Solution-Temperature of hot gas entering turbine

Temperature of hot gas entering turbine

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Reference no: EM133215439

Natural gas is burned in the combustor of the NGCC's gas turbine with excess air to ensure complete combustion and to limit the temperature of the hot gas entering the turbine. In addition, liquid water is injected into the combustor to reduce the combustion temperature and increase the mass flow of gas through the turbine. Based on the fuel and flue gas compositions given, calculate:

The excess air (in %) fed to the combustor and

The water injection rate (in kg/hr).

Reference no: EM133215439

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Temperature of hot gas entering turbine : NGCC's gas turbine with excess air to ensure complete combustion and to limit the temperature of the hot gas entering the turbine

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Temperature of hot gas entering turbine

Reference no: EM133215439

Reference no: EM133215439

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