Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe411-il-1000000 Airfoil,goe411-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,48.6812 Max Cl/Cd alpha,6.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe411-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.500,-0.7000,0.08704,0.08492,-0.0438,1.0000,0.0079 -13.250,-0.7131,0.08155,0.07936,-0.0469,1.0000,0.0079 -13.000,-0.7329,0.07559,0.07330,-0.0502,1.0000,0.0079 -12.750,-0.7494,0.07066,0.06826,-0.0525,1.0000,0.0079 -12.500,-0.7714,0.06595,0.06342,-0.0543,1.0000,0.0079 -12.250,-0.7921,0.06193,0.05927,-0.0548,1.0000,0.0079 -12.000,-0.8104,0.05868,0.05589,-0.0541,1.0000,0.0079 -11.750,-0.8219,0.05581,0.05293,-0.0528,1.0000,0.0079 -11.500,-0.8404,0.05330,0.05029,-0.0501,1.0000,0.0079 -11.250,-0.8665,0.05129,0.04811,-0.0453,1.0000,0.0080 -11.000,-0.8840,0.04956,0.04627,-0.0404,1.0000,0.0080 -10.750,-0.9074,0.04833,0.04492,-0.0333,1.0000,0.0080 -10.500,-0.9212,0.04679,0.04328,-0.0275,1.0000,0.0080 -10.250,-0.9356,0.04492,0.04126,-0.0216,1.0000,0.0080 -10.000,-0.9469,0.04324,0.03941,-0.0160,1.0000,0.0080 -9.750,-0.9521,0.04132,0.03735,-0.0113,1.0000,0.0080 -9.500,-0.9606,0.03962,0.03545,-0.0058,1.0000,0.0080 -8.750,-0.9139,0.02658,0.02171,-0.0035,0.9961,0.0073 -8.500,-0.8859,0.02452,0.01946,-0.0043,0.9948,0.0073 -8.250,-0.8573,0.02309,0.01790,-0.0050,0.9931,0.0075 -8.000,-0.8301,0.02106,0.01574,-0.0053,0.9913,0.0074 -7.750,-0.8030,0.01934,0.01394,-0.0056,0.9896,0.0074 -7.500,-0.7738,0.01823,0.01274,-0.0064,0.9876,0.0076 -7.250,-0.7432,0.01744,0.01189,-0.0074,0.9859,0.0079 -7.000,-0.7197,0.01554,0.00992,-0.0074,0.9841,0.0084 -6.750,-0.6934,0.01449,0.00884,-0.0078,0.9819,0.0090 -6.500,-0.6711,0.01386,0.00817,-0.0070,0.9771,0.0094 -6.250,-0.6417,0.01323,0.00750,-0.0077,0.9744,0.0100 -6.000,-0.6107,0.01259,0.00680,-0.0087,0.9725,0.0106 -5.750,-0.5773,0.01218,0.00637,-0.0103,0.9712,0.0115 -5.500,-0.5438,0.01174,0.00590,-0.0117,0.9701,0.0121 -5.250,-0.5241,0.01107,0.00513,-0.0101,0.9645,0.0130 -5.000,-0.4956,0.01050,0.00449,-0.0105,0.9614,0.0147 -4.750,-0.4622,0.01011,0.00405,-0.0119,0.9593,0.0164 -4.500,-0.4263,0.00980,0.00372,-0.0139,0.9576,0.0182 -4.250,-0.3907,0.00944,0.00331,-0.0157,0.9558,0.0252 -4.000,-0.3802,0.00821,0.00270,-0.0126,0.9461,0.1729 -3.750,-0.3505,0.00749,0.00235,-0.0136,0.9421,0.2540 -3.500,-0.3321,0.00695,0.00212,-0.0119,0.9324,0.3293 -3.250,-0.3043,0.00654,0.00192,-0.0122,0.9253,0.3882 -3.000,-0.2783,0.00627,0.00178,-0.0119,0.9159,0.4307 -2.750,-0.2528,0.00606,0.00167,-0.0115,0.9052,0.4652 -2.500,-0.2260,0.00591,0.00157,-0.0114,0.8940,0.4912 -2.250,-0.1994,0.00580,0.00148,-0.0112,0.8816,0.5123 -2.000,-0.1730,0.00573,0.00140,-0.0109,0.8681,0.5256 -1.750,-0.1476,0.00569,0.00133,-0.0104,0.8531,0.5384 -1.500,-0.1232,0.00566,0.00127,-0.0096,0.8345,0.5510 -1.250,-0.0997,0.00564,0.00122,-0.0086,0.8157,0.5660 -1.000,-0.0774,0.00561,0.00118,-0.0074,0.7953,0.5838 -0.750,-0.0556,0.00561,0.00114,-0.0061,0.7717,0.5989 -0.500,-0.0348,0.00562,0.00110,-0.0046,0.7417,0.6141 -0.250,-0.0166,0.00567,0.00107,-0.0024,0.6993,0.6318 0.000,-0.0001,0.00572,0.00105,0.0000,0.6573,0.6579 0.250,0.0167,0.00567,0.00107,0.0024,0.6317,0.6983 0.500,0.0346,0.00561,0.00110,0.0046,0.6140,0.7431 0.750,0.0555,0.00561,0.00114,0.0061,0.5988,0.7722 1.000,0.0773,0.00561,0.00118,0.0075,0.5832,0.7951 1.500,0.1231,0.00566,0.00127,0.0096,0.5506,0.8349 1.750,0.1476,0.00569,0.00133,0.0104,0.5380,0.8524 2.000,0.1730,0.00573,0.00140,0.0109,0.5256,0.8680 2.250,0.1992,0.00580,0.00148,0.0112,0.5110,0.8816 2.500,0.2260,0.00591,0.00157,0.0114,0.4911,0.8940 2.750,0.2528,0.00606,0.00167,0.0115,0.4649,0.9051 3.000,0.2781,0.00627,0.00178,0.0120,0.4302,0.9158 3.250,0.3041,0.00655,0.00192,0.0122,0.3864,0.9253 3.500,0.3320,0.00695,0.00212,0.0119,0.3294,0.9324 3.750,0.3512,0.00743,0.00233,0.0135,0.2629,0.9420 4.000,0.3806,0.00819,0.00270,0.0125,0.1761,0.9461 4.250,0.3910,0.00943,0.00331,0.0156,0.0259,0.9558 4.500,0.4266,0.00980,0.00371,0.0138,0.0183,0.9576 4.750,0.4620,0.01012,0.00407,0.0119,0.0161,0.9593 5.000,0.4956,0.01051,0.00449,0.0105,0.0144,0.9614 5.250,0.5242,0.01107,0.00512,0.0101,0.0130,0.9644 5.500,0.5442,0.01169,0.00584,0.0117,0.0120,0.9701 5.750,0.5776,0.01215,0.00634,0.0102,0.0113,0.9712 6.000,0.6106,0.01259,0.00680,0.0088,0.0102,0.9725 6.250,0.6417,0.01322,0.00748,0.0077,0.0099,0.9744 6.500,0.6718,0.01380,0.00808,0.0068,0.0092,0.9770 6.750,0.6943,0.01446,0.00879,0.0076,0.0088,0.9818 7.000,0.7206,0.01545,0.00983,0.0073,0.0086,0.9840 7.250,0.7408,0.01796,0.01239,0.0078,0.0080,0.9858 7.500,0.7709,0.01902,0.01351,0.0068,0.0079,0.9874 7.750,0.8029,0.01933,0.01393,0.0057,0.0073,0.9895 8.000,0.8303,0.02105,0.01573,0.0053,0.0074,0.9913 8.250,0.8572,0.02325,0.01807,0.0050,0.0075,0.9930 8.500,0.8863,0.02429,0.01923,0.0043,0.0072,0.9948 8.750,0.9133,0.02697,0.02212,0.0037,0.0074,0.9961 9.250,0.9500,0.03703,0.03263,0.0042,0.0080,0.9987 9.500,0.9605,0.03968,0.03551,0.0058,0.0080,1.0000 9.750,0.9550,0.04137,0.03737,0.0108,0.0080,1.0000 10.000,0.9492,0.04326,0.03941,0.0156,0.0080,1.0000 10.250,0.9353,0.04508,0.04141,0.0217,0.0080,1.0000 10.500,0.9258,0.04685,0.04331,0.0267,0.0080,1.0000 10.750,0.8947,0.04789,0.04453,0.0356,0.0079,1.0000 11.000,0.8894,0.04966,0.04635,0.0395,0.0080,1.0000 11.250,0.8670,0.05133,0.04815,0.0453,0.0080,1.0000 11.500,0.8427,0.05331,0.05030,0.0499,0.0079,1.0000 11.750,0.8251,0.05581,0.05292,0.0525,0.0079,1.0000 12.000,0.8048,0.05888,0.05613,0.0542,0.0079,1.0000 12.250,0.7913,0.06211,0.05945,0.0547,0.0079,1.0000 12.500,0.7755,0.06587,0.06332,0.0544,0.0079,1.0000 12.750,0.7567,0.07020,0.06777,0.0530,0.0079,1.0000 13.000,0.7317,0.07585,0.07357,0.0499,0.0079,1.0000 13.250,0.7157,0.08129,0.07910,0.0470,0.0079,1.0000