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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The maximum temperature in a gas turbine is

1000°C
500°C
700°C
200°C

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is 5 m/min refers to

Compressed air
Standard air
Free air
Compressed air at delivery pressure

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Compressors, Gas Turbines and Jet Engines
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Equal
Higher
Can't be compared
Lower

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Compressors, Gas Turbines and Jet Engines
After-cooler is used to

Decrease the delivery temperature for ease in handling
Reduce volume
Cool the air
Cause moisture and oil vapour to drop out

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency of a compressor

Decreases with increase in compression ratio
Decreases with decrease in compression ratio
Increases with increase in compression ratio
Increases with decrease in compression ratio

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Compressors, Gas Turbines and Jet Engines
The air entry velocity m a rocket as compared to aircraft is

Same
Less
Zero
More

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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