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 is denoted by CD,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 (CL), Oswald Efficiency Factor (e) & 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 -> 0.188801 = (1.1^2)/(pi*0.51*4).