Numerical Cold Flow and Combustion Characterization of Swirl Coaxial Injectors
Author:
Affiliation:
1. Sierra Engineering Inc
2. Sierra Enginering Inc
3. University of Alabama Birmingham
4. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-124
Reference13 articles.
1. Cohn, R.K., Strakey, P.A., Bates, R.W., Talley, D.G., Muss, J.A. and Johnson, C.W. "Swirl Coaxial Injector Development", AIAA-2003-0124, 2003.
2. Swirl Coaxial Injector Development. Part I: Test Results
3. Cheng, G.C. and Farmer, R.C. "CFD Spray Combustion Model for Liquid Rocket Engine InjectorAnalyses,"AIAAPaper2002-0785.
4. Cheng, G.C., Anderson, P.G., and Farmer, R.C. "Development of CFD Model for Simulating Gas/Liquid Injectors in Rocket Engine Design," AIAAPaper97-3228,1997.
5. Farmer, R.C., Cheng, G.C., Trinh, H., and Tucker, K. "A design Tool for Liquid Rocket Engine Injectors,"AIAA2000-3499,2000.
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