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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
If the flow of air through the compressor is perpendicular to its axis, then it is a

Turbo compressor
Axial flow compressor
Centrifugal compressor
Reciprocating compressor

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

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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
In turbo fan engine, the jet velocity as compared to turbojet engine is

May be less or more depending upon speed
Same
More
Less

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Compressors, Gas Turbines and Jet Engines
Actual compression curve is

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

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Compressors, Gas Turbines and Jet Engines
A rocket engine for the combustion of its fuel

Uses compressed atmospheric air
Does not require oxygen
Uses surrounding air
Carries its own oxygen

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