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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

Produces uniform torque
Can be driven at a very high speed
Has more efficiency
All of the listed here

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Compressors, Gas Turbines and Jet Engines
A rocket works with maximum overall efficiency when air craft velocity is equal to the

Half the jet velocity
Jet velocity
Average of the jet velocity
Twice the jet velocity

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Compressors, Gas Turbines and Jet Engines
In gas turbines, high thermal efficiency is obtained in

Closed cycle & Open cycle
Closed cycle
Open cycle
Closed/open depending on other considerations

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Compressors, Gas Turbines and Jet Engines
Gas turbine blades are given a rake

Equal to zero
In the direction of motion of blades
Depending on the velocity
Opposite to the direction of motion of blades

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

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

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Compressors, Gas Turbines and Jet Engines
The pressure of air at the beginning of the compression stroke is ___ the atmospheric pressure.

Less than
Equal to
More than
None of the listed here

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