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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

Polytropic
None of these
Isothermal
Adiabatic

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Compressors, Gas Turbines and Jet Engines
A jet engine has

Propeller on the top
Propeller at back
Propeller in front
No propeller

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Compressors, Gas Turbines and Jet Engines
The ratio of the indicated power to the shaft power or brake power of the motor or engine required to drive the compressor, is called

Volumetric efficiency
Isothermal efficiency
Mechanical efficiency
Compressor efficiency

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Compressors, Gas Turbines and Jet Engines
The compressor performance at higher altitude compared to sea level will be

Lower
Dependent on other factors
Same
Higher

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

Cool the air
Reduce volume
Decrease the delivery temperature for ease in handling
Cause moisture and oil vapour to drop out

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Compressors, Gas Turbines and Jet Engines
Ram compression in turbojet involves

Increasing speed of incoming air
Lost work
Compression of inlet air
Reduction of speed of incoming air and conversion of part of it into pressure energy

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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