Characterization of the Primary Ignition Process of a Coaxial GH2/LOX Spray-Reference-Cited by-同舟云学术

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Characterization of the Primary Ignition Process of a Coaxial GH2/LOX Spray

Published:2004-01-05 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Aerospace Sciences Meeting and Exhibit
language:
Short-container-title:

Author:

Schmidt Volker¹,Wepler Ulrich¹,Haidn Oskar¹,Oschwald Michael¹

Affiliation:

1. DLR Lampoldshausen

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-1167

Reference19 articles.

1. 2Preclik,D.andSpagna,P."LowFrequencyandHighFrequencyCombustionOscillationPhenomenyinsideaRocketCombustionChamberFed byLiquidorGaseousPropellants," AGARDCP-450,April1989.

2. 3Alliot,P.,Jover,V.,Caruna,J.N.,Dutheil,J.P.,andJuhls,A."Ariane 5CryogenicUpperStagePropulsionSystems," AIAA2001-3259,2001.

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1. Ignition Transition of GOx/Kerosene Spray Combustion with Nitrogen Film Cooling;53rd AIAA/SAE/ASEE Joint Propulsion Conference;2017-07-07

2. A Numerical Study of Oxygen/Hydrogen Mixing and Combustion of a Shear Coaxial Injector;42nd AIAA Thermophysics Conference;2011-06-14

3. CFD Analysis of a Model Combustor Ignition and Comparison with Experimental Results;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08

4. Cryogenic Spray Ignition at High Altitude Conditions;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

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