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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

25 kg/cm²
6 kg/cm²
16 kg/cm²
10 kg/cm²

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Compressors, Gas Turbines and Jet Engines
The area of actual indicator diagram on an air compressor as compared to area of ideal indicator diagram is

More
Same
More/less depending on compressor capacity
Less

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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
Slip factor
None of these

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

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

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitudes will require ___ power.

More
Same
None of the listed here
Less

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Compressors, Gas Turbines and Jet Engines
Stalling of blades in axial flow compressor is the phenomenon of

Air stream not able to follow the blade contour
Motion of air at sonic velocity
Unsteady periodic and reversed flow
Air stream blocking the passage

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