Enclosures and housings
HAWT Blade with Integrated Tapered Winglet
- Bounding box
- 200.0 × 145.0 × 1076.1 mm
- Engine
- Precision B-rep
- Parameters
- 26
- Published
- October 30, 2026
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The prompt
Create a detailed 3D CAD model of a horizontal-axis wind turbine blade featuring an integrated **tapered winglet** at its outer tip. **Blade geometry:** - Use a smooth aerodynamic airfoil cross-section along the entire blade. - Create a realistic wind turbine blade with gradual chord reduction from root to tip. - Include realistic blade twist (decreasing pitch angle toward the tip). - Maintain smooth aerodynamic transitions between all blade sections. **Tapered winglet design:** - Integrate an upward-projecting tapered winglet at the blade tip. - The winglet must gradually decrease in chord width toward its upper end. - Use a smooth, continuous transition between the main blade and winglet. - Maintain an aerodynamic profile consistent with the main blade. - Avoid sharp edges, abrupt thickness changes, and unnecessary structural details. **CAD and engineering requirements:** - Generate a single continuous, watertight 3D solid body. - Ensure accurate dimensions and smooth surfaces. - Make the geometry suitable for SolidWorks import and ANSYS Fluent CFD simulation. - Do not include the turbine hub, nacelle, tower, or surrounding components. **Output:** A clean, fully editable 3D wind turbine blade with an integrated tapered winglet, suitable for aerodynamic performance evaluation.
Parameters
| Name | Value | Range |
|---|---|---|
| Blade span (root to tip) | 900 mm | 200 – 3000 |
| Root chord | 160 mm | 60 – 400 |
| Root max thickness | 64 mm | 20 – 160 |
| Root trailing-edge thickness | 4 mm | 0.5 – 20 |
| Root camber height | 6 mm | 0 – 30 |
| Tip chord | 45 mm | 10 – 200 |
| Tip max thickness | 9 mm | 3 – 60 |
| Tip trailing-edge thickness | 1.5 mm | 0.2 – 10 |
| Tip camber height | 2 mm | 0 – 15 |
| Tip lateral sweep | 60 mm | -300 – 300 |
| Root twist | 22 deg | 0 – 45 |
| Tip twist | 2 deg | -10 – 20 |
| Winglet length | 180 mm | 20 – 600 |
| Winglet cant angle | 60 deg | 10 – 120 |
| Winglet tip chord | 22 mm | 5 – 120 |
| Winglet tip max thickness | 6 mm | 1 – 40 |
| Tip cap width (chord dir.) | 26 mm | 5 – 100 |
| Tip cap height (thickness dir.) | 10 mm | 2 – 60 |
| Tip cap thickness | 5 mm | 1 – 40 |
| Tip cap corner radius | 3 mm | 0 – 10 |
| Root flange thickness | 20 mm | 5 – 80 |
| Root flange margin | 20 mm | 2 – 80 |
| Root bolt hole diameter | 12 mm | 4 – 30 |
| Span loft sections | 12 count | 4 – 40 |
| Airfoil points per side | 32 count | 10 – 60 |
| Winglet loft sections | 7 count | 3 – 25 |
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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