How to Calculate Wing area for given yawing moment coefficient?
Wing area for given yawing moment coefficient calculator uses Reference Area = Vertical tail moment arm*Vertical tail area*Vertical tail dynamic pressure*Vertical tail Lift curve slope*(Sideslip angle+Sidewash angle)/(Yawing moment coefficient*Wingspan*Wing dynamic pressure) to calculate the Reference Area, The Wing area for given yawing moment coefficient is a function of the vertical tail's moment arm, lift curve slope, dynamic pressure (at vertical tail), area, sideslip angle, sidewash angle, wingspan, and dynamic pressure at wing. Reference Area is denoted by S symbol.
How to calculate Wing area for given yawing moment coefficient using this online calculator? To use this online calculator for Wing area for given yawing moment coefficient, enter Vertical tail moment arm (πv), Vertical tail area (Sv), Vertical tail dynamic pressure (Qv), Vertical tail Lift curve slope (Cv), Sideslip angle (Ξ²), Sidewash angle (Ο), Yawing moment coefficient (Cn), Wingspan (b) & Wing dynamic pressure (Qw) and hit the calculate button. Here is how the Wing area for given yawing moment coefficient calculation can be explained with given input values -> 0.117 = 1.2*5*11*0.7*(0.05+0.067)/(1.4*50*0.66).