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Compressors, Gas Turbines and Jet Engines

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

Radial flow compressors
Axial flow compressors
All of these
Pumps

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Compressors, Gas Turbines and Jet Engines
The area of actual indicator diagram on an air compressor as compared to area of ideal indicator diagram is

More
More/less depending on compressor capacity
Same
Less

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

500°C
200°C
1000°C
700°C

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor has the following advantage over centrifugal compressor

Higher pressure ratio per stage
Aerofoil blades are used
Larger air handling ability per unit frontal area
Higher average velocities

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor

Increases with increase in compression ratio
Decreases with increase in compression ratio
Increases with decrease in compression ratio
Decreases with decrease in compression ratio

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Compressors, Gas Turbines and Jet Engines
The compression ratio for the compressor is always _________ unity.

None of these
Less than
More than
Equal to

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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