Receptivity of Mach 6 Flow over a Flared Cone to Freestream Disturbance
Author:
Affiliation:
1. University of California Los Angeles
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-253
Reference46 articles.
1. 96-0782, January 1996.
2. No. 12,December 1996.
3. Wind Tunnel," AIAA Paper 97-1819, 1997.
4. AIAAPaper 2001-0211, January 2001.
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