Which wing tends to stall first during a climbing turn?

During a climbing turn, the higher wing tends to stall first due to the difference in angle of attack and the variation in lift experienced by each wing. In a turn, the aircraft bank is increased, leading to an increased load factor on the wings. The higher wing experiences a smaller angle of attack compared to the lower wing. As the turn continues and if the angle of attack increases, the higher wing will reach its critical angle of attack sooner, resulting in a stall before the lower wing does.

Additionally, the physics of flight dictate that during a turn, the increased load and reduced airflow over the higher wing can contribute to its stall characteristics. This understanding is crucial for pilots to anticipate stall behavior and maintain control during sharp climbs or turns, ensuring safety and aircraft performance.

The other options reflect various considerations, such as the role of load distribution in turns, but they do not accurately characterize the dynamics of stall behavior in relation to the wings during a climbing turn. The tendency for the higher wing to stall first is a fundamental concept in aerodynamics pertinent to pilot training and safety.