Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe403-il-200000-n5 Airfoil,goe403-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,72.9791 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe403-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.750,-0.3354,0.08996,0.08667,-0.0269,1.0000,0.0133 -7.500,-0.3431,0.08642,0.08323,-0.0280,1.0000,0.0116 -7.250,-0.3442,0.08423,0.08111,-0.0275,1.0000,0.0114 -7.000,-0.3415,0.08179,0.07873,-0.0280,1.0000,0.0113 -6.750,-0.3434,0.07869,0.07567,-0.0280,1.0000,0.0110 -6.500,-0.3377,0.07485,0.07187,-0.0308,0.9982,0.0109 -6.250,-0.3093,0.06886,0.06585,-0.0398,0.9896,0.0107 -6.000,-0.2775,0.06248,0.05941,-0.0495,0.9800,0.0109 -5.750,-0.2429,0.05568,0.05254,-0.0597,0.9697,0.0114 -5.500,-0.2105,0.05013,0.04687,-0.0678,0.9595,0.0126 -5.250,-0.1738,0.04423,0.04079,-0.0757,0.9504,0.0133 -5.000,-0.1350,0.03663,0.03284,-0.0838,0.9411,0.0136 -4.750,-0.0984,0.02478,0.02016,-0.0907,0.9307,0.0142 -4.500,-0.0663,0.01899,0.01338,-0.0930,0.9221,0.0168 -4.250,-0.0337,0.01639,0.01002,-0.0940,0.9138,0.0210 -4.000,-0.0028,0.01560,0.00905,-0.0947,0.9038,0.0261 -3.750,0.0291,0.01481,0.00787,-0.0954,0.8942,0.0330 -3.500,0.0605,0.01463,0.00759,-0.0962,0.8844,0.0394 -3.250,0.0899,0.01386,0.00654,-0.0964,0.8736,0.0445 -3.000,0.1187,0.01321,0.00574,-0.0965,0.8628,0.0477 -2.750,0.1472,0.01273,0.00509,-0.0965,0.8522,0.0507 -2.500,0.1752,0.01232,0.00450,-0.0963,0.8416,0.0532 -2.250,0.2027,0.01200,0.00401,-0.0961,0.8307,0.0553 -2.000,0.2294,0.01166,0.00363,-0.0958,0.8196,0.0601 -1.750,0.2562,0.01142,0.00331,-0.0954,0.8084,0.0644 -1.500,0.2829,0.01121,0.00298,-0.0950,0.7972,0.0693 -1.250,0.3095,0.01101,0.00277,-0.0946,0.7855,0.0814 -1.000,0.3359,0.01087,0.00262,-0.0942,0.7732,0.1007 -0.750,0.3622,0.01076,0.00248,-0.0938,0.7600,0.1200 -0.500,0.3884,0.01067,0.00237,-0.0934,0.7457,0.1383 -0.250,0.4145,0.01056,0.00228,-0.0930,0.7304,0.1613 0.000,0.4401,0.01037,0.00225,-0.0926,0.7133,0.2177 0.250,0.4643,0.00995,0.00225,-0.0920,0.6947,0.3670 0.750,0.5265,0.00873,0.00212,-0.0930,0.6534,1.0000 1.000,0.5519,0.00888,0.00210,-0.0924,0.6326,1.0000 1.250,0.5773,0.00904,0.00211,-0.0918,0.6126,1.0000 1.500,0.6026,0.00922,0.00215,-0.0912,0.5945,1.0000 1.750,0.6281,0.00941,0.00224,-0.0907,0.5783,1.0000 2.000,0.6536,0.00961,0.00234,-0.0902,0.5639,1.0000 2.250,0.6792,0.00980,0.00246,-0.0897,0.5508,1.0000 2.500,0.7050,0.01000,0.00261,-0.0893,0.5392,1.0000 2.750,0.7307,0.01021,0.00281,-0.0889,0.5285,1.0000 3.000,0.7556,0.01045,0.00298,-0.0883,0.5103,1.0000 3.250,0.7789,0.01076,0.00315,-0.0874,0.4779,1.0000 3.500,0.8035,0.01101,0.00337,-0.0868,0.4555,1.0000 3.750,0.8262,0.01137,0.00357,-0.0858,0.4122,1.0000 4.000,0.8454,0.01208,0.00382,-0.0844,0.3217,1.0000 4.250,0.8489,0.01502,0.00515,-0.0814,0.0271,1.0000 4.500,0.8724,0.01555,0.00572,-0.0805,0.0194,1.0000 4.750,0.8957,0.01609,0.00644,-0.0796,0.0158,1.0000 5.000,0.9182,0.01675,0.00728,-0.0786,0.0142,1.0000 5.250,0.9393,0.01756,0.00830,-0.0774,0.0132,1.0000 5.500,0.9546,0.01902,0.01000,-0.0754,0.0117,1.0000 5.750,0.9753,0.01975,0.01080,-0.0742,0.0106,1.0000 6.000,0.9920,0.02092,0.01207,-0.0724,0.0101,1.0000 6.250,1.0080,0.02221,0.01348,-0.0705,0.0098,1.0000 6.500,1.0242,0.02362,0.01496,-0.0686,0.0096,1.0000 6.750,1.0417,0.02516,0.01655,-0.0669,0.0094,1.0000 7.000,1.0614,0.02686,0.01833,-0.0655,0.0093,1.0000 7.250,1.0827,0.02853,0.02009,-0.0644,0.0089,1.0000 7.500,1.1031,0.03011,0.02173,-0.0634,0.0078,1.0000 7.750,1.1250,0.03286,0.02448,-0.0631,0.0071,1.0000 8.000,1.1476,0.03556,0.02736,-0.0623,0.0070,1.0000 8.250,1.1672,0.03776,0.02988,-0.0610,0.0071,1.0000 8.500,1.1849,0.03998,0.03239,-0.0594,0.0072,1.0000 8.750,1.1981,0.04246,0.03545,-0.0565,0.0080,1.0000 9.000,1.2093,0.04619,0.03961,-0.0540,0.0090,1.0000 9.250,1.2142,0.05027,0.04403,-0.0515,0.0100,1.0000 9.500,1.2309,0.05319,0.04727,-0.0494,0.0139,1.0000 9.750,1.2307,0.05637,0.05076,-0.0466,0.0139,1.0000 10.000,1.2267,0.05952,0.05417,-0.0439,0.0139,1.0000 10.250,1.2173,0.06245,0.05733,-0.0407,0.0138,1.0000 10.500,1.2043,0.06539,0.06047,-0.0377,0.0137,1.0000 10.750,1.1900,0.06857,0.06385,-0.0355,0.0137,1.0000 11.000,1.1741,0.07220,0.06766,-0.0343,0.0137,1.0000 11.250,1.1575,0.07624,0.07189,-0.0341,0.0136,1.0000 11.500,1.1402,0.08079,0.07662,-0.0349,0.0137,1.0000 11.750,1.1220,0.08593,0.08194,-0.0367,0.0137,1.0000 12.000,1.1032,0.09177,0.08794,-0.0395,0.0138,1.0000 12.250,1.0838,0.09841,0.09474,-0.0433,0.0139,1.0000 12.500,1.0645,0.10586,0.10234,-0.0482,0.0141,1.0000