How to Calculate Weight of aircraft for given coefficients of lift and drag?
Weight of aircraft for given coefficients of lift and drag calculator uses Weight of Body = Lift Coefficient*Thrust/Drag Coefficient to calculate the Weight of Body, The Weight of aircraft for given coefficients of lift and drag is given by lift coefficient times thrust of aircraft divided by drag coefficient. Weight of Body is denoted by Wbody symbol.
How to calculate Weight of aircraft for given coefficients of lift and drag using this online calculator? To use this online calculator for Weight of aircraft for given coefficients of lift and drag, enter Lift Coefficient (CL), Thrust (T) & Drag Coefficient (CD) and hit the calculate button. Here is how the Weight of aircraft for given coefficients of lift and drag calculation can be explained with given input values -> 3.666667 = 1.1*100/0.5.