NACA 0012 Airfoil Wing

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Bounding box: 150.0 × 18.0 × 600.0 mm
Engine: Precision B-rep
Parameters: 4
Published: October 5, 2026

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3D NACA 0012 airfoil

Parameters

Name	Value	Range
Chord Length	150 mm	40 – 500
Span (Extrusion Length)	600 mm	50 – 2000
Thickness Ratio (t/c)	0.12 ratio	0.06 – 0.24
Points Per Surface	80 count	20 – 300

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