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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
The pressure ratio for an open cycle gas turbine compared to closed cycle gas turbine of same h.p. is

High
Same
Low/high depending on make and type
Low

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

All of these
Pumps
Radial flow compressors
Axial flow compressors

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Compressors, Gas Turbines and Jet Engines
In a jet propulsion unit, the products of combustion after passing through the gas turbine are discharged into

Atmosphere
Back to the compressor
Discharge nozzle
Vacuum

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to steam turbine

Has less efficiency
Has compressor and combustion chamber
All of these
Requires less space for installation

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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