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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

500°C
1000°C
200°C
700°C

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor resembles

Sliding vane compressor
Reciprocating pump
Centrifugal pump
Turbine

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Compressors, Gas Turbines and Jet Engines
The degree of reaction of an axial flow turbine is the ratio of isentropic temperature drop in a blade row to the

Total temperature drop in the stage
Adiabatic temperature drop in the stage
Total temperature drop
Total adiabatic temperature drop

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency for reciprocating air compressors is about

70 to 90%
60 to 70%
10 to 40%
40 to 60%

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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
600 KW
15 KW
150 KW

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Compressors, Gas Turbines and Jet Engines
If the flow of air through the compressor is parallel to its axis, then the compressor is

Centrifugal compressor
Reciprocating compressor
Axial flow compressor
Turbo compressor

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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