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In axial flow compressor exit flow angle deviation from the blade...

This question belongs to Mechanical Engineering Compressors, Gas Turbines And Jet Engines
Compressors, Gas Turbines and Jet Engines
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In axial flow compressor, exit flow angle deviation from the blade angle is a function of

Answer & Solution
Correct Answer: Option B
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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