Computation of Hypersonic Shock Wave Flows of Diatomic Gases Using the Generalized Boltzmann Equation
Author:
Affiliation:
1. Washington University in St. Louis
2. Computing Center of Russian Academy of Science
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-4541
Reference8 articles.
1. A set of model cross sections for the Monte Carlo simulation of rarefied real gases: Atom–diatom collisions
2. 4 Carlo direct simulation of rotational relaxation of diatomic molecules using classical trajectory calculations: Nitrogen shock wave
3. Solution of the Wang-Chang-Uhlenbeck master equation
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1. Numerical Solution of Boltzmann Equation;Encyclopedia of Microfluidics and Nanofluidics;2014
2. Computation of Hypersonic Shock Wave Flows of Diatomic Gases and Gas Mixtures Using the Generalized Boltzmann Equation;48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition;2010-01-04
3. Hypersonic Aerodynamics Using BGK Approach for Oscillatory Membrane-on-Ballute with Bow Shock Wave;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
4. A Conservative Numerical Method for Solving the Generalized Boltzmann Equation for an Inert Mixture of Diatomic Gases;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
5. A Two-Level Kinetic Model for Rotational-Translational Relaxations in a Diatomic Gas;40th Thermophysics Conference;2008-06-15
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