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Compressors, Gas Turbines and Jet Engines

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

Remain constant
Decreases
Increases
First decreases and then increases

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Compressors, Gas Turbines and Jet Engines
Gas turbines use following type of air compressor

Centrifugal type
Lobe type
Axial flow type
Reciprocating type

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Compressors, Gas Turbines and Jet Engines
The air entry velocity m a rocket as compared to aircraft is

Zero
Same
Less
More

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

Axial flow
Radial flow
Centrifugal
None of these

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

Carnot cycle
Ericsson cycle
Rankine cycle
Brayton or Atkinson cycle

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Compressors, Gas Turbines and Jet Engines
The indicated work per unit mass of air delivered is

Greatly affected by clearance volume
Directly proportional to clearance volume
Inversely proportional to clearance volume
Not affected by clearance volume

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