A shock-layer theory based on thirteen-moment equations and DSMC calculations of rarefied hypersonic flows
Author:
Affiliation:
1. Southern California, University, Los Angeles, CA
2. Vigyan Research Associates, Inc, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1991-783
Reference64 articles.
1. paper 89-1663 (1989)
2. Conf. Hypersonic Aerodynamics,Sept. 4-6, 1989,Univ.
3. Manchester, Manchester,England, pp. 15-1 thru 15-16
4. (1989)
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