Computation of Rarefied Hypersonic Flows Using Modified Form of Conventional Burnett Equations
Author:
Affiliation:
1. College of Aeronautics and Astronautics, Zhejiang University, 310027 Hangzhou, People’s Republic of China
2. School of Engineering and Applied Science, Washington University in St. Louis, St. Louis, Missouri 63130
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A33059
Reference36 articles.
1. The Distribution of Molecular Velocities and the Mean Motion in a Non-Uniform Gas
2. Stabilization of the Burnett equations and application to hypersonicflows
3. A comparative study of several higher-order kinetic formulations beyond Navier-Stokes for computing the shock structure
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