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

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

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Compressors, Gas Turbines and Jet Engines
Volumetric efficiency of a compressor with clearance volume

May increase/decrease depending on compressor capacity
Decreases with increase in compression ratio
Increases with increase in compression ratio
In not dependent upon compression ratio

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