How to Calculate Aspect Ratio given Induced Drag Coefficient?
Aspect Ratio given Induced Drag Coefficient calculator uses Wing Aspect Ratio ELD = Lift Coefficient ELD^2/(pi*Induced Drag Coefficient ELD) to calculate the Wing Aspect Ratio ELD, The Aspect ratio given induced drag coefficient formula calculates the aspect ratio of the wing by using the induced drag coefficient and the coefficient of lift. Wing Aspect Ratio ELD is denoted by ARELD symbol.
How to calculate Aspect Ratio given Induced Drag Coefficient using this online calculator? To use this online calculator for Aspect Ratio given Induced Drag Coefficient, enter Lift Coefficient ELD (CL,ELD) & Induced Drag Coefficient ELD (CD,i,ELD) and hit the calculate button. Here is how the Aspect Ratio given Induced Drag Coefficient calculation can be explained with given input values -> 2.486796 = 1.49^2/(pi*0.288).