Abstract
We study a coupled fluid–structure system involving boundary conditions on the pressure. The fluid is described by the incompressible Navier–Stokes equations in a 2D rectangular-type domain where the upper part of the domain is described by a damped Euler–Bernoulli beam equation. Existence and uniqueness of local strong solutions without assumptions of smallness on the initial data are proved.
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References
R. A. Adams. Sobolev spaces. Academic Press [A subsidiary of Harcourt Brace Jovanovich, Publishers], New York-London, 1975. Pure and Applied Mathematics, Vol. 65.
S. Agmon, A. Douglis, and L. Nirenberg. Estimates near the boundary for solutions of elliptic partial differential equations satisfying general boundary conditions. I. Comm. Pure Appl. Math., 12:623–727, 1959.
S. Agmon, A. Douglis, and L. Nirenberg. Estimates near the boundary for solutions of elliptic partial differential equations satisfying general boundary conditions. II. Comm. Pure Appl. Math., 17:35–92, 1964.
G. Avalos and R. Triggiani. The coupled PDE system arising in fluid/structure interaction. I. Explicit semigroup generator and its spectral properties. In Fluids and waves, volume 440 of Contemp. Math., pages 15–54. Amer. Math. Soc., Providence, RI, 2007.
G. Avalos and R. Triggiani. Mathematical analysis of PDE systems which govern fluid-structure interactive phenomena. Bol. Soc. Parana. Mat. (3), 25(1-2):17–36, 2007.
H. Beirão da Veiga. On the existence of strong solutions to a coupled fluid-structure evolution problem. J. Math. Fluid Mech., 6(1):21–52, 2004.
A. Bensoussan, G. Da Prato, M. C. Delfour, and S. K. Mitter. Representation and control of infinite dimensional systems. Systems & Control: Foundations & Applications. Birkhäuser Boston, Inc., Boston, MA, second edition, 2007.
J. M. Bernard. Non-standard Stokes and Navier-Stokes problems: existence and regularity in stationary case. Math. Methods Appl. Sci., 25(8):627–661, 2002.
J. M. Bernard. Time-dependent Stokes and Navier-Stokes problems with boundary conditions involving pressure, existence and regularity. Nonlinear Anal. Real World Appl., 4(5):805–839, 2003.
F. Boyer and P. Fabrie. Mathematical tools for the study of the incompressible Navier-Stokes equations and related models, volume 183 of Applied Mathematical Sciences. Springer, New York, 2013.
S. P. Chen and R. Triggiani. Proof of extensions of two conjectures on structural damping for elastic systems. Pacific J. Math., 136(1):15–55, 1989.
C. Conca, F. Murat, and O. Pironneau. The Stokes and Navier-Stokes equations with boundary conditions involving the pressure. Japan. J. Math. (N.S.), 20(2):279–318, 1994.
V. Girault and P.-A. Raviart. Finite element methods for Navier-Stokes equations, volume 5 of Springer Series in Computational Mathematics. Springer-Verlag, Berlin, 1986. Theory and algorithms.
C. Grandmont and M. Hillairet. Existence of global strong solutions to a beam-fluid interaction system. Arch. Ration. Mech. Anal., 220(3):1283–1333, 2016.
C. Grandmont, M. Hillairet, and J. Lequeurre. Existence of local strong solutions to fluid-beam and fluid-rod interaction systems. Ann. Inst. H. Poincaré Anal. Non Linéaire, 36(4):1105–1149, 2019.
J. Lequeurre. Existence of strong solutions to a fluid-structure system. SIAM J. Math. Anal., 43(1):389–410, 2011.
J.-L. Lions and E. Magenes. Non-homogeneous boundary value problems and applications. Vol. I. Springer-Verlag, New York-Heidelberg, 1972. Translated from the French by P. Kenneth, Die Grundlehren der mathematischen Wissenschaften, Band 181.
J.-L. Lions and E. Magenes. Non-homogeneous boundary value problems and applications. Vol. II. Springer-Verlag, New York-Heidelberg, 1972. Translated from the French by P. Kenneth, Die Grundlehren der mathematischen Wissenschaften, Band 182.
B. Muha and S. Canić. Existence of a weak solution to a nonlinear fluid-structure interaction problem modeling the flow of an incompressible, viscous fluid in a cylinder with deformable walls. Arch. Ration. Mech. Anal., 207(3):919–968, 2013.
A. Pazy. Semi-groups of linear operators and applications to partial differential equations. Department of Mathematics, University of Maryland, College Park, Md., 1974. Department of Mathematics, University of Maryland, Lecture Note, No. 10.
J.-P. Raymond. Stokes and Navier-Stokes equations with nonhomogeneous boundary conditions. Ann. Inst. H. Poincaré Anal. Non Linéaire, 24(6):921–951, 2007.
J.-P. Raymond. Feedback stabilization of a fluid-structure model. SIAM J. Control Optim., 48(8):5398–5443, 2010.
H. Sohr. The Navier-Stokes equations. Modern Birkhäuser Classics. Birkhäuser/Springer Basel AG, Basel, 2001. An elementary functional analytic approach.
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Appendix
Appendix
1.1 Steady Stokes equations
Consider the steady Stokes equations
with \(\mathbf{f }\in \mathbf{L }^{2}(\Omega _{0})\), \(\mathbf{g }=(0,g)^{T}\in {\mathcal {H}}^{3/2}_{00}(\Gamma _{0})\) and \(h\in H^{1/2}(\Gamma _{i,o})\). We prove in Theorem 5.4 the existence and uniqueness of a pair \((\mathbf{u },p)\in \mathbf{H }^{2}(\Omega _{0})\times H^{1}(\Omega _{0})\) solution to (5.1). An existence and uniqueness result for (5.1) with weaker data is given in Theorem 5.7. The non-homogeneous boundary condition on the pressure is handled directly with a lifting operator \({\mathcal {R}}\in {\mathcal {L}}(H^{1/2}(\Gamma _{i,o}),H^{1}(\Omega _{0}))\). For the non-homogeneous Dirichlet boundary condition, we use the following theorem.
Theorem 5.1
For all \(\mathbf{g }=(0,g)^{T}\in {\mathcal {H}}^{3/2}_{00}(\Gamma _{0})\), the system
admits a solution \(\mathbf{w }\in \mathbf{H }^{2}(\Omega _{0})\) satisfying the estimate
Proof
We look for \(\mathbf{w }\) under the form \(\mathbf{w }=(-\partial _{2}\phi ,\partial _{1}\phi )^{T}\), which ensures the property \(\text {div }\mathbf{w }=0\). The boundary conditions on \(\mathbf{w }\) imply the following conditions on \(\phi \)
Let \(\eta ^{0}_{e}\) be an \(H^{3}({\mathbb {R}})\) extension of \(\eta ^{0}\). We consider the change of variables
Let \({\widehat{v}}\) be a function in \(H^{3}({\mathbb {R}}^{2})\). Thanks to the \(H^{3}\)-regularity of \(\eta ^{0}_{e}\), the function \({\widehat{v}}\circ \psi ^{\pm }\) is still in \(H^{3}({\mathbb {R}}^{2})\). We search for \(\phi \) solution to (5.3) under the form \(\phi ={\widehat{\phi }}\circ \psi ^{-}\) with \({\widehat{\phi }}\in H^{3}((0,L)\times (-\infty ,1))\) satisfying
with \({\widehat{g}}=g\circ \psi ^{+}\) and
for a fixed \(\alpha \in (0,1)\). This condition is used to ensure that the function \(\phi ={\widehat{\phi }}\circ \psi ^{-}\) is equal to zero near \(\Gamma _{b}\), in order to fulfil the boundary conditions \(\partial _{1}\phi =\partial _{2}\phi =0\) on \(\Gamma _{b}\). To build \({\widehat{\phi }}\), we first search for \({\widehat{\phi }}_{o}\) such that
The boundary conditions on \(\Gamma _{s}\) are handled directly thanks to a lifting and a symmetry argument is used to obtain the homogeneous Neumann boundary condition on \(\Gamma _{o}\). We set
Denote by \({\widehat{g}}_{s}\) the odd extension of \({\widehat{g}}\) on \(\Gamma _{s,s}=(0,2L)\times \{1\}\). As \({\widehat{g}}\in H^{3/2}_{00}(\Gamma _{s})\), the function \({\widehat{g}}_{s}\) belongs to \(H^{3/2}(\Gamma _{s,s})\). Indeed, odd and even symmetries preserve the \(H^1\)-regularity (resp. \(H^2\)-regularity) for functions in \(H^{1}_{0}(\Gamma _{0})\) (resp. in \(H^{2}_{0}(\Gamma _{0})\)); thus, by interpolation, the \(H^{3/2}\)-regularity is also preserved for functions in \(H^{3/2}_{00}(\Gamma _{0})=[H^{1}_{0}(\Gamma _{0}),H^{2}_{0}(\Gamma _{0})]_{1/2}\).
As \(\partial _{1}G^{*}(\cdot ,1)={\widehat{g}}_{s}(\cdot )\), we have \(G^{*}\in H^{5/2}(\Gamma _{s,s})\). We still denote by \(G^{*}\) a regular extension of \(G^{*}\) on \({\mathbb {R}}\times \{1\}\). The lifting results in [18] in the case of the half-plan give a function \({\widehat{\phi }}_{1}\in H^{3}({\mathbb {R}}\times (-\infty ,1))\) such that \({\widehat{\phi }}_{1}=G^{*}\) and \(\frac{\partial {\widehat{\phi }}_{1}}{\partial \mathbf{n }}=0\) on \({\mathbb {R}}\times \{1\}\). We then use cut-off functions to ensure that \({\widehat{\phi }}_{1}=0\) on \((0,2L)\times (-\infty ,1-\delta )\).
Introduce the symmetric function \({\widehat{\phi }}_{2}\) to \({\widehat{\phi }}\) with respect to the axis \(x=L\) defined by \({\widehat{\phi }}_{2}(x,y)={\widehat{\phi }}_{2}(2L-x,y)\) for \((x,y)\in (0,2L)\times (-\infty ,1)\). As the Dirichlet boundary condition \(G^{*}\) is symmetric, \({\widehat{\phi }}_{2}\) satisfies the same boundary conditions as \({\widehat{\phi }}_{1}\) on \(\Gamma _{s,s}\). We finally set \({\widehat{\phi }}_{o}=\frac{{\widehat{\phi }}_{1}+{\widehat{\phi }}_{1,s}}{2}\). The function \({\widehat{\phi }}_{o}\) belongs to \(H^{3}((0,2L)\times (-\infty ,1))\) and admits \(x=L\) as an axis of symmetry. Hence, we have \(\frac{\partial {\widehat{\phi }}_{o}}{\partial \mathbf{n }}=0\) on \(\Gamma _{o}\) and the restriction on \((0,L)\times (-\infty ,1)\) is a solution to (5.6).
Using the same tools, we obtain a function \({\widehat{\phi }}_{i}\in H^{3}((0,L)\times (-\infty ,1))\) such that
Then, we combine \({\widehat{\phi }}_{o}\) and \({\widehat{\phi }}_{i}\). Let \(\alpha \) be a function defined on [0, L] such that \(\alpha =1\) near \(\Gamma _{i}\), \(\alpha =0\) near \(\Gamma _{o}\) and \(\alpha \in {\mathcal {C}}^{\infty }([0,L])\). The function \({\widehat{\phi }}\) defined by
is a solution to (5.4). Finally, the restriction to \(\Omega _{0}\) of the function \(\phi ={\widehat{\phi }}\circ \psi ^{-}\) is a solution to (5.3). Indeed,
and \(\mathbf{w }=(-\partial _2 \phi ,\partial _1 \phi )^{T}\) is a solution of (5.2). We have \(\mathbf{w }\in \mathbf{H }^{2}(\Omega _{0})\) and the estimate follows from the continuity of the lifting operator in [18]. \(\square \)
Let \(\mathbf{w }\in \mathbf{H }^{2}(\Omega _{0})\) be the lifting of \(\mathbf{g }\) given by Theorem 5.1 and \(H={\mathcal {R}}(h)\). By setting \((\mathbf{v },q)=(\mathbf{u },p)-(\mathbf{w },H)\), the Stokes system (5.1) is equivalent to
with \(\overline{\mathbf{f }}=\mathbf{f }+\nu \Delta \mathbf{w }-\nabla H\). Using Green formula, one can derive the following variational formulation for (5.8).
Theorem 5.2
Let \((\mathbf{v },q)\in \mathbf{H }^{2}(\Omega _{0})\times H^{1}(\Omega _{0})\) be a solution to (5.8). Then, \(\mathbf{v }\) satisfies the variational formulation:
Find \(\mathbf{v }\in V\) such that \(\quad \displaystyle \nu {\int }_{\Omega _{0}}\nabla \mathbf{v }:\nabla \varvec{\varphi }={\int }_{\Omega _{0}}\overline{\mathbf{f }}\cdot \varvec{\varphi }\text { for all }\varvec{\varphi }\in V.\quad (\star )\)
Theorem 5.3
The variational formulation \((\star )\) admits a unique solution \(\mathbf{v }\in V\). Moreover, there exists a pressure \({\mathcal {Q}}\in L^{2}(\Omega _{0})\), unique up to an additive constant, such that \(\displaystyle -\nu \Delta \mathbf{v }+\nabla {\mathcal {Q}} = \overline{\mathbf{f }}\,\) in \(\mathbf{H }^{-1}\).
The pressure \({\mathcal {Q}}\) is mentioned as a pressure associated with \(\mathbf{v }\).
Proof
As the only constant in V is the null function, we can use a Poincaré inequality to prove that the bilinear form
is coercive on V. Hence, the Lax–Milgram lemma gives us the existence of a unique solution \(\mathbf{v }\in V\) to the variational formulation \((\star )\). For the pressure, we use the equality
and [10, Chap 4, Theorem 2.3] to prove the existence of \({\mathcal {Q}}\in L^{2}(\Omega _{0})\), unique up to an additive constant and such that \(-\nu \Delta \mathbf{v }+\nabla {\mathcal {Q}} = \overline{\mathbf{f }}\) in \(\mathbf{H }^{-1}\). \(\square \)
We now state the main theorem of this section.
Theorem 5.4
For all \((\mathbf{f },\mathbf{g },h)\in \mathbf{L }^{2}(\Omega _{0})\times {\mathcal {H}}^{3/2}_{00}(\Gamma _0)\times H^{1/2}(\Gamma _{i,o})\), equation (5.1) admits a unique solution \((\mathbf{u },p)\in \mathbf{H }^{2}(\Omega _{0})\times H^{1}(\Omega _{0})\). This solution satisfies the estimate
Proof
Let us work directly on the homogeneous system (5.8). We prove the existence of a unique pair \((\mathbf{v },q)\in \mathbf{H }^{2}(\Omega _{0})\times H^{1}(\Omega _{0})\) solution to this system. According to Theorems 5.2 and 5.3, \(\mathbf{v }\) has to solve the variational formulation \((\star )\). Hence, we start with the solution of the variational formulation \((\star )\) and we prove that it is the solution to (5.8). The plan is the following:
-
Step 1: We extend the variational formulation \((\star )\) on a larger domain \(\Omega _{0,e}\) with a solution denoted by \(\mathbf{v }_{e}\).
-
Step 2: We prove that the solution \(\mathbf{v }_{e}\) to this new variational formulation is in \(\mathbf{H }^{2}\) in a neighbourhood of \(\Gamma _{i}\).
-
Step 3: We prove that the restriction of \(\mathbf{v }_{e}\) to the initial domain \(\Omega _{0}\) is the solution \(\mathbf{v }\) to \((\star )\), which implies that \(\mathbf{v }\) is \(\mathbf{H }^{2}\) in a neighbourhood of \(\Gamma _{i}\), and finally that \(\mathbf{v }\in \mathbf{H }^{2}(\Omega _{0})\).
-
Step 4: We prove that all the pressures associated with \(\mathbf{v }\) are in \(H^{1}(\Omega _{0})\) and are constant on \(\Gamma _{i,o}\).
-
Step 5: We conclude by taking the pressure satisfying \(q=0\) on \(\Gamma _{i,o}\), so that the pair \((\mathbf{v },q)\) is the unique solution to (5.8).
Step 1: Let \(\eta ^{0}_{e}\) be the function defined by
We recall that \(\eta ^{0}\) is in \(H^{3}(0,L)\) and that \(\eta ^{0}(0)=\eta ^{0}_{x}(0)=0\). Due to the even symmetry, we have \(\eta ^{0}_{e}(0^{-})=\eta ^{0}_{e}(0^{+})=0\), \(\eta ^{0}_{e,x}(0^{-})=\eta ^{0}_{e,x}(0^{+})=0\), \(\eta ^{0}_{e,xx}(0^{-})=\eta ^{0}_{e,xx}(0^{+})\) and thus we obtain \(\eta ^{0}_{e}\in H^{3}(-L,L)\) and the curve \(\Gamma _{0,e}=\{(x,y)\in {\mathbb {R}}^{2}\mid x\in (-L,L),\,y=1+\eta ^{0}_{e}(x)\}\) is \({\mathcal {C}}^{2}\). We set \(\Omega _{0,e}=\{(x,y)\in {\mathbb {R}}^{2}\mid x\in (-L,L),\,0<y<1+\eta ^{0}_{e}(x)\}\).
Let \(\mathbf{v }_e\) be the solution to
where
and \(\overline{\mathbf{f }}_e\) is the function defined by
with \(\Omega _{0,s}=\{(x,y)\in {\mathbb {R}}^{2}\mid x\in (-L,0),\,0<y<1+\eta ^{0}_{e}(x)\}\) .
Step 2: We use cut-off functions to prove the \(\mathbf{H }^{2}\) regularity result near \(\Gamma _{i}\). Let \(\varphi \) be a function in \({\mathcal {C}}^{\infty }_{0}({\mathbb {R}}^{2})\) such that \(\varphi =1\) on \(\Omega _{\varphi ,1}\) and \(\text {support}(\varphi )\subset \Omega _{\varphi ,2}\), with \(\Omega _{\varphi ,1}\) and \(\Omega _{\varphi ,2}\) two open sets with smooth boundaries such that \(\overline{\Omega _{\varphi ,1}}\subset \overline{\Omega _{\varphi ,2}}\subset \Omega _{0,e}\) and \(\Omega _{\varphi ,1}\) containing a neighbourhood of \(\Gamma _i\).
Let \({\mathcal {Q}}_{e}\) be a pressure associated to \(\mathbf{v }_{e}\). The pair \((\mathbf{v }_{c},q_{c})=(\varphi \mathbf{v }_{e},\varphi {\mathcal {Q}}_{e})\) satisfies, in \(\mathbf{H }^{-1}(\Omega _{\varphi ,2})\),
Since \((\mathbf{v }_{c},q_{c})\) belongs to \(\mathbf{H }^{1}_{0}(\Omega _{\varphi ,2})\times L^{2}(\Omega _{\varphi ,2})\), the previous equality implies that \((\mathbf{v }_{c},q_{c})\) is a solution to the following Stokes equations (in the usual variational sense)
We then use known results for Stokes equations with Dirichlet boundary conditions (see, for example, [10, Chap IV, Theorem 5.8]) to obtain \((\mathbf{v }_{c},q_{c})\in \mathbf{H }^{2}(\Omega _{\varphi ,2})\times H^{1}(\Omega _{\varphi ,2})\). As \((\mathbf{v }_{c},q_{c})\) is equal to \((\mathbf{v }_{e},{\mathcal {Q}}_{e})\) on \(\Omega _{\varphi ,1}\), we obtain the regularity result for \((\mathbf{v }_{e},{\mathcal {Q}}_{e})\) in a neighbourhood of \(\Gamma _{i}\).
Step 3: We want to prove that the restriction to \(\Omega _{0}\) of \(\mathbf{v }_{e}\) is the solution \(\mathbf{v }\) to the variational formulation \((\star )\). Using the Lax–Milgram lemma, we know that \(\mathbf{v }_{e}\) satisfies
Hence, using the symmetry properties of \(\overline{\mathbf{f }}_e\) we can prove that the function \(\mathbf{v }_s\) defined by
is also a solution to the minimization problem (5.10). As (5.10) admits a unique solution, we obtain that \(\mathbf{v }_s=\mathbf{v }_{e}\). The symmetry properties and the regularity of \(\mathbf{v }_{e}\) imply that \(v_{e,2}=0\) on \(\Gamma _{i}\). We can now prove that the restriction to \(\Omega _{0}\) of \(\mathbf{v }_{e}\) is the solution \(\mathbf{v }\) to \((\star )\). Let \(\varvec{\varphi }\) be a test function in V and denote by \(\varvec{\varphi }_{e}\) the function defined by
Thanks to the condition \(\varphi _{2}=0\) on \(\Gamma _{i,o}\), we notice that \(\varvec{\varphi }_{e}\) is in \(\mathbf{H }^{1}(\Omega _{0,e})\) and more precisely in \(V_{e}\). Hence, we can use \(\varvec{\varphi }_{e}\) as a test function in the variational formulation satisfied by \(\mathbf{v }_{e}\), we obtain
Using the symmetry properties of \(\mathbf{v }_{e}\), \(\varvec{\varphi }_{e}\) and \(\overline{\mathbf{f }}_e\), we have
and
Hence,
for all \(\varvec{\varphi }\) in V, which proves that the restriction to \(\Omega _{0}\) of \(\mathbf{v }_{e}\) is the solution \(\mathbf{v }\) to the variational formulation \((\star )\). Hence, \(\mathbf{v }\) is \(\mathbf{H }^{2}\) in a neighbourhood of \(\Gamma _{i}\). The same technique works for the boundary \(\Gamma _{o}\), which implies the regularity result on the whole domain \(\Omega _{0}\).
Step 4: Let \({\mathcal {Q}}\) be a pressure associated with \(\mathbf{v }\). The regularity of \(\mathbf{v }\) and the equality (in the sense of the distributions)
imply that \({\mathcal {Q}}\) belongs to \(H^{1}(\Omega _{0})\). We now have to prove that \({\mathcal {Q}}\) is equal to a constant on \(\Gamma _{i,o}\). Thanks to the regularity of \((\mathbf{v },{\mathcal {Q}})\), the equality \(-\Delta \mathbf{v }+ \nabla {\mathcal {Q}}=\overline{\mathbf{f }}\) holds in \(\mathbf{L }^{2}(\Omega _{0})\). For all \(\varvec{\psi }\) in V, we have
and, using the definition of \(\mathbf{v }\),
This implies that \({\mathcal {Q}}\) is constant on \(\Gamma _{i,o}\). To see this, it is sufficient to prove that for all \(\phi \in {\mathcal {C}}^{\infty }_{c}(\Gamma _{i,o})\) satisfying
there exists \(\varvec{\psi }\in V\) such that \(\varvec{\psi }\cdot \mathbf{n }=\phi \) on \(\Gamma _{i,o}\). Let \(\varvec{\phi }\) be the function defined by
Using [13, Lemma 2.2], the equations
admit a solution \(\varvec{\psi }\) in \(\mathbf{H }^{1}(\Omega _{0})\). Such a \(\varvec{\psi }\) belongs to V and satisfies \(\varvec{\psi }\cdot \mathbf{n }=\phi \) on \(\Gamma _{i,o}\). Hence, \({\mathcal {Q}}\) is constant on \(\Gamma _{i,o}\).
Step 5: Among the pressures \({\mathcal {Q}}\) associated with \(\mathbf{v }\), there exists a unique q in \(H^{1}(\Omega _{0})\) satisfying \(q=0\) in \(\Gamma _{i,o}\) in the sense of the trace for Sobolev functions. The pair \((\mathbf{v },q)\) in \(\mathbf{H }^{2}(\Omega _{0})\times H^{1}(\Omega _{0})\) is the unique solution to (5.8) and \((\mathbf{u },p)=(\mathbf{v },q)+(\mathbf{w },H)\) is the unique solution to (5.1). The estimate on \((\mathbf{u },p)\) follows from classical estimate for the Stokes equations (5.9) and Theorem 5.1 to estimate \(\mathbf{w }\). \(\square \)
According to Theorem 5.4, the Stokes operator A associated with (5.1) with homogeneous boundary condition is defined by
and for all \(\mathbf{u }\in {\mathcal {D}}(A)\), \(A\mathbf{u }=\nu \Pi \Delta \mathbf{u }\).
Theorem 5.5
The operator \((A,{\mathcal {D}}(A))\) is the infinitesimal generator of an analytic semigroup on \(\mathbf{V }^{0}_{n,\Gamma _{d}}(\Omega _{0})\). Moreover, we have \({\mathcal {D}}(A^{1/2})=V\).
Proof
The bilinear form associated with the operator A defined by
is continuous and coercive; hence, [7, Part 2, Theorem 2.2] proves that the operator A is the infinitesimal generator of an analytic semigroup. For the second part of the theorem, we have, for all \(\mathbf{u }\in {\mathcal {D}}(A)\),
By density, the previous equality is still true for \(\mathbf{u }\in V\), which concludes the proof. \(\square \)
We now want to study (5.1) for weaker data using transposition method. The following lemma, used to solve nonzero divergence Stokes equations, is needed to obtain weak estimates on the pressure in Theorem 5.6.
Lemma 5.1
For all \(\Phi \in H^{1}_{0}(\Omega _{0})\), the system
admits a solution \(\mathbf{w }\in \mathbf{H }^{2}(\Omega _{0})\) satisfying the estimate
Proof
If \(\Phi \) has a zero average, the result comes directly from [23, Chap II.2, Lemma 2.3.1]. This lemma gives the existence of a function \(\mathbf{w }\in \mathbf{H }^{2}_{0}(\Omega _{0})\) such that \(\text {div }\mathbf{w }=\Phi \). In the general case, the idea is to find a pair \((\mathbf{w }_{0},\Phi _{0})\) solution to (5.11), where \(\Phi _{0}\) has a nonzero average, and to use it to come back to the previous framework.
Let \(\delta >0\) be the constant defined by (5.5) in Theorem 5.1 and \(\rho \in {\mathcal {C}}^{\infty }({\mathbb {R}})\) be a nonzero non-negative function compactly supported in \((0,\delta )\). Let \(\theta \in {\mathcal {C}}^{\infty }(0,L)\) be such that \(\theta =0\) near 0 and \(\theta =1\) near L. Define \(\mathbf{w }_{0}(x,y)=(\rho (y)\theta (x),0)^{T}\) for all \((x,y)\in \Omega _{0}\). The function \(\mathbf{w }_{0}\) is smooth and satisfies the boundary conditions in (5.11). Finally, set \(\Phi _{0}(x,y)=\text {div }\mathbf{w }_{0}(x,y)=\rho (y)\theta '(x)\) for all \((x,y)\in \Omega _{0}\) and remark that \(\Phi _{0}\in H^{1}_{0}(\Omega _{0})\) and
We look for a solution to (5.11) under the form \(\mathbf{w }={\widetilde{\mathbf{w }}}+c\mathbf{w }_{0}\) with \(c={\int }_{\Omega _{0}}\Phi /{\int }_{\Omega _{0}}\Phi _{0}\). The function \({\widetilde{\mathbf{w }}}\) needs to satisfy
The function \({\widetilde{\Phi }}=\Phi -c\Phi _{0}\) is in \(H^{1}_{0}(\Omega _{0})\) and has a zero average. The existence of \({\widetilde{\mathbf{w }}}\) follows from [23, Chap II.2, Lemma 2.3.1]. To prove the estimate on \(\mathbf{w }\), remark that
\(\square \)
Theorem 5.6
For all \((\mathbf{f },\mathbf{g },h)\in \mathbf{L }^{2}(\Omega _{0})\times {\mathcal {H}}^{3/2}_{00}(\Gamma _{0})\times H^{1/2}(\Gamma _{i,o})\), the solution \((\mathbf{u },p)\) of equation (5.1) satisfies the estimate
Proof
The fluid part estimate is similar to [21, Lemma A.3] using as test function the solution \((\varvec{\Psi },\pi )\), given by Theorem 5.4, to
with \(\varvec{\varphi }\in \mathbf{L }^{2}(\Omega _{0})\). Let us prove the pressure estimate. For all \(\Phi \in H^{1}_{0}(\Omega _{0})\), consider the system
Using Lemma 5.1 and Theorem 5.4, this system admits a unique solution \((\mathbf{v },q)\) in \(\mathbf{H }^{2}(\Omega _{0})\times H^{1}(\Omega _{0})\), which satisfies
Using Green’s formula, the following computations hold
and
where \(\mathbf{g }=(0,g)^{T}\) and \(P_{2}\) is the vectorial projection on the second component. As \(\partial _1 v_1+\partial _2 v_2=\Phi \) and \(v_2=0\) on \(\Gamma _{i,o}\), we notice that \(\partial _1 v_1=\Phi \) on \(\Gamma _{i,o}\), and as \(\Phi \in H^{1}_{0}(\Omega _{0})\), we obtain \(\partial _1 v_1=0\) on \(\Gamma _{i,o}\). Finally,
which implies the pressure estimate. \(\square \)
As for [21, Theorem A.1], we now define a notion of weak solutions for (5.1). For \((\mathbf{f },\mathbf{g },h)\) in \((\mathbf{H }^{2}(\Omega _{0}))'\times ({\mathcal {H}}^{1/2}(\Gamma _0))'\times (H^{3/2}(\Gamma _{i,o}))'\), consider the following variational formulation:
Find \((\mathbf{u },p)\in \mathbf{L }^{2}(\Omega _{0})\times H^{-1}(\Omega _{0})\) such that
for all \(\varvec{\varphi }\in \mathbf{L }^{2}(\Omega _{0})\) and \((\varvec{\Psi },\pi )\) solution of (5.13), and
for all \(\Phi \in H^{1}_{0}(\Omega _{0})\) and \((\mathbf{v },q)\) solution of (5.14).
Theorem 5.7
For all \((\mathbf{f },\mathbf{g },h)\in (\mathbf{H }^{2}(\Omega _{0}))'\times ({\mathcal {H}}^{1/2}(\Gamma _0))'\times (H^{3/2}(\Gamma _{i,o}))'\), there exists a unique solution \((\mathbf{u },p)\in \mathbf{L }^{2}(\Omega _{0})\times H^{-1}(\Omega _{0})\) of (5.1) in the sense of the variational formulation (5.15)–(5.16). This solution satisfies the following estimate
Proof
See [21, Theorem A.1]. \(\square \)
1.2 Unsteady Stokes equations
Consider the unsteady Stokes equations
As for the steady Stokes equations, a non-homogeneous boundary condition on the pressure \(p=h\) in (5.18) can be handled directly with a lifting; hence, through this section, we assume that \(h=0\). We prove the existence and uniqueness of a solution to (5.18) in Theorem 5.8. Then, we transform (5.18) to prove existence uniqueness and regularity result when the Dirichlet boundary condition \(\mathbf{g }\) is less regular (see Theorem 5.9). We use this result to prove Lemma 3.2. Finally, we specify the regularity result used in the study of the fluid–structure system in Theorem 5.11 and we apply this result in Lemma 5.3.
Writing the equations satisfied by \(\mathbf{u }-D\mathbf{g }\) and using standard semigroup techniques, we obtain the following theorem. Remark that the assumption \(\mathbf{u }^0-D\mathbf{g }(0)\in V\) is equivalent to \(\mathbf{u }^{0}\in \mathbf{V }^{1}(\Omega _{0})\), \(\mathbf{u }^{0}=\mathbf{g }\) on \(\Gamma _{0}\) and \(u^{0}_{2}=0\) on \(\Gamma _{i,o}\).
Theorem 5.8
For all \(\mathbf{g }\in L^{2}(0,T;{\mathcal {H}}^{3/2}_{00}(\Gamma _0))\cap H^{1}(0,T;({\mathcal {H}}^{1/2}(\Gamma _0))')\), \(\mathbf{f }\in \mathbf{L }^{2}(Q_{T})\) and \(\mathbf{u }^0\in \mathbf{H }^{1}(\Omega _{0})\) satisfying the compatibility condition \(\mathbf{u }^0-D\mathbf{g }(0)\) belongs to V, equation (5.18) admits a unique solution \((\mathbf{u },p)\in \mathbf{H }^{2,1}(Q_{T})\times L^{2}(0,T;H^{1}(\Omega _{0}))\). This solution satisfies the following estimate
We now want to study (5.18) for \(\mathbf{g }\in L^{2}(0,T;{\mathcal {L}}^{2}(\Gamma _0))\). We follow the approach of [21]. The operator A, using extrapolation method, can be extended to an unbounded operator \(\overset{\sim }{A}\) defined on \(({\mathcal {D}}(A^{*}))'\) with domain \({\mathcal {D}}(\overset{\sim }{A})=\mathbf{V }^{0}_{n,\Gamma _{d}}(\Omega _{0})\).
Definition 5.1
A function \(\mathbf{u }\in \mathbf{L }^{2}(Q_{T})\) is called a weak solution to (5.18) if \(\Pi \mathbf{u }\) is a weak solution to the evolution equation
and \(({\mathbb {I}}-\Pi )\mathbf{u }\) is given by
Remark that \(A=A^{*}\) (the operator A is symmetric and onto from \({\mathcal {D}}(A)\) into \(\mathbf{V }^{0}_{n,\Gamma _{d}}(\Omega _{0})\)). By definition to a weak solution for (5.19) (see [7]), \(\Pi \mathbf{u }\in L^{2}(0,T,\mathbf{V }^{0}_{n,\Gamma _{d}}(\Omega _{0}))\) is solution to (5.19) if and only if for all \(\Phi \in {\mathcal {D}}(A^{*})={\mathcal {D}}(A)\) the map \(t\mapsto {\int }_{\Omega _{0}}\Pi \mathbf{u }\cdot \Phi \) belongs to \(H^{1}(0,T)\) and
Using Green formula, we compute the adjoint of the operator D.
Lemma 5.2
For all \(\mathbf{f }\in \mathbf{L }^{2}(\Omega _{0})\), the adjoint operator \(D^{*}\) of D is defined by
where \((\mathbf{v },q)\in \mathbf{H }^{2}(\Omega _{0})\times H^{1}(\Omega _{0})\) is the solution to
Using that \(\overset{\sim }{A}^{*}=A\) on \({\mathcal {D}}(A)\), the variational formulation (5.21) becomes
with \(\nabla q=\nu ({\mathbb {I}}-\Pi )\Delta \Phi \). The previous equality follows from the uniqueness of the stationary Stokes system and the identity \(-\nu \Delta \Phi + \nu ({\mathbb {I}}-\Pi )\Delta \Phi =-A\Phi \). Finally, \(\Pi \mathbf{u }\) is a weak solution to 5.19 if and only if
We can now state a theorem analogue to [21, Theorem 2.3].
Theorem 5.9
For all \(\Pi \mathbf{u }^0\in \mathbf{V }^{0}_{n,\Gamma _{d}}(\Omega _{0})\), \(\mathbf{g }\in L^{2}(0,T;{\mathcal {L}}^{2}(\Gamma _0))\) and \(\mathbf{f }\in \mathbf{L }^{2}(Q_{T})\), equation (5.18) admits a unique weak solution \(\mathbf{u }\) in the sense Definition 5.1. This solution satisfies the following estimate
Proof
See [21, Theorem 2.3]. \(\square \)
As in [21] we can prove that for \(\mathbf{g }\in L^{2}(0,T;{\mathcal {H}}^{3/2}_{00}(\Gamma _0))\cap H^{1}(0,T;{\mathcal {H}}^{-1/2}(\Gamma _0))\) a function \(\mathbf{u }\) is solution to (5.18) in the sense of Theorem 5.8 if and only if \(\mathbf{u }\) is a weak solution to (5.18)(in the sense of Definition 5.1). The following theorem characterizes the pressure.
Theorem 5.10
For all \(\mathbf{g }\in L^{2}(0,T;{\mathcal {H}}^{3/2}_{00}(\Gamma _0))\cap H^{1}(0,T;({\mathcal {H}}^{1/2}(\Gamma _0))')\), \(\mathbf{f }\in \mathbf{L }^{2}(Q_{T})\) and \(\mathbf{u }^0\in \mathbf{H }^{1}(\Omega _{0})\) satisfying the compatibility condition \(\mathbf{u }^0-D\mathbf{g }(0)\) belongs to V, a pair \((\mathbf{u },p)\in \mathbf{H }^{2,1}(Q_{T})\times L^{2}(0,T;H^{1}(\Omega _{0}))\) is solution of (5.18) if and only if
where
-
\(q\in H^{1}(0,T;H^{1}(\Omega _{0}))\) is the solution to
$$\begin{aligned} \Delta q=0\,\text { in }Q_{T},\,\,\,\rho =0\,\text { on }\Sigma ^{i,o}_{T},\,\,\,\frac{\partial q}{\partial \mathbf{n }}=\mathbf{g }\cdot \mathbf{n }\,\text { on }\Sigma ^{0}_{T},\,\,\,\frac{\partial q}{\partial \mathbf{n }}=0\,\text { on }\Sigma ^{b}_{T}. \end{aligned}$$(5.24) -
\(\rho \in L^{2}(0,T;H^{1}(\Omega _{0}))\) is the solution to
$$\begin{aligned} \Delta \rho =0\,\text { in }Q_{T},\,\,\,\rho =0\,\text { on }\Sigma ^{i,o}_{T},\,\,\,\frac{\partial \rho }{\partial \mathbf{n }}=\nu \Delta \Pi \mathbf{u }\cdot \mathbf{n }\,\text { on }\Sigma ^{d}_{T}, \end{aligned}$$(5.25)where \(\nu \Delta \Pi \mathbf{u }\cdot \mathbf{n }\) is in \(L^{2}(0,T;H^{-1/2}(\Gamma _{d}))\) thanks to the divergence theorem.
-
\(p_{\mathbf{f }}\in L^{2}(0,T;H^{1}(\Omega _{0}))\) is given by the identity \((I-\Pi )\mathbf{f }=\nabla p_{\mathbf{f }}\).
Proof
Writing \(\mathbf{u }=\Pi \mathbf{u }+ ({\mathbb {I}}-\Pi )\mathbf{u }\) in Equation (5.18), we have
By definition of \(({\mathbb {I}}-\Pi )\), there exists \(q\in H^{1}_{\Gamma _{i,o}}(\Omega _{0})\) such that \(\nabla q=({\mathbb {I}}-\Pi )\mathbf{u }\). Using the condition \(\text {div }\mathbf{u }=0\) and \(({\mathbb {I}}-\Pi )\mathbf{u }=({\mathbb {I}}-\Pi )D\mathbf{g }\), we obtain that q is solution to (5.24). As \(\mathbf{g }\in H^{1}(0,T;{\mathcal {H}}^{-1/2}(\Gamma _0))\), the function q belongs to \(H^{1}(0,T;H^{1}(\Omega _{0}))\).
The function \(\Pi \mathbf{u }\) is solution to the equation
with \(\rho = p-\nu \Delta q + q_t=p+q_t\). Taking the divergence of the previous equation and the normal trace on \(\Gamma _{d}\) (which is well defined as \(\Delta \Pi \mathbf{u }\) is in \(L^{2}(0,T;\mathbf{L }^{2}(\Omega _{0}))\) with a divergence equal to zero), we obtain (5.25) and \(\rho \in L^{2}(0,T;H^{1}(\Omega _{0}))\). \(\square \)
We conclude this section with a regularity result, coming from the interpolation of the regularity results stated in Theorem 5.8 and Theorem 5.9, and an application to the operator \({\mathcal {A}}_{1}\) defined in Section 3.3.
Theorem 5.11
For all \(\mathbf{g }\in L^{2}(0,T;{\mathcal {H}}^{1}_{0}(\Gamma _0))\cap H^{1/2}(0,T;{\mathcal {L}}^{2}(\Gamma _0))\), \(\mathbf{f }=0\) and \(\Pi \mathbf{u }^{0}=0\), the solution \(\mathbf{u }\) to (5.19)–(5.20) satisfies the estimate
Lemma 5.3
The operator \(({\mathcal {A}}_{1},{\mathcal {D}}({\mathcal {A}}_{1}))\) is the infinitesimal generator of a strongly continuous semigroup on \(\mathbf{H }\).
Proof
The first part is to prove that the unbounded operator \((\overset{\sim }{{\mathcal {A}}_1},{\mathcal {D}}(\overset{\sim }{{\mathcal {A}}_1}))\), defined by
and
is the infinitesimal generator of a strongly continuous semigroup on \(V^{-1}\times H_s\). Here, \(V^{-1}\) is the dual of V endowed with the norm
This proof is similar to [22, Theorem 3.5]. Then, we consider the evolution equation
The solution to (5.26) can be found in two steps. First, we determine \((\eta _{1},\eta _{2})\) and then \(\Pi \mathbf{u }\). We recall that \((A_s,{\mathcal {D}}(A_s))\) is the infinitesimal generator of an analytic semigroup on \(H_s\) (see [11]). Let \((\Pi \mathbf{u }^{0},\eta ^{0}_{1},\eta ^{0}_{2})\) be in \(V^{-1}\times H_s\). Using [7, Chap 3, Theorem 2.2], we obtain \(\eta _{1}\in H^{3,3/2}(\Sigma ^{s}_{T})\) and \(\eta _{2}\in H^{1,1/2}(\Sigma ^{s}_{T})\). Now let us assume that \((\Pi \mathbf{u }^{0},\eta ^{0}_{1},\eta ^{0}_{2})\in \mathbf{H }\). We have to solve
We split this equation into two parts \(\Pi \mathbf{u }=\Pi \mathbf{u }_{1} + \Pi \mathbf{u }_{2}\) with
and
Using Theorem 5.11, we remark that \(\Pi \mathbf{u }_{1}\in \mathbf{H }^{3/2-\varepsilon ,3/4-\varepsilon /2}(Q_{T})\). For \(\Pi \mathbf{u }_{2}\), [7, Chap 3, Theorem 2.2] shows that \(\Pi \mathbf{u }_{2}\in L^{2}(0,T;V)\cap H^{1}(0,T;V^{-1})\). Interpolation result [18, Theorem 3.1] ensures that \(\Pi \mathbf{u }_{2}\in {\mathcal {C}}([0,T];\mathbf{V }^{0}_{n,\Gamma _{d}}(\Omega _{0}))\).
Hence, \((\Pi \mathbf{u },\eta _{1},\eta _2)\in {\mathcal {C}}([0,T];\mathbf{H })\) and the restriction to the semigroup \((e^{t\overset{\sim }{{\mathcal {A}}_1}})_{t\in {\mathbb {R}}^{+}}\) to \(\mathbf{H }\) is a strongly continuous semigroup on \(\mathbf{H }\). Finally, we can verify that the infinitesimal generator associated with this restriction is exactly the operator \(({\mathcal {A}}_1,{\mathcal {D}}({\mathcal {A}}_{1}))\).
\(\square \)
1.3 Elliptic equations for the projector \(\Pi \)
In this section, we prove higher regularity result for an elliptic equation, which implies the regularity result on the projector \(\Pi \) given in Lemma 3.1.
Lemma 5.4
Let f be in \(H^{1}(\Omega _{0})\) such that \(f=0\) on \(\Gamma _{i,o}\) and g be in \(H^{3/2}_{00}(\Gamma _{0})\). Then, the elliptic equation
admits a unique solution \(\rho \in H^{3}(\Omega _{0})\).
Proof
\(H^{3}\) regularity far from the corners of \(\Omega _{0}\) is obtained through classical arguments. To prove the \(H^{3}\) regularity at the corners, say along \(x=0\), we first perform a symmetry with respect to \(x=0\) (step 1) and then a change of variables to transport the PDE on \((-L,L)\times (0,1)\) (step 2).
Step 1: Using the notations of step 1 in the proof of Theorem 5.4 for \(\eta ^{0}_{e}\), \(\Gamma _{0,e}\), \(\Omega _{0,s}\) and \(\Omega _{0,e}\) we define \(f_{e}\) and \(g_{e}\) by
Assumptions on f and g ensure that \((f_{e},g_{e})\) is in \(H^{1}(\Omega _{0,e})\times \mathbf{H }^{3/2}(\Gamma _{0,e})\). Define \(\rho _{e}\) by
Then, \(\rho _{e}\in H^{2}(\Omega _{0,e})\) and satisfies
Step 2: Let \(\Omega _{e}=(-L,L)\times (0,1)\) and \(\varphi \) be the change of variables
As in Theorem 5.1, the function \(\varphi \) transports \(H^{3}(\Omega _{0,e})\) to \(H^{3}(\Omega _{e})\). Hence, it is sufficient to prove the \(H^{3}\) regularity after transport. Let \(\mathbf{J }_{\varphi }\) be the Jacobian matrix of \(\varphi \). Setting \(\widetilde{\rho _{e}}=\rho \circ \varphi ^{-1}\), \(\widetilde{f_{e}}=\vert \mathbf{J }_{\varphi }\vert ^{-1} f_{e}\circ \varphi ^{-1}\) and \(\displaystyle \widetilde{g_{e}}(x,1)=g_{e}(x,1+\eta ^{0}_{e }(x))\) the function \(\widetilde{\rho _{e}}\) is solution to
where the matrix \(A=(A_{i,j})_{1\le i,j\le 2}=\vert \text {det}(\mathbf{J }_{\varphi }) \vert ^{-1}\mathbf{J }_{\varphi }\mathbf{J }_{\varphi }^{T}\) is uniformly positive definite symmetric with coefficients in \(W^{1,\infty }\cap H^{2}\).
Step 3: Deriving (5.28) with respect to x shows that \(\partial _{x}\widetilde{\rho _{e}}\) satisfies (with \(\partial _{1}=\partial _{x}\) and \(\partial _{2}=\partial _{z}\))
with
in the sense of the distributions on \(\Omega _{e}\). From here on, we localize near (0, 1).
Step 4: We use a bootstrap argument. The first step is to find an \(L^{\infty }\) estimate on \(\nabla \widetilde{\rho _e}\). In the right hand-side of (5.29) the least regular terms are under the form \(\left( \partial _{11}A_{11}\right) \partial _{x}\widetilde{\rho _e}\) or \(\left( \partial _{12}A_{22}\right) \partial _{z}\widetilde{\rho _e}\). Sobolev embeddings show that these terms are in \(L^{r}\) for all \(1<r<2\). Moreover, the Neumann boundary condition involves \(\partial _{x}\widetilde{g_e}-\left( \partial _{1}A_{21}\right) \partial _{x}\widetilde{\rho _e}-\left( \partial _{1}A_{22}\right) \partial _{z}\widetilde{\rho _e}\), where the least regular terms are traces of \(W^{1,r}\) functions. Using the results of [2] and [3], we obtain that \(\partial _{x}\widetilde{\rho _e}\) is in \(W^{2,r}\). Then, the embeddings \(W^{2,r}\subset W^{1,r^{*}}\subset L^{\infty }\) with \(r^{*}=\frac{2r}{2-r}>2\) show that the terms under the form \(\left( \partial _{11}A_{11}\right) \partial _{x}\widetilde{\rho _e}\) are in \(L^{2}\) and \(\left( \partial _{1}A_{21}\right) \partial _{x}\widetilde{\rho _e}\) is in \(H^{1/2}\) (on the boundary). Moreover, using equation (5.28) we obtain that \(\partial _{zz}\widetilde{\rho _e}\) is in \(L^{r^{*}}\) and thus \(\partial _{z}\widetilde{\rho _e}\in W^{1,r^{*}}\subset L^{\infty }\). Finally, the right-hand side is in \(L^{2}\) and the Neumann boundary condition in \(H^{1/2}\) and thus \(\partial _{x}\widetilde{\rho _e}\) is \(H^{2}\) near (0, 1). For the regularity with respect to z, we can use equation (5.28) and \(\widetilde{\rho _e}\) is \(H^{3}\) in a neighbourhood of (0, 0).
Step 5: The strategy applies for (0, 0). If we come back to the initial equation on the domain \(\Omega _{0}\), we have proved that \(\rho \) is \(H^{3}\) near \(\Gamma _{i}\). The same proof can be used for the regularity near \(\Gamma _{o}\) and finally \(\rho \in H^{3}(\Omega _{0})\). \(\square \)
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Casanova, J . Fluid–structure system with boundary conditions involving the pressure. J. Evol. Equ. 21, 107–149 (2021). https://doi.org/10.1007/s00028-020-00581-2
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DOI: https://doi.org/10.1007/s00028-020-00581-2