Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ea61012-il-200000 Airfoil,ea61012-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,34.6795 Max Cl/Cd alpha,6.5 Url,http://airfoiltools.com/polar/csv?polar=xf-ea61012-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.500,-0.6744,0.12052,0.11658,0.0005,1.0000,0.0930 -12.250,-0.6527,0.11966,0.11569,0.0028,1.0000,0.0946 -12.000,-0.8951,0.06951,0.06516,-0.0324,1.0000,0.0694 -11.750,-0.9118,0.06485,0.06033,-0.0326,1.0000,0.0670 -11.500,-0.9332,0.06059,0.05592,-0.0318,1.0000,0.0666 -11.250,-0.9565,0.05703,0.05217,-0.0292,1.0000,0.0664 -11.000,-0.9722,0.05326,0.04815,-0.0269,1.0000,0.0663 -10.750,-0.9819,0.04976,0.04433,-0.0246,1.0000,0.0666 -10.500,-0.9859,0.04665,0.04086,-0.0223,1.0000,0.0671 -10.250,-0.9842,0.04403,0.03786,-0.0202,1.0000,0.0676 -9.750,-0.9684,0.03753,0.03076,-0.0174,1.0000,0.0693 -9.500,-0.9499,0.03549,0.02866,-0.0168,1.0000,0.0707 -9.250,-0.9299,0.03383,0.02693,-0.0162,1.0000,0.0718 -9.000,-0.9108,0.03213,0.02507,-0.0154,1.0000,0.0729 -8.750,-0.8908,0.03066,0.02342,-0.0146,1.0000,0.0744 -8.500,-0.8704,0.02920,0.02177,-0.0138,1.0000,0.0758 -8.250,-0.8489,0.02776,0.02013,-0.0130,1.0000,0.0768 -8.000,-0.8266,0.02650,0.01868,-0.0123,1.0000,0.0779 -7.750,-0.8042,0.02565,0.01763,-0.0115,1.0000,0.0790 -7.500,-0.7805,0.02374,0.01566,-0.0112,1.0000,0.0806 -7.250,-0.7567,0.02249,0.01444,-0.0108,1.0000,0.0822 -7.000,-0.7348,0.02158,0.01353,-0.0100,1.0000,0.0836 -6.750,-0.7186,0.02087,0.01282,-0.0083,1.0000,0.0850 -6.500,-0.7032,0.02029,0.01222,-0.0067,0.9977,0.0867 -6.250,-0.6649,0.01949,0.01136,-0.0092,0.9891,0.0894 -6.000,-0.6256,0.01879,0.01057,-0.0117,0.9823,0.0915 -5.750,-0.5908,0.01755,0.00943,-0.0135,0.9746,0.0944 -5.250,-0.5194,0.01621,0.00813,-0.0174,0.9594,0.1025 -5.000,-0.4842,0.01547,0.00742,-0.0192,0.9527,0.1072 -4.750,-0.4544,0.01486,0.00687,-0.0200,0.9432,0.1135 -4.500,-0.4241,0.01430,0.00633,-0.0207,0.9352,0.1225 -4.250,-0.3988,0.01373,0.00588,-0.0205,0.9260,0.1398 -4.000,-0.3798,0.01262,0.00532,-0.0195,0.9176,0.2288 -3.750,-0.3683,0.01126,0.00491,-0.0173,0.9085,0.4206 -3.500,-0.3512,0.01077,0.00509,-0.0150,0.9015,0.5631 -3.250,-0.3273,0.01083,0.00527,-0.0138,0.8944,0.6194 -3.000,-0.3019,0.01100,0.00546,-0.0128,0.8886,0.6522 -2.750,-0.2765,0.01120,0.00567,-0.0119,0.8822,0.6758 -2.500,-0.2505,0.01142,0.00588,-0.0110,0.8764,0.6936 -2.250,-0.2243,0.01167,0.00609,-0.0102,0.8718,0.7094 -2.000,-0.1989,0.01199,0.00642,-0.0092,0.8658,0.7263 -1.750,-0.1742,0.01229,0.00672,-0.0079,0.8591,0.7422 -1.500,-0.1497,0.01256,0.00696,-0.0065,0.8530,0.7566 -1.250,-0.1252,0.01283,0.00729,-0.0051,0.8461,0.7703 -1.000,-0.1012,0.01309,0.00757,-0.0033,0.8405,0.7846 -0.750,-0.0770,0.01325,0.00775,-0.0019,0.8345,0.7960 -0.500,-0.0520,0.01329,0.00776,-0.0013,0.8276,0.8050 -0.250,-0.0260,0.01327,0.00773,-0.0004,0.8222,0.8097 0.000,0.0000,0.01327,0.00776,0.0000,0.8154,0.8154 0.250,0.0259,0.01327,0.00773,0.0004,0.8097,0.8222 0.500,0.0519,0.01329,0.00776,0.0013,0.8050,0.8277 0.750,0.0769,0.01325,0.00775,0.0020,0.7959,0.8345 1.000,0.1011,0.01309,0.00757,0.0034,0.7845,0.8405 1.250,0.1251,0.01284,0.00729,0.0051,0.7705,0.8461 1.500,0.1497,0.01256,0.00696,0.0065,0.7566,0.8530 1.750,0.1742,0.01229,0.00672,0.0079,0.7422,0.8591 2.000,0.1988,0.01198,0.00642,0.0092,0.7262,0.8658 2.250,0.2242,0.01167,0.00609,0.0102,0.7094,0.8718 2.500,0.2504,0.01142,0.00588,0.0111,0.6936,0.8764 2.750,0.2765,0.01120,0.00567,0.0119,0.6758,0.8822 3.000,0.3019,0.01100,0.00546,0.0128,0.6523,0.8886 3.250,0.3273,0.01083,0.00527,0.0138,0.6192,0.8944 3.500,0.3511,0.01077,0.00509,0.0150,0.5628,0.9015 3.750,0.3682,0.01126,0.00491,0.0173,0.4207,0.9085 4.000,0.3799,0.01260,0.00531,0.0195,0.2302,0.9176 4.250,0.3988,0.01373,0.00588,0.0205,0.1399,0.9260 4.500,0.4241,0.01430,0.00633,0.0207,0.1224,0.9353 4.750,0.4544,0.01486,0.00687,0.0200,0.1135,0.9432 5.000,0.4842,0.01547,0.00742,0.0192,0.1072,0.9527 5.250,0.5195,0.01620,0.00813,0.0174,0.1025,0.9594 5.500,0.5534,0.01678,0.00871,0.0159,0.0981,0.9683 5.750,0.5909,0.01754,0.00943,0.0135,0.0944,0.9747 6.000,0.6258,0.01879,0.01057,0.0116,0.0915,0.9824 6.250,0.6650,0.01949,0.01136,0.0091,0.0894,0.9891 6.500,0.7033,0.02028,0.01221,0.0067,0.0867,0.9978 6.750,0.7185,0.02086,0.01282,0.0084,0.0850,1.0000 7.000,0.7348,0.02157,0.01353,0.0100,0.0836,1.0000 7.250,0.7567,0.02248,0.01443,0.0108,0.0822,1.0000 7.500,0.7805,0.02375,0.01566,0.0112,0.0806,1.0000 7.750,0.8041,0.02563,0.01761,0.0115,0.0790,1.0000 8.000,0.8266,0.02649,0.01867,0.0123,0.0778,1.0000 8.250,0.8489,0.02776,0.02013,0.0130,0.0768,1.0000 8.500,0.8704,0.02919,0.02176,0.0138,0.0757,1.0000 8.750,0.8909,0.03064,0.02341,0.0146,0.0743,1.0000 9.000,0.9109,0.03211,0.02504,0.0154,0.0729,1.0000 9.250,0.9300,0.03384,0.02694,0.0162,0.0718,1.0000 9.500,0.9499,0.03549,0.02866,0.0168,0.0707,1.0000 9.750,0.9685,0.03754,0.03076,0.0174,0.0693,1.0000 10.250,0.9841,0.04402,0.03785,0.0202,0.0676,1.0000 10.500,0.9860,0.04667,0.04088,0.0223,0.0671,1.0000 10.750,0.9824,0.04984,0.04441,0.0245,0.0667,1.0000 11.000,0.9723,0.05330,0.04819,0.0268,0.0663,1.0000 11.250,0.9560,0.05696,0.05211,0.0292,0.0663,1.0000 11.500,0.9340,0.06066,0.05599,0.0317,0.0666,1.0000 11.750,0.9130,0.06496,0.06043,0.0325,0.0671,1.0000 12.000,0.8966,0.07018,0.06574,0.0321,0.0677,1.0000