Effect of reaction mechanism in shock-induced combustion simulations
Author:
Affiliation:
1. Florida, Univ., Gainesville; Wilfred Baker Engineering, Inc., San Antonio, TX
2. Florida, Univ., Gainesville
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-274
Reference57 articles.
1. Review of shock-induced supersonic combustion research and hypersonic applications
2. Numerical simulation of hypervelocity projectiles in detonable gases
3. 5Lee, S. and Deiwert, G.S."Calculation of Nonequilibrium Hydrogen-Air Reactions With Implicit Flux Vector Splitting Method,"AIAA Paper 89-1700,1989.
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