NACA Airfoil and Basic Wing Design CAD Model
About this design
Detailed CAD model featuring a NACA airfoil integrated with a simple wing structure, suitable for aerodynamic analysis and engineering applications.
The files are shared to help you get inspired and speed up your workflow. They may not be fully accurate or production-ready, so review carefully before use.
| View Name | Extension | Action |
|---|---|---|
| Design file | step | |
| Front View | webp | |
| Top View | webp | |
| Bottom View | webp | |
| Left Side View | webp | |
| Right Side View | webp | |
| Isometric View | webp |
| File Name | Action |
|---|---|
| No supporting files | |
About CAD
The CAD model comprises 81 faces, 225 edges, 150 vertices, 3 solids. Surface types include 45 planar, 33 cylindrical, 3 other surfaces. Orientations: 6 along the X-axis, 54 along the Y-axis, 21 along the Z-axis. Model dimensions: 1130.00 mm wide, 76.24 mm high, 604.50 mm deep. Volumetric data: maximum volume of 362462.85 mm³, minimum volume of 362462.85 mm³, average volume of 362462.85 mm³, total volume of 1087388.55 mm³
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