PHAK 3-3 lists Bernoulli, Newton, and Magnus as the prime culprits in the production of lift. I understand how Bernoulli and Newton apply, but I feel that the Magnus effect only applies to rotating cylinders and balls, not wings. As I understand Magnus; the boundary layer moves with the rotating cylinder on the top side, therefore entrailing other layers of passing air at increased velocities, and thus lower pressure exists on the top side of the object. The opposite effect takes place on the bottom of the object (the side advancing toward the relative wind) creating lower velocity and consequently higher pressure. So I can see how this applies to golf balls and rotating cylinders, but with planes the boundary layers are attached to a stationary wing... Yes, highs and lows are being created, and a stagnation point exists, but not for the reasons associated with Magnus and 'moving' boundary layers. So am I misunderstanding the Magnus effect? Or does it actually apply to traditional airfoils? Thanks Jon
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