Attenuation of Gas Turbine Combustor Pressure Oscillations Using Symmetry Breaking-Reference-Cited by-同舟云学术

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Attenuation of Gas Turbine Combustor Pressure Oscillations Using Symmetry Breaking

Published:2011-01-04 Issue: Volume: Page:
ISSN:
Container-title:49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Cohen Jeffrey¹,Hagen Gregory¹,Banaszuk Andrzej¹,Becz Sandor¹,Mehta Prashant²

Affiliation:

1. United Technologies Research Center

2. University of Illinois, Urbana-Champaign

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-60

Reference11 articles.

1. 3Konrad, W., N. Brehm, F. Kameier, C. Freeman and I.J. Day, "Combustion Instability Investigations On The BR710 Jet Engine," ASMEpaper96-TA-36,1996.

2. Low-Order Modeling of Low-Frequency Combustion Instabilities in AeroEngines

3. Experimental Study on the Role of Entropy Waves in Low-Frequency Oscillations in a RQL Combustor

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