Fully coupled implicit method for thermochemical nonequilibrium air at suborbital flight speeds
Author:
Affiliation:
1. NASA Ames Research Center, Moffett Field, California
2. MCAT Institute, Moffett Field, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26205
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4. 5Candler, G. V. "On the Computation of Shock Shapes in Nonequilibrium Hypersonic Flows,"AIAA Paper 89-0312, Jan. 1989.
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