How to Calculate Coefficient of Drag for given thrust-to-weight ratio?
Coefficient of Drag for given thrust-to-weight ratio calculator uses Drag Coefficient=lift coefficient*Thrust-to-weight ratio to calculate the Drag Coefficient, The Coefficient of Drag for given thrust-to-weight ratio is given by the product of the coefficient of lift and thrust-to-weight ratio of the aircraft. Drag Coefficient and is denoted by C_{D} symbol.
How to calculate Coefficient of Drag for given thrust-to-weight ratio using this online calculator? To use this online calculator for Coefficient of Drag for given thrust-to-weight ratio, enter lift coefficient (C_{L}) and Thrust-to-weight ratio (T/W) and hit the calculate button. Here is how the Coefficient of Drag for given thrust-to-weight ratio calculation can be explained with given input values -> 600 = 10*60.