Compressors, Gas Turbines and Jet Engines - Mechanical Engineering Questions and Answers

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In axial flow compressor, exit flow angle deviation from the blade angle is a function of

Blade camber

Blade camber and incidence angle

Space-chord ratio

Blade camber and space-chord ratio

Answer : Option B

Explanation :

In axial flow compressor, exit flow angle deviation from the blade angle is a function of Blade camber and incidence angle

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