Development of GOX/Kerosene Swirl-Coaxial Injector Technology
Author:
Affiliation:
1. University of Alabama in Birmingham
2. Air Force Research Laboratory
3. Sierra Engineering Inc.
4. Convergence Engineering Corp.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-4751
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. Muss,J.A.,Johnson,C.W.,Cheng,G.C.,andCohn, R.K. "Numerical Cold Flow and Combustion Characterization of Swirl Coaxial Injectors," AIAA-2003-0125,2003.
3. Swirl Coaxial Injector Development. Part I: Test Results
4. Swirl Coaxial Injector Development. Part II: CFD Modeling
5. Cheng, G.C. and Farmer, R.C. "CFD Spray Combustion Model for Liquid Rocket Engine InjectorAnalyses,"AIAAPaper2002-0785.
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