Numerical solution of Space Shuttle Orbiter flow field including real gas effects
Author:
Affiliation:
1. Iowa State University of Science andTechnology, Ames, IA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1984-1747
Reference36 articles.
1. Computation of Space Shuttle Flowfields Using Noncentered Finite-Difference Schemes
2. Journal, Vol. 11, May 1973, pp. 657-664.
3. ments," AIAA Paper 82-0937,June 1982.
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1. Characteristics of the Shuttle Orbiter leeside flow during a re-entry condition;Journal of Spacecraft and Rockets;1994-01
2. Characteristics of the Shuttle Orbiter leeside flow during a reentrycondition;27th Thermophysics Conference;1992-07-06
3. Upwind parabolized Navier-Stokes code for chemically reacting flows;Journal of Thermophysics and Heat Transfer;1990-04
4. Three-dimensional upwind parabolized Navier-Stokes code for real gasflows;Journal of Spacecraft and Rockets;1990-03
5. A three-dimensional upwind parabolized Navier-Stokes code for real gas flows;24th Thermophysics Conference;1989-06-12
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