Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe198-il-100000-n5 Airfoil,goe198-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,64.0313 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe198-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.2709,0.12208,0.11707,-0.0343,1.0000,0.0401 -9.500,-0.2744,0.12037,0.11542,-0.0322,1.0000,0.0405 -9.250,-0.2796,0.11899,0.11409,-0.0300,1.0000,0.0410 -9.000,-0.2739,0.11647,0.11159,-0.0307,0.9977,0.0417 -8.750,-0.2604,0.11324,0.10835,-0.0338,0.9939,0.0428 -8.500,-0.2482,0.11025,0.10536,-0.0368,0.9892,0.0443 -8.250,-0.2355,0.10785,0.10295,-0.0420,0.9838,0.0458 -8.000,-0.2280,0.10622,0.10132,-0.0473,0.9754,0.0462 -7.750,-0.2109,0.10249,0.09760,-0.0519,0.9705,0.0465 -7.500,-0.1952,0.09797,0.09307,-0.0516,0.9670,0.0471 -7.250,-0.1755,0.09424,0.08932,-0.0547,0.9626,0.0481 -7.000,-0.1528,0.09064,0.08570,-0.0595,0.9588,0.0494 -6.750,-0.1371,0.08777,0.08281,-0.0629,0.9513,0.0508 -6.500,-0.1080,0.08481,0.07979,-0.0723,0.9456,0.0532 -6.250,-0.0814,0.08216,0.07708,-0.0816,0.9370,0.0539 -6.000,-0.0659,0.07798,0.07291,-0.0805,0.9330,0.0546 -5.750,-0.0412,0.07445,0.06934,-0.0837,0.9293,0.0558 -5.250,0.0042,0.06885,0.06367,-0.0911,0.9165,0.0591 -5.000,0.0522,0.06622,0.06082,-0.1036,0.9115,0.0616 -4.750,0.0761,0.06316,0.05771,-0.1069,0.9048,0.0621 -4.500,0.0913,0.05997,0.05457,-0.1060,0.9006,0.0633 -4.250,0.1185,0.05726,0.05180,-0.1087,0.8971,0.0658 -4.000,0.1461,0.05507,0.04952,-0.1123,0.8895,0.0687 -3.750,0.2059,0.05282,0.04686,-0.1235,0.8850,0.0710 -3.500,0.2249,0.04942,0.04353,-0.1237,0.8804,0.0717 -3.250,0.2451,0.04712,0.04123,-0.1241,0.8730,0.0729 -3.000,0.2759,0.04477,0.03880,-0.1265,0.8685,0.0748 -2.750,0.3074,0.04274,0.03665,-0.1290,0.8620,0.0773 -2.500,0.3569,0.04112,0.03457,-0.1347,0.8555,0.0819 -2.250,0.3795,0.03828,0.03183,-0.1351,0.8502,0.0841 -2.000,0.4056,0.03664,0.03012,-0.1358,0.8407,0.0873 -1.750,0.4587,0.03309,0.02586,-0.1401,0.8356,0.0616 -1.250,0.5224,0.02879,0.02112,-0.1422,0.8197,0.0532 -1.000,0.5503,0.02744,0.01965,-0.1426,0.8095,0.0524 -0.750,0.5829,0.02593,0.01788,-0.1433,0.8025,0.0517 -0.500,0.6132,0.02471,0.01636,-0.1435,0.7921,0.0529 -0.250,0.6442,0.02355,0.01484,-0.1437,0.7828,0.0537 0.000,0.6741,0.02249,0.01356,-0.1437,0.7734,0.0536 0.250,0.7022,0.02163,0.01253,-0.1435,0.7616,0.0538 0.500,0.7305,0.02083,0.01161,-0.1432,0.7499,0.0544 0.750,0.7593,0.02012,0.01078,-0.1429,0.7386,0.0553 1.000,0.7867,0.01960,0.01020,-0.1426,0.7259,0.0567 1.250,0.8138,0.01921,0.00973,-0.1421,0.7134,0.0602 1.500,0.8414,0.01880,0.00927,-0.1417,0.7007,0.0635 1.750,0.8689,0.01841,0.00884,-0.1413,0.6876,0.0665 2.000,0.8959,0.01809,0.00840,-0.1407,0.6738,0.0706 2.250,0.9229,0.01782,0.00809,-0.1402,0.6593,0.0773 2.500,0.9499,0.01766,0.00786,-0.1398,0.6445,0.0929 2.750,0.9772,0.01750,0.00770,-0.1394,0.6297,0.1210 3.000,0.9973,0.01604,0.00773,-0.1378,0.6142,1.0000 3.250,1.0234,0.01625,0.00767,-0.1371,0.5964,1.0000 3.500,1.0488,0.01650,0.00770,-0.1364,0.5767,1.0000 3.750,1.0735,0.01681,0.00781,-0.1356,0.5556,1.0000 4.000,1.0980,0.01717,0.00797,-0.1348,0.5352,1.0000 4.250,1.1224,0.01753,0.00822,-0.1341,0.5172,1.0000 4.500,1.1468,0.01791,0.00849,-0.1334,0.5006,1.0000 4.750,1.1709,0.01829,0.00881,-0.1328,0.4841,1.0000 5.000,1.1944,0.01868,0.00914,-0.1320,0.4661,1.0000 5.250,1.2174,0.01909,0.00950,-0.1312,0.4470,1.0000 5.500,1.2401,0.01951,0.00987,-0.1303,0.4281,1.0000 5.750,1.2626,0.01995,0.01026,-0.1294,0.4107,1.0000 6.000,1.2844,0.02042,0.01069,-0.1285,0.3939,1.0000 6.250,1.3053,0.02096,0.01114,-0.1274,0.3771,1.0000 6.500,1.3257,0.02153,0.01163,-0.1262,0.3625,1.0000 6.750,1.3458,0.02214,0.01217,-0.1250,0.3500,1.0000 7.000,1.3664,0.02271,0.01277,-0.1239,0.3386,1.0000 7.250,1.3867,0.02331,0.01338,-0.1228,0.3288,1.0000 7.500,1.4063,0.02393,0.01402,-0.1216,0.3195,1.0000 7.750,1.4262,0.02452,0.01471,-0.1205,0.3103,1.0000 8.000,1.4436,0.02521,0.01541,-0.1189,0.2993,1.0000 8.250,1.4620,0.02582,0.01613,-0.1176,0.2885,1.0000 8.500,1.4795,0.02646,0.01688,-0.1161,0.2785,1.0000 8.750,1.4947,0.02717,0.01766,-0.1142,0.2668,1.0000 9.000,1.5087,0.02789,0.01850,-0.1123,0.2507,1.0000 9.250,1.5198,0.02867,0.01937,-0.1098,0.2296,1.0000 9.500,1.5283,0.02967,0.02037,-0.1072,0.2048,1.0000 9.750,1.5313,0.03111,0.02166,-0.1041,0.1745,1.0000 10.000,1.5325,0.03288,0.02328,-0.1011,0.1478,1.0000 10.250,1.5340,0.03478,0.02511,-0.0984,0.1241,1.0000 10.500,1.5352,0.03680,0.02706,-0.0958,0.1079,1.0000 10.750,1.5367,0.03884,0.02911,-0.0935,0.0976,1.0000 11.000,1.5380,0.04096,0.03126,-0.0913,0.0906,1.0000 11.250,1.5369,0.04335,0.03368,-0.0891,0.0850,1.0000 11.500,1.5365,0.04574,0.03617,-0.0872,0.0807,1.0000 11.750,1.5342,0.04840,0.03892,-0.0854,0.0771,1.0000 12.000,1.5288,0.05146,0.04209,-0.0838,0.0744,1.0000 12.250,1.5250,0.05448,0.04524,-0.0824,0.0719,1.0000 12.500,1.5209,0.05764,0.04857,-0.0813,0.0695,1.0000 12.750,1.5144,0.06120,0.05226,-0.0804,0.0673,1.0000 13.000,1.5049,0.06522,0.05638,-0.0797,0.0652,1.0000 13.250,1.4961,0.06929,0.06053,-0.0792,0.0632,1.0000 13.500,1.4931,0.07284,0.06428,-0.0789,0.0610,1.0000 13.750,1.4886,0.07664,0.06823,-0.0788,0.0588,1.0000 14.000,1.4833,0.08056,0.07225,-0.0788,0.0567,1.0000 14.250,1.4785,0.08417,0.07589,-0.0784,0.0546,1.0000 14.500,1.4768,0.08780,0.07973,-0.0785,0.0521,1.0000 14.750,1.4742,0.09159,0.08369,-0.0788,0.0493,1.0000 15.000,1.4715,0.09522,0.08738,-0.0790,0.0467,1.0000 15.250,1.4690,0.09902,0.09133,-0.0794,0.0440,1.0000