Computation of inviscid flowfield around 3-D aerospace vehicles and comparison with experimental and flight data
Author:
Affiliation:
1. Lockheed Engineering & Sciences Co., Houston, TX
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-885
Reference20 articles.
1. Gnoffo, P. A, "An Unwind-Biased, Point-Implicit Relaxation Algorithm for Viscous Compressible Perfect-GasFlow,"NASATp-2953,Oct. 1989.
2. "Calculations of Inviscid Flow Over Shuttle-Like Vehiclesat High Angles of Attack and Comparisons WithExperimentalData,"NASA Tp-2103,1983.
3. Tam, L. T. "LU-SGS Implicit Scheme for Entry Vehicle Flow Computation and Comparison with AerodynamicData,''AIAA-92-2671-CP,June 1992.
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