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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Losses in a centrifugal compressor are due to

Diffuser losses
Impeller channel losses
Inlet losses
All of the listed here

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Compressors, Gas Turbines and Jet Engines
The weight per horse power ratio for gas in Turbine as compared to I.C. engine and steam turbine is

Higher
Lower
None of these
Same

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Compressors, Gas Turbines and Jet Engines
In a double acting compressor, the air is compressed

In two cylinders
In two cylinders on both sides of the piston
In a single cylinder on both sides of the piston
In one cylinder

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Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

50 bar
20 bar
30 bar
10 bar

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Compressors, Gas Turbines and Jet Engines
For slow speed large capacity compressor, following type of valve will be best suited

Any of the above
Disc or feather type
Mechanical valve of the Corliss, sleeve, rotary or semi rotary type
Poppet valve

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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