How to Calculate Wing Area for given Vertical Tail Volume Ratio?
Wing Area for given Vertical Tail Volume Ratio calculator uses Reference Area = Vertical Tail Moment Arm*Vertical Tail Area/(Wingspan*Vertical Tail Volume Ratio) to calculate the Reference Area, Wing Area for given Vertical Tail Volume Ratio is a measure of the reference area of an aircraft's wing required for directional stability, calculated by considering the vertical tail moment arm, vertical tail area, wingspan, and vertical tail volume ratio, ensuring stable and controlled flight dynamics. Reference Area is denoted by S symbol.
How to calculate Wing Area for given Vertical Tail Volume Ratio using this online calculator? To use this online calculator for Wing Area for given Vertical Tail Volume Ratio, enter Vertical Tail Moment Arm (𝒍v), Vertical Tail Area (Sv), Wingspan (b) & Vertical Tail Volume Ratio (Vv) and hit the calculate button. Here is how the Wing Area for given Vertical Tail Volume Ratio calculation can be explained with given input values -> 5.11509 = 1.2*5/(1.15*1.02).