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

Questions › Category: Compressors Gas Turbines and Jet Engines › In axial flow compressor, exit flow angle deviation from the blade angle is a function of
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VideRime Staff asked 2 years ago
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In axial flow compressor, exit flow angle deviation from the blade angle is a function of

(A) Blade camber
(B) Blade camber and incidence angle           (Ans)
(C) Space-chord ratio
(D) Blade camber and space-chord ratio