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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

Toughness
Fatigue
Creep
Corrosion resistance

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Compressors, Gas Turbines and Jet Engines
Pick up the wrong statement about advantages of multistage compression

Better lubrication is possible advantages of multistage
Air can be cooled perfectly in between
More loss of air due to leakage past the cylinder
Mechanical balance is better

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Compressors, Gas Turbines and Jet Engines
The efficiency of a jet engine is higher at

High altitudes
Low altitudes
Low speeds
High speeds

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Compressors, Gas Turbines and Jet Engines
Inter cooling in compressors

Enables compression in two stages
Is the standard practice for big compressors
Results in saving of power in compressing a given volume to given pressure
Cools the delivered air

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

Cooling chamber
All of these
Heating chamber
Compressor

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Compressors, Gas Turbines and Jet Engines
The ratio of the discharge pressure to the inlet pressure of air is called

Expansion ratio
Volumetric efficiency
Compressor efficiency
Compression ratio

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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