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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

Has more efficiency
Can be driven at a very high speed
Produces uniform torque
All of the listed here

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Compressors, Gas Turbines and Jet Engines
If the flow of air through the compressor is perpendicular to its axis, then it is a

Axial flow compressor
Centrifugal compressor
Turbo compressor
Reciprocating compressor

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Compressors, Gas Turbines and Jet Engines
A large clearance volume in a reciprocating compressor results in

Lower suction pressure
Reduced volume flow rate
Increased volume flow rate
Lower delivery pressure

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

at the tip
at the base
in the center
between ~ to i of the blade height

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Compressors, Gas Turbines and Jet Engines
The efficiency of roots blower ________ with the increase in pressure ratio.

Does not change
None of these
Increases
Decreases

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

Higher
Lower
Same
Dependent on other factors

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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