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COMPRESSORS, GAS TURBINES AND JET ENGINES

Compressors, Gas Turbines and Jet Engines
In jet propulsion power unit, the inlet duct of diverging shape is used in order to

Convert kinetic energy of air into pressure energy
Provide robust structure
Beautify the shape
Collect more air

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Compressors, Gas Turbines and Jet Engines
Gas turbine cycle with regenerator

Allows high compression ratio
Decreases heat loss is exhaust
Increases thermal efficiency
Allows operation at very high altitudes

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Compressors, Gas Turbines and Jet Engines
The ratio of the net work obtained from the gas turbine plant to the turbine work is known as

None of these
Work ratio
Pressure ratio
Compression ratio

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler work is known as

Polytropic reaction
Work coefficient
Pressure coefficient
Slip factor

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Compressors, Gas Turbines and Jet Engines
The ratio of isentropic work to Euler’s work is known as

Compressor efficiency
Isentropic efficiency
Pressure coefficient
Euler

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