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COMPRESSORS, GAS TURBINES AND JET ENGINES

Compressors, Gas Turbines and Jet Engines
Ratio of indicated h.p. to shaft h.p. in known as

Volumetric efficiency
Compressor efficiency
Isothermal efficiency
Mechanical efficiency

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Compressors, Gas Turbines and Jet Engines
Ratio of indicated H.P. and brake H.P. is known as

Adiabatic efficiency
Mechanical efficiency
Volumetric efficiency
Isothermal efficiency

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Compressors, Gas Turbines and Jet Engines
The output of a gas turbine is 300 KW and its efficiency is 20 percent, the heat supplied is

6000 KW
600 KW
15 KW
150 KW

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Compressors, Gas Turbines and Jet Engines
Reheating in a gas turbine

Increases the compressor work
Increases the thermal efficiency
Increases the turbine work
Decreases the thermal efficiency

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Compressors, Gas Turbines and Jet Engines
In axial flow compressor, exit flow angle deviation from the blade angle is a function of

Space-chord ratio
Blade camber and space-chord ratio
Blade camber and incidence angle
Blade camber

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