How to Calculate Tail moment arm for given horizontal tail volume ratio?
Tail moment arm for given horizontal tail volume ratio calculator uses Horizontal tail moment arm=Horizontal Tail Volume Ratio*Reference Area*Mean aerodynamic chord/Horizontal tail area to calculate the Horizontal tail moment arm, The Tail moment arm for given horizontal tail volume ratio is a function of the wing reference area, wing mean aerodynamic chord, tail volume ratio, and tail area. Horizontal tail moment arm and is denoted by 𝒍_{t} symbol.
How to calculate Tail moment arm for given horizontal tail volume ratio using this online calculator? To use this online calculator for Tail moment arm for given horizontal tail volume ratio, enter Horizontal Tail Volume Ratio (V_{H}), Reference Area (S), Mean aerodynamic chord (c_{ma}) and Horizontal tail area (S_{t}) and hit the calculate button. Here is how the Tail moment arm for given horizontal tail volume ratio calculation can be explained with given input values -> 1.375 = 1.1*5*0.2/0.8.