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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency can be attained by running the compressor

At very high speed
At zero speed
At average speed
At very slow speed

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Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Decrease of work ratio
Both (A) and (B) above
Decrease of thermal efficiency
Increase of work ratio

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Compressors, Gas Turbines and Jet Engines
Mining industry usually employs following motive power

C. electric motor
Compressed air
Diesel engine
Petrol engine

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor has the following advantage over centrifugal compressor

Larger air handling ability per unit frontal area
Higher pressure ratio per stage
Higher average velocities
Aerofoil blades are used

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Compressors, Gas Turbines and Jet Engines
The volume of air sucked by the compressor during its suction stroke is called

Swept volume
Compressor capacity
Free air delivery
None of these

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Compressors, Gas Turbines and Jet Engines
A jet engine has

Propeller on the top
No propeller
Propeller in front
Propeller at back

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