How to Calculate Total Lift Coefficient of wing-tail combination?
Total Lift Coefficient of wing-tail combination calculator uses Lift Coefficient = Wing Lift Coefficient+(Tail Efficiency*Horizontal tail area*Tail Lift Coefficient/Reference Area) to calculate the Lift Coefficient, The Total Lift Coefficient of wing-tail combination is dependent on the tail efficiency, horizontal tail area, wing lift coefficient, and lift coefficient of the horizontal tail of an aircraft. Lift Coefficient is denoted by CL symbol.
How to calculate Total Lift Coefficient of wing-tail combination using this online calculator? To use this online calculator for Total Lift Coefficient of wing-tail combination, enter Wing Lift Coefficient (CWlift), Tail Efficiency (η), Horizontal tail area (St), Tail Lift Coefficient (CTlift) & Reference Area (S) and hit the calculate button. Here is how the Total Lift Coefficient of wing-tail combination calculation can be explained with given input values -> 1.107795 = 1.01+(0.92*1.8*0.3/5.08).