Interaction between crossing oblique shocks and a turbulent boundarylayer
Author:
Affiliation:
1. Rutgers University, Piscataway, New Jersey 08855
2. Princeton University, Princeton, New Jersey 08540
3. NASA Ames Research Center, Moffett Field, California 94035
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.11164
Reference23 articles.
1. Swept shock/boundary-layer interactions - Tutorial and update
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