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Research article

Incompressible limit of Euler equations with damping

  • Received: 12 September 2021 Revised: 02 October 2021 Accepted: 09 October 2021 Published: 13 December 2021
  • The Cauchy problem for the compressible Euler system with damping is considered in this paper. Based on previous global existence results, we further study the low Mach number limit of the system. By constructing the uniform estimates of the solutions in the well-prepared initial data case, we are able to prove the global convergence of the solutions in the framework of small solutions.

    Citation: Fei Shi. Incompressible limit of Euler equations with damping[J]. Electronic Research Archive, 2022, 30(1): 126-139. doi: 10.3934/era.2022007

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  • The Cauchy problem for the compressible Euler system with damping is considered in this paper. Based on previous global existence results, we further study the low Mach number limit of the system. By constructing the uniform estimates of the solutions in the well-prepared initial data case, we are able to prove the global convergence of the solutions in the framework of small solutions.



    We are concerned with the 3D compressible Euler equations with frictional damping

    {tρ+(ρu)=0,ρ(tu+(u)u)+1ε2p(ρ)=Aρu. (1.1)

    Here, xT3, t>0, the unknown functions ρ and u denote the density and velocity of the fluid respectively; the pressure-density function p is given by

    p(ρ)=aργ,a>0,γ>1;

    the constant A>0 is the friction coefficient and ε is the Mach number. The system can be used to model the compressible fluid flow through a porous media.

    The compressible Euler equations with damping can be used to simulate the motion for the compressible gas flow through a porous medium. The medium induces a friction force, proportional to the linear momentum in the opposite direction. Usually, this model has many variations. For example, the friction coefficient A may depend on time [1] and, more generally, one can consider the nonlinear damping [2]. Here, we only study the constant-coefficient linear damping case.

    It is well-known that the compressible Euler equations will develop singularity in finite time for general initial data [3]. However, the damping effect will prevent the formation of singularities in small amplitude flows, but large solutions may still break down [31]. Due to strong physical background and significant mathematical challenge, system (1.1) with fixed Mach number has been studied by many researchers. The readers are referred to [30] for BV solutions and [4,5] for L solution. For the existence of weak solutions, we refer to [6,7]. While for global classical solution, see [8,9,10,11,12]. We also refer to [13,14,15,16,17,18] and references therein for further studies in this direction and related problems.

    In particular, the global-in-time existence and asymptotic behavior of the classical solution were obtained by Wang and Yang [11]. By employing the Green's function method and energy estimate, they proved that if the suitable Sobolev norm of the initial data is small, then the global existence of classical solution can be obtained, and the L2 norm of the solution decays at the rate of t3/4 in the whole space.

    Physically, the Mach number represents the ratio of the typical speed of the flow to the speed of sound. In practical applications, the incompressible equations are often used when the Mach number is sufficiently small. So it is natural to think, under appropriate conditions on the initial data, that solutions of the compressible system converge to the solution of the incompressible system when the Mach number goes to zero. This is the low Mach number limit problem in fluid mechanics.

    Over the past four decades, many results have been obtained about the incompressible limit of fluid dynamic equations, which is a special case of the low Mach number limit. In their ground-breaking works [19,20], Klainerman and Majda setup a general framework for the study of singular limit of hyperbolic PDEs. With the general theory, they proved the incompressible limit of isentropic Euler equations in the well-prepared initial data case. For general initial data, Ukai [21] obtained the convergence of the solutions in the whole space. Finally by using the filtering method, Schochet [22] solved the incompressible limit problem for Euler equations in the torus case. Concerning the low Mach number limit of the non-isentropic Euler equations, we refer to [23,24,25].

    Since these pioneering works, the mathematical analysis of the low Mach number limit to the isentropic Navier-Stokes equations also attracted a lot of attention. In the framework of weak solutions, the incompressible limit of Navier-Stokes equations in the periodic case and bounded domain was studied in [26] and [27] respectively. For global-in-time regular solutions, Bessaih [28] established the uniform estimates of the solutions with almost incompressible initial data and proved the convergence to the solution of incompressible system with no-slip boundary conditions. Ou [29] further extended this result to the slip-type boundary conditions.

    For the local classical solutions, the incompressible limit of the system (1.1) can be established in a similar fashion as the compressible Euler equations. If the damping effect is considered, it is possible to study the incompressible limit of the system (1.1) for all time since we have global small solutions. To the best of our knowledge, there are no results studying the global incompressible limit of Euler equations with damping. Incompressible fluid flow differs from compressible fluid flow in that the continuity equation is replaced by the divergence-free condition on the velocity field. Mathematically, the low Mach number limit attempts to bridge the gap between those two different descriptions and, in some sense, it is relatively easy to study the incompressible system instead of the compressible equations.

    In this paper, based on the previous global existence results of the Euler system with damping, we are going to study the global incompressible limit to system (1.1) in the framework of small amplitude solutions. Namely, we will show that as the Mach number goes to zero, the solutions to Eqs (1.1) will converge to the solution of the following system

    {ˉρ(tv+(v)v)+π=Aˉρv,v=0, (1.2)

    where ˉρ is some constant and π can be formally obtained by applying to the first equation.

    The rest of the paper is arranged as follows. In Section 2, we reformulate the Cauchy problem for Eq (1.1) into a symmetric hyperbolic system and state the global existence of classical solutions to the system with fixed Mach number. In Section 3, the global uniform estimates of the solution are obtained. Finally with the uniform estimates, we will prove the convergence of the solutions of the original equations (1.1) to the solution of the limit system in Section 4.

    Notation. Throughout the paper C will denote a positive constant whose value may be different in each occurrence, that may depend PDEs, domain, and Sobolev index, but are independent of the small parameter ε. The small letter c and its variants denote similar constants whose value is fixed. αx or simply α with multi-index α stands for the usual spatial derivatives. For any integer s0, Hs denote the inhomogeneous Sobolev space Hs(T3) with the norm Hs. We denote =L2 for simplicity. Generally, the solution is dependent on the small parameter ε in this paper, so it is better to write the solution uε(t,x) rather than u(t,x) for example. But for simplicity, we always omit the superscript ε and use u(t,x) instead when there is no confusion.

    In this short section, we will give a reformulation of the problem. To simplify the presentation, we introduce

    h(ρ)=aγγ1ργ1. (2.1)

    Using h and u as the new unknown functions, we get from the original equation (1.1) that

    {e(h)(th+(u)h)+u=0,tu+(u)u+1ε2h=Au, (2.2)

    where

    e(h)=1(γ1)h

    is a smooth functions of h>0.

    In this paper, we will consider the perturbative solutions of the above equations. Thus we choose the constant equilibrium state (h,0) with h>0 and set

    h=h+εq.

    The system satisfied by q and u is

    {e(h)(tq+(u)q)+1εu=0,tu+(u)u+1εq=Au. (2.3)

    Initial data is given by

    q(t=0)=q0(x),u(t=0)=u0(x). (2.4)

    For fixed ε>0, it has been proved by many authors, c.f. [11,31], that (2.3)–(2.4) admits a global classical solution provided that the certain Sobolev norm of the initial data is sufficiently small. Namely, we have the following global existence theorem.

    Theorem 2.1. For any fixed ε>0, suppose that the initial data (q0(x),u0(x))Hs(T3) with s3 and (q0(x),u0(x))Hs(T3) is sufficiently small. Then there exists a unique, global, classical solution (qε(x,t),uε(x,t)) to the Cauchy problem of (2.3)–(2.4).

    The aim of the present paper is to show that the sequences of the solution (qε(x,t),uε(x,t)) actually converge to the solution of a limit system for all time. The key step is to establish the uniform estimates both in Mach number and time.

    In this part, we are going to prove the uniform estimates of the solution. To this end, we define a weighted norm

    E(w)=w2H3+tw2H2+ε2ttw2H1+ε4tttw2. (3.1)

    First, we have the following estimate.

    Lemma 3.1. If U=(q,u)C([0,T];H3) is a solution of the system (2.3)–(2.4) for any given T>0, then we have

    ddtE(U)+AE(u)CE(U)32. (3.2)

    Proof. The proof is divided into two parts. First, we will show that

    ddtU2H3+Au2H3CE(U)32. (3.3)

    Second, we shall prove that

    ddt3k=1ε2k2ktU2H3k+A3k=1ε2k2ktu2H3kCE(U)32. (3.4)

    Thus, by the definition of the functional E(U), it is obvious that (3.2) holds.

    Part Ⅰ: For 0|α|3, applying αx to (2.3) and testing by αxU gives

    T3e(h)(tαxq+(u)αxq)αxqdx+T3(tαxu+(u)αxu)αxudx+AT3αxuαxudx=T3C1αxqdx+T3C2αxudx, (3.5)

    where the singular terms are cancelled by integration by parts and the commutators C1 and C2 are given by

    C1=[αx,e(h)]tq[αx,e(h)u]qC2=[αx,u]u.

    By direct calculation, we get

    T3e(h)(tαxq+(u)αxq)αxqdx=12ddtT3e(h)|αxq|2dx12T3te(h)|αxq|2dx12T3(e(h)u)|αxq|2dx

    and

    T3(tαxu+(u)αxu)αxudx=12ddtT3|αxu|2dx12T3u|αxu|2dx.

    Combining the above two equalities with (3.5), one finds

    12ddtT3e(h)|αxq|2dx+12ddtT3|αxu|2dx+AT3αxuαxudx12|T3te(h)|αxq|2dx|+12|T3(e(h)u)|αxq|2dx|+12|T3u|αxu|2dx|+|T3C1αxqdx+T3C2αxudx|. (3.6)

    Clearly, the first three terms on the right-hand side of (3.6) can be controlled by

    te(h)Lαxq2+(e(h)u)Lαxq2+uLαxu2CE(U)32, (3.7)

    where standard Sobolev embedding inequalities are used here. The commutator estimates is given by

    |T3C1αxqdx|=|T3{[αx,e(h)]tq[αx,e(h)u]q}αxqdx|β+γ=α,|β|>0CβαT3[|βxe(h)γxtq|+|βx(e(h)u)γxq|]αxqdx.

    We only consider the case |α|=3, because other cases are relatively easy to deal with. When |β|=1,|γ|=2, we have

    T3[|βxe(h)γxtq|+|βx(e(h)u)γxq|]αxqdxC[βxe(h)Lγxtq+βx(e(h)u)Lγxq]αxqCE(U)32. (3.8)

    When |β|=2,|γ|=1,

    T3[|βxe(h)γxtq|+|βx(e(h)u)γxq|]αxqdxC[βxe(h)L3γxtqL6+βx(e(h)u)L3γxqL6]αxqC[βxe(h)γxtq+βx(e(h)u)γxq]αxqCE(U)32. (3.9)

    When |β|=3,|γ|=0,

    T3[|βxe(h)γxtq|+|βx(e(h)u)γxq|]αxqdxC[βxe(h)tqL+βx(e(h)u)qL]αxqCE(U)32. (3.10)

    Collecting (3.8)–(3.10), we get the following estimate

    |T3C1αxqdx|CE(U)32.

    In a similar fashion, one can show that

    |T3C2αxudx|CE(U)32.

    Substituting the commutator estimates and (3.7) into (3.6) and taking summation over 0|α|3, we get

    ddtU2H3+Au2H3CE(U)32. (3.11)

    This completes the proof of the first part.

    Part Ⅱ: For 1k3 and k+|α|3, applying ktαx to (2.3) and testing by ε2k2ktαxU gives

    ε2k2T3e(h)(tktαxq+(u)ktαxq)ktαxqdx+ε2k2T3(tktαxu+(u)ktαxu)ktαxudx+Aε2k2T3ktαxuktαxudx=ε2k2T3C3ktαxqdx+ε2k2T3C4ktαxudx, (3.12)

    where

    C3=[ktαx,e(h)]tq[ktαx,e(h)u]q,C4=[ktαx,u]u.

    By integrating by parts, we still have

    ε2k2ddtT3[e(h)|ktαxq|2+|ktαxu|2]dx+Aε2k2T3|ktαxu|2dxε2k2T3C3ktαxqdx+ε2k2T3C4ktαxudx+CE(U)32. (3.13)

    It remains to give the estimates of the commutators. Basically, the commutator estimates is similar to (3.8)–(3.10) except that we need to guarantee there are enough powers of ε to balance the norms of the unknowns. We should be careful when we encountered with higher time derivatives. For example, the estimate of the first term in C3 will involve

    2tqαxe(h),

    with |α|=2. The definition of E(U) suggests that there should be a ε to balance 2tq. Fortunately, since h=h+εq, taking derivative to e(h) will give us an additional ε. The other terms in the commutator is similar, we just omit the details for the sake of simplicity.

    Using the strategy we explained above to estimate the commutators, we get

    εk1C3+εk1C4CE(U). (3.14)

    Combined with (3.13), one has

    ε2k2ddt[ktαxq2+ktαxu2]+Aε2k2ktαxu2dxCE(U)32. (3.15)

    By taking summation over 1k3 and k+|α|3, we get the desired results (3.4). This completes the proof of Lemma 3.1.

    Next, we have the following lemma.

    Lemma 3.2. If U=(q,u)C([0,T];H3) is a solution of the system (2.3)–(2.4), then

    1ε2q2H3C(ut2H2+u2H2)+CE(U)2CE(u)+CE(U)2, (3.16)

    and

    ddt0|α|+k2ε2kT3[k+1tαxuktαxu+(u)ktαxuktαxu]dx+0|α|+k2ε2kk+1tαxq2CE(u)+CE(U)32. (3.17)

    Proof. For 0|α|2, taking αx to the second equation of (2.3) yields

    αx[tu+(u)u]+1εαxq=Aαxu. (3.18)

    This further gives

    1ε2αxq2αx[tu+(u)u]2+Aαxu2. (3.19)

    Taking summation over 0|α|2 gives

    1ε2q2H3C(ut2H2+u2H2)+CE(U)2, (3.20)

    where we have used the Poincaré inequality to control qL2.

    Next, for 0k+|α|2, taking ktαx to the first equation of (2.3) gives

    e(h)(k+1tαxq+(u)ktαxq)+1εktαxu=C5, (3.21)

    where the commutator C5 is given by

    C5=[ktαx,e(h)]tq[ktαx,e(h)u]q.

    Then, multiplying the above equation by k+1tαxq and integrating over T3, we have

    T3e(h)|k+1tαxq|2dx+T3e(h)(u)ktαxqk+1tαxqdx+1εT3ktαxuk+1tαxqdx=T3C5k+1tαxqdx. (3.22)

    Applying k+1tαx to the second equation of (2.3) gives

    k+2tαxu+(u)k+1tαxu+1εk+1tαxq=Ak+1tαxu+C6, (3.23)

    with

    C6=[k+1tαx,u]u. (3.24)

    Multiplying the above equation by ktαxu and integrating over T3, one has

    T3k+2tαxuktαxudx+T3(u)k+1tαxuktαxudx+1εT3k+1tαxqktαxudx=AT3k+1tαxuktαxudx+T3C6ktαxudx. (3.25)

    Adding (3.22) to (3.25), then multiplying by ε2k yields

    ε2kT3e(h)|k+1tαxq|2dx=ε2kT3e(h)(u)ktαxqk+1tαxqdxε2kT3k+2tαxuktαxudxε2kT3(u)k+1tαxuktαxudxAε2kT3k+1tαxuktαxudx+ε2kT3C5k+1tαxq+ε2kT3C6ktαxudx6j=1Ij. (3.26)

    Each term on the right-hand side of the above equality need to be estimated now. For I1, we have

    |I1|ε2ke(h)uLktαxqk+1tαxqCE(U)32.

    The second term I2 can be reformulated into

    I2=ε2kddtT3k+1tαxuktαxudx+ε2kT3|k+1tαxu|2dx.

    Similarly, we have

    I3=ε2kddtT3(u)ktαxuktαxudx+ε2kT3(tu)ktαxuktαxudx+ε2kT3(u)ktαxuk+1tαxudx.

    While for I4, it is easy to find that

    |I4|Cε2kk+1tαxuktαxuCE(u).

    For the estimates of the commutators, we mention that there are enough powers of ε to balance the time derivatives of the solution. Thus, I5 and I6 can be handled in a similar way as Lemma 3.1. For simplicity, we omit the details of the estimates and give

    |I5|+|I6|CE(U)32.

    Finally, putting the above estimates of Ij into (3.26) and taking summation over0k+|α|2, we get

    ddt0|α|+k2ε2kT3[k+1tαxuktαxu+(u)ktαxuktαxu]dx+ε2k0|α|+k2T3e(h)|k+1tαxq|2dxCE(u)+CE(U)32. (3.27)

    This completes the proof of Lemma 3.2.

    Now, following the two lemmas above, we are ready to give the uniform estimates of the solutions. Multiplying (3.16) and (3.17) by a sufficiently small constant κ, adding them onto (3.2), we get

    ddt[E(U)+κ0|α|+k2ε2kT3[k+1tαxuktαxu+(u)ktαxuktαxu]dx]+AE(u)+κε2q2H3+κ0|α|+k2ε2kk+1tαxq2CκE(u)+CE(U)3/2+CE(U)2. (3.28)

    Notice that the first term CκE(u) on the right-hand side of (3.28) can be absorbed by AE(u) due to the smallness of κ, thus one has

    ddt˜E(U)+c1E(U)+c2ε2q2H3CE(U)3/2+CE(U)2, (3.29)

    where

    ˜E(U)=E(U)+κ0|α|+k2ε2kT3[k+1tαxuktαxu+(u)ktαxuktαxu]dx.

    Now, assume a priori that

    E(U)δ,

    with δ being sufficiently small. Then by the smallness of ε and κ, we find that ˜E(U) is equivalent to E(U). Namely, there exist positive constant c3 and c4 such that

    c3E(U)˜E(U)c4E(U). (3.30)

    Moreover, since δ is small, we find all the terms on the right-hand side of (3.29) can be absorbed by the c1E(U). This gives

    ˜E(U(t))+c5t0[E(U(τ))+1ε2q(τ)2H3]dτ˜E(U0). (3.31)

    Thus if we assume that the initial data is sufficiently small such that

    E(U0)δ0<c3c4δ,

    we can get from (3.30) and (3.31) that

    c3E(U)˜E(U(t))˜E(U0)c4E(U0)c3δ.

    This closes the a priori assumption and we get the uniform estimates of the solution. In a word, we have proved:

    Theorem 3.3. Suppose that the initial data (q0(x),u0(x))H3(T3). Then there exist positive constants δ0 and ε0 such that if

    E(U0)δ0

    and 0<ε<ε0 hold, system (2.3)–(2.4) admits a global classical solution (q(x,t),u(x,t)) satisfying

    E(U(t))+ct0[E(U(τ))+1ε2q(τ)2H3]dτCδ0, (3.32)

    for all tR+.

    With the uniform estimates established in previous section, we shall study the convergence of the solution in this section.

    Actually, from the uniform estimates (3.32) and the Aubin-Lions compactness lemma, we can find a limit function

    u0L(R+;H3(T3))C(R+;H3η(T3))

    with η>0 such that, by passing to a subsequence,

    uεu0,weak in L(R+;H3(T3)), (4.1)
    uεu0,strongly in C(R+;H3η(T3)). (4.2)

    Let P be the orthogonal projection of (L2(Ω))3 onto the subspace

    Hσ={u(L2(Ω))3|Ωuϕdx=0,ϕH1(Ω)}.

    Applying P to the second equation of (2.3) yields

    P[tuε+(uε)uε+Auε]=0.

    Letting ε goes to zero in the above equations and using (4.1), (4.2), one has

    P[tu0+(u0)u0+Au0]=0.

    By the properties of P, there exists a function π0L(R+;H3(T3)) such that

    tu0+(u0)u0+Au0=π0. (4.3)

    On the other hand, the first equation in (2.3) gives

    εe(hε)(tqε+(uε)qε)+uε=0.

    The uniform estimates (3.32) enables us to take ε0 in the above equation to get

    u0=0. (4.4)

    Equations (4.3) and (4.4) constitute the limit system

    {tu0+(u0)u0+Au0=π0,u0=0,u0|t=0=u00(x), (4.5)

    where the initial data u00(x) is given by uε0u00(x)H30 as ε0.

    The author declares there is no conflict of interest.



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