How to Calculate Vertical tail moment arm for given yawing moment coefficient?
Vertical tail moment arm for given yawing moment coefficient calculator uses Vertical tail moment arm = Yawing moment coefficient/(Vertical tail area*Vertical tail dynamic pressure*Vertical tail Lift curve slope*(Sideslip angle+Sidewash angle)/(Reference Area*Wingspan*Wing dynamic pressure)) to calculate the Vertical tail moment arm, The Vertical tail moment arm for given yawing moment coefficient is a function of the vertical tail's lift curve slope, dynamic pressure, area, sideslip angle, side wash angle, wing's reference area, wingspan, and dynamic pressure at wing. Vertical tail moment arm is denoted by 𝒍v symbol.
How to calculate Vertical tail moment arm for given yawing moment coefficient using this online calculator? To use this online calculator for Vertical tail moment arm for given yawing moment coefficient, enter Yawing moment coefficient (Cn), Vertical tail area (Sv), Vertical tail dynamic pressure (Qv), Vertical tail Lift curve slope (Cv), Sideslip angle (β), Sidewash angle (σ), Reference Area (S), Wingspan (b) & Wing dynamic pressure (Qw) and hit the calculate button. Here is how the Vertical tail moment arm for given yawing moment coefficient calculation can be explained with given input values -> 52.10256 = 1.4/(5*11*0.7*(0.05+0.067)/(5.08*50*0.66)).