Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag46c03-il-100000 Airfoil,ag46c03-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,44.5308 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-ag46c03-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.500,-0.5888,0.10860,0.10390,0.0239,1.0000,0.0688 -7.250,-0.5927,0.10594,0.10133,0.0170,1.0000,0.0700 -7.000,-0.5910,0.10225,0.09768,0.0062,1.0000,0.0705 -6.750,-0.5819,0.09652,0.09199,0.0145,1.0000,0.0723 -6.500,-0.5710,0.09284,0.08833,0.0164,1.0000,0.0753 -6.250,-0.5631,0.08901,0.08453,0.0131,1.0000,0.0792 -6.000,-0.5502,0.08401,0.07945,-0.0033,1.0000,0.0836 -5.750,-0.5424,0.07894,0.07446,-0.0016,1.0000,0.0860 -5.500,-0.5304,0.07583,0.07137,0.0001,1.0000,0.0922 -5.250,-0.5116,0.06986,0.06522,-0.0119,1.0000,0.0990 -5.000,-0.4998,0.06680,0.06227,-0.0082,1.0000,0.1044 -4.750,-0.4791,0.06160,0.05689,-0.0154,1.0000,0.1136 -4.500,-0.4606,0.05820,0.05346,-0.0162,1.0000,0.1225 -4.250,-0.4417,0.05397,0.04917,-0.0180,1.0000,0.1307 -4.000,-0.4200,0.05010,0.04513,-0.0205,1.0000,0.1437 -3.750,-0.3980,0.04661,0.04153,-0.0219,1.0000,0.1582 -3.500,-0.3752,0.04341,0.03823,-0.0230,1.0000,0.1751 -3.250,-0.3218,0.03305,0.02633,-0.0291,1.0000,0.0815 -3.000,-0.2905,0.02758,0.02011,-0.0293,1.0000,0.0619 -2.750,-0.2590,0.02501,0.01670,-0.0286,1.0000,0.0570 -2.500,-0.2325,0.02210,0.01360,-0.0286,1.0000,0.0610 -2.250,-0.2042,0.02010,0.01132,-0.0281,1.0000,0.0634 -2.000,-0.1758,0.01829,0.00925,-0.0274,1.0000,0.0670 -1.750,-0.1485,0.01678,0.00768,-0.0269,1.0000,0.0785 -1.500,-0.1216,0.01531,0.00626,-0.0262,1.0000,0.0958 -1.250,-0.0957,0.01380,0.00511,-0.0257,1.0000,0.1488 -1.000,-0.0795,0.01051,0.00438,-0.0234,1.0000,0.6615 -0.750,-0.0412,0.00973,0.00387,-0.0235,1.0000,1.0000 -0.500,-0.0150,0.00971,0.00355,-0.0232,1.0000,1.0000 -0.250,0.0110,0.00970,0.00334,-0.0230,1.0000,1.0000 0.000,0.0366,0.00972,0.00320,-0.0228,1.0000,1.0000 0.250,0.0617,0.00977,0.00313,-0.0226,1.0000,1.0000 0.500,0.0858,0.00987,0.00313,-0.0224,1.0000,1.0000 0.750,0.1080,0.01007,0.00326,-0.0224,1.0000,1.0000 1.000,0.1371,0.01037,0.00348,-0.0240,0.9950,1.0000 1.250,0.1962,0.01051,0.00355,-0.0307,0.9703,1.0000 1.500,0.2476,0.01060,0.00357,-0.0354,0.9414,1.0000 1.750,0.2880,0.01068,0.00360,-0.0374,0.9079,1.0000 2.000,0.3191,0.01082,0.00364,-0.0373,0.8747,1.0000 2.250,0.3446,0.01100,0.00373,-0.0359,0.8434,1.0000 2.500,0.3683,0.01124,0.00385,-0.0342,0.8127,1.0000 2.750,0.3918,0.01152,0.00401,-0.0326,0.7830,1.0000 3.000,0.4153,0.01185,0.00422,-0.0310,0.7541,1.0000 3.250,0.4390,0.01221,0.00450,-0.0295,0.7258,1.0000 3.500,0.4629,0.01261,0.00479,-0.0282,0.6973,1.0000 3.750,0.4874,0.01289,0.00502,-0.0270,0.6672,1.0000 4.000,0.5123,0.01303,0.00515,-0.0259,0.6352,1.0000 4.250,0.5371,0.01314,0.00522,-0.0248,0.6018,1.0000 4.500,0.5619,0.01329,0.00534,-0.0237,0.5654,1.0000 4.750,0.5867,0.01351,0.00545,-0.0226,0.5253,1.0000 5.000,0.6114,0.01384,0.00564,-0.0216,0.4803,1.0000 5.250,0.6359,0.01428,0.00591,-0.0208,0.4329,1.0000 5.500,0.6604,0.01484,0.00633,-0.0200,0.3825,1.0000 5.750,0.6848,0.01555,0.00681,-0.0194,0.3343,1.0000 6.000,0.7092,0.01637,0.00742,-0.0188,0.2901,1.0000 6.250,0.7337,0.01725,0.00814,-0.0183,0.2517,1.0000 6.500,0.7583,0.01823,0.00900,-0.0179,0.2200,1.0000 6.750,0.7828,0.01925,0.00999,-0.0174,0.1926,1.0000 7.000,0.8074,0.02036,0.01104,-0.0170,0.1691,1.0000 7.250,0.8319,0.02157,0.01232,-0.0165,0.1476,1.0000 7.500,0.8561,0.02287,0.01360,-0.0160,0.1295,1.0000 7.750,0.8800,0.02453,0.01519,-0.0156,0.1138,1.0000 8.000,0.9037,0.02621,0.01704,-0.0150,0.0996,1.0000 8.250,0.9274,0.02802,0.01902,-0.0145,0.0881,1.0000 8.500,0.9502,0.02986,0.02125,-0.0138,0.0776,1.0000 8.750,0.9715,0.03304,0.02482,-0.0130,0.0714,1.0000 9.000,0.9925,0.03488,0.02680,-0.0126,0.0635,1.0000 9.250,1.0085,0.03916,0.03171,-0.0118,0.0602,1.0000 9.500,1.0204,0.04402,0.03734,-0.0111,0.0584,1.0000 9.750,1.0269,0.04923,0.04320,-0.0108,0.0567,1.0000 10.000,1.0448,0.05080,0.04469,-0.0104,0.0516,1.0000 10.250,1.0468,0.05655,0.05074,-0.0105,0.0504,1.0000 10.500,1.0424,0.06201,0.05670,-0.0109,0.0508,1.0000 10.750,0.9817,0.07494,0.07044,-0.0181,0.0583,1.0000 11.000,0.9635,0.08219,0.07775,-0.0236,0.0599,1.0000 11.250,0.9499,0.08966,0.08522,-0.0286,0.0610,1.0000 11.500,0.9410,0.09671,0.09226,-0.0320,0.0617,1.0000