Enhancements to viscous-shock-layer technique
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Virginia 23681
2. ViGYAN, Inc., Hampton, Virginia 23666
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.25545
Reference35 articles.
1. Hypersonic viscous shock-layer solutions over long slender bodies. I- High Reynolds number flows
2. Hypersonic viscous shock-layer solutions over long slender bodies. II - Low Reynolds number flows
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