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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The following property is most important for material used for gas turbine blade

Fatigue
Corrosion resistance
Creep
Toughness

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Compressors, Gas Turbines and Jet Engines
Isothermal compression efficiency can be attained by running the compressor

At zero speed
At average speed
At very slow speed
At very high speed

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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
Less
Same
More/less depending on compressor capacity

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

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

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, an increase in speed at a given pressure ratio causes

Decrease in flow
Increase in efficiency
Increase in flow
Increase in flow and decrease in efficiency

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Compressors, Gas Turbines and Jet Engines
The mass of gas turbine per kW developed is about ________ as that of an I.C. engine.

One-half
One fourth
Same
One sixth

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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