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Compressors, Gas Turbines and Jet Engines

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

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

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Compressors, Gas Turbines and Jet Engines
As the turbine inlet temperature increases, the thermal efficiency of gas turbine for the optimum pressure ratio

Remain same
Decreases
Increases
First increases and then decreases

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Compressors, Gas Turbines and Jet Engines
Inter-cooling in multistage compressors is done

To cool the air at delivery
To enable compression in two stages
To cool the air during compression
To minimize the work of compression

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

Reduce volume of air
Cool the air
Cause moisture and oil vapour to drop out
Remove impurities from air

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Compressors, Gas Turbines and Jet Engines
Rotary compressors are suitable for

Large discharge at low pressure
Large discharge at high pressure
Low discharge at low pressure
Low discharge at high pressure

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

m³/kg
m³/min
kg/m²
kg/m³

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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