Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-sc1012r8-il-50000-n5 Airfoil,sc1012r8-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,26.7318 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-sc1012r8-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.3940,0.10854,0.10148,-0.0084,1.0000,0.1370 -8.500,-0.4227,0.10623,0.09930,-0.0157,1.0000,0.1425 -7.750,-0.4297,0.08421,0.07720,-0.0293,1.0000,0.0750 -7.500,-0.4182,0.08125,0.07428,-0.0284,1.0000,0.0726 -7.250,-0.4176,0.07743,0.07048,-0.0291,1.0000,0.0706 -7.000,-0.4378,0.07086,0.06360,-0.0323,1.0000,0.0654 -6.750,-0.4325,0.06793,0.06069,-0.0314,1.0000,0.0647 -6.500,-0.4298,0.06490,0.05762,-0.0303,1.0000,0.0640 -6.250,-0.4276,0.06183,0.05448,-0.0291,1.0000,0.0633 -6.000,-0.4246,0.05876,0.05128,-0.0278,1.0000,0.0626 -5.750,-0.4203,0.05577,0.04812,-0.0264,1.0000,0.0622 -5.500,-0.4142,0.05294,0.04509,-0.0249,1.0000,0.0623 -5.250,-0.4061,0.05024,0.04215,-0.0234,1.0000,0.0627 -5.000,-0.3961,0.04766,0.03930,-0.0220,1.0000,0.0633 -4.750,-0.3840,0.04519,0.03653,-0.0206,1.0000,0.0638 -4.500,-0.3700,0.04285,0.03388,-0.0192,1.0000,0.0641 -4.250,-0.3542,0.04067,0.03140,-0.0180,1.0000,0.0642 -4.000,-0.3368,0.03864,0.02905,-0.0168,1.0000,0.0645 -3.750,-0.3180,0.03677,0.02685,-0.0158,1.0000,0.0649 -3.500,-0.2924,0.03509,0.02493,-0.0159,0.9975,0.0663 -3.250,-0.2489,0.03357,0.02332,-0.0194,0.9875,0.0694 -3.000,-0.2027,0.03189,0.02130,-0.0227,0.9768,0.0724 -2.750,-0.1552,0.03028,0.01936,-0.0259,0.9654,0.0748 -2.500,-0.1098,0.02910,0.01825,-0.0290,0.9524,0.0796 -2.250,-0.0644,0.02799,0.01698,-0.0315,0.9392,0.0853 -2.000,-0.0207,0.02696,0.01604,-0.0338,0.9256,0.0915 -1.750,0.0208,0.02606,0.01514,-0.0357,0.9109,0.1010 -1.500,0.0583,0.02522,0.01431,-0.0368,0.8949,0.1133 -1.250,0.0927,0.02435,0.01355,-0.0374,0.8776,0.1329 -1.000,0.1246,0.02334,0.01277,-0.0376,0.8589,0.1702 -0.750,0.1385,0.02045,0.01244,-0.0343,0.8414,0.6294 -0.500,0.2598,0.01993,0.01207,-0.0455,0.8190,1.0000 -0.250,0.2836,0.01972,0.01159,-0.0438,0.7882,1.0000 0.000,0.3056,0.01952,0.01114,-0.0417,0.7537,1.0000 0.250,0.3262,0.01939,0.01074,-0.0394,0.7156,1.0000 0.500,0.3463,0.01934,0.01040,-0.0371,0.6749,1.0000 0.750,0.3665,0.01936,0.01011,-0.0349,0.6336,1.0000 1.000,0.3866,0.01948,0.00988,-0.0327,0.5926,1.0000 1.250,0.4065,0.01970,0.00975,-0.0307,0.5533,1.0000 1.500,0.4263,0.02001,0.00970,-0.0288,0.5163,1.0000 1.750,0.4462,0.02037,0.00974,-0.0271,0.4822,1.0000 2.000,0.4666,0.02080,0.00984,-0.0256,0.4512,1.0000 2.250,0.4877,0.02126,0.01003,-0.0242,0.4225,1.0000 2.500,0.5091,0.02176,0.01025,-0.0230,0.3964,1.0000 2.750,0.5309,0.02228,0.01055,-0.0219,0.3717,1.0000 3.000,0.5530,0.02283,0.01088,-0.0209,0.3496,1.0000 3.250,0.5754,0.02340,0.01124,-0.0199,0.3293,1.0000 3.500,0.5983,0.02400,0.01166,-0.0191,0.3111,1.0000 3.750,0.6216,0.02461,0.01212,-0.0183,0.2946,1.0000 4.000,0.6449,0.02524,0.01262,-0.0176,0.2797,1.0000 4.250,0.6684,0.02590,0.01311,-0.0169,0.2672,1.0000 4.500,0.6920,0.02656,0.01365,-0.0162,0.2555,1.0000 4.750,0.7159,0.02726,0.01432,-0.0156,0.2447,1.0000 5.000,0.7395,0.02796,0.01482,-0.0150,0.2363,1.0000 5.250,0.7636,0.02875,0.01566,-0.0145,0.2272,1.0000 5.500,0.7872,0.02949,0.01625,-0.0139,0.2203,1.0000 5.750,0.8108,0.03038,0.01719,-0.0134,0.2128,1.0000 6.000,0.8343,0.03121,0.01797,-0.0128,0.2067,1.0000 6.250,0.8582,0.03213,0.01878,-0.0124,0.2019,1.0000 6.500,0.8808,0.03322,0.02003,-0.0118,0.1962,1.0000 6.750,0.9034,0.03418,0.02098,-0.0112,0.1913,1.0000 7.000,0.9272,0.03510,0.02174,-0.0108,0.1874,1.0000 7.250,0.9473,0.03647,0.02335,-0.0101,0.1829,1.0000 7.500,0.9679,0.03783,0.02485,-0.0095,0.1791,1.0000 7.750,0.9888,0.03909,0.02616,-0.0089,0.1759,1.0000 8.000,1.0108,0.04024,0.02726,-0.0084,0.1731,1.0000 8.250,1.0300,0.04176,0.02887,-0.0078,0.1702,1.0000 8.500,1.0429,0.04374,0.03118,-0.0067,0.1669,1.0000 8.750,1.0564,0.04561,0.03326,-0.0058,0.1639,1.0000 9.000,1.0706,0.04740,0.03518,-0.0049,0.1615,1.0000 9.250,1.0853,0.04919,0.03710,-0.0041,0.1595,1.0000 9.500,1.1011,0.05093,0.03888,-0.0033,0.1579,1.0000 9.750,1.1161,0.05283,0.04081,-0.0026,0.1563,1.0000 10.000,1.1054,0.05654,0.04497,-0.0007,0.1547,1.0000 10.250,1.0849,0.06085,0.04969,0.0012,0.1533,1.0000 10.500,1.0454,0.06646,0.05564,0.0028,0.1523,1.0000 10.750,0.8534,0.09912,0.08901,-0.0156,0.1508,1.0000