A Two-Level Kinetic Model for Rotational-Translational Relaxations in a Diatomic Gas
Author:
Affiliation:
1. Russian Academy of Science
2. Washington University in St. Louis
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-3932
Reference7 articles.
1. Computation of Hypersonic Shock Wave Flows of Diatomic Gases Using the Generalized Boltzmann Equation
2. Chen, R., Agarwal, R.K. and Cheremisin, F.G. "ComputationofHypersonic Flowof a Diatomic Gas in rotational Non-equilibrium Past a Blunt Body Using the generalized Boltzmann Equation," AIAA Paper 2007-4550,39thAIAAThermophysicsConference,Miami,FL,25-28June2007.
3. Solution of the Wang-Chang-Uhlenbeck master equation
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1. Computation of Hypersonic Flow past a Blunt Body in an Inert Binary Gas Mixture in Rotational Non-equilibrium Using the Generalized Boltzmann Equation;51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2013-01-05
2. Computation of Shock Waves in Inert Diatomic Gas Mixtures in Non-equilibrium Using the Generalized Boltzmann Equation;43rd AIAA Thermophysics Conference;2012-06-25
3. Computation of Shock Waves in Inert Binary Gas Mixtures in Non-equilibrium Using the Generalized Boltzmann Equation;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09
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