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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The thrust on the rotor in a centrifugal compressor is produced by

None of these
Tangential component
Radial component
Axial component

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Compressors, Gas Turbines and Jet Engines
The capacity of compressor will be highest when its intake temperature is

Lowest
Anything
Atmospheric
Highest

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

Low speeds
Low altitudes
High altitudes
High speeds

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

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

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

Axial compressor
Centrifugal compressor
All of these
Pumps

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Compressors, Gas Turbines and Jet Engines
Efficiency of gas turbine is increased by

All of the listed here
Reheating
Adding a regenerator
Inter cooling

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