Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-stf86361-il-100000-n5 Airfoil,stf86361-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,34.9328 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-stf86361-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.250,-0.3228,0.13082,0.12565,-0.0886,0.9538,0.0559 -12.000,-0.3322,0.12730,0.12218,-0.0917,0.9520,0.0564 -11.750,-0.3408,0.12340,0.11832,-0.0945,0.9506,0.0566 -11.500,-0.3154,0.12017,0.11505,-0.0887,0.9507,0.0599 -11.250,-0.3114,0.11739,0.11227,-0.0887,0.9499,0.0625 -10.250,-0.3774,0.10312,0.09825,-0.0940,0.9412,0.0701 -9.750,-0.3669,0.09701,0.09221,-0.0902,0.9389,0.0742 -9.250,-0.3127,0.08301,0.07856,-0.0846,0.9268,0.0782 -7.750,-0.4849,0.06293,0.05691,-0.0872,0.9149,0.0327 -7.500,-0.4764,0.05907,0.05290,-0.0871,0.9131,0.0307 -7.250,-0.4588,0.05428,0.04735,-0.0874,0.9112,0.0256 -7.000,-0.4368,0.05089,0.04349,-0.0887,0.9098,0.0257 -6.750,-0.4116,0.04749,0.03960,-0.0905,0.9087,0.0271 -6.500,-0.3955,0.04533,0.03726,-0.0899,0.9067,0.0279 -6.250,-0.3736,0.04318,0.03449,-0.0891,0.9045,0.0269 -6.000,-0.3487,0.04149,0.03242,-0.0890,0.9025,0.0266 -5.750,-0.3222,0.03975,0.03035,-0.0891,0.9009,0.0265 -5.500,-0.2953,0.03799,0.02837,-0.0892,0.8996,0.0268 -5.250,-0.2683,0.03651,0.02685,-0.0896,0.8983,0.0285 -5.000,-0.2396,0.03557,0.02582,-0.0902,0.8970,0.0309 -4.750,-0.2101,0.03461,0.02476,-0.0905,0.8959,0.0316 -4.500,-0.1836,0.03386,0.02396,-0.0905,0.8944,0.0322 -4.250,-0.1677,0.03328,0.02332,-0.0887,0.8908,0.0328 -4.000,-0.1424,0.03276,0.02274,-0.0889,0.8883,0.0340 -3.750,-0.1132,0.03221,0.02215,-0.0901,0.8864,0.0377 -3.500,-0.0819,0.03194,0.02174,-0.0914,0.8846,0.0398 -3.250,-0.0488,0.03178,0.02141,-0.0929,0.8831,0.0419 -3.000,-0.0141,0.03168,0.02117,-0.0948,0.8818,0.0456 -2.750,0.0045,0.03162,0.02108,-0.0939,0.8774,0.0531 -2.250,0.0638,0.03151,0.02326,-0.0960,0.8722,0.6615 -2.000,0.0888,0.03209,0.02371,-0.0948,0.8695,0.6786 -1.750,0.1230,0.03239,0.02384,-0.0963,0.8678,0.6885 -1.500,0.1314,0.03269,0.02412,-0.0927,0.8609,0.6944 -1.250,0.1523,0.03313,0.02453,-0.0909,0.8574,0.7095 -1.000,0.1768,0.03350,0.02484,-0.0897,0.8550,0.7230 -0.750,0.1906,0.03388,0.02522,-0.0869,0.8504,0.7356 -0.500,0.2037,0.03421,0.02557,-0.0838,0.8454,0.7494 -0.250,0.2324,0.03437,0.02567,-0.0843,0.8426,0.7555 0.000,0.2678,0.03447,0.02568,-0.0866,0.8407,0.7571 0.250,0.2890,0.03473,0.02589,-0.0866,0.8353,0.7586 0.500,0.3138,0.03491,0.02605,-0.0869,0.8311,0.7598 0.750,0.3447,0.03501,0.02613,-0.0881,0.8284,0.7610 1.000,0.3788,0.03508,0.02619,-0.0899,0.8264,0.7618 1.250,0.3935,0.03537,0.02651,-0.0885,0.8188,0.7630 1.500,0.4245,0.03541,0.02656,-0.0897,0.8152,0.7643 1.750,0.4605,0.03534,0.02652,-0.0917,0.8127,0.7655 2.000,0.4775,0.03550,0.02672,-0.0906,0.8037,0.7665 2.250,0.5124,0.03538,0.02664,-0.0924,0.8004,0.7674 2.500,0.5329,0.03555,0.02687,-0.0920,0.7927,0.7685 2.750,0.5636,0.03555,0.02696,-0.0931,0.7884,0.7698 3.000,0.5985,0.03549,0.02698,-0.0950,0.7859,0.7711 3.250,0.6142,0.03589,0.02747,-0.0939,0.7767,0.7722 3.750,0.6646,0.03619,0.02802,-0.0945,0.7649,0.7739 4.000,0.6962,0.03604,0.02802,-0.0955,0.7608,0.7747 4.250,0.7157,0.03620,0.02832,-0.0947,0.7515,0.7755 4.500,0.7497,0.03576,0.02808,-0.0959,0.7469,0.7766 4.750,0.7696,0.03583,0.02831,-0.0950,0.7364,0.7779 5.000,0.8069,0.03508,0.02778,-0.0964,0.7321,0.7792 5.250,0.8282,0.03495,0.02783,-0.0955,0.7201,0.7804 5.500,0.8555,0.03413,0.02725,-0.0950,0.7065,0.7815 5.750,0.8784,0.03295,0.02624,-0.0932,0.6825,0.7827 6.000,0.9077,0.03108,0.02446,-0.0916,0.6386,0.7838 6.250,0.9617,0.02753,0.01914,-0.0910,0.3633,0.7848 6.500,0.9590,0.02959,0.02025,-0.0870,0.2203,0.7858 6.750,0.9593,0.03180,0.02155,-0.0838,0.0850,0.7868 7.000,0.9680,0.03336,0.02281,-0.0815,0.0464,0.7878 7.250,0.9804,0.03455,0.02404,-0.0797,0.0385,0.7889 7.500,0.9937,0.03566,0.02531,-0.0780,0.0348,0.7903 7.750,1.0053,0.03690,0.02669,-0.0762,0.0324,0.7917 8.000,1.0132,0.03846,0.02838,-0.0739,0.0306,0.7931 8.250,1.0236,0.03987,0.02994,-0.0720,0.0296,0.7946 8.500,1.0353,0.04125,0.03151,-0.0702,0.0283,0.7960 8.750,1.0486,0.04259,0.03299,-0.0688,0.0263,0.7973 9.000,1.0626,0.04397,0.03446,-0.0675,0.0245,0.7987 9.250,1.0792,0.04548,0.03605,-0.0665,0.0234,0.8002 9.750,1.1390,0.04929,0.04008,-0.0669,0.0217,0.8031 10.000,1.1632,0.05117,0.04232,-0.0664,0.0208,0.8047 10.250,1.1801,0.05321,0.04473,-0.0652,0.0193,0.8063 10.500,1.1953,0.05570,0.04756,-0.0640,0.0184,0.8081 10.750,1.2060,0.05863,0.05087,-0.0623,0.0180,0.8099 11.000,1.2101,0.06177,0.05439,-0.0600,0.0177,0.8117 11.250,1.2085,0.06508,0.05807,-0.0573,0.0175,0.8135 11.500,1.2022,0.06857,0.06194,-0.0545,0.0174,0.8154 11.750,1.1919,0.07218,0.06591,-0.0515,0.0173,0.8171 12.000,1.1784,0.07602,0.07008,-0.0487,0.0173,0.8189 12.250,1.1624,0.08009,0.07447,-0.0463,0.0173,0.8208 12.500,1.1447,0.08438,0.07904,-0.0443,0.0173,0.8227 12.750,1.1252,0.08906,0.08401,-0.0430,0.0173,0.8245 13.000,1.1045,0.09412,0.08933,-0.0424,0.0173,0.8264 13.250,1.0823,0.09988,0.09534,-0.0428,0.0174,0.8283 13.750,1.0357,0.11364,0.10954,-0.0472,0.0178,0.8316 14.000,1.0120,0.12203,0.11814,-0.0516,0.0181,0.8332