So far, no multielement airfoils are included in the database. the trailing edge has aįinite thickness as designed. Listed do not close at the trailing edge, i.e. Leading edge to trailing edge (e.g., see Clark Y). Surface points leading edge to trailing edge and then lower surface Upper surface to the leading edge and back around the lower surface to Selig are in an x,y format starting from trailing edge, along the For questions, see the Airfoils FAQ.įor reference, the original airfoils in the list and new ones added by Web-browser "find" button to search for keywords. You canīrowse the directory, but it is suggested that you use your The file name, which most often is the airfoil name or close. Currently, the airfoils are listed in alphabetical order by Since this time, the number of airfoils hasĮxpanded to include over 1500, and more will be added as they becomeĪvailable. This addition brought the total number ofĪirfoils to over 1000. Originally the site included mostly low Reynolds numberĪirfoils (about 160), but in December 1995 the site was greatlyĮxpanded when David Lednicer of Analytical Methods, Inc. The UIUC Airfoil Coordinates Database includes the airfoils, and theyĬover a wide range of applications from low Reynolds numberĪirfoils for UAVs and model aircraft to jet transports and wind The UIUC Airfoil Data Site is a collection of airfoil coordinatesĪnd airfoil related links.
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