Parametric equation of inverse zimmerman planform?

The inverse Zimmerman planform can be represented using parametric equations that define the shape of the wing. Typically, these equations involve parameters such as the chord length, span, and angle of incidence. A common approach is to express the coordinates in terms of a parameter (u) that varies along the span, allowing for the definition of the wing's geometry in three dimensions. For specific applications, the exact form of the equations may vary based on design requirements and aerodynamic considerations.