Calculation of nonequilibrium hydrogen-air reactions with implicit flux vector splitting method
Author:
Affiliation:
1. Eloret Institute, Sunnyvale, CA
2. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-1700
Reference21 articles.
1. A survey of modern research in hypersonic aerodynamics
2. Drummond, J.P., Rogers, R.C. and Hussaini, M.Y. "ADetailedNumerical ModelofaSupersonicReacting MixingLayer,"AIAAPaperNo. 86-1427,June 1986.
3. Jachimowski,C.J. "AnAnalyticalStudyoftheHydrogen-Air Reaction Mechanism With Application toScramjet Combustion,"NASATP2791,February 1988.
4. COMPLEX CHEMICAL KINETICS IN SUPERSONIC NOZZLE FLOW
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