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Compressors, Gas Turbines and Jet Engines

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

Decreases
Remain constant
First decreases and then increases
Increases

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

500°C
700°C
1000°C
200°C

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Compressors, Gas Turbines and Jet Engines
The inlet pressure is always ___ the discharge pressure.

Less than
None of the listed here
Equal to
More than

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Compressors, Gas Turbines and Jet Engines
Maximum temperature in a gas turbine is of the order of

1500°C
1000°C
2000°C
700°C

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Compressors, Gas Turbines and Jet Engines
Reheating in gas turbine results in

Decrease of thermal efficiency
Both (A) and (B) above
Increase of work ratio
Decrease of work ratio

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Compressors, Gas Turbines and Jet Engines
The hottest point in a gas turbine is

between ~ to i of the blade height
in the center
at the tip
at the base

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