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Air enters the compressor of a simple gas turbine at p1 = 14 lbf/in2, T1 =...

Air enters the compressor of a simple gas turbine at p1 = 14 lbf/in2, T1 = 520°R. The isentropic efficiencies of the compressor and turbine are 83 and 87%, respectively. The compressor pressure ratio is 16 and the temperature at the turbine inlet is 2500°R. The volumetric flow rate of the air entering the compressor is 9000 ft3/min. Use an air-standard analysis.

Determine all temperatures at each state.

A) Determine the net power developed, in Btu/h. (Already did this part, answer is  4.636E+6 Btu/H)

B) Determine the thermal efficiency of the cycle

C) the temperature at the turbine exit in °R (Temp. at compressor exit is 1277  oR)

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