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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine consists of a

Heating chamber
All of these
Compressor
Cooling chamber

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Compressors, Gas Turbines and Jet Engines
The compressor capacity with decrease in suction temperature

Remain unaffected
Decreases
May increase or decrease depending on compressor capacity
Increases

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Compressors, Gas Turbines and Jet Engines
In multistage compressor, the isothermal compression is achieved by

By constantly cooling the cylinder
By insulating the cylinder
Employing inter-cooler
By running compressor at very slow speed

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Compressors, Gas Turbines and Jet Engines
1 m of air at atmospheric condition weighs approximately

1.3 kg
0.5 kg
1.0 kg
2.2 kg

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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

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

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

Radial flow compressors
Pumps
All of these
Axial flow compressors

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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