Abstract
In this paper we introduce a numerical scheme for fluid–structure interaction problems in two or three space dimensions. A flexible elastic plate is interacting with a viscous, compressible barotropic fluid. Hence the physical domain of definition (the domain of Eulerian coordinates) is changing in time. We introduce a fully discrete scheme that is stable, satisfies geometric conservation, mass conservation and the positivity of the density. We also prove that the scheme is consistent with the definition of continuous weak solutions.
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Notes
Throughout the paper we make use of the standard notation of Bochner, Sobolev and Lebesgue spaces, see for instance [26] for more details.
Such an approximation can be made precise by taking a cut-off function. We take \(\phi _\epsilon \in C^\infty (-\infty ,\infty )\), such that the s-th derivative \(\phi ^{(s)}_\epsilon (x)=0\) for all \(s\in \mathbb {N}\) and \(x\le 0\) and \(\phi _\epsilon (x)\equiv 1\) for all \(x\in [\epsilon ,\infty )\) and \(0\le \phi '_\epsilon \le \frac{2}{\epsilon }\) and \( | \phi ''_\epsilon |\le \frac{8}{\epsilon ^2}\). Moreover, we denote \((b)_\epsilon \) as the standard convolution for a function \(b:C^\alpha ([0,T])\). Recall that since \(\eta \in C^\alpha \) uniformly we find in particular \(\eta - \epsilon ^\alpha \le (\eta )_\epsilon \le \eta + \epsilon ^\alpha \). Then (for a fixed t) we define \( \Psi _{\epsilon }(t,r, x_d):= (1-\phi _\epsilon ({ x_d-H-(\eta )_\epsilon (t)+2\epsilon ^\alpha }))\Psi (t,r, x_d)+\phi _\epsilon ({ x_d-H-(\eta )_\epsilon (t)+2\epsilon ^\alpha })\psi (t,r), \) which satisfies (3.10).
For the consistency actually we will assume that \(h\sim \tau \).
Note that due to (4.7) the assumption \(\left\Vert \Pi _p \eta _{h,\tau }-\eta \right\Vert _\infty <\epsilon \) follows from \(\left\Vert \eta _{h,\tau }-\eta \right\Vert _\infty <\epsilon \), provided h is sufficiently small.
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Both authors thank the support of the primus research programme of Charles University, PRIMUS/19/SCI/01 and the program GJ19-11707Y of the Czech national grant agency (GAČR). S. S also thanks the University Centre UNCE/SCI/023 from Charles University. The institute of Mathematics of the Czech Academy of Sciences is supported by RVO: 67985840.
A: Appendix
A: Appendix
1.1 A.1 Proof of Theorem 3: existence of a numerical solution
We aim to prove Theorem 3 for the existence of a numerical solution. Before that let us first introduce an abstract theorem, see [30, Theorem A.1].
Theorem 6
([30, Theorem A.1]) Let M and N be positive integers. Let \( C_2>\epsilon >0\) and \(C_1>0\) be real numbers. Let V and W be defined as follows:
where the notation \(x > c\) means that each component of x is greater than c, and \(\Vert \cdot \Vert \) is a norm defined over \(R ^N\). Let F be a continuous function from \(V \times [0,1]\) to \(R ^M \times R ^N\) satisfying:
-
1.
\(\forall \, \zeta \in [0,1] \), if \( v \in V \) is such that \( F(v,\zeta )=0 \) then \( v \in W \);
-
2.
The equation \(F (v, 0)=0\) is a linear system on v and has a solution in W.
Then there exists at least a solution \( v \in W\) such that \(F(v,1) = 0\).
Now we are ready to show Theorem 3.
Proof
Let us denote , and define
It is obvious that the degrees of freedom of the spaces \(Q_{h,\tau }\) and \(\mathbb {Q}\) are finite. Indeed, the space \(Q_{h,\tau }\) can be identified by the set of values \(\varrho _K\) for all \(K \in \mathcal {T}_{h,\tau }^{k}\), therefore \(Q_{h,\tau }\subset \mathbb {R}^M\), where M is the total number of elements of \(\mathcal {T}_{h,\tau }^{k}\). Analogously, \(\mathbb {Q}\subset \mathbb {R}^N\), where N is the sum of d times degrees of freedom of \(\mathcal {E}^k\) and the degrees of freedom of \(\Sigma \). Let us consider the mapping
where \(( \varrho ^\star , U^\star ) \in Q_{h,\tau }\times \mathbb {Q}\) is such that
where \( {\varvec{\Psi }}_{h,\tau }= ({\varvec{\Psi }}_{h,\tau }, {\psi }_{h,\tau }), \quad \eta _{h,\tau }^k = \eta _{h,\tau }^{k-1} + \tau z_{h,\tau }^k, \quad \mathbf {u}_{h,\tau }^k|_{\Sigma } = z_{h,\tau }^k \mathbf {e}_d , \quad \mathcal {F}_k^{k-1}= \left( H + \eta _{h,\tau }^{k-1}\right) /\left( H + \eta _{h,\tau }^{k}\right) . \)
It is easy to check that F is continuous. Indeed, it is a one to one mapping, since the values of \(\varrho ^\star \) and \(U^\star \) can be determined by setting \({\varphi }_{h,\tau }= 1_{K}\) in (A.1a), and \((\Phi _\tau )_i=1_{D_\sigma }, (\Phi _\tau )_j=0\) for \(j\ne i\) in (A.1b).
Let \((\varrho _{h,\tau }^k,U_{h,\tau }^k ) \in Q_h\times \mathbb {Q}\) and \(\zeta \in [0,1]\) such that \(F(\varrho _{h,\tau }^k,U_{h,\tau }^k , \zeta )=(0,0)\) (in particular \(\varrho _{h,\tau }^k>0\)). Then for any \(\big ({\varphi }_{h,\tau }, {\varvec{\Phi }}_{h,\tau }= ({\varvec{\Psi }}_{h,\tau }, {\psi }_{h,\tau }) \big )\in Q_h\times \mathbb {Q}\)
Taking \({\varphi }_{h,\tau }=1\) as a test function in (A.2a) we obtain
which indicates the boundedness of \(\varrho _{h,\tau }^k\) in the \(L^1\) norm, and thus in all norms as the problem is of finite dimension. Following the same argument as Lemma 3 we know that \(\varrho _{h,\tau }^k \ge 0\) provided \(\varrho _{h,\tau }^{k-1} \ge 0\).
Taking \({\varvec{\Phi }}_{h,\tau }=(\mathbf {u}_{h,\tau }^k, z_{h,\tau }^k)\) as the test function in (A.2b) and follow the proof of Theorem (1) gives
where \(C_1\) depends on the data of the problem.
Further, let \(K\in \mathcal {T}_{h,\tau }^{k}\) be such that \(\varrho _K^k\) is the smallest, i.e., \( \varrho _K^k \le \varrho _L^k\) for all \(L\in \mathcal {T}_{h,\tau }^{k}\). We denote \(K'= \mathcal {A}_{h,\tau }^{k-1}\circ (\mathcal {A}_{h,\tau }^{k})^{-1}(K)\). Then a straightforward computation gives
Thus \( \varrho _{h,\tau }^k \ge \varrho _K^k \ge \frac{ | K' |}{ | K |} \frac{\varrho ^{k-1}_{K'} }{1 + \tau \zeta | (\mathrm{div}\mathbf {v}_{h,\tau }^k)_K | } >0. \) Consequently, by virtue of (A.4) \( \varrho _{h,\tau }^k > \epsilon \), where \(\epsilon \) depends only on the data of the problem. Further, we get from (A.3) that \( \varrho _{h,\tau }^k \le \frac{ \int _{\Omega _{h,\tau }^{k-1}} \varrho _{h,\tau }^{k-1} \,\mathrm{d} {x}}{\min _{K\in \mathcal {T}_{h,\tau }^{k}} |K|}\), which indicates the existence of \(C_2>0\) such that \(\varrho _{h,\tau }^k <C_2\). Therefore, Hypothesis 1 of Theorem 6 is satisfied.
Next, we proceed to show that Hypothesis 2 of Theorem 6 is satisfied. Let \(\zeta =0\) then the system \(F(\varrho _{h,\tau }^k,U_{h,\tau }^k )=0\) reads
To solve the above system (A.5), we further reformulate it on the reference domain according to (2.10)
where \(\mathcal {F}^{k-1}= 1+ \eta _{h,\tau }^{k-1}/H\) is determined by \(\eta _{h,\tau }^{k-1}\). Realizing that (A.6b) is a linear system with a matrix being block-wise symmetric positive definite, we know that there exists exactly one solution \(\widehat{U}_{h,\tau }^k =(\widehat{\mathbf {u}}_{h,\tau }^k, z_{h,\tau }^k)\). Then using the fact \(\eta _{h,\tau }^k = \eta _{h,\tau }^{k-1} + \tau z_{h,\tau }^k\) we get \(\eta _{h,\tau }^k\) and \(\mathcal {A}_{h,\tau }^{k}\). Further, it is straightforward that \(\mathbf {u}_{h,\tau }^k=\widehat{\mathbf {u}}_{h,\tau }^k\circ \mathcal {A}_{h,\tau }^{k}(\widehat{x})\). Finally, substituting \(\eta _{h,\tau }^k\) into (A.6a) we obtain the solution for \(\varrho _{h,\tau }^k\). Obviously, \(\varrho _{h,\tau }^k>0\) as long as no self touching. Thus the solution \((\varrho _{h,\tau }^k,U_{h,\tau }^k )\) belongs to W, which implies Hypothesis 2 of Theorem 6.
We have shown that both hypotheses of Theorem 6 hold. Applying Theorem 6 finishes the proof. \(\square \)
1.2 A.2 Proof of Lemma 8: renormalization
Here we show the validity of the discrete renormalized equation stated in Lemma 8 for the discrete continuity problem (4.17a).
Proof
Firstly, we set \({\varphi }_{h,\tau }=B'(\varrho )\) in (4.17a) and obtain
Next, recalling (3.4), we know there exist \(\xi \in \mathrm{co}\{ \varrho _{h,\tau }^{k-1}\circ {X}_k^{k-1} , \varrho _{h,\tau }^{k} \}\) such that
where
Further, by recalling the definition of the upwind flux (4.10), and using again the Taylor expansion, we reformulate the convective term as
where
Moreover, using the facts
we obtain
Consequently, we derive
Finally, collecting the above terms and seeing \(\mathbf {v}_{h,\tau }^k + \mathbf {w}_{h,\tau }^k= \mathbf {u}_{h,\tau }^k\), we complete the proof, i.e.,
\(\square \)
1.3 A.3 Proof of Theorem 4: energy stability
Here we prove the energy stability stated in Theorem 4 for the discrete scheme (4.17).
Proof
Setting \({\varphi }_{h,\tau }= - \frac{\left| \Pi _\mathcal {T}[ \mathbf {u}_{h,\tau }^{k}]\right| ^2}{2}\) in (4.17a) and \(({\varvec{\Psi }}_{h,\tau },{\psi }_{h,\tau }) = (\mathbf {u}_{h,\tau }^{k}, z_{h,\tau }^{k})\) in (4.17b) we get \(\sum _{i=1}^2 I_i=0\) and \(\sum _{i=3}^{9} I_i=0\) respectively, where
Now we proceed with the summation of all the \(I_i\) terms for \(i=1,\ldots ,9\).
Term \((I_1+I_3+I_8)+(I_6+I_7)+I_9\). Firstly, analogously as in the proof of Theorem 1 we have
Term \(I_2+I_4\). For the convective terms, we have using the fact that \(\Pi _\mathcal {T}[\mathbf {u}_{h,\tau }]\) and \(\mathrm{div}^{\mathrm{up}}_{h,\tau }\left( \varrho _{h,\tau }^k \Pi _\mathcal {T}[ \mathbf {u}]^{k}_h , \mathbf {v}_{h,\tau }^{k} \right) \) are constant on each \(K\in \mathcal {T}_{h,\tau }\) and the upwind divergence
Pressure term \(I_{5} \). Recalling the discrete internal energy equation (4.20), we can rewrite the pressure term as
where \(D_1\) and \(D_2\) are given in (4.21). Collecting all the above terms, we get
We finish the proof by summing up the above equation for \(k=1,\ldots ,N\) and multiplying with \(\tau \). \(\square \)
1.4 A.4 Proof of Lemma 10: useful estimates
Proof
Item 1 has been reported by [23, Lemma 3.5]. Item 2 has been reported by [31, Lemma 4.3]. Item 4 has been reported by [25, Chaper 9, Lemma 7]. We are only left with the proof of Item 3. We start the proof with the a-priori estimates on \(\mathbf {v}_{h,\tau }\)
where we used (4.14) for \(\mathbf {u}_{h,\tau }\) and (4.28) for \(\mathbf {w}_{h,\tau }\). On one hand, for \(\gamma \ge 2\), we employ (4.30) to get
On the other hand, it is easy to check for \(\gamma \in (1,2)\) that \(\mathcal {H}''(r)=a r^{\gamma -2} \ge a\) if \(r\le 1\) and \(r \mathcal {H}''(r)= ar^{\gamma -1} \ge a\) if \(r\ge 1\). Therefore
Applying these inequalities together with Hölder’s inequality, and the estimate (4.22) we derive (by choosing \(\varrho _{h,\tau }^\dagger \) conveniently and (4.13)) that
Then, for \(\gamma \in [6/5, 2)\) we have \(I_1 {\mathop {\sim }\limits ^{<}}h^{-\frac{1}{2}}\tau ^{-\frac{1}{4}}\). Concerning \(\gamma \in (1,6/5)\) we deduce by inverse estimate (4.14) that
which completes the proof of the first estimate (4.31a).
Similarly, we prove the second estimate (4.31b) in two steps. First for \(\gamma \ge 2\) we may derive it due to Hölder’s inequality, trace theorem, and the inverse estimate (4.14) that
Next, we proceed to show the second estimates for \(\gamma \in (1, 2)\).
where we have used the algebraic inequality for \(\gamma \in (1,2)\) that . On the other hand, if \(1<\gamma < \frac{4}{3}\) we complete the proof by the inverse estimates (4.14) and find
which finishes the estimate. \(\square \)
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Schwarzacher, S., She, B. On numerical approximations to fluid–structure interactions involving compressible fluids. Numer. Math. 151, 219–278 (2022). https://doi.org/10.1007/s00211-022-01275-2
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DOI: https://doi.org/10.1007/s00211-022-01275-2