3D preview of Clark Y Semi-Span Wind Tunnel Wing
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Interactive 3D model of Clark Y Semi-Span Wind Tunnel Wing

Brackets and mounts

Clark Y Semi-Span Wind Tunnel Wing

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Bounding box
150.0 × 80.0 × 350.2 mm
Engine
Precision B-rep
Parameters
7
Published
October 18, 2026

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The prompt

Create a watertight solid model of a semi-span aircraft main wing for wind tunnel testing. Airfoil: Clark Y, flat-bottomed. Semi-span: 350 mm. Root chord: 130 mm. Tip chord: 70 mm. The chord tapers linearly from 130 mm at the root to 70 mm at the tip. Apply exactly 2 degrees of linear washout from root to tip. The tip must end with a flat planar cut perpendicular to the span direction. Do not add a wingtip socket or winglet connector. At the root, integrate a solid mounting flange measuring 150 mm x 80 mm x 5 mm for attachment to a wind tunnel wall. The entire result must be one watertight solid suitable for export as STEP and STL. Use millimeters for all dimensions.

Parameters

NameValueRange
Semi-Span350 mm100 – 1000
Root Chord130 mm50 – 300
Tip Chord70 mm30 – 250
Washout2 deg0 – 10
Flange Length150 mm80 – 300
Flange Width80 mm40 – 200
Flange Thickness5 mm2 – 20

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.

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Clark Y Semi-Span Wind Tunnel Wing - Free CAD Model (STEP, STL) | TextoCAD