Hypersonic shock-wave turbulent-boundary-layer interaction flows - Experiment and computation
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-1760
Reference18 articles.
1. Experience with two-layer models combining the k-epsilon model with a one-equation model near the wall
2. The prediction of laminarization with a two-equation model of turbulence
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