Enclosures and housings
eVTOL QuadPlane Wing
- Bounding box
- 240.2 × 801.5 × 25.4 mm
- Engine
- Precision B-rep
- Parameters
- 14
- Published
- August 8, 2026
Download
Free to download and use. See the terms.
The prompt
Create a parametric main wing for a small eVTOL QuadPlane, units mm. Wing type: tapered fixed wing Total span: 800 Root chord: 240 Tip chord: 200 Airfoil: Clark Y Dihedral: 1.5 degrees per side Twist: 0 degrees Create a symmetric wing about the aircraft centerline. Wing geometry: - Half-span: 400 mm each side - Root chord: 240 mm - Tip chord: 200 mm - Tip leading edge setback: 12 mm - Smooth loft from root airfoil to tip airfoil - No wingtip cap bulging outside dimensions Main spar: - Position at 28% chord - Add internal cylindrical spar passage - Spar outer diameter: 8 mm - Center spar continuously through the wing Ailerons: - One per side - Each aileron span: 150 mm - Root-side chord: 45 mm - Tip-side chord: 40 mm - Place near outer trailing edge - Leave 1.5 mm hinge gap Wing root interface: - Center section must mate with a fuselage approximately 72 mm wide - Provide a flat/controlled wing-seat region at the center - Do not create motor booms or motors in this part Output: One clean editable solid suitable for STEP export.
Parameters
| Name | Value | Range |
|---|---|---|
| Half Span | 400 mm | 100 – 1000 |
| Root Chord | 240 mm | 100 – 500 |
| Tip Chord | 200 mm | 50 – 300 |
| Tip LE Setback | 12 mm | 0 – 100 |
| Dihedral per Side | 1.5 deg | 0 – 10 |
| Spar Outer Diameter | 8 mm | 2 – 20 |
| Spar Position (% chord) | 0.28 | 0.2 – 0.4 |
| Aileron Span | 150 mm | 50 – 300 |
| Aileron Span Start (from root) | 250 mm | 0 – 400 |
| Aileron Root Chord | 45 mm | 20 – 100 |
| Aileron Tip Chord | 40 mm | 10 – 80 |
| Aileron Hinge Gap | 1.5 mm | 0.5 – 5 |
| Fuselage Width (seat width) | 72 mm | 30 – 150 |
| Wing Seat Flat Z Offset | 0 mm | -10 – 10 |
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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