Nonequilibrium effects for hypersonic transitional flows using continuum approach
Author:
Affiliation:
1. Stanford University, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-461
Reference20 articles.
1. Rarefied Gas Dynamics
2. Molecular Gas Dynamics
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