A critical hurdle in potential flow theory is the inability to predict lift without introducing circulation artificially. This is resolved mathematically by the Kutta condition, which dictates that the rear stagnation point must be located at the sharp trailing edge. In traditional teaching, this is often presented as an abstract mathematical rule.
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As air flows over the curved top of a wing, it sticks to the surface and is pulled downward. A critical hurdle in potential flow theory is