airfoil - What is the effect of flow separation on lift, pressure distribution and drag? - Aviation Stack Exchange

Consider an airfoil (a wing) in an airflow. When angle of attack increases, at some point the flow start to separate from trailing edge. By increasing the angle of attack more, this separation area

Does laminar flow reduce drag? - Quora

Airfoil thickness effects on flow and acoustic characteristics

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Is early flow separation over a wing desired in any case? If yes

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If the boundary layer separates from the airfoil, does the lift

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Aerodynamics of Airfoil Sections – Introduction to Aerospace

Velocity data-based determination of airfoil characteristics with