Shear coaxial injector atomization in a LOX/GH2 propellant rocket
Author:
Affiliation:
1. Pennsylvania State Univ., University Park
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-2775
Reference3 articles.
1. August, 1993. [71 Reitz, R. D., and Bracco, F. V.
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1. High Speed Visualization of LOX/GH2 Rocket Injector Flowfield: Hot-Fire and Cold-Flow Experiments;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25
2. GOX/Methane Injector Effects on Combustion Efficiency;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21
3. LOX/GH2 Shear Coaxial Injector Atomization Studies: Effect of Recess and Non-Concentricity;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08
4. LOX/GH2 Shear Coaxial Injector Atomization Studies at Large Momentum Flux Ratios;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09
5. Shear and Swirl Coaxial Injector Studies of LOX/GCH4 Rocket Combustion Using Non-Intrusive Laser Diagnostics;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09
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