Lift for given Load Factor evaluator uses Lift Force = Load Factor*Aircraft Weight to evaluate the Lift Force, Lift for Given Load Factor is a measure of the upward force exerted on an aircraft during a turn, which is calculated by multiplying the load factor during a turn by the weight of the aircraft during a turn, providing a critical factor in determining the safety and stability of flight during various maneuvers. Lift Force is denoted by FL symbol.
How to evaluate Lift for given Load Factor using this online evaluator? To use this online evaluator for Lift for given Load Factor, enter Load Factor (n) & Aircraft Weight (W) and hit the calculate button.