Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe780-il-200000-n5 Airfoil,goe780-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,34.3157 Max Cl/Cd alpha,2.25 Url,http://airfoiltools.com/polar/csv?polar=xf-goe780-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.5007,0.07831,0.07509,-0.0594,1.0000,0.0095 -9.500,-0.5126,0.07407,0.07083,-0.0606,1.0000,0.0102 -9.250,-0.5242,0.06904,0.06573,-0.0632,0.9814,0.0081 -9.000,-0.5249,0.06391,0.06042,-0.0660,0.9605,0.0096 -8.750,-0.5285,0.05921,0.05551,-0.0668,0.9415,0.0089 -8.500,-0.5309,0.05501,0.05108,-0.0659,0.9238,0.0084 -8.250,-0.5289,0.05144,0.04724,-0.0642,0.9091,0.0092 -8.000,-0.5272,0.04798,0.04350,-0.0618,0.8970,0.0092 -7.750,-0.5250,0.04456,0.03976,-0.0587,0.8868,0.0094 -7.500,-0.5231,0.04102,0.03588,-0.0550,0.8784,0.0094 -7.250,-0.5174,0.03803,0.03255,-0.0519,0.8719,0.0090 -7.000,-0.5127,0.03444,0.02853,-0.0477,0.8657,0.0090 -6.750,-0.5022,0.03152,0.02520,-0.0445,0.8607,0.0088 -6.500,-0.4877,0.02851,0.02172,-0.0418,0.8565,0.0087 -6.250,-0.4684,0.02566,0.01836,-0.0398,0.8521,0.0088 -6.000,-0.4426,0.02317,0.01543,-0.0392,0.8485,0.0090 -5.750,-0.4137,0.02148,0.01340,-0.0393,0.8456,0.0104 -5.500,-0.3823,0.01972,0.01138,-0.0401,0.8430,0.0108 -5.250,-0.3541,0.01763,0.00910,-0.0404,0.8401,0.0128 -5.000,-0.3338,0.01663,0.00799,-0.0391,0.8367,0.0145 -4.750,-0.3138,0.01598,0.00719,-0.0377,0.8335,0.0177 -4.250,-0.2749,0.01489,0.00595,-0.0346,0.8270,0.0374 -4.000,-0.2553,0.01449,0.00542,-0.0333,0.8237,0.0510 -3.750,-0.2381,0.01390,0.00502,-0.0315,0.8208,0.0837 -3.500,-0.2194,0.01342,0.00462,-0.0300,0.8182,0.1392 -3.250,-0.2161,0.01227,0.00428,-0.0257,0.8150,0.3387 -3.000,-0.2208,0.01125,0.00405,-0.0193,0.8108,0.5209 -2.750,-0.1275,0.01091,0.00467,-0.0328,0.8115,0.7904 -2.500,-0.0962,0.01129,0.00497,-0.0331,0.8091,0.8268 -2.250,-0.0733,0.01162,0.00521,-0.0318,0.8067,0.8518 -2.000,-0.0452,0.01198,0.00547,-0.0315,0.8045,0.8674 -1.750,-0.0066,0.01258,0.00595,-0.0333,0.8029,0.8805 -1.500,0.0227,0.01284,0.00616,-0.0336,0.8002,0.8888 -1.000,0.0730,0.01299,0.00621,-0.0331,0.7950,0.9003 -0.750,0.1099,0.01313,0.00631,-0.0353,0.7929,0.9022 -0.500,0.1426,0.01320,0.00634,-0.0367,0.7908,0.9043 -0.250,0.1765,0.01336,0.00647,-0.0382,0.7891,0.9089 0.000,0.1948,0.01337,0.00651,-0.0366,0.7863,0.9148 0.250,0.2311,0.01351,0.00668,-0.0387,0.7838,0.9171 0.500,0.2642,0.01361,0.00684,-0.0402,0.7813,0.9202 0.750,0.2914,0.01363,0.00689,-0.0404,0.7775,0.9242 1.000,0.3128,0.01359,0.00688,-0.0392,0.7709,0.9286 1.250,0.3440,0.01355,0.00692,-0.0401,0.7641,0.9303 1.500,0.3753,0.01354,0.00698,-0.0411,0.7608,0.9323 1.750,0.4021,0.01352,0.00709,-0.0412,0.7527,0.9353 2.000,0.4181,0.01307,0.00657,-0.0380,0.7182,0.9403 2.250,0.4413,0.01286,0.00638,-0.0368,0.6744,0.9431 2.500,0.4311,0.01472,0.00643,-0.0292,0.2863,0.9484 2.750,0.4260,0.01623,0.00715,-0.0234,0.0732,0.9552 3.000,0.4494,0.01690,0.00765,-0.0230,0.0214,0.9573 3.250,0.4720,0.01748,0.00837,-0.0223,0.0166,0.9598 3.500,0.4916,0.01805,0.00913,-0.0210,0.0154,0.9630 3.750,0.5034,0.01867,0.00986,-0.0180,0.0145,0.9675 4.000,0.5257,0.01943,0.01072,-0.0175,0.0126,0.9695 4.250,0.5461,0.02039,0.01175,-0.0165,0.0111,0.9724 4.500,0.5661,0.02150,0.01293,-0.0152,0.0108,0.9762 4.750,0.5906,0.02287,0.01439,-0.0147,0.0104,0.9786 5.000,0.6214,0.02434,0.01603,-0.0153,0.0103,0.9795 5.250,0.6524,0.02752,0.01944,-0.0157,0.0086,0.9792 5.500,0.6800,0.02886,0.02108,-0.0155,0.0082,0.9803 5.750,0.7062,0.03108,0.02366,-0.0148,0.0080,0.9814 6.000,0.7277,0.03398,0.02689,-0.0137,0.0083,0.9829 6.500,0.7752,0.04061,0.03423,-0.0094,0.0185,0.9856 6.750,0.7908,0.04361,0.03762,-0.0068,0.0191,0.9878 7.000,0.8048,0.04671,0.04096,-0.0056,0.0184,0.9898 7.250,0.8144,0.05014,0.04458,-0.0040,0.0179,0.9921 7.500,0.8168,0.05458,0.04927,-0.0017,0.0174,0.9946 7.750,0.8134,0.06061,0.05557,0.0006,0.0170,0.9972 8.000,0.8191,0.06426,0.05954,0.0023,0.0169,0.9997 8.250,0.8124,0.06684,0.06229,0.0065,0.0169,1.0000 8.500,0.8013,0.06923,0.06483,0.0115,0.0169,1.0000 8.750,0.7888,0.07148,0.06720,0.0164,0.0169,1.0000 9.000,0.7725,0.07372,0.06955,0.0217,0.0169,1.0000 9.250,0.7521,0.07518,0.07108,0.0277,0.0169,1.0000 9.500,0.7319,0.07687,0.07283,0.0329,0.0169,1.0000 9.750,0.7105,0.07890,0.07493,0.0375,0.0169,1.0000 10.000,0.6913,0.08140,0.07751,0.0407,0.0169,1.0000 10.250,0.6732,0.08425,0.08042,0.0429,0.0169,1.0000 10.500,0.6553,0.08765,0.08388,0.0443,0.0169,1.0000