How to Calculate Wing Reference area for given horizontal tail volume ratio?
Wing Reference area for given horizontal tail volume ratio calculator uses Reference Area = Horizontal tail moment arm*Horizontal tail area/(Horizontal Tail Volume Ratio*Mean aerodynamic chord) to calculate the Reference Area, The Wing Reference area for given horizontal tail volume ratio depends on the tail moment arm, tail area, tail volume ratio, and mean aerodynamic chord of the wing. Reference Area is denoted by S symbol.
How to calculate Wing Reference area for given horizontal tail volume ratio using this online calculator? To use this online calculator for Wing Reference area for given horizontal tail volume ratio, enter Horizontal tail moment arm (𝒍t), Horizontal tail area (St), Horizontal Tail Volume Ratio (VH) & Mean aerodynamic chord (cma) and hit the calculate button. Here is how the Wing Reference area for given horizontal tail volume ratio calculation can be explained with given input values -> 5.106383 = 0.8*1.8/(1.42*0.2).