Abstract
We study a 3D fluid–rigid body interaction problem. The fluid flow is governed by 3D incompressible Navier–Stokes equations, while the motion of the rigid body is described by a system of ordinary differential equations describing conservation of linear and angular momentum. Our aim is to prove that any weak solution satisfying certain regularity conditions is smooth. This is a generalization of the classical result for the 3D incompressible Navier–Stokes equations, which says that a weak solution that additionally satisfy Prodi–Serrin \(L^r-L^s\) condition is smooth. We show that in the case of fluid–rigid body the Prodi–Serrin conditions imply \(W^{2,p}\) and \(W^{1,p}\) regularity for the fluid velocity and fluid pressure, respectively. Moreover, we show that solutions are \(C^{\infty }\) if additionally we assume that the rigid body acceleration is bounded almost anywhere in time variable.
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Notes
Let us mention also the conditional regularity of the type that one component of the velocity field is more regular, see [28].
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Acknowledgements
The authors express their sincere gratitude to the anonymous referee for providing a detailed and insightful review of the manuscript. The suggestions and comments provided by the referee helped us to improve the clarity and quality of the paper.
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Šárka Nečasová as the corresponding author declares on behalf of all authors, that there is no conflict of interest.
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The research of B.M. leading to these results has been supported by Croatian Science Foundation under the project IP-2018-01-3706.
The research of Š.N. leading to these results has received funding from the Czech Sciences Foundation (GAČR), 22-01591S. Moreover, Š. N. has been supported by Praemium Academiae of Š. Nečasová. CAS is supported by RVO:67985840.
The research of A.R. leading to these results has been supported by Croatian Science Foundation under the project IP-2019-04-1140. Moreover, The research of A.R. leading to these results has received funding from the Czech Sciences Foundation (GAČR) 22-01591S, and by Praemium Academiae of Š. Nečasová.
Appendices
Appendix
1.1 Time derivatives-general case
In Sect. 4, we have presented the proof of Proposition 2.2 for case \(l=1\). Here we are going to present the induction step for general \(l\in {{\mathbb {N}}}\). The proof in general case is conceptually the same, but with more complicated expressions in the equations.
Let \(l\ge 1\) and let us assume that
for all \(\varepsilon >0\) and \(1\le p <\infty \). We consider the problem (3.1) with right hand side
where
Subscript \(l-p\) in operators \(\mathcal {L}_{l-p}\), \(\mathcal {M}_{l-p}\), \(\mathcal {N}_{l-p}\) and \(\mathcal {G}_{l-p}\) denotes \((l-p)\)th order time derivative of the coefficients in operators \(\mathcal {L}\), \(\mathcal {M}\), \(\mathcal {N}\) and \(\mathcal {G}\). As for \(l=1\), to show that described problem has a unique solution \((\textbf{U}_l^{*},P_l^{*},\textbf{A}_l^{*},\varvec{\Omega }_l^{*})\) such that
it is sufficient to show that
satisfy
All the terms can be estimated as in Sect. 4, so by Proposition 3.1 there exists a unique strong solution \((\textbf{U}_l^{*},P_l^{*},\textbf{A}_l^{*},\varvec{\Omega }_l^{*})\) of (3.1) with the right hand side (6.1) satisfying (6.4). Again, we have to prove that the obtained solution equals \( \left( t\partial _t^l\textbf{U},t\partial _t^l P,t\frac{\textrm{d} ^l}{\textrm{d} t ^l}\textbf{A},t\frac{\textrm{d} ^l}{\textrm{d} t ^l}\varvec{\Omega }\right) \).
Lemma 6.1
Let \((\textbf{U},P,\textbf{A},\varvec{\Omega })\) be a unique strong solution for (2.4), and \((\textbf{U}_l^{*},P_l^{*},\textbf{A}_l^{*},\varvec{\Omega }_l^{*})\) be a unique strong solution for (3.1) with the right hand side (6.1) satisfying (6.4). Suppose that
hold for some \(l\in {{\mathbb {N}}}\) and for all \(\varepsilon >0\) and all \(1\le p<\infty \). Then
1.2 Proof of Lemma 6.1
Let \((\textbf{U},P,\textbf{A},\varvec{\Omega })\) be a unique strong solution for (2.4) satisfying (6.5) and let \((\textbf{U}_{l}^{*},P_{l}^{*},\textbf{A}_{l}^{*},\varvec{\Omega }_{l}^{*})\) be a unique strong solution for (3.1) with the right hand side (6.1). We want to show (6.6). Since we have already shown that the statement is valid for \(l=1\) in Sect. 4.1, we can suppose that \(l\ge 2\).
We use Galerkin approximations \((\textbf{U}^m,\textbf{A}^m,\varvec{\Omega }^m)\), as in Sect. 4.1, and assume that
for some constant \(M>0\). This assumption comes from the previous step of the induction.
We want to show that
for some constant \(M>0\), which implies that
By (4.16) approximation \((\textbf{U}^m,\textbf{A}^m,\varvec{\Omega }^m)\) satisfies
for \(i=1,\ldots m\). We differentiate the equation in time l times
multiply by \(\frac{\textrm{d} ^l}{\textrm{d} t ^l}c_{im}\) and sum over i form 1 to m to obtain
Then we integrate the equation on \([t_1,t_2]\subset (0,T]\) and, in the same way as in Sect. 4.1.1, estimate
The only difference from Sect. 4.1.1 is in the following estimate
The last inequality follows from the fact that \( \widetilde{\textbf{A}}, \widetilde{\varvec{\Omega }}\in W^{l,4}(\varepsilon ,T)\cap W^{1,\infty }(\varepsilon ,T) \) and embedding \(W^{l-2,4}(t_1,t_2;H^{1}(\Omega _F))\hookrightarrow H^{l-1}(t_1,t_2;H^{1}(\Omega _F))\) for \(l\ge 2\). Therefore, we get
All together, we get
for arbitrary \(\mu >0\), where \(\Vert g_{ik}g^{il}-\delta _{ik}\delta _{il}\Vert _{L^{\infty }(0,T;L^{\infty }(\Omega ))}\) is small for small T. Now, we take sufficiently small T, integrate the inequality on \(t_1\in (\varepsilon ,t_2)\) and by Gronwall’s Lemma we find
where constant \(M>0\) depends on the norms \(\Vert \widetilde{\textbf{U}}\Vert _{H^{l-1}(\varepsilon ,T;H^1(\Omega ))}\), \(\Vert \textbf{U}^m\Vert _{H^{l-1}(0,T;H^1(\Omega ))}\), \(\Vert \widetilde{\textbf{A}}\Vert _{W^{1,\infty }(\varepsilon ,T)}\), \(\Vert \widetilde{\textbf{A}}\Vert _{W^{l,4}(\varepsilon ,T)}\), \(\Vert \widetilde{\varvec{\Omega }}\Vert _{W^{1,\infty }(\varepsilon ,T)}\), \(\Vert \widetilde{\varvec{\Omega }}\Vert _{W^{l,4}(\varepsilon ,T)}\) and T. Finally, in the limit we get that \(\partial _t^l\textbf{U}\in L^2(\varepsilon ,T;H^1(\Omega ))\cap L^{\infty }(\varepsilon ,T;L^2(\Omega ))\), for all \(\varepsilon >0\).
1.2.1 Uniqueness
In previous section, we showed that \(\partial _t^l\textbf{U}\in L^2(\varepsilon ,T;H^1(\Omega ))\cap L^{\infty }(\varepsilon ,T;L^2(\Omega ))\), for all \(\varepsilon >0\). Now we are able to show that \(\textbf{U}_{l}^{*}=t\partial _t^l\textbf{U}\). We know that \((\textbf{U}, P)\) satisfies
for all \(\varvec{\psi }\in V(0)\), and \((\textbf{U}_{l}^{*}, P_{l}^{*},\textbf{A}_{l}^{*},\varvec{\Omega }_{l}^{*})\) satisfies
where
For \((\varvec{\psi },\varvec{\psi }_{\textbf{a}},\varvec{\psi }_{\varvec{\omega }})=h(t)({\varvec{\Psi }}_j,{\varvec{\Psi }}_j^{\textbf{a}},{\varvec{\Psi }}_j^{\varvec{\omega }})\) we have
where
We multiply the above equation by t and subtract from the previous one with
Then, by using (6.7), we obtain
It can be shown that the terms with the pressure cancels, i.e. it holds
and after integrating above equation on (0, t), we get
We let \(m\rightarrow \infty \) and obtain the equation
where
By the linearity and the density, the above equality holds for all \((\varvec{\psi },\varvec{\psi }_{\textbf{a}},\varvec{\psi }_{\varvec{\omega }})\in \mathbb {V}\). Then we can substitute
and get the equality
Now, as in Sect. 4, we can get the estimate
for all \(\mu >0\) and for sufficiently small \(\mu \) we get
Finally, Gronwall’s Lemma implies \(\widehat{\textbf{U}}=0\) which means that \(\textbf{U}_{l}^{*}=t\partial _t^l\textbf{U}\). Then the equations for \(\textbf{U}\) and \(\textbf{U}_l^{*}\) give \(\nabla P_l^{*}=t\nabla \partial _t P\), and since \(\textbf{U}_l^{*}=\textbf{A}_l^{*}+ \varvec{\Omega }_l^{*}\times \textbf{y}\) and \(\partial _t\textbf{U}=\frac{\textrm{d} ^l}{\textrm{d} t ^l}\textbf{A}+ \frac{\textrm{d} ^l}{\textrm{d} t ^l}\varvec{\Omega }\times \textbf{y}\) on \(\overline{S_0}\), it follows that \(\textbf{A}_l^{*}=t\frac{\textrm{d} ^l}{\textrm{d} t ^l}\textbf{A}\) and \(\varvec{\Omega }_l^{*}=t\frac{\textrm{d} ^l}{\textrm{d} t ^l}\varvec{\Omega }\).
Notation
Label | Description | Definition/1st appearance |
---|---|---|
\((\widetilde{\textbf{u}}, \widetilde{p},\widetilde{\varvec{\omega }},\widetilde{\textbf{a}})\) | Solution for the original nonlinear problem (1.6) on physical domain | Section 2.1 |
\((\textbf{u}, p,\varvec{\omega },\textbf{a})\) | Solution for the linear problem (2.1) on the physical domain | Section 2.1 |
\((\widetilde{\textbf{U}}, \widetilde{P},\widetilde{\varvec{\Omega }},\widetilde{\textbf{A}})\) | Solution for the nonlinear problem on the cylindrical domain | |
\((\textbf{U}, P,\varvec{\Omega },\textbf{A})\) | Solution for the linear problem (2.4) on the cylindrical domain | |
\((\varvec{\varphi }, \varvec{\varphi }_{\varvec{\omega }}, \varvec{\varphi }_{\textbf{a}})\) | Test function on the physical domain | Definition 1.1 |
\((\varvec{\psi }, \varvec{\psi }_{\varvec{\omega }}, \varvec{\psi }_{\textbf{a}})\) | Test function on the cylindrical domain | Section 4.1 |
\(\textbf{X}(t,\textbf{y})\) | Changes of variables | Section 2.2 |
\(\textbf{Y}(t,\textbf{x})\) | Changes of variables | Section 2.2 |
\(F(\textbf{U},P)\), \(G(\textbf{A}), H(\varvec{\Omega })\) | Right-hand side of the linear problem (2.4) on the cylindrical domain, | |
\(F(\textbf{U},P) = (\mathcal {L}-\Delta )\textbf{U}-\mathcal {M}\textbf{U}-\mathcal {N}\textbf{U}-(\mathcal {G}-\nabla )P\) | ||
\(\mathcal {L}\textbf{U}\) | The transformed Laplace operator | Equation (2.7) |
\(\mathcal {M}\textbf{U}\) | The transformation of time derivative and gradient | Equation (2.9) |
\(\mathcal {N}\textbf{U}\) | The transformation of the convection term | Equation (2.8) |
\(\mathcal {G}P\) | \(\mathcal {G}P=\nabla \textbf{Y}\nabla \textbf{Y}^T\nabla P\), the transformation of the gradient of the pressure | Equation (2.10) |
\(\mathcal {F}\textbf{U}\) | \(\mathcal {F}\textbf{U}= \mathcal {L}\textbf{U}-\mathcal {M}\textbf{U}-\mathcal {N}\textbf{U}-\mathcal {G}P\) | Equation (4.12) |
\(({\textbf{U}}^{*}, {P}^{*},{\varvec{\Omega }}^{*},{\textbf{A}}^{*})\) | The fixed point, the solution for the transformed problem | Section 3 |
\((\widehat{\textbf{U}}, \widehat{P},\widehat{\varvec{\Omega }},\widehat{\textbf{A}})\) | The fixed point, functions on the right-hand side | Section 3 |
\(F^{*}\), \(G^{*}\), \(H^{*}\) | The right-hand side for the Stokes problem | Section 3 |
\(X_{p,q}^T\), \(Y_{p,q}^T\) | \(X_{p,q}^T :=W^{1,p}(0,T;L^q(\Omega _{F}))\cap L^p(0,T;W^{2,q}(\Omega _F))\) \(Y_{p,q}^T := L^p(0,T; {W}^{1,q}(\Omega _{F}))\) | |
\(F_l(\textbf{U},P)\) | “\(F_l(\textbf{U},P)=\partial _{t}^l(F({\textbf{U}},{P}))-F(\partial _{t}^l{\textbf{U}},\partial _{t}^l{P})\)” | |
\(G_l(\textbf{A})\) | “\(G_l(\textbf{A})=\frac{d^l}{{dt}^l}(G(\textbf{A}))-G\left( \frac{d^l}{{dt}^l}\textbf{A}\right) \)” | |
\(H_l(\varvec{\Omega })\) | “\(H_l(\varvec{\Omega })=\frac{d^l}{{dt}^l}(H(\varvec{\Omega }))-H\left( \frac{d^l}{{dt}^l}\varvec{\Omega }\right) \)” | |
\(\mathcal {G}_l(P)\) | The operator obtained by taking lth order time derivative of the coefficients in operator \(\mathcal {G}\), i.e. \(\mathcal {G}_l(P)=\partial _t^l(\nabla \textbf{Y}\nabla \textbf{Y}^T)\nabla P\) | |
\(\mathcal {F}_l(\textbf{U})\) | \(\mathcal {F}_l(\textbf{U}) = \mathcal {L}_l(\textbf{U})-\mathcal {M}_l(\textbf{U})-\mathcal {N}_l(\textbf{U})-\mathcal {G}_l(P)\), \(\mathcal {L}_l, \mathcal {M}_l, \mathcal {N}_l\) are operators obtained by taking lth order time derivative of the coefficients in operators \(\mathcal {L}, \mathcal {M}, \mathcal {N}\) | |
\(\mathbb {G}\) | \(\mathbb {G}=\nabla \textbf{X}^T\nabla \textbf{X}\) | Section 4.1 |
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Muha, B., Nečasová, Š. & Radošević, A. On the regularity of weak solutions to the fluid–rigid body interaction problem. Math. Ann. (2023). https://doi.org/10.1007/s00208-023-02664-0
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DOI: https://doi.org/10.1007/s00208-023-02664-0