Decreasing lift force with increasing angle of attack
I'm looking at a plot between the lift coefficient and the angle of attach (AoA) and I see that the lift coefficient increases with AoA. I understand that this happens because the net upward force is higher at higher AoAs. However, as we increase the AoA further, the wing experiences a sharp decreases in the lift force. Why does this happen? Any help here is appreciated!
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