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Air modeled as an ideal gas enters a turbine operating at steady state at 1040 K, 278 kPa and exits and 120 kPa. The mass flow rate is 5.5 kg/s, and the power developed is 1120kW. Stray heat transfer and kinetic and potential energy effects are negligible. Determine (a) the temperature of the air at the turbine exit, in K, and (b) the isentropic turbine efficiency.
Air modeled as an ideal gas enters a turbine operating at steady state at 1040 K, 278 kPa and exits and 120 kPa. The mass flow rate is 5.5 kg/s, and the power developed is 1120kW. Stray heat transfer and kinetic and potential energy effects are negligible. Determine (a) the temperature of the air at the turbine exit, in K, and (b) the isentropic turbine efficiency.
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