LES for Supersonic Ramp Control Flow Using MVG at M=2.5 and Re?=1440
Author:
Affiliation:
1. University of Texas, Arlington
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-592
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5. 5Charles W. Pitt Ford and Holger Babinsky, "Micro-Ramp Control for Oblique Shock Wave/Boundary Layer Interaction," AIAApaper2007-4115.
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