants \(\alpha \) and a.
\(\square \)
Lemma 3.11
Let \(m\ge 1\) be an integer and \(g=g(y)\in H^2(-1,1)\cap \, H^1_0(-1,1)\). Then we have
Proof
Since \(H^2 \hookrightarrow C^1\) and \(g(\pm 1)=0\), we get by the mean value theorem that
Therefore we obtain thanks to (3.16) and (3.18) (with \(p=\infty \)) that
This finishes the proof. \(\square \)
To obtain the desired decay estimate, we will use the following.
Lemma 3.12
Let \(E, D : [0,\infty )\rightarrow [0,\infty )\) be absolutely continuous functions such that
and
where \(a, b>0\), \(\alpha >1\) and \(\beta > 0\). Then there exists \(\varepsilon >0\) and \(\nu >0\) such that
Proof
Choose \(\varepsilon >0\) small enough such that \(1-a\varepsilon ^\beta >0\) and
Suppose that \(E(0)<\varepsilon \) and define
By continuity of E we deduce that \(T^*>0\). For \(0\le t<T^*\), we have
Using (3.25) we deduce that
where \(\nu \) is given by (3.27). This finally leads to
In particular \(T^*=\infty \) and, for all \(t\in [0,\infty )\), we have
\(\square \)
From the above Lemma we deduce the following.
Corollary 3.13
Let \(E, D : [0,\infty )\rightarrow [0,\infty )\) be absolutely continuous functions such that
and
where \(a, b>0\), \(\alpha _1, \alpha _2>1\) and \(\beta _1, \beta _2> 0\). Then, for \(c_0>0\) satisfying \(1-a(c_0^{\beta _1}+c_0^{\beta _2})>0\) and
we have
4 The Energy Estimate
In this section we will see how to estimate all terms \({{\mathbf {I}}}_k\) to get the following energy inequality leading to the desired decay rate.
Proposition 4.1
We have
Proof
The proof uses similar ideas to those in [6, 22]. We have thanks to (2.12) that
where the energy and the dissipation are given respectively by (2.10) and (2.11).
In what follows we will estimate each term \({{\mathbf {I}}}_k\) for \(k=1,2,\ldots ,10\).
Estimation of \({{\mathbf {I}}}_1\): By Cauchy–Schwarz’s inequality, and using (3.16), (3.18), we get
This leads to
Estimation of \({{\mathbf {I}}}_2\): Using (3.16), we obtain that
Estimation of \({{\mathbf {I}}}_3\): We have
Using (3.16) and (3.18) (with \(p=6\)), we obtain that
Estimation of \({{\mathbf {I}}}_{4}\): We have
Using (3.20) with \(p=4,\) we obtain
Estimation of \({{\mathbf {I}}}_5\): By using an integration by parts, (Note that \((1+g)^5-1=0\) for \(y=\pm 1)\) we can write
Therefore
Estimation of \({{\mathbf {I}}}_6\): By using an integration by parts, we can write
Estimation of \({{\mathbf {I}}}_7\): Making use of (3.16) and (3.21), we can write
Estimation of \({{\mathbf {I}}}_9\): By Hölder’s inequality, (3.16), (3.18) and (3.19), we get
Estimation of \({{\mathbf {I}}}_8\): By integration by parts using the fact that \(y=-\partial _y(\frac{1-y^2}{2})\), we have
Hence
Estimation of \({{\mathbf {I}}}_{10}\): Using integration by parts, we get
Hence we obtain thanks to (3.16), (4.6) and (4.9)
Putting all the estimates (4.2)–(4.12) together, we get
Using the fact that
for \(\alpha _n>\alpha _{n-1}>\cdots>\alpha _1>0\) and \(x\ge 0,\) we conclude that
By Young’s inequality, we have
Using again (4.13) we conclude the proof. \(\square \)
5 Proof of the Main Results
This section is devoted to the proof of the main results stated in the introduction. We begin by proving Theorem 1.1. Using the equivalent expression of the energy E given in (2.10), it suffices to prove the following.
Theorem 5.1
Let g be a global smooth solution of (2.7) with initial data \(g_0\). There exists \(\varepsilon >0\) such that, if
then there exists \(\gamma >0\) such that
Proof
The proof follows by using Proposition 4.1 and Corollary 3.13 with \(\alpha _1=2,\; \alpha _2=10,\; \beta _1={1/3},\; \beta _2={5/2}.\) \(\square \)
Proof of Corollary 1.5
In particular, for \(t=0\) we have
where \(g_0\) in the initial data for g and \(Z(0,y):=Z_0(y)\) is the initial data for Z. The proof follows by using (3.16). \(\square \)
Proof of Corollary 1.6
By (2.3), we have \(Z_y(t,y)=\frac{1}{1+g(t,y)}\). Integrating with respect to y and using \(Z(t,\pm 1)=\lambda _{\pm }(t)\), we find that
It follows from (1.10) and (3.16) that, for t sufficiently large, we have
where \(\gamma \) is as in (1.10). Next, we integrate \((y-\frac{y^3}{3})Z_y\) to get
where we have used
Taking advantage of the fact that \(\displaystyle \int _{-1}^1\,\left( y-\frac{y^3}{3}\right) \,dy=0\), we infer
We conclude the proof of (1.19) by using (5.2), (1.10) and (3.16). Combining (1.18) and (1.19) we obtain (1.20). This finishes the proof of Corollary 1.6. \(\square \)
Proof of Corollary 1.7
By (2.3) and (2.6) we have the equality
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The authors thank the reviewers for the careful reading of the manuscript and helpful comments. The work of N. M is supported by NSF Grant DMS-1716466 and by Tamkeen under the NYU Abu Dhabi Research Institute grant of the center SITE.
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Majdoub, M., Masmoudi, N. & Tayachi, S. Relaxation to Equilibrium in the One-Dimensional Thin-Film Equation with Partial Wetting and Linear Mobility. Commun. Math. Phys. 385, 837–857 (2021). https://doi.org/10.1007/s00220-021-04111-0
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DOI: https://doi.org/10.1007/s00220-021-04111-0