The initial design of a fluidically controlled variable geometry fuel injector for gas turbine combustion systems
Author:
Affiliation:
1. Defence Evaluation and Research Agency, Farnborough, United Kingdom
2. Loughborough Univ., United Kingdom
3. Sheffield, Univ., United Kingdom
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-3908
Reference15 articles.
1. NOXFormation in Counter-Flow Opposed-Jet Diffusion CH4/Air Flames.Bonturi ,S, Pourkashanian,M, Williams,A,Oskam, Gand Wilson, C(1996).Combustion Science and Technology, Vol. 1221,pp 217-233.
2. Ignition and PropagationRates forFlames in a FuelMist, FAA-RD-75-155,PolymeropoulosCE, 1975
3. ADoubleActingVariableGeometryCombustion. ASME79-GT-197. Adkins,RCandElsaftawy, A S. 1979.
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1. Air Flow Control by Fluidic Diverter for Low NOx Jet Engine Combustion;1st Flow Control Conference;2002-06-24
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