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.

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.

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.

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 generator (NACA 2412 AIRFOIL). Enter the airfoil thickness, camber and camber postion to generate a 4 digit NACA airfoil

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.

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 2412 (naca2412-il) NACA 2412 - NACA 2412 airfoil ... Polars for NACA 2412 (naca2412-il)

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 …

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 …