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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The velocity of air entering in a rocket is ___ as compared to an aircraft.

Same
More
Less
Zero

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

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

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered by the compressor is called

None of the listed here
Compressor capacity
Swept volume
Free air delivery

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

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

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Compressors, Gas Turbines and Jet Engines
The maximum compression ratio in an actual single stage axial flow compressor is of the order of

0.045138888888889
0.048611111111111
0.00070833333333333
0.043055555555556

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to steam turbine

Requires less space for installation
All of these
Has less efficiency
Has compressor and combustion chamber

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