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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
After-cooler is used to

Decrease the delivery temperature for ease in handling
Cool the air
Reduce volume
Cause moisture and oil vapour to drop out

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Compressors, Gas Turbines and Jet Engines
Propulsive efficiency is defined as ratio of

Engine output and propulsive power
Propulsive power and fuel input
Thrust power and fuel energy
Thrust power and propulsive power

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

Radial flow compressors
Axial flow compressors
All of these
Pumps

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Compressors, Gas Turbines and Jet Engines
Which is false statement about advantages of multistage compressor in comparison to single stage compressor?

Lower volumetric efficiency
Less power requirement
Better mechanical balance
Less loss of air due to leakage past the cylinder

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Compressors, Gas Turbines and Jet Engines
The effective power of gas turbines is increased by adding the following in compressor

Ammonia and water vapour
Carbon dioxide
Nitrogen
Hydrogen

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Compressors, Gas Turbines and Jet Engines
The capacity of compressor will be highest when its intake temperature is

Lowest
Anything
Atmospheric
Highest

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