Kutta Condition

The Kutta condition is a principle used in aerodynamics to determine how air flows smoothly around the sharp trailing edge of an airfoil or wing. Essentially, it states that the airflow leaves the trailing edge smoothly, without any abrupt changes or tears. This condition helps predict the overall lift generated by the wing, ensuring realistic and stable flow patterns in calculations. By applying the Kutta condition, engineers can accurately analyze and design wings to improve aircraft performance and efficiency.