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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The efficiency of roots blower ________ with the increase in pressure ratio.

Does not change
None of these
Increases
Decreases

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Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine may be improved by

Both (A) and (C) above
Decreasing the compression work
Increasing the turbine work
Increasing the compression work

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Compressors, Gas Turbines and Jet Engines
To avoid moisture troubles, the compressed air main line should

Be laid exactly horizontally
Drop gradually towards the point of use
Be laid vertically
Rise gradually towards the point of use

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Compressors, Gas Turbines and Jet Engines
In axial flow compressor, exit flow angle deviation from the blade angle is a function of

Blade camber and incidence angle
Blade camber
Space-chord ratio
Blade camber and space-chord ratio

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Compressors, Gas Turbines and Jet Engines
A jet engine has

Propeller at back
Propeller on the top
No propeller
Propeller in front

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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
Same
One sixth
One fourth

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