Transition Effect on Shock Wave / Boundary Layer Interaction at M=1.47
Author:
Affiliation:
1. Russian Academy of Sciences
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-1974
Reference7 articles.
1. J.E. Green. Laminar Flow Control - Back to the Future? AIAA Paper 2008-3738.
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