Navier-Stokes simulation of the Space Shuttle launch vehicle flight transonic flowfield using a large scale chimera grid system
Author:
Affiliation:
1. Lockheed Engineering and Sciences Co., Houston, TX
2. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-1860
Reference40 articles.
1. "Results of Cold Plume Test of the 0.010-Scale Model (75-OTS) in the NASAIAmes Research Center 11x 11Foot Wind Tunnel(IA-300): DMS-DR2511, NASA CR 167,September 1983.
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