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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
An air compressor may be controlled by

Clearance control
Any one of the above
Throttle control
Blow off control

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

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

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

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

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Compressors, Gas Turbines and Jet Engines
The mass of gas turbine per kW developed is about ________ as that of an I.C. engine.

One-half
One fourth
Same
One sixth

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Compressors, Gas Turbines and Jet Engines
The air entry velocity m a rocket as compared to aircraft is

Zero
Less
More
Same

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Compressors, Gas Turbines and Jet Engines
Losses in a centrifugal compressor are due to

All of the listed here
Impeller channel losses
Diffuser losses
Inlet losses

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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