Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca63a210-il-100000 Airfoil,naca63a210-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,37.6177 Max Cl/Cd alpha,6.25 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca63a210-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.5670,0.09530,0.09078,-0.0037,0.7256,0.0921 -8.500,-0.5800,0.08917,0.08470,-0.0134,0.7256,0.0947 -8.250,-0.6019,0.08414,0.07953,-0.0220,0.7258,0.0957 -8.000,-0.5816,0.07960,0.07514,-0.0182,0.7256,0.1003 -7.750,-0.5788,0.07565,0.07113,-0.0203,0.7256,0.1060 -7.500,-0.6004,0.07114,0.06614,-0.0277,0.7258,0.1113 -7.250,-0.5745,0.06698,0.06230,-0.0248,0.7257,0.1193 -7.000,-0.5709,0.06276,0.05794,-0.0266,0.7259,0.1300 -6.750,-0.5612,0.05945,0.05452,-0.0269,0.7260,0.1460 -5.250,-0.4379,0.03512,0.02698,-0.0287,0.7265,0.0810 -5.000,-0.4091,0.03098,0.02241,-0.0277,0.7267,0.0646 -4.750,-0.3807,0.02800,0.01887,-0.0267,0.7269,0.0568 -4.500,-0.3506,0.02707,0.01748,-0.0259,0.7272,0.0536 -4.250,-0.3222,0.02460,0.01486,-0.0255,0.7276,0.0530 -4.000,-0.2946,0.02239,0.01263,-0.0252,0.7279,0.0562 -3.750,-0.2681,0.02094,0.01119,-0.0248,0.7283,0.0616 -3.500,-0.2424,0.01971,0.00994,-0.0240,0.7287,0.0655 -3.250,-0.2191,0.01848,0.00870,-0.0231,0.7291,0.0732 -3.000,-0.1952,0.01732,0.00762,-0.0224,0.7295,0.1049 -2.750,-0.1992,0.01444,0.00779,-0.0148,0.7300,0.7341 -2.500,-0.1890,0.01497,0.00851,-0.0069,0.7304,0.8421 -2.250,-0.1531,0.01606,0.00942,-0.0026,0.7304,0.9118 -2.000,-0.1116,0.01602,0.00910,-0.0054,0.7307,0.9263 -1.750,-0.0677,0.01596,0.00880,-0.0090,0.7310,0.9399 -1.500,-0.0221,0.01588,0.00851,-0.0131,0.7313,0.9530 -1.250,0.0246,0.01580,0.00822,-0.0176,0.7316,0.9660 -1.000,0.0743,0.01567,0.00795,-0.0229,0.7319,0.9778 -0.750,0.1229,0.01553,0.00770,-0.0282,0.7322,0.9899 -0.500,0.1683,0.01539,0.00746,-0.0330,0.7325,1.0000 -0.250,0.1932,0.01533,0.00738,-0.0339,0.7328,1.0000 0.000,0.2179,0.01533,0.00736,-0.0348,0.7331,1.0000 0.250,0.2417,0.01539,0.00741,-0.0353,0.7328,1.0000 0.500,0.2651,0.01551,0.00753,-0.0357,0.7322,1.0000 0.750,0.2885,0.01567,0.00770,-0.0361,0.7316,1.0000 1.000,0.3116,0.01588,0.00794,-0.0364,0.7309,1.0000 1.250,0.3350,0.01616,0.00825,-0.0367,0.7305,1.0000 1.500,0.3582,0.01649,0.00862,-0.0369,0.7289,1.0000 1.750,0.3814,0.01686,0.00906,-0.0370,0.7265,1.0000 2.000,0.4051,0.01729,0.00953,-0.0372,0.7249,1.0000 2.250,0.4290,0.01775,0.01005,-0.0373,0.7230,1.0000 2.500,0.4529,0.01825,0.01061,-0.0373,0.7210,1.0000 2.750,0.4763,0.01876,0.01113,-0.0368,0.7175,1.0000 3.000,0.4987,0.01936,0.01191,-0.0369,0.7119,1.0000 3.250,0.5214,0.01976,0.01233,-0.0357,0.7041,1.0000 3.500,0.5429,0.02032,0.01301,-0.0350,0.6948,1.0000 3.750,0.5643,0.02074,0.01348,-0.0335,0.6830,1.0000 4.000,0.5854,0.02111,0.01395,-0.0316,0.6688,1.0000 4.250,0.6063,0.02148,0.01438,-0.0296,0.6529,1.0000 4.500,0.6272,0.02188,0.01482,-0.0274,0.6359,1.0000 4.750,0.6482,0.02241,0.01536,-0.0251,0.6184,1.0000 5.000,0.6679,0.02292,0.01604,-0.0234,0.5989,1.0000 5.250,0.6896,0.02323,0.01639,-0.0211,0.5788,1.0000 5.500,0.7112,0.02366,0.01688,-0.0187,0.5570,1.0000 5.750,0.7278,0.02543,0.01872,-0.0163,0.5299,1.0000 6.000,0.7405,0.02769,0.02112,-0.0137,0.4944,1.0000 6.250,0.7753,0.02061,0.01415,-0.0116,0.3172,1.0000 6.500,0.7836,0.02212,0.01449,-0.0091,0.1909,1.0000 6.750,0.7972,0.02340,0.01533,-0.0071,0.1435,1.0000 7.000,0.8111,0.02471,0.01645,-0.0050,0.1068,1.0000 7.250,0.8226,0.02657,0.01800,-0.0023,0.0845,1.0000 7.500,0.8387,0.02820,0.01966,-0.0005,0.0678,1.0000 7.750,0.8553,0.03061,0.02191,0.0014,0.0582,1.0000 8.000,0.8758,0.03197,0.02356,0.0027,0.0497,1.0000 8.250,0.8969,0.03578,0.02729,0.0039,0.0454,1.0000 8.500,0.9173,0.03858,0.03057,0.0054,0.0440,1.0000 8.750,0.9337,0.04202,0.03450,0.0070,0.0429,1.0000 9.000,0.9453,0.04540,0.03838,0.0085,0.0412,1.0000 9.250,0.9527,0.04891,0.04232,0.0099,0.0396,1.0000 9.500,0.9547,0.05302,0.04685,0.0113,0.0394,1.0000 9.750,0.9503,0.05771,0.05194,0.0124,0.0403,1.0000 10.000,0.9414,0.06235,0.05689,0.0131,0.0413,1.0000 10.250,0.9277,0.06668,0.06144,0.0135,0.0421,1.0000 10.500,0.9117,0.07130,0.06623,0.0125,0.0427,1.0000 10.750,0.8950,0.07666,0.07173,0.0095,0.0433,1.0000 11.000,0.8787,0.08264,0.07781,0.0058,0.0439,1.0000 11.250,0.8795,0.08759,0.08283,0.0049,0.0464,1.0000 11.500,0.8339,0.09742,0.09285,-0.0044,0.0477,1.0000 11.750,0.6793,0.10057,0.09620,0.0010,0.0552,1.0000 12.000,0.6723,0.10620,0.10181,-0.0002,0.0569,1.0000