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Gas Turbine Combustion Systems Gas Turbine minCpTin (min+mF)CpTout Shaft power mFqR comb Consider Centaur and Mercury Known P ratio = 10 TIT = 1350 K Compressor Eff. = 0.86 Turbine Eff. = 0.89 Heat exchanger effectiveness = 0.8 Ambient temperature and pressure, 300 K, 1 bar Specific heat Cp = 1.005 kJ/Kg-K Specific heat ratio = 1.4 Calculate (a) Compressor outlet temperature (b) Turbine …