Calculation of shock shapes over simple geometry in intermediate hypersonic air flow
Author:
Affiliation:
1. Tohoku Univ., Sendai, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-3686
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4. I 4Anderson, J. D. Jr., Hypersonic and High TimperatureGasDynamics,McGraw-Hill, 1989,pp.548- sqo.
5. , `Furudate,M., Nonaka,S.andSawada,K. "Behavior of Two-TemperatureModel in Intermediate Hypersonic Regime,"AIAA Paper99-0223,1999.
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