Numerical study of shock-wave/boundary-layer interactions with bleed
Author:
Affiliation:
1. Carnegie Mellon University, Pittsburgh, Pennsylvania 15213
2. 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/10.2514/3.11698
Reference7 articles.
1. Shock wave/turbulent boundary layer interaction and its control
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