Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag46c03-il-50000-n5 Airfoil,ag46c03-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,33.2809 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-ag46c03-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.000,-0.5934,0.11852,0.11179,0.0269,1.0000,0.0949 -7.750,-0.6004,0.11635,0.10973,0.0215,1.0000,0.0972 -7.500,-0.6048,0.11355,0.10708,0.0160,1.0000,0.0978 -7.250,-0.5877,0.10750,0.10098,0.0195,1.0000,0.0994 -7.000,-0.5794,0.10336,0.09687,0.0190,1.0000,0.1010 -6.750,-0.5737,0.09950,0.09306,0.0174,1.0000,0.1022 -6.250,-0.5548,0.08681,0.08031,0.0031,1.0000,0.0556 -6.000,-0.5448,0.08229,0.07581,0.0019,1.0000,0.0514 -5.750,-0.5280,0.07444,0.06777,-0.0094,1.0000,0.0439 -5.500,-0.5160,0.07018,0.06351,-0.0105,1.0000,0.0427 -5.250,-0.5011,0.06544,0.05869,-0.0133,1.0000,0.0416 -5.000,-0.4839,0.06045,0.05356,-0.0166,1.0000,0.0405 -4.750,-0.4644,0.05541,0.04830,-0.0198,1.0000,0.0399 -4.500,-0.4428,0.05054,0.04313,-0.0227,1.0000,0.0402 -4.250,-0.4193,0.04590,0.03808,-0.0251,1.0000,0.0412 -4.000,-0.3942,0.04155,0.03322,-0.0268,1.0000,0.0421 -3.750,-0.3683,0.03765,0.02879,-0.0278,1.0000,0.0426 -3.500,-0.3415,0.03412,0.02470,-0.0284,1.0000,0.0429 -3.250,-0.3139,0.03098,0.02093,-0.0285,1.0000,0.0436 -3.000,-0.2861,0.02822,0.01768,-0.0283,1.0000,0.0450 -2.750,-0.2603,0.02630,0.01565,-0.0283,1.0000,0.0505 -2.500,-0.2322,0.02442,0.01334,-0.0277,1.0000,0.0561 -2.250,-0.2055,0.02256,0.01136,-0.0270,1.0000,0.0611 -2.000,-0.1787,0.02123,0.00992,-0.0265,1.0000,0.0744 -1.750,-0.1516,0.01991,0.00845,-0.0259,1.0000,0.0915 -1.500,-0.1247,0.01861,0.00727,-0.0256,1.0000,0.1304 -1.250,-0.0988,0.01698,0.00633,-0.0257,1.0000,0.2483 -1.000,-0.0853,0.01457,0.00597,-0.0224,1.0000,0.6585 -0.750,-0.0435,0.01378,0.00526,-0.0234,1.0000,1.0000 -0.500,-0.0177,0.01375,0.00483,-0.0231,1.0000,1.0000 -0.250,0.0079,0.01374,0.00454,-0.0228,1.0000,1.0000 0.000,0.0331,0.01375,0.00432,-0.0225,1.0000,1.0000 0.250,0.0579,0.01378,0.00418,-0.0223,1.0000,1.0000 0.500,0.0822,0.01385,0.00409,-0.0220,1.0000,1.0000 0.750,0.1055,0.01396,0.00411,-0.0217,1.0000,1.0000 1.000,0.1284,0.01414,0.00421,-0.0217,0.9990,1.0000 1.250,0.1761,0.01436,0.00431,-0.0261,0.9647,1.0000 1.500,0.2214,0.01456,0.00441,-0.0298,0.9302,1.0000 1.750,0.2630,0.01474,0.00451,-0.0324,0.8954,1.0000 2.000,0.2997,0.01494,0.00463,-0.0337,0.8611,1.0000 2.250,0.3315,0.01517,0.00476,-0.0338,0.8290,1.0000 2.500,0.3590,0.01544,0.00492,-0.0331,0.7981,1.0000 2.750,0.3847,0.01574,0.00512,-0.0319,0.7690,1.0000 3.000,0.4095,0.01609,0.00536,-0.0306,0.7411,1.0000 3.250,0.4339,0.01647,0.00565,-0.0293,0.7140,1.0000 3.500,0.4585,0.01686,0.00605,-0.0281,0.6848,1.0000 3.750,0.4829,0.01718,0.00638,-0.0270,0.6541,1.0000 4.000,0.5074,0.01745,0.00666,-0.0260,0.6217,1.0000 4.250,0.5317,0.01770,0.00691,-0.0248,0.5878,1.0000 4.500,0.5559,0.01797,0.00721,-0.0236,0.5521,1.0000 4.750,0.5800,0.01827,0.00746,-0.0223,0.5144,1.0000 5.000,0.6041,0.01865,0.00778,-0.0213,0.4738,1.0000 5.250,0.6282,0.01911,0.00816,-0.0203,0.4318,1.0000 5.500,0.6522,0.01966,0.00862,-0.0194,0.3893,1.0000 5.750,0.6766,0.02033,0.00927,-0.0188,0.3474,1.0000 6.000,0.7010,0.02110,0.00997,-0.0183,0.3068,1.0000 6.250,0.7254,0.02197,0.01080,-0.0179,0.2699,1.0000 6.500,0.7493,0.02294,0.01172,-0.0174,0.2378,1.0000 6.750,0.7729,0.02399,0.01280,-0.0170,0.2095,1.0000 7.000,0.7965,0.02513,0.01399,-0.0166,0.1844,1.0000 7.250,0.8197,0.02636,0.01529,-0.0160,0.1629,1.0000 7.500,0.8426,0.02767,0.01668,-0.0155,0.1434,1.0000 7.750,0.8649,0.02910,0.01813,-0.0150,0.1271,1.0000 8.000,0.8874,0.03071,0.01991,-0.0144,0.1123,1.0000 8.250,0.9091,0.03238,0.02184,-0.0139,0.0983,1.0000 8.500,0.9308,0.03437,0.02404,-0.0133,0.0883,1.0000 8.750,0.9510,0.03639,0.02640,-0.0128,0.0772,1.0000 9.000,0.9705,0.03919,0.02957,-0.0121,0.0704,1.0000 9.250,0.9885,0.04176,0.03242,-0.0116,0.0640,1.0000 9.500,1.0028,0.04504,0.03619,-0.0113,0.0579,1.0000 9.750,1.0149,0.04872,0.04035,-0.0110,0.0540,1.0000 10.000,1.0256,0.05224,0.04415,-0.0107,0.0514,1.0000 10.250,1.0300,0.05667,0.04891,-0.0108,0.0494,1.0000 10.500,1.0228,0.06241,0.05523,-0.0118,0.0483,1.0000 10.750,1.0096,0.06830,0.06150,-0.0137,0.0479,1.0000 11.000,0.9916,0.07417,0.06758,-0.0164,0.0481,1.0000 11.250,0.9730,0.08101,0.07453,-0.0215,0.0487,1.0000 11.500,0.9557,0.08877,0.08233,-0.0274,0.0493,1.0000 11.750,0.9401,0.09707,0.09064,-0.0332,0.0498,1.0000 12.000,0.9266,0.10545,0.09900,-0.0384,0.0501,1.0000