airfoil - What is the effect of flow separation on lift, pressure
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
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If flow separation occurs, does it always accompanies a wake region? I mean, behind the flow separation, does the region always have a wake region whose pressure is low? - Quora
How does flow separation over the wing reduce lift of an aircraft? - Quora
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