Airfoil Generator (NACA)
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Maximum camber
2.0%
first digit
Camber location
40%
second digit
Maximum thickness
12.0%
last two digits
NACA 2412 geometry
51 stations
The generated section shows the upper and lower surfaces around the mean camber line.
Open Source and Easy to Use Elsewhere
This tool is open source and the underlying logic is fully transparent. You can inspect the code, understand the calculations, and contribute improvements. If you want to use the tool in your own website, course page, or learning platform, you can also embed it directly and start from a ready-made iframe setup for this exact tool.
Open source: review the implementation and see how the results are produced.
Embeddable: preview this tool, copy the iframe, and use it in your own site or LMS.