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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The ratio of the increase in pressure in rotor blades to total increase in pressure in the stage is called

Degree of reaction
Slip factor
Pressure ratio
Pressure coefficient

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Compressors, Gas Turbines and Jet Engines
The absolute pressure of air at the outlet of a compressor is called

Discharge pressure
None of the listed here
Critical pressure
Back pressure

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Compressors, Gas Turbines and Jet Engines
Atmospheric pressure is 1.03 kg/cm and vapour pressure is 0.03 kg/cm. The air pressure will be

0.53 kg/cm²
1.03 kg/cm²
1.06 kg/cm²
1.00 kg/cm²

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Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

256 bar
64 bar
16 bar
1 bar

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Compressors, Gas Turbines and Jet Engines
The ratio of the net work obtained from the gas turbine plant to the turbine work is known as

None of these
Pressure ratio
Work ratio
Compression ratio

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered by the compressor is called

Free air delivery
None of the listed here
Compressor capacity
Swept volume

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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