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[American Institute of Aeronautics and Astronautics Flight Simulation Technologies Conference and Exhibit - Dayton,OH,U.S.A. (17 September 1990 - 19 September 1990)] Flight Simulation Technologies Conference and Exhibit - The effect of separation on turbulent boundary layer characteristicsover a smooth surface at Mach 6.0

✍ Scribed by DISIMILE, P.; SCAGGS, N.

Book ID: 121036870
Publisher: American Institute of Aeronautics and Astronautics
Year: 1990
Weight: 563 KB
Category: Article
DOI: 10.2514/6.1990-3028

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