Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe242-il-100000-n5 Airfoil,goe242-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,54.4004 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe242-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,0.0091,0.10222,0.09724,-0.0961,0.8712,0.0679 -9.500,-0.0025,0.09930,0.09434,-0.1022,0.8601,0.0727 -9.250,-0.0032,0.09574,0.09078,-0.1055,0.8493,0.0730 -8.750,0.0055,0.08028,0.07519,-0.1091,0.8327,0.0412 -8.500,0.0124,0.07722,0.07212,-0.1099,0.8222,0.0408 -8.250,0.0167,0.07338,0.06824,-0.1117,0.8130,0.0404 -8.000,0.0149,0.06836,0.06323,-0.1149,0.8018,0.0403 -7.750,0.0067,0.06156,0.05640,-0.1206,0.7913,0.0401 -7.500,0.0024,0.05209,0.04670,-0.1353,0.7814,0.0398 -7.250,0.0330,0.04189,0.03578,-0.1605,0.7691,0.0403 -7.000,0.0755,0.03657,0.02967,-0.1731,0.7597,0.0409 -6.750,0.1132,0.03314,0.02573,-0.1794,0.7506,0.0421 -6.500,0.1431,0.03139,0.02386,-0.1817,0.7409,0.0440 -6.250,0.1783,0.02951,0.02164,-0.1849,0.7331,0.0457 -6.000,0.2122,0.02784,0.01964,-0.1873,0.7240,0.0466 -5.750,0.2462,0.02651,0.01796,-0.1892,0.7170,0.0485 -5.500,0.2791,0.02557,0.01669,-0.1908,0.7089,0.0503 -5.250,0.3081,0.02446,0.01550,-0.1912,0.7023,0.0513 -5.000,0.3362,0.02369,0.01470,-0.1913,0.6954,0.0525 -4.750,0.3649,0.02310,0.01407,-0.1915,0.6887,0.0542 -4.500,0.3946,0.02265,0.01352,-0.1919,0.6832,0.0570 -4.250,0.4234,0.02235,0.01316,-0.1921,0.6765,0.0590 -4.000,0.4538,0.02207,0.01275,-0.1925,0.6713,0.0604 -3.750,0.4878,0.02169,0.01227,-0.1941,0.6668,0.0626 -3.500,0.5230,0.02134,0.01184,-0.1964,0.6614,0.0660 -3.250,0.5586,0.02104,0.01138,-0.1985,0.6568,0.0722 -3.000,0.5969,0.02061,0.01085,-0.2013,0.6531,0.0824 -2.750,0.6441,0.01953,0.01022,-0.2073,0.6485,0.2206 -2.500,0.6731,0.01980,0.01110,-0.2076,0.6438,0.3756 -2.250,0.7021,0.02025,0.01139,-0.2075,0.6398,0.4174 -2.000,0.7310,0.02069,0.01164,-0.2074,0.6365,0.4402 -1.750,0.7587,0.02108,0.01192,-0.2073,0.6328,0.4535 -1.500,0.7833,0.02161,0.01244,-0.2063,0.6291,0.4656 -1.250,0.8079,0.02216,0.01296,-0.2053,0.6257,0.4803 -1.000,0.8339,0.02260,0.01333,-0.2046,0.6227,0.4935 -0.750,0.8636,0.02280,0.01339,-0.2049,0.6199,0.5015 -0.500,0.8921,0.02302,0.01354,-0.2054,0.6164,0.5076 -0.250,0.9182,0.02329,0.01381,-0.2051,0.6127,0.5122 0.000,0.9475,0.02349,0.01394,-0.2058,0.6097,0.5183 0.250,0.9772,0.02367,0.01403,-0.2064,0.6069,0.5239 0.500,1.0051,0.02388,0.01419,-0.2064,0.6043,0.5282 0.750,1.0343,0.02409,0.01433,-0.2069,0.6015,0.5329 1.000,1.0627,0.02436,0.01459,-0.2077,0.5978,0.5370 1.250,1.0908,0.02458,0.01480,-0.2082,0.5942,0.5395 1.500,1.1189,0.02472,0.01490,-0.2084,0.5899,0.5417 1.750,1.1492,0.02475,0.01481,-0.2089,0.5854,0.5445 2.000,1.1724,0.02502,0.01516,-0.2085,0.5782,0.5475 2.250,1.2013,0.02507,0.01513,-0.2089,0.5723,0.5507 2.500,1.2314,0.02516,0.01512,-0.2096,0.5676,0.5539 2.750,1.2550,0.02548,0.01553,-0.2092,0.5619,0.5562 3.000,1.2811,0.02566,0.01573,-0.2092,0.5571,0.5585 3.250,1.3101,0.02576,0.01580,-0.2095,0.5532,0.5614 3.500,1.3342,0.02610,0.01620,-0.2092,0.5484,0.5648 3.750,1.3583,0.02643,0.01660,-0.2090,0.5432,0.5684 4.000,1.3858,0.02660,0.01677,-0.2092,0.5387,0.5718 4.250,1.4143,0.02670,0.01684,-0.2094,0.5349,0.5742 4.500,1.4331,0.02721,0.01755,-0.2083,0.5290,0.5769 4.750,1.4570,0.02749,0.01789,-0.2079,0.5239,0.5802 5.000,1.4851,0.02761,0.01799,-0.2081,0.5197,0.5844 5.250,1.5048,0.02809,0.01859,-0.2072,0.5140,0.5882 5.500,1.5251,0.02845,0.01908,-0.2062,0.5080,0.5913 5.750,1.5515,0.02852,0.01916,-0.2060,0.5030,0.5950 6.000,1.5663,0.02912,0.01992,-0.2043,0.4959,0.5986 6.250,1.5870,0.02943,0.02030,-0.2034,0.4894,0.6027 6.500,1.6061,0.02976,0.02071,-0.2021,0.4832,0.6061 6.750,1.6184,0.03037,0.02148,-0.2000,0.4755,0.6097 7.000,1.6397,0.03055,0.02168,-0.1990,0.4695,0.6144 7.250,1.6442,0.03151,0.02284,-0.1958,0.4605,0.6187 7.500,1.6590,0.03181,0.02319,-0.1938,0.4537,0.6226 7.750,1.6570,0.03300,0.02457,-0.1899,0.4439,0.6260 8.000,1.6653,0.03384,0.02549,-0.1874,0.4351,0.6302 8.250,1.6714,0.03488,0.02661,-0.1849,0.4252,0.6348 8.500,1.6721,0.03637,0.02825,-0.1820,0.4143,0.6385 8.750,1.6771,0.03765,0.02960,-0.1797,0.4040,0.6431 9.000,1.6840,0.03887,0.03084,-0.1776,0.3939,0.6485 9.250,1.6855,0.04065,0.03270,-0.1753,0.3831,0.6532 9.500,1.6909,0.04214,0.03423,-0.1733,0.3735,0.6582 9.750,1.6975,0.04359,0.03567,-0.1715,0.3644,0.6640 10.000,1.6989,0.04561,0.03776,-0.1696,0.3546,0.6692 10.250,1.7028,0.04736,0.03949,-0.1677,0.3449,0.6749 10.500,1.7026,0.04957,0.04168,-0.1658,0.3342,0.6813 10.750,1.6997,0.05217,0.04434,-0.1639,0.3239,0.6872 11.000,1.6990,0.05452,0.04667,-0.1622,0.3138,0.6945 11.250,1.6959,0.05729,0.04950,-0.1606,0.3044,0.7017 11.500,1.6959,0.05982,0.05212,-0.1592,0.2965,0.7104 11.750,1.6948,0.06257,0.05496,-0.1580,0.2885,0.7198 12.000,1.6941,0.06532,0.05781,-0.1569,0.2809,0.7315 12.500,1.6900,0.07135,0.06411,-0.1551,0.2655,0.7710 12.750,1.6825,0.07454,0.06752,-0.1539,0.2588,1.0000 13.000,1.6833,0.07736,0.07033,-0.1533,0.2521,1.0000 13.250,1.6790,0.08115,0.07429,-0.1529,0.2456,1.0000 13.500,1.6776,0.08437,0.07757,-0.1525,0.2388,1.0000 13.750,1.6738,0.08812,0.08146,-0.1523,0.2324,1.0000 14.000,1.6683,0.09209,0.08551,-0.1522,0.2247,1.0000 14.250,1.6611,0.09639,0.08992,-0.1522,0.2167,1.0000 14.500,1.6544,0.10063,0.09424,-0.1523,0.2085,1.0000 14.750,1.6473,0.10509,0.09885,-0.1526,0.2008,1.0000 15.000,1.6398,0.10958,0.10340,-0.1530,0.1920,1.0000 15.250,1.6311,0.11446,0.10846,-0.1537,0.1822,1.0000 15.500,1.6220,0.11942,0.11353,-0.1546,0.1697,1.0000 15.750,1.6100,0.12481,0.11892,-0.1557,0.1438,1.0000 16.000,1.5848,0.13232,0.12608,-0.1577,0.1017,1.0000 16.250,1.5614,0.13991,0.13353,-0.1601,0.0876,1.0000