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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The closed cycle in gas turbines

Provides greater flexibility
Is used when gas is to be burnt
Provides lesser flexibility
In never used

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Compressors, Gas Turbines and Jet Engines
The maximum combustion pressure in gas turbine as compared to I.C. engine is

Less
Depends on other factors
More
Same

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Compressors, Gas Turbines and Jet Engines
Separators in compressor installations are located

Between after-cooler and air receiver
After receiver
Before inter-cooler
After inter-cooler

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

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

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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
Ramjet engine

Is not self operating at zero flight speed
Requires no air for its operation
Produces a jet consisting of plasma
Is self operating at zero flight speed

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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