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Category > Management Posted 03 Nov 2017 My Price 5.00

simple gas turbine

Solve Problem 9.35 on a cold air-standard basis with specific heats evaluated at 520°R.

Problem 9.35:

Air enters the compressor of a simple gas turbine at p1 14 lbf/in.2 , T1 = 520°R. The isentropic efficiencies of the compressor and turbine are 83 and 87%, respectively. The compressor pressure ratio is 14 and the temperature at the turbine inlet is 2500°R. The net power developed is 5 × 106 Btu/h. On the basis of an air-standard analysis, calculate

(a) the volumetric flow rate of the air entering the compressor, in ft3 /min.

(b) the temperatures at the compressor and turbine exits, each in °R.

(c) the thermal efficiency of the cycle.

 

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Maurice Tutor
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Status NEW Posted 03 Nov 2017 10:11 PM My Price 5.00

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