How to Calculate Vertical Tail Moment Arm for given Vertical Tail Volume Ratio?
Vertical Tail Moment Arm for given Vertical Tail Volume Ratio calculator uses Vertical Tail Moment Arm = Vertical Tail Volume Ratio*Reference Area*Wingspan/Vertical Tail Area to calculate the Vertical Tail Moment Arm, Vertical Tail Moment Arm for given Vertical Tail Volume Ratio is a measure of the distance from the aircraft's center of gravity to the vertical tail, calculated by multiplying the vertical tail volume ratio, reference area, and wingspan, and dividing by the vertical tail area, which is critical in determining the aircraft's stability and control during flight. Vertical Tail Moment Arm is denoted by πv symbol.
How to calculate Vertical Tail Moment Arm for given Vertical Tail Volume Ratio using this online calculator? To use this online calculator for Vertical Tail Moment Arm for given Vertical Tail Volume Ratio, enter Vertical Tail Volume Ratio (Vv), Reference Area (S), Wingspan (b) & Vertical Tail Area (Sv) and hit the calculate button. Here is how the Vertical Tail Moment Arm for given Vertical Tail Volume Ratio calculation can be explained with given input values -> 1.273556 = 1.02*5.08*1.15/5.