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Compressors, Gas Turbines and Jet Engines

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

500°C
1000°C
200°C
700°C

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Compressors, Gas Turbines and Jet Engines
Cylinder clearance in a compressor should be

About 100% of swept volume
About 50% of swept volume
As small as possible
As large as possible

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Compressors, Gas Turbines and Jet Engines
The area of actual indicator diagram on an air compressor as compared to area of ideal indicator diagram is

Less
Same
More
More/less depending on compressor capacity

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, an increase in speed at a given pressure ratio causes

Decrease in flow
Increase in flow
Increase in efficiency
Increase in flow and decrease in efficiency

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

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

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Compressors, Gas Turbines and Jet Engines
A closed cycle gas turbine works on

Joule cycle
Ericsson cycle
Rankine cycle
Carnot cycle

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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