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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A closed gas turbine in which fuel is burnt directly in the air is not possible because of

High specific volume
Paucity of O2
High friction losses
Increasing gas temperature

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor falls roughly as follows for every 5°C increase in atmospheric temperature

0.005
0.001
0.01
0.05

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Compressors, Gas Turbines and Jet Engines
A compressor mostly used for supercharging of I.C. engines is

Axial flow compressor
Roots blower
Reciprocating compressor
Radial flow compressor

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Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Decrease of work ratio
Decrease of thermal efficiency
Both (A) and (B) above
Increase of work ratio

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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

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

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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