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Compressors, Gas Turbines and Jet Engines

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

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

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

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

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Compressors, Gas Turbines and Jet Engines
For an irreversible gas turbine cycle, the efficiency and work ratio both depend on

Both pressure ratio and maximum cycle temperature
Minimum cycle temperature alone
Pressure ratio alone
Maximum cycle temperature alone

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Compressors, Gas Turbines and Jet Engines
In a jet engine, the air-fuel ratio is

2.5006944444444
1.6673611111111
1.2506944444444
2.0840277777778

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency for reciprocating air compressors is about

60 to 70%
40 to 60%
10 to 40%
70 to 90%

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Compressors, Gas Turbines and Jet Engines
The pressure ratio of an ideal vaned compressor with increase in mass flow rate

Remain constant
Increases
First decreases and then increases
Decreases

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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