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Compressors, Gas Turbines and Jet Engines

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

200°C
1000°C
500°C
700°C

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Compressors, Gas Turbines and Jet Engines
The ratio of outlet whirl velocity to blade velocity in case of centrifugal compressor is called

Slip factor
None of these
Velocity factor
Velocity coefficient

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

m³/min
kg/m³
kg/m²
m³/kg

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Compressors, Gas Turbines and Jet Engines
The ratio of work done per cycle to the swept volume in case of compressor is called

Compression index
Compressor efficiency
Mean effective pressure
Compression ratio

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Compressors, Gas Turbines and Jet Engines
The work done per unit mass of air in compression will be least when 'n' is equal to

1.3
1.2
1
1.4

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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

Increases
Remain same
Decreases
First increases and then decreases

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