Combustion Instability Mechanisms in a Pressure-coupled Gas-gas Coaxial Rocket Injector-Reference-Cited by-同舟云学术

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Combustion Instability Mechanisms in a Pressure-coupled Gas-gas Coaxial Rocket Injector

Published:2013-07-12 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
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Author:

Harvazinski Matthew E.¹,Huang Cheng²,Sankaran Venkateswaran¹,Feldman Thomas²,Anderson William²,Merkle Charles²,Talley Doug G.¹

Affiliation:

1. Air Force Research Laboratory

2. Purdue University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-3990

Reference38 articles.

1. 1Harrje, D. and Reardon, F. “Liquid Propellant Rocket Combustion Instability,” Technical Report SP-194, NASA, Washington D.C., 1972.

2. Combustion instabilities - Mating dance of chemical, combustion, and combustor dynamics

3. Combustion Dynamics and Instabilities: Elementary Coupling and Driving Mechanisms

4. 4Culick, F. “Combustion Instabilities in Liquid-Fueled Propulsion Systems an Overview,” Tech. Rep. CP-450, AGARD, 1989.

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