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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The ratio of outlet whirl velocity to blade velocity in case of centrifugal compressor is called

Velocity coefficient
Velocity factor
None of these
Slip factor

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

10 bar
20 bar
30 bar
50 bar

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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

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

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitude will draw

More power
Same power
Less power
More/less power depending on other factors

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Compressors, Gas Turbines and Jet Engines
A gas turbine used in air craft should have

High speed and high h.p.
Small frontal area and high h.p.
Low weight and small frontal area
High h.p. and low weight

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Compressors, Gas Turbines and Jet Engines
Reciprocating air compressor is best suited for

Small quantity of air at low pressure
Large quantity of air at high pressure
Large quantity of air at low pressure
Small quantity of air at high pressure

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