Mixing Enhancement in a Scramjet Combustor Using Fuel Jet Injection Swirl.
Author:
Affiliation:
1. Ottawa University
2. University of Kansas, Lawrence
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-5381
Reference26 articles.
1. Segal, C.,TheScramjet Engine - Processessand Characteristics, CambridgeUniversityPress, NewYork, 2009.
2. Experimental and theoretical investigation of backward-facing step flow
3. Abdel-Salam, T.M., Tiwari, S. N., Chaturvedi, S. K., and Mohieldin, T. O. "Mixing and Combustion in Scramjet Combustor with Raised and Relieved Ramp,"AIAA2000-3709,2000.
4. Jeong, E., O'Byrne, S., Jeung, I., and Houwing, A. F. P. "Supersonic Combustion on Hydrogen Fuel Injection Locations in a CavityBased Combustor," AIAA2008-4576,2008.
5. Ramp Injector Scale Effects on Supersonic Combustion
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