Search for airfoils available on the web or in online databases, filtering by thickness and camber with preview images of the airfoil sections. Download the dat file data in various formats or use the dat file data in the tools.

Airfoil database search (NACA 4 digit) 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.

Airfoil database search (NACA 6 series) 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.

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.

Common simple airfoil shapes with associated xfoil polar files. Cambered plate airfoils used on wind turbines (HAWT)

Airfoil database search (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.

Airfoil database list. A list of all the airfoils in the database in alphabetic order. 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.

Airfoil database search (NACA 5 digit) 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.

(b737c-il) BOEING 737 MIDSPAN AIRFOIL Boeing Commercial Airplane Company model 737 airfoils Max thickness 10% at 39.9% chord. Max camber 1.5% at 20.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format: BOEING 737 MIDSPAN AIRFOIL 23. 23.

Naca 4 digit airfoil generator(NACA 0012 AIRFOIL). Enter the airfoil thickness, camber and camber postion to generate a 4 digit NACA airfoil