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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Gas turbine works on

Brayton or Atkinson cycle
Carnot cycle
Rankine cycle
Ericsson cycle

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Compressors, Gas Turbines and Jet Engines
The pressure ratio of an ideal vaned compressor with increase in mass flow rate

Remain constant
Decreases
Increases
First decreases and then increases

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

50: 1.
30: 1
7: 1
15: 1

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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
Diffuser inlet radius
Impeller outlet radius
Impeller inlet radius

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

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

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of compressor with increase in compression ratio will

Decrease
Remain same
May increase or decrease depending on clearance volume
Increase

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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