Airfoil database search
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.
(naca0018-il) NACA 0018 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
NACA 0018 airfoil Max thickness 18% at 30% chord Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database |
Please see the source web site or designer for any license conditions.