Compressors, Gas Turbines and Jet Engines
Propulsive efficiency is defined as ratio of

Thrust power and propulsive power
Engine output and propulsive power
Propulsive power and fuel input
Thrust power and fuel energy

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Compressors, Gas Turbines and Jet Engines
Inter-cooling in gas turbine results in

Increase in thermal efficiency but decrease in net output
Decrease in both thermal efficiency and net output
Increase in both thermal efficiency and net output
Increase in net output but decrease in thermal efficiency

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