Numerical simulation of 3-D hypersonic Euler flows around space vehicles using adapted finite elements
Author:
Affiliation:
1. Avions Marcel Dassault-Breguet Aviation, Saint-Cloud, France
2. Institut National de Recherche en Informatique et en Automatique, Valbonne, France
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-560
Reference30 articles.
1. A comparison of finite volume flux vector splittings for the Euler equations
2. 2-D and 3-D Euler flow calculations with a second-order accurate Galerkin finite element method
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