Vibration-dissociation coupling effects on shock standoff distances
Author:
Affiliation:
1. Tohoku Univ., Sendai, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-2499
Reference24 articles.
1. AIAAPaper 97-0563,1997.
2. 2Nonaka, S., and Takayama,K. "BallisticRange MeasurementofShockShapesinNonequilibriwnRegime," AIAAPaper 99-1025,1999.
3. Assessment of two-temperature kinetic model for ionizing air
4. 4Furudate,M.,Nonaka,S.andSawada,K.''Behaviorof Two-TemperatureModel in Intermediate Hypersonic Regime," Journal of Thennophysicsand Heat Transfer, Vol.13,No.4,1999,pp.424-230.
5. 5Furudate,M.,Nonaka,S.andSawada,K."Calculation of ShockShapesover SimpleGeometryin Intermediate HypersonicAirFlow,"AIAAPaper 99-3686,1999.
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1. Ballistic Range Experiment of Shock Stand-Off Distance for Spheres in Air with Flight Speeds Between 5.08 and 6.49 km/s;Shock Wave Interactions;2018
2. Effect of rotational nonequilibrium on shock standoff distances;39th Aerospace Sciences Meeting and Exhibit;2001-01-08
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