Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe693-il-100000-n5 Airfoil,goe693-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,55.6648 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-goe693-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.4077,0.09369,0.08841,-0.0468,1.0000,0.0517 -9.500,-0.4115,0.09038,0.08516,-0.0475,1.0000,0.0526 -9.250,-0.4207,0.08672,0.08157,-0.0480,1.0000,0.0532 -9.000,-0.4364,0.08286,0.07780,-0.0482,1.0000,0.0535 -8.750,-0.4615,0.07911,0.07418,-0.0475,1.0000,0.0534 -8.500,-0.4944,0.07482,0.07000,-0.0470,1.0000,0.0530 -8.250,-0.5160,0.06674,0.06189,-0.0524,0.9964,0.0530 -8.000,-0.5231,0.05190,0.04650,-0.0650,0.9852,0.0535 -7.750,-0.5154,0.04340,0.03731,-0.0702,0.9761,0.0549 -7.500,-0.4988,0.03731,0.03036,-0.0732,0.9688,0.0574 -7.250,-0.4749,0.03329,0.02561,-0.0751,0.9623,0.0589 -7.000,-0.4439,0.03163,0.02380,-0.0769,0.9575,0.0602 -6.750,-0.4154,0.03022,0.02219,-0.0779,0.9505,0.0617 -6.500,-0.3815,0.02882,0.02053,-0.0799,0.9463,0.0642 -6.250,-0.3534,0.02736,0.01872,-0.0806,0.9391,0.0672 -6.000,-0.3222,0.02583,0.01684,-0.0817,0.9332,0.0698 -5.750,-0.2876,0.02490,0.01586,-0.0834,0.9293,0.0721 -5.500,-0.2618,0.02415,0.01500,-0.0832,0.9202,0.0749 -5.250,-0.2285,0.02320,0.01382,-0.0844,0.9153,0.0794 -5.000,-0.2008,0.02257,0.01313,-0.0846,0.9073,0.0837 -4.750,-0.1694,0.02199,0.01247,-0.0854,0.9012,0.0895 -4.500,-0.1394,0.02128,0.01162,-0.0858,0.8949,0.0956 -4.250,-0.1108,0.02081,0.01114,-0.0861,0.8876,0.1025 -4.000,-0.0780,0.02023,0.01047,-0.0870,0.8830,0.1117 -3.750,-0.0523,0.01989,0.01010,-0.0867,0.8741,0.1206 -3.500,-0.0211,0.01941,0.00960,-0.0873,0.8690,0.1305 -3.250,0.0060,0.01914,0.00923,-0.0872,0.8612,0.1409 -3.000,0.0355,0.01874,0.00888,-0.0875,0.8553,0.1512 -2.750,0.0637,0.01842,0.00855,-0.0876,0.8488,0.1619 -2.500,0.0917,0.01814,0.00826,-0.0876,0.8419,0.1735 -2.250,0.1224,0.01779,0.00790,-0.0880,0.8373,0.1866 -2.000,0.1476,0.01758,0.00775,-0.0876,0.8291,0.1995 -1.750,0.1769,0.01727,0.00749,-0.0878,0.8237,0.2176 -1.500,0.2038,0.01702,0.00733,-0.0876,0.8170,0.2407 -1.250,0.2313,0.01673,0.00718,-0.0876,0.8106,0.2772 -1.000,0.2606,0.01627,0.00697,-0.0878,0.8057,0.3491 -0.750,0.2836,0.01575,0.00701,-0.0870,0.7973,0.4898 -0.500,0.3064,0.01492,0.00698,-0.0850,0.7911,0.7248 -0.250,0.3614,0.01460,0.00698,-0.0893,0.7822,0.9485 0.000,0.4105,0.01448,0.00667,-0.0933,0.7733,1.0000 0.250,0.4340,0.01453,0.00659,-0.0923,0.7622,1.0000 0.500,0.4588,0.01459,0.00653,-0.0916,0.7531,1.0000 0.750,0.4843,0.01467,0.00649,-0.0910,0.7453,1.0000 1.000,0.5095,0.01478,0.00652,-0.0904,0.7380,1.0000 1.250,0.5347,0.01490,0.00655,-0.0898,0.7302,1.0000 1.500,0.5606,0.01501,0.00659,-0.0893,0.7228,1.0000 1.750,0.5856,0.01513,0.00665,-0.0887,0.7140,1.0000 2.000,0.6108,0.01524,0.00670,-0.0881,0.7049,1.0000 2.250,0.6368,0.01532,0.00671,-0.0875,0.6955,1.0000 2.500,0.6609,0.01546,0.00683,-0.0867,0.6844,1.0000 2.750,0.6864,0.01555,0.00687,-0.0860,0.6741,1.0000 3.000,0.7118,0.01566,0.00694,-0.0854,0.6636,1.0000 3.250,0.7361,0.01582,0.00711,-0.0846,0.6527,1.0000 3.500,0.7615,0.01595,0.00723,-0.0840,0.6426,1.0000 3.750,0.7867,0.01608,0.00734,-0.0834,0.6314,1.0000 4.000,0.8107,0.01624,0.00752,-0.0825,0.6182,1.0000 4.250,0.8348,0.01639,0.00769,-0.0817,0.6046,1.0000 4.500,0.8591,0.01656,0.00786,-0.0810,0.5909,1.0000 4.750,0.8831,0.01673,0.00805,-0.0801,0.5765,1.0000 5.000,0.9066,0.01691,0.00824,-0.0792,0.5597,1.0000 5.250,0.9295,0.01711,0.00842,-0.0782,0.5409,1.0000 5.500,0.9525,0.01733,0.00861,-0.0771,0.5223,1.0000 5.750,0.9748,0.01759,0.00885,-0.0760,0.5019,1.0000 6.000,0.9964,0.01790,0.00912,-0.0748,0.4797,1.0000 6.500,1.0383,0.01866,0.00975,-0.0723,0.4383,1.0000 6.750,1.0583,0.01911,0.01016,-0.0709,0.4184,1.0000 7.000,1.0778,0.01962,0.01060,-0.0695,0.3995,1.0000 7.250,1.0967,0.02016,0.01108,-0.0681,0.3818,1.0000 7.500,1.1153,0.02072,0.01162,-0.0666,0.3646,1.0000 7.750,1.1334,0.02130,0.01221,-0.0651,0.3481,1.0000 8.000,1.1508,0.02191,0.01282,-0.0635,0.3320,1.0000 8.250,1.1677,0.02254,0.01346,-0.0618,0.3163,1.0000 8.500,1.1837,0.02320,0.01414,-0.0601,0.3004,1.0000 8.750,1.1991,0.02386,0.01486,-0.0582,0.2847,1.0000 9.000,1.2133,0.02455,0.01563,-0.0562,0.2690,1.0000 9.250,1.2254,0.02527,0.01639,-0.0539,0.2534,1.0000 9.500,1.2367,0.02607,0.01722,-0.0516,0.2384,1.0000 9.750,1.2465,0.02698,0.01812,-0.0492,0.2229,1.0000 10.000,1.2542,0.02803,0.01913,-0.0467,0.2068,1.0000 10.250,1.2599,0.02927,0.02031,-0.0442,0.1914,1.0000 10.500,1.2646,0.03066,0.02162,-0.0418,0.1767,1.0000 10.750,1.2699,0.03210,0.02305,-0.0397,0.1633,1.0000 11.000,1.2757,0.03358,0.02453,-0.0377,0.1518,1.0000 11.250,1.2821,0.03506,0.02608,-0.0360,0.1408,1.0000 11.500,1.2917,0.03637,0.02755,-0.0346,0.1281,1.0000 11.750,1.2993,0.03787,0.02914,-0.0333,0.1136,1.0000 12.000,1.3035,0.03970,0.03100,-0.0319,0.0983,1.0000 12.250,1.3030,0.04202,0.03326,-0.0305,0.0866,1.0000 12.500,1.2999,0.04468,0.03589,-0.0291,0.0770,1.0000 12.750,1.2979,0.04737,0.03865,-0.0279,0.0666,1.0000 13.000,1.2966,0.05009,0.04145,-0.0269,0.0566,1.0000 13.250,1.2937,0.05305,0.04447,-0.0261,0.0496,1.0000 13.500,1.2887,0.05634,0.04780,-0.0255,0.0454,1.0000 13.750,1.2837,0.05973,0.05128,-0.0251,0.0424,1.0000 14.000,1.2767,0.06349,0.05512,-0.0249,0.0402,1.0000 14.250,1.2692,0.06746,0.05918,-0.0250,0.0385,1.0000 14.500,1.2632,0.07137,0.06326,-0.0253,0.0368,1.0000 14.750,1.2563,0.07555,0.06757,-0.0258,0.0353,1.0000 15.000,1.2482,0.08003,0.07217,-0.0266,0.0341,1.0000 15.250,1.2390,0.08480,0.07704,-0.0277,0.0332,1.0000 15.500,1.2305,0.08954,0.08187,-0.0288,0.0323,1.0000 15.750,1.2252,0.09394,0.08644,-0.0299,0.0313,1.0000