The Kutta Condition is a principle in fluid dynamics that states that the flow of air must be smooth and continuous at the trailing edge of an airfoil, ensuring that there is no abrupt change in velocity. This condition is crucial for understanding how lift is generated, as it influences the pressure distribution over the airfoil and ensures that the airflow leaves the wing without any disturbances. Essentially, the Kutta Condition helps explain why airfoils are designed with specific shapes to achieve efficient lift while minimizing drag.
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