High-speed Turbulence Modeling of Shock-Wave/ Boundary-Layer Interaction
Author:
Affiliation:
1. Universita di Roma "La Sapienza", Rome 00184, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference28 articles.
1. Dilatation dissipation: The concept and application in modeling compressible mixing layers
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