Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe55-il-100000 Airfoil,goe55-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,42.3501 Max Cl/Cd alpha,5.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe55-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.6211,0.11228,0.10724,0.0386,1.0000,0.0842 -8.250,-0.6202,0.10922,0.10421,0.0354,1.0000,0.0872 -8.000,-0.6275,0.10713,0.10219,0.0249,1.0000,0.0889 -7.750,-0.6215,0.10214,0.09720,0.0160,1.0000,0.0898 -7.500,-0.6100,0.09728,0.09238,0.0247,1.0000,0.0913 -7.250,-0.5985,0.09359,0.08871,0.0261,1.0000,0.0935 -7.000,-0.5877,0.08987,0.08500,0.0239,1.0000,0.0964 -6.750,-0.5658,0.08555,0.08038,0.0012,1.0000,0.1031 -6.500,-0.5580,0.08008,0.07509,0.0062,1.0000,0.1046 -6.250,-0.5464,0.07682,0.07188,0.0097,1.0000,0.1073 -6.000,-0.5292,0.07314,0.06818,0.0072,1.0000,0.1121 -5.750,-0.5021,0.06761,0.06241,-0.0039,1.0000,0.1190 -5.500,-0.4877,0.06428,0.05916,-0.0020,1.0000,0.1217 -5.250,-0.4551,0.06011,0.05462,-0.0110,1.0000,0.1332 -5.000,-0.4408,0.05661,0.05128,-0.0087,1.0000,0.1362 -4.750,-0.4127,0.05309,0.04755,-0.0130,1.0000,0.1494 -4.500,-0.3930,0.05031,0.04485,-0.0123,1.0000,0.1562 -4.250,-0.3665,0.04704,0.04146,-0.0147,1.0000,0.1682 -4.000,-0.3328,0.04543,0.03947,-0.0186,1.0000,0.1931 -3.750,-0.3136,0.04149,0.03573,-0.0179,1.0000,0.1989 -3.500,-0.2721,0.02399,0.01866,-0.0182,1.0000,0.2269 -3.250,-0.2520,0.02183,0.01660,-0.0174,1.0000,0.2480 -3.000,-0.2303,0.01974,0.01454,-0.0171,1.0000,0.2802 -2.750,-0.1574,0.02671,0.01862,-0.0285,1.0000,0.1186 -2.500,-0.1272,0.02431,0.01611,-0.0288,1.0000,0.1117 -2.250,-0.0961,0.02249,0.01402,-0.0290,1.0000,0.1104 -2.000,-0.0654,0.02094,0.01224,-0.0291,1.0000,0.1100 -1.750,-0.0350,0.01953,0.01062,-0.0290,1.0000,0.1091 -1.500,-0.0053,0.01837,0.00935,-0.0288,1.0000,0.1103 -1.250,0.0240,0.01740,0.00834,-0.0286,1.0000,0.1137 -1.000,0.0530,0.01642,0.00741,-0.0284,1.0000,0.1201 -0.750,0.0818,0.01553,0.00672,-0.0282,1.0000,0.1271 -0.500,0.1113,0.01460,0.00610,-0.0283,1.0000,0.1366 -0.250,0.1452,0.01491,0.00573,-0.0276,0.6712,0.1602 0.000,0.1712,0.01472,0.00535,-0.0266,0.6013,0.2091 0.250,0.1922,0.01224,0.00482,-0.0240,0.5717,1.0000 0.500,0.2205,0.01264,0.00480,-0.0236,0.5487,1.0000 0.750,0.2487,0.01304,0.00490,-0.0234,0.5314,1.0000 1.000,0.2773,0.01343,0.00506,-0.0232,0.5174,1.0000 1.250,0.3058,0.01383,0.00528,-0.0231,0.5043,1.0000 1.500,0.3339,0.01422,0.00550,-0.0229,0.4889,1.0000 1.750,0.3620,0.01461,0.00573,-0.0227,0.4731,1.0000 2.000,0.3900,0.01502,0.00599,-0.0224,0.4591,1.0000 2.250,0.4180,0.01546,0.00631,-0.0222,0.4470,1.0000 2.500,0.4465,0.01584,0.00668,-0.0222,0.4347,1.0000 2.750,0.4748,0.01628,0.00710,-0.0221,0.4227,1.0000 3.000,0.5027,0.01675,0.00753,-0.0219,0.4106,1.0000 3.250,0.5305,0.01724,0.00795,-0.0216,0.3976,1.0000 3.500,0.5581,0.01767,0.00835,-0.0214,0.3819,1.0000 3.750,0.5856,0.01799,0.00871,-0.0211,0.3627,1.0000 4.000,0.6127,0.01824,0.00895,-0.0208,0.3425,1.0000 4.250,0.6398,0.01847,0.00913,-0.0204,0.3232,1.0000 4.500,0.6669,0.01869,0.00930,-0.0200,0.3048,1.0000 4.750,0.6943,0.01878,0.00951,-0.0197,0.2838,1.0000 5.000,0.7216,0.01859,0.00936,-0.0194,0.2608,1.0000 5.250,0.7492,0.01841,0.00928,-0.0191,0.2349,1.0000 5.500,0.7767,0.01834,0.00917,-0.0188,0.1998,1.0000 5.750,0.8021,0.01971,0.01007,-0.0187,0.1416,1.0000 6.000,0.8277,0.02129,0.01151,-0.0185,0.1162,1.0000 6.250,0.8537,0.02258,0.01279,-0.0181,0.1046,1.0000 6.500,0.8793,0.02408,0.01426,-0.0177,0.0983,1.0000 6.750,0.9057,0.02550,0.01583,-0.0172,0.0936,1.0000 7.000,0.9314,0.02702,0.01738,-0.0168,0.0901,1.0000 7.250,0.9564,0.02917,0.01951,-0.0165,0.0873,1.0000 7.500,0.9817,0.03094,0.02170,-0.0161,0.0846,1.0000 7.750,1.0058,0.03307,0.02419,-0.0157,0.0822,1.0000 8.000,1.0286,0.03570,0.02721,-0.0154,0.0810,1.0000 8.250,1.0493,0.03883,0.03079,-0.0152,0.0802,1.0000 8.500,1.0671,0.04247,0.03494,-0.0150,0.0795,1.0000 8.750,1.0841,0.04579,0.03858,-0.0149,0.0783,1.0000 9.000,1.1000,0.04914,0.04212,-0.0148,0.0769,1.0000 9.250,1.0819,0.05961,0.05382,-0.0177,0.0792,1.0000 9.500,1.0253,0.07659,0.07149,-0.0284,0.0841,1.0000 9.750,0.9890,0.09133,0.08628,-0.0408,0.0889,1.0000 10.000,0.9980,0.09324,0.08819,-0.0390,0.0881,1.0000