Experimental and computational analysis of Shuttle Orbiter hypersonic trim anomaly
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681-0001
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26680
Reference27 articles.
1. Addressing the hypersonic simulation problem
2. Real-gas simulation for the Shuttle Orbiter and planetary entry configurations including flight results
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