Is lift is generated due to large pressure gradients on the upper side of the airfoil?

A)
True
B)
False
C)
Can Not Say
D)
None of the above

Correct Answer :   True


Explanation : At higher angles, very large adverse pressure gradients that develop on the upper side as the airfoil attempts to generate more lift causes the boundary layer to separate, leading to a major disruption of the flow over the airfoil and the wing stalls.