Publisher
American Institute of Aeronautics and Astronautics
Reference17 articles.
1. Stability limits of cavity-stabilized flames in supersonic flow
2. 2Quick, A., King, P. I., Gruber M. R., Carter, C. D., Hsu, K. “Upstream Mixing Cavity Coupled with Downstream Flameholding Cavity Behavior in Supersonic Flow,” 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2005-3709, 2005.
3. Figure 8. Stream line of ethylene colored with temperature (F06138AP). Based Flameholder In a Supersonic Flow,” 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2005-4105, 2005.
4. 4Li, J., MaF., Yang, V., Lin, K.CandJackson, T.A. “AComprehensiveStudyofIgnitionTransientinanEthylene-Fueled Scramjet Combustor,” 43th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2007-5025, Cincinnati, OH, July 2007.
5. 5Liu, J., Tam, C.J., Lu, T. and Law, C. K. “Simulations of Cavity-stabilized Flames in Supersonic Flows using Reduced Chemical Kinetics Mechanisms,” 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, AIAA 2006-4863, Sacramento, California, July 2006.
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