How to Calculate Normal component of aircraft side velocity for given dihedral angle?
Normal component of aircraft side velocity for given dihedral angle calculator uses Side Velocity Normal Component = Sideslip velocity*sin(Dihedral angle) to calculate the Side Velocity Normal Component, The Normal component of aircraft side velocity for given dihedral angle is a function of the sideslip velocity of the aircraft. Side Velocity Normal Component is denoted by Vn symbol.
How to calculate Normal component of aircraft side velocity for given dihedral angle using this online calculator? To use this online calculator for Normal component of aircraft side velocity for given dihedral angle, enter Sideslip velocity (Vβ) & Dihedral angle (Γ) and hit the calculate button. Here is how the Normal component of aircraft side velocity for given dihedral angle calculation can be explained with given input values -> 4.283602 = 20.54*sin(0.4).