Airfoil database search (NACA 4 digit)
Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.
(naca2412-il) NACA 2412 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
NACA 2412 airfoil Max thickness 12% at 30% chord Max camber 2% at 40% chord Source UIUC Airfoil Coordinates Database |
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