Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe289-il-100000 Airfoil,goe289-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,38.6075 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe289-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.500,-0.1607,0.12784,0.12329,-0.0589,0.9737,0.1153 -10.250,-0.1585,0.12536,0.12081,-0.0661,0.9674,0.1201 -10.000,-0.1680,0.12264,0.11813,-0.0744,0.9590,0.1215 -9.750,-0.1186,0.11582,0.11123,-0.0747,0.9572,0.1235 -9.500,-0.0951,0.11218,0.10757,-0.0766,0.9496,0.1262 -9.250,-0.0734,0.10839,0.10375,-0.0811,0.9445,0.1304 -9.000,-0.0916,0.10698,0.10238,-0.0890,0.9329,0.1358 -8.750,-0.0637,0.10115,0.09653,-0.0923,0.9292,0.1380 -8.500,-0.0203,0.09671,0.09203,-0.0946,0.9271,0.1422 -8.250,-0.0080,0.09386,0.08918,-0.0969,0.9176,0.1467 -8.000,-0.0540,0.09313,0.08853,-0.1060,0.9009,0.1525 -7.750,0.0024,0.08644,0.08177,-0.1074,0.9013,0.1548 -7.500,0.0419,0.08246,0.07774,-0.1102,0.8977,0.1585 -7.250,0.0648,0.07861,0.07384,-0.1161,0.8929,0.1652 -7.000,-0.0164,0.07824,0.07354,-0.1189,0.8661,0.1700 -6.750,0.0325,0.07380,0.06909,-0.1177,0.8641,0.1719 -6.500,-0.0573,0.05657,0.05131,-0.1277,0.8442,0.1064 -6.250,-0.0885,0.04879,0.04292,-0.1262,0.8315,0.0959 -6.000,-0.0723,0.04437,0.03794,-0.1273,0.8253,0.0942 -5.750,-0.0657,0.04201,0.03525,-0.1253,0.8155,0.0942 -5.500,-0.0440,0.03902,0.03172,-0.1254,0.8090,0.0947 -5.250,-0.0089,0.03576,0.02799,-0.1273,0.8057,0.0954 -5.000,-0.0035,0.03478,0.02688,-0.1239,0.7939,0.0962 -4.750,0.0354,0.03273,0.02461,-0.1258,0.7900,0.0985 -4.500,0.0502,0.03198,0.02371,-0.1236,0.7801,0.1005 -4.250,0.0842,0.03046,0.02184,-0.1243,0.7746,0.1053 -4.000,0.1272,0.02885,0.02011,-0.1266,0.7712,0.1126 -3.750,0.1367,0.02867,0.01982,-0.1233,0.7597,0.1180 -3.500,0.1769,0.02718,0.01825,-0.1249,0.7553,0.1314 -3.250,0.1931,0.02673,0.01778,-0.1228,0.7461,0.1492 -3.000,0.2237,0.02577,0.01688,-0.1229,0.7397,0.1818 -2.750,0.2659,0.02477,0.01585,-0.1250,0.7358,0.2109 -2.500,0.2732,0.02508,0.01618,-0.1215,0.7243,0.2257 -2.250,0.3125,0.02455,0.01561,-0.1231,0.7194,0.2565 -2.000,0.3244,0.02486,0.01597,-0.1204,0.7094,0.2753 -1.750,0.3581,0.02438,0.01557,-0.1210,0.7034,0.2996 -1.500,0.3835,0.02424,0.01544,-0.1203,0.6962,0.3239 -1.250,0.4043,0.02415,0.01543,-0.1188,0.6878,0.3540 -1.000,0.4426,0.02337,0.01473,-0.1201,0.6831,0.4132 -0.750,0.4494,0.02360,0.01518,-0.1165,0.6730,0.4583 -0.500,0.4825,0.02294,0.01473,-0.1168,0.6674,0.5257 -0.250,0.5023,0.02293,0.01492,-0.1151,0.6597,0.5863 0.000,0.5259,0.02262,0.01493,-0.1139,0.6522,0.6746 0.250,0.6593,0.02141,0.01396,-0.1333,0.6462,1.0000 0.500,0.6653,0.02203,0.01447,-0.1297,0.6367,1.0000 0.750,0.7001,0.02192,0.01407,-0.1307,0.6313,1.0000 1.000,0.7093,0.02251,0.01459,-0.1276,0.6225,1.0000 1.250,0.7378,0.02255,0.01443,-0.1275,0.6161,1.0000 1.500,0.7626,0.02277,0.01449,-0.1269,0.6096,1.0000 1.750,0.7767,0.02326,0.01490,-0.1246,0.6016,1.0000 2.000,0.8130,0.02315,0.01458,-0.1258,0.5966,1.0000 2.250,0.8202,0.02389,0.01532,-0.1224,0.5882,1.0000 2.500,0.8490,0.02397,0.01525,-0.1224,0.5820,1.0000 2.750,0.8772,0.02416,0.01529,-0.1224,0.5762,1.0000 3.000,0.8868,0.02483,0.01597,-0.1194,0.5681,1.0000 3.250,0.9219,0.02481,0.01578,-0.1205,0.5631,1.0000 3.500,0.9327,0.02559,0.01658,-0.1178,0.5562,1.0000 3.750,0.9522,0.02604,0.01698,-0.1165,0.5496,1.0000 4.000,0.9911,0.02597,0.01673,-0.1182,0.5451,1.0000 4.250,0.9914,0.02706,0.01791,-0.1139,0.5375,1.0000 4.500,1.0156,0.02740,0.01818,-0.1133,0.5317,1.0000 4.750,1.0563,0.02736,0.01796,-0.1154,0.5276,1.0000 5.000,1.0479,0.02881,0.01958,-0.1099,0.5204,1.0000 5.250,1.0678,0.02938,0.02012,-0.1088,0.5151,1.0000 5.500,1.1072,0.02940,0.02001,-0.1106,0.5113,1.0000 5.750,1.1010,0.03091,0.02165,-0.1057,0.5051,1.0000 6.000,1.1081,0.03190,0.02268,-0.1028,0.4993,1.0000 6.250,1.1451,0.03194,0.02264,-0.1042,0.4954,1.0000 6.500,1.1728,0.03248,0.02314,-0.1044,0.4917,1.0000 6.750,1.1177,0.03573,0.02664,-0.0930,0.4845,1.0000 7.000,1.1379,0.03641,0.02733,-0.0921,0.4805,1.0000 7.250,1.1847,0.03629,0.02714,-0.0950,0.4777,1.0000 7.500,0.9239,0.05571,0.04700,-0.0702,0.4575,1.0000 7.750,0.9822,0.05265,0.04388,-0.0709,0.4578,1.0000 8.000,1.0478,0.04948,0.04067,-0.0727,0.4581,1.0000 8.250,1.1307,0.04584,0.03697,-0.0767,0.4585,1.0000 9.500,0.6109,0.12096,0.11287,-0.0720,0.4686,1.0000 9.750,0.6254,0.12296,0.11488,-0.0720,0.4642,1.0000