How to Calculate Coefficient of lift given drag?
Coefficient of lift given drag calculator uses Lift Coefficient = (Gross Weight*Drag Coefficient)/Drag Force to calculate the Lift Coefficient, The Coefficient of lift given drag formula is defined as the a dimensionless quantity specifying the lift generated by the aircraft engines considering its gross weight, drag force and drag coefficient. Lift Coefficient is denoted by C_{L} symbol.
How to calculate Coefficient of lift given drag using this online calculator? To use this online calculator for Coefficient of lift given drag, enter Gross Weight (W_{0}), Drag Coefficient (C_{D}) & Drag Force (F_{D}) and hit the calculate button. Here is how the Coefficient of lift given drag calculation can be explained with given input values -> 1875 = (5000*30)/80.