Joukowski Aerofoil Mapping

This form calculates the geometric properties of two dimensional aerofoil sections based on Joukowski transformation of a circular cylinder. The geometry of various families of sections can be created; symmetric, cambered, flat and curved.

Input Parameters
Cylinder Radius (a)

X-Coord Center Shift (e)

Y-Coord Center Shift (f)

Transformation Constant (k)

Number of Coordinates

Angle of Attack


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