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June 8, 2010, 06:25
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pressure drop in gas turbine combustor
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New Member
Join Date: Jun 2010
Posts: 2
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Dear Sir's/Madams
I’m working on my M.S thesis “numerical modeling gas turbine combustor” Combustor contain dilution hole for cooling combustor liner. Problem is that pressure drop in combustor is so much.(pressure drop in experimental case is approximately 0.2 bar while is CFD simulation with Fluent software this lost is about 7 bar. I try with all turbulence models for improvement. But I didn’t find any better results. That’s very kind of you if you help me. best Regards, |
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