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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
Euler's equation is applicable for

Axial compressor
Centrifugal compressor
Pumps
All of these

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, the flow of air is ________ to the axis of compressor.

None of these
Parallel
Perpendicular
Inclined

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Compressors, Gas Turbines and Jet Engines
In jet engines, for the efficient production of large power, fuel is burnt in an atmosphere of

Compressed air
Oxygen alone
Vacuum
Atmospheric air

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Compressors, Gas Turbines and Jet Engines
Axial flow compressor has the following advantage over centrifugal compressor

Larger air handling ability per unit frontal area
Aerofoil blades are used
Higher pressure ratio per stage
Higher average velocities

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Compressors, Gas Turbines and Jet Engines
The compressor capacity with decrease in suction temperature

May increase or decrease depending on compressor capacity
Increases
Decreases
Remain unaffected

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Compressors, Gas Turbines and Jet Engines
The weight per horse power ratio for gas in Turbine as compared to I.C. engine and steam turbine is

None of these
Same
Lower
Higher

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