Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe14k-il-200000 Airfoil,goe14k-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,60.7797 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-goe14k-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.6035,0.09265,0.08949,-0.0346,0.9962,0.0622 -8.500,-0.6221,0.08652,0.08332,-0.0393,0.9918,0.0630 -8.250,-0.6497,0.08286,0.07963,-0.0372,0.9893,0.0630 -8.000,-0.6743,0.07898,0.07568,-0.0346,0.9875,0.0638 -7.750,-0.6908,0.07365,0.07015,-0.0336,0.9827,0.0650 -7.500,-0.7175,0.06976,0.06601,-0.0281,0.9825,0.0665 -6.750,-0.8300,0.04869,0.04366,0.0014,0.9943,0.0419 -6.500,-0.8355,0.04509,0.03966,0.0070,0.9939,0.0415 -6.250,-0.8348,0.04187,0.03599,0.0119,0.9920,0.0418 -6.000,-0.8263,0.03960,0.03322,0.0156,0.9893,0.0432 -5.750,-0.8135,0.03860,0.03162,0.0191,0.9869,0.0448 -5.500,-0.8010,0.03510,0.02769,0.0217,0.9853,0.0458 -5.250,-0.7899,0.03357,0.02602,0.0247,0.9849,0.0470 -5.000,-0.7761,0.03284,0.02530,0.0269,0.9835,0.0496 -4.750,-0.7562,0.03173,0.02392,0.0285,0.9797,0.0519 -4.500,-0.7287,0.03121,0.02301,0.0289,0.9764,0.0547 -4.250,-0.7000,0.02984,0.02141,0.0285,0.9746,0.0579 -4.000,-0.6851,0.02905,0.02060,0.0307,0.9740,0.0617 -3.750,-0.6120,0.02843,0.01964,0.0221,0.9487,0.0680 -3.500,-0.5858,0.02708,0.01834,0.0220,0.9452,0.0744 -3.250,-0.5532,0.02675,0.01792,0.0209,0.9417,0.0798 -3.000,-0.5160,0.02610,0.01726,0.0188,0.9370,0.0859 -2.750,-0.4985,0.02567,0.01684,0.0206,0.9332,0.0913 -2.500,-0.4715,0.02538,0.01652,0.0206,0.9301,0.0975 -2.250,-0.4365,0.02523,0.01641,0.0188,0.9273,0.1053 -2.000,-0.4151,0.02491,0.01612,0.0199,0.9222,0.1142 -1.750,-0.3934,0.02469,0.01594,0.0209,0.9186,0.1266 -1.500,-0.1160,0.02427,0.01910,-0.0350,0.9318,0.9502 -1.250,0.0039,0.02629,0.02088,-0.0546,0.9359,0.9968 -1.000,0.0402,0.02649,0.02098,-0.0570,0.9335,1.0000 -0.750,0.0647,0.02658,0.02098,-0.0569,0.9300,1.0000 -0.500,0.0940,0.02675,0.02106,-0.0577,0.9277,1.0000 -0.250,0.1288,0.02699,0.02122,-0.0595,0.9259,1.0000 0.000,0.1325,0.02699,0.02117,-0.0552,0.9189,1.0000 0.250,0.1595,0.02714,0.02128,-0.0555,0.9158,1.0000 0.500,0.1935,0.02731,0.02140,-0.0572,0.9134,1.0000 0.750,0.2078,0.02738,0.02145,-0.0549,0.9064,1.0000 1.000,0.2397,0.02738,0.02142,-0.0560,0.9018,1.0000 1.250,0.2837,0.02734,0.02135,-0.0594,0.8989,1.0000 1.500,0.2938,0.02743,0.02144,-0.0562,0.8905,1.0000 1.750,0.3295,0.02737,0.02139,-0.0580,0.8867,1.0000 2.000,0.3697,0.02733,0.02136,-0.0606,0.8844,1.0000 2.250,0.3803,0.02742,0.02146,-0.0575,0.8749,1.0000 2.500,0.4186,0.02726,0.02133,-0.0596,0.8715,1.0000 2.750,0.4630,0.02690,0.02102,-0.0627,0.8682,1.0000 3.000,0.4777,0.02688,0.02104,-0.0602,0.8585,1.0000 3.250,0.5466,0.02545,0.01969,-0.0673,0.8549,1.0000 3.500,0.5931,0.02388,0.01819,-0.0696,0.8426,1.0000 3.750,0.6965,0.02034,0.01480,-0.0821,0.8394,1.0000 4.000,0.7134,0.01990,0.01443,-0.0793,0.8277,1.0000 4.250,0.7532,0.01865,0.01331,-0.0805,0.8187,1.0000 5.000,0.8473,0.01567,0.01059,-0.0793,0.7630,1.0000 5.250,0.8965,0.01475,0.00848,-0.0816,0.5194,1.0000 5.500,0.8721,0.01605,0.00914,-0.0708,0.4192,1.0000 5.750,0.8573,0.01728,0.00988,-0.0625,0.3302,1.0000 6.000,0.8451,0.01871,0.01066,-0.0551,0.2220,1.0000 6.250,0.8429,0.01999,0.01147,-0.0498,0.1558,1.0000 6.500,0.8491,0.02092,0.01218,-0.0460,0.1266,1.0000 6.750,0.8589,0.02168,0.01286,-0.0428,0.1110,1.0000 7.000,0.8695,0.02245,0.01357,-0.0399,0.0989,1.0000 7.250,0.8828,0.02310,0.01425,-0.0373,0.0895,1.0000 7.500,0.8940,0.02403,0.01514,-0.0345,0.0808,1.0000 7.750,0.9072,0.02485,0.01594,-0.0321,0.0734,1.0000 8.000,0.9225,0.02578,0.01691,-0.0301,0.0662,1.0000 8.250,0.9392,0.02675,0.01782,-0.0284,0.0605,1.0000 8.500,0.9624,0.02783,0.01897,-0.0277,0.0559,1.0000 8.750,0.9795,0.02854,0.01973,-0.0260,0.0517,1.0000 9.000,1.0186,0.03037,0.02153,-0.0284,0.0475,1.0000 9.250,1.0394,0.03129,0.02264,-0.0272,0.0451,1.0000 9.500,1.0569,0.03218,0.02363,-0.0256,0.0421,1.0000 9.750,1.0781,0.03329,0.02475,-0.0249,0.0400,1.0000 10.000,1.1215,0.03631,0.02802,-0.0282,0.0379,1.0000 10.250,1.1397,0.03823,0.03028,-0.0266,0.0370,1.0000 10.500,1.1465,0.03952,0.03181,-0.0230,0.0352,1.0000 10.750,1.1575,0.04152,0.03408,-0.0205,0.0343,1.0000 11.000,1.1654,0.04305,0.03575,-0.0176,0.0333,1.0000 11.250,1.1717,0.04478,0.03762,-0.0146,0.0325,1.0000 11.500,1.1748,0.04705,0.04011,-0.0112,0.0320,1.0000 11.750,1.1743,0.04957,0.04285,-0.0075,0.0317,1.0000