How to Calculate Tail moment arm for given tail moment coefficient?
Tail moment arm for given tail moment coefficient calculator uses Horizontal tail moment arm=-Tail pitching moment coefficient*Reference Area*Mean aerodynamic chord/(Tail Efficiency*Horizontal tail area*Tail Lift Coefficient) to calculate the Horizontal tail moment arm, The Tail moment arm for given tail moment coefficient is a function of tail pitching moment coefficient, wing reference area, wing mean aerodynamic chord, tail efficiency, tail area, and tail lift coefficient. Horizontal tail moment arm and is denoted by 𝒍_{t} symbol.
How to calculate Tail moment arm for given tail moment coefficient using this online calculator? To use this online calculator for Tail moment arm for given tail moment coefficient, enter Tail pitching moment coefficient (C_{mt}), Reference Area (S), Mean aerodynamic chord (c_{ma}), Tail Efficiency (η), Horizontal tail area (S_{t}) and Tail Lift Coefficient (C_{Lt}) and hit the calculate button. Here is how the Tail moment arm for given tail moment coefficient calculation can be explained with given input values -> -4.704301 = -0.7*5*0.2/(0.93*0.8*0.2).