Questions › Category: Compressors Gas Turbines and Jet Engines › In axial flow compressor, exit flow angle deviation from the blade angle is a function of 0 Vote Up Vote Down VideRime Staff asked 7 months ago 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 Share this Now with Friends:WhatsAppTelegramMore Related