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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The maximum delivery pressure in a rotary air compressor is

50 bar
30 bar
20 bar
10 bar

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Compressors, Gas Turbines and Jet Engines
Pick up wrong statement. Surging phenomenon in centrifugal compressor depends on

Change in load
Stagnation pressure at the outlet
Pressure ratio
Mass flow rate

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

Has more efficiency
Can be driven at a very high speed
Produces uniform torque
All of the listed here

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Compressors, Gas Turbines and Jet Engines
The maximum compression ratio in an actual single stage axial flow compressor is of the order of

0.00070833333333333
0.043055555555556
0.045138888888889
0.048611111111111

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Compressors, Gas Turbines and Jet Engines
Gas turbine cycle with regenerator

Increases thermal efficiency
Allows operation at very high altitudes
Decreases heat loss is exhaust
Allows high compression ratio

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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