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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

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

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

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

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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

Pressure ratio
None of these
Work ratio
Compression ratio

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

Slip factor
Work coefficient
Polytropic reaction
Pressure coefficient

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

Euler
Isentropic efficiency
Pressure coefficient
Compressor efficiency

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