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Compressors, Gas Turbines and Jet Engines

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

Lower
Same
None of these
Higher

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the ratio of the ________ to the blade velocity is called slip factor.

Inlet whirl velocity
Outlet velocity of flow
Outlet whirl velocity
Inlet velocity of flow

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

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Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In a single phase
In two phases
In the form of air and water mixture
In three phases

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Compressors, Gas Turbines and Jet Engines
In an axial flow compressor, the ratio of pressure in the rotor blades to the pressure rise in the compressor in one stage is known as

Degree of reaction
Pressure coefficient
Slip factor
Work factor

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine gives ________ efficiency as compared to an open cycle gas turbine.

Same
None of these
Higher
Lower

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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