Glide angle for given lift-to-drag ratio evaluator uses Glide Angle = atan(1/Lift-to-drag Ratio) to evaluate the Glide Angle, The Glide angle for given lift-to-drag ratio equation provides the glide angle corresponding to the given lift-to-drag ratio. It's an essential parameter for pilots to optimize the aircraft's glide performance and plan safe landing approaches, especially during gliding or emergency situations, the inverse tangent function allows you to find the angle whose tangent is equal to the inverse of the lift-to-drag ratio. Glide Angle is denoted by θ symbol.
How to evaluate Glide angle for given lift-to-drag ratio using this online evaluator? To use this online evaluator for Glide angle for given lift-to-drag ratio, enter Lift-to-drag Ratio (LD) and hit the calculate button.