Numerical Simulations and Planar Laser-Induced Fluorescence Imaging Results of Hypersonic Reactive Flows
Author:
Affiliation:
1. Kyushu University, Fukuoka 812-81, Japan
2. Keio University, Yokohama 223, Japan
3. Stanford University, Stanford, California 94305-3032
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.5558
Reference22 articles.
1. Modeling supersonic combustion using a fully implicit numerical method
2. Computation of unsteady shock-induced combustion using logarithmic species conservation equations
3. Numerical simulation of hypervelocity projectiles in detonable gases
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