Airfoil Conformal Mapping - Joukowski Transformation

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α: Angle of attack

f: Meanline curvature

ν: Thickness

ρ: Equidistant offset

n: Number streamlines

Kutta condition Kutta Condition enable/disable

Γ: Circulation

  Streamlines
  Equipotential lines
  Isotach

Created by: airfoil.conf@gmail.com