Shock Detachment Distance on Blunt Bodies in Nonequilibrium Flow
Author:
Affiliation:
1. Hassan II University, Casablanca, Morocco
2. Tohoku University, Sendai 980, Japan
3. Université de Provence, Marseille, France
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.17806
Reference19 articles.
1. Non-equilibrium dissociating nitrogen flow over spheres and circular cylinders
2. Non-equilibrium dissociating flow over spheres
3. Experimental Measurement of Shock Detachment Distance on Spheres Fired in Air at Hypervelocities
4. Behavior of Two-Temperature Model in Intermediate Hypersonic Regime
5. Hashimoto, T. "Analytical and Experimental Study of Hypersonic Nozzle Flows in Free Piston Shock Tunnel," Ph.D. Thesis, A0TD1606,Tohoku University, Sendai, Japan,2003.
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