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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The work ratio of simple gas turbine cycle depends on

All of these
Pressure ratio
Minimum cycle temperature
Maximum cycle temperature

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Compressors, Gas Turbines and Jet Engines
The compressor performance at higher altitude compared to sea level will be

Lower
Same
Higher
Dependent on other factors

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Compressors, Gas Turbines and Jet Engines
Gas turbine blades are given a rake

Equal to zero
Depending on the velocity
Opposite to the direction of motion of blades
In the direction of motion of blades

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor resembles

Reciprocating pump
Turbine
Centrifugal pump
Sliding vane compressor

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Compressors, Gas Turbines and Jet Engines
The pressure ratio in gas turbines is of the order of

0.16736111111111
0.084027777777778
0.37569444444444
2.5423611111111

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Compressors, Gas Turbines and Jet Engines
In a high pressure compressor, the delivery pressure is

5 to 8 bar
10 to 15 bar
1 to 5 bar
8 to 10 bar

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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