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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
The compression ratio for the compressor is always _________ unity.

More than
Less than
None of these
Equal to

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Compressors, Gas Turbines and Jet Engines
Ram compression in turbojet involves

Compression of inlet air
Increasing speed of incoming air
Lost work
Reduction of speed of incoming air and conversion of part of it into pressure energy

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Compressors, Gas Turbines and Jet Engines
The main purpose of reheating in gas turbine is to

Increase speed
Increase power output
Increase temperature
Reduce turbine size

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

Tangential component
None of these
Axial component
Radial component

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Compressors, Gas Turbines and Jet Engines
Euler's equation can be used for

All of these
Pumps
Axial flow compressors
Radial flow compressors

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Compressors, Gas Turbines and Jet Engines
The efficiency and work ratio of a gas turbine plant can be increased by

Reheating the air after partial expansion in the turbine
All of these
Adding heat exchanger
Injecting water in/around combustion chamber

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