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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Actual compression curve is

Better than isothermal and adiabatic
In between isothermal and adiabatic
Same as isothermal
Same as adiabatic

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Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine plant is ratio of

Work done by turbine and net work output
Net work output and work done by turbine
Work done by turbine and heat supplied
Net work output and heat supplied

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Compressors, Gas Turbines and Jet Engines
In jet propulsion power unit, the inlet duct of diverging shape is used in order to

Provide robust structure
Collect more air
Beautify the shape
Convert kinetic energy of air into pressure energy

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Compressors, Gas Turbines and Jet Engines
The air power of the compressor is also known as

None of these
Frictional power
Brake power
Indicated power

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

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

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Compressors, Gas Turbines and Jet Engines
The minimum work required for a three stage reciprocating air compressor is ___ the work required for each stage.

Six times
Double
Equal to
Three times

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