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Compressors, Gas Turbines and Jet Engines

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

1.3
1.4
1
1.2

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

Same
Zero
Less
More

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

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

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, an increase in speed at a given pressure ratio causes

Increase in flow and decrease in efficiency
Increase in efficiency
Increase in flow
Decrease in flow

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Compressors, Gas Turbines and Jet Engines
In multistage compressor, the isothermal compression is achieved by

Employing inter-cooler
By constantly cooling the cylinder
By insulating the cylinder
By running compressor at very slow speed

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Compressors, Gas Turbines and Jet Engines
Euler's equation is applicable for

Pumps
All of these
Axial compressor
Centrifugal compressor

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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