Air enters an adiabatic gas turbine at 600 kPa and 400 C. It leaves the turbine at

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Air enters an adiabatic gas turbine at 600 kPa and 400° C. It leaves the turbine at atmospheric pressure and a temperature of 140° C. Calculate the specific work output and the isentropic efficiency of this turbine. Assume constant specific heats.
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Thermodynamics for Engineers

ISBN: ?978-1133112860

1st edition

Authors: Kenneth A. Kroos, Merle C. Potter

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