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    A gas turbine takes in air at 300 K and discharges it to the

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    A gas turbine takes in air at 300 K and discharges it to the combustion chamber at 620 K. See attached file for full problem description with diagram.


    a/ the theoretical compressor power input
    b/ the theoretical turbine power output
    c/ the thermal efficiency of the turbine
    d/ the work ratio of the turbine

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    Solution Preview

    Please see the attached file.

    There is an error in the problem. The Cp value of 1.13 kJ/kg.K is for the combustion process, not the compression.

    Draw a simplified diagram:

    a. The theoretical compressor power input is equal to the power that the ...

    Solution Summary

    The solution provides step-by-step instructions and calculations for the gas turbine problem.