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
Aerodynamic performance enhancement of the DU99W405 airfoil for
Aerodynamics of Airfoil Sections – Introduction to Aerospace
Aerodynamics of Airfoil Sections – Introduction to Aerospace
Is early flow separation over a wing desired in any case? If yes
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Applied Sciences, Free Full-Text
Wind-tunnel tests of synthetic jet control effects on airfoil flow
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