Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca64210-il-50000-n5 Airfoil,naca64210-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,32.1903 Max Cl/Cd alpha,5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca64210-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.5569,0.09848,0.09133,-0.0223,1.0000,0.0524 -9.750,-0.5592,0.09323,0.08613,-0.0253,1.0000,0.0518 -9.500,-0.5643,0.08737,0.08032,-0.0293,1.0000,0.0514 -9.250,-0.5723,0.08163,0.07462,-0.0334,1.0000,0.0506 -9.000,-0.5847,0.07644,0.06945,-0.0368,1.0000,0.0500 -8.750,-0.5984,0.07200,0.06499,-0.0387,1.0000,0.0494 -8.500,-0.6084,0.06759,0.06047,-0.0400,1.0000,0.0493 -8.250,-0.6147,0.06340,0.05612,-0.0408,1.0000,0.0495 -8.000,-0.6169,0.05941,0.05189,-0.0410,1.0000,0.0500 -7.750,-0.6157,0.05555,0.04773,-0.0409,1.0000,0.0506 -7.500,-0.6111,0.05180,0.04361,-0.0404,1.0000,0.0512 -7.250,-0.6029,0.04822,0.03965,-0.0396,1.0000,0.0513 -7.000,-0.5918,0.04485,0.03587,-0.0387,1.0000,0.0514 -6.750,-0.5782,0.04175,0.03234,-0.0376,1.0000,0.0518 -6.500,-0.5625,0.03891,0.02902,-0.0364,1.0000,0.0524 -6.250,-0.5451,0.03649,0.02609,-0.0350,1.0000,0.0542 -6.000,-0.5272,0.03422,0.02358,-0.0339,1.0000,0.0569 -5.750,-0.5081,0.03236,0.02158,-0.0328,1.0000,0.0597 -5.500,-0.4875,0.03058,0.01959,-0.0314,1.0000,0.0617 -5.250,-0.4664,0.02899,0.01780,-0.0299,1.0000,0.0642 -5.000,-0.4458,0.02776,0.01630,-0.0283,1.0000,0.0686 -4.750,-0.4279,0.02653,0.01514,-0.0267,1.0000,0.0742 -4.500,-0.4097,0.02551,0.01399,-0.0248,1.0000,0.0793 -4.250,-0.3931,0.02449,0.01290,-0.0230,1.0000,0.0848 -4.000,-0.3766,0.02365,0.01199,-0.0214,1.0000,0.0960 -3.750,-0.3601,0.02265,0.01096,-0.0200,1.0000,0.1096 -3.500,-0.3428,0.02148,0.00995,-0.0191,1.0000,0.1342 -3.250,-0.3301,0.01887,0.00900,-0.0185,1.0000,0.3639 -3.000,-0.3224,0.01845,0.00949,-0.0137,1.0000,0.6063 -2.750,-0.3143,0.01872,0.00997,-0.0086,0.9994,0.7017 -2.500,-0.3029,0.01961,0.01110,-0.0015,0.9879,0.8014 -2.250,-0.2806,0.02010,0.01146,0.0021,0.9786,0.8540 -2.000,-0.2434,0.02008,0.01114,0.0001,0.9701,0.8701 -1.750,-0.2029,0.02006,0.01085,-0.0028,0.9623,0.8840 -1.500,-0.1643,0.02001,0.01055,-0.0055,0.9536,0.8972 -1.250,-0.1230,0.01998,0.01032,-0.0087,0.9459,0.9103 -1.000,-0.0797,0.01997,0.01013,-0.0123,0.9383,0.9231 -0.750,-0.0333,0.01996,0.00996,-0.0166,0.9313,0.9348 -0.500,0.0153,0.01995,0.00983,-0.0213,0.9245,0.9458 -0.250,0.0654,0.01994,0.00972,-0.0264,0.9181,0.9567 0.000,0.1144,0.01993,0.00965,-0.0313,0.9108,0.9678 0.250,0.1658,0.01990,0.00959,-0.0367,0.9045,0.9782 0.500,0.2131,0.01988,0.00958,-0.0414,0.8963,0.9905 0.750,0.2514,0.01992,0.00963,-0.0444,0.8875,1.0000 1.000,0.2782,0.02000,0.00972,-0.0450,0.8778,1.0000 1.250,0.2956,0.02018,0.00994,-0.0440,0.8657,1.0000 1.500,0.3139,0.02041,0.01018,-0.0430,0.8544,1.0000 1.750,0.3368,0.02063,0.01043,-0.0427,0.8448,1.0000 2.000,0.3618,0.02088,0.01073,-0.0428,0.8356,1.0000 2.250,0.3831,0.02121,0.01114,-0.0422,0.8250,1.0000 2.500,0.4101,0.02149,0.01151,-0.0424,0.8163,1.0000 2.750,0.4363,0.02179,0.01191,-0.0424,0.8067,1.0000 3.000,0.4598,0.02214,0.01242,-0.0420,0.7956,1.0000 3.250,0.4865,0.02243,0.01285,-0.0420,0.7852,1.0000 3.500,0.5167,0.02261,0.01322,-0.0421,0.7757,1.0000 3.750,0.5408,0.02293,0.01374,-0.0415,0.7630,1.0000 4.000,0.5680,0.02300,0.01407,-0.0408,0.7483,1.0000 4.250,0.5958,0.02234,0.01361,-0.0384,0.7198,1.0000 4.500,0.6177,0.02072,0.01195,-0.0328,0.6551,1.0000 4.750,0.6345,0.02006,0.01113,-0.0283,0.5728,1.0000 5.000,0.6496,0.02018,0.01090,-0.0246,0.4289,1.0000 5.250,0.6504,0.02269,0.01165,-0.0208,0.1882,1.0000 5.500,0.6603,0.02492,0.01325,-0.0191,0.1223,1.0000 5.750,0.6749,0.02659,0.01474,-0.0177,0.1003,1.0000 6.000,0.6923,0.02803,0.01622,-0.0163,0.0887,1.0000 6.250,0.7118,0.02940,0.01768,-0.0152,0.0786,1.0000 6.500,0.7337,0.03094,0.01925,-0.0144,0.0715,1.0000 6.750,0.7620,0.03248,0.02100,-0.0138,0.0661,1.0000 7.000,0.7889,0.03427,0.02274,-0.0137,0.0606,1.0000 7.250,0.8182,0.03626,0.02505,-0.0134,0.0566,1.0000 7.500,0.8460,0.03869,0.02780,-0.0131,0.0543,1.0000 7.750,0.8703,0.04131,0.03080,-0.0126,0.0526,1.0000 8.000,0.8908,0.04388,0.03362,-0.0120,0.0503,1.0000 8.250,0.9088,0.04708,0.03688,-0.0117,0.0479,1.0000 8.500,0.9209,0.05004,0.04048,-0.0102,0.0466,1.0000 8.750,0.9303,0.05356,0.04451,-0.0088,0.0460,1.0000 9.000,0.9356,0.05731,0.04872,-0.0074,0.0457,1.0000 9.250,0.9369,0.06117,0.05298,-0.0061,0.0456,1.0000 9.500,0.9337,0.06513,0.05729,-0.0048,0.0456,1.0000 9.750,0.9261,0.06913,0.06159,-0.0037,0.0456,1.0000 10.000,0.9136,0.07302,0.06571,-0.0026,0.0458,1.0000 10.250,0.8977,0.07705,0.06992,-0.0020,0.0459,1.0000 10.500,0.8806,0.08154,0.07455,-0.0027,0.0462,1.0000 10.750,0.8629,0.08667,0.07979,-0.0047,0.0464,1.0000 11.000,0.8460,0.09244,0.08564,-0.0077,0.0467,1.0000