Brackets and mounts
Parametric UAV Wing Section with Root Flange
- Bounding box
- 201.0 × 105.8 × 25.0 mm
- Engine
- Precision B-rep
- Parameters
- 9
- Published
- August 7, 2026
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The prompt
Create a parametric UAV wing section with an aerodynamic airfoil profile, a chord length of 200mm, and a solid wing root flange for structural mounting.
Parameters
| Name | Value | Range |
|---|---|---|
| Chord Length | 200 mm | 50 – 500 |
| Span Length | 100 mm | 20 – 300 |
| Flange Thickness | 5 mm | 1 – 20 |
| Thickness (%) | 12 % | 3 – 30 |
| Camber (%) | 0 % | 0 – 9 |
| Camber Position (%) | 40 % | 5 – 95 |
| Hole Diameter | 4.2 mm | 2 – 10 |
| Hole X Position (fraction of chord) | 0.3 fraction | 0.1 – 0.8 |
| Hole Z Offset (fraction of half-thickness) | 0.5 fraction | 0.1 – 1 |
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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