Numerical Investigation of Transitional Shock-Wave/Boundary-Layer Interaction in Supersonic Regime
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Title
Numerical Investigation of Transitional Shock-Wave/Boundary-Layer Interaction in Supersonic Regime
Authors
Keywords
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Journal
AIAA JOURNAL
Volume 56, Issue 7, Pages 2712-2724
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2018-04-03
DOI
10.2514/1.j056650
References
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