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Compressors, Gas Turbines and Jet Engines

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

Hydrogen
Nitrogen
Carbon dioxide
Ammonia and water vapour

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

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

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Compressors, Gas Turbines and Jet Engines
Gas turbine blades are given a rake

Opposite to the direction of motion of blades
Equal to zero
In the direction of motion of blades
Depending on the velocity

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Compressors, Gas Turbines and Jet Engines
Cylinder clearance in a compressor should be

About 100% of swept volume
As large as possible
As small as possible
About 50% of swept volume

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

Zero
More
Less
Same

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the flow of air is ________ to the axis of compressor.

Perpendicular
None of these
Inclined
Parallel

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