Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe144-il-500000 Airfoil,goe144-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,106.147 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-goe144-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.750,-0.3448,0.08855,0.08645,-0.0227,1.0000,0.0223 -7.500,-0.3533,0.08687,0.08482,-0.0207,1.0000,0.0232 -7.250,-0.3693,0.08579,0.08380,-0.0170,1.0000,0.0234 -7.000,-0.3530,0.08089,0.07890,-0.0261,0.9968,0.0254 -6.750,-0.3245,0.07533,0.07332,-0.0356,0.9933,0.0257 -6.500,-0.2980,0.06946,0.06742,-0.0441,0.9890,0.0258 -6.250,-0.2670,0.06264,0.06054,-0.0539,0.9855,0.0258 -6.000,-0.2446,0.01912,0.01502,-0.0895,0.9747,0.0201 -5.750,-0.2095,0.01839,0.01426,-0.0915,0.9727,0.0217 -5.500,-0.1731,0.01713,0.01277,-0.0937,0.9711,0.0235 -5.250,-0.1468,0.01594,0.01132,-0.0935,0.9654,0.0249 -5.000,-0.1134,0.01448,0.00952,-0.0948,0.9622,0.0263 -4.750,-0.0791,0.01284,0.00766,-0.0965,0.9598,0.0295 -4.500,-0.0416,0.01207,0.00676,-0.0984,0.9580,0.0322 -4.250,-0.0126,0.01144,0.00600,-0.0984,0.9520,0.0340 -4.000,0.0222,0.01050,0.00489,-0.0998,0.9480,0.0367 -3.750,0.0592,0.00985,0.00420,-0.1015,0.9445,0.0401 -3.500,0.0896,0.00945,0.00373,-0.1018,0.9367,0.0428 -3.250,0.1263,0.00899,0.00321,-0.1034,0.9308,0.0466 -3.000,0.1573,0.00870,0.00293,-0.1038,0.9210,0.0528 -2.750,0.1901,0.00851,0.00275,-0.1045,0.9109,0.0658 -2.500,0.2211,0.00839,0.00256,-0.1049,0.8992,0.0795 -2.250,0.2492,0.00822,0.00235,-0.1046,0.8851,0.0883 -2.000,0.2758,0.00815,0.00220,-0.1041,0.8675,0.0937 -1.750,0.3019,0.00803,0.00205,-0.1034,0.8448,0.0991 -1.500,0.3275,0.00797,0.00191,-0.1026,0.8100,0.1037 -1.250,0.3518,0.00805,0.00174,-0.1015,0.7601,0.1090 -1.000,0.3757,0.00823,0.00173,-0.1003,0.7221,0.1156 -0.750,0.4003,0.00837,0.00170,-0.0994,0.6948,0.1213 -0.500,0.4253,0.00847,0.00172,-0.0987,0.6720,0.1296 -0.250,0.4508,0.00855,0.00173,-0.0980,0.6517,0.1405 0.000,0.4765,0.00863,0.00175,-0.0974,0.6334,0.1528 0.250,0.5024,0.00871,0.00177,-0.0969,0.6174,0.1640 0.500,0.5283,0.00875,0.00177,-0.0964,0.6027,0.1730 0.750,0.5542,0.00879,0.00177,-0.0958,0.5889,0.1799 1.000,0.5801,0.00884,0.00179,-0.0953,0.5750,0.1865 1.250,0.6060,0.00891,0.00182,-0.0948,0.5610,0.1926 1.500,0.6319,0.00896,0.00186,-0.0943,0.5483,0.2007 1.750,0.6579,0.00904,0.00191,-0.0938,0.5368,0.2081 2.000,0.6839,0.00909,0.00197,-0.0934,0.5250,0.2185 2.500,0.7359,0.00917,0.00215,-0.0925,0.5022,0.2662 2.750,0.7613,0.00911,0.00224,-0.0920,0.4919,0.3368 3.000,0.7988,0.00795,0.00243,-0.0944,0.4803,1.0000 3.250,0.8244,0.00808,0.00253,-0.0939,0.4683,1.0000 3.500,0.8500,0.00822,0.00263,-0.0933,0.4560,1.0000 3.750,0.8754,0.00838,0.00275,-0.0927,0.4438,1.0000 4.000,0.9007,0.00854,0.00287,-0.0921,0.4317,1.0000 4.250,0.9256,0.00872,0.00301,-0.0915,0.4141,1.0000 4.500,0.9497,0.00897,0.00315,-0.0907,0.3887,1.0000 4.750,0.9737,0.00923,0.00331,-0.0899,0.3645,1.0000 5.000,0.9978,0.00951,0.00350,-0.0892,0.3391,1.0000 5.250,1.0201,0.00994,0.00376,-0.0882,0.3005,1.0000 5.500,1.0417,0.01046,0.00407,-0.0872,0.2617,1.0000 5.750,1.0639,0.01095,0.00441,-0.0862,0.2309,1.0000 6.000,1.0854,0.01150,0.00479,-0.0852,0.1959,1.0000 6.250,1.1001,0.01275,0.00550,-0.0832,0.1081,1.0000 6.500,1.1173,0.01376,0.00620,-0.0815,0.0595,1.0000 6.750,1.1342,0.01479,0.00704,-0.0796,0.0231,1.0000 7.000,1.1557,0.01531,0.00766,-0.0785,0.0208,1.0000 7.250,1.1759,0.01597,0.00841,-0.0771,0.0187,1.0000 7.500,1.1940,0.01681,0.00939,-0.0753,0.0170,1.0000 7.750,1.2137,0.01745,0.01010,-0.0739,0.0162,1.0000 8.000,1.2315,0.01821,0.01095,-0.0722,0.0155,1.0000 8.250,1.2479,0.01906,0.01189,-0.0703,0.0148,1.0000 8.500,1.2624,0.02000,0.01291,-0.0682,0.0142,1.0000 8.750,1.2751,0.02103,0.01401,-0.0658,0.0138,1.0000 9.000,1.2857,0.02214,0.01522,-0.0631,0.0134,1.0000 9.250,1.2914,0.02340,0.01653,-0.0597,0.0129,1.0000 9.500,1.2895,0.02523,0.01842,-0.0553,0.0123,1.0000 9.750,1.2911,0.02727,0.02054,-0.0517,0.0119,1.0000 10.000,1.3019,0.02833,0.02169,-0.0494,0.0117,1.0000 10.250,1.3119,0.02962,0.02306,-0.0472,0.0116,1.0000 10.500,1.3218,0.03090,0.02445,-0.0450,0.0113,1.0000 10.750,1.3317,0.03251,0.02616,-0.0430,0.0111,1.0000 11.000,1.3421,0.03431,0.02808,-0.0411,0.0111,1.0000 11.250,1.3513,0.03607,0.02997,-0.0393,0.0108,1.0000 11.500,1.3618,0.03832,0.03237,-0.0376,0.0109,1.0000 11.750,1.3712,0.04089,0.03510,-0.0360,0.0110,1.0000 12.000,1.3783,0.04403,0.03844,-0.0344,0.0112,1.0000