Laminar boundary layer stability experiments on a cone at Mach 8. V - Tests with a cooled model
Author:
Affiliation:
1. USAF, Wright Research and Development Center, Wright-Patterson AFB, OH
2. Calspan Corp., Arnold Engineering Development Center, Arnold AFB, TN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-1895
Reference23 articles.
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