Rotational and vibrational nonequilibrium effects in rarefied hypersonic flow
- 1 October 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Thermophysics and Heat Transfer
- Vol. 4 (4) , 478-484
- https://doi.org/10.2514/3.211
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Rotational–translational energy transfer in rarefied nonequilibrium flowsPhysics of Fluids A: Fluid Dynamics, 1990
- On the computation of shock shapes in nonequilibrium hypersonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Assessment of a two-temperature kinetic model for dissociating and weakly ionizing nitrogenJournal of Thermophysics and Heat Transfer, 1988
- Direct simulation of stagnation streamline flow for hypersonic reentryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Rocket nozzle lip flow by direct simulation Monte Carlo methodJournal of Spacecraft and Rockets, 1986
- Direct simulation of typical AOTV entry flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Statistical collision model for Monte Carlo simulation of polyatomic gas mixtureJournal of Computational Physics, 1975
- Rotational Relaxation in Nonpolar Diatomic GasesPhysics of Fluids, 1970
- Systematics of Vibrational RelaxationThe Journal of Chemical Physics, 1963
- Rotational and Vibrational Relaxation in Diatomic GasesPhysics of Fluids, 1959