Swirl Cup Modeling Part VII: Partially-Premixed Laminar Flamelet Model Validation and Simulation of a Single-Cup Combustor with Gaseous n-Heptane
Author:
Affiliation:
1. GE Aircraft Engines
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-488
Reference31 articles.
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2. Held,T.J. andMongia,H.C."Applicationofa Partially Premixed Laminar Flamelet Model to a Low Emissions GasTurbineCombustor",ASME Paper98-GT-217(1998).
3. Held,T.J. andMongia,H.C."Emissions ModelingofGas Turbine CombustorsUsing a Partially-Premixed Laminar Flamelet Model", AIAAPaper98-3950(1998).
4. Held,T.J.,Mueller, M.A.,Li, S.C.,and Mongia, H. C. "AData-Driven ModelforNOx,CO,and UHCEmissions fora Dry Low EmissionsGas TurbineCombustor",AIAAPaper2001-3425 (2001).
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