pressure drop in gas turbine combustor
Iím working on my M.S thesis ďnumerical modeling gas turbine combustorĒ
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 didnít find any better results.
Thatís very kind of you if you help me.
You should put CFD related threads into the appropriate forum section.
In you case the FLUENT forum.
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