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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the highest Mach number leading to shock wave in the fluid flow occurs at

Impeller outlet radius
Diffuser outlet radius
Diffuser inlet radius
Impeller inlet radius

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Compressors, Gas Turbines and Jet Engines
In a high pressure compressor, the delivery pressure is

5 to 8 bar
8 to 10 bar
10 to 15 bar
1 to 5 bar

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Compressors, Gas Turbines and Jet Engines
The mass of gas turbine per kW developed is about ________ as that of an I.C. engine.

One-half
One sixth
One fourth
Same

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Compressors, Gas Turbines and Jet Engines
An after-cooler is used to

Cool the air
Reduce volume of air
Cause moisture and oil vapour to drop out
Remove impurities from air

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Compressors, Gas Turbines and Jet Engines
The efficiency and work ratio of a gas turbine plant can be increased by

Injecting water in/around combustion chamber
Adding heat exchanger
Reheating the air after partial expansion in the turbine
All of these

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of compressor with increase in compression ratio will

Remain same
May increase or decrease depending on clearance volume
Increase
Decrease

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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