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Airfoil database search (NACA 6 series)

Search the 1636 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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(naca663418-il) NACA 66(3)-418

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NACA 66(3)-418NACA 66(3)-418 airfoil
Max thickness 18% at 44.9% chord
Max camber 2.2% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca664221-il) NACA 66(4)-221

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NACA 66(4)-221NACA 66(4)-221 airfoil
Max thickness 21% at 45% chord
Max camber 1.1% at 50% chord
Source UIUC Airfoil Coordinates Database

(naca671215-il) NACA 67

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NACA 67NACA 67
Max thickness 15% at 50% chord
Max camber 1.1% at 50% chord
Source UIUC Airfoil Coordinates Database
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