Airfoil database search (NACA 6 series Symmetrical)
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.
(naca64a010-il) NACA 64A-010 10.0% | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 64A010 airfoil Max thickness 10% at 40% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database | |
(naca66-018-il) NACA 66-018 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | NACA 66-018 airfoil Max thickness 18% at 45% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database | |
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