The uiuc airfoil data site gives some background on the database. Included below are coordinates for nearly 1,600 airfoils version 2. The airfoils are listed alphabetically by the airfoil filename which is usually close to the airfoil name. Max camber 0% at 0% chord source uiuc airfoil coordinates database source dat file the dat file. Links to the original data source for more information. The purpose of this site is to provide material about aerodynamics of model airplanes. Parser clarky il clark y airfoil clark y airfoil max thickness 11.
Most of the information is the result of work dedicated to high performance contest model aircraft. Uiuc airfoil coordinates database university of illinois. Parser naca23018il naca 23018 naca 23018 airfoil max thickness 18% at 30% chord. Media in category naca 4digit airfoils the following 7 files are in this category, out of 7 total. A read is counted each time someone views a publication summary such as the title, abstract, and list of authors, clicks on a figure, or views or downloads the fulltext. Naca profile 0018 stations and ordinates given in per cent of airfoil chord x. Naca airfoils are the best known aerodynamic airfoils, but where did they come from. Naca and you work hard to protect your identity and your personal information from online thieves. Parser naca0024il naca 0024 naca 0024 airfoil max thickness 24% at 30% chord. Beware of phishers who send emails or create websites posing as naca to get your personal information. Welcome to read the docs naca0012 latest documentation. Max camber 0% at 0% chord source uiuc airfoil coordinates database source dat file the dat file is in selig format. Download the dat file data in various formats or use the dat file data in the tools.
122 928 644 544 173 918 990 1008 769 1044 477 697 49 1135 1184 40 568 5 906 1119 1424 1294 285 344 949 1015 1252 526 170 849 557 1095 1096 1154 1066 1308