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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In a single phase
In three phases
In two phases
In the form of air and water mixture

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Compressors, Gas Turbines and Jet Engines
Euler's equation is applicable for

All of these
Pumps
Centrifugal compressor
Axial compressor

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Compressors, Gas Turbines and Jet Engines
The air is delivered ________ in one revolution in case of a three lobbed rotor.

Four times
Three times
Six times
Two times

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Compressors, Gas Turbines and Jet Engines
Ratio of indicated H.P. and brake H.P. is known as

Adiabatic efficiency
Mechanical efficiency
Volumetric efficiency
Isothermal efficiency

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered by the compressor is called

Swept volume
Compressor capacity
Free air delivery
None of the listed here

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Compressors, Gas Turbines and Jet Engines
For an irreversible gas turbine cycle, the efficiency and work ratio both depend on

Both pressure ratio and maximum cycle temperature
Pressure ratio alone
Maximum cycle temperature alone
Minimum cycle temperature alone

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