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Compressors, Gas Turbines and Jet Engines

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

Same
More
Zero
Less

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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
Velocity factor
Velocity coefficient
None of these

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor resembles

Centrifugal pump
Turbine
Reciprocating pump
Sliding vane compressor

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Compressors, Gas Turbines and Jet Engines
Reheating in a gas turbine

Decreases the thermal efficiency
Increases the thermal efficiency
Increases the turbine work
Increases the compressor work

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Compressors, Gas Turbines and Jet Engines
A closed gas turbine in which fuel is burnt directly in the air is not possible because of

High friction losses
Paucity of O2
High specific volume
Increasing gas temperature

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Compressors, Gas Turbines and Jet Engines
The volumetric efficiency for reciprocating air compressors is about

70 to 90%
10 to 40%
40 to 60%
60 to 70%

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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