What type of stall can be caused by centrifugal force in flight?

An accelerated stall occurs when the aircraft experiences a stall due to increased load factor or G-forces that exceed the normal limits during maneuvers, such as turns or climbs. When an aircraft is subjected to centrifugal force during a turn, the load factor increases, which essentially means the wing must generate more lift to maintain level flight. If the angle of attack exceeds the critical angle while in this state, a stall will occur.

This type of stall can happen when the aircraft is maneuvering aggressively or at higher airspeeds, leading to higher G-forces that can push the aircraft beyond its stall threshold. It is essential for pilots to understand this concept to prevent unintended stalls during turns or other high-performance maneuvers.

In contrast, other types of stalls don't directly relate to the effects of centrifugal force in the same way. A stable stall typically refers to a situation that occurs under normal aerodynamic conditions without excessive loads. A base stall might refer more to specific landing scenarios, while a controlled stall usually denotes a practice maneuver done under controlled conditions to understand stall recognition and recovery without the influencing factors of centrifugal force. Understanding these distinctions helps pilots manage flight maneuvers safely and effectively.