Maurice Tutor

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  • MCS,PHD
    Argosy University/ Phoniex University/
    Nov-2005 - Oct-2011

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    Phoniex University
    Oct-2001 - Nov-2016

Category > Management Posted 10 Oct 2017 My Price 4.00

simple gas turbine

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.

Answers

Maurice Tutor
(5)
Status NEW Posted 10 Oct 2017 10:10 PM My Price 4.00

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