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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The thrust on the rotor in a centrifugal compressor is produced by

Radial component
Axial component
None of these
Tangential component

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Compressors, Gas Turbines and Jet Engines
The reason for volumetric efficiency of reciprocating compressor being less than 100 percent is

Clearance volume and leakages
All of these
Superheating in compressor
Pressure drop across the valves

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Compressors, Gas Turbines and Jet Engines
Which is false statement about advantages of multistage compressor in comparison to single stage compressor?

Less loss of air due to leakage past the cylinder
Less power requirement
Better mechanical balance
Lower volumetric efficiency

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Compressors, Gas Turbines and Jet Engines
An after-cooler is used to

Cool the air
Cause moisture and oil vapour to drop out
Remove impurities from air
Reduce volume of air

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Compressors, Gas Turbines and Jet Engines
A rocket works with maximum overall efficiency when air craft velocity is equal to the

Jet velocity
Average of the jet velocity
Twice the jet velocity
Half the jet velocity

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Compressors, Gas Turbines and Jet Engines
Fighter bombers use following type of engine

Rocket
Turbo-propeller
Ramjet
Turbojet

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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