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Airfoil Tools View and plot a full size plan of the airfoil to your chord width The camber, thickness can be adjusted and the pitch set to allow for wing angle of attack, wash out or wind turbine blade angle
Airfoil database search 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
NACA 4 digit Airfoil database search 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
Symmetrical Airfoil database search 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
Airfoil database list Follow the links for details of the airfoil, image and polar diagrams Alternatively, you can use the airfoil database search page to filter and order the airfoils by camber, thickness and name
NACA 6 series Airfoil database search 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
Generated airfoil shapes The angle and twist of the blade can be controlled by the shape of the cut and the curve of the pipe approximates to an airfoil shape When the airfoil is normalised, the camber and thickness of the blade depends on size of the section through the pipe
Airfoil data information Some airfoil formulae, like the NACA series, calculate maximum thickness perpendicular to the camber line so there can be some small discrepancies During parsing the top and bottom surfaces of the airfoil are stored separately The surface with the larger number of points is used as the master