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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.

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(naca653218-il) NACA 65(3)-218

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Source dat file
NACA 65(3)-218NACA 65(3)-218 airfoil
Max thickness 18% at 39.9% chord
Max camber 1.1% at 50% chord
Source UIUC Airfoil Coordinates Database
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