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Interactive 3D model of Parametric NACA0015 Half Wing with Split Scimitar Winglets

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Parametric NACA0015 Half Wing with Split Scimitar Winglets

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Bounding box
302.5 × 100.2 × 1391.7 mm
Engine
Precision B-rep
Parameters
19
Published
September 26, 2026

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Half span wing of NACA0015 with Split Scimitar Winglets (use dimensions useful for ansys simulation or meshing)

Parameters

NameValueRange
Root Chord300 mm50 – 1000
Tip Chord150 mm20 – 800
Main Half Span1200 mm200 – 5000
Tip Sweep Distance80 mm0 – 500
Upper Winglet Height200 mm50 – 500
Upper Cant Angle20 deg0 – 60
Upper Sweep Angle30 deg0 – 60
Upper Curvature0.10 – 0.3
Upper Root X Fraction0.20.05 – 0.5
Upper Root Chord Fraction0.40.2 – 0.8
Upper Taper Ratio0.60.2 – 1
Lower Strake Height80 mm20 – 300
Lower Cant Angle15 deg0 – 50
Lower Sweep Angle25 deg0 – 50
Lower Curvature0.10 – 0.3
Lower Root X Fraction0.20.05 – 0.5
Lower Root Chord Fraction0.30.1 – 0.6
Lower Taper Ratio0.50.2 – 1
Winglet Root Overlap10 mm1 – 50

Every value above is a live dimension. Open a model like this in the editor and each one becomes a slider you can drag before exporting.

Parametric NACA0015 Half Wing with Split Scimitar Winglets - Free CAD Model (STEP, STL) | TextoCAD