Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-s6062-il-1000000 Airfoil,s6062-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,91.02 Max Cl/Cd alpha,2.5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-s6062-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.5322,0.08300,0.08144,-0.0128,1.0000,0.0086 -8.500,-0.5377,0.07765,0.07612,-0.0160,1.0000,0.0079 -8.250,-0.5410,0.07347,0.07197,-0.0189,1.0000,0.0088 -8.000,-0.5505,0.06797,0.06649,-0.0244,1.0000,0.0085 -7.750,-0.5521,0.06099,0.05946,-0.0309,1.0000,0.0087 -7.500,-0.5507,0.05416,0.05253,-0.0353,1.0000,0.0087 -7.250,-0.5455,0.04757,0.04576,-0.0379,1.0000,0.0092 -7.000,-0.5328,0.04174,0.03972,-0.0387,1.0000,0.0100 -6.750,-0.5180,0.03777,0.03549,-0.0386,1.0000,0.0103 -6.500,-0.5079,0.03413,0.03156,-0.0377,1.0000,0.0104 -6.250,-0.4983,0.02503,0.02176,-0.0394,0.9948,0.0111 -6.000,-0.4691,0.02307,0.01966,-0.0411,0.9900,0.0117 -5.750,-0.4376,0.02170,0.01816,-0.0428,0.9855,0.0126 -5.500,-0.4075,0.02001,0.01624,-0.0438,0.9789,0.0138 -5.250,-0.3746,0.02042,0.01653,-0.0443,0.9720,0.0154 -4.750,-0.3302,0.01196,0.00708,-0.0414,0.9500,0.0087 -4.500,-0.3069,0.01059,0.00550,-0.0401,0.9397,0.0080 -4.250,-0.2830,0.00979,0.00457,-0.0391,0.9296,0.0080 -4.000,-0.2579,0.00919,0.00388,-0.0384,0.9194,0.0084 -3.750,-0.2322,0.00874,0.00334,-0.0379,0.9098,0.0091 -3.500,-0.2062,0.00840,0.00290,-0.0373,0.9005,0.0099 -3.250,-0.1795,0.00811,0.00255,-0.0370,0.8904,0.0103 -3.000,-0.1528,0.00778,0.00212,-0.0366,0.8807,0.0110 -2.750,-0.1259,0.00753,0.00179,-0.0362,0.8710,0.0132 -2.500,-0.0990,0.00723,0.00150,-0.0359,0.8606,0.0305 -2.250,-0.0730,0.00665,0.00128,-0.0358,0.8501,0.1280 -2.000,-0.0465,0.00628,0.00114,-0.0357,0.8397,0.2079 -1.750,-0.0202,0.00588,0.00103,-0.0355,0.8289,0.3061 -1.500,0.0057,0.00541,0.00093,-0.0354,0.8175,0.4325 -1.250,0.0315,0.00495,0.00086,-0.0351,0.8058,0.5645 -1.000,0.0575,0.00463,0.00083,-0.0348,0.7937,0.6668 -0.750,0.0832,0.00440,0.00082,-0.0342,0.7813,0.7504 -0.500,0.1095,0.00431,0.00081,-0.0337,0.7681,0.7971 -0.250,0.1357,0.00425,0.00081,-0.0332,0.7541,0.8357 0.000,0.1615,0.00422,0.00081,-0.0325,0.7392,0.8699 0.250,0.1871,0.00421,0.00082,-0.0318,0.7239,0.8979 0.500,0.2124,0.00421,0.00082,-0.0310,0.7079,0.9226 0.750,0.2382,0.00425,0.00083,-0.0304,0.6913,0.9458 1.000,0.2677,0.00429,0.00084,-0.0305,0.6737,0.9661 1.250,0.3019,0.00436,0.00084,-0.0319,0.6540,0.9810 1.500,0.3386,0.00446,0.00086,-0.0338,0.6333,0.9905 1.750,0.3752,0.00455,0.00088,-0.0358,0.6101,0.9977 2.000,0.4047,0.00467,0.00091,-0.0362,0.5864,1.0000 2.250,0.4298,0.00482,0.00096,-0.0357,0.5612,1.0000 2.500,0.4551,0.00500,0.00103,-0.0352,0.5291,1.0000 2.750,0.4798,0.00530,0.00111,-0.0347,0.4742,1.0000 3.000,0.5054,0.00556,0.00122,-0.0344,0.4333,1.0000 3.250,0.5308,0.00589,0.00135,-0.0340,0.3832,1.0000 3.500,0.5558,0.00631,0.00152,-0.0337,0.3216,1.0000 3.750,0.5808,0.00676,0.00172,-0.0334,0.2603,1.0000 4.000,0.6052,0.00734,0.00198,-0.0331,0.1894,1.0000 4.250,0.6297,0.00791,0.00226,-0.0327,0.1255,1.0000 4.500,0.6528,0.00875,0.00270,-0.0322,0.0458,1.0000 4.750,0.6779,0.00928,0.00308,-0.0319,0.0162,1.0000 5.000,0.7043,0.00957,0.00340,-0.0316,0.0145,1.0000 5.250,0.7303,0.00993,0.00379,-0.0313,0.0130,1.0000 5.500,0.7561,0.01034,0.00427,-0.0309,0.0121,1.0000 5.750,0.7809,0.01094,0.00497,-0.0304,0.0112,1.0000 6.000,0.8047,0.01170,0.00585,-0.0298,0.0108,1.0000 6.250,0.8291,0.01229,0.00651,-0.0293,0.0107,1.0000 6.500,0.8536,0.01285,0.00712,-0.0288,0.0106,1.0000 6.750,0.8775,0.01350,0.00786,-0.0282,0.0104,1.0000 7.000,0.9011,0.01420,0.00863,-0.0276,0.0101,1.0000 7.250,0.9241,0.01501,0.00952,-0.0269,0.0098,1.0000 7.500,0.9463,0.01598,0.01058,-0.0261,0.0095,1.0000 7.750,0.9678,0.01715,0.01185,-0.0251,0.0093,1.0000 8.000,0.9896,0.01825,0.01305,-0.0243,0.0090,1.0000 8.250,1.0113,0.01935,0.01425,-0.0235,0.0086,1.0000 8.500,1.0317,0.02089,0.01595,-0.0225,0.0085,1.0000 8.750,1.0515,0.02251,0.01773,-0.0215,0.0084,1.0000 9.000,1.0699,0.02441,0.01983,-0.0204,0.0083,1.0000 9.250,1.0861,0.02664,0.02229,-0.0190,0.0083,1.0000 9.500,1.1000,0.02902,0.02493,-0.0176,0.0082,1.0000 9.750,1.0960,0.03524,0.03176,-0.0141,0.0090,1.0000 10.000,1.1007,0.03807,0.03484,-0.0121,0.0086,1.0000 10.250,1.1351,0.03475,0.03112,-0.0134,0.0074,1.0000 10.500,1.1360,0.03776,0.03436,-0.0112,0.0073,1.0000 10.750,1.0680,0.03017,0.02718,-0.0047,0.0072,1.0000 11.000,1.0494,0.03324,0.03042,-0.0021,0.0072,1.0000 11.250,1.0313,0.03666,0.03403,-0.0007,0.0073,1.0000 11.500,1.0117,0.04104,0.03857,-0.0006,0.0072,1.0000 11.750,0.9917,0.04637,0.04407,-0.0018,0.0073,1.0000 12.000,0.9696,0.05288,0.05071,-0.0041,0.0072,1.0000