Parametric NACA-4 Airfoil 3d model
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Parametric NACA-4 Airfoil

Parametric NACA-4 Airfoil

by GrabCAD
Last crawled date: 1 year, 10 months ago
Creates a NACA-4 airfoil via equation driven curves instead of a spline through points

Design 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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