Using ideal gas model and considering the specific heat

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A turbine operating at steady state receives air at a pressure of P1=3.0 Bars and a temperature T1=390K. Air exits the turbine at pressure of P2=1.0Bars. The work developed by the turbine is measured as 74Kj/Kg of air flowing through the turbine. The turbine operates adiabatically and changes i Kinetic and potential energy between inlet and outlet can be neglected. Using ideal gas model and considering the specific heat variation with temperature, determine the turbine isentropic (adiabatic) efficiency.

Reference no: EM13637981

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