Abstract
We establish the vanishing viscosity limit of the Navier–Stokes equations to the Euler equations for three-dimensional compressible isentropic flow in the whole space. When the viscosity coefficients are given as constant multiples of the density’s power (\(\rho ^\delta \) with \(\delta >1\)), it is shown that there exists a unique regular solution of compressible Navier–Stokes equations with arbitrarily large initial data and vacuum, whose life span is uniformly positive in the vanishing viscosity limit. It is worth paying special attention to the fact that, via introducing a “quasi-symmetric hyperbolic”–“degenerate elliptic” coupled structure to control the behavior of the velocity of the fluid near the vacuum, we can also give some uniform estimates for \(\displaystyle \big (\rho ^{\frac{\gamma -1}{2}}, u\big )\) in \(H^3\) and \(\rho ^{\frac{\delta -1}{2}}\) in \(H^2\) with respect to the viscosity coefficients (adiabatic exponent \(\gamma >1\) and \(1<\delta \leqq \min \{3, \gamma \}\)), which lead to the strong convergence of the regular solution of the viscous flow to that of the inviscid flow in \(L^{\infty }([0, T]; H^{s'})\) (for any \(s'\in {[}2, 3)\)) with the rate of \(\varepsilon ^{2(1-s'/3)}\). Furthermore, we point out that our framework in this paper is applicable to other physical dimensions, say 1 and 2, with some minor modifications.
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1 Introduction
In this paper, we investigate the inviscid limit problem of the 3D isentropic compressible Navier–Stokes equations with degenerate viscosities, when the initial data contain a vacuum and are arbitrarily large. For this purpose, we consider the following isentropic compressible Navier–Stokes equations (ICNS) in \({\mathbb {R}}^3\):
We look for the above system’s local regular solutions with initial data
and the far field behavior
Usually, such kinds of far field behavior occurs naturally under some physical assumptions on (1.1)’s solutions, such as finite total mass and total energy.
In system (1.1), \(x=(x_1,x_2,x_3)\in \mathbb {R}^3\), \(t\geqq 0\) are the space and time variables, respectively, \(\rho \) is the density, and \(u=\left( u^{(1)},u^{(2)},u^{(3)}\right) ^\top \in \mathbb {R}^3\) is the velocity of the fluid. In considering the polytropic gases, the constitutive relation, which is also called the equations of state, is given by
where \(A>0\) is an entropy constant and \(\gamma \) is the adiabatic exponent. \(\mathbb {T}\) denotes the viscous stress tensor with the form
where \(\mathbb {I}_3\) is the \(3\times 3\) identity matrix,
\(\mu (\rho )\) is the shear viscosity coefficient, \(\lambda (\rho )+\frac{2}{3}\mu (\rho )\) is the bulk viscosity coefficient, \(\varepsilon \in (0,1]\) is a constant, \(\alpha \) and \(\beta \) are both constants satisfying
and in this paper, we assume that the constant \(\delta \) satisfies
In addition, when \(\varepsilon =0\), from (1.1), we naturally have the compressible isentropic Euler equations for the inviscid flow:
which is a fundamental example of a system of hyperbolic conservation laws.
Throughout this paper, we adopt the following simplified notations, most of which are for the standard homogeneous and inhomogeneous Sobolev spaces:
A detailed study of homogeneous Sobolev spaces can be found in Galdi [14].
1.1 Existence Theories of Compressible Flow with Vacuum
Before formulating our problem, we first briefly recall a series of frameworks on the well-posedness of multi-dimensional strong solutions with initial vacuum established for the hydrodynamics equations mentioned above in the whole space. For the inviscid flow, in 1987, via writing (1.9) as a symmetric hyperbolic form that allows the density to vanish, Makino–Ukai–Kawshima [31] obtained the local-in-time existence of the unique regular solution with \(\inf \rho _0=0\), which can be shown by
Theorem 1.1
[31] Let \( \gamma >1\). If the initial data \(( \rho _0, u_0)\) satisfy
then there exist a time \(T_0>0\) and a unique regular solution \((\rho , u)\) to Cauchy problem (1.9) with (1.2)–(1.3) satisfying
where the regular solution \((\rho , u)\) to (1.9) with (1.2)–(1.3) is defined by
It should be pointed out that the condition \((\text {C})\) ensures the uniqueness of the regular solution and makes the velocity u well defined in vacuum region. Without \((\text {C})\), it is difficult to get enough information on velocity even for considering special cases such as point vacuum or continuous vacuum on some surface. In 1997, by extracting a dispersive effect after some invariant transformation, Serre [36] obtained the global existence of the regular solution shown in Theorem 1.1 with small density.
For the constant viscous flow (i.e., \(\delta =0\) in (1.6)), the corresponding local-in-time well-posedness of strong solutions with vacuum was firstly solved by Cho–Choe–Kim [8, 9] in 2004–2006; to compensate the lack of a positive lower bound of the initial density, they introduced an initial compatibility condition
which plays a key role in getting some uniform a priori estimates with respect to the lower bound of \(\rho _0\); see also Duan–Luo–Zheng [12] for the 2D case. Later, based on the uniform estimate on the upper bound of the density, Huang–Li–Xin [20] extended this solution to be a global one under some initial smallness assumption for the isentropic flow in \(\mathbb {R}^3\).
Recently, the degenerate viscous flow (i.e., \(\delta =0\) in (1.6)) described by (1.1) has received extensive attention from the mathematical community (see the review papers [2, 28]), based on the following two main considerations: on the one hand, through the second-order Chapman-Enskog expansion from Boltzmann equations to the compressible Navier–Stokes equations, it is known that the viscosity coefficients are not constants but functions of the absolute temperature (cf. Chapman–Cowling [6] and Li–Qin [25]), which can be reduced to the dependence on density for isentropic flow from laws of Boyle and Gay-Lussac (see [25]); on the other hand, we do have some good models in the following 2D shallow water equations for the height h of the free surface and the mean horizontal velocity field U:
It is clear that system (1.13) is a special case or a simple variant of system (1.1) for some appropriately chosen viscous term \(\mathcal {V}(h, U)\) (see [5, 15, 16, 32]). Some important progress has been obtained in the development of the global existence of weak solutions with a vacuum for system (1.1) and related models, see Bresh–Desjardins [2,3,4], Mellet–Vasseur [33] and some other interesting results, c.f. [24, 29, 40, 41].
However, in the presence of a vacuum, compared with the constant viscosity case [8], there appear to be some new mathematical challenges in dealing with such systems for constructing solutions with high regularities. In particular, these systems become highly degenerate, the result of which is that the velocity cannot even be defined in the vacuum domain and hence it is difficult to get uniform estimates for the velocity near the vacuum. Recently Li–Pan–Zhu [26, 27]-via carefully analyzing the mathematical structure of these systems-reasonably gave the time evolution mechanism of the fluid velocity in the vacuum domain. Taking \(\delta =1\), for example, via considering the following parabolic equations with a special source term:
we could transfer the degenearcy shown in system (1.1) caused by the far field vacuum to the possible singualrity of the quantity \(\nabla \rho /\rho \), which was luckily shown to be well defined in \(L^6\cap D^1\). Based on this, by making full use of the symmetrical structure of the hyperbolic operator and the weak smoothing effect of the elliptic operator, they established a series of a priori estimates independent of the lower bound of \(\rho _0\), and successfully gave the local existence theory of classical solutions with arbitrarily large data and vacuum for the case \(1\leqq \delta \leqq \min \Big \{3,\frac{\gamma +1}{2}\Big \}\). We refer readers to Zhu [42, 43] for more details and progress.
1.2 Vanishing Viscosity Limit from Viscous Flow to Inviscid Flow
Based on the well-posedness theory mentioned above, naturally there is an important question can we regard the regular solution of inviscid flow [31, 36] as those of viscous flow [8, 12, 20, 26, 27] with vanishing real physical viscosities?
Actually, there is a lot of literature on the uniform bounds and the vanishing viscosity limit in the whole space. The idea of regarding inviscid flow as viscous flow with vanishing real physical viscosity dates back to Dafermos [10], Hugoniot [22], Rankine [34], Rayleigh [35] and Stokes [39]. However, until 1951, Gilbarg [17] gave us the first rigorous convergence analysis of vanishing physical viscosities from the Navier–Stokes equations (1.1) to the isentropic Euler equations (1.9), and established the mathematical existence and vanishing viscous limit of the Navier–Stokes shock layers. The framework on the convergence analysis of piecewise smooth solutions has been established by G\(\grave{\text {u}}\)es–M\(\acute{\text {e}}\)tivier–Williams–Zumbrun [18], Hoff–Liu [19], and the references cited therein. The convergence of vanishing physical viscosity with general initial data was first studied by Serre–Shearer [37] for a \(2\times 2\) system in nonlinear elasticity with severe growth conditions on the nonlinear function in the system. In 2009, based on the uniform energy estimates and compactness compensated argument, Chen–Perepelitsa [7] established the first convergence result for the vanishing physical viscosity limit of solutions of the Navier–Stokes equations to a finite-energy entropy weak solution of the isentropic Euler equations with finite-energy initial data, which has been extended to the density-dependent viscosity case (experiencing degeneracy near vacuum states) by Huang–Pan–Wang–Wang–Zhai [21].
However, even in 1D space, due to the complex mathematical structure of hydrodynamics equations near the vacuum, the existence of strong solutions to the viscous flow and inviscid flow are usually established in totally different frameworks, for example, [8] and [31]. The proofs shown in [8, 12, 26] essentially depend on the uniform ellipticity of the Lamé operator L, and the a priori estimates on the solutions and their life spans \(T^{v}\) obtained in the above references both strictly depend on the real physical viscosities. For example, when \(\delta =0\) (i.e., \(\mu =\varepsilon \alpha \) and \(\lambda =\varepsilon \beta \)), we have
which implies that the current frameworks do not seem to work for verifying the expected limit relation. Thus the vanishing viscosity limit for the multi-dimensional strong solutions in the whole space from Navier–Stokes equations to Euler equations for compressible flow with initial vacuum in some open set or at the far field is still an open problem.
In this paper, motivated by the uniform estimates on \(\varepsilon ^{\frac{1}{2}}\nabla ^3\rho ^{\frac{\delta -1}{2}} \) and \(\varepsilon ^{\frac{1}{2}}\rho ^{\frac{\delta -1}{2}} \nabla ^4 u\), when the viscous stress tensor has the form (1.6)–(1.8), we aim at giving a positive answer for this question by introducing a “quasi-symmetric hyperbolic"–“degenerate elliptic" coupled structure to control the behavior of the velocity near the vacuum. We believe that the method developed in this work could give us a good understanding of the mathematical theory of vacuum, and also can be adapted to some other related vacuum problems in a more general framework, such as the inviscid limit problem for multi-dimensional finite-energy weak solutions in the whole space.
1.3 Symmetric Formulation and Main Results
We first need to analyze the mathematical structure of the momentum equations (1.1)\(_2\) carefully, which can be divided into hyberbolic, elliptic and source parts as follows:
For smooth solutions \((\rho ,u)\) away from the vacuum, these equations could be written as
Then if \(\rho \) is smooth enough, we could pass to the limit as \(\rho \rightarrow 0\) on both sides of (1.17) and formally have
which, along with (1.17), implies that the velocity u can be governed by a nonlinear degenerate parabolic system if the density function contains vacuum.
In order to establish uniform a priori estimates for u in \(H^3\) that is independent of \(\varepsilon \) and the lower bound of the initial density, we hope that the first order terms on the left-hand side of (1.17) could be put into a symmetric hyperbolic structure, then we can deal with the estimates on u in \(H^3\) without being affected by the \(\varepsilon \)-dependent degenerate elliptic operator. However, this is impossible. The problem is that the term \( \nabla \rho ^{\delta -1} \cdot \mathbb {S}(u)\) is actually a product of two first order derivatives with the form \(\sim \rho ^{\delta -2} \nabla \rho \cdot \nabla u\), and obviously there is no similar term in the continuity equation (1.1)\(_1\). This also tells us that it is not enough if we only have the estimates on \(\rho \). Some more elaborate estimates for the density related quantities are really needed.
By introducing two new quantities,
equations (1.1) can be rewritten into a new system that consists of a transport equation for \(\varphi \), and a “quasi-symmetric hyperbolic"–“degenerate elliptic" coupled system with some special lower order source terms for \((\phi ,u)\):
where \(W=(\phi , u)^\top \) and
with \(a_1=\frac{(\gamma -1)^2}{4A\gamma }>0\) and \(Q(u)=\frac{\delta }{\delta -1}\mathbb {S}(u)\). Meanwhile, \(\partial _j W=\partial {x_j}W\), and
Here \(e_j=(\delta _{1j},\delta _{2j},\delta _{3j})\)\((j=1,2,3)\) is the Kronecker symbol satisfying \(\delta _{ij}=1\), when \( i=j\) and \(\delta _{ij}=0\), otherwise. For any \(\xi \in {{\mathbb {R}}}^4\), we have
For simplicity, we denote the symmetric hyperbolic structure shown in the right-hand side of (1.19)\(_2\) as SH.
Considering the above system (1.19), first SH does not include all the first order terms related on \(\big (\rho ^{\frac{\gamma -1}{2}},u\big )\,\big (\hbox { i.e.},\,\varepsilon {\mathbb {H}}(\varphi ) \cdot \mathbb {{Q}}(W)\big )\), so we called the equations (1.19)\(_2\) a “quasi-symmetric hyperbolic"–“degenerate elliptic" system. Second, the characteristic speeds of SH in the direction \(\mathbf l \in S^2\) are \(u\cdot \mathbf l \), with multiplicity two, and \(u\cdot \mathbf l \pm \sqrt{P_\rho }\), with multiplicity one, which means that this structure fails to be strictly hyperbolic near the vacuum even in one-dimensional or two-dimensional spaces. At last, this formulation implies that if we can give some reasonable analysis on the additional variable \(\rho ^{\frac{\delta -1}{2}}\), such that the \(\rho ^{\frac{\delta -1}{2}}\)-related terms will vanish as \(\varepsilon \rightarrow 0\) and also do not influence the estimates on \(\big (\rho ^{\frac{\gamma -1}{2}},u\big )\), then it is hopeful for us to get the desired uniform estimates on \(\big (\rho ^{\frac{\gamma -1}{2}},u\big )\) in \(H^3\).
Based on the above observations, we first introduce a proper class of solutions to system (1.1) with arbitrarily large initial data and vacuum.
Definition 1.1
(Regular solution to the Cauchy problem (1.1)-(1.3)) Let \(T> 0\) be a finite constant. A solution \((\rho ,u)\) to the Cauchy problem (1.1)–(1.3) is called a regular solution in \( [0,T]\times \mathbb {R}^3\) if \((\rho ,u)\) satisfies this problem in the sense of distributions and:
where \(s'\in [2,3)\) is an arbitrary constant.
In order to establish the vanishing viscosity limit from the viscous flow to the inviscid flow, first we give the following uniform (with respect to \(\varepsilon \)) local-in-time well-posedness to the Cauchy problem (1.1)–(1.3).
Theorem 1.2
(Uniform Regularity) Let (1.8) hold. If initial data \(( \rho _0, u_0)\) satisfies
then there exists a time \(T_*>0\) independent of \(\varepsilon \), and a unique regular solution \((\rho , u)\) in \([0,T_*]\times \mathbb {R}^3\) to the Cauchy problem (1.1)–(1.3) satisfying the following uniform estimates:
for arbitrary constant \(s'\in [2,3)\) and positive constant \(C^0=C^0(\alpha , \beta , A, \gamma , \delta , \rho _0, u_0)\). Actually, \((\rho , u)\) satisfies the Cauchy problem (1.1)–(1.3) classically in positve time \((0, T_*]\).
Moreover, if the following condition holds:
we still have
Remark 1.1
The new varible \(\phi \) is actually the constant multiple of local sound speed c of the hydrodynamics equations:
Remark 1.2
Compared with [27], we not only extend the viscosity power parameter \(\delta \) to a broder region \(1< \min \{\delta , \gamma \}\leqq 3\), but also establish a more precise estimate that the life span of the regular solution has a uniformly positive lower bound with respect to \(\varepsilon \). Actually, our desired a priori estimates mainly come from the “quasi-symmetric hyperbolic”–“degenerate elliptic” coupled structure (1.19)\(_2\), and the details could be seen in Section 3. Moreover, we point out that the regular solution obtained in the above theorem will break down in finite time, if the initial data contain “isolated mass group” or “hyperbolic singularity set”, which could be rigorously proved via the same arguments used in [27].
Remark 1.3
If we relax the initial assumption from \(\rho ^{\frac{\gamma -1}{2}}_0 \in H^3\) to \(\rho ^{\gamma -1}_0 \in H^3\), then the correspongding local-in-time well-posedness for quantities \((\rho ^{\gamma -1},\rho ^{\frac{\delta -1}{2}},u)\) still can be obtained by the similar argument used to prove Theorem 1.2. However, for this case, the uniform positive lower bound of the life span and the uniform a priori estimates with respect to \(\varepsilon \) are not available, because the change of variable from c to \(c^2\) has directly destroyed the symmetric hyperbolic structure as shown in the left hand side of (1.19)\(_2\).
Letting \(\varepsilon \rightarrow 0,\) the solution obtained in Theorem 1.2 will strongly converge to that of the compressible Euler equations (1.9) in \(C([0,T];H^{s'})\) for any \( s'\in [1,3)\). Meanwhile, we can also obtain the detail convergence rates, that is
Theorem 1.3
(Inviscid Limit) Let (1.8) hold. Suppose that \((\rho ^\varepsilon , u^\varepsilon )\) is the regular solution to the Cauchy problem (1.1)–(1.3) obtained in Theorem 1.2, and \((\rho , u)\) is the regular solution to the Cauchy problem (1.9) with (1.2)–(1.3) obtained in Theorem 1.1. If
satisfies (1.23), then \(\big (\rho ^{\varepsilon }, u^{\varepsilon }\big )\) converges to \((\rho , u)\) as \(\varepsilon \rightarrow 0\) in the that sense
for any constant \(s'\in [0, 3)\). Moreover, we also have
where \(C>0\) is a constant depending only on the fixed constants \(A, \delta , \gamma , \alpha , \beta , T_*\) and \( \rho _0, u_0\).
Furthermore, if the condition (1.25) holds, we still have
Remark 1.4
It should be pointed out that conclusions of Theorems 1.2–1.3 still hold when viscosities \(\mu \) and \(\lambda \) are in the general form
where \(\alpha (\rho )\) and \(\beta (\rho )\) are functions of \(\rho \), satisfying
For function pairs \((g_1(\rho ),g_2(\rho ))\) have the form \(\sim \rho ^p\), it is obviously that they do not belong to \(C^4(\mathbb {R}^+)\) when \(p<4\) due to the presence of the vacuum. However, Theorems 1.2–1.3 still hold if the initial data satisfies the additional initial assumptions
where \(P_{k_i}(\rho )\)\((i=1,2)\) is a \(k_i\)-th degree polynomial of \(\rho \) with vanishing constant term, and the minimum power of density in all the terms of \(P_{k_i}(\rho )\) should be greater than or equal to \(\frac{\delta -1}{2}\). Furthermore, our framework in this paper is applicable to other physical dimensions, say 1 and 2, after some minor modifications.
The rest of the paper is organized as follows: in Section 2, we list some basic lemmas that will be used in our proof. In Section 3, based on some uniform estimates for
we will give the proof for the uniform (with respect to \(\varepsilon \)) local-in-time well-posedness of the strong solution to the reformulated Cauchy problem (3.1), which is achieved in the following four steps:
-
(1)
Via introducing a uniform elliptic operator \(\varepsilon (\varphi ^2+\eta ^2)Lu\) with artificial viscosity coefficients \(\eta ^2>0\) in momentum equations, the global well-posedness of the approximation solution to the corresponding linearized problem (3.6) for \((\varphi ,\phi ,u)\) has been established (Section 3.1).
-
(2)
We establish the uniform a priori estimates with respect to \((\eta , \varepsilon )\) for
$$\begin{aligned} \displaystyle \big (\phi , u\big ) \quad \text {in} \quad H^3, \quad \text {and} \quad \varphi \quad \text {in} \quad H^2, \end{aligned}$$to the linearized problem (3.6) in \([0,T_*]\), where the time \(T_*\) is also independent of \((\eta , \varepsilon )\) (Section 3.2).
-
(3)
Via passing to the limit as \(\eta \rightarrow 0\), we obtain the solution of the linearized problem (3.60), which allows that the elliptic operator appearing in the reformulated momentum equations is degenerate (Section 3.3).
-
(4)
Based on the uniform analysis for the linearized problem, we prove the uniform (with respect to \(\varepsilon \)) local-in-time well-posedness of the non-linear reformulated problem through the Picard iteration approach (Section 3.4).
According to the uniform local-in-time well-posedness and a priori estimates (with respect to \(\varepsilon \)) to non-linearized problem (3.1) obtained in Section 3, in Section 4, we will give the proof for Theorem 1.2. Finally in Section 5, the convergence rates from the viscous flow to inviscid flow will be obtained, which is the proof of Theorem 1.3.
2 Preliminaries
In this section, we show some basic lemmas that will be frequently used in the proofs to follow. The first one is the well-known Gagliardo-Nirenberg inequality.
Lemma 2.1
[23] For \(p\in [2,6]\), \(q\in (1,\infty )\), and \(r\in (3,\infty )\), there exists some generic constant \(C> 0\) that may depend on q and r such that for
we have
Some special versions of this inequality can be written as
The second one can be found in Majda [30]. Here we omit its proof.
Lemma 2.2
[30] Let constants r, a and b satisfy the relation
\( \forall s\geqq 1\), if \(f, g \in W^{s,a} \cap W^{s,b}(\mathbb {R}^3)\), then we have
where \(C_s> 0\) is a constant only depending on s, and \(\nabla ^s f\) (\(s>1\)) is the set of all \(\partial ^\zeta _x f\) with \(|\zeta |=s\). Here \(\zeta =(\zeta _1,\zeta _2,\zeta _3)\in \mathbb {R}^3\) is a multi-index.
The third one will show some compactness results from the Aubin-Lions Lemma.
Lemma 2.3
[38] Let \(X_0\), X and \(X_1\) be three Banach spaces with \(X_0\subset X\subset X_1\). Suppose that \(X_0\) is compactly embedded in X and that X is continuously embedded in \(X_1\). Then:
-
I)
Let G be bounded in \(L^p(0,T;X_0)\) where \(1\leqq p < \infty \), and \(\frac{\partial G}{\partial t}\) be bounded in \(L^1(0,T;X_1)\), then G is relatively compact in \(L^p(0,T;X)\).
-
II)
Let F be bounded in \(L^\infty (0,T;X_0)\) and \(\frac{\partial F}{\partial t}\) be bounded in \(L^p(0,T;X_1)\) with \(p>1\), then F is relatively compact in C(0, T; X).
The following lemma will be used to show the time continuity for the higher order terms of our solution:
Lemma 2.4
[1] If \(f(t,x)\in L^2([0,T]; L^2)\), then there exists a sequence \(s_k\) such that
Next we give some Sobolev inequalities on the interpolation estimate, product estimate, composite function estimate and so on in the following three lemmas:
Lemma 2.5
[30] Let \(u\in H^s\), then for any \(s'\in [0,s]\), there exists a constant \(C_s\) only depending on s such that
Lemma 2.6
[30] Let functions \(u,\ v \in H^s\) and \(s>\frac{3}{2}\), then \(u\cdot v \in H^s\), and there exists a constant \(C_s\) only depending on s such that
Lemma 2.7
[30]
-
(1)
For functions \(f,\ g \in H^s \cap L^\infty \) and \(|\nu |\leqq s\), there exists a constant \(C_s\) only depending on s such that
$$\begin{aligned} \begin{aligned} \Vert \nabla ^\nu (fg)\Vert _s\leqq C_s(|f|_{\infty }|\nabla ^s g|_2+|g|_{\infty }|\nabla ^s f|_{2}). \end{aligned} \end{aligned}$$(2.5) -
(2)
Assume that g(u) is a smooth vector-valued function on G, u(x) is a continuous function with \(u\in H^s \cap L^\infty \). Then for \(s\geqq 1\), there exists a constant \(C_s\) only depending on s such that
$$\begin{aligned} \begin{aligned} |\nabla ^s g(u)|_2\leqq C_s\Big \Vert \frac{\partial g}{\partial u }\Big \Vert _{s-1}|u|^{s-1}_{\infty }|\nabla ^s u|_{2}. \end{aligned} \end{aligned}$$(2.6)
The last lemma is a useful tool for improving the weak convergence to a strong one.
Lemma 2.8
[30] If function sequence \(\{w_n\}^\infty _{n=1}\) converges weakly in a Hilbert space X to w, then \(w_n\) converges strongly to w in X if and only if
For simplicity, by introducing four matrices \(A_1, A_2, A_3, B=(b_{ij})=(\mathbf b _1,\mathbf b _2,\mathbf b _3)\), a vector \(W=(w_1,w_2,w_3)^\top \), and letting \(A=(A_1,A_2, A_3)\), we denote
The above symbols will be used throughtout the rest of the paper.
3 Uniform Regularity
In this section, we will establish the desired uniform regularity shown in Theorem 1.2. As the discussion shown in Subsection 1.3, for this purpose we need to consider the following reformulated problem:
where \(W=(\phi , u)^\top \) and
The definitions of \(A_j\) (\(j=0,1,...,3\)), \(\mathbb {L}\), \(\mathbb {H}\) and \(\mathbb {Q}\) can be found in (1.20)–(1.22).
To prove Theorem 1.2, our first step is to establish the following existence of the unique strong solutions for the reformulated problem (3.1):
Theorem 3.1
If the initial data \(( \varphi _0, \phi _0, u_0)\) satisfy
then there exists a positive time \(T_*\) independent of \(\varepsilon \), and a unique strong solution \((\varphi , \phi , u)\) in \([0,T_*] \times \mathbb {R}^3\) to the Cauchy problem (3.1) satisfying
for any constant \(s' \in [2,3)\). Moreover, we can also obtain the following uniform estimates:
where \(C^0\) is a positive constant depending only on \(T_*\), \((\varphi _0, \phi _0,u_0 )\) and the fixed constants A, \(\delta \), \(\gamma \), \(\alpha \) and \(\beta \), and is independent of \(\varepsilon \).
We will subsequently prove Theorem 3.1 through the next four Subsections (3.1–3.4), and in the next section, we will show that this theorem indeed implies Theorem 1.2.
3.1 Linearization with an Artificial Strong Elliptic Operator
Let T be any positive time. In order to construct the local strong solutions for the nonlinear problem, we need to consider the following linearized approximation problem:
where \(\eta \in (0,1]\) is a constant, \(W=(\phi , u)^\top , V=\left( \psi , v\right) ^\top \) and \(W_0=(\phi _0,u_0)^\top \). \((\omega , \psi )\) are both known functions and \(v=(v^{(1)},v^{(2)},v^{(3)})^\top \in \mathbb {R}^3\) is a known vector satisfying the initial assumption \((\omega , \psi , v)(t=0,x)=(\varphi _0,\phi _0, u_0)\) and
for any constant \(s'\in [2,3)\). Moreover, we assume that
Now we have the following global existence of a strong solution \((\varphi , \phi , u)\) to (3.6) by the standard methods at least when \(\eta >0\):
Lemma 3.1
Assume that the initial data \((\varphi _0, \phi _0,u_0)\) satisfy (3.8). Then there exists a unique strong solution \((\varphi ,\phi ,u)\) in \([0,T]\times \mathbb {R}^3\) to (3.6) when \(\eta >0\) such that
Proof
First, the existence and regularities of a unique solution \(\varphi \) in \((0,T)\times \mathbb {R}^3\) to the equation (3.6)\(_1\) can be obtained by the standard theory of transport equation (see [13]).
Second, when \(\eta >0\), based on the regularities of \(\varphi \), it is not difficult to solve W from the linear symmetric hyperbolic-parabolic coupled system (3.6)\(_2\) to complete the proof of this lemma (see [13]). Here we omit its details.\(\quad \square \)
In the next two subsections, we first establish the uniform estimates for \((\phi ,u)\) in \(H^3\) space with respect to both \(\eta \) and \(\varepsilon \), then we pass to the limit for the case: \(\eta =0\).
3.2 A Priori Estimates Independent of \((\eta , \varepsilon )\)
Let \((\varphi , \phi , u)\) be the unique strong solution to (3.6) in \([0,T] \times \mathbb {R}^3\) obtained in Lemma 3.1. In this subsection, we will get some local (in time) a priori estimates for \((\phi ,u)\) in \(H^3\) space, which are independent of \((\eta , \varepsilon )\) listed in the following Lemmas 3.2–3.5. For this purpose, we fix \(T>0\) and a positive constant \(c_0\) large enough such that
and
for some time \(T^*\in (0,T)\) and constants \(c_i\) (\(i=1,2,3\)) such that
The constants \(c_i\) (\(i=1,2,3\)) and \(T^*\) will be determined later (see (3.58)) and depend only on \(c_0\) and the fixed constants \(\alpha \), \(\beta \), \(\gamma \), A, \(\delta \) and T.
Hereinafter, we use \(C\geqq 1\) to denote a generic positive constant depending only on fixed constants \(\alpha \), \(\beta \), \(\gamma \), A, \(\delta \) and T, but is independent of \((\eta , \varepsilon )\), which may be different from line to line. We start from the estimates for \(\varphi \).
Lemma 3.2
Let \((\varphi ,W)\) be the unique strong solution to (3.6) on \([0,T] \times \mathbb {R}^3\). Then
for \(0\leqq t \leqq T_1=\min (T^*, (1+c_3)^{-2})\).
Proof
We apply the operator \(\partial ^\zeta _x\)\((0\leqq |\zeta |\leqq 3)\) to (3.6)\(_1\), and obtain
Then multiplying both sides of (3.12) by \(\partial ^\zeta _x {\varphi }\), and integrating over \(\mathbb {R}^3\), we get
where
First, when \(|\zeta |\leqq 2\), we consider the term \(\Lambda ^\zeta _1\) and \(\Lambda ^\zeta _2\). It follows from Lemma 2.1 and Hölder’s inequality that
which, along with (3.13)–(3.14), implies that
Then, according to Gronwall’s inequality, one has
for \(0\leqq t\leqq T_1=\min \{T^*,(1+c_3)^{-2}\}\).
Second, when \(|\zeta |=3\), it follows from Lemma 2.1 and Hölder’s inequality that
Then, combining (3.13)–(3.17), we arrive at
which, along with Gronwall’s inequality, implies that
Therefore, observing that
from (3.19), one can obtain that
At last, the estimates for \(\varphi _t\) follow from the relation:
For \(0\leqq t \leqq T_1\), we easily have
Thus, we complete the proof of this lemma. \(\quad \square \)
Based on Gagliardo-Nirenberg-Sobolev and interpolation inequalities, we firstly present several useful inequalities
which will be frequently used in the proofs to follow.
Using the notations in (2.7), now we show the estimate for \(\Vert W\Vert _1\).
Lemma 3.3
Let \((\varphi , W)\) be the unique strong solution to (3.6) on \([0,T] \times \mathbb {R}^3\). Then
for \(0\leqq t\leqq T_2=\min \{T_1,(1+c_3)^{-4}\}\).
Proof
Applying the operator \(\partial ^\zeta _x\) to (3.6)\(_2\), we have
Then multiplying (3.22) by \(\partial ^\zeta _x W\) on both sides and integrating over \(\mathbb {R}^3\) by parts, we have
Now we consider the terms on the right-hand side of (3.23) when \(|\zeta |\leqq 1\). First, it follows from Lemmas 2.1, 3.2, Hölder’s inequality and Young’s inequality that
where we have used the fact (3.21).
Similarly, for the terms \(I_{5}\)-\(I_{6}\), using (3.21), one can obtain that
Then from (3.23)–(3.25), we have
which, along with Gronwall’s inequality, implies that
for \(0\leqq t\leqq T_2=\min \{T_1,(1+c_3)^{-4}\}\). \(\quad \square \)
Next we show the estimate for \(|W|_{D^2}\).
Lemma 3.4
Let \((\varphi , W)\) be the unique strong solution to (3.6) on \([0,T] \times \mathbb {R}^3\). Then
Proof
We divide the proof into two steps.
Step 1: the estimate of \(|W|_{D^2}\). First we need to consider the terms on the right-hand side of (3.23) when \(|\zeta | =2\). It follows from Lemmas 2.1 and (3.23), Hölder’s inequlaity and Young’s inequality that
where we have used (3.21) and
For the term \(I_3\), via integration by parts and (3.21), one has
For the term \(I_4\), one gets
For the terms \(I_{5}\)-\(I_6\), using (3.21)and (3.29), one has
Then, from (3.23) and (3.28)–(3.32), we have
which, along with Gronwall’s inequaltiy, implies that
Step 2: the estimate for \(W_t\). First, the estimate for \(\phi _t\) follows from
For \(0\leqq t \leqq T_2\), we easily have that
Second, we consider the estimate for \(|\partial ^\zeta _x u_t|_2\) when \(|\zeta |\leqq 1\). From the relation
one can obtain
Similarly, for \(|u_t|_{D^1}\), using (3.29), we have
which implies that
\(\square \)
Finally, we give the estimates on the highest order terms: \(\nabla ^3 W\) and \(\varphi \nabla ^4 u\).
Lemma 3.5
Let \((\varphi , W)\) be the unique strong solution to (3.6) on \([0,T] \times \mathbb {R}^3\). Then
Proof
We divide the proof into two steps.
Step 1: the estimate of \(|W|_{D^3}\). First we need to consider the terms on the right-hand side of (3.23) when \(|\zeta | =3\). For the term \(I_1\), it is easy to see that
For the terms \(I_2\)-\(I_3\), via integration by parts, (3.21) and (3.29), one has
For the term \(I_4\), letting \(r=b=2\), \(a=\infty \), \(f=A_j\), \(g=\partial _j W\) in (2.3) of Lemma 2.2, one can obtain
For the term \(I_{5}\), using (3.21) and (3.29), one gets
For the term \(I_{6}\), we notice that
where \(\zeta =\zeta ^1+\zeta ^2+\zeta ^3\) are three multi-indexes \(\zeta ^i\in \mathbb {R}^3\)\((i=1,2,3)\) satisfying \(|\zeta ^i|=1\); \(C_{1ijk}\) and \(C_{2ijk}\) are all constants; \(l_{ijk}=1\) if i, j and k are different from each other, otherwise \(l_{ijk}=0\). Then, one has
Using (3.21) and (3.29), we first consider the first two terms on the right-hand side of (3.43):
For the term \(I_{63}\), it follows from the integration by parts that
For simplicity, we only consider the case that \(i=1\), the rest terms can be estimated similarly. When \(i=1\), similarly to the estimates on \(I_{61}\) in (3.44), we first have
Next, for the term \(I_{632}\), one has
For the term \(I_A\), it is not hard to show that
For the term \(I_B\), it follows from integration by parts that
Via an argument similar to that used in (3.49), we also have
which, along with (3.43)–(3.48), implies that
Then from (3.24)–(3.42) and (3.51), one has
which, along with Gronwall’s inequaltiy, implies that
for \(0\leqq t\leqq T_2\).
Step 2: the estimates for \(|\partial ^\zeta _x W_t|_2\) when \(1\leqq |\zeta |\leqq 2\). First from (3.35), we have
Second, it follows from (3.38) that
Finally, for \(|W_t|_{D^2}\), from Lemma 2.6, one gets
which implies that
\(\square \)
Combining the estimates obtained in Lemmas 3.2-3.5, we have
for \(0 \leqq t \leqq \min \{T, (1+c_3)^{-4}\}\). Therefore, if we define the constants \(c_i\) (\(i=1,2,3\)) and \(T^*\) by
then we deduce that
In other words, given fixed \(c_0\) and T, there exist positive constants \(T^*\) and \(c_i\) (\(i=1,2,3\)), depending solely on \(c_0\), T and the generic constant C, independent of \((\eta ,\varepsilon )\), such that if (3.11) holds for \(\omega \) and V, then (3.59) holds for the strong solution of (3.6) in \([0, T^*]\times \mathbb {R}^3\).
3.3 Passing to the Limit as \(\eta \rightarrow 0\)
Based on the local (in time) a priori estimates (3.59), we have the following existence result under the assumption that \(\varphi _0\geqq 0\) to the following Cauchy problem:
Lemma 3.6
Assume \((\varphi _0, W_0)\) satisfy (3.8). Then there exists a time \(T^*>0\) that is independent of \(\varepsilon \), and a unique strong solution \((\varphi , W)\) in \([0,T^*]\times \mathbb {R}^3\) to (3.60) such that
for any constant \(s'\in [2,3)\). Moreover, \((\varphi , W)\) also satisfies the a priori estimates (3.59).
Proof
We prove the existence, uniqueness and time continuity in three steps.
Step 1 existence. Due to Lemma 3.1 and the uniform estimates (3.59), for every \(\eta >0\), there exists a unique strong solution \((\varphi ^\eta , W^\eta )\) in \([0,T^*]\times \mathbb {R}^3\) to the linearized problem (3.6) satisfying estimates (3.59), where the time \(T^*>0\) is also independent of \((\eta , \varepsilon )\).
By virtue of the uniform estimates (3.59) independent of \((\eta ,\varepsilon )\) and the compactness in Lemma 2.3 (see [38]), we know that for any \(R> 0\), there exists a subsequence of solutions (still denoted by) \((\varphi ^\eta , W^\eta )\), which converges to a limit \((\varphi ,W)=(\varphi , \phi , u)\) in the following strong sense:
Again by virtue of the uniform estimates (3.59) independent of \((\eta ,\varepsilon )\), we also know that there exists a subsequence of solutions (still denoted by) \((\varphi ^\eta , W^\eta )\), which converges to \((\varphi , W)\) in the following weak or weak* sense:
which, along with the lower semi-continuity of weak convergence, implies that \((\varphi , W)\) also satisfies the corresponding estimates (3.59) except those of \(\varphi \nabla ^4 u\).
Combining the strong convergence in (3.62) and the weak convergence in (3.63), we easily obtain that \((\varphi , W) \) also satisfies the local estimates (3.59) and
Now we want to show that \((\varphi , W) \) is a weak solution in the sense of distributions to the linearized problem (3.60). Multiplying (3.6)\(_2\) by test function \(f(t,x)=(f^1,f^2,f^3)\in C^\infty _c ([0,T^*)\times \mathbb {R}^3)\) on both sides, and integrating over \([0,T^*]\times \mathbb {R}^3\), we have
Combining the strong convergence in (3.62) and the weak convergences in (3.63)–(3.64), and letting \(\eta \rightarrow 0\) in (3.65), we have
Thus it is obvious that \((\varphi , W) \) is a weak solution in the sense of distributions to the linearized problem (3.60), satisfying the regularities
Step 2 uniqueness. Let \((\varphi _1,W_1)\) and \((\varphi _2,W_2)\) be two solutions obtained in the above step. We denote
Then from (3.60)\(_{1}\), we have
which quickly implies that \(\overline{\varphi }=0\).
Let \(\overline{W}=(\overline{\phi },\overline{u})^\top \), from (3.60)\(_{2}\) and \(\varphi _1=\varphi _2\), we have
Then multiplying (3.68) by \(\overline{W}\) on both sides, and integrating over \(\mathbb {R}^3\), we have
From Gronwall’s inequality, we obtain that \(\overline{W}=0\) in \(\mathbb {R}^3\), which gives the uniqueness.
Step 3 time continuity. First for \( \varphi \), via the regularities shown in (3.67) and the classical Sobolev imbedding theorem, we have
Using the same arguments as in Lemma 3.2, we have
which implies that
Then according to Lemma 2.8 and (3.70), we know that \(\varphi \) is right continuous at \(t=0\) in \(H^3\) space. From the reversibility on the time to equation (3.60)\(_1\), we know
For \(\varphi _t\), from
we only need to consider the term \(\omega \text {div}v\). Due to
and the Sobolev imbedding theorem, we have
which implies that
The similar arguments can be used to deal with \(\phi \).
For velocity u, from the regularity shown in (3.67) and Sobolev’s imbedding theorem, we obtain that
Then from Lemma 2.5, for any \(s'\in [2,3)\), we have
Together with the upper bound shown in (3.59) and the time continuity (3.77), we have
Finally, we consider \(u_t\). From equations (3.60)\(_2\) we have
where
From (3.67), we have
which means that
Then combining (3.7), (3.73), (3.78) and (3.81), we deduce that
\(\square \)
3.4 Proof of Theorem 3.1
Our proof is based on the classical iteration scheme and the existence results for the linearized problem obtained in Section 3.4. Like in Section 3.3, we define constants \(c_{0}\) and \(c_{i}\) (\(i=1,2,3\)), and assume that
Let \((\varphi ^0, W^0=(\phi ^0,u^0))\), with the regularities
be the solution to the problem
We take a time \(T^{**}\in (0,T^*]\) small enough such that
Proof
We prove the existence, uniqueness and time continuity in three steps.
Step 1 existence. Let \((\omega ,\psi , v)=(\varphi ^0,\phi ^0,u^0)\), we define \((\varphi ^1, W^1)\) as a strong solution to problem (3.60). Then we construct approximate solutions
inductively, by assuming that \((\varphi ^{k}, W^{k})\) was defined for \(k\geqq 1\), let \((\varphi ^{k+1},W^{k+1})\) be the unique solution to problem (3.60) with \((\omega ,\psi ,v)\) replaced by \( (\varphi ^k, W^k)\) as follows:
It follows from Lemma 3.6 that the sequence \((\varphi ^k, W^{k})\) satisfies the uniform a priori estimates (3.59) for \(0 \leqq t \leqq T^{**}\).
Now we prove the convergence of the whole sequence \((\varphi ^k, W^k)\) of approximate solutions to a limit \((\varphi , W)\) in some strong sense. Let
with
Then, from (3.85), one has
First, we consider \(|\overline{\varphi }^{k+1}|_2\). Multiplying (3.86)\(_1\) by \(2\overline{\varphi }^{k+1}\) and integrating over \(\mathbb {R}^3\), one has
which means that (\(0<\nu \leqq \frac{1}{10}\) is a constant)
with \(A^k_\nu (t)=C\big (1+\nu ^{-1} \big )\).
Second, we consider \(|\overline{W}^{k+1}|_2\). Multiplying (3.86)\(_2\) by \(\overline{W}^{k+1}\) and integrating over \(\mathbb {R}^3\), one gets
For the terms \(J_1-J_4\), it follows from (3.21) and (3.29) that
where we have used the fact (see Lemma 2.1) that
Next, we begin to consider the term \(J_5\). First we have
where \(u^{k,j}\) represents the j-th component of \(u^k\) (\(k\geqq 1\)),
and the quantity \(a^{ij}_k\) is given by
and \(\delta _{ij}\) is the Kronecker symbol satisfying \(\delta _{ij}=1,\ i=j\) and \(\delta _{ij}=0\), otherwise.
For terms \(J_{51}\)-\(J_{53}\), using (3.21), (3.29) and (3.90), one can obtain
For the last term on the right-hand side of (3.91), one has
which, along with (3.91)–(3.93), implies that
For the term \(J_6\), we have
which, together with (3.88)-(3.89) and (3.94)–(3.95), immediately implies that
Finally, we denote
From (3.87) and (3.96), one has
for some \(E^k_\nu \) such that \(\int _{0}^{t}E^k_\nu (s)\,\text {d}s\leqq C+C_\nu t\). From Gronwall’s inequality, one gets
We can choose \(\nu _0>0\) and \(T_*\in (0,\min (1,T^{**}))\) small enough such that
which implies that
Thus, from the above estimate for \(\Gamma ^{k+1}(T_*)\) and (3.59), we know that the whole sequence \((\varphi ^k,W^k)\) converges to a limit \((\varphi , W)\) in the following strong sense:
Due to the local estimates (3.59) and the lower-continuity of norm for weak or \(\hbox {weak}^*\) convergence, we know that \((\varphi , W)\) satisfies the estimates (3.59). According to the strong convergence in (3.97), it is easy to show that \((\varphi , W)\) is a weak solution of (3.1) in the sense of distribution with the regularities:
Thus the existence of strong solutions is proved.
Step 2 uniqueness. Let \((W_1,\varphi _1)\) and \((W_2,\varphi _2)\) be two strong solutions to Cauchy problem (3.1) satisfying the uniform a priori estimates (3.59). We denote that
then according to (3.86), \((\overline{\varphi },\overline{\phi },\overline{u})\) satisfies the system
Using the same arguments as in the derivation of (3.87)–(3.96), and letting
we similarly have
From Gronwall’s inequality, we have \(\overline{\varphi }=\overline{\phi }=\overline{u}=0\). Then the uniqueness is obtained.
Step 3 the time-continuity. It can be obtained via the same arguments used in in the proof of Lemma 3.6. \(\quad \square \)
4 Proof of Theorem 1.2
Based on Theorem 3.1, now we are ready to prove the uniform local-in-time well-posedenss (with respect to \(\varepsilon \)) of the regular solution to the original Cauchy problem (1.1)–(1.3), i.e., the proof of Theorem 1.2. Moreover, we will show that the regular solutions that we obtained satisfy system (1.1) classically in positive time \((0,T_*]\).
Proof
We divide the proof into three steps.
Step 1 existence of regular solutions. First, for the initial assumption (1.23), it follows from Theorem 3.1 that there exists a positive time \(T_*\) independent of \(\varepsilon \) such that the problem (3.1) has a unique strong solution \((\varphi ,\phi ,u)\) in \([0,T_*]\times \mathbb {R}^3\) satisfying the regularities in (3.4), which means that
Noticing that \(\rho =\varphi ^{\frac{2}{\delta -1}}\) and \(\frac{2}{\delta -1}\geqq 1\), it is easy to show that
Second, the system (3.1)\(_2\) for \(W=(\phi ,u)\) could be written as
Multiplying (4.2)\(_1\) by \( \frac{\partial \rho }{\partial \phi }(t,x)=\frac{2}{\gamma -1}\phi ^{\frac{3-\gamma }{\gamma -1}}(t,x)\in C((0,T_*)\times \mathbb {R}^3) \) on both sides, we get the continuity equation in (1.1)\(_1\):
Multiplying (4.2)\(_2\) by \( \phi ^{\frac{2}{\gamma -1}}=\rho (t,x)\in C^1((0,T_*)\times \mathbb {R}^3) \) on both sides, we get the momentum equations in (1.1)\(_2\):
Finally, recalling that \(\rho \) can be represented by the formula
where \(U\in C^1([0,T_*]\times [0,T_*]\times \mathbb {R}^3)\) is the solution to the initial value problem
it is obvious that
That is to say, \((\rho ,u)\) satisfies the problem (1.1)–(1.3) in the sense of distributions, and has the regularities shown in Definition 1.1, which means that the Cauchy problem (1.1)–(1.3) has a unique regular solution \((\rho ,u)\). \(\quad \square \)
Step 2 the smoothness of regular solutions. Now we will show that the regular solution that we obtained in the above step is indeed a classcial one in positive time \((0, T_*]\).
Due to the definition of regular solution and the classical Sobolev imbedding theorem, we immediately know that
Now we only need to prove that
Proof
According to Theorem 1.2 in Section 3, the solution \((\varphi , \phi ,u)\) of problem (3.1) satisfies the regularities (3.4) and \((\phi ,\varphi ) \in C^1([0,T_*]\times \mathbb {R}^3)\).
Next, we first give the continuity of \(u_t\). We differentiate (4.2)\(_2\) with respect to t:
which, along with (3.4), easily implies that
Applying the operator \(\partial ^\zeta _x\)\((|\zeta |=2)\) to (4.6), multiplying the resulting equations by \(\partial ^\zeta _x u_t\) and integrating over \(\mathbb {R}^3\), we have
Now we consider the terms on the right-hand side of (4.8). It follows from the Hölder’s inequality, Lemma 2.1 and Young’s inequality that
where the term \(J_{121}\) can be estimated as follows:
Via intergration by parts, for the last term \(J_{1211}\) on the right-hand side of (4.10), one has
It follows from (4.8)–(4.11) that
Then multiplying both sides of (4.12) with t and integrating over \([\tau ,t]\) for any \(\tau \in (0,t)\), one gets
According to the definition of the regular solution, we know that
which, along with Lemma 2.4, implies that there exists a sequence \(s_k\) such that
Then, letting \(\tau =s_k \rightarrow 0\) in (4.13), we have
so we have
Based on the classical Sobolev imbedding theorem
for any \(q\in (3,6)\), from (4.7) and (4.15), we have
which implies that \( u_t \in C((0,T_*]\times \mathbb {R}^3) \).
Finally, we consider the continuity of \(\text {div}\mathbb {T}\). Denote \(\mathbb {N}=\varepsilon \varphi ^2 Lu-\varepsilon \nabla \varphi ^2\cdot Q(u).\) Based on (3.4) and (4.15), we have
From \(\mathbb {N}_t\in L^2(0,T_*; L^2)\) and (4.16), we obtain \(t\mathbb {N}\in C([0,T_*];W^{1,4}),\) which implies that \(\mathbb {N}\in C((0,T_*]\times {{\mathbb {R}}}^3)\). Since \(\rho \in C([0,T_*]\times {{\mathbb {R}}}^3)\) and \(\text {div}\mathbb {T}=\rho \mathbb {N},\) then we obtain the desired conclusion. \(\square \)
Step 3 the proof of (1.26). If \(1<\delta \leqq \frac{5}{3},\) that is \(\frac{2}{\delta -1}\geqq 3.\) Due to
then we have
Noticing
it is not difficult to show that
From the continuity equation (1.1)\(_1\), and (4.17)-(4.18), we have
Similarly, we can deal with cases: \(\delta =2\) or 3. Then the proof of Theorem 1.2 is finished.
5 Vanishing Viscosity Limit
In this section, we will establish the vanishing viscosity limit stated in Theorem 1.3. First we denote by
the solution of problem (3.1), that is
The definitions of \(A_j\) (\(j=0,1,...,3\)), \(\mathbb {L}\), \(\mathbb {H}\) and \(\mathbb {Q}\) could be find in (1.20)–(1.22).
Second, based on [31], we denote by
the regular solution of compressible Euler equations (1.9), which can be written as the following symmetric system:
From Theorem 3.1, there exists a time \(T^1_*>0\) that is independent of \(\varepsilon \) such that the solution \((\varphi ^\varepsilon , W^\varepsilon )\) of Cauchy problem (5.1) satisfies
where \(C^0\) is a positive constant depending only on \(T^1_*\), \(( \varphi _0, W_0)\) and the fixed constants A, \(\delta \), \(\gamma \), \(\alpha \) and \(\beta \), and is independent of \(\varepsilon \).
From [31] (see Theorem 1.1), we know that there exits a time \(T^2_{*}\) such that there is a unique regular solution W of Cauchy problem (5.2) satisfies
Denote \(T^*=\min \{T^1_*, T^2_* \}\). Then, letting \(\overline{W}^\varepsilon =W^\varepsilon -W\), (5.1)\(_2\) and (5.2)\(_1\) lead to
If the initial data
satisfies (1.23), it is obviously to see that \(\overline{W}^\varepsilon (x,0)\equiv 0.\)
Next we give some lemmas for establishing the vanishing viscosity limit.
Lemma 5.1
If \((\varphi ^\varepsilon , W^\varepsilon )\) and W are the regular solutions of Navier–Stokes (5.1) and Euler equations (5.2) respectively, then we have
where the constant \(C>0\) depends on A, \(\alpha \), \(\beta \), \(\delta \), \((\rho _0, u_0)\) and \( T_*\).
Proof
Multiplying (5.5) by \(2\overline{W}^\varepsilon \) on both sides and integrating over \({{\mathbb {R}}}^3\), then one has
It follows from the integrating by parts and Hölder’s inequality that
where we used (3.21). According to the Gronwall’s inequality, (5.7) follows immediately. \(\quad \square \)
Now we consider the estimate of \(|\partial _x^\zeta \overline{W}^\varepsilon |_2,\) as \(|\zeta |=1.\)
Lemma 5.2
If \((\varphi ^\varepsilon , W^\varepsilon )\) and W are the regular solutions of Navier–Stokes (5.1) and Euler equations (5.2) respectively, then we have
where the constant \(C>0\) depends on A, \(\alpha \), \(\beta \), \(\delta \), \((\rho _0, u_0)\) and \( T_*\).
Proof
Applying the operator \(\partial _x^\zeta \) on (5.5), one gets
Then multiplying (5.10) by \(2\partial ^\zeta _x \overline{W}^\varepsilon \) and integrating over \(\mathbb {R}^3\) by parts, one can obtain that
where \(\overline{u}^\varepsilon =u^\varepsilon -u\). For \(|\zeta |=1\), one gets
Substituting (5.12) into (5.11), one has
Then, according to the Gronwall’s inequality, (5.9) follows immediately. \(\square \)
For \(|\zeta |=2,\) we have
Lemma 5.3
If \((\varphi ^\varepsilon ,W^\varepsilon )\) and W are the regular solutions of Navier–Stokes (5.1) and Euler equations (5.2) respectively, then we have
where the constant \(C>0\) depends on A, \(\alpha \), \(\beta \), \(\delta \), \((\rho _0, u_0)\) and \( T_*\).
Proof
For \(|\zeta |=2,\) it follows from (3.21) and (5.11) that
Substituting (5.14) into (5.11), we have
Then, according to Gronwall’s inequality, (5.13) follows immediately. \(\quad \square \)
Finally, we have
Lemma 5.4
If \((\varphi ^\varepsilon ,W^\varepsilon )\) and W are the regular solutions of Navier–Stokes (5.1) and Euler equations (5.2) respectively, then we have
where \(s'\in (2,3)\) and the constant \(C>0\) depends on A, \(\alpha \), \(\beta \), \(\delta \), \((\rho _0, u_0)\) and \( T_*\).
Proof
Based on Lemma 2.5, (3.3), (5.3) and (5.4), we have
\(\square \)
Finally, we give the proof for Theorem 1.3.
Proof
First, according to Lemmas 5.1-5.4, when \(\varepsilon \rightarrow 0\), the solutions \(\big (\rho ^{\varepsilon }, u^{\varepsilon }\big )\) of compressible Navier–Stokes solutions converges to the solution \((\rho , u)\) of compressible Euler equations in the following sense:
for any constant \(s'\in [0, 3)\). Moreover, one can also obtain that
where \(C>0\) is a constant depending only on the fixed constants \(A, \delta , \gamma , \alpha , \beta , T_*\) and \( \rho _0, u_0\).
Further more, if the condition (1.25) holds, one has \(\frac{2}{\delta -1}\geqq 3\). Then, from (5.16)–(5.17), it is not hard to see that
Thus the proof of Theorem 1.3 is finished. \(\quad \square \)
Remark 5.1
For the case \(\delta =1\) with vacuum at the far field, via introducing two different symmetric structures in Ding–Zhu [11], some uniform estimates with respect to the viscosity coefficients for \(\displaystyle \Big (\rho ^{\frac{\gamma -1}{2}}, u\Big )\) in \(H^3(\mathbb {R}^2)\) and \(\displaystyle \nabla \rho /\rho \) in \(L^6\cap D^1(\mathbb {R}^2)\) have been obtained, which lead the convergence of the regular solution of the viscous flow to that of the inviscid flow still in \(L^{\infty }([0, T]; H^{s'}(\mathbb {R}^2))\) (for any \(s'\in [2, 3)\)) with the rate of \(\varepsilon ^{2(1-\frac{s'}{3})}\); their conclusion also applies to the 2-D shallow water equations (1.13).
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Acknowledgements
This research was funded in part by National Natural Science Foundation of China under Grants 11201308, 11231006, 11571232 and 11831011. The research of Shengguo Zhu was also supported in part by the Royal Society– Newton International Fellowships NF170015.
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Geng, Y., Li, Y. & Zhu, S. Vanishing Viscosity Limit of the Navier–Stokes Equations to the Euler Equations for Compressible Fluid Flow with Vacuum. Arch Rational Mech Anal 234, 727–775 (2019). https://doi.org/10.1007/s00205-019-01401-9
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DOI: https://doi.org/10.1007/s00205-019-01401-9