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Compressors, Gas Turbines and Jet Engines

Compressors, Gas Turbines and Jet Engines
In jet engines the products of combustion after passing through the gas turbine are discharged into

Vacuum
Back to the compressor
Discharge nozzle
Atmosphere

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Compressors, Gas Turbines and Jet Engines
Gas turbine as compared to internal combustion engine

All of the listed here
Produces uniform torque
Can be driven at a very high speed
Has more efficiency

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Compressors, Gas Turbines and Jet Engines
Isothermal compression though most efficient, but is not practicable because

Compressor has to run at very slow speed to achieve it
It does not increase pressure much
It is impossible in practice
It requires very big cylinder

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Compressors, Gas Turbines and Jet Engines
Maximum work is done in compressing air when the compression is

Isothermal
Adiabatic
None of these
Polytropic

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

Axial flow compressors
Radial flow compressors
Pumps
All of these

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Compressors, Gas Turbines and Jet Engines
The temperature of air at the beginning of the compression stroke is ________ the atmospheric temperature.

Less than
None of these
More than
Equal to

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