Viscous shock layer at the stagnation point with nonequilibrium air chemistry
Author:
Affiliation:
1. Sandia Laboratories, Albuquerque, N.Mex.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.5528
Reference40 articles.
1. Shock Wave and Flow Field Development in Hypersonic Re-Entry
2. Nonequilibrium hypersonic stagnation flow with arbitrary surface catalycity including low reynolds number effects
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