Assessment of thermochemical nonequilibrium and slip effects for Orbital Reentry Experiment (OREX)
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[1] R. Gupta,et al. Reevaluation of flight-derived surface recombination-rate expressions for oxygen and nitrogen , 1996 .
[2] G. Bird. Molecular Gas Dynamics and the Direct Simulation of Gas Flows , 1994 .
[3] Robert C. Blanchard,et al. Three-dimensional rarefied flow simulations for the Aeroassist Flight Experiment vehicle , 1991 .
[4] James N. Moss,et al. Nonequilibrium effects for hypersonic transitional flows , 1987 .
[5] Y. Inouye,et al. OREX flight - quick report and lessons learned , 1995 .
[6] T. Akimoto,et al. Computational and experimental studies on an electrostatic probe and catalytic effect sensor for a reentry experiment , 1993 .
[7] L. Jacchia,et al. Thermospheric temperature, density, and composition: New models , 1977 .
[8] R. N. Gupta,et al. Hypersonic low-density solutions of the Navier-Stokes equations with chemical nonequilibrium and multicomponent surface slip , 1986 .
[9] Takashi Abe,et al. Experimental Investigation of Air Radiation from Behind a Strong Shock Wave , 1998 .
[10] R. Gupta. Stagnation flowfield analysis for an aeroassisted vehicle , 1993 .
[11] W. L. Jones,et al. Electrostatic-probe measurements of plasma parameters for two reentry flight experiments at 25000 feet per second , 1972 .
[12] R. Gupta,et al. Viscous shock-layer study of thermochemical nonequilibrium , 1996 .