Lift Force for given Glide Angle evaluator uses Lift Force = Drag Force/tan(Glide Angle) to evaluate the Lift Force, The Lift force for given glide angle equation is derived from the relationship between lift force, drag force, and glide angle in gliding flight. It shows that the lift force is proportional to the drag force and inversely proportional to the tangent of the glide angle, using this equation, you can determine the lift force required to sustain a particular glide angle during gliding flight. Lift Force is denoted by FL symbol.
How to evaluate Lift Force for given Glide Angle using this online evaluator? To use this online evaluator for Lift Force for given Glide Angle, enter Drag Force (FD) & Glide Angle (θ) and hit the calculate button.