Hypersonic flow over a blunt body with plasma injection
Author:
Affiliation:
1. USAF, Wright-Patterson AFB, OH
2. Wright State Univ., Dayton, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-344
Reference30 articles.
1. Experiments on shock stand-off distance in non-equilibrium flow
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