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Compressors, Gas Turbines and Jet Engines

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

Adding a regenerator
All of the listed here
Reheating
Inter cooling

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Compressors, Gas Turbines and Jet Engines
Turbofan engine employs

No air stream
Two or more air streams
Solid fuel firing
One air stream

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Compressors, Gas Turbines and Jet Engines
In axial flow compressor, exit flow angle deviation from the blade angle is a function of

Space-chord ratio
Blade camber
Blade camber and space-chord ratio
Blade camber and incidence angle

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

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

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Compressors, Gas Turbines and Jet Engines
The efficiency of the vane blower is (where W₁ = Workdone due to compression, and W₂ = Workdone due to back flow)

W₂/(W₁ + W₂)
(W₁ + W₂)/W₂
(W₁ + W₂)/W₁
W₁/(W₁ + W₂)

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Compressors, Gas Turbines and Jet Engines
In a centrifugal compressor, an increase in speed at a given pressure ratio causes

Increase in flow and decrease in efficiency
Decrease in flow
Increase in flow
Increase in efficiency

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MORE MCQ ON Compressors, Gas Turbines and Jet Engines

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