Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n63010a-il-500000-n5 Airfoil,n63010a-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,51.0015 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-n63010a-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.750,-0.9715,0.06212,0.05959,-0.0152,1.0000,0.0066 -12.500,-1.0090,0.05253,0.04968,-0.0210,1.0000,0.0065 -12.250,-1.0246,0.04761,0.04456,-0.0229,1.0000,0.0066 -12.000,-1.0348,0.04398,0.04073,-0.0233,1.0000,0.0066 -11.750,-1.0411,0.04115,0.03773,-0.0226,1.0000,0.0067 -11.500,-1.0423,0.03908,0.03550,-0.0211,1.0000,0.0068 -11.250,-1.0406,0.03727,0.03353,-0.0193,1.0000,0.0070 -11.000,-1.0347,0.03539,0.03144,-0.0178,1.0000,0.0072 -10.750,-1.0266,0.03343,0.02925,-0.0164,1.0000,0.0075 -10.500,-1.0168,0.03141,0.02699,-0.0150,1.0000,0.0079 -10.250,-1.0051,0.02939,0.02470,-0.0137,1.0000,0.0082 -10.000,-0.9911,0.02752,0.02256,-0.0124,1.0000,0.0085 -9.750,-0.9747,0.02593,0.02073,-0.0113,1.0000,0.0088 -9.500,-0.9563,0.02465,0.01924,-0.0104,1.0000,0.0090 -9.250,-0.9409,0.02260,0.01695,-0.0091,1.0000,0.0094 -9.000,-0.9218,0.02136,0.01558,-0.0083,1.0000,0.0097 -8.750,-0.9007,0.02052,0.01464,-0.0076,1.0000,0.0101 -8.500,-0.8785,0.01987,0.01392,-0.0070,1.0000,0.0105 -8.250,-0.8562,0.01920,0.01317,-0.0064,1.0000,0.0110 -8.000,-0.8340,0.01844,0.01232,-0.0057,1.0000,0.0116 -7.750,-0.8121,0.01762,0.01140,-0.0049,1.0000,0.0120 -7.500,-0.7903,0.01683,0.01050,-0.0041,1.0000,0.0123 -7.250,-0.7683,0.01612,0.00969,-0.0033,1.0000,0.0127 -7.000,-0.7461,0.01549,0.00898,-0.0024,1.0000,0.0129 -6.750,-0.7260,0.01462,0.00804,-0.0012,1.0000,0.0136 -6.500,-0.7052,0.01395,0.00734,-0.0002,1.0000,0.0144 -6.250,-0.6836,0.01344,0.00680,0.0008,1.0000,0.0150 -6.000,-0.6620,0.01298,0.00630,0.0019,1.0000,0.0157 -5.750,-0.6353,0.01252,0.00578,0.0018,0.9976,0.0164 -5.500,-0.6026,0.01207,0.00527,0.0005,0.9922,0.0173 -5.250,-0.5699,0.01167,0.00481,-0.0009,0.9859,0.0182 -5.000,-0.5382,0.01123,0.00433,-0.0019,0.9779,0.0200 -4.750,-0.5064,0.01085,0.00395,-0.0030,0.9689,0.0238 -4.500,-0.4745,0.01053,0.00361,-0.0041,0.9587,0.0290 -4.250,-0.4435,0.01022,0.00331,-0.0049,0.9467,0.0374 -4.000,-0.4143,0.00991,0.00302,-0.0053,0.9327,0.0513 -3.750,-0.3870,0.00959,0.00276,-0.0053,0.9170,0.0738 -3.500,-0.3614,0.00920,0.00250,-0.0050,0.9008,0.1153 -3.250,-0.3378,0.00860,0.00220,-0.0045,0.8845,0.2000 -3.000,-0.3162,0.00775,0.00188,-0.0037,0.8689,0.3394 -2.750,-0.2928,0.00723,0.00168,-0.0031,0.8542,0.4370 -2.500,-0.2675,0.00699,0.00156,-0.0026,0.8407,0.4896 -2.250,-0.2424,0.00676,0.00148,-0.0021,0.8277,0.5461 -2.000,-0.2171,0.00657,0.00142,-0.0016,0.8156,0.5958 -1.750,-0.1909,0.00648,0.00138,-0.0012,0.8038,0.6280 -1.500,-0.1642,0.00642,0.00134,-0.0009,0.7924,0.6507 -1.250,-0.1372,0.00638,0.00131,-0.0006,0.7813,0.6696 -1.000,-0.1100,0.00635,0.00127,-0.0005,0.7708,0.6846 -0.750,-0.0826,0.00635,0.00125,-0.0003,0.7602,0.6960 -0.500,-0.0550,0.00634,0.00123,-0.0002,0.7493,0.7067 0.000,0.0000,0.00633,0.00121,0.0000,0.7282,0.7283 0.500,0.0551,0.00634,0.00123,0.0002,0.7067,0.7493 0.750,0.0826,0.00635,0.00125,0.0003,0.6959,0.7601 1.000,0.1100,0.00635,0.00127,0.0005,0.6846,0.7708 1.250,0.1372,0.00638,0.00131,0.0006,0.6695,0.7813 1.500,0.1642,0.00642,0.00134,0.0009,0.6507,0.7924 1.750,0.1910,0.00648,0.00138,0.0012,0.6280,0.8039 2.000,0.2171,0.00657,0.00142,0.0016,0.5958,0.8156 2.250,0.2424,0.00676,0.00148,0.0021,0.5453,0.8277 2.500,0.2676,0.00699,0.00156,0.0026,0.4893,0.8407 2.750,0.2929,0.00723,0.00168,0.0031,0.4369,0.8541 3.000,0.3163,0.00774,0.00188,0.0037,0.3402,0.8687 3.250,0.3380,0.00859,0.00220,0.0044,0.2011,0.8843 3.500,0.3615,0.00920,0.00250,0.0050,0.1151,0.9007 3.750,0.3871,0.00959,0.00276,0.0053,0.0738,0.9169 4.000,0.4143,0.00991,0.00302,0.0053,0.0513,0.9328 4.250,0.4435,0.01022,0.00331,0.0049,0.0373,0.9467 4.500,0.4745,0.01053,0.00361,0.0040,0.0290,0.9586 4.750,0.5064,0.01085,0.00395,0.0030,0.0238,0.9688 5.000,0.5382,0.01123,0.00433,0.0019,0.0200,0.9779 5.250,0.5699,0.01167,0.00481,0.0009,0.0182,0.9859 5.500,0.6026,0.01207,0.00527,-0.0005,0.0173,0.9923 5.750,0.6353,0.01252,0.00578,-0.0018,0.0164,0.9977 6.000,0.6620,0.01298,0.00630,-0.0019,0.0156,1.0000 6.250,0.6836,0.01344,0.00680,-0.0008,0.0150,1.0000 6.500,0.7052,0.01395,0.00733,0.0002,0.0144,1.0000 6.750,0.7260,0.01462,0.00804,0.0012,0.0136,1.0000 7.000,0.7461,0.01549,0.00898,0.0024,0.0129,1.0000 7.250,0.7683,0.01612,0.00969,0.0033,0.0127,1.0000 7.500,0.7903,0.01683,0.01051,0.0041,0.0123,1.0000 7.750,0.8122,0.01762,0.01140,0.0049,0.0120,1.0000 8.000,0.8341,0.01845,0.01233,0.0057,0.0116,1.0000 8.250,0.8563,0.01920,0.01318,0.0064,0.0111,1.0000 8.500,0.8788,0.01987,0.01392,0.0070,0.0105,1.0000 8.750,0.9009,0.02053,0.01465,0.0075,0.0101,1.0000 9.000,0.9222,0.02137,0.01560,0.0082,0.0097,1.0000 9.250,0.9414,0.02260,0.01695,0.0090,0.0094,1.0000 9.500,0.9567,0.02467,0.01926,0.0103,0.0090,1.0000 9.750,0.9752,0.02595,0.02075,0.0112,0.0088,1.0000 10.000,0.9916,0.02754,0.02258,0.0123,0.0085,1.0000 10.250,1.0056,0.02941,0.02472,0.0136,0.0082,1.0000 10.500,1.0174,0.03142,0.02699,0.0149,0.0079,1.0000 10.750,1.0273,0.03344,0.02926,0.0163,0.0075,1.0000 11.000,1.0354,0.03542,0.03147,0.0176,0.0072,1.0000 11.250,1.0419,0.03723,0.03349,0.0190,0.0070,1.0000 11.500,1.0441,0.03901,0.03542,0.0209,0.0068,1.0000 11.750,1.0421,0.04119,0.03776,0.0223,0.0067,1.0000 12.000,1.0363,0.04396,0.04071,0.0230,0.0066,1.0000 12.250,1.0266,0.04755,0.04449,0.0227,0.0066,1.0000 12.500,1.0114,0.05241,0.04955,0.0208,0.0065,1.0000 12.750,0.9725,0.06225,0.05972,0.0148,0.0066,1.0000