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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The power available for takeoff and climb in case of turbojet engine as compared to reciprocating engine is

May be less or more depending on ambient conditions
Less
Same
More

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Compressors, Gas Turbines and Jet Engines
The ratio of the discharge pressure to the inlet pressure of air is called

Compression ratio
Compressor efficiency
Expansion ratio
Volumetric efficiency

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

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

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Compressors, Gas Turbines and Jet Engines
The air-fuel ratio in gas turbines is of the order of

7: 1
30: 1
50: 1.
15: 1

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

To increase the output
To increase the efficiency
To save fuel
To reduce the exit temperature

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Compressors, Gas Turbines and Jet Engines
The net work input required for compressor with increase in clearance volume

Remains same
Decreases
Increases/decreases depending on compressor capacity
Increases

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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