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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

All of the listed here
Produces uniform torque
Has more efficiency
Can be driven at a very high speed

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

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

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Compressors, Gas Turbines and Jet Engines
The degree of reaction is usually kept ________ for all types of axial flow compressors.

0.2
0.4
0.3
0.5

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

Ericsson cycle
Brayton or Atkinson cycle
Rankine cycle
Carnot cycle

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

Same as adiabatic
Better than isothermal and adiabatic
Same as isothermal
In between isothermal and adiabatic

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Compressors, Gas Turbines and Jet Engines
Which is false statement about advantages of multistage compressor in comparison to single stage compressor?

Better mechanical balance
Less power requirement
Less loss of air due to leakage past the cylinder
Lower volumetric efficiency

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