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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
The thrust on the rotor in a centrifugal compressor is produced by

None of these
Radial component
Tangential component
Axial component

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Compressors, Gas Turbines and Jet Engines
Pick up the wrong statement about advantages of multistage compression

Better lubrication is possible advantages of multistage
Mechanical balance is better
More loss of air due to leakage past the cylinder
Air can be cooled perfectly in between

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Compressors, Gas Turbines and Jet Engines
The material commonly used for air craft gas turbine is

High alloy steel
Stainless steel
Duralumin
Timken, Haste alloys

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Compressors, Gas Turbines and Jet Engines
In gas turbines, high thermal efficiency is obtained in

Closed cycle & Open cycle
Closed/open depending on other considerations
Closed cycle
Open cycle

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Compressors, Gas Turbines and Jet Engines
There is a certain pressure ratio (optimum) for a gas turbine at which its thermal efficiency is maximum. With increase in turbine temperature, the value of pressure ratio for the peak efficiency would

Remain same
Decrease
Increase
None of these

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