Drag for given Glide Angle evaluator uses Drag Force = Lift Force*tan(Glide Angle) to evaluate the Drag Force, The Drag for given glide angle equation represents the relationship between the lift force and the drag force when the aircraft is in gliding flight. The drag force is proportional to the lift force and the tangent of the glide angle. Drag Force is denoted by FD symbol.
How to evaluate Drag for given Glide Angle using this online evaluator? To use this online evaluator for Drag for given Glide Angle, enter Lift Force (FL) & Glide Angle (θ) and hit the calculate button.