Boundary-Layer Transition on Cones at Angle of Attack in a Mach-6 Quiet Tunnel
Author:
Affiliation:
1. Purdue University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2010-1062
Reference59 articles.
1. 2Holden, M. S. "Experimental Studies of the Effects of Asymmetric Transition on the Aerothermal Characteristicsof HypersonicBlunted Slender Cones,"AIAAPaper85-0325,January1985.
2. 3Schneider, Steven P. "Hypersonic Laminar-Turbulent Transition on Circular Cones and Scramjet Forebodies," Progress in AerospaceSciences,Vol.40,February2004,pp.1-50.
3. 5Bertin, John J., Hypersonic Aerothermodynamics, American Institute of Aeronautics and Astronautics, Washington,D.C.,1994.
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