Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-oaf117-il-50000 Airfoil,oaf117-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,28.2878 Max Cl/Cd alpha,8.25 Url,http://airfoiltools.com/polar/csv?polar=xf-oaf117-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.750,-0.4969,0.10103,0.09397,0.0239,1.0000,0.3279 -7.500,-0.4937,0.09837,0.09135,0.0234,1.0000,0.3409 -7.250,-0.5601,0.07210,0.06504,-0.0172,1.0000,0.1938 -7.000,-0.5491,0.06546,0.05829,-0.0221,1.0000,0.1913 -6.750,-0.5380,0.05727,0.04985,-0.0298,1.0000,0.1899 -6.500,-0.5210,0.04813,0.04014,-0.0390,1.0000,0.1906 -6.250,-0.4973,0.04401,0.03580,-0.0417,1.0000,0.1977 -6.000,-0.4694,0.03917,0.03039,-0.0460,1.0000,0.2070 -5.750,-0.4430,0.03718,0.02838,-0.0464,1.0000,0.2185 -5.500,-0.4143,0.03459,0.02555,-0.0480,1.0000,0.2324 -5.250,-0.3858,0.03266,0.02349,-0.0489,1.0000,0.2499 -5.000,-0.3565,0.03092,0.02158,-0.0498,1.0000,0.2716 -4.750,-0.3283,0.02963,0.02025,-0.0501,1.0000,0.2945 -4.500,-0.3017,0.02885,0.01958,-0.0496,1.0000,0.3180 -4.250,-0.2733,0.02783,0.01849,-0.0499,1.0000,0.3447 -4.000,-0.2478,0.02727,0.01807,-0.0490,1.0000,0.3688 -3.750,-0.2199,0.02640,0.01714,-0.0493,1.0000,0.3959 -3.500,-0.1957,0.02583,0.01672,-0.0484,1.0000,0.4192 -3.250,-0.1694,0.02506,0.01592,-0.0486,1.0000,0.4456 -3.000,-0.1475,0.02445,0.01542,-0.0477,1.0000,0.4681 -2.750,-0.1290,0.02400,0.01509,-0.0465,1.0000,0.4906 -2.500,-0.1107,0.02362,0.01472,-0.0458,1.0000,0.5149 -2.250,-0.0944,0.02340,0.01458,-0.0449,1.0000,0.5376 -2.000,-0.0779,0.02332,0.01458,-0.0441,1.0000,0.5615 -1.750,-0.0592,0.02330,0.01460,-0.0441,1.0000,0.5883 -1.500,-0.0419,0.02342,0.01481,-0.0437,1.0000,0.6152 -1.250,-0.0229,0.02361,0.01509,-0.0437,1.0000,0.6451 -1.000,0.0324,0.02338,0.01495,-0.0490,0.9820,0.6937 -0.750,0.0851,0.02306,0.01473,-0.0537,0.9616,0.7420 -0.500,0.1345,0.02264,0.01446,-0.0570,0.9430,0.7941 -0.250,0.1752,0.02211,0.01410,-0.0581,0.9247,0.8564 0.000,0.2228,0.02149,0.01365,-0.0608,0.9018,0.9680 0.250,0.2905,0.02147,0.01334,-0.0710,0.8773,1.0000 0.500,0.3371,0.02177,0.01337,-0.0751,0.8561,1.0000 0.750,0.3710,0.02228,0.01369,-0.0766,0.8339,1.0000 1.000,0.4025,0.02280,0.01405,-0.0772,0.8137,1.0000 1.250,0.4319,0.02334,0.01446,-0.0772,0.7945,1.0000 1.500,0.4601,0.02389,0.01492,-0.0768,0.7760,1.0000 1.750,0.4874,0.02448,0.01542,-0.0763,0.7579,1.0000 2.000,0.5141,0.02507,0.01593,-0.0756,0.7400,1.0000 2.250,0.5405,0.02568,0.01649,-0.0749,0.7223,1.0000 2.500,0.5666,0.02629,0.01705,-0.0740,0.7046,1.0000 2.750,0.5925,0.02692,0.01764,-0.0732,0.6871,1.0000 3.000,0.6183,0.02754,0.01823,-0.0722,0.6695,1.0000 3.250,0.6440,0.02817,0.01884,-0.0713,0.6519,1.0000 3.500,0.6696,0.02881,0.01947,-0.0703,0.6344,1.0000 3.750,0.6952,0.02945,0.02012,-0.0693,0.6170,1.0000 4.000,0.7207,0.03012,0.02078,-0.0683,0.5995,1.0000 4.250,0.7462,0.03078,0.02146,-0.0673,0.5821,1.0000 4.500,0.7716,0.03144,0.02214,-0.0662,0.5645,1.0000 4.750,0.7970,0.03210,0.02282,-0.0651,0.5469,1.0000 5.000,0.8224,0.03271,0.02345,-0.0639,0.5291,1.0000 5.250,0.8478,0.03333,0.02409,-0.0627,0.5112,1.0000 5.500,0.8732,0.03386,0.02463,-0.0613,0.4931,1.0000 5.750,0.8988,0.03437,0.02512,-0.0600,0.4750,1.0000 6.000,0.9220,0.03555,0.02647,-0.0594,0.4536,1.0000 6.250,0.9462,0.03631,0.02730,-0.0583,0.4332,1.0000 6.500,0.9712,0.03679,0.02778,-0.0569,0.4133,1.0000 6.750,0.9971,0.03695,0.02790,-0.0552,0.3935,1.0000 7.000,1.0222,0.03730,0.02819,-0.0537,0.3728,1.0000 7.250,1.0444,0.03822,0.02924,-0.0526,0.3496,1.0000 7.500,1.0702,0.03825,0.02913,-0.0509,0.3278,1.0000 7.750,1.0928,0.03902,0.02992,-0.0497,0.3048,1.0000 8.000,1.1155,0.03971,0.03058,-0.0483,0.2816,1.0000 8.250,1.1400,0.04030,0.03092,-0.0469,0.2601,1.0000 8.500,1.1572,0.04226,0.03312,-0.0460,0.2388,1.0000 8.750,1.1765,0.04395,0.03485,-0.0449,0.2204,1.0000 9.000,1.1947,0.04598,0.03694,-0.0438,0.2049,1.0000 9.250,1.2100,0.04858,0.03970,-0.0429,0.1921,1.0000 9.500,1.2275,0.05102,0.04217,-0.0420,0.1815,1.0000 9.750,1.2387,0.05409,0.04549,-0.0410,0.1724,1.0000 10.000,1.2424,0.05823,0.04994,-0.0402,0.1663,1.0000 10.250,1.2268,0.06416,0.05641,-0.0396,0.1633,1.0000 10.500,1.1979,0.07112,0.06377,-0.0397,0.1626,1.0000 10.750,1.1453,0.08015,0.07307,-0.0415,0.1654,1.0000 11.000,1.0956,0.09166,0.08465,-0.0475,0.1682,1.0000