Active Combustion Control for a Low-Emissions Aircraft Engine Combustor Prototype: Experimental Results-Reference-Cited by-同舟云学术

Active Combustion Control for a Low-Emissions Aircraft Engine Combustor Prototype: Experimental Results

Published:2013-07 Issue:4 Volume:29 Page:991-1000
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

DeLaat John C.¹,Kopasakis George¹,Saus Joseph R.¹,Chang Clarence T.¹,Wey Changlie²

Affiliation:

1. Controls and Dynamics Branch, NASA John H. Glenn Research Center at Lewis Field, Cleveland, Ohio 44135

2. Vantage Partners, LLC, Brook Park, Ohio 44142

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B34653

Reference30 articles.

1. LefebvreA. H., Gas Turbine Combustion, 2nd ed., Taylor and Francis, Philadelphia, PA, 1999, pp. 260–267.

2. Progress in Astronautics and Aeronautics;Zinn B. T.,2005

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

4. LieuwenT. C.YangV., Combustion Instabilities in Gas Turbine Engines: Operational Experience, Fundamental Mechanisms, and Modeling, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2005, pp. 29–112, Chaps. 2–8.

5. SchadowK.YangV.CulickF.RosfjordT.SturgessG.ZinnB. “Active Combustion Control for Propulsion Systems,” AGARD, Rept. 820, Sept. 1997.

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