Induced Drag Coefficient given Induced Drag Factor evaluator uses Induced Drag Coefficient GLD = ((1+Induced Drag Factor)*Lift Coefficient GLD^2)/(pi*Wing Aspect Ratio GLD) to evaluate the Induced Drag Coefficient GLD, The Induced drag coefficient given induced drag factor 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 GLD is denoted by CD,i,GLD symbol.
How to evaluate Induced Drag Coefficient given Induced Drag Factor using this online evaluator? To use this online evaluator for Induced Drag Coefficient given Induced Drag Factor, enter Induced Drag Factor (δ), Lift Coefficient GLD (CL,GLD) & Wing Aspect Ratio GLD (ARGLD) and hit the calculate button.