Geometric conservation laws for flow problems with moving boundaries and deformable meshes, and their impact on aeroelastic computations-Reference-Cited by-同舟云学术

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Geometric conservation laws for flow problems with moving boundaries and deformable meshes, and their impact on aeroelastic computations

Published:1996-07 Issue:1-2 Volume:134 Page:71-90
ISSN:0045-7825
Container-title:Computer Methods in Applied Mechanics and Engineering
language:en
Short-container-title:Computer Methods in Applied Mechanics and Engineering

Author:

Lesoinne Michel,Farhat Charbel

Publisher

Elsevier BV

Subject

Computer Science Applications,General Physics and Astronomy,Mechanical Engineering,Mechanics of Materials,Computational Mechanics

Reference18 articles.

1. Unsteady Euler airfoil solutions using unstructured dynamic meshes;Batina,1989

2. Arbitrary Lagrangian Eulerian methods, Computational Methods in Mechanics 1, Computational Methods for Transient Analysis;Donéa,1983

3. Unsteady vortex-dominated flows around maneuvering wings over a wide range of Mach numbers;Kandil,1988

4. Transient aeroelastic computations using multiple moving frames of reference;Farhat,1990

5. A structure attached corotational fluid grid for transient aeroelastic computations;Farhat;AIAA J.,1993

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