a gas turbine power plant operating on brayton cycle with a fuel compressor isentropic efficiency of...

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Mechanical Engineering

a gas turbine power plant operating on brayton cycle with a fuelcompressor isentropic efficiency of 80 and turbine isentropicefficiency of 85 percent and it has a pressure ratio of rp. The gastemperature is 300K at a compressor inlet and 1300K at the turbineinlet. Heat is received from a source of 1700K. Utilizing theair-standard assumption (Hot Assumption) and for pressure ratio rpwhich varies from 3 to 10, determine:

a) The gas temperature at the exits of the compressor and theturbine.

b) the back work ratio

c) the thermal efficiency

d) the second law efficiency

e) exergy destruction for each component

plot your results as functions of gas cycle pressure ratio, anddiscuss the results.

Please solve this using EES software

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