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Compressors, Gas Turbines and Jet Engines

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

Increases
Decreases
Remains same
Increases/decreases depending on compressor capacity

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

Centrifugal compressor
Pumps
All of these
Axial compressor

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Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine plant is ratio of

Work done by turbine and net work output
Net work output and work done by turbine
Net work output and heat supplied
Work done by turbine and heat supplied

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Compressors, Gas Turbines and Jet Engines
In turbo fan engine, the jet velocity as compared to turbojet engine is

Less
May be less or more depending upon speed
More
Same

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

at the base
at the tip
in the center
between ~ to i of the blade height

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

Adiabatic efficiency
Isothermal efficiency
Volumetric efficiency
Mechanical efficiency

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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