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Parametric NACA-4 Airfoil

Parametric NACA-4 Airfoil

grabcad

Creates a NACA-4 airfoil via equation driven curves instead of a spline through pointsDesign parameters are:Chord length (mm)Maximum camber (as a fraction of chord)Maximum thickness (as a fraction of chord)Maximum camber position (as a fraction of chord)Aspect ratio

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