Aerodynamic-And-Mechanical-Engineering The camber of a thin aerofoil with unit chord is given by the equation: Admin ?(?) = ??(? _ 1)(? _ ?) where k 0 and b 0. Depending on the choice of b, this equation can represent a reflex aerofoil in which the mean…Continue readingThe camber of a thin aerofoil with unit chord is given by the equation: