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Compressors, Gas Turbines and Jet Engines

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

Decreases the thermal efficiency
Increases the turbine work
Increases the thermal efficiency
Increases the compressor work

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Compressors, Gas Turbines and Jet Engines
The capacity of a compressor is expressed in

kg/m²
kg/m³
m³/min
m³/kg

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

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

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

First decreases and then increases
Remain constant
Increases
Decreases

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Compressors, Gas Turbines and Jet Engines
In a high pressure compressor, the delivery pressure is

8 to 10 bar
1 to 5 bar
5 to 8 bar
10 to 15 bar

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Compressors, Gas Turbines and Jet Engines
The pressure ratio for an open cycle gas turbine compared to closed cycle gas turbine of same h.p. is

Low
Low/high depending on make and type
High
Same

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