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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency, even when running at high speed, can be approached by using

Fully insulating the cylinder
Cold water spray
Multistage compression
Both (A) and (B) above

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Compressors, Gas Turbines and Jet Engines
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Higher
Can't be compared
Equal
Lower

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Compressors, Gas Turbines and Jet Engines
Reheating in a multistage expansion gas turbine ________ compressor work.

Decreases
Increases
None of these
Has no effect on

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

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

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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

Isothermal efficiency
Volumetric efficiency
Compressor efficiency
Mechanical efficiency

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Compressors, Gas Turbines and Jet Engines
In jet propulsion power unit, the inlet duct of diverging shape is used in order to

Provide robust structure
Convert kinetic energy of air into pressure energy
Beautify the shape
Collect more air

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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