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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
High air-fuel ratio in gas turbines

Reduces exhaust temperature
Do not damage turbine blades
Increases power output
Improves thermal efficiency

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Compressors, Gas Turbines and Jet Engines
Reheating in a multistage expansion gas turbine ________ compressor work.

None of these
Has no effect on
Decreases
Increases

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the highest Mach number leading to shock wave in the fluid flow occurs at

Diffuser inlet radius
Diffuser outlet radius
Impeller inlet radius
Impeller outlet radius

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Compressors, Gas Turbines and Jet Engines
Propulsion efficiency of the following order is obtained in practice

0.72
0.34
0.6
0.5

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Compressors, Gas Turbines and Jet Engines
The compressed air may be used

All of the listed here
In starting and supercharging of I.C. engines
For operating pneumatic drills
In gas turbine plants

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

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

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