Computation of Hypersonic Shock Waves in Inert Gas Mixtures Using the Generalized Boltzmann Equation
Author:
Affiliation:
1. Washington University in Saint Louis
2. Russian Academy of Sciences
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3134
Reference9 articles.
1. Conservative evaluation of Boltzmann collision integral in discrete ordinates approximation
2. Solution of the Wang-Chang-Uhlenbeck master equation
3. A Conservative Numerical Method for Solving the Generalized Boltzmann Equation for an Inert Mixture of Diatomic Gases
4. 4Kosuge, S., Aoki, K., and Takata, S. "Shock-Wave Structure for a Binary Gas Mixture: Finite-Difference Analysis of the BoltzmannEquation forHard-Sphere Molecules.EuropeanJournal of MechanicsB - Fluids, Vol.20:2001, pp.87-126.
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