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 is denoted by CD 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 (CL) & Thrust-to-Weight Ratio (TW) 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 -> 66 = 1.1*0.45.