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 is a measure of the aircraft's wingspan for the stable flight condition, calculated by considering the vertical tail's moment arm, area, dynamic pressure, and lift curve slope, as well as the sideslip angle and sidewash angle, in relation to the reference area and dynamic pressure of the wing, and the yawing moment coefficient. 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 (𝒍v), Vertical Tail Area (Sv), Vertical Tail Dynamic Pressure (Qv), Vertical Tail Lift Curve Slope (Cv), Sideslip Angle (β), Sidewash Angle (σ), 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).