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Compressors, Gas Turbines and Jet Engines

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

Less
More
Same
Zero

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Compressors, Gas Turbines and Jet Engines
The compressed air may be used

In starting and supercharging of I.C. engines
All of the listed here
For operating pneumatic drills
In gas turbine plants

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

Centrifugal compressor
Pumps
All of these
Axial compressor

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor has the following advantage over centrifugal compressor

Higher average velocities
Aerofoil blades are used
Larger air handling ability per unit frontal area
Higher pressure ratio per stage

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Compressors, Gas Turbines and Jet Engines
The maximum propulsion efficiency of a turbojet is attained at around following speed

2400 km/hr
550 km/hr
1700 km/hr
1050 km/hr

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Compressors, Gas Turbines and Jet Engines
When air is to be compressed at a high pressure, then it is advantageous to use

Single stage compression
Multistage compression with intercooling
Multistage compression without intercooling
None of these

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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