Heating measurements on Space Shuttle orbiter models with differentially deflected elevons
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25720
Reference14 articles.
1. ^indlay, J.T. and Compton, H.R. "On the Flight Derived/ Aerodynamic Data Base Performance Comparisons for the NASA Space Shuttle Entries During the Hypersonic Regime," AIAA Paper 83-0115,1983.
2. Tunnel/' NASA TM-74026, 1977.
3. 5Shaefer, W.T. Jr. "Characteristics of Major Active Wind Tunnels at the Langley Research Center," NASA TM X-1130,1965.
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