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Keyword [exit temperature]
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1. Numerical Research On Mixing Characteristic Of R0110 Heavy Gas Turbine Combustor
2. Research On The Flow Field Mixing Characteristics In The Combustor Excited By Synthetic Jets
3. Effects of fuel nozzle condition upon gas turbine combustion chamber exit temperature profiles
4. Effects of combustion chamber geometry upon exit temperature profiles
5. Experimental Investigation of the Effect of Engine Representative Combustor Exit Temperature Profile and Disc Cavity Leakage Flow on the Film Cooling of Contoured Hub Endwall of a High Pressure Gas Turbine Rotor Cascade
6. Effects of inlet distortion on gas turbine combustion chamber exit temperature profiles
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