Load Factor (g)

Load Factor (g)

Load Factor (g) refers to the measure of the load experienced by an aircraft wing during flight. It is the ratio of aerodynamic force to the weight of the aircraft, expressed in ‘g’ units. In simpler terms, it is the extent to which an aircraft wing experiences a load that exceeds its weight during flight.

Load Factor is an important concept in aviation engineering as it determines the structural limits of an aircraft. Pilots must ensure that the load factor remains within safe limits to prevent structural damage or failure. High load factors are typically seen during air combat maneuvers or aerobatic flights, while commercial flights typically operate at lower load factors to ensure passenger safety and comfort.

Factors that affect load factor include aircraft speed, altitude, and maneuvering. The load factor can be increased by performing tight turns or steep climb/descent maneuvers. This can lead to increased stress on the aircraft wing and can potentially cause damage if not done safely and within the aircraft’s limitations.

Overall, understanding load factor is crucial for safe and efficient flight operations. By managing load factor effectively, pilots and engineers can ensure the safe and successful operation of aircraft.