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
C. Space-chord ratio
D. Blade camber and space-chord ratio
Answer: Option B
Solution(By Examveda Team)
In axial flow compressor, exit flow angle deviation from the blade angle is a function of Blade camber and incidence angleThis Question Belongs to Mechanical Engineering >> Compressors, Gas Turbines And Jet Engines
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