An interactive adaptive remeshing algorithm for the two-dimensional Euler equations
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg
2. George Washington University, Washington, DC
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1990-331
Reference18 articles.
1. The use of direct solvers for compressible flow computations
2. The design and application of upwind schemes on unstructured meshes
3. LGhner, R.=ImprovedAdaptiveRefinement Strategies for Finite Element Aerodynamic Cornputations", AIAA Paper 86-0499, January 1986.
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3. A fully implicit Navier-Stokes algorithm using an unstructured grid and flux difference splitting;31st Aerospace Sciences Meeting;1993-01-11
4. Upwind scheme for solving the Euler equations on unstructured tetrahedral meshes;AIAA Journal;1992-01
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