Supersonic/Hypersonic Laminar Heating Correlations for Rectangular and Impact-Induced Open and Closed Cavities
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/10.2514/1.36830
Reference41 articles.
1. A REVIEW OF HEAT TRANSFER IN SEPARATED AND REATTACHED FLOWS
2. Assessment of LAURA for Laminar Supersonic Shallow Cavities
3. Computational Aerothermodynamic Assessment of Space Shuttle Orbiter Tile Damage - Open Cavities
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