How to Calculate Zero-lift drag coefficient at minimum required thrust?
Zero-lift drag coefficient at minimum required thrust calculator uses Zero-lift drag coefficient=(lift coefficient^2)/(pi*Oswald efficiency factor*Aspect Ratio of a wing) to calculate the Zero-lift drag coefficient, The Zero-lift drag coefficient at minimum required thrust for steady, level flight condition is equal to the coefficient of drag due to lift (or induced drag). Zero-lift drag coefficient and is denoted by C_{D,0} symbol.
How to calculate Zero-lift drag coefficient at minimum required thrust using this online calculator? To use this online calculator for Zero-lift drag coefficient at minimum required thrust, enter lift coefficient (C_{L}), Oswald efficiency factor (e) and Aspect Ratio of a wing (AR) and hit the calculate button. Here is how the Zero-lift drag coefficient at minimum required thrust calculation can be explained with given input values -> 15.91549 = (10^2)/(pi*0.5*4).