Correlations to Predict the Streamwise Influence Regions in Supersonic Turbulent Flows
Author:
Affiliation:
1. Iowa State University, Ames, Iowa 50011
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.9322
Reference30 articles.
1. Parabolized Navier-Stokes Algorithm for Solving Supersonic Flows with Upstream Influences
2. RTO WG 10 - CFD validation for shock wave turbulent boundary layer interactions
3. Hypersonic shock/boundary-layer interaction database
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