Reviews of Studies of Boundary Layer Transition in Hypersonic Flows Over Axisymmetric and Elliptic Cones Conducted in the CUBRC Shock Tunnels
Author:
Affiliation:
1. CUBRC
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-782
Reference18 articles.
1. Reda, D.C. "Boundary Layer Transition Experiments on Sharp, Slender Cones in Supersonic Free Flight,"AIAAPaperNo.78-1129,July1978.
2. Muir, J.F. and Trujillo, A.A. "Experimental Investigation of the Effects of Nose Bluntness, Freestream Unit Reynolds Number and Angle of Attack on Cone Boundary Layer Transition at a Mach Number of 6,"AIAA Paper72-216,January1972.
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