Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe233-il-200000-n5 Airfoil,goe233-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,87.1012 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe233-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.1294,0.10263,0.09882,-0.0762,0.9541,0.0321 -9.750,-0.1174,0.09945,0.09564,-0.0780,0.9464,0.0316 -9.500,-0.1119,0.09492,0.09109,-0.0813,0.9381,0.0321 -9.250,-0.1070,0.09053,0.08668,-0.0841,0.9287,0.0323 -9.000,-0.0987,0.08732,0.08346,-0.0856,0.9196,0.0321 -8.750,-0.0918,0.08380,0.07992,-0.0874,0.9106,0.0320 -8.500,-0.0869,0.07997,0.07608,-0.0894,0.9011,0.0319 -8.000,-0.1185,0.05898,0.05497,-0.1062,0.8780,0.0323 -7.750,-0.0560,0.02985,0.02448,-0.1727,0.8656,0.0323 -7.500,-0.0063,0.02597,0.02013,-0.1838,0.8605,0.0330 -7.250,0.0262,0.02440,0.01847,-0.1867,0.8541,0.0338 -7.000,0.0616,0.02286,0.01673,-0.1902,0.8476,0.0346 -6.750,0.0957,0.02158,0.01526,-0.1927,0.8425,0.0351 -6.500,0.1283,0.02058,0.01411,-0.1946,0.8358,0.0356 -6.250,0.1601,0.01975,0.01315,-0.1960,0.8295,0.0361 -6.000,0.1917,0.01905,0.01231,-0.1971,0.8237,0.0366 -5.750,0.2232,0.01844,0.01159,-0.1983,0.8163,0.0375 -5.500,0.2541,0.01791,0.01099,-0.1991,0.8102,0.0383 -5.250,0.2852,0.01745,0.01051,-0.2001,0.8038,0.0390 -5.000,0.3174,0.01695,0.00994,-0.2014,0.7968,0.0397 -4.750,0.3504,0.01642,0.00929,-0.2028,0.7909,0.0404 -4.500,0.3831,0.01591,0.00870,-0.2043,0.7832,0.0413 -4.250,0.4157,0.01545,0.00809,-0.2056,0.7765,0.0423 -4.000,0.4477,0.01505,0.00755,-0.2067,0.7695,0.0434 -3.500,0.5112,0.01427,0.00660,-0.2087,0.7537,0.0496 -3.250,0.5424,0.01393,0.00627,-0.2095,0.7452,0.0613 -3.000,0.5730,0.01369,0.00593,-0.2101,0.7382,0.0809 -2.750,0.6045,0.01330,0.00562,-0.2111,0.7304,0.1128 -2.500,0.6347,0.01310,0.00538,-0.2116,0.7238,0.1483 -2.250,0.6646,0.01294,0.00521,-0.2120,0.7169,0.1715 -2.000,0.6941,0.01281,0.00517,-0.2124,0.7100,0.2055 -1.750,0.7226,0.01289,0.00530,-0.2123,0.7038,0.2415 -1.500,0.7510,0.01297,0.00535,-0.2123,0.6968,0.2606 -1.250,0.7792,0.01310,0.00541,-0.2121,0.6907,0.2729 -1.000,0.8074,0.01325,0.00553,-0.2119,0.6847,0.2840 -0.750,0.8354,0.01341,0.00564,-0.2117,0.6783,0.2957 -0.500,0.8632,0.01362,0.00576,-0.2114,0.6727,0.3060 -0.250,0.8905,0.01387,0.00603,-0.2110,0.6660,0.3136 0.000,0.9182,0.01404,0.00614,-0.2107,0.6593,0.3203 0.250,0.9464,0.01412,0.00612,-0.2106,0.6528,0.3255 0.500,0.9736,0.01429,0.00631,-0.2103,0.6451,0.3287 0.750,1.0009,0.01448,0.00643,-0.2099,0.6383,0.3337 1.000,1.0290,0.01456,0.00645,-0.2099,0.6309,0.3404 1.250,1.0560,0.01472,0.00663,-0.2095,0.6242,0.3431 1.500,1.0831,0.01486,0.00677,-0.2092,0.6175,0.3461 1.750,1.1104,0.01497,0.00687,-0.2090,0.6099,0.3495 2.000,1.1379,0.01510,0.00691,-0.2088,0.6032,0.3538 2.250,1.1652,0.01518,0.00702,-0.2086,0.5962,0.3573 2.500,1.1921,0.01532,0.00717,-0.2083,0.5896,0.3595 2.750,1.2189,0.01544,0.00731,-0.2080,0.5825,0.3617 3.000,1.2456,0.01554,0.00742,-0.2078,0.5745,0.3638 3.250,1.2724,0.01567,0.00754,-0.2075,0.5676,0.3662 3.500,1.2988,0.01578,0.00767,-0.2072,0.5591,0.3691 3.750,1.3249,0.01593,0.00777,-0.2067,0.5501,0.3721 4.000,1.3505,0.01606,0.00797,-0.2062,0.5401,0.3738 4.250,1.3759,0.01621,0.00816,-0.2057,0.5309,0.3756 4.500,1.4012,0.01639,0.00835,-0.2052,0.5215,0.3776 4.750,1.4265,0.01656,0.00858,-0.2047,0.5126,0.3799 5.000,1.4513,0.01677,0.00879,-0.2041,0.5034,0.3824 5.250,1.4761,0.01698,0.00904,-0.2035,0.4935,0.3851 5.500,1.5001,0.01723,0.00929,-0.2027,0.4836,0.3878 5.750,1.5234,0.01749,0.00961,-0.2019,0.4722,0.3899 6.000,1.5463,0.01778,0.00994,-0.2010,0.4605,0.3923 6.250,1.5685,0.01811,0.01029,-0.1999,0.4490,0.3947 6.750,1.6103,0.01890,0.01110,-0.1975,0.4219,0.3998 7.000,1.6289,0.01940,0.01156,-0.1959,0.4046,0.4023 7.250,1.6455,0.01997,0.01210,-0.1940,0.3838,0.4044 7.500,1.6598,0.02063,0.01274,-0.1917,0.3581,0.4068 7.750,1.6697,0.02149,0.01348,-0.1888,0.3271,0.4092 8.000,1.6741,0.02251,0.01436,-0.1850,0.2973,0.4116 8.250,1.6772,0.02359,0.01534,-0.1811,0.2765,0.4139 8.500,1.6848,0.02465,0.01635,-0.1782,0.2621,0.4162 8.750,1.6928,0.02575,0.01745,-0.1754,0.2503,0.4184 9.000,1.6995,0.02697,0.01867,-0.1726,0.2396,0.4203 9.250,1.7083,0.02810,0.01985,-0.1702,0.2299,0.4225 9.500,1.7156,0.02938,0.02117,-0.1678,0.2211,0.4249 9.750,1.7232,0.03070,0.02253,-0.1654,0.2115,0.4278 10.000,1.7311,0.03203,0.02393,-0.1633,0.2027,0.4309 10.250,1.7373,0.03355,0.02548,-0.1610,0.1928,0.4338 10.500,1.7454,0.03495,0.02696,-0.1591,0.1807,0.4365 10.750,1.7503,0.03667,0.02871,-0.1570,0.1647,0.4392 11.000,1.7504,0.03887,0.03086,-0.1547,0.1405,0.4416 11.250,1.7414,0.04201,0.03380,-0.1520,0.1092,0.4436 11.500,1.7317,0.04535,0.03700,-0.1494,0.0880,0.4456 11.750,1.7261,0.04839,0.04002,-0.1473,0.0758,0.4479 12.000,1.7225,0.05134,0.04300,-0.1454,0.0676,0.4502 12.250,1.7199,0.05426,0.04599,-0.1438,0.0613,0.4528 12.500,1.7185,0.05715,0.04897,-0.1424,0.0568,0.4559 12.750,1.7169,0.06017,0.05208,-0.1412,0.0529,0.4594 13.000,1.7130,0.06355,0.05552,-0.1400,0.0499,0.4629 13.250,1.7128,0.06653,0.05865,-0.1391,0.0472,0.4667 13.500,1.7106,0.06984,0.06208,-0.1383,0.0449,0.4706 13.750,1.7062,0.07351,0.06584,-0.1376,0.0429,0.4746 14.000,1.7013,0.07733,0.06976,-0.1370,0.0412,0.4788 14.250,1.6996,0.08076,0.07334,-0.1365,0.0394,0.4836 14.500,1.6965,0.08442,0.07715,-0.1362,0.0377,0.4892 14.750,1.6916,0.08842,0.08126,-0.1360,0.0363,0.4956 15.000,1.6845,0.09280,0.08575,-0.1360,0.0351,0.5026 15.500,1.6762,0.10086,0.09412,-0.1363,0.0326,0.5308 15.750,1.6732,0.10458,0.09827,-0.1366,0.0313,0.8378 16.000,1.6660,0.10860,0.10240,-0.1368,0.0303,1.0000 16.250,1.6601,0.11307,0.10695,-0.1374,0.0293,1.0000