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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
The work done per unit mass of air in compression will be least when 'n' is equal to

1.4
1.2
1
1.3

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Compressors, Gas Turbines and Jet Engines
Which is false statement about air receivers?

These act as reservoir to take care of sudden demands
These knock out some oil and moisture
These increase compressor efficiency
These are used to dampen pulsations

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 5°C increase in atmospheric temperature

0.05
0.005
0.001
0.01

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Compressors, Gas Turbines and Jet Engines
Gas turbines use following type of air compressor

Axial flow type
Reciprocating type
Centrifugal type
Lobe type

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Compressors, Gas Turbines and Jet Engines
The work-done on a compressor will be minimum if air is taken from

A source at 0° C
A source of high temperature air
A source of low temperature air
The atmosphere

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