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Compressors, Gas Turbines and Jet Engines

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

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

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

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

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

Lower power consumption per unit of air delivered
All of these
Higher volumetric efficiency
Decreased discharge temperature

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine works on

Rankine cycle
Ericsson cycle
Joule cycle
Carnot cycle

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Compressors, Gas Turbines and Jet Engines
A jet engine works on the principle of conservation of

Linear momentum
Flow
Mass
Energy

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Compressors, Gas Turbines and Jet Engines
As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio

Increases
Decreases
Remain same
First increases and then decreases

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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