Load factor given Lift Force and Weight of Aircraft evaluator uses Load Factor = Lift Force/Aircraft Weight to evaluate the Load Factor, Load Factor Given Lift Force and Weight of Aircraft is a measure that quantifies the stress imposed on an aircraft during turns, calculated by dividing the lift force generated during a turn by the weight of the aircraft, providing a critical metric for aircraft performance and safety analysis. Load Factor is denoted by n symbol.
How to evaluate Load factor given Lift Force and Weight of Aircraft using this online evaluator? To use this online evaluator for Load factor given Lift Force and Weight of Aircraft, enter Lift Force (FL) & Aircraft Weight (W) and hit the calculate button.