Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-s6062-il-100000 Airfoil,s6062-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,50.4446 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-s6062-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.5270,0.11791,0.11292,0.0005,1.0000,0.0805 -9.750,-0.5375,0.11541,0.11051,-0.0050,1.0000,0.0826 -9.500,-0.5490,0.11270,0.10789,-0.0107,1.0000,0.0831 -9.250,-0.5219,0.10634,0.10148,-0.0054,1.0000,0.0859 -9.000,-0.5129,0.10281,0.09796,-0.0054,1.0000,0.0894 -8.750,-0.5116,0.09939,0.09458,-0.0075,1.0000,0.0929 -8.500,-0.5278,0.09635,0.09167,-0.0144,1.0000,0.0960 -8.250,-0.4269,0.08244,0.07806,-0.0149,1.0000,0.1081 -8.000,-0.4543,0.07871,0.07445,-0.0215,1.0000,0.1099 -7.750,-0.4814,0.07409,0.06985,-0.0289,1.0000,0.1103 -7.500,-0.4281,0.07000,0.06573,-0.0180,1.0000,0.1179 -7.250,-0.5207,0.07537,0.07088,-0.0259,1.0000,0.1123 -7.000,-0.5080,0.07238,0.06792,-0.0241,1.0000,0.1167 -6.750,-0.5147,0.06721,0.06259,-0.0323,1.0000,0.1251 -6.500,-0.4985,0.06408,0.05954,-0.0293,1.0000,0.1290 -6.250,-0.4946,0.05984,0.05515,-0.0327,1.0000,0.1399 -6.000,-0.4866,0.05663,0.05178,-0.0341,1.0000,0.1528 -5.750,-0.4757,0.05363,0.04875,-0.0336,1.0000,0.1669 -5.250,-0.4402,0.03877,0.03275,-0.0364,1.0000,0.0887 -5.000,-0.4198,0.03191,0.02442,-0.0342,1.0000,0.0578 -4.750,-0.4006,0.02918,0.02142,-0.0327,1.0000,0.0556 -4.500,-0.3814,0.02632,0.01822,-0.0312,1.0000,0.0537 -4.250,-0.3605,0.02397,0.01550,-0.0297,1.0000,0.0527 -4.000,-0.3387,0.02200,0.01320,-0.0281,1.0000,0.0529 -3.750,-0.3166,0.02040,0.01138,-0.0267,1.0000,0.0542 -3.500,-0.2946,0.01912,0.00991,-0.0252,1.0000,0.0567 -3.250,-0.2743,0.01772,0.00861,-0.0240,1.0000,0.0654 -3.000,-0.2537,0.01655,0.00748,-0.0226,1.0000,0.0816 -2.750,-0.2348,0.01378,0.00608,-0.0215,1.0000,0.2900 -2.500,-0.2252,0.01207,0.00625,-0.0175,1.0000,0.6751 -2.250,-0.2115,0.01182,0.00646,-0.0123,1.0000,0.8837 -2.000,-0.1301,0.01178,0.00594,-0.0220,1.0000,1.0000 -1.750,-0.1216,0.01181,0.00575,-0.0195,1.0000,1.0000 -1.500,-0.1077,0.01191,0.00563,-0.0179,1.0000,1.0000 -1.250,-0.0913,0.01206,0.00558,-0.0168,1.0000,1.0000 -1.000,-0.0738,0.01225,0.00559,-0.0158,1.0000,1.0000 -0.750,-0.0556,0.01248,0.00564,-0.0151,1.0000,1.0000 -0.500,-0.0107,0.01288,0.00586,-0.0194,0.9913,1.0000 -0.250,0.0390,0.01329,0.00612,-0.0244,0.9812,1.0000 0.000,0.0896,0.01364,0.00634,-0.0295,0.9709,1.0000 0.250,0.1364,0.01389,0.00652,-0.0337,0.9591,1.0000 0.500,0.1831,0.01410,0.00668,-0.0378,0.9471,1.0000 0.750,0.2309,0.01424,0.00680,-0.0419,0.9354,1.0000 1.000,0.2809,0.01429,0.00687,-0.0463,0.9240,1.0000 1.250,0.3269,0.01429,0.00691,-0.0496,0.9117,1.0000 1.500,0.3672,0.01427,0.00694,-0.0517,0.8977,1.0000 1.750,0.4016,0.01424,0.00695,-0.0524,0.8819,1.0000 2.000,0.4325,0.01420,0.00695,-0.0522,0.8653,1.0000 2.250,0.4609,0.01412,0.00696,-0.0514,0.8483,1.0000 2.500,0.4875,0.01404,0.00690,-0.0501,0.8313,1.0000 2.750,0.5102,0.01404,0.00696,-0.0483,0.8108,1.0000 3.000,0.5342,0.01398,0.00692,-0.0465,0.7912,1.0000 3.250,0.5573,0.01395,0.00694,-0.0446,0.7697,1.0000 3.500,0.5810,0.01388,0.00694,-0.0427,0.7476,1.0000 3.750,0.6041,0.01388,0.00698,-0.0409,0.7219,1.0000 4.000,0.6274,0.01388,0.00701,-0.0391,0.6943,1.0000 4.250,0.6508,0.01390,0.00705,-0.0373,0.6643,1.0000 4.500,0.6740,0.01399,0.00719,-0.0356,0.6302,1.0000 4.750,0.6970,0.01413,0.00731,-0.0339,0.5925,1.0000 5.000,0.7183,0.01430,0.00741,-0.0319,0.5393,1.0000 5.250,0.7375,0.01462,0.00748,-0.0298,0.4652,1.0000 5.500,0.7554,0.01529,0.00776,-0.0279,0.3716,1.0000 5.750,0.7721,0.01642,0.00838,-0.0263,0.2604,1.0000 6.000,0.7793,0.01959,0.01022,-0.0238,0.0931,1.0000 6.250,0.7960,0.02151,0.01200,-0.0220,0.0706,1.0000 6.500,0.8158,0.02308,0.01360,-0.0205,0.0616,1.0000 6.750,0.8361,0.02496,0.01539,-0.0194,0.0553,1.0000 7.000,0.8605,0.02680,0.01738,-0.0184,0.0524,1.0000 7.250,0.8858,0.02898,0.01976,-0.0175,0.0506,1.0000 7.500,0.9106,0.03150,0.02254,-0.0167,0.0497,1.0000 7.750,0.9333,0.03449,0.02593,-0.0155,0.0497,1.0000 8.000,0.9523,0.03799,0.02998,-0.0141,0.0507,1.0000 8.250,0.9672,0.04182,0.03435,-0.0125,0.0516,1.0000 8.500,0.9780,0.04561,0.03864,-0.0109,0.0515,1.0000 8.750,0.9845,0.04977,0.04328,-0.0093,0.0518,1.0000 9.000,0.9872,0.05451,0.04843,-0.0079,0.0534,1.0000 9.250,0.9908,0.05989,0.05399,-0.0070,0.0555,1.0000 9.500,0.9611,0.06648,0.06141,-0.0051,0.0636,1.0000 9.750,0.9388,0.07296,0.06820,-0.0047,0.0726,1.0000 10.000,0.8991,0.07942,0.07482,-0.0068,0.0757,1.0000 10.250,0.8085,0.07385,0.06947,-0.0033,0.0655,1.0000