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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The closed cycle in gas turbines

Provides greater flexibility
In never used
Is used when gas is to be burnt
Provides lesser flexibility

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Compressors, Gas Turbines and Jet Engines
The velocity of air entering in a rocket is ___ as compared to an aircraft.

Less
Zero
Same
More

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Compressors, Gas Turbines and Jet Engines
If infinite number of heaters be used in a gas turbine, then expansion process in turbine approaches

Isentropic
Isothermal
Isochoric
Adiabatic

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

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

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Compressors, Gas Turbines and Jet Engines
Work ratio of a gas turbine plant is ratio of

Net work output and work done by turbine
Work done by turbine and net work output
Work done by turbine and heat supplied
Net work output and heat supplied

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Compressors, Gas Turbines and Jet Engines
The net work input required for compressor with increase in clearance volume

Increases/decreases depending on compressor capacity
Decreases
Increases
Remains same

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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