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Radiation-Spray Coupling for Realistic Flow ConfigurationsThree Large Eddy Simulations (LES) for a lean-direct injection (LDI) combustor are performed and compared. In addition to the cold flow simulation, the effect of radiation coupling with the multi-physics reactive flow is analyzed. The flame let progress variable approach is used as a subgrid combustion model combined with a stochastic subgrid model for spray atomization and an optically thin radiation model. For accurate chemistry modeling, a detailed Jet-A surrogate mechanism is utilized. To achieve realistic inflow, a simple recycling technique is performed at the inflow section upstream of the swirler. Good comparison is shown with the experimental data mean and root mean square profiles. The effect of combustion is found to change the shape and size of the central recirculation zone. Radiation is found to change the spray dynamics and atomization by changing the heat release distribution and the local temperature values impacting the evaporation process. The simulation with radiation modeling shows wider range of droplet size distribution by altering the evaporation rate. The current study proves the importance of radiation modeling for accurate prediction in realistic spray combustion configurations, even for low pressure systems.
Document ID
20110020835
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
El-Asrag, Hossam
(Massachusetts Inst. of Tech. Cambridge, MA, United States)
Iannetti, Anthony C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
October 1, 2011
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/TM-2011-217111
E-17787
Report Number: NASA/TM-2011-217111
Report Number: E-17787
Funding Number(s)
WBS: WBS 984754.02.07.03.19.02
Distribution Limits
Public
Copyright
Public Use Permitted.
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