Active Combustion Control for Aircraft Gas-Turbine Engines - Experimental Results for an Advanced, Low-Emissions Combustor Prototype-Reference-Cited by-同舟云学术

Active Combustion Control for Aircraft Gas-Turbine Engines - Experimental Results for an Advanced, Low-Emissions Combustor Prototype

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Delaat John¹,Kopasakis George¹,Saus Joseph¹,Chang Clarence¹,Wey Changlie²

Affiliation:

1. NASA Glenn Research Center

2. ASRC Aerospace Corporation

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-783

Reference25 articles.

1. Lefebvre,A.H."GasTurbineCombustion",2ndedition,Taylor&Francis,1999.

2. Zinn,B.T.;andLieuwen,T.C."CombustionInstabilities:BasicConcepts,"CombustionInstabilitiesinGasTurbineEngines: OperationalExperience, Fundamental Mechanisms, and Modeling, edited by T. Lieuwenand V. Yang, Progress inAstronautics and Aeronautics, AIAA, Reston,VA, 2005, Chap1, pp. 3-26.

3. Challenges and Progress in Controlling Dynamics in Gas Turbine Combustors

4. Schadow,K.;Yang,V.,Culick,F.;Rosfjord,T.;Sturgess,G.;Zinn,B."ActiveCombustionControlforPropulsionSystems", AGARD Report 820, September1997.

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