Analysis of a Single H2-air Pulse Detonation in a Supersonic Combustor
Author:
Affiliation:
1. Air Force Research Laboratory
2. Embry-Riddle Aeronautical University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1028
Reference14 articles.
1. Malo-Molina, F. J., et.al."NumericalAnalysis of a DirectConnect Supersonic Combustor,"AIAApaper 2010-403, Jan2011.
2. Malo-Molina, F. J., et. al. "Three Dimensional Analysis of a Fully Coupled Hypersonic Air-breathing Inlet-Combustor Flowpath," AIAApaper2010-412,Jan2010.
3. Experimental investigation of kerosene fuel combustion in supersonic flow
4. Ortweth, P., et.al. "Experimental and Numerical Investigation of Hydrogen and Ethylene Combustion in a Mach 3-5 Channel with a Single Injector,"AIAA-96-3245,July1996.
5. Flame-Holding Configurations for Kerosene Combustion in a Mach 1.8 Airflow
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