Shock Wave Boundary Layer Interaction at High Flap Angles and High Incidence of Space Vehicles in Hypersonic Flow
25th, AIAA applied aerodynamics conference ; 2007 ; Miami, FL
2007-01-01
113 pages
Held on CD-ROM. Papers in range 2007 3800 to 4620 with gaps; Held in e-store (RMS)
Conference paper
English
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