How to Calculate Vertical tail moment arm for given lift curve slope?
Vertical tail moment arm for given lift curve slope calculator uses Vertical tail moment arm = Moment produced by vertical tail/(Vertical tail Lift curve slope*(Sideslip angle+Sidewash angle)*Vertical tail dynamic pressure*Vertical tail area) to calculate the Vertical tail moment arm, The Vertical tail moment arm for given lift curve slope is defined as the distance between center of gravity of the wing and the aerodynamic center of the stab. Vertical tail moment arm is denoted by 𝒍v symbol.
How to calculate Vertical tail moment arm for given lift curve slope using this online calculator? To use this online calculator for Vertical tail moment arm for given lift curve slope, enter Moment produced by vertical tail (Nv), Vertical tail Lift curve slope (Cv), Sideslip angle (β), Sidewash angle (σ), Vertical tail dynamic pressure (Qv) & Vertical tail area (Sv) and hit the calculate button. Here is how the Vertical tail moment arm for given lift curve slope calculation can be explained with given input values -> 0.444 = 2/(0.7*(0.05+0.067)*11*5).