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 Add Circulation

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