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Compressors, Gas Turbines and Jet Engines

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

Axial flow compressors
All of these
Radial flow compressors
Pumps

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Compressors, Gas Turbines and Jet Engines
High air-fuel ratio is used in gas turbines

To increase the efficiency
To increase the output
To save fuel
To reduce the exit temperature

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

Atmosphere
Discharge nozzle
Vacuum
Back to the compressor

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

Inter cooling
All of the listed here
Reheating
Adding a regenerator

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Compressors, Gas Turbines and Jet Engines
The thermal efficiency of a simple gas turbine for a given turbine inlet temperature with increase in pressure ratio

First increases and then decreases
Decreases
First decreases and then increases
Increases

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

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

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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