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Compressors, Gas Turbines and Jet Engines

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

20 bar
10 bar
30 bar
50 bar

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

Velocity factor
Velocity coefficient
None of these
Slip factor

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

Lower power consumption per unit of air delivered
Higher volumetric efficiency
Decreased discharge temperature
All of these

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Compressors, Gas Turbines and Jet Engines
The air entry velocity m a rocket as compared to aircraft is

More
Same
Less
Zero

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Compressors, Gas Turbines and Jet Engines
A turboprop is preferred to turbojet because

It can fly at high elevations
It has high propulsive efficiency at high speeds
It can fly at supersonic speeds
It has high power for take off

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler’s work is known as

Compressor efficiency
Pressure coefficient
Euler
Isentropic efficiency

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