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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The weight per horse power ratio for gas in Turbine as compared to I.C. engine and steam turbine is

Higher
Lower
Same
None of these

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Compressors, Gas Turbines and Jet Engines
To avoid moisture troubles, the branch connections from compressed air lines should be taken from

Right side of main
Left side of main
Bottom side of main
Top side of main

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

Ramjet engine
Propellers
Turbojet engine
Rockets

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Compressors, Gas Turbines and Jet Engines
Inter-cooling in multistage compressors is done

To minimize the work of compression
To cool the air during compression
To cool the air at delivery
To enable compression in two stages

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Compressors, Gas Turbines and Jet Engines
Separators in compressor installations are located

After receiver
Before inter-cooler
Between after-cooler and air receiver
After inter-cooler

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Compressors, Gas Turbines and Jet Engines
The type of rotary compressor used in aeroplanes, is of

Centrifugal type
None of these
Radial flow type
Axial flow type

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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