LOX/GH2 Shear Coaxial Injector Atomization Studies: Effect of Recess and Non-Concentricity
Author:
Affiliation:
1. Pennsylvania State University
2. Pratt & Whitney Rocketdyne
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-571
Reference34 articles.
1. Rocket engine coaxial injector liquid/gas interface flow phenomena
2. 2Herding, G., Snyder, R., Scouflaire, P., Rolon, C., and Candel, S. "Flame Stabilization in Cryogenic Propellant Combustion,"26thSymposium(International)onCombustion,TheCombustionInstitute,1996,pp.2041-2047.
3. 3Villermaux,E."MixingandSprayFormationinCoaxialJets,"JPP,Vol.14,No.5,Sep-Oct1998,pp.807-817.
4. Experimental Investigation of Shear Coaxial Cryogenic Jet Flames
5. Modeling of supercritical vaporization, mixing, and combustion processes in liquid-fueled propulsion systems
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