Welcome to read the docs naca0012 latest documentation. Uiuc airfoil coordinates database university of illinois. Max camber 0% at 0% chord source uiuc airfoil coordinates database source dat file the dat file. Naca and you work hard to protect your identity and your personal information from online thieves. Naca profile 0018 stations and ordinates given in per cent of airfoil chord x. Media in category naca 4digit airfoils the following 7 files are in this category, out of 7 total.
Max camber 0% at 0% chord source uiuc airfoil coordinates database source dat file the dat file is in selig format. Parser naca0024il naca 0024 naca 0024 airfoil max thickness 24% at 30% chord. Parser naca23018il naca 23018 naca 23018 airfoil max thickness 18% at 30% chord. The airfoils are listed alphabetically by the airfoil filename which is usually close to the airfoil name. The purpose of this site is to provide material about aerodynamics of model airplanes. Naca airfoils are the best known aerodynamic airfoils, but where did they come from. Links to the original data source for more information. Download the dat file data in various formats or use the dat file data in the tools. Parser clarky il clark y airfoil clark y airfoil max thickness 11. Included below are coordinates for nearly 1,600 airfoils version 2. Beware of phishers who send emails or create websites posing as naca to get your personal information. Most of the information is the result of work dedicated to high performance contest model aircraft. The uiuc airfoil data site gives some background on the database.
579 52 608 987 1349 613 1011 1071 652 1241 843 771 820 236 1263 423 622 1414 1498 1111 1017 5 374 922 928 879 631 489 729 286 1226 1363 58 921 70 358 1487 1478 844 1429 803 1141 170 670 678 958 508 84 1475