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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Losses in a centrifugal compressor are due to

Impeller channel losses
All of the listed here
Inlet losses
Diffuser losses

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Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

Polytropic
Isothermal
None of these
Adiabatic

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

Corrosion resistance
Fatigue
Creep
Toughness

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Compressors, Gas Turbines and Jet Engines
The closed cycle in gas turbines

In never used
Is used when gas is to be burnt
Provides greater flexibility
Provides lesser flexibility

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Compressors, Gas Turbines and Jet Engines
With the decrease in compression ratio, the volumetric efficiency

First decrease and then increase
Does not change
Decreases
Increases

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Compressors, Gas Turbines and Jet Engines
In air breathing jet engine, the jet is formed by expanding

Highly heated atmospheric air
Liquid
Plasma
Solids

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