Calculation of intermediate hypersonic flow using multi-temperature model
Author:
Affiliation:
1. Tohoku Univ., Sendai, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-343
Reference14 articles.
1. onaka, S., and Takayama,K. "Ballistic Range Measurementof Shock Shapesin Nonequilibrium Regime,"AIAA Paper99-1025, 1999.
2. Assessment of two-temperature kinetic model for ionizing air
3. 4Park c. "Validation of CFD Codes for Real-gas Regime0022, AIAA Paper97-2530,1997.
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