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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

Tangential component
Axial component
Radial component
None of these

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Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

None of these
Adiabatic
Polytropic
Isothermal

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

Zero
Same
More
Less

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Compressors, Gas Turbines and Jet Engines
Euler's equation is applicable for

Pumps
All of these
Axial compressor
Centrifugal compressor

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

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

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Compressors, Gas Turbines and Jet Engines
The stagnation pressure rise in a centrifugal compressor takes place

In the inlet guide vanes only
In the diffuser only
In the diffuser and impeller
In the impeller only

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