On numerical solutions of Burnett equations for hypersonic flow past2-D circular blunt leading edges in continuum transition regime
Author:
Affiliation:
1. California Univ., Los Angeles
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-3092
Reference30 articles.
1. v versity Press, 1960. [4] 11-S Tsien. Superaerodynamics,mechanics of rarefied gases. I.of Aero. Sci.,13(12),Dcc. 1946.
2. On Higher Order Hydrodynamic Theories of Shock Structure
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