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[American Institute of Aeronautics and Astronautics 21st Fluid Dynamics, Plasma Dynamics and Lasers Conference - Seattle,WA,U.S.A. (18 June 1990 - 20 June 1990)] 21st Fluid Dynamics, Plasma Dynamics and Lasers Conference - A numerical study of supersonic flow over a compression corner with different incoming boundary-layer profiles

✍ Scribed by HOLMES, S.; SQUIRE, L.

Book ID: 121036331
Publisher: American Institute of Aeronautics and Astronautics
Year: 1990
Weight: 609 KB
Category: Article
DOI: 10.2514/6.1990-1453

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