Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe346-il-200000-n5 Airfoil,goe346-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,72.7841 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe346-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.3314,0.10673,0.10325,-0.0213,1.0000,0.0221 -9.500,-0.3313,0.10370,0.10024,-0.0228,1.0000,0.0221 -9.250,-0.3310,0.10052,0.09709,-0.0244,1.0000,0.0222 -9.000,-0.3292,0.09707,0.09366,-0.0256,1.0000,0.0222 -8.750,-0.3154,0.09093,0.08752,-0.0230,1.0000,0.0228 -8.500,-0.3102,0.08744,0.08405,-0.0229,1.0000,0.0232 -8.250,-0.3068,0.08419,0.08081,-0.0233,1.0000,0.0236 -8.000,-0.3042,0.08103,0.07767,-0.0237,1.0000,0.0241 -7.750,-0.3026,0.07797,0.07465,-0.0241,1.0000,0.0248 -7.500,-0.3028,0.07511,0.07184,-0.0242,1.0000,0.0256 -7.250,-0.3069,0.07275,0.06953,-0.0237,1.0000,0.0269 -7.000,-0.3163,0.07122,0.06809,-0.0231,1.0000,0.0282 -6.750,-0.3177,0.06916,0.06605,-0.0270,0.9983,0.0289 -6.500,-0.2950,0.06418,0.06099,-0.0358,0.9929,0.0292 -6.250,-0.2724,0.05909,0.05581,-0.0420,0.9881,0.0293 -6.000,-0.2485,0.05404,0.05066,-0.0475,0.9839,0.0294 -5.750,-0.2231,0.04936,0.04585,-0.0524,0.9792,0.0295 -5.500,-0.2104,0.04237,0.03887,-0.0547,0.9762,0.0303 -5.250,-0.1921,0.03854,0.03502,-0.0561,0.9713,0.0312 -5.000,-0.1679,0.03486,0.03127,-0.0590,0.9667,0.0323 -4.750,-0.1393,0.03119,0.02749,-0.0628,0.9630,0.0340 -4.500,-0.0986,0.02908,0.02503,-0.0677,0.9563,0.0397 -4.250,-0.0633,0.02597,0.02161,-0.0711,0.9513,0.0401 -4.000,-0.0352,0.02305,0.01846,-0.0728,0.9437,0.0402 -3.750,-0.0055,0.02020,0.01538,-0.0745,0.9374,0.0403 -3.500,0.0141,0.01582,0.01101,-0.0764,0.9314,0.0417 -3.250,0.0380,0.01399,0.00916,-0.0773,0.9245,0.0438 -3.000,0.0661,0.01233,0.00733,-0.0783,0.9187,0.0465 -2.750,0.0997,0.01193,0.00645,-0.0783,0.9107,0.0517 -2.500,0.1285,0.01063,0.00487,-0.0786,0.9045,0.0520 -2.000,0.1825,0.02222,0.01598,-0.0838,0.9121,0.0472 -1.750,0.2045,0.00640,0.00030,-0.0798,0.8832,0.0554 -1.250,0.2734,0.01859,0.01147,-0.0834,0.8909,0.0399 -1.000,0.3005,0.01724,0.00998,-0.0832,0.8817,0.0391 -0.750,0.3285,0.01627,0.00887,-0.0830,0.8739,0.0388 -0.500,0.3558,0.01548,0.00793,-0.0826,0.8639,0.0387 -0.250,0.3827,0.01479,0.00712,-0.0821,0.8512,0.0389 0.000,0.4091,0.01421,0.00641,-0.0813,0.8359,0.0392 0.250,0.4354,0.01374,0.00583,-0.0806,0.8193,0.0396 0.500,0.4613,0.01315,0.00516,-0.0799,0.8000,0.0416 0.750,0.4872,0.01268,0.00466,-0.0792,0.7786,0.0429 1.000,0.5133,0.01233,0.00423,-0.0785,0.7584,0.0429 1.250,0.5399,0.01203,0.00390,-0.0780,0.7415,0.0430 1.500,0.5665,0.01179,0.00365,-0.0776,0.7242,0.0433 1.750,0.5930,0.01161,0.00344,-0.0772,0.7051,0.0439 2.000,0.6195,0.01150,0.00328,-0.0767,0.6846,0.0449 2.250,0.6461,0.01143,0.00318,-0.0764,0.6624,0.0463 2.500,0.6725,0.01143,0.00311,-0.0759,0.6382,0.0484 2.750,0.6986,0.01150,0.00306,-0.0755,0.6096,0.0508 3.000,0.7237,0.01164,0.00304,-0.0748,0.5689,0.0578 3.250,0.7478,0.01193,0.00311,-0.0740,0.5191,0.0677 3.500,0.7686,0.01056,0.00331,-0.0726,0.4693,1.0000 3.750,0.7928,0.01101,0.00348,-0.0719,0.4188,1.0000 4.000,0.8167,0.01151,0.00371,-0.0713,0.3709,1.0000 4.250,0.8405,0.01204,0.00401,-0.0707,0.3275,1.0000 4.500,0.8645,0.01256,0.00433,-0.0702,0.2903,1.0000 4.750,0.8887,0.01305,0.00467,-0.0697,0.2587,1.0000 5.000,0.9129,0.01355,0.00503,-0.0693,0.2285,1.0000 5.250,0.9373,0.01400,0.00539,-0.0688,0.2068,1.0000 5.500,0.9622,0.01440,0.00576,-0.0684,0.1907,1.0000 5.750,0.9868,0.01482,0.00616,-0.0680,0.1751,1.0000 6.000,1.0113,0.01526,0.00660,-0.0675,0.1579,1.0000 6.250,1.0347,0.01583,0.00706,-0.0669,0.1255,1.0000 6.500,1.0552,0.01683,0.00773,-0.0661,0.0749,1.0000 6.750,1.0765,0.01774,0.00850,-0.0652,0.0514,1.0000 7.000,1.0987,0.01850,0.00928,-0.0644,0.0442,1.0000 7.250,1.1203,0.01931,0.01012,-0.0636,0.0397,1.0000 7.500,1.1415,0.02014,0.01106,-0.0627,0.0366,1.0000 7.750,1.1628,0.02091,0.01197,-0.0617,0.0338,1.0000 8.000,1.1825,0.02185,0.01304,-0.0607,0.0313,1.0000 8.250,1.1984,0.02323,0.01449,-0.0591,0.0286,1.0000 8.500,1.2172,0.02422,0.01561,-0.0579,0.0267,1.0000 8.750,1.2355,0.02525,0.01678,-0.0566,0.0249,1.0000 9.000,1.2528,0.02636,0.01801,-0.0552,0.0230,1.0000 9.250,1.2689,0.02752,0.01923,-0.0539,0.0213,1.0000 9.500,1.2813,0.02921,0.02100,-0.0520,0.0198,1.0000 9.750,1.2976,0.03040,0.02238,-0.0505,0.0188,1.0000 10.000,1.3119,0.03185,0.02401,-0.0488,0.0177,1.0000 10.250,1.3252,0.03330,0.02562,-0.0471,0.0167,1.0000 10.500,1.3375,0.03458,0.02703,-0.0454,0.0158,1.0000 10.750,1.3467,0.03580,0.02834,-0.0433,0.0150,1.0000 11.000,1.3516,0.03756,0.03022,-0.0409,0.0143,1.0000 11.250,1.3570,0.03951,0.03239,-0.0385,0.0138,1.0000 11.500,1.3604,0.04171,0.03485,-0.0362,0.0134,1.0000 11.750,1.3614,0.04415,0.03754,-0.0339,0.0130,1.0000 12.000,1.3598,0.04683,0.04048,-0.0318,0.0126,1.0000 12.250,1.3559,0.04977,0.04368,-0.0301,0.0123,1.0000 12.500,1.3498,0.05302,0.04718,-0.0287,0.0121,1.0000 12.750,1.3418,0.05658,0.05098,-0.0278,0.0119,1.0000 13.000,1.3323,0.06051,0.05514,-0.0276,0.0117,1.0000 13.250,1.3215,0.06484,0.05970,-0.0281,0.0115,1.0000 13.500,1.3086,0.06979,0.06487,-0.0294,0.0114,1.0000 13.750,1.2949,0.07520,0.07048,-0.0314,0.0113,1.0000 14.000,1.2776,0.08173,0.07723,-0.0344,0.0113,1.0000 14.250,1.2577,0.08927,0.08499,-0.0384,0.0113,1.0000 14.500,1.2342,0.09818,0.09413,-0.0436,0.0114,1.0000 14.750,1.2067,0.10893,0.10511,-0.0503,0.0116,1.0000 15.000,1.1740,0.12201,0.11840,-0.0585,0.0119,1.0000 15.250,1.1358,0.13796,0.13453,-0.0684,0.0124,1.0000