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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The thrust on the rotor in a centrifugal compressor is produced by

Radial component
None of these
Tangential component
Axial component

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

Two or more air streams
Solid fuel firing
One air stream
No air stream

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Compressors, Gas Turbines and Jet Engines
In multistage compressor, the isothermal compression is achieved by

By running compressor at very slow speed
By insulating the cylinder
Employing inter-cooler
By constantly cooling the cylinder

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Compressors, Gas Turbines and Jet Engines
For speed above 3000 km/hour, it is more advantageous to use

Ramjet engine
Turbojet engine
Rockets
Propellers

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Compressors, Gas Turbines and Jet Engines
The performance of air compressor at high altitudes will be ________ as compared to that at sea level.

Same
Lower
Higher
None of these

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitude will draw

Same power
Less power
More power
More/less power depending on other factors

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