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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Maximum delivery pressure is a rotary air compressor is of the order of

25 kg/cm²
10 kg/cm²
6 kg/cm²
16 kg/cm²

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

Propellers
Rockets
Ramjet engine
Turbojet engine

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

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

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Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine plant is ratio of

Work done by turbine and heat supplied
Net work output and work done by turbine
Net work output and heat supplied
Work done by turbine and net work output

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Compressors, Gas Turbines and Jet Engines
The ratio of outlet whirl velocity to blade velocity in case of centrifugal compressor is called

Velocity coefficient
Velocity factor
None of these
Slip factor

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to steam turbine

Has compressor and combustion chamber
Has less efficiency
All of these
Requires less space for installation

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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