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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The net work input required for compressor with increase in clearance volume

Decreases
Increases/decreases depending on compressor capacity
Remains same
Increases

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Compressors, Gas Turbines and Jet Engines
The stagnation pressure rise in a centrifugal compressor takes place

In the impeller only
In the diffuser only
In the inlet guide vanes only
In the diffuser and impeller

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Compressors, Gas Turbines and Jet Engines
The blades of gas turbine are made of

Carbon steel
Stainless steel
High alloy steel
High nickel alloy

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

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

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

High speeds
Low altitudes
High altitudes
Low speeds

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Compressors, Gas Turbines and Jet Engines
Ramjet engine

Is self operating at zero flight speed
Requires no air for its operation
Produces a jet consisting of plasma
Is not self operating at zero flight speed

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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