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A gas turbine operates on a pressure ratio of 6. The inlet air temperature to the compressor is 300 K and the temperature of
A gas turbine operates on a pressure ratio of 6. The inlet air temperature to the compressor is 300 K and the temperature of air entering to the turbine is 580C. If the volume rate of air entering the compressor is 250 m/s, calculate the net power output of the cycle. Also, calculate the efficiency.
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Thermodynamics for Engineers
Authors: Kenneth A. Kroos, Merle C. Potter
1st edition
1133112862, 978-113311286
