Aerodynamics And Fluid Mechanics. An Aerofoil In A Flow Table During My Aerodynamics Lab Session, Showing The Stagnation Point And Flow Separation (Turbulent) Due To Excessive Pitch Angle Exceeding The Critical Angle Of Attack (Typically 15° For Most Commercial Airliners) This Amount Of Pitch Results In Stalling Of The Aerofoil (Which Generates Turbulent Flow), Which Is Catastrophic In A Real Aircraft If Stall Recovery Procedure Is Not Applied Immediately.

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