LU-SGS implicit scheme for entry vehicle flow computation and comparison with aerodynamic data
Author:
Affiliation:
1. Lockheed Engineering and Sciences Co., Houston, TX
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-2671
Reference31 articles.
1. kke. H.C. 'OnSymmetric and UpwindTVD Schemes,' NASA TM-86842, 1985.
2. Uniformly High-Order Accurate Nonoscillatory Schemes. I
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