How to Calculate Lift-to-drag ratio for given required thrust of aircraft?
Lift-to-drag ratio for given required thrust of aircraft calculator uses Lift-to-drag Ratio = Weight of Body/Thrust to calculate the Lift-to-drag Ratio, The Lift-to-drag ratio for given required thrust of aircraft in a steady, level flight is given by the weight divided by the required thrust of an aircraft. Lift-to-drag Ratio is denoted by LD symbol.
How to calculate Lift-to-drag ratio for given required thrust of aircraft using this online calculator? To use this online calculator for Lift-to-drag ratio for given required thrust of aircraft, enter Weight of Body (Wbody) & Thrust (T) and hit the calculate button. Here is how the Lift-to-drag ratio for given required thrust of aircraft calculation can be explained with given input values -> 2.21 = 221/100.