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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Ratio of indicated H.P. and brake H.P. is known as

Volumetric efficiency
Adiabatic efficiency
Mechanical efficiency
Isothermal efficiency

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Compressors, Gas Turbines and Jet Engines
A turboprop is preferred to turbojet because

It can fly at high elevations
It has high power for take off
It can fly at supersonic speeds
It has high propulsive efficiency at high speeds

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Compressors, Gas Turbines and Jet Engines
Euler's equation is applicable for

Pumps
All of these
Centrifugal compressor
Axial compressor

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Compressors, Gas Turbines and Jet Engines
The net work input required for compressor with increase in clearance volume

Increases
Remains same
Decreases
Increases/decreases depending on compressor capacity

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Compressors, Gas Turbines and Jet Engines
The air power of the compressor is also known as

Frictional power
Brake power
Indicated power
None of these

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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
64 bar
256 bar
1 bar

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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