Flame Flashback in a Supersonic Combustor Fueled by Ethylene with Cavity Flameholder
Author:
Affiliation:
1. Science and Technology on Scramjet Laboratory, National University of Defense Technology, 410073 Changsha, People’s Republic of China
2. Department of Physics, Umeå University, SE-90187 Umeå, Sweden
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/10.2514/1.B35580
Reference15 articles.
1. Supersonic Combustion Experiments with a Cavity-Based Fuel Injector
2. OH PLIF Imaging of Supersonic Combustion Using Cavity Injection
3. Numerical Investigation of Combustion/Shock-train Interactions in a Dual-Mode Scramjet Engine
4. Ram-Scram Transition and Flame/Shock-Train Interactions in a Model Scramjet Experiment
5. Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder
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