How to Calculate Wingspan for yawing moment coefficient given sideslip angle and sidewash angle?
Wingspan for yawing moment coefficient given sideslip angle and sidewash angle calculator uses Wingspan = Vertical tail moment arm*Vertical tail area*Vertical tail dynamic pressure*Vertical tail Lift curve slope*(Sideslip angle+Sidewash angle)/(Reference Area*Yawing moment coefficient*Wing dynamic pressure) to calculate the Wingspan, Wingspan for yawing moment coefficient given sideslip angle and sidewash angle depends on the vertical tail's moment arm, lift curve slope, dynamic pressure (at vertical tail), area, sideslip angle, sidewash angle, wing's reference area, and dynamic pressure at wing. Wingspan is denoted by b symbol.
How to calculate Wingspan for yawing moment coefficient given sideslip angle and sidewash angle using this online calculator? To use this online calculator for Wingspan for yawing moment coefficient given sideslip angle and sidewash angle, 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), Reference Area (S), Yawing moment coefficient (Cn) & Wing dynamic pressure (Qw) and hit the calculate button. Here is how the Wingspan for yawing moment coefficient given sideslip angle and sidewash angle calculation can be explained with given input values -> 1.151575 = 1.2*5*11*0.7*(0.05+0.067)/(5.08*1.4*0.66).