Question: For an ideal gas with constant specific heats show that the compressor and turbine isentropic efficiencies may be written as The states 1 and 2

For an ideal gas with constant specific heats show that the compressor and turbine isentropic efficiencies may be written as

For an ideal gas with constant specific heats show that

The states 1 and 2 represent the compressor inlet and exit states and the states 3 and 4 represent the turbine inlet and exit states.

(TVT.) _ I P4P1 and (T/T1)-1 ,- Tr

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