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Compressors, Gas Turbines and Jet Engines

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

Same
One sixth
One fourth
One-half

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Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

16 bar
1 bar
256 bar
64 bar

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Compressors, Gas Turbines and Jet Engines
Diffuser in a compressor is used to

Convert kinetic energy into pressure energy
Make the flow streamline
Increase velocity
Convert pressure energy into kinetic energy

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Compressors, Gas Turbines and Jet Engines
The degree of reaction is usually kept ________ for all types of axial flow compressors.

0.5
0.2
0.3
0.4

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the flow of air is ________ to the axis of compressor.

Parallel
None of these
Perpendicular
Inclined

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

In between isothermal and adiabatic
Same as isothermal
Same as adiabatic
Better than isothermal and adiabatic

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