How to Calculate Vertical tail area for given yawing moment coefficient?
Vertical tail area for given yawing moment coefficient calculator uses Vertical tail area = Yawing moment coefficient*(Reference Area*Wingspan*Wing dynamic pressure)/(Vertical tail moment arm*Vertical tail dynamic pressure*Vertical tail Lift curve slope*(Sideslip angle+Sidewash angle)) to calculate the Vertical tail area, The Vertical tail area for given yawing moment coefficient is a function of the vertical tail's moment arm, dynamic pressure (at vertical tail), lift curve slope, sideslip angle, sidewash angle, wing's reference area, wingspan, and dynamic pressure at wing. Vertical tail area is denoted by Sv symbol.
How to calculate Vertical tail area for given yawing moment coefficient using this online calculator? To use this online calculator for Vertical tail area for given yawing moment coefficient, enter Yawing moment coefficient (Cn), Reference Area (S), Wingspan (b), Wing dynamic pressure (Qw), Vertical tail moment arm (𝒍v), Vertical tail dynamic pressure (Qv), Vertical tail Lift curve slope (Cv), Sideslip angle (β) & Sidewash angle (σ) and hit the calculate button. Here is how the Vertical tail area for given yawing moment coefficient calculation can be explained with given input values -> 217.094 = 1.4*(5.08*50*0.66)/(1.2*11*0.7*(0.05+0.067)).