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 CL 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 (W0), Drag Coefficient (CD) & Drag Force (FD) 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.