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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compressor capacity with decrease in suction temperature

Increases
Decreases
May increase or decrease depending on compressor capacity
Remain unaffected

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Compressors, Gas Turbines and Jet Engines
Aeroplanes employ following type of compressor

Radial flow
None of these
Axial flow
Centrifugal

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Compressors, Gas Turbines and Jet Engines
In a reciprocating air compressor, the compression work per kg of air

Decreases as clearance volume increases
Increases as clearance volume decreases
Increases as clearance volume increases
Is independent of clearance volume

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

Rankine cycle
Brayton or Atkinson cycle
Carnot cycle
Ericsson cycle

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Compressors, Gas Turbines and Jet Engines
In a four stage compressor, if the pressure at the first and third stage is 1 bar and 16 bar, then the delivery pressure at the fourth stage will be

256 bar
1 bar
64 bar
16 bar

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Compressors, Gas Turbines and Jet Engines
The main purpose of reheating in gas turbine is to

Increase power output
Reduce turbine size
Increase speed
Increase temperature

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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