How to Calculate Sideslip angle for given yawing moment coefficient?
Sideslip angle for given yawing moment coefficient calculator uses Sideslip angle = (Yawing moment coefficient/(Vertical tail moment arm*Vertical tail area*Vertical tail dynamic pressure*Vertical tail Lift curve slope/(Reference Area*Wingspan*Wing dynamic pressure)))-Sidewash angle to calculate the Sideslip angle, The Sideslip angle for given yawing moment coefficient is a function of the vertical tail's moment arm, lift curve slope, dynamic pressure (at vertical tail), area, sidewash angle, wing's reference area, wingspan, and dynamic pressure at wing. Sideslip angle is denoted by β symbol.
How to calculate Sideslip angle for given yawing moment coefficient using this online calculator? To use this online calculator for Sideslip angle for given yawing moment coefficient, enter Yawing moment coefficient (Cn), Vertical tail moment arm (𝒍v), Vertical tail area (Sv), Vertical tail dynamic pressure (Qv), Vertical tail Lift curve slope (Cv), Reference Area (S), Wingspan (b), Wing dynamic pressure (Qw) & Sidewash angle (σ) and hit the calculate button. Here is how the Sideslip angle for given yawing moment coefficient calculation can be explained with given input values -> 5.013 = (1.4/(1.2*5*11*0.7/(5.08*50*0.66)))-0.067.