question\n\nthe amount of excess load that can be imposed on the wing of an airplane depends upon…

question\n\nthe amount of excess load that can be imposed on the wing of an airplane depends upon the\n\nanswer choices\n\nposition of the cg.\n\nspeed of the airplane.\n\nabruptness at which the load is applied.

question\n\nthe amount of excess load that can be imposed on the wing of an airplane depends upon the\n\nanswer choices\n\nposition of the cg.\n\nspeed of the airplane.\n\nabruptness at which the load is applied.

Answer

Brief Explanations:

The amount of excess load (load factor) that can be imposed on an airplane wing before reaching the critical angle of attack or structural failure is directly related to the speed of the airplane. At low speeds, the airplane will stall before the load factor becomes excessive. However, at higher speeds, the wing can produce enough lift to exceed the structural design load limit. This relationship is often illustrated in a V-n diagram (Velocity vs. G-load), which shows that the maximum available load factor increases with the square of the airspeed.

Answer:

speed of the airplane.