![]() ![]() The airfoil file name is raf6prop_sm.dat, and it is in the Which he states is often used on propellers. Gasparovic provided a smoothed version of the RAF 6 airfoil, 8/16/20 - Thanks to Koen Stegen for catching a link typo.Renaming the first line to "Wortmann FX 76-120" (or "_FX 76-120") resolves the Seen using the XFOIL GDES command after loading the airfoil. Attempting to analyze thisĪirfoil (file) will create a bogus airfoil shape in XFOIL, e.g. Workable solution to this 'feature'." For instance, the FX 76-120Īirfoil file begins with "FX 76-120". Will be interpreted as logical variables, defeating the Will also choke on airfoil names that begin with T or F. Helped identify some coordinate files needing minor fixes to makeįrom XFOIL documentation verbatim: "Some Fortran implementations This file contains all airfoils (approx 1,600). Meeting, AIAA Paper 2018-0310, Kissimmee, FL, January 2018: and Selig, M.S., "Design ofĪIAA SciTech, 2018 AIAA Aerospace Sciences 6/27/21 - Updated some of the airfoil file names in the updates.Of the design was taking special care of the turbulent situationĬlose to the ground level boundary layer of the wind at a slope." Most remarkable aspect of these airfoils is their completeĪrtificial design made with an enhanced version of Xoptfoil by Dan JX-GS-10, JX-GS-15 airfoils - a family of airfoils for building aĬomplete wing for fast slope racing (F3F). Single webpage showing plots of all the airfoils (snapshot from ):įor more details, check out his script: ink ![]() ![]() - Thanks to Alan Eliasen, a script was written in his programming.- Coordinates for the MH112 and MH120 were incorrect.Thanks to WANG Ziyin for the contributions and the nice email description - Added Delft University airfoils: DU 80-176 V1.The code removes bad kinks in the airfoil surface curvature that can give rise to spikes (non-smoothness) in the velocity distributions.Īdded online at PDAS by Ralph Carmichael. Added mention of AFSMO: For coordinates that are not smooth, the NASA AFSMO smoothing code (airfoil smoothing code) can be used to smooth the points. The plug-in builds off his prior Rhino Script: ImportAirfoil.rvb. Installed using the Rhino Package Manager. - Added the YS-920 airfoil contributed byĪlso contributed the YS900, YS-915, and YS930įor plotting *.dat airfoil files.Than a 10% improvement in maximum lift coefficient." Compared with the S1223, the S9104 shows more Number of 200,000 with Ncrit = 9, which is the default Ncrit Of 11 deg) reaches a maximum lift coefficient 2.59 at a Reynolds From XFOIL predictions, the S9104 (at an angle of attack - Added the new S9104 and S9104BTE (blunt trailing edge)Ī snippet is this: "The S9104 airfoil was designed using PROFOIL.- Added the Drela AG23 used for the wing root on theĬross-country RC sailplane.airfoils.html - uses HTML5 Canvas for rendering and may not be displayed in large browser windows or older browsers due to browser limitationsįor more background, see the update below dated.airfoils.svg - uses SVG graphics (scalable vector graphics) to create the plots.The airfoils are in theĮliasen for updates to the graphical airfoil pages that he created: Coordinates for these airfoils were firstĥ but somehow they slipped by there inclusion here in theĪirfoil coordinates database. - This update includes the Chris Lyon CAL2263m, CAL4014l,Īnd CAL1215j airfoils.Home UIUC Airfoil Data Site UIUC Airfoil Coordinates Database Update History
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