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
aerodynamics - Why is the pressure lowest towards the front of an
Why does Aerodynamic Center move to 50% chord when supersonic
Evolutionary understanding of airfoil lift
Evolutionary understanding of airfoil lift
Boundary Layer Separation and Pressure Drag
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aerodynamics - How do you calculate total drag on a wing
Sequence of flow separation.
How is the pressure distribution on a NACA 0012 reversed airfoil
Velocity data-based determination of airfoil characteristics with