Abstract
The structural stability for supersonic solutions of the Euler–Poisson system for hydrodynamical model in semiconductor devices and plasmas in two dimensional domain is established, under the perturbation of the flow velocity and the strength of electric field in the horizontal direction at the entrance of a channel. First, the Euler–Poisson system in the supersonic region is reformulated into a second order hyperbolic–elliptic coupled system together with several transport equations. One of the key ingredients of the analysis is to obtain the well-posedness of the boundary value problem for the associated linearized hyperbolic–elliptic coupled system, which is achieved via a delicate choice of multiplier to gain energy estimate. The nonlinear structural stability of supersonic solution in the general situation is established by combining the iteration method with the estimate for hyperbolic–elliptic system and the transport equations together.
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Acknowledgements
The authors thank the referees for their helpful comments to improve the presentation of the paper. The research of Myoungjean Bae was supported in part by Samsung Science and Technology Foundation under Project No. SSTF-BA1502-02. The research of Ben Duan was supported in part by NSFC No. 11871133, No. 11671412, the Fundamental Research Funds for the Central Universities Grant DUT18RC(3)000 and the High-level innovative and entrepreneurial talents support plan in Dalian Grant 2017RQ041. The research of Chunjing Xie was supported in part by NSFC Grants 11971307, 11631008, 11422105, and 11511140276, and Young Changjiang Scholar of Ministry of Education in China. The authors would like to thank the hospitalities and support for many visits in Korea Institute for Advanced Study, Pohang University of Science and Technology, and Shanghai Jiao Tong University.
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Appendices
Appendix A. Proof of Lemma 2.8
In this appendix, we prove Lemma 2.8.
Proof of Lemma 2.8
The proof is divided into 3 steps. For a fixed \(n\in \mathbb {N}\), let \((\hat{\mathfrak {f}}_1^{(n)}, \hat{\mathfrak {f}}_2^{(n)})\) be given by (2.68). To simplify notations, \((\hat{\mathfrak {f}}_1^{(n)}, \hat{\mathfrak {f}}_2^{(n)})\) is abbreviated as \((\hat{\mathfrak {f}}_1, \hat{\mathfrak {f}}_2)\) hereafter. Note that \((\hat{\mathfrak {f}}_1, \hat{\mathfrak {f}}_2)\) are smooth in \(\overline{\Omega _L}\). For the rest of proof, we also fix \(m\in \mathbb {N}\), and set
where \(\{\eta _j\}_{j=0}^\infty \) is the orthonormal basis given in (2.73). And, let \((V_m, W_m)\) given in the form (2.74) be the solution to (2.75)–(2.76).
Step 1. \(H^2\) estimate for \(W_m\). It follows from the definition of \(\mathcal {L}_2\) given by (2.12), (2.13) and (2.75) that
By (2.76)–(2.77) and (A.2), \(W_m\) becomes a classical solution to the elliptic boundary value problem:
Applying [12, Theorems 8.8 and 8.12] and the method of reflection to (A.3) yields
for a constant \(C>0\) depending only on \((\gamma , S_0, J_0, \rho _0, E_0, \epsilon _0, L)\). Combining this estimate with (2.80) gives
for a constant \(C>0\) depending only on \((\gamma , S_0, J_0, \rho _0, E_0, \epsilon _0, L)\).
Step 2. \(H^2\) estimate for \(V_m\). The proof for the \(H^2\)-estimate for \(V_m\) is divided into three parts.
Part 1. Energy estimate. The first equation in (2.75) can be written as
We define a linear hyperbolic differential operator \(\mathcal {L}_\mathrm{{hyp}}\) by
and use this definition to rewrite (A.5) as
Denote
One can differentiate (A.6) with respect to \(x_1\), then multiply the resultant equation by \(\vartheta ''_k\) for each \(k=0,1,\ldots ,m\), and add up the results over \(k=0\) to m, finally integrate the summation with respect to \(x_1\) on the interval [0, t] for t varying in the interval [0, L] to get
for \(\Omega _t:=\{\mathrm{x}=(x_1,x_2){:}\,0<x_1<t,\,\, -1<x_2<1\}\). Using (2.78) gives
for \(\Gamma _t=\{(t,x_2)\in \mathbb {R}^2{:}\,-1<x_2<1\}\). By Lemmas 2.1 and 2.3, (2.78), Morrey’s inequality and Cauchy-Schwarz inequality, there exist positive constants \(\lambda \), \(\mu \), and C depending only on \((\gamma , J_0, S_0, \rho _0, E_0, \epsilon _0)\) to satisfy
Substituting this inequality into the left-hand side of (A.7) and applying (A.4) and Cauchy–Schwarz inequality yield
for some constant \(C>0\) depending only on \((\gamma , J_0, S_0, \rho _0, E_0, \epsilon _0)\). Next, one can estimate \(\int _{\Gamma _0} |\nabla _{\mathrm{x}}q_m|^2\,\mathrm{d}x_2\) and \(\int _{\Omega _t}(\partial _{x_2}^2V_m)^2\,\mathrm{d}\mathrm{x}\), separately.
Part 2. Estimate of \(\int _{\Gamma _0} |\nabla _{\mathrm{x}}q_m|^2\,\mathrm{d}x_2\). Differentiating the boundary condition \(\partial _{x_1}V_m=\sum _{j=0}^m \langle g_1, \eta _j\rangle \eta _j\) on \(\Gamma _0\) with respect to \(x_2\) gives
By (2.73), for \(0\leqq j,k\leqq m\), one has
For any \(j\in \mathbb {N}\), since \(-\eta _j''=(j\pi )^2\eta _j\), integration by parts with using \(\eta _j'(\pm 1)=0\) yields
Note that the set \(\{\frac{\eta _j'}{j\pi }\}_{j=1}^\infty \) forms an orthonormal basis in \(L^2([-1,1])\). Therefore, it is concluded from (A.9)–(A.11) that
For each \(k=0, 1,\ldots , m\), multiplying (A.6) by \(\vartheta _k''\), summing up over \(k=0\) to m, and integrating the result over \(\Gamma _0\) with respect to \(x_2\) give
where \(V_m=\partial _{x_1}W_m=0\) on \(\Gamma _0\) because of (2.76). It follows from (2.76), (2.80), (A.4), (A.10), Cauchy-Schwarz inequality and trace inequality, and (A.13) that
where the constant \(C>0\) depends only on \((\gamma , J_0, S_0, \rho _0, E_0, \epsilon _0, L)\). Combining this integral estimate with (A.12) yields
where the constant \(C>0\) depends only on \((\gamma , J_0, S_0, \rho _0, E_0, \epsilon _0, L)\).
Part 3. Estimate of \(\int _{\Omega _t}(\partial _{x_2}^2V_m)^2\,\mathrm{d}\mathrm{x}\). First, (A.6) can be rewritten as
for \(x_1\in (0,L)\), \(k=0,1,\ldots , m\). Since \(\eta _k''=-(k\pi )^2\eta _k\) for each \(k\in \mathbb {Z}^+\), it follows from (A.15) that
which is the same as
Combining Lemmas 2.1 and 2.3, (2.78), Morrey’s inequality and Cauchy–Schwarz inequality, (A.4), and (A.16) yields that
for some constant \(C>0\) depending only on \((\gamma , J_0, S_0, \rho _0, E_0, \epsilon _0,L)\).
For notational convenience, define
and
It follows from (A.8), (A.14), and (A.17) that \( \mathscr {Z}_m\) satisfies a differential inequality
where the constants \(\alpha \) and \(\beta \) depend only on \((\gamma , J_0, S_0, \rho _0, \epsilon _0, L)\). Applying Gronwall’s inequality to (A.19) gives
Finally, the estimate (A.20), together with (A.16), yields
In (A.20)–(A.21), the constants C may vary, but they depend only on \((\gamma , J_0, S_0, \rho _0, \epsilon _0, L)\).
Step 3. Estimate for higher order weak derivatives of \((V_m, W_m)\). In order to complete a priori \(H^4\) estimates of \((V_m, W_m)\) in \(\Omega _L\), one can apply the bootstrap argument. All the details can be given by employing the ideas in Steps 1 and 2, but they are much more lengthy and technical. So, in this step, we only describe main differences in establishing the estimate for higher order weak derivatives of \((V_m, W_m)\) in \(\Omega _L\).
Note that the extension of \(\hat{\mathfrak {f}}_{2,m}+\bar{h}_2\partial _{x_1}V_m\) given by even reflection about \(\Lambda _L\) is \(H^1\) across \(\Lambda _L\) without any additional compatibility condition. Therefore, back to (A.3), applying Lemma 2.4, (A.21) and the method of reflection yield
where the constant \(C>0\) depends only on \((\gamma , S_0, J_0, \rho _0, E_0, \epsilon _0, L)\) and \(\mathscr {E}(\hat{\mathfrak f}_1, \hat{\mathfrak f}_2, g_1)\) is given in (A.18).
For a priori \(H^3\) estimate of \(V_m\), we adapt the argument in Step 2. The main difference is that the compatibility condition
derived from (1.47) is used. For example, it follows from
that there is a differential inequality similar to (A.19). This, together with (A.23), gives
from which one has
Furthermore, it can be directly checked from (2.8), (2.20), (2.67) and (2.68) that
Using this yields
With the aid of (A.21)– (A.23), it follows from lengthy but straightforward computations that
where the constant \(C>0\) depending only on \((\gamma , S_0, J_0, \rho _0, E_0, \epsilon _0, L)\).
Similar to \(H^3\) estimate of \(W_m\) given in (A.22), a priori \(H^4\)-estimate of \(W_m\) can be obtained by applying (A.24), [12, Theorems 8.8 and 8.12] and the method of reflection to (A.3) because the compatibility condition \(\partial _{x_2}(\hat{\mathfrak {f}}_{2,m}+\bar{h}_2\partial _{x_1}V_m)=0\) holds on \(\Lambda _{L}\). Furthermore, it can be directly checked from (2.20), (2.14), (2.67) and (2.68) that one has
Thus it holds that
Therefore, one has
Finally, adapting the argument in Step 2 and using the estimate (A.25) yield
This finishes the proof of Lemma 2.8. \(\square \)
Appendix B. Proof of Lemma 3.5
Proof of Lemma 3.5
For a fixed \(\tilde{Y}\in \mathcal {J}^\mathrm{ent}_{\delta _\mathrm{e}, L}\), denote \({{\varvec{{\mathcal {M}}}}}(\mathrm{x})=(\mathcal {M}_1, \mathcal {M}_2)(\mathrm{x})\) by
for \(\mathbf{M}(\mathrm{x}, \tilde{Y}, \Psi , \nabla \psi , \nabla \phi )\) defined by Definition 3.1(iii). Define a function \(w:\overline{\Omega _L}\rightarrow \mathbb {R}\) by
By adjusting the proof of [4, Lemma 3.3] with using (1.55), (3.40), (3.41) and Lemma 3.3(a), the following properties hold:
-
(i)
\(\displaystyle {\nabla ^{\perp } w={\varvec{\mathcal {M}}}}\) in \(\overline{\Omega _L}\);
-
(ii)
\(\displaystyle {0=w(0,-1)\leqq w(\mathrm{x})\leqq w(0,1)}\) in \(\overline{\Omega _L}\);
-
(iii)
The function \(w_0:=w(0,\cdot ):[-1,1]\rightarrow [0, w(0,1)]\) is strictly increasing, and its inverse \(w_0^{-1}{:}\,[0, w(0,1)] \rightarrow [-1,1]\) is well defined;
-
(iv)
Define a Lagrangian coordinate mapping \(\mathscr {L}_{\tilde{Y}}:\overline{\Omega _L}\rightarrow [-1,1]\) by
$$\begin{aligned} \mathscr {L}_{\tilde{Y}}(\mathrm{x}):=w_0^{-1}\circ w(\mathrm{x}). \end{aligned}$$(B.1)From the definition of \(\mathscr {L}_{\tilde{Y}}\), (3.44) stated in Lemma 3.5(a) can be directly checked. And, the function Y given by
$$\begin{aligned} Y=\left( S_\mathrm{en}-S_0\right) \circ \mathscr {L}_{\tilde{Y}} \end{aligned}$$solves the boundary value problem (3.43).
In order to complete the proof of Lemma 3.5, it suffices to show that there exists a constant \(C_{**}>0\) depending only on \((\gamma , J_0, S_0, \rho _0, E_0, \epsilon _0, L)\) to satisfy
Once (B.2) is verified, then the rest of Lemma 3.5 can be easily proved by direct computations. In particular, the continuity of \(\mathscr {L}_{\tilde{Y}}\) with respect to \(\tilde{Y}\) in \(H^3(\Omega _L)\) stated in Lemma 3.5(a) follows from the smooth dependence of \(\mathbf{M}\) on \((\mathrm{x}, \tilde{Y},\Psi , \nabla \psi , \nabla \phi )\), and the continuous dependence of the fixed point \((\psi , \Psi , \phi )\in \mathcal {J}^\mathrm{pot}_{\delta _\mathrm{p},L}\times \mathcal {J}^\mathrm{vort}_{\delta _\mathrm{v},L}\) of the iteration mapping \(\mathfrak {F}_1^{\tilde{Y}}\) on \(\tilde{Y}\in \mathcal {J}^\mathrm{ent}_{\delta _\mathrm{e},L}\).
The rest of the proof devotes to verify (B.2). Due to the smooth dependence of \(\mathbf{M}\) on \((\mathrm{x}, \tilde{Y}, \Psi , \nabla \psi , \nabla \phi )\), there exists a constant \(C>0\) depending only on \((\gamma , J_0, S_0, \rho _0, E_0, \epsilon _0, L)\) to satisfy
It follows from (1.31), (3.13), (3.15), (3.17), and Definition 3.1(iii) that one has
Note that the fixed point \((\psi , \Psi , \phi )\in \mathcal {J}^\mathrm{pot}_{\delta _\mathrm{p},L}\times \mathcal {J}^\mathrm{vort}_{\delta _\mathrm{v},L}\) of the iteration mapping \(\mathfrak {F}_1^{\tilde{Y}}\) solves the nonlinear boundary value problem (3.11) with boundary conditions (3.13)–(3.15) with Y being replaced by \(\tilde{Y}\). Thus \(\Psi \) can be considered as a solution to the linear boundary value problem
where
with \((\bar{h}_1, \bar{h}_2)\) given by (2.13), and \(f_2\) given by Definition 3.1(v). Using (3.32) and (3.35) yields
for \(\sigma _\mathrm{v}\) given by (3.28). From (3.13), (3.14) and Definition 3.1, it can be directly checked that
Applying the Morrey’s inequality to \(F_2\) to obtain from (B.6) and (B.7) that
In addition, one has \(\partial _{x_2}(E_\mathrm{en}-E_0)(\pm 1)=0\) due to (1.55). Then, by the standard Schauder estimates and the method of reflection, one has
The estimate constants C appeared so far vary, but they all depend only on \((\gamma , J_0, S_0, \rho _0, E_0, \epsilon _0, L)\). It follows from (B.4) and (B.8) that \( \mathbf{M}(\mathrm{x}, \tilde{Y},\Psi , \nabla \psi , \nabla \phi )\cdot \mathbf{e}_1\in C^3(\overline{\Gamma _0})\). Hence straightforward computations together with (3.42), (3.44), (B.3), (B.4), (B.8), the chain rule and the Sobolev inequality show that there exists a constant \(C_{**}>0\) depending only on \((\gamma , J_0, S_0, \rho _0, E_0, \epsilon _0, L)\) to satisfy the estimate (B.2). This finishes the proof of Lemma 3.5. \(\square \)
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Bae, M., Duan, B., Xiao, J. et al. Structural Stability of Supersonic Solutions to the Euler–Poisson System. Arch Rational Mech Anal 239, 679–731 (2021). https://doi.org/10.1007/s00205-020-01583-7
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DOI: https://doi.org/10.1007/s00205-020-01583-7