Mach 6 Quiet Tunnel Laminar to Turbulent Investigation of a Generic Hypersonic Forebody
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-3575
Reference12 articles.
1. 2Schneider,S.P."FlightDataforBoundary-Layer Transition at Hypersonic and Supersonic Speeds,"JournalofSpacecraft and Rockets,Vol. 36, No.1,1999, pp.8-20.
2. Hypersonic Boundary-Layer Trip Development for Hyper-X
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