This course explores the physics of airflow over a wing, tracing the development of the thin laminar boundary layer as it grows into turbulence, transitions, and ultimately separates to produce a stall. It explains how the lift coefficient increases with angle of attack until reaching a critical point, at which the boundary layer detaches—causing lift to decrease and drag to rise.

The course examines stall warning systems, recovery techniques, and the influence of factors such as wing design, sweep, icing, and load factor. It also addresses the aerodynamic and operational consequences of stalls, emphasizing the value of early detection and effective pilot response.