Injector Element Instability Mode Assessment in a Laboratory-Scale Burner-Reference-Cited by-同舟云学术

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Injector Element Instability Mode Assessment in a Laboratory-Scale Burner

Published:2008-07-21 Issue: Volume: Page:
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Container-title:44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Byrd Robert,Huynh Huy,Frederick Robert

Publisher

American Institute of Aeronautics and Astronautics

Reference9 articles.

1. 1Lee, K. and “Combustion Stability Assessment of Double Swirl Coaxial Injectors Using Simulant Propellants,” AIAA Joint Propulsion Conference, No. 2005-4443, American Institute of Aeronautics and Astronautics, Tucson, AZ, 2005.

2. 5Cavitt,R.andetal.“OntheLaboratoryScaleSurveyofPentadInjectorStabilityCharacteristics,”AIAAJointPropulsion Conference, No. 2008-5587, American Institute of Aeronautics and Astronautics, Cincinatti, OH, 2008.

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1. Hazard Assessment of Oxygen Propellant Systems at UAHuntsville Propulsion Research Center;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25

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