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

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 …

Naca 5 digit airfoil generator(NACA24012 AIRFOIL). Enter the airfoils coefficient of lift thickness, camber postion and thickness to generate an airfoil from the NACA 5 digit family

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

Airfoil Comparison. Select airfoils from the airfoil database or add your own airfoils and compare the airfoil shape and lift/drag polars.

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 …

Reynolds number calculator for airfoils. Input the speed (velocity), chord width and viscousity to calculate the Reynolds number for a wing, blade, or keel. Example viscousity values for air …

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 …

Description of how the airfoil dat files are parsed and the camber and thickness calculated

Details of airfoil (aerofoil)(naca0018-il) NACA 0018 NACA 0018 airfoil. Airfoil Tools Search 1638 airfoils Tweet. You have 0 airfoils loaded. Your Reynold number range is 50,000 to 1,000,000. …