Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe310-il-100000 Airfoil,goe310-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,59.5917 Max Cl/Cd alpha,7 Url,http://airfoiltools.com/polar/csv?polar=xf-goe310-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.2520,0.10333,0.09869,-0.0339,1.0000,0.0898 -9.250,-0.2647,0.10234,0.09779,-0.0350,1.0000,0.0921 -9.000,-0.2828,0.10191,0.09746,-0.0360,1.0000,0.0927 -8.750,-0.2632,0.09534,0.09090,-0.0336,1.0000,0.0951 -8.500,-0.2566,0.09222,0.08780,-0.0319,1.0000,0.0984 -8.250,-0.2597,0.08995,0.08560,-0.0309,1.0000,0.1017 -8.000,-0.3347,0.09627,0.09160,-0.0309,1.0000,0.0965 -7.750,-0.3350,0.09403,0.08943,-0.0292,1.0000,0.0997 -7.500,-0.3448,0.09254,0.08804,-0.0275,1.0000,0.1021 -7.250,-0.3624,0.09167,0.08728,-0.0251,1.0000,0.1039 -7.000,-0.3853,0.09165,0.08736,-0.0256,1.0000,0.1059 -6.750,-0.4040,0.09214,0.08786,-0.0293,1.0000,0.1067 -6.500,-0.3916,0.08572,0.08156,-0.0216,1.0000,0.1091 -6.250,-0.3905,0.08345,0.07933,-0.0186,1.0000,0.1129 -6.000,-0.3966,0.08187,0.07779,-0.0184,1.0000,0.1180 -5.750,-0.4047,0.08110,0.07696,-0.0236,1.0000,0.1211 -5.500,-0.4045,0.07714,0.07311,-0.0179,1.0000,0.1231 -5.250,-0.4048,0.07492,0.07094,-0.0153,1.0000,0.1256 -4.750,-0.3502,0.06719,0.06301,-0.0266,0.9877,0.1381 -4.500,-0.3044,0.06344,0.05896,-0.0367,0.9773,0.1498 -4.250,-0.2762,0.05926,0.05484,-0.0378,0.9710,0.1554 -4.000,-0.2375,0.05561,0.05094,-0.0445,0.9600,0.1655 -3.750,-0.2051,0.05210,0.04735,-0.0472,0.9514,0.1706 -3.500,-0.1569,0.03735,0.03113,-0.0568,0.9439,0.0942 -3.250,-0.1254,0.03353,0.02684,-0.0581,0.9346,0.0911 -3.000,-0.0879,0.02953,0.02222,-0.0603,0.9283,0.0873 -2.750,-0.0560,0.02642,0.01836,-0.0607,0.9189,0.0848 -2.500,-0.0121,0.02441,0.01586,-0.0633,0.9132,0.0853 -2.250,0.0221,0.02342,0.01463,-0.0643,0.9029,0.0900 -2.000,0.0695,0.02213,0.01308,-0.0675,0.8979,0.0934 -1.750,0.1020,0.02134,0.01234,-0.0682,0.8875,0.0983 -1.500,0.1505,0.02041,0.01143,-0.0717,0.8829,0.1103 -1.250,0.1826,0.02001,0.01124,-0.0722,0.8723,0.1448 -1.000,0.2275,0.02002,0.01120,-0.0749,0.8669,0.2209 -0.750,0.2535,0.02008,0.01125,-0.0744,0.8552,0.2495 -0.500,0.2867,0.01990,0.01104,-0.0752,0.8464,0.2688 -0.250,0.3233,0.01962,0.01078,-0.0766,0.8388,0.2892 0.000,0.3521,0.01956,0.01072,-0.0767,0.8288,0.3072 0.250,0.3926,0.01918,0.01035,-0.0787,0.8227,0.3302 0.500,0.4196,0.01916,0.01038,-0.0785,0.8121,0.3539 0.750,0.4606,0.01868,0.00995,-0.0806,0.8068,0.3877 1.000,0.4841,0.01855,0.00995,-0.0798,0.7957,0.4191 1.250,0.5095,0.01808,0.00974,-0.0793,0.7873,0.4726 1.500,0.6469,0.01654,0.00909,-0.1013,0.7824,1.0000 1.750,0.6728,0.01666,0.00911,-0.1007,0.7733,1.0000 2.000,0.6993,0.01675,0.00910,-0.1000,0.7642,1.0000 2.250,0.7212,0.01695,0.00927,-0.0986,0.7528,1.0000 2.500,0.7457,0.01699,0.00924,-0.0974,0.7409,1.0000 2.750,0.7705,0.01691,0.00907,-0.0961,0.7267,1.0000 3.000,0.7946,0.01681,0.00889,-0.0945,0.7108,1.0000 3.250,0.8182,0.01678,0.00880,-0.0929,0.6950,1.0000 3.500,0.8413,0.01679,0.00876,-0.0913,0.6794,1.0000 3.750,0.8640,0.01685,0.00877,-0.0897,0.6640,1.0000 4.000,0.8865,0.01698,0.00887,-0.0882,0.6499,1.0000 4.250,0.9090,0.01714,0.00905,-0.0868,0.6368,1.0000 4.500,0.9310,0.01726,0.00917,-0.0853,0.6222,1.0000 4.750,0.9525,0.01738,0.00930,-0.0836,0.6070,1.0000 5.000,0.9742,0.01754,0.00948,-0.0821,0.5930,1.0000 5.250,0.9956,0.01770,0.00971,-0.0805,0.5787,1.0000 5.500,1.0163,0.01786,0.00992,-0.0788,0.5637,1.0000 5.750,1.0360,0.01801,0.01014,-0.0769,0.5474,1.0000 6.000,1.0548,0.01814,0.01035,-0.0749,0.5293,1.0000 6.250,1.0735,0.01827,0.01056,-0.0728,0.5104,1.0000 6.500,1.0921,0.01843,0.01078,-0.0707,0.4916,1.0000 6.750,1.1077,0.01863,0.01109,-0.0681,0.4677,1.0000 7.000,1.1239,0.01886,0.01139,-0.0657,0.4439,1.0000 7.250,1.1386,0.01914,0.01172,-0.0629,0.4163,1.0000 7.500,1.1500,0.01953,0.01210,-0.0597,0.3784,1.0000 7.750,1.1550,0.02025,0.01252,-0.0555,0.3236,1.0000 8.000,1.1556,0.02138,0.01327,-0.0508,0.2640,1.0000 8.250,1.1529,0.02284,0.01431,-0.0460,0.2026,1.0000 8.500,1.1475,0.02454,0.01557,-0.0409,0.1411,1.0000 8.750,1.1420,0.02616,0.01685,-0.0358,0.1065,1.0000 9.000,1.1384,0.02777,0.01829,-0.0312,0.0917,1.0000 9.250,1.1361,0.02943,0.01989,-0.0271,0.0820,1.0000 9.500,1.1330,0.03126,0.02176,-0.0233,0.0757,1.0000 9.750,1.1311,0.03324,0.02371,-0.0199,0.0711,1.0000 10.000,1.1371,0.03535,0.02574,-0.0171,0.0675,1.0000 10.250,1.1557,0.03726,0.02765,-0.0156,0.0626,1.0000 10.500,1.2209,0.04136,0.03163,-0.0199,0.0563,1.0000 10.750,1.2511,0.04415,0.03476,-0.0202,0.0546,1.0000 11.000,1.2702,0.04686,0.03778,-0.0192,0.0527,1.0000 11.250,1.2902,0.05004,0.04114,-0.0188,0.0501,1.0000 11.500,1.3003,0.05314,0.04456,-0.0168,0.0498,1.0000 11.750,1.2973,0.05580,0.04759,-0.0131,0.0500,1.0000 12.000,1.2867,0.05842,0.05060,-0.0088,0.0507,1.0000 12.250,1.2731,0.06127,0.05382,-0.0049,0.0516,1.0000 12.500,1.2584,0.06457,0.05745,-0.0018,0.0525,1.0000 12.750,1.2438,0.06820,0.06138,0.0006,0.0535,1.0000 13.000,1.2273,0.07232,0.06577,0.0024,0.0545,1.0000 13.250,1.2124,0.07685,0.07051,0.0034,0.0556,1.0000 13.500,1.0760,0.07598,0.07013,0.0093,0.0547,1.0000 13.750,1.0508,0.08151,0.07587,0.0088,0.0553,1.0000 14.000,1.0238,0.08727,0.08182,0.0076,0.0558,1.0000 14.250,0.9970,0.09328,0.08799,0.0058,0.0565,1.0000 14.500,0.9945,0.09846,0.09328,0.0053,0.0583,1.0000 14.750,0.9524,0.10397,0.09900,0.0019,0.0586,1.0000 15.000,0.8989,0.11152,0.10677,-0.0043,0.0592,1.0000