Parallel heterogeneous algorithms for the solution of three-dimensional transient coupled aeroelastic problems-Reference-Cited by-同舟云学术

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Parallel heterogeneous algorithms for the solution of three-dimensional transient coupled aeroelastic problems

Published:1995-04-10 Issue: Volume: Page:
ISSN:
Container-title:36th Structures, Structural Dynamics and Materials Conference
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Author:

Farhat C,Lesoinne M,Chen P,Lanteri S

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1995-1290

Reference27 articles.

1. An arbitrary lagrangian-eulerian finite element method for transient dynamic fluid-structure interactions

2. Unsteady Euler airfoil solutions using unstructured dynamic meshes

3. Structure-attached corotational fluid grid for transient aeroelasticcomputations

4. A new strategy for finite element computations involving moving boundaries and interfaces—The deforming-spatial-domain/space-time procedure: I. The concept and the preliminary numerical tests

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1. Multidisciplinary Design Aspects;Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles;2009

2. Flow-Structure Interactions on Helicopter Rotors in Forward Flight;GAMM-Mitteilungen;2005-06

3. Application of a three-field nonlinear fluid–structure formulation to the prediction of the aeroelastic parameters of an F-16 fighter;Computers & Fluids;2003-01

4. Navier–Stokes solvers in European aircraft design;Progress in Aerospace Sciences;2002-11

5. Aeroelastic computations using algebraic grid motion;The Aeronautical Journal;2002-10

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