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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In turbo fan engine, the jet velocity as compared to turbojet engine is

More
May be less or more depending upon speed
Same
Less

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

Zero
Less
Same
More

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Compressors, Gas Turbines and Jet Engines
In axial flow compressor, exit flow angle deviation from the blade angle is a function of

Space-chord ratio
Blade camber and incidence angle
Blade camber
Blade camber and space-chord ratio

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Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in aeroplanes, is of

Axial flow type
None of these
Radial flow type
Centrifugal type

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Compressors, Gas Turbines and Jet Engines
The inlet pressure is always ___ the discharge pressure.

More than
Less than
None of the listed here
Equal to

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the flow of air is ________ to the axis of compressor.

Perpendicular
None of these
Parallel
Inclined

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