NACA 64A210 Wing CAD Model for Aerodynamic Design
About this design
Explore the detailed CAD model of the NACA 64A210 wing, designed for aerodynamic analysis and engineering applications. Ideal for aerospace projects and simulations.
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 4955 faces, 12900 edges, 8048 vertices, 33 solids. Surface types include 509 planar, 2745 cylindrical, 140 conical, 12 toroidal, 1549 other surfaces. Orientations: 2520 along the X-axis, 571 along the Y-axis, 1858 along the Z-axis, 6 with various orientations. Model dimensions: 217.04 mm wide, 250.61 mm high, 658.50 mm deep. Volumetric data: maximum volume of 263777.56 mm³, minimum volume of 309.58 mm³, average volume of 26902.34 mm³, total volume of 887777.16 mm³
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Supported formats: STEP (.step, .stp), IGES (.igs, .iges), STL (.stl), PLY (.ply), OFF (.off), BREP (.brp, .brep)
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