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Compressors, Gas Turbines and Jet Engines

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

Parallel
Inclined
Perpendicular
None of these

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

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

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

Centrifugal compressor
All of these
Axial compressor
Pumps

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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
Isochoric
Adiabatic
Isothermal

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Compressors, Gas Turbines and Jet Engines
With the decrease in compression ratio, the volumetric efficiency

Increases
First decrease and then increase
Decreases
Does not change

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

Low altitudes
High altitudes
Low speeds
High speeds

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