Direct Numerical Simulation Database for Supersonic and Hypersonic Turbulent Boundary Layers
Author:
Affiliation:
1. Missouri University of Science and Technology, Rolla, Missouri 65409
2. NASA Langley Research Center, Hampton, Virginia 23681
Funder
Langley Research Center
Office of Cyberinfrastructure
Division of Chemical, Bioengineering, Environmental, and Transport Systems
Office of Naval Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J057296
Reference55 articles.
1. SmitsA. J.DussaugeJ. P., Turbulent Shear Layers in Supersonic Flow, 2nd ed., Springer–Verlag, New York, 2006, pp. 119–134.doi:10.1007/b137383
2. WalzA., Boundary Layers of Flow and Temperature, MIT Press, Cambridge, MA, 1969, pp. 27–75.
3. Reynolds analogies and experimental study of heat transfer in the supersonic boundary layer
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