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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The working fluid in a turbine is

In three phases
In a single phase
In two phases
In the form of air and water mixture

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Compressors, Gas Turbines and Jet Engines
For a two stage compressor, if index of compression for higher stage is greater than index of compression for lower stage, then the optimum pressure as compared to ideal case will

Remain unaffected
Decrease
Increase
Other factors control it

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Compressors, Gas Turbines and Jet Engines
Adiabatic compression is one in which

Work done is maximum
Temperature during compression remains constant
Temperature rise follows a linear relationship
No heat leaves or enters the compressor cylinder during compression

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Compressors, Gas Turbines and Jet Engines
The volume of air delivered by the compressor is called

None of the listed here
Compressor capacity
Swept volume
Free air delivery

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Compressors, Gas Turbines and Jet Engines
The efficiency of a jet engine is higher at

Low speeds
High speeds
High altitudes
Low altitudes

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Compressors, Gas Turbines and Jet Engines
1 m of air at atmospheric condition weighs approximately

0.5 kg
1.3 kg
2.2 kg
1.0 kg

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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