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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
1 m of air at atmospheric condition weighs approximately

2.2 kg
1.0 kg
0.5 kg
1.3 kg

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Compressors, Gas Turbines and Jet Engines
A compressor at high altitude will draw

More/less power depending on other factors
Less power
More power
Same power

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Compressors, Gas Turbines and Jet Engines
Gas turbines use following type of air compressor

Reciprocating type
Lobe type
Centrifugal type
Axial flow type

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Compressors, Gas Turbines and Jet Engines
The ratio of outlet whirl velocity to blade velocity in case of centrifugal compressor is called

None of these
Velocity coefficient
Slip factor
Velocity factor

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Compressors, Gas Turbines and Jet Engines
The closed cycle in gas turbines

Provides lesser flexibility
Is used when gas is to be burnt
In never used
Provides greater flexibility

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Compressors, Gas Turbines and Jet Engines
Standard air is the air at ___ and relative humidity of 36 percent.

0.1 bar and 40°C
1 bar and 40°C
0.1 bar and 20°C
1 bar and 20°C

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