Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe06k-il-100000-n5 Airfoil,goe06k-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,44.5679 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe06k-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.000,-0.4709,0.10411,0.09956,-0.0290,1.0000,0.0357 -7.750,-0.4817,0.10213,0.09766,-0.0277,1.0000,0.0358 -7.500,-0.4934,0.10004,0.09564,-0.0273,1.0000,0.0358 -7.250,-0.4992,0.09727,0.09291,-0.0280,1.0000,0.0359 -7.000,-0.5023,0.09419,0.08985,-0.0290,1.0000,0.0360 -6.750,-0.4883,0.08897,0.08461,-0.0342,0.9966,0.0362 -6.500,-0.4810,0.08462,0.08028,-0.0320,0.9948,0.0370 -6.250,-0.4676,0.08042,0.07604,-0.0344,0.9912,0.0380 -6.000,-0.4501,0.07592,0.07146,-0.0386,0.9876,0.0397 -5.750,-0.4322,0.07147,0.06690,-0.0430,0.9829,0.0420 -5.500,-0.3972,0.06729,0.06220,-0.0521,0.9774,0.0445 -5.250,-0.3870,0.06180,0.05674,-0.0526,0.9737,0.0454 -5.000,-0.3739,0.05807,0.05304,-0.0526,0.9708,0.0477 -4.750,-0.3496,0.05385,0.04860,-0.0552,0.9681,0.0489 -4.500,-0.3228,0.04770,0.04189,-0.0556,0.9634,0.0252 -4.250,-0.3029,0.04378,0.03774,-0.0561,0.9599,0.0235 -4.000,-0.2774,0.03999,0.03353,-0.0569,0.9572,0.0222 -3.750,-0.2523,0.03650,0.02958,-0.0569,0.9548,0.0211 -3.500,-0.2321,0.03358,0.02620,-0.0554,0.9508,0.0208 -3.250,-0.2071,0.03115,0.02326,-0.0547,0.9477,0.0222 -3.000,-0.1791,0.02883,0.02038,-0.0543,0.9453,0.0233 -2.750,-0.1496,0.02673,0.01774,-0.0541,0.9435,0.0236 -2.500,-0.1188,0.02498,0.01548,-0.0540,0.9421,0.0255 -2.250,-0.0962,0.02368,0.01401,-0.0530,0.9390,0.0289 -2.000,-0.0723,0.02266,0.01284,-0.0520,0.9355,0.0321 -1.750,-0.0459,0.02181,0.01186,-0.0517,0.9326,0.0390 -1.500,-0.0184,0.02109,0.01104,-0.0516,0.9301,0.0518 -1.250,0.0104,0.02043,0.01033,-0.0519,0.9282,0.0800 -1.000,0.0947,0.01754,0.01015,-0.0649,0.9344,1.0000 -0.750,0.1228,0.01769,0.00997,-0.0652,0.9313,1.0000 -0.500,0.1538,0.01785,0.00985,-0.0662,0.9288,1.0000 -0.250,0.1783,0.01801,0.00981,-0.0658,0.9246,1.0000 0.000,0.2011,0.01818,0.00982,-0.0651,0.9199,1.0000 0.250,0.2294,0.01836,0.00985,-0.0655,0.9168,1.0000 0.500,0.2609,0.01854,0.00991,-0.0666,0.9143,1.0000 0.750,0.2823,0.01875,0.01004,-0.0657,0.9093,1.0000 1.000,0.3060,0.01896,0.01019,-0.0652,0.9048,1.0000 1.250,0.3358,0.01914,0.01033,-0.0659,0.9015,1.0000 1.500,0.3681,0.01931,0.01049,-0.0672,0.8991,1.0000 1.750,0.3858,0.01954,0.01074,-0.0655,0.8920,1.0000 2.000,0.4179,0.01960,0.01083,-0.0665,0.8872,1.0000 2.250,0.4553,0.01960,0.01089,-0.0686,0.8840,1.0000 2.500,0.4725,0.01980,0.01116,-0.0666,0.8750,1.0000 2.750,0.5058,0.01985,0.01133,-0.0679,0.8713,1.0000 3.000,0.5268,0.02007,0.01165,-0.0668,0.8641,1.0000 3.250,0.5564,0.02015,0.01190,-0.0672,0.8588,1.0000 3.500,0.5935,0.02008,0.01204,-0.0690,0.8555,1.0000 3.750,0.6120,0.02022,0.01238,-0.0672,0.8449,1.0000 4.000,0.6455,0.01967,0.01210,-0.0675,0.8321,1.0000 4.250,0.6904,0.01801,0.01079,-0.0684,0.8093,1.0000 4.500,0.7220,0.01620,0.00919,-0.0659,0.7488,1.0000 4.750,0.7558,0.01911,0.00826,-0.0657,0.0727,1.0000 5.000,0.7690,0.02042,0.00939,-0.0628,0.0378,1.0000 5.250,0.7835,0.02148,0.01052,-0.0601,0.0286,1.0000 5.500,0.7963,0.02265,0.01186,-0.0571,0.0254,1.0000 5.750,0.8109,0.02380,0.01317,-0.0545,0.0221,1.0000 6.000,0.8286,0.02542,0.01488,-0.0526,0.0199,1.0000 6.250,0.8626,0.02850,0.01805,-0.0540,0.0180,1.0000 6.500,0.8942,0.03044,0.02036,-0.0542,0.0162,1.0000 6.750,0.9271,0.03338,0.02370,-0.0547,0.0156,1.0000 7.000,0.9526,0.03658,0.02738,-0.0536,0.0154,1.0000 7.250,0.9709,0.03988,0.03118,-0.0514,0.0155,1.0000 7.500,0.9832,0.04300,0.03478,-0.0484,0.0152,1.0000 7.750,0.9917,0.04593,0.03810,-0.0450,0.0148,1.0000 8.000,0.9971,0.04874,0.04126,-0.0415,0.0143,1.0000 8.250,1.0001,0.05148,0.04425,-0.0382,0.0138,1.0000 8.500,0.9972,0.05536,0.04861,-0.0332,0.0143,1.0000 8.750,0.9912,0.05916,0.05277,-0.0285,0.0148,1.0000 9.000,0.9825,0.06269,0.05658,-0.0239,0.0152,1.0000 9.250,0.9704,0.06580,0.05990,-0.0193,0.0156,1.0000 9.500,0.9549,0.06905,0.06334,-0.0148,0.0159,1.0000 9.750,0.9390,0.07236,0.06681,-0.0111,0.0161,1.0000 10.000,0.9237,0.07568,0.07027,-0.0084,0.0164,1.0000 10.250,0.9060,0.07950,0.07423,-0.0065,0.0166,1.0000 10.500,0.8881,0.08374,0.07858,-0.0057,0.0167,1.0000 10.750,0.8716,0.08828,0.08322,-0.0061,0.0169,1.0000 11.000,0.8551,0.09353,0.08855,-0.0077,0.0170,1.0000 11.250,0.8407,0.09944,0.09452,-0.0106,0.0171,1.0000 11.500,0.8292,0.10603,0.10114,-0.0144,0.0174,1.0000 11.750,0.8212,0.11190,0.10699,-0.0171,0.0179,1.0000