How to Calculate Lift-induced drag coefficient for given required thrust?
Lift-induced drag coefficient for given required thrust calculator uses Coefficient of drag due to lift=(Thrust of an aircraft/(Dynamic Pressure*Area))-Zero-lift drag coefficient to calculate the Coefficient of drag due to lift, The Lift-induced drag coefficient for given required thrust in a steady, level flight depends upon the zero-lift drag coefficient of an aircraft. . Coefficient of drag due to lift and is denoted by C_{D,i} symbol.
How to calculate Lift-induced drag coefficient for given required thrust using this online calculator? To use this online calculator for Lift-induced drag coefficient for given required thrust, enter Thrust of an aircraft (T), Dynamic Pressure (P_{dynamic)}, Area (A) and Zero-lift drag coefficient (C_{D,0}) and hit the calculate button. Here is how the Lift-induced drag coefficient for given required thrust calculation can be explained with given input values -> 0.1839 = (100/(10*50))-0.0161.