Hypersonic Mach number and real gas effects on Space Shuttle Orbiteraerodynamics
- 1 March 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 21 (2), 136-141
- https://doi.org/10.2514/3.8624
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Laminar viscous flow-field prediction of Shuttle-like vehicle aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- A preliminary correlation of the orbiter stability and control aerodynamics from the first two Space Shuttle flights /STS-1 & 2/ with preflight predictionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Space Shuttle entry aerodynamic comparisons of flight 1 with preflight predictionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Flow-Field Measurements in the Windward Surface Shock Layer of Space Shuttle Orbiter Configurations at Mach Number 8Published by Defense Technical Information Center (DTIC) ,1975