Design of Efficient Partitioned Procedures for the Transient Solution of Aeroelastic Problems

DOI10.1080/12506559.2000.10511480zbMath1003.74081OpenAlexW53072800MaRDI QIDQ4762158

Charbel Farhat, Serge Piperno

Publication date: 22 February 2001

Published in: Revue Européenne des Éléments Finis (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/12506559.2000.10511480

zbMATH Keywords

time domainfluid-structure partitioned procedurelarge-scale nonlinear dynamic aeroelasticitystaggering algorithmwingpanel

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Finite difference methods applied to problems in solid mechanics (74S20) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Related Items (13)

A reduced unified continuum formulation for vascular fluid-structure interaction ⋮ Algorithms for strong coupling procedures ⋮ Linearized hydro-elasticity: a numerical study ⋮ Feedback stabilization of a linear hydro-elastic system ⋮ Towards stable coupling methods for high-order discretization of fluid-structure interaction: algorithms and observations ⋮ Mathematical and Numerical Analysis of Some FSI Problems ⋮ Partitioned algorithms for fluid-structure interaction problems in haemodynamics ⋮ Analysis of the immersed boundary method for turbulent fluid-structure interaction with lattice Boltzmann method ⋮ Coupling schemes for incompressible fluid-structure interaction: implicit, semi-implicit and explicit ⋮ Fluid-structure partitioned procedures based on Robin transmission conditions ⋮ Time accurate partitioned algorithms for the solution of fluid-structure interaction problems in haemodynamics ⋮ Artificial added mass instabilities in sequential staggered coupling of nonlinear structures and incompressible viscous flows ⋮ Well-Posedness Analysis for a Linearization of a Fluid-Elasticity Interaction

This page was built for publication: Design of Efficient Partitioned Procedures for the Transient Solution of Aeroelastic Problems