What causes the lowered aileron to create more drag when rolling out of a steep-banked turn?

The correct answer centers on the concept of angle of attack, which is crucial when discussing the aerodynamics of ailerons during a rollout from a steep turn. When the aircraft is in a steep-banked turn, the lowered aileron on the wing that is being raised may increase the wing's angle of attack as the rollout occurs.

In this scenario, when the pilot initiates the rollout from the turn, the wing with the lowered aileron experiences an increase in angle of attack due to the increased lift required to counteract the lateral forces acting on the aircraft. As the angle of attack rises, it can lead to an increase in induced drag on that wing, which results in more drag compared to the wing that is raised.

This greater angle of attack contributes to the generation of more lift, but it also comes with the trade-off of increased drag, especially when transitioning out of the steep bank. By understanding that the aileron position directly affects the angle of attack, it becomes evident why the lowered aileron generates additional drag during this phase of flight.

The other options do not accurately capture the dynamics involved during the rollout from a steep turn. The relative speeds of the wings or lift production alone do not adequately explain