exit temperature/mass flow rate/cycle efficiency

Project Description:

consider an ideal simple gas turbine cycle. for a net power output of 10,000 horse power, an inlet air temperature of t1=500 r, an inlet turbine temperature of t3=2000 r, and a compression ratio of 10, calculate: (assume constant specific heat of cp=0.24 btu/lbm.r and k=1.4)

i.)the compressor exit temperature (t2) and the turbine exit temperature (t4),
ii.)the air mass flow rate, and
iii.)the cycle efficiency.
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Price Type: Negotiable

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