Computational Analyses of Complex Flows for Realistic Reusable Launch and Reentry Vehicles
Author:
Affiliation:
1. The Boeing Company
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2734
Reference16 articles.
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2. Chen, C. L., Ramakrishnan, S., Szema, K. Y., Dresser, H. S., and Rajagopal, K. "Multi-zonal Navier-Stokes Solutions for theMulti-bodySpaceShuttleConfiguration,"AIAA90-0434, Jan.1990.
3. Ramakrishnan, S., Chen, C. L. and Dominik, D. F. "Scale Effects on the Flow Past the Mated Space Shuttle Configuration,"AIAA92-2680,Jan. 1992.
4. Chen, C. L., Ramakrishnan, S., Ota, D.A., Rajagopal, K., and Wisneski, J. "Computation of Underexpanded Solid Rocket Plumeand its Effects on theMated ShuttleConfiguration,"AIAA92-2612, June1992.
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