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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The most efficient method of compressing air is to compress it

Isochronically
Isothermally
Adiabatically
Isentropically

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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
Adiabatic
Isochoric

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

Decreases
Increases
Remains same
Increases/decreases depending on compressor capacity

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Compressors, Gas Turbines and Jet Engines
High air-fuel ratio in gas turbines

Reduces exhaust temperature
Improves thermal efficiency
Increases power output
Do not damage turbine blades

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Compressors, Gas Turbines and Jet Engines
The advantage of multistage compression over single stage compression is

Higher volumetric efficiency
Decreased discharge temperature
Lower power consumption per unit of air delivered
All of these

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Compressors, Gas Turbines and Jet Engines
During base load operation, the best method of controlling compressor is

Start-stop motor
Constant speed unloader
Variable speed
Relief valve

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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