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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In jet engines, for the efficient production of large power, fuel is burnt in an atmosphere of

Atmospheric air
Oxygen alone
Compressed air
Vacuum

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

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

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

None of these
Decreases
Increases
Does not change

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Compressors, Gas Turbines and Jet Engines
To avoid moisture troubles, the compressed air main line should

Be laid exactly horizontally
Rise gradually towards the point of use
Drop gradually towards the point of use
Be laid vertically

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

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

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is expressed in

kg/m³
kg/m²
m³/kg
m³/min

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