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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The closed cycle in gas turbines

Provides lesser flexibility
Is used when gas is to be burnt
In never used
Provides greater flexibility

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Compressors, Gas Turbines and Jet Engines
Aeroplanes employ following type of compressor

Axial flow
None of these
Centrifugal
Radial flow

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Compressors, Gas Turbines and Jet Engines
When the outlet angle from the rotor of a centrifugal compressor is more than 90°, then the blades are said to be

Forward curved
Backward curved
Radial
None of the listed here

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Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

10 bar
30 bar
50 bar
20 bar

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Compressors, Gas Turbines and Jet Engines
The axial flow compressor is preferred in aircraft gas turbines because of

Higher thrust
High pressure rise
Low frontal area
None of the listed here

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Compressors, Gas Turbines and Jet Engines
The pressure ratio of an ideal vaned compressor with increase in mass flow rate

Remain constant
Decreases
Increases
First decreases and then increases

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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