Hypersonic Mach number and real gas effects on Space Shuttle Orbiteraerodynamics
Author:
Affiliation:
1. Calspan Field Services, Inc., Arnold Air Force Station, TN
2. Arnold Engineering Development Center, Arnold Air Force Station, TN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-343
Reference10 articles.
1. Space Shuttle entry aerodynamic comparisons of flight 1 with preflight predictions
2. A preliminary correlation of the orbiter stability and control aerodynamics from the first two Space Shuttle flights /STS-1 & 2/ with preflight predictions
3. 4ELarconi, F., Salas, M., and Yaeger, L. S. "Development of a Computer Code far Calculating the Steady SuperIHypersonic Inviscid Flow Around Real Configurations,"NASA CR-2675, April 1976.
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