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A finite element method for incompressible Navier-Stokes equations in a time-dependent domain Yuri Vassilevski1,2 Maxim Olshanskii3 Alexander Lozovskiy1 Alexander Danilov1,2 1 2 Institute of Numerical Mathematics RAS Moscow Institute of Physics and Technology 3 University of Houston Ginzburg Centennial Conference on Physics May 30, 2017, Moscow The work was supported by the Russian Science Foundation Fluid-Structure Interaction problem Prerequisites for FSI I reference subdomains Ωf , Ωs Fluid-Structure Interaction problem Prerequisites for FSI I reference subdomains Ωf , Ωs I transformation ξ maps Ωf , Ωs to Ωf (t), Ωs (t) Fluid-Structure Interaction problem Prerequisites for FSI I reference subdomains Ωf , Ωs I transformation ξ maps Ωf , Ωs to Ωf (t), Ωs (t) I b := Ωf ∪ Ωs v and u denote velocities and displacements in Ω Fluid-Structure Interaction problem Prerequisites for FSI I reference subdomains Ωf , Ωs I transformation ξ maps Ωf , Ωs to Ωf (t), Ωs (t) I b := Ωf ∪ Ωs v and u denote velocities and displacements in Ω I ξ(x) := x + u(x), F := ∇ξ = I + ∇u, J := det(F) Fluid-Structure Interaction problem Prerequisites for FSI I reference subdomains Ωf , Ωs I transformation ξ maps Ωf , Ωs to Ωf (t), Ωs (t) I b := Ωf ∪ Ωs v and u denote velocities and displacements in Ω I ξ(x) := x + u(x), F := ∇ξ = I + ∇u, J := det(F) I Cauchy stress tensors σ f , σ s Fluid-Structure Interaction problem Prerequisites for FSI I reference subdomains Ωf , Ωs I transformation ξ maps Ωf , Ωs to Ωf (t), Ωs (t) I b := Ωf ∪ Ωs v and u denote velocities and displacements in Ω I ξ(x) := x + u(x), F := ∇ξ = I + ∇u, J := det(F) I Cauchy stress tensors σ f , σ s I pressures pf ,ps Fluid-Structure Interaction problem Prerequisites for FSI I reference subdomains Ωf , Ωs I transformation ξ maps Ωf , Ωs to Ωf (t), Ωs (t) I b := Ωf ∪ Ωs v and u denote velocities and displacements in Ω I ξ(x) := x + u(x), F := ∇ξ = I + ∇u, J := det(F) I Cauchy stress tensors σ f , σ s I pressures pf ,ps I densities ρs , ρf are constant Fluid-Structure Interaction problem Universal equations in reference subdomains Dynamic equations −T ρ−1 ) in Ωs , s div (Jσ s F ∂v = ∂u −1 −T −1 ∂t v− in Ωf (Jρf ) div (Jσ f F ) − ∇v F ∂t Fluid-Structure Interaction problem Universal equations in reference subdomains Dynamic equations −T ρ−1 ) in Ωs , s div (Jσ s F ∂v = ∂u −1 −T −1 ∂t v− in Ωf (Jρf ) div (Jσ f F ) − ∇v F ∂t Kinematic equation ∂u =v ∂t in Ωs Fluid-Structure Interaction problem Universal equations in reference subdomains Dynamic equations −T ρ−1 ) in Ωs , s div (Jσ s F ∂v = ∂u −1 −T −1 ∂t v− in Ωf (Jρf ) div (Jσ f F ) − ∇v F ∂t Kinematic equation ∂u =v ∂t in Ωs Fluid incompressibility div (JF−1 v) = 0 in Ωf or J∇v : F−T = 0 in Ωf Fluid-Structure Interaction problem Universal equations in reference subdomains Dynamic equations −T ρ−1 ) in Ωs , s div (Jσ s F ∂v = ∂u −1 −T −1 ∂t v− in Ωf (Jρf ) div (Jσ f F ) − ∇v F ∂t Kinematic equation ∂u =v ∂t in Ωs Fluid incompressibility div (JF−1 v) = 0 in Ωf or J∇v : F−T = 0 in Ωf Constitutive relation for the fluid stress tensor σ f = −pf I + µf ((∇v)F−1 + F−T (∇v)T ) in Ωf FSI problem User-dependent equations in reference subdomains Constitutive relation for the solid stress tensor σ s = σ s (J, F, ps , λs , µs , . . . ) in Ωs FSI problem User-dependent equations in reference subdomains Constitutive relation for the solid stress tensor σ s = σ s (J, F, ps , λs , µs , . . . ) in Ωs Monolithic approach: Extension of the displacement field to the fluid domain G (u) = 0 in Ωf , u = u∗ on ∂Ωf FSI problem User-dependent equations in reference subdomains Constitutive relation for the solid stress tensor σ s = σ s (J, F, ps , λs , µs , . . . ) in Ωs Monolithic approach: Extension of the displacement field to the fluid domain G (u) = 0 in Ωf , u = u∗ on ∂Ωf for example, vector Laplace equation or elasticity equation FSI problem User-dependent equations in reference subdomains Constitutive relation for the solid stress tensor σ s = σ s (J, F, ps , λs , µs , . . . ) in Ωs Monolithic approach: Extension of the displacement field to the fluid domain G (u) = 0 in Ωf , u = u∗ on ∂Ωf for example, vector Laplace equation or elasticity equation + Initial, boundary, interface conditions (σ f F−T n = σ s F−T n) Numerical scheme I b Conformal triangular or tetrahedral mesh Ωh in Ω I LBB-stable pairs for velocity and pressure P2 /P1 or P2 /P0 I Fortran open source software Ani2D, Ani3D (Advanced numerical instruments 2D/3D) http://sf.net/p/ani2d/ I I I mesh generation FEM systems algebraic solvers http://sf.net/p/ani3d/: Numerical scheme Find {uk+1 , vk+1 , p k+1 } ∈ V0h × Vh × Qh s.t. ∂u k+1 = vk+1 on Γfs v = gh (·, (k + 1)∆t) on Γf 0 , ∂t k+1 Numerical scheme Find {uk+1 , vk+1 , p k+1 } ∈ V0h × Vh × Qh s.t. ∂u k+1 = vk+1 on Γfs v = gh (·, (k + 1)∆t) on Γf 0 , ∂t k+1 where b 3 , Qh ⊂ L2 (Ω), b V0 = {v ∈ Vh : v|Γ ∪Γ = 0}, V00 = {v ∈ V0 : v|Γ = 0} Vh ⊂ H 1 (Ω) h h h s0 f0 fs ∂f ∂t := k+1 3f k+1 − 4f k + f k−1 2∆t Numerical scheme Z Z ∂v ψ dΩ + Jk F(e uk )S(uk+1 , e uk ) : ∇ψ dΩ + ∂t k+1 Ωs g ! Z ∂v ∂u k+1 −1 k k ψ dΩ + ρf J k ψ dΩ + ρf Jk ∇v F (e u ) e v − ∂t k+1 ∂t k Ωf Z p k+1 Jk F−T (e uk ) : ∇ψ dΩ = 0 ∀ψ ∈ V0h 2µf Jk Deuk vk+1 : Deuk ψ dΩ − ρs Ωs Z Ωf Z Ωf Jk := J(e uk ), Ω e f k := 2f k − f k−1 , Du v := {∇vF−1 (u)}s , {A}s := 1 (A + AT ) 2 Numerical scheme Z ∂v ψ dΩ + Jk F(e uk )S(uk+1 , e uk ) : ∇ψ dΩ + ∂t k+1 Ωs g ! Z ∂v ∂u k+1 −1 k k ψ dΩ + ρf J k ψ dΩ + ρf Jk ∇v F (e u ) e v − ∂t k+1 ∂t k Ωf Z p k+1 Jk F−T (e uk ) : ∇ψ dΩ = 0 ∀ψ ∈ V0h 2µf Jk Deuk vk+1 : Deuk ψ dΩ − Z ρs Ωs Z Ωf Z Ω Ωf Z Ωs ∂u ∂t Jk := J(e uk ), Z φ dΩ − k+1 vk+1 φ dΩ + Ωs e f k := 2f k − f k−1 , Z G (uk+1 )φ dΩ = 0 ∀φ ∈ V00 h Ωf Du v := {∇vF−1 (u)}s , {A}s := 1 (A + AT ) 2 Numerical scheme Z ∂v ψ dΩ + Jk F(e uk )S(uk+1 , e uk ) : ∇ψ dΩ + ∂t k+1 Ωs g ! Z ∂v ∂u k+1 −1 k k ψ dΩ + ρf J k ψ dΩ + ρf Jk ∇v F (e u ) e v − ∂t k+1 ∂t k Ωf Z p k+1 Jk F−T (e uk ) : ∇ψ dΩ = 0 ∀ψ ∈ V0h 2µf Jk Deuk vk+1 : Deuk ψ dΩ − Z ρs Ωs Z Ωf Z Ω Ωf Z Ωs ∂u ∂t Z φ dΩ − k+1 Z vk+1 φ dΩ + Ωs Z G (uk+1 )φ dΩ = 0 ∀φ ∈ V00 h Ωf Jk ∇vk+1 : F−T (e uk )q dΩ = 0 ∀ q ∈ Qh Ωf Jk := J(e uk ), e f k := 2f k − f k−1 , Du v := {∇vF−1 (u)}s , {A}s := 1 (A + AT ) 2 Numerical scheme Z ... + Ωs I ek ) : ∇ψ dΩ + . . . Jk F(e uk )S(uk+1 , u St. Venant–Kirchhoff model (geometrically nonlinear) : S(u1 , u2 ) = λs tr(E(u1 , u2 ))I + 2µs E(u1 , u2 ); E(u1 , u2 ) = {F(u1 )T F(u2 ) − I}s I inc. Blatz–Ko model: S(u1 , u2 ) = µs (tr({F(u1 )T F(u2 )}s )I − {F(u1 )T F(u2 )}s ) I inc. Neo-Hookean model: S(u1 , u2 ) = µs I; F(e uk ) → F(uk+1 ) {A}s := 12 (A + AT ) Numerical scheme The scheme I provides strong coupling on interface I semi-implicit I produces one linear system per time step I second order in time Numerical scheme The scheme I provides strong coupling on interface I semi-implicit I produces one linear system per time step I second order in time unconditionally stable (no CFL restriction), proved with assumptions: I I I I I 1st order in time St. Venant–Kirchhoff inc./comp. (experiment: Neo-Hookean inc./comp.) extension of u to Ωf guarantees Jk > 0 ∆t is not large A.Lozovskiy, M.Olshanskii, V.Salamatova, Yu.Vassilevski. An unconditionally stable semi-implicit FSI finite element method. Comput.Methods Appl.Mech.Engrg., 297, 2015 2D validation: FSI3 2D benchmark problem S. Turek and J. Hron. Proposal for numerical benchmarking of fluid-structure interaction between an elastic object and laminar incompressible flow. In: Fluid-structure interaction, Springer Berlin Heidelberg, 371–385, 2006. I fluid: 2D Navier-Stokes I stick: Saint Venant-Kirchoff constitutive relation I inflow: parabolic profile I outflow: “do-nothing” I rigid walls: Dirichlet 2D validation: FSI3 2D benchmark problem S. Turek and J. Hron. Proposal for numerical benchmarking of fluid-structure interaction between an elastic object and laminar incompressible flow. In: Fluid-structure interaction, Springer Berlin Heidelberg, 371–385, 2006. 0 ×10-3 0.04 Y-displacement X-displacement -1 -2 -3 -4 -5 0.02 0 -0.02 -6 -0.04 7 I 7.2 7.4 7.6 Time 7.8 8 7 7.2 7.4 7.6 Time 7.8 8 Fortran open source software Ani2D Advanced numerical instruments 2D, http://sf.net/p/ani2d/ 2D validation: FSI3 2D benchmark problem S. Turek and J. Hron. Proposal for numerical benchmarking of fluid-structure interaction between an elastic object and laminar incompressible flow. In: Fluid-structure interaction, Springer Berlin Heidelberg, 371–385, 2006. 0 ×10-3 0.04 Y-displacement X-displacement -1 -2 -3 -4 -5 0.02 0 -0.02 -6 -0.04 7 7.2 7.4 7.6 Time 7.8 8 7 7.2 7.4 7.6 Time 7.8 8 I Fortran open source software Ani2D Advanced numerical instruments 2D, http://sf.net/p/ani2d/ I Displacement in fluid equation: Laplace → mesh tangling, heterogeneous elastisity (more stiff close-to-stick) → OK 2D validation: FSI3 2D benchmark problem S. Turek and J. Hron. Proposal for numerical benchmarking of fluid-structure interaction between an elastic object and laminar incompressible flow. In: Fluid-structure interaction, Springer Berlin Heidelberg, 371–385, 2006. 0 ×10-3 0.04 Y-displacement X-displacement -1 -2 -3 -4 -5 0.02 0 -0.02 -6 -0.04 7 7.2 7.4 7.6 Time 7.8 8 7 7.2 7.4 7.6 Time 7.8 8 I Fortran open source software Ani2D Advanced numerical instruments 2D, http://sf.net/p/ani2d/ I Displacement in fluid equation: Laplace → mesh tangling, heterogeneous elastisity (more stiff close-to-stick) → OK I Simulations are fast, stable, reproduce I displacements I drag, lift I Strouhal numbers 3D benchmark: unsteady flow around silicon filament A. Hessenthaler et al. Experiment for validation of fluid-structure interaction models and algorithms. Int.J.Numer.Meth.Biomed.Engng.,2016. Incompressible fluid flow in a moving domain Navier-Stokes equations in reference domain Ωf Let ξ mapping Ωf to Ωf (t), F = ∇ξ = I + ∇u, J = det(F) be given Incompressible fluid flow in a moving domain Navier-Stokes equations in reference domain Ωf Let ξ mapping Ωf to Ωf (t), F = ∇ξ = I + ∇u, J = det(F) be given Dynamic equations ∂v ∂u −1 −T −1 = (Jρf ) div (Jσ f F ) − ∇v F v− ∂t ∂t in Ωf Incompressible fluid flow in a moving domain Navier-Stokes equations in reference domain Ωf Let ξ mapping Ωf to Ωf (t), F = ∇ξ = I + ∇u, J = det(F) be given Dynamic equations ∂v ∂u −1 −T −1 = (Jρf ) div (Jσ f F ) − ∇v F v− ∂t ∂t in Ωf Fluid incompressibility div (JF−1 v) = 0 in Ωf or J∇v : F−T = 0 in Ωf Incompressible fluid flow in a moving domain Navier-Stokes equations in reference domain Ωf Let ξ mapping Ωf to Ωf (t), F = ∇ξ = I + ∇u, J = det(F) be given Dynamic equations ∂v ∂u −1 −T −1 = (Jρf ) div (Jσ f F ) − ∇v F v− ∂t ∂t in Ωf Fluid incompressibility div (JF−1 v) = 0 in Ωf or J∇v : F−T = 0 in Ωf Constitutive relation for the fluid stress tensor σ f = −pf I + µf ((∇v)F−1 + F−T (∇v)T ) in Ωf Incompressible fluid flow in a moving domain Navier-Stokes equations in reference domain Ωf Let ξ mapping Ωf to Ωf (t), F = ∇ξ = I + ∇u, J = det(F) be given Dynamic equations ∂v ∂u −1 −T −1 = (Jρf ) div (Jσ f F ) − ∇v F v− ∂t ∂t in Ωf Fluid incompressibility div (JF−1 v) = 0 in Ωf or J∇v : F−T = 0 in Ωf Constitutive relation for the fluid stress tensor σ f = −pf I + µf ((∇v)F−1 + F−T (∇v)T ) in Ωf Mapping ξ does not define material trajectories → quasi-Lagrangian formulation Finite element scheme Find {vhk , phk } ∈ Vh × Qh satisfying b.c. (”do nothing” σF−T n = 0 or no-penetration no-slip vk = (ξk − ξk−1 )/∆t) Finite element scheme Find {vhk , phk } ∈ Vh × Qh satisfying b.c. (”do nothing” σF−T n = 0 or no-penetration no-slip vk = (ξk − ξk−1 )/∆t) Z Ωf Z Ωf Z Ωf vhk − vhk−1 · ψ dx + Jk ∆t Z k −T Jk ph Fk : ∇ψ dx + Z Ωf Ωf Jk ∇vhk F−1 k vhk−1 ξ k − ξ k−1 − ∆t Jk qF−T : ∇vhk dx+ k −T k T −T νJk (∇vhk F−1 + F−T k Fk k (∇vh ) Fk ) : ∇ψ dx = 0 for all ψ and q from the appropriate FE spaces ! · ψ dx− Finite element scheme The scheme I semi-implicit I produces one linear system per time step I first order in time (may be generalized to the second order) Finite element scheme The scheme I semi-implicit I produces one linear system per time step I first order in time (may be generalized to the second order) I unconditionally stable (no CFL restriction), proved with assumptions: supQ (kFkF + kF−1 kF ) ≤ CF I inf Q J ≥ cJ > 0, I LBB-stable pairs (e.g. P2 /P1 or P2 /P0 ) I ∆t is not large A.Danilov, A.Lozovskiy, M.Olshanskii, Yu.Vassilevski. A finite element method for the Navier-Stokes equations in moving domain with application to hemodynamics of the left ventricle. Russian J. Numer. Anal. Math. Modelling, 32, 2017 Energy equality for the weak solution Let ∂Ω(t) = ∂Ωns (t) and ξ t be given on ∂Ωns (t). Then there exists v1 ∈ C 1 (Q)d , v1 = ξ t , div (JF−1 v1 ) = 0 [Miyakawa1982] and we can decompose the solution v = w + v1 , w = 0 on ∂Ωns A.Danilov, A.Lozovskiy, M.Olshanskii, Yu.Vassilevski. A finite element method for the Navier-Stokes equations in moving domain with application to hemodynamics of the left ventricle. Russian J. Numer. Anal. Math. Modelling, 32, 2017 Energy equality for the weak solution Let ∂Ω(t) = ∂Ωns (t) and ξ t be given on ∂Ωns (t). Then there exists v1 ∈ C 1 (Q)d , v1 = ξ t , div (JF−1 v1 ) = 0 [Miyakawa1982] and we can decompose the solution v = w + v1 , w = 0 on ∂Ωns Energy balance for w: 1 1 d kJ 2 wk2 |2 dt {z } variation of kinetic energy 1 +2νkJ 2 Dξ (w)k2 | {z } +(J(∇v1 F−1 w), w) | {z } = (ef, w) | {z } energy of viscous dissipation intensification due to b.c. work of ext. forces Dξ (v) = 12 (∇vF−1 + F−T (∇v)T ) A.Danilov, A.Lozovskiy, M.Olshanskii, Yu.Vassilevski. A finite element method for the Navier-Stokes equations in moving domain with application to hemodynamics of the left ventricle. Russian J. Numer. Anal. Math. Modelling, 32, 2017 Stability estimate for the FE solution Energy equality for wh = vh − v1,h : 1 1 12 k 2 2 kJk wh k − kJk−1 whk−1 k2 |2∆t {z } 2 1 2 (∆t) 21 k +2ν Jk2 Dk (whk ) + Jk−1 [wh ]t {z } | 2 | {z } variation of kinetic energy energy of viscous dissipation O(∆t) dissipative term +(Jk (∇v1k F−1 )whk , whk ) {zk } | intensification due to b.c. = (ef k , wk ) | {z h } work of ext. forces A.Danilov, A.Lozovskiy, M.Olshanskii, Yu.Vassilevski. A finite element method for the Navier-Stokes equations in moving domain with application to hemodynamics of the left ventricle. Russian J. Numer. Anal. Math. Modelling, 32, 2017 Stability estimate for the FE solution Stability estimate: C1 k∇v1k k ≤ ν/2: n n k=1 k=1 X X 1 n 2 1 kwh kn + ν ∆tkDk (whk )k2k ≤ kw0 k20 + C ∆tkef k k2 2 2 A.Danilov, A.Lozovskiy, M.Olshanskii, Yu.Vassilevski. A finite element method for the Navier-Stokes equations in moving domain with application to hemodynamics of the left ventricle. Russian J. Numer. Anal. Math. Modelling, 32, 2017 Stability estimate for the FE solution Stability estimate: C1 k∇v1k k ≤ ν/2: n n k=1 k=1 X X 1 n 2 1 kwh kn + ν ∆tkDk (whk )k2k ≤ kw0 k20 + C ∆tkef k k2 2 2 C1 k∇v1k k > ν/2: n X 2C2 1 n 2 ∆tkDk (whk )k2k ≤ e α T kwh kn +ν 2 k=1 n X 1 ∆tkef k k2 kw0 k20 + C 2 ! k=1 A.Danilov, A.Lozovskiy, M.Olshanskii, Yu.Vassilevski. A finite element method for the Navier-Stokes equations in moving domain with application to hemodynamics of the left ventricle. Russian J. Numer. Anal. Math. Modelling, 32, 2017 , Stability estimate for the FE solution Stability estimate: C1 k∇v1k k ≤ ν/2: n n k=1 k=1 X X 1 n 2 1 kwh kn + ν ∆tkDk (whk )k2k ≤ kw0 k20 + C ∆tkef k k2 2 2 C1 k∇v1k k > ν/2: n X 2C2 1 n 2 ∆tkDk (whk )k2k ≤ e α T kwh kn +ν 2 k=1 n X 1 ∆tkef k k2 kw0 k20 + C 2 ! k=1 if (1 − 2C2 ∆t) = α > 0 A.Danilov, A.Lozovskiy, M.Olshanskii, Yu.Vassilevski. A finite element method for the Navier-Stokes equations in moving domain with application to hemodynamics of the left ventricle. Russian J. Numer. Anal. Math. Modelling, 32, 2017 , Application to the left ventricle hemodynamics I Boundary conditions: no-penetration no-slip v = ”do-nothing” ∂u ∂t and Application to the left ventricle hemodynamics ∂u ∂t and I Boundary conditions: no-penetration no-slip v = ”do-nothing” I Computational meshes contain 14033 nodes, 69257 tetrahedra, 88150 edges (320k unknowns) 100 meshes with varying node positions Application to the left ventricle hemodynamics ∂u ∂t and I Boundary conditions: no-penetration no-slip v = ”do-nothing” I Computational meshes contain 14033 nodes, 69257 tetrahedra, 88150 edges (320k unknowns) 100 meshes with varying node positions I Time step between given frames 0.0127 s =⇒ interpolate intermediate meshes with ∆t = 0.0127/20 Application to the left ventricle hemodynamics ∂u ∂t and I Boundary conditions: no-penetration no-slip v = ”do-nothing” I Computational meshes contain 14033 nodes, 69257 tetrahedra, 88150 edges (320k unknowns) 100 meshes with varying node positions I Time step between given frames 0.0127 s =⇒ interpolate intermediate meshes with ∆t = 0.0127/20 I ρf = 103 kg/m , µf = 4 · 10−2 Pa ·s 3 (= 10µblood ) Application to the left ventricle hemodynamics ∂u ∂t I Boundary conditions: no-penetration no-slip v = ”do-nothing” I Computational meshes contain 14033 nodes, 69257 tetrahedra, 88150 edges (320k unknowns) 100 meshes with varying node positions I Time step between given frames 0.0127 s =⇒ interpolate intermediate meshes with ∆t = 0.0127/20 I ρf = 103 kg/m , µf = 4 · 10−2 Pa ·s I Large volume rate =⇒ extremely high influx velocities at the diastole phase 3 (= 10µblood ) 110 100 Volume (ml) 90 80 70 60 50 40 30 20 0 200 400 600 800 Time (ms) and 1000 1200 1400 Application to the left ventricle hemodynamics ∂u ∂t I Boundary conditions: no-penetration no-slip v = ”do-nothing” I Computational meshes contain 14033 nodes, 69257 tetrahedra, 88150 edges (320k unknowns) 100 meshes with varying node positions I Time step between given frames 0.0127 s =⇒ interpolate intermediate meshes with ∆t = 0.0127/20 I ρf = 103 kg/m , µf = 4 · 10−2 Pa ·s I Large volume rate =⇒ extremely high influx velocities at the diastole phase (= 10µblood ) =⇒ need time smoothing for the wall displacements 110 100 90 Volume (ml) I 3 and 80 70 60 A B C D E original 50 40 30 20 0 200 400 600 800 Time (ms) 1000 1200 1400 Application to the left ventricle hemodynamics Conclusions I We proposed unconditionally stable semi-implicit FE schemes for FSI problem and NS eqs in moving domain Conclusions I We proposed unconditionally stable semi-implicit FE schemes for FSI problem and NS eqs in moving domain I The FSI scheme can incorporate diverse elasticity models Conclusions I We proposed unconditionally stable semi-implicit FE schemes for FSI problem and NS eqs in moving domain I The FSI scheme can incorporate diverse elasticity models I Only one linear system is solved per time step Conclusions I We proposed unconditionally stable semi-implicit FE schemes for FSI problem and NS eqs in moving domain I The FSI scheme can incorporate diverse elasticity models I Only one linear system is solved per time step I Ventricle hemodynamics: the NS scheme suffers from convection instability due to large inflows Conclusions I We proposed unconditionally stable semi-implicit FE schemes for FSI problem and NS eqs in moving domain I The FSI scheme can incorporate diverse elasticity models I Only one linear system is solved per time step I Ventricle hemodynamics: the NS scheme suffers from convection instability due to large inflows I We work on its stabilization