- 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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