Flowfield and vehicle parameter influence on results of engineering aerothermal methods
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23665
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26203
Reference36 articles.
1. Theory of Stagnation Point Heat Transfer in Dissociated Air
2. Laminar Heat Transfer Around Blunt Bodies in Dissociated Air
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