generated at
Angle of attack
>
AoAを大きくしすぎると失速する
>As the angle of attack increases, the lift reaches a maximum at some angle;
>increasing the angle of attack beyond this critical angle of attack causes the upper-surface flow to separate from the wing; there is less deflection downward so the airfoil generates less lift. The airfoil is said to be stalled.
stallした状態
>

>