OH* Chemiluminescence in a Multipoint Combustion System: Steady State and Limit Cycle Behavior
Author:
Affiliation:
1. University of Cincinnati
2. United Technologies Aerospace Systems
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-560
Reference30 articles.
1. 1Tacina, K.M., Lee, C-M., and Wey, C. "NASA Glenn High pressure Low NOx Emissions Research," NASA/TM-2008-214974.
2. 2Tacina, R., Laing, P.,Wey, C., and Mansour,A. "SectorTestsofa LowNOx, Lean-Direct-Injection, Multipoint Integrated Module Combustor Concept,"ASME Turbo Expo2002,Amsterdam, Netherlands, GT-2002-30089
3. 3Tacina, R., Mao C-P. and Wey, C. "Experimental Investigation of a Multiplex Fuel Injector Module for Low Emission Combustors," AIAA2003-0827.
4. 4Tacina, R., Wey, C., Laing, P. and Mansour, A. "A Low NOx Lean Direct Injection, Multipoint Integrated Module Combustor Concept forAdvancedAircraftGasTurbines," NASA/TM-2002-211347.
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