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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Water is injected in gas turbine cycle to

Control temperature
Control fire hazards
Increase efficiency
Control output of turbine

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Compressors, Gas Turbines and Jet Engines
Aeroplanes employ following type of compressor

Radial flow
None of these
Axial flow
Centrifugal

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

Same as isothermal
Better than isothermal and adiabatic
In between isothermal and adiabatic
Same as adiabatic

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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
0.048611111111111
0.045138888888889

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the highest Mach number leading to shock wave in the fluid flow occurs at

Diffuser outlet radius
Impeller outlet radius
Diffuser inlet radius
Impeller inlet radius

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Compressors, Gas Turbines and Jet Engines
The output of a gas turbine is 300 KW and its efficiency is 20 percent, the heat supplied is

6000 KW
15 KW
150 KW
600 KW

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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