Turbulence amplification in shock-wave boundary-layer interaction
Author:
Affiliation:
1. NASA Langley Research Center, Hampton, Va.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.7954
Reference27 articles.
1. A theory of turbulent flow round two-dimensional bluff bodies
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