How to Calculate Coefficient of Drag for given thrust and weight?
Coefficient of Drag for given thrust and weight calculator uses Drag Coefficient=Thrust of an aircraft*lift coefficient/Weight to calculate the Drag Coefficient, The Coefficient of Drag for given thrust and weight in a steady, level flight is given by the required thrust times coefficient of lift divided by the weight of aircraft. Drag Coefficient and is denoted by C_{D} symbol.
How to calculate Coefficient of Drag for given thrust and weight using this online calculator? To use this online calculator for Coefficient of Drag for given thrust and weight, enter Thrust of an aircraft (T), lift coefficient (C_{L}) and Weight (W) and hit the calculate button. Here is how the Coefficient of Drag for given thrust and weight calculation can be explained with given input values -> 10 = 100*10/100.