Airfoil Tools
WEBSearch 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 list
WEBAirfoil 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
WEBAirfoil 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.
Airfoil Comparison
WEBAirfoil Comparison. Select airfoils from the airfoil database or add your own airfoils and compare the airfoil shape and lift/drag polars.
NACA 4 digit airfoil generator (NACA 2412 AIRFOIL)
WEBNaca 4 digit airfoil generator(NACA 2412 AIRFOIL). Enter the airfoil thickness, camber and camber postion to generate a 4 digit NACA airfoil
NACA 4 digit Airfoil database search
WEBAirfoil 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 lift and drag polar diagrams
WEBAirfoil lift and drag polars with details of how the information was calculated and parsed using Xfoil
Generated airfoil shapes
WEBCommon simple airfoil shapes with associated xfoil polar files. Cambered plate airfoils used on wind turbines (HAWT)
NACA 6 series Airfoil database search
WEBAirfoil 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 list(N) n0009sm-il to n63012a-il
WEBAirfoil details. Send to airfoil plotter. Add to comparison. Lednicer format dat file. Selig format dat file. Source dat file. NACA 11-H-9 rotorcraft airfoil. Max thickness 9% at 40.2% chord. Max camber 4.5% at 30% chord.