Originally Posted by
HSLD
To understand the stall, or lack of sufficient lift, one must understand how an airfoil creates lift in the first place. The camber, or curvature, of the airfoil increases the airflow over the upper wing surface, and the lowered pressure creates the upward force called lift. The pilot controls the amount of lift by adjusting the wing's angle of attack.
So, I'm a little confused.... does increased airflow (increased kinetic energy)
create low pressure.... or does low pressure
create increased airflow?
Also does Bernoulli's principle work in the boundary layer?