How to Calculate Tail Lift Coefficient of wing-tail combination?
Tail Lift Coefficient of wing-tail combination calculator uses Tail Lift Coefficient = Reference Area*(Lift Coefficient-Wing Lift Coefficient)/(Tail Efficiency*Horizontal tail area) to calculate the Tail Lift Coefficient, The Tail Lift Coefficient of wing-tail combination is a function of total lift coefficient, tail efficiency, horizontal tail area, and wing lift coefficient. Tail Lift Coefficient is denoted by CTlift symbol.
How to calculate Tail Lift Coefficient of wing-tail combination using this online calculator? To use this online calculator for Tail Lift Coefficient of wing-tail combination, enter Reference Area (S), Lift Coefficient (CL), Wing Lift Coefficient (CWlift), Tail Efficiency (η) & Horizontal tail area (St) and hit the calculate button. Here is how the Tail Lift Coefficient of wing-tail combination calculation can be explained with given input values -> 0.276087 = 5.08*(1.108-1.01)/(0.92*1.8).