Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe429-il-100000 Airfoil,goe429-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,35.5418 Max Cl/Cd alpha,6.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe429-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.250,-0.9074,0.09431,0.08937,0.0117,1.0000,0.0738 -12.000,-0.9377,0.08407,0.07907,0.0049,1.0000,0.0728 -11.750,-0.9732,0.07448,0.06935,-0.0021,1.0000,0.0714 -11.500,-1.0089,0.06658,0.06123,-0.0074,1.0000,0.0701 -11.250,-1.0393,0.06087,0.05524,-0.0092,1.0000,0.0696 -11.000,-1.0563,0.05600,0.04999,-0.0095,1.0000,0.0702 -10.750,-1.0653,0.05144,0.04496,-0.0093,1.0000,0.0716 -10.500,-1.0687,0.04716,0.04004,-0.0086,1.0000,0.0735 -10.250,-1.0594,0.04336,0.03597,-0.0082,1.0000,0.0763 -10.000,-1.0405,0.04167,0.03426,-0.0078,1.0000,0.0812 -9.750,-1.0301,0.03912,0.03097,-0.0069,1.0000,0.0864 -9.500,-1.0090,0.03653,0.02858,-0.0067,1.0000,0.0926 -9.250,-0.9919,0.03437,0.02590,-0.0061,1.0000,0.1002 -9.000,-0.9694,0.03255,0.02420,-0.0059,1.0000,0.1083 -8.750,-0.9480,0.03059,0.02205,-0.0055,1.0000,0.1167 -8.500,-0.9254,0.02934,0.02058,-0.0052,1.0000,0.1261 -8.250,-0.9013,0.02790,0.01926,-0.0050,1.0000,0.1349 -8.000,-0.8772,0.02654,0.01772,-0.0047,1.0000,0.1440 -7.750,-0.8520,0.02550,0.01662,-0.0045,1.0000,0.1531 -7.500,-0.8264,0.02437,0.01554,-0.0043,1.0000,0.1618 -7.250,-0.8005,0.02330,0.01434,-0.0040,1.0000,0.1717 -7.000,-0.7744,0.02242,0.01343,-0.0038,1.0000,0.1827 -6.750,-0.7483,0.02144,0.01254,-0.0036,1.0000,0.1945 -6.500,-0.7222,0.02051,0.01164,-0.0034,1.0000,0.2092 -6.250,-0.6961,0.01957,0.01074,-0.0033,1.0000,0.2283 -6.000,-0.6705,0.01858,0.00995,-0.0030,1.0000,0.2532 -5.750,-0.6452,0.01770,0.00928,-0.0028,1.0000,0.2882 -5.500,-0.6192,0.01707,0.00879,-0.0026,1.0000,0.3260 -5.250,-0.5928,0.01664,0.00847,-0.0023,1.0000,0.3586 -5.000,-0.5659,0.01630,0.00819,-0.0021,1.0000,0.3877 -4.750,-0.5389,0.01597,0.00798,-0.0019,1.0000,0.4131 -4.500,-0.5115,0.01566,0.00771,-0.0017,1.0000,0.4392 -4.250,-0.4843,0.01536,0.00752,-0.0015,1.0000,0.4641 -4.000,-0.4570,0.01508,0.00733,-0.0013,1.0000,0.4894 -3.750,-0.4298,0.01484,0.00719,-0.0010,1.0000,0.5157 -3.500,-0.4032,0.01469,0.00719,-0.0005,1.0000,0.5413 -3.250,-0.3767,0.01462,0.00723,-0.0001,1.0000,0.5685 -3.000,-0.3512,0.01462,0.00737,0.0006,1.0000,0.5923 -2.750,-0.3268,0.01460,0.00742,0.0012,1.0000,0.6158 -2.500,-0.3062,0.01463,0.00755,0.0024,1.0000,0.6350 -2.250,-0.2875,0.01466,0.00764,0.0036,1.0000,0.6534 -2.000,-0.2685,0.01469,0.00772,0.0046,1.0000,0.6717 -1.750,-0.2486,0.01473,0.00780,0.0054,1.0000,0.6900 -1.500,-0.2062,0.01474,0.00781,0.0022,0.9894,0.7122 -1.250,-0.1562,0.01470,0.00787,-0.0018,0.9751,0.7324 -1.000,-0.1076,0.01463,0.00787,-0.0054,0.9595,0.7529 -0.750,-0.0648,0.01456,0.00784,-0.0075,0.9411,0.7732 -0.500,-0.0334,0.01451,0.00783,-0.0073,0.9197,0.7927 -0.250,-0.0093,0.01447,0.00785,-0.0053,0.8984,0.8113 0.000,0.0107,0.01444,0.00787,-0.0022,0.8785,0.8316 0.250,0.0289,0.01439,0.00786,0.0011,0.8579,0.8542 0.500,0.0471,0.01430,0.00782,0.0044,0.8369,0.8768 0.750,0.0674,0.01419,0.00772,0.0074,0.8161,0.8988 1.000,0.0915,0.01405,0.00757,0.0095,0.7947,0.9211 1.250,0.1238,0.01393,0.00744,0.0098,0.7690,0.9419 1.500,0.1629,0.01382,0.00727,0.0086,0.7415,0.9615 1.750,0.2066,0.01372,0.00711,0.0063,0.7096,0.9801 2.000,0.2550,0.01361,0.00691,0.0027,0.6704,0.9971 2.250,0.2770,0.01345,0.00665,0.0033,0.6346,1.0000 2.500,0.2946,0.01336,0.00643,0.0047,0.5938,1.0000 2.750,0.3164,0.01341,0.00625,0.0056,0.5441,1.0000 3.000,0.3411,0.01368,0.00618,0.0061,0.4899,1.0000 3.250,0.3670,0.01419,0.00632,0.0063,0.4416,1.0000 3.500,0.3936,0.01481,0.00661,0.0064,0.4050,1.0000 3.750,0.4210,0.01542,0.00701,0.0063,0.3761,1.0000 4.000,0.4486,0.01604,0.00747,0.0062,0.3538,1.0000 4.250,0.4763,0.01658,0.00791,0.0061,0.3335,1.0000 4.500,0.5037,0.01706,0.00828,0.0061,0.3144,1.0000 4.750,0.5311,0.01753,0.00869,0.0060,0.2978,1.0000 5.000,0.5587,0.01804,0.00918,0.0060,0.2846,1.0000 5.250,0.5861,0.01853,0.00965,0.0059,0.2720,1.0000 5.500,0.6133,0.01902,0.01008,0.0059,0.2600,1.0000 5.750,0.6404,0.01939,0.01049,0.0059,0.2464,1.0000 6.000,0.6672,0.01971,0.01085,0.0060,0.2306,1.0000 6.250,0.6936,0.02006,0.01124,0.0060,0.2137,1.0000 6.500,0.7199,0.02034,0.01169,0.0060,0.1888,1.0000 6.750,0.7446,0.02095,0.01219,0.0061,0.1536,1.0000 7.000,0.7692,0.02197,0.01311,0.0064,0.1269,1.0000 7.250,0.7939,0.02312,0.01421,0.0068,0.1142,1.0000 7.500,0.8185,0.02438,0.01546,0.0072,0.1068,1.0000 7.750,0.8432,0.02551,0.01660,0.0076,0.1008,1.0000 8.000,0.8674,0.02688,0.01798,0.0079,0.0961,1.0000 8.250,0.8919,0.02827,0.01955,0.0084,0.0920,1.0000 8.500,0.9159,0.02975,0.02110,0.0088,0.0891,1.0000 8.750,0.9397,0.03146,0.02278,0.0091,0.0868,1.0000 9.000,0.9617,0.03366,0.02525,0.0096,0.0848,1.0000 9.250,0.9815,0.03592,0.02790,0.0100,0.0825,1.0000 9.500,0.9995,0.03847,0.03080,0.0105,0.0808,1.0000 9.750,1.0145,0.04154,0.03424,0.0110,0.0798,1.0000 10.000,1.0261,0.04485,0.03791,0.0114,0.0789,1.0000 10.250,1.0372,0.04790,0.04122,0.0118,0.0777,1.0000 10.500,1.0484,0.05079,0.04426,0.0121,0.0763,1.0000 10.750,1.0517,0.05485,0.04856,0.0123,0.0755,1.0000 11.000,1.0337,0.06031,0.05453,0.0120,0.0760,1.0000 11.250,0.8384,0.09555,0.09058,-0.0151,0.0873,1.0000 11.500,0.8469,0.09777,0.09278,-0.0145,0.0865,1.0000