Overview of Combustion Instabilities in Liquid Rocket Engines - Coupling Mechanisms & Control Techniques-Reference-Cited by-同舟云学术

Overview of Combustion Instabilities in Liquid Rocket Engines - Coupling Mechanisms & Control Techniques

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

Bennewitz John W.¹,Frederick Robert A.¹

Affiliation:

1. University of Alabama, Huntsville

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4106

Reference27 articles.

1. Pożarlik, A., Vibro-Acoustical Instabilities Induced by Combustion Dynamics in Gas Turbine Combustors, Doctoral dissertation,University of Twente, 2010.

2. Hubbard, H. H. “Aeroacoustics of Flight Vehicles: Theory & Practice,” Technical Report WRDC-TR-90-3052, National Aeronautics & Space Administration, Langley Research Center, 1991.

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