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/(Dynamic Pressure*Reference 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 is denoted by CD,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 (T), Dynamic Pressure (Pdynamic), Reference Area (S) & Zero Lift Drag Coefficient (CD,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 -> 0.94 = (100/(10*8))-0.31.