AIAA 2006-1107 Numerical Simulation and Experiment Comparison of Leading-Edge Receptivity of A Mach 5.92 Boundary Layer
44th, Aerospace sciences meeting ; 2006 ; Reno, NV
Aerospace sciences meeting ; 13381-13396
2006-01-01
16 pages
VOL 18 of 24 VOLS
Conference paper
English
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Interaction of an Oblique Shock with a Transitional Mach 5.92 Boundary Layer (AIAA 2016-3647)
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