How to Calculate Glide angle for given lift-to-drag ratio?
Glide angle for given lift-to-drag ratio calculator uses Glide Angle = atan(1/Lift-to-drag Ratio) to calculate the Glide Angle, The Glide angle for given lift-to-drag ratio is given by the inverse tangent of reciprocal of the lift-to-drag ratio of aircraft. Glide Angle is denoted by θ symbol.
How to calculate Glide angle for given lift-to-drag ratio using this online calculator? To use this online calculator for Glide angle for given lift-to-drag ratio, enter Lift-to-drag Ratio (LD) and hit the calculate button. Here is how the Glide angle for given lift-to-drag ratio calculation can be explained with given input values -> 0.02702 = atan(1/6.61).