How to Calculate Coefficient of Drag due to lift for minimum power required?
Coefficient of Drag due to lift for minimum power required calculator uses Coefficient of drag due to lift=3*Zero-lift drag coefficient to calculate the Coefficient of drag due to lift, The Coefficient of Drag due to lift for minimum power required in a steady, level flight is thrice of zero-lift drag coefficient of the aircraft. Coefficient of drag due to lift and is denoted by C_{D,i} symbol.
How to calculate Coefficient of Drag due to lift for minimum power required using this online calculator? To use this online calculator for Coefficient of Drag due to lift for minimum power required, enter Zero-lift drag coefficient (C_{D,0}) and hit the calculate button. Here is how the Coefficient of Drag due to lift for minimum power required calculation can be explained with given input values -> 0.0483 = 3*0.0161.