Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe359-il-100000-n5 Airfoil,goe359-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,62.9958 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-goe359-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.500,-0.2493,0.09787,0.09350,-0.0282,1.0000,0.0310 -7.250,-0.2535,0.09612,0.09187,-0.0268,1.0000,0.0315 -7.000,-0.2629,0.09489,0.09076,-0.0245,1.0000,0.0318 -6.750,-0.2492,0.09162,0.08753,-0.0283,0.9931,0.0332 -6.500,-0.2181,0.08771,0.08361,-0.0388,0.9786,0.0372 -6.250,-0.1798,0.08408,0.07991,-0.0532,0.9600,0.0382 -6.000,-0.1455,0.07956,0.07531,-0.0624,0.9465,0.0384 -5.750,-0.1109,0.07468,0.07032,-0.0704,0.9353,0.0385 -5.500,-0.0874,0.06878,0.06442,-0.0742,0.9261,0.0391 -5.250,-0.0713,0.06462,0.06026,-0.0738,0.9155,0.0406 -5.000,-0.0438,0.06111,0.05668,-0.0773,0.9050,0.0447 -4.500,0.0358,0.05215,0.04736,-0.0934,0.8826,0.0529 -4.250,0.0633,0.04900,0.04408,-0.0960,0.8703,0.0562 -4.000,0.0989,0.04552,0.04039,-0.1012,0.8582,0.0661 -3.750,0.1291,0.04293,0.03763,-0.1041,0.8463,0.0792 -3.500,0.1728,0.03789,0.03211,-0.1093,0.8359,0.0604 -3.250,0.2052,0.03459,0.02851,-0.1117,0.8241,0.0586 -3.000,0.2384,0.03139,0.02489,-0.1137,0.8123,0.0567 -2.750,0.2773,0.02737,0.01996,-0.1158,0.8017,0.0515 -2.500,0.3034,0.02608,0.01863,-0.1163,0.7900,0.0553 -2.250,0.3334,0.02440,0.01655,-0.1167,0.7788,0.0569 -2.000,0.3632,0.02266,0.01433,-0.1169,0.7669,0.0555 -1.750,0.3925,0.02129,0.01253,-0.1169,0.7555,0.0549 -1.500,0.4212,0.02022,0.01109,-0.1168,0.7443,0.0550 -1.250,0.4496,0.01936,0.00994,-0.1166,0.7334,0.0556 -1.000,0.4770,0.01867,0.00903,-0.1163,0.7216,0.0565 -0.750,0.5043,0.01822,0.00840,-0.1160,0.7103,0.0604 -0.500,0.5316,0.01779,0.00778,-0.1156,0.6996,0.0624 -0.250,0.5587,0.01735,0.00720,-0.1152,0.6893,0.0626 0.000,0.5853,0.01700,0.00678,-0.1148,0.6779,0.0628 0.250,0.6118,0.01672,0.00644,-0.1143,0.6676,0.0633 0.500,0.6384,0.01651,0.00611,-0.1139,0.6583,0.0643 0.750,0.6652,0.01641,0.00591,-0.1135,0.6477,0.0658 1.000,0.6922,0.01636,0.00578,-0.1132,0.6372,0.0682 1.250,0.7192,0.01635,0.00567,-0.1128,0.6269,0.0721 1.500,0.7460,0.01634,0.00564,-0.1125,0.6164,0.0833 1.750,0.7723,0.01595,0.00579,-0.1124,0.6048,0.3015 2.250,0.8232,0.01500,0.00581,-0.1110,0.5823,1.0000 2.750,0.8744,0.01542,0.00599,-0.1100,0.5592,1.0000 3.000,0.9001,0.01565,0.00614,-0.1095,0.5491,1.0000 3.500,0.9517,0.01614,0.00653,-0.1087,0.5316,1.0000 3.750,0.9773,0.01639,0.00676,-0.1083,0.5229,1.0000 4.000,1.0027,0.01665,0.00700,-0.1078,0.5138,1.0000 4.250,1.0279,0.01692,0.00728,-0.1074,0.5044,1.0000 4.500,1.0533,0.01719,0.00755,-0.1069,0.4962,1.0000 4.750,1.0781,0.01748,0.00789,-0.1064,0.4862,1.0000 5.000,1.1025,0.01776,0.00821,-0.1058,0.4754,1.0000 5.250,1.1266,0.01805,0.00853,-0.1051,0.4635,1.0000 5.500,1.1502,0.01834,0.00884,-0.1044,0.4508,1.0000 5.750,1.1734,0.01865,0.00917,-0.1036,0.4373,1.0000 6.000,1.1944,0.01896,0.00950,-0.1024,0.4139,1.0000 6.250,1.2135,0.01933,0.00981,-0.1009,0.3824,1.0000 6.500,1.2329,0.01978,0.01019,-0.0996,0.3507,1.0000 6.750,1.2512,0.02036,0.01064,-0.0982,0.3120,1.0000 7.000,1.2665,0.02122,0.01122,-0.0965,0.2705,1.0000 7.250,1.2816,0.02219,0.01198,-0.0948,0.2392,1.0000 7.500,1.2953,0.02331,0.01289,-0.0931,0.2062,1.0000 7.750,1.3083,0.02448,0.01389,-0.0913,0.1598,1.0000 8.000,1.3130,0.02632,0.01523,-0.0886,0.0989,1.0000 8.250,1.3147,0.02836,0.01691,-0.0854,0.0513,1.0000 8.500,1.3230,0.02974,0.01828,-0.0830,0.0245,1.0000 8.750,1.3281,0.03121,0.01973,-0.0801,0.0214,1.0000 9.000,1.3370,0.03244,0.02110,-0.0779,0.0200,1.0000 9.250,1.3451,0.03376,0.02258,-0.0757,0.0192,1.0000 9.500,1.3513,0.03529,0.02433,-0.0735,0.0185,1.0000 9.750,1.3553,0.03707,0.02638,-0.0714,0.0176,1.0000 10.000,1.3572,0.03914,0.02868,-0.0695,0.0168,1.0000 10.250,1.3575,0.04148,0.03124,-0.0679,0.0162,1.0000 10.500,1.3568,0.04404,0.03402,-0.0665,0.0158,1.0000 10.750,1.3544,0.04691,0.03711,-0.0654,0.0156,1.0000 11.000,1.3503,0.05012,0.04054,-0.0647,0.0154,1.0000 11.250,1.3447,0.05367,0.04430,-0.0643,0.0152,1.0000 11.500,1.3375,0.05756,0.04839,-0.0641,0.0150,1.0000 11.750,1.3294,0.06173,0.05277,-0.0643,0.0149,1.0000 12.000,1.3204,0.06618,0.05740,-0.0648,0.0148,1.0000 12.250,1.3108,0.07082,0.06223,-0.0654,0.0147,1.0000 12.500,1.3010,0.07558,0.06716,-0.0662,0.0147,1.0000 12.750,1.2915,0.08042,0.07217,-0.0671,0.0146,1.0000 13.000,1.2827,0.08525,0.07714,-0.0680,0.0145,1.0000 13.250,1.2751,0.08987,0.08190,-0.0689,0.0144,1.0000 13.500,1.2693,0.09414,0.08628,-0.0695,0.0142,1.0000