How to Calculate Induced Drag Coefficient given Aspect Ratio?
Induced Drag Coefficient given Aspect Ratio calculator uses Induced Drag Coefficient ELD = Lift Coefficient ELD^2/(pi*Wing Aspect Ratio ELD) to calculate the Induced Drag Coefficient ELD, The Induced drag coefficient given aspect ratio formula calculates the coefficient of induced drag which has been caused due to the element of the air deflected downward which is not vertical to the flight path but is tilted slightly rearward from it. Induced Drag Coefficient ELD is denoted by CD,i,ELD symbol.
How to calculate Induced Drag Coefficient given Aspect Ratio using this online calculator? To use this online calculator for Induced Drag Coefficient given Aspect Ratio, enter Lift Coefficient ELD (CL,ELD) & Wing Aspect Ratio ELD (ARELD) and hit the calculate button. Here is how the Induced Drag Coefficient given Aspect Ratio calculation can be explained with given input values -> 0.288789 = 1.49^2/(pi*2.48).