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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine may be improved by

Increasing the turbine work
Both (A) and (C) above
Decreasing the compression work
Increasing the compression work

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Compressors, Gas Turbines and Jet Engines
The work-done on a compressor will be minimum if air is taken from

A source at 0° C
The atmosphere
A source of high temperature air
A source of low temperature air

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

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

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Compressors, Gas Turbines and Jet Engines
In a compressor, free air delivered is the actual volume delivered at the stated pressure reduced to

Intake temperature and pressure conditions
20°C and 1 kg/cm²
N.T.P. conditions
0°C and 1 kg/cm²

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Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Decrease of work ratio
Decrease of thermal efficiency
Increase of work ratio
Both (A) and (B) above

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Compressors, Gas Turbines and Jet Engines
The degree of reaction of an axial flow turbine is the ratio of isentropic temperature drop in a blade row to the

Total adiabatic temperature drop
Adiabatic temperature drop in the stage
Total temperature drop
Total temperature drop in the stage

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