What occurs to the down-going wing if an aircraft experiences a stall and a wing drop?

When an aircraft experiences a stall followed by a wing drop, the down-going wing has a larger angle of attack, which significantly affects its aerodynamic performance. During a stall, airflow over the wing becomes turbulent, leading to a reduction in lift. However, because the down-going wing is at a higher angle of attack relative to the critical angle of attack, it experiences less lift due to stall conditions, while also encountering an increase in drag.

In this situation, the down-going wing is already in a compromised aerodynamic state. As the angle of attack increases further during the stall, the lift diminishes and drag increases. This combination leads to a loss of control and potential yawing motions towards the stalled side, exacerbating the stall scenario.

The dynamics of the wings during a stall highlight the importance of angle of attack in maintaining lift. Understanding the impacts of increased angle of attack on lift and drag is crucial for pilots to manage and recover from stalls effectively.