Products of combustion enter a gas turbine with a stagnation pressure of 1.0 MPa and a stagnation

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Products of combustion enter a gas turbine with a stagnation pressure of 1.0 MPa and a stagnation temperature of 750°C, and they expand to a stagnation pressure of 100 kPa. Taking k = 1.33 and R = 0.287 kJ/kg • K for the products of combustion, and assuming the expansion process to be isentropic, determine the power output of the turbine per unit mass flow.
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Thermodynamics An Engineering Approach

ISBN: 978-0073398174

8th edition

Authors: Yunus A. Cengel, Michael A. Boles

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