On the accuracy, stability, and performance of the solution of three-dimensional nonlinear transient aeroelastic problems by partitioned procedures
- 15 April 1996
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 19 references indexed in Scilit:
- Mixed explicit/implicit time integration of coupled aeroelastic problems: Three‐field formulation, geometric conservation and distributed solutionInternational Journal for Numerical Methods in Fluids, 1995
- A scalable Lagrange multiplier based domain decomposition method for time‐dependent problemsInternational Journal for Numerical Methods in Engineering, 1995
- Partitioned procedures for the transient solution of coupled aroelastic problems Part I: Model problem, theory and two-dimensional applicationComputer Methods in Applied Mechanics and Engineering, 1995
- TOP/DOMDEC—A software tool for mesh partitioning and parallel processingComputing Systems in Engineering, 1995
- Matching fluid and structure meshes for aeroelastic computations: A parallel approachComputers & Structures, 1995
- A transient FETI methodology for large‐scale parallel implicit computations in structural mechanicsInternational Journal for Numerical Methods in Engineering, 1994
- Numerical model of unsteady subsonic aeroelastic behaviorAIAA Journal, 1990
- An arbitrary lagrangian-eulerian finite element method for transient dynamic fluid-structure interactionsComputer Methods in Applied Mechanics and Engineering, 1982
- Geometric Conservation Law and Its Application to Flow Computations on Moving GridsAIAA Journal, 1979
- Errata: "Doublet-Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows"AIAA Journal, 1969