Analysis of Compressibility Corrections for Turbulence Models in Hypersonic Boundary-Layer Applications
Author:
Affiliation:
1. China Academy of Aerospace Aerodynamics, 100074 Beijing, People’s Republic of China
2. China Academy of Launch Vehicle Technology, 100076 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference26 articles.
1. Compressibility Considerations for k-w Turbulence Models in Hypersonic Boundary-Layer Applications
2. The Physics of Supersonic Turbulent Boundary Layers
3. WilcoxD. C., Turbulence Modeling for CFD, 3rd ed., DCW Industries., La Cañada, CA, 2006, pp. 239–254.
4. Reynolds-stress and dissipation-rate budgets in a turbulent channel flow
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