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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
30 bar
50 bar
10 bar

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Compressors, Gas Turbines and Jet Engines
In an axial flow compressor, the ratio of pressure in the rotor blades to the pressure rise in the compressor in one stage is known as

Slip factor
Work factor
Pressure coefficient
Degree of reaction

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

Same as isothermal
Same as adiabatic
In between isothermal and adiabatic
Better than isothermal and adiabatic

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

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

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Compressors, Gas Turbines and Jet Engines
With the decrease in compression ratio, the volumetric efficiency

First decrease and then increase
Does not change
Increases
Decreases

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

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

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