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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The most efficient method of compressing air is to compress it

Isochronically
Isothermally
Isentropically
Adiabatically

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Compressors, Gas Turbines and Jet Engines
The ratio of the increase in pressure in rotor blades to total increase in pressure in the stage is called

Degree of reaction
Pressure coefficient
Pressure ratio
Slip factor

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Compressors, Gas Turbines and Jet Engines
The area of actual indicator diagram on an air compressor as compared to area of ideal indicator diagram is

Same
Less
More/less depending on compressor capacity
More

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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

256 bar
64 bar
1 bar
16 bar

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Compressors, Gas Turbines and Jet Engines
Aeroplanes employ following type of compressor

Centrifugal
Radial flow
Axial flow
None of these

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Compressors, Gas Turbines and Jet Engines
The thrust of a jet propulsion power unit can be increased by

All of these
Injecting water into the compressor
Burning fuel after gas turbine
Injecting ammonia into the combustion chamber

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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