Numerical solution of Space Shuttle Orbiter flowfield including real-gas effects
- 1 May 1986
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 23 (3) , 264-272
- https://doi.org/10.2514/3.25108
Abstract
No abstract availableKeywords
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