Characteristics of the Shuttle Orbiter leeside flow during a re-entry condition
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26396
Reference40 articles.
1. Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas Effects
2. Implicit Solution for the Shock-Layer Flow around General Bodies
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