Compressors, Gas Turbines and Jet Engines
The pressure and temperature conditions of air at the suction of compressor are

Pressure slightly less than atmospheric and temperature slightly more than atmospheric
Slightly more than atmospheric
Atmospheric
Slightly less than atmospheric

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Compressors, Gas Turbines and Jet Engines
The overall isothermal efficiency of compressor is defined as the ratio of

Isothermal h.p. to the BHP of motor
Work to compress air isothermally to work for actual compression
Isothermal h.p. to adiabatic h.p.
Power to drive compressor to isothermal h.p.

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