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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
1 m of air at atmospheric condition weighs approximately

2.2 kg
0.5 kg
1.3 kg
1.0 kg

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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
Inclined
Parallel

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Compressors, Gas Turbines and Jet Engines
The stagnation pressure rise in a centrifugal compressor takes place

In the diffuser and impeller
In the inlet guide vanes only
In the impeller only
In the diffuser only

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

Axial flow compressors
Radial flow compressors
All of these
Pumps

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Compressors, Gas Turbines and Jet Engines
The air is delivered ________ in one revolution in case of a three lobbed rotor.

Two times
Six times
Three times
Four times

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Compressors, Gas Turbines and Jet Engines
The efficiency of roots blower ________ with the increase in pressure ratio.

Increases
Decreases
None of these
Does not change

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