stlfinder - 3d models search engine stlfinder - 3d models search engine
Parametric NACA-4 Airfoil

Parametric NACA-4 Airfoil

grabcad

The NACA-4 airfoil can be generated using equation-driven curves rather than creating a spline through points. Key design parameters include the chord length, maximum camber (in terms of chord length), maximum thickness (related to chord length), and maximum camber position (measured by chord length). Additionally, the aspect ratio is taken into account for this airfoil design.

Download Model from grabcad

With this file you will be able to print Parametric NACA-4 Airfoil with your 3D printer. Click on the button and save the file on your computer to work, edit or customize your design. You can also find more 3D designs for printers on Parametric NACA-4 Airfoil.