Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe506-il-50000 Airfoil,goe506-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,10.1975 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe506-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.750,-0.4343,0.11874,0.11333,-0.0097,1.0000,0.2779 -7.500,-0.4363,0.11543,0.11005,-0.0085,1.0000,0.2786 -7.250,-0.5680,0.09776,0.09249,-0.0228,1.0000,0.1655 -7.000,-0.5486,0.09534,0.09011,-0.0191,1.0000,0.1613 -6.750,-0.6209,0.07845,0.07286,-0.0280,1.0000,0.1368 -6.500,-0.6220,0.07416,0.06849,-0.0270,1.0000,0.1353 -6.250,-0.6251,0.06894,0.06308,-0.0266,1.0000,0.1324 -6.000,-0.6464,0.05725,0.05003,-0.0280,1.0000,0.1238 -5.750,-0.6371,0.05351,0.04595,-0.0266,1.0000,0.1233 -5.500,-0.6260,0.05004,0.04204,-0.0252,1.0000,0.1229 -5.250,-0.6136,0.04698,0.03837,-0.0237,1.0000,0.1237 -5.000,-0.5980,0.04501,0.03635,-0.0223,1.0000,0.1266 -4.750,-0.5816,0.04337,0.03453,-0.0209,1.0000,0.1297 -4.500,-0.5641,0.04154,0.03236,-0.0195,1.0000,0.1324 -4.250,-0.5454,0.03988,0.03029,-0.0181,1.0000,0.1360 -4.000,-0.5273,0.03887,0.02925,-0.0168,1.0000,0.1414 -3.750,-0.5089,0.03807,0.02832,-0.0155,1.0000,0.1488 -3.500,-0.4904,0.03736,0.02763,-0.0141,1.0000,0.1568 -3.250,-0.4714,0.03676,0.02698,-0.0128,1.0000,0.1678 -3.000,-0.4538,0.03648,0.02680,-0.0116,1.0000,0.1862 -2.750,-0.4355,0.03611,0.02658,-0.0103,1.0000,0.2186 -2.500,-0.4216,0.03573,0.02664,-0.0081,1.0000,0.3002 -2.250,-0.4135,0.03619,0.02725,-0.0051,1.0000,0.3655 -2.000,-0.4033,0.03671,0.02783,-0.0027,1.0000,0.4049 -1.750,-0.3926,0.03719,0.02836,-0.0007,1.0000,0.4358 -1.500,-0.3816,0.03769,0.02883,0.0010,1.0000,0.4636 -1.250,-0.2720,0.04181,0.03304,-0.0127,0.9366,0.5440 -1.000,-0.2157,0.04262,0.03376,-0.0178,0.9078,0.5788 -0.750,-0.1632,0.04295,0.03400,-0.0226,0.8834,0.6061 -0.500,-0.1116,0.04312,0.03424,-0.0268,0.8621,0.6499 -0.250,0.0553,0.04310,0.03520,-0.0531,0.8381,1.0000 0.000,0.1040,0.04335,0.03477,-0.0576,0.8188,1.0000 0.250,0.1369,0.04354,0.03461,-0.0588,0.7973,1.0000 0.500,0.1724,0.04366,0.03442,-0.0601,0.7770,1.0000 0.750,0.2114,0.04367,0.03417,-0.0617,0.7592,1.0000 1.000,0.2497,0.04360,0.03386,-0.0630,0.7423,1.0000 1.250,0.2848,0.04351,0.03357,-0.0638,0.7260,1.0000 1.500,0.3177,0.04339,0.03328,-0.0642,0.7101,1.0000 1.750,0.3453,0.04348,0.03321,-0.0639,0.6947,1.0000 2.000,0.3687,0.04378,0.03337,-0.0632,0.6797,1.0000 2.250,0.3861,0.04447,0.03394,-0.0621,0.6655,1.0000 2.500,0.4012,0.04542,0.03477,-0.0608,0.6527,1.0000 2.750,0.4470,0.04472,0.03394,-0.0624,0.6466,1.0000 3.000,0.4488,0.04651,0.03565,-0.0601,0.6334,1.0000 3.250,0.4520,0.04839,0.03745,-0.0580,0.6220,1.0000 3.500,0.4904,0.04809,0.03706,-0.0588,0.6165,1.0000 3.750,0.4730,0.05170,0.04061,-0.0557,0.6056,1.0000 4.000,0.5060,0.05196,0.04080,-0.0563,0.6011,1.0000 4.250,0.4754,0.05688,0.04571,-0.0529,0.5933,1.0000 4.500,0.4852,0.05894,0.04772,-0.0522,0.5883,1.0000 4.750,0.5247,0.05890,0.04762,-0.0531,0.5845,1.0000 5.000,0.4811,0.06493,0.05365,-0.0498,0.5801,1.0000 5.250,0.4715,0.06864,0.05735,-0.0486,0.5789,1.0000 5.500,0.4659,0.07214,0.06085,-0.0477,0.5791,1.0000 5.750,0.4630,0.07528,0.06398,-0.0469,0.5782,1.0000 6.000,0.4631,0.07815,0.06684,-0.0462,0.5767,1.0000 6.250,0.4973,0.07872,0.06738,-0.0466,0.5674,1.0000 6.500,0.4906,0.08204,0.07071,-0.0457,0.5663,1.0000 6.750,0.4875,0.08469,0.07336,-0.0446,0.5610,1.0000 7.000,0.5104,0.08547,0.07412,-0.0440,0.5472,1.0000 7.250,0.5395,0.08599,0.07463,-0.0437,0.5344,1.0000 7.500,0.5376,0.08876,0.07743,-0.0428,0.5280,1.0000 7.750,0.5649,0.08990,0.07858,-0.0428,0.5193,1.0000 8.000,0.5525,0.09378,0.08250,-0.0421,0.5163,1.0000 8.250,0.5543,0.09675,0.08551,-0.0418,0.5111,1.0000 8.500,0.5678,0.09875,0.08754,-0.0413,0.5000,1.0000 8.750,0.5965,0.09969,0.08851,-0.0410,0.4866,1.0000 9.000,0.5798,0.10393,0.09280,-0.0405,0.4796,1.0000 9.250,0.5969,0.10599,0.09488,-0.0402,0.4683,1.0000 9.500,0.5871,0.11087,0.09982,-0.0407,0.4683,1.0000 9.750,0.5248,0.12469,0.11380,-0.0463,0.5536,1.0000