Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe746-il-50000 Airfoil,goe746-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,7.89983 Max Cl/Cd alpha,2.25 Url,http://airfoiltools.com/polar/csv?polar=xf-goe746-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.250,-0.4456,0.14531,0.13984,0.0262,1.0000,0.1011 -11.000,-0.4456,0.14426,0.13889,0.0222,1.0000,0.1036 -10.750,-0.4497,0.14415,0.13890,0.0175,1.0000,0.1044 -10.500,-0.4175,0.13410,0.12887,0.0183,1.0000,0.1090 -10.250,-0.4056,0.13033,0.12516,0.0156,1.0000,0.1140 -10.000,-0.4023,0.12856,0.12350,0.0109,1.0000,0.1181 -9.750,-0.4071,0.12852,0.12359,0.0045,1.0000,0.1193 -9.500,-0.3706,0.11911,0.11416,0.0052,1.0000,0.1281 -9.250,-0.3678,0.11753,0.11268,-0.0007,1.0000,0.1335 -9.000,-0.3494,0.11214,0.10735,-0.0039,1.0000,0.1380 -8.750,-0.3329,0.10830,0.10356,-0.0077,1.0000,0.1455 -8.500,-0.3363,0.10775,0.10313,-0.0154,1.0000,0.1493 -8.250,-0.3082,0.10126,0.09666,-0.0161,0.9917,0.1563 -8.000,-0.3013,0.09961,0.09498,-0.0263,0.9485,0.1643 -7.750,-0.2696,0.09354,0.08882,-0.0274,0.9321,0.1741 -7.500,-0.2781,0.09367,0.08891,-0.0349,0.9142,0.1800 -7.250,-0.2567,0.08868,0.08387,-0.0330,0.9015,0.1928 -7.000,-0.2466,0.08562,0.08079,-0.0337,0.8898,0.2025 -6.750,-0.2491,0.08456,0.07971,-0.0377,0.8791,0.2125 -6.500,-0.2443,0.08321,0.07831,-0.0399,0.8689,0.2265 -6.000,-0.2259,0.07805,0.07310,-0.0405,0.8519,0.2574 -5.750,-0.2129,0.07458,0.06968,-0.0401,0.8439,0.2745 -5.500,-0.2006,0.07161,0.06671,-0.0380,0.8368,0.2948 -5.250,-0.1941,0.06968,0.06478,-0.0389,0.8293,0.3210 -5.000,-0.1848,0.06708,0.06219,-0.0361,0.8230,0.3540 -4.750,0.1484,0.04581,0.04039,-0.0386,0.8093,1.0000 -4.500,0.1650,0.04432,0.03890,-0.0412,0.8030,1.0000 -4.250,0.1800,0.04302,0.03760,-0.0433,0.7966,1.0000 -4.000,-0.0378,0.05337,0.04849,-0.0115,0.7977,0.7604 -3.750,0.0714,0.04824,0.04312,-0.0217,0.7897,0.8775 -3.500,0.0478,0.04816,0.04315,-0.0191,0.7848,0.8410 -3.250,0.0175,0.04805,0.04313,-0.0158,0.7805,0.8084 -3.000,-0.0131,0.04761,0.04283,-0.0134,0.7763,0.7786 -2.750,-0.0594,0.04778,0.04316,-0.0083,0.7723,0.7615 -2.500,-0.0881,0.04699,0.04246,-0.0069,0.7685,0.7369 -2.250,-0.1127,0.04608,0.04152,-0.0080,0.7652,0.7059 -2.000,0.0283,0.04866,0.04135,-0.0552,0.7566,0.2688 -1.750,0.0632,0.04746,0.03931,-0.0566,0.7523,0.2087 -1.500,0.0905,0.04636,0.03777,-0.0566,0.7482,0.1872 -1.250,0.1033,0.04627,0.03732,-0.0557,0.7443,0.1761 -1.000,0.1200,0.04600,0.03674,-0.0550,0.7406,0.1697 -0.750,0.1447,0.04586,0.03618,-0.0547,0.7367,0.1664 -0.500,0.1683,0.04592,0.03591,-0.0544,0.7329,0.1642 -0.250,0.1775,0.04624,0.03612,-0.0534,0.7303,0.1626 0.000,0.1904,0.04664,0.03635,-0.0527,0.7282,0.1610 0.250,0.2131,0.04709,0.03657,-0.0532,0.7253,0.1600 0.500,0.2648,0.04728,0.03644,-0.0566,0.7181,0.1616 0.750,0.2743,0.04825,0.03730,-0.0558,0.7170,0.1630 1.000,0.2831,0.04920,0.03818,-0.0547,0.7167,0.1668 1.250,0.2927,0.05021,0.03920,-0.0538,0.7167,0.1740 1.500,0.3052,0.05133,0.04030,-0.0532,0.7178,0.1830 1.750,0.2890,0.05356,0.04253,-0.0519,0.7487,0.1832 2.000,0.4020,0.05184,0.04298,-0.0650,0.7069,1.0000 2.250,0.4243,0.05371,0.04430,-0.0647,0.7042,1.0000 3.250,0.3431,0.06069,0.05124,-0.0552,0.8231,1.0000 3.500,0.3561,0.06211,0.05238,-0.0539,0.8029,1.0000 3.750,0.3774,0.06407,0.05409,-0.0539,0.7835,1.0000 4.000,0.3996,0.06627,0.05611,-0.0541,0.7668,1.0000 5.000,0.4699,0.07463,0.06403,-0.0531,0.7060,1.0000 5.250,0.4819,0.07647,0.06580,-0.0523,0.6917,1.0000 5.500,0.4917,0.07831,0.06759,-0.0514,0.6784,1.0000 5.750,0.5025,0.08032,0.06956,-0.0506,0.6659,1.0000 6.000,0.5178,0.08271,0.07190,-0.0505,0.6548,1.0000 6.250,0.5504,0.08626,0.07541,-0.0518,0.6434,1.0000 6.500,0.5481,0.08719,0.07633,-0.0499,0.6308,1.0000 6.750,0.5516,0.08900,0.07814,-0.0489,0.6203,1.0000 7.000,0.5749,0.09223,0.08136,-0.0495,0.6119,1.0000 7.250,0.5846,0.09405,0.08318,-0.0488,0.5999,1.0000 7.500,0.5847,0.09578,0.08490,-0.0478,0.5902,1.0000 7.750,0.6133,0.09945,0.08859,-0.0488,0.5834,1.0000 8.000,0.6055,0.10050,0.08964,-0.0473,0.5734,1.0000 8.250,0.6342,0.10452,0.09373,-0.0483,0.5673,1.0000 8.500,0.6281,0.10539,0.09460,-0.0469,0.5565,1.0000 8.750,0.6494,0.10915,0.09841,-0.0476,0.5518,1.0000 9.000,0.6439,0.11024,0.09952,-0.0466,0.5425,1.0000 9.250,0.6741,0.11470,0.10409,-0.0477,0.5376,1.0000 9.500,0.6601,0.11523,0.10462,-0.0464,0.5285,1.0000 9.750,0.6891,0.11952,0.10900,-0.0473,0.5227,1.0000 10.000,0.6765,0.12039,0.10988,-0.0464,0.5152,1.0000 10.250,0.6953,0.12373,0.11331,-0.0468,0.5090,1.0000