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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

Solid fuel firing
No air stream
One air stream
Two or more air streams

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

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Compressors, Gas Turbines and Jet Engines
In jet engines, paraffin is usually used as the fuel because of its

Low freezing point
Both (A) and (C) above
High calorific value
Ease of atomisation

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Compressors, Gas Turbines and Jet Engines
Mechanical efficiency of gas turbines as compared to I.C engines is

Lower
Same
None of these
Higher

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Compressors, Gas Turbines and Jet Engines
As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio

Decreases
First increases and then decreases
Increases
Remain same

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