Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe269-il-100000-n5 Airfoil,goe269-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,61.4997 Max Cl/Cd alpha,5.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe269-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.3479,0.10774,0.10276,-0.0155,1.0000,0.0486 -8.250,-0.3483,0.10631,0.10140,-0.0188,1.0000,0.0491 -8.000,-0.3463,0.10442,0.09958,-0.0229,1.0000,0.0493 -7.750,-0.3379,0.10161,0.09680,-0.0278,1.0000,0.0494 -7.500,-0.3283,0.09578,0.09099,-0.0224,1.0000,0.0501 -7.250,-0.3192,0.09230,0.08754,-0.0218,1.0000,0.0511 -7.000,-0.3108,0.08938,0.08466,-0.0226,1.0000,0.0523 -6.750,-0.3027,0.08673,0.08206,-0.0239,1.0000,0.0545 -6.500,-0.2941,0.08442,0.07980,-0.0273,1.0000,0.0577 -6.250,-0.2813,0.08250,0.07790,-0.0348,1.0000,0.0589 -6.000,-0.2690,0.07996,0.07533,-0.0393,1.0000,0.0591 -5.750,-0.2470,0.07647,0.07179,-0.0449,0.9973,0.0593 -5.500,-0.2346,0.07144,0.06683,-0.0429,0.9915,0.0602 -5.250,-0.2120,0.06787,0.06325,-0.0441,0.9850,0.0628 -5.000,-0.1734,0.06407,0.05934,-0.0518,0.9762,0.0675 -4.750,-0.1085,0.05984,0.05470,-0.0679,0.9672,0.0699 -4.500,-0.0685,0.05536,0.05003,-0.0745,0.9598,0.0703 -4.250,-0.0524,0.05170,0.04652,-0.0737,0.9511,0.0723 -4.000,-0.0199,0.04886,0.04360,-0.0771,0.9418,0.0761 -3.750,0.0230,0.04552,0.04005,-0.0832,0.9338,0.0785 -3.250,0.1174,0.03634,0.02990,-0.0952,0.9126,0.0590 -3.000,0.1431,0.03489,0.02853,-0.0960,0.8981,0.0627 -2.500,0.2187,0.02896,0.02158,-0.1007,0.8704,0.0590 -2.250,0.2497,0.02698,0.01928,-0.1015,0.8574,0.0590 -2.000,0.2804,0.02517,0.01711,-0.1021,0.8439,0.0592 -1.750,0.3091,0.02374,0.01548,-0.1024,0.8304,0.0600 -1.500,0.3363,0.02306,0.01476,-0.1025,0.8168,0.0623 -1.250,0.3652,0.02218,0.01366,-0.1026,0.8037,0.0654 -1.000,0.3950,0.02104,0.01219,-0.1026,0.7912,0.0669 -0.750,0.4244,0.02002,0.01083,-0.1024,0.7791,0.0683 -0.500,0.4534,0.01917,0.00964,-0.1021,0.7672,0.0702 -0.250,0.4810,0.01849,0.00890,-0.1019,0.7543,0.0727 0.000,0.5085,0.01811,0.00844,-0.1016,0.7418,0.0779 0.250,0.5363,0.01764,0.00780,-0.1012,0.7297,0.0836 0.500,0.5635,0.01720,0.00732,-0.1008,0.7178,0.0878 0.750,0.5907,0.01696,0.00696,-0.1003,0.7056,0.0950 1.000,0.6176,0.01663,0.00668,-0.1000,0.6928,0.1018 1.250,0.6444,0.01641,0.00642,-0.0995,0.6800,0.1075 1.500,0.6712,0.01626,0.00625,-0.0990,0.6673,0.1157 1.750,0.6984,0.01618,0.00611,-0.0986,0.6546,0.1225 2.000,0.7255,0.01614,0.00599,-0.0981,0.6416,0.1283 2.250,0.7526,0.01614,0.00599,-0.0978,0.6278,0.1393 2.500,0.7798,0.01615,0.00602,-0.0974,0.6134,0.1523 2.750,0.8069,0.01616,0.00606,-0.0971,0.5990,0.1728 3.000,0.8292,0.01471,0.00612,-0.0959,0.5849,1.0000 3.250,0.8560,0.01494,0.00621,-0.0954,0.5699,1.0000 3.500,0.8827,0.01517,0.00635,-0.0950,0.5547,1.0000 3.750,0.9091,0.01541,0.00651,-0.0946,0.5393,1.0000 4.000,0.9352,0.01564,0.00667,-0.0940,0.5213,1.0000 4.250,0.9606,0.01589,0.00681,-0.0934,0.4996,1.0000 4.500,0.9857,0.01618,0.00696,-0.0928,0.4767,1.0000 4.750,1.0107,0.01652,0.00720,-0.0921,0.4576,1.0000 5.250,1.0616,0.01727,0.00787,-0.0912,0.4290,1.0000 5.500,1.0867,0.01767,0.00826,-0.0907,0.4149,1.0000 5.750,1.1117,0.01808,0.00870,-0.0901,0.4005,1.0000 6.000,1.1364,0.01851,0.00916,-0.0896,0.3863,1.0000 6.250,1.1611,0.01894,0.00964,-0.0891,0.3724,1.0000 6.500,1.1853,0.01939,0.01016,-0.0885,0.3572,1.0000 6.750,1.2090,0.01985,0.01067,-0.0878,0.3402,1.0000 7.000,1.2322,0.02035,0.01121,-0.0871,0.3216,1.0000 7.250,1.2549,0.02087,0.01178,-0.0863,0.3009,1.0000 7.500,1.2766,0.02147,0.01242,-0.0854,0.2768,1.0000 7.750,1.2974,0.02215,0.01310,-0.0845,0.2507,1.0000 8.000,1.3172,0.02296,0.01386,-0.0834,0.2269,1.0000 8.250,1.3362,0.02384,0.01472,-0.0823,0.2064,1.0000 8.500,1.3541,0.02482,0.01566,-0.0810,0.1891,1.0000 8.750,1.3708,0.02588,0.01671,-0.0797,0.1732,1.0000 9.000,1.3869,0.02696,0.01778,-0.0784,0.1575,1.0000 9.250,1.4022,0.02806,0.01890,-0.0770,0.1428,1.0000 9.500,1.4165,0.02919,0.02006,-0.0755,0.1289,1.0000 9.750,1.4300,0.03034,0.02125,-0.0739,0.1151,1.0000 10.000,1.4429,0.03149,0.02253,-0.0723,0.1014,1.0000 10.250,1.4556,0.03263,0.02380,-0.0706,0.0861,1.0000 10.500,1.4639,0.03404,0.02525,-0.0685,0.0684,1.0000 10.750,1.4636,0.03591,0.02704,-0.0655,0.0544,1.0000 11.000,1.4616,0.03809,0.02923,-0.0628,0.0446,1.0000 11.250,1.4594,0.04048,0.03169,-0.0605,0.0386,1.0000 11.500,1.4554,0.04319,0.03448,-0.0587,0.0350,1.0000 11.750,1.4519,0.04604,0.03747,-0.0572,0.0327,1.0000 12.000,1.4482,0.04909,0.04069,-0.0562,0.0308,1.0000 12.250,1.4432,0.05248,0.04422,-0.0556,0.0292,1.0000 12.500,1.4359,0.05630,0.04818,-0.0555,0.0281,1.0000 12.750,1.4275,0.06045,0.05248,-0.0557,0.0271,1.0000 13.000,1.4211,0.06449,0.05673,-0.0560,0.0261,1.0000 13.250,1.4136,0.06881,0.06124,-0.0565,0.0253,1.0000 13.500,1.4051,0.07338,0.06598,-0.0574,0.0245,1.0000 13.750,1.3957,0.07820,0.07096,-0.0585,0.0239,1.0000 14.000,1.3859,0.08322,0.07614,-0.0598,0.0234,1.0000 14.250,1.3760,0.08840,0.08147,-0.0613,0.0230,1.0000 14.500,1.3664,0.09368,0.08689,-0.0629,0.0226,1.0000