Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-fx74080-il-1000000-n5 Airfoil,fx74080-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,164.503 Max Cl/Cd alpha,2.5 Url,http://airfoiltools.com/polar/csv?polar=xf-fx74080-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.1667,0.08302,0.08050,-0.0892,0.8143,0.0032 -8.250,-0.1560,0.07975,0.07723,-0.0920,0.8123,0.0032 -8.000,-0.1500,0.07549,0.07297,-0.0949,0.8102,0.0029 -7.750,-0.1413,0.07148,0.06896,-0.0986,0.8081,0.0027 -7.500,-0.1313,0.06785,0.06533,-0.1024,0.8063,0.0026 -7.250,-0.1207,0.06431,0.06180,-0.1069,0.8044,0.0026 -7.000,-0.1070,0.05974,0.05723,-0.1133,0.8022,0.0025 -6.750,-0.0917,0.05507,0.05253,-0.1192,0.8000,0.0024 -6.500,-0.0746,0.05112,0.04853,-0.1238,0.7981,0.0023 -6.250,-0.0571,0.04620,0.04352,-0.1284,0.7959,0.0023 -6.000,-0.0386,0.04147,0.03866,-0.1319,0.7935,0.0023 -5.750,-0.0200,0.03670,0.03376,-0.1341,0.7908,0.0023 -5.500,-0.0010,0.03121,0.02804,-0.1354,0.7882,0.0026 -5.000,0.0398,0.02253,0.01881,-0.1353,0.7840,0.0038 -4.750,0.0636,0.02194,0.01812,-0.1356,0.7824,0.0043 -4.250,0.1116,0.01878,0.01457,-0.1352,0.7793,0.0059 -4.000,0.1354,0.01637,0.01189,-0.1345,0.7776,0.0060 -3.750,0.1593,0.01384,0.00900,-0.1337,0.7759,0.0057 -3.500,0.1839,0.01160,0.00642,-0.1328,0.7742,0.0053 -3.250,0.2088,0.01002,0.00459,-0.1321,0.7726,0.0051 -3.000,0.2336,0.00897,0.00337,-0.1314,0.7708,0.0050 -2.750,0.2588,0.00832,0.00258,-0.1309,0.7691,0.0051 -2.250,0.3110,0.00759,0.00168,-0.1304,0.7659,0.0074 -2.000,0.3379,0.00750,0.00159,-0.1304,0.7640,0.0092 -1.750,0.3643,0.00727,0.00129,-0.1302,0.7619,0.0114 -1.500,0.3911,0.00712,0.00109,-0.1300,0.7599,0.0138 -1.250,0.4179,0.00701,0.00100,-0.1299,0.7578,0.0229 -1.000,0.4445,0.00690,0.00093,-0.1299,0.7559,0.0454 -0.750,0.4711,0.00678,0.00089,-0.1298,0.7540,0.0812 -0.500,0.4930,0.00606,0.00091,-0.1292,0.7519,0.3611 -0.250,0.5172,0.00574,0.00091,-0.1288,0.7495,0.4885 0.000,0.5386,0.00529,0.00093,-0.1277,0.7469,0.6673 0.250,0.5568,0.00497,0.00106,-0.1255,0.7443,0.8434 0.500,0.5815,0.00494,0.00108,-0.1249,0.7419,0.8728 0.750,0.6064,0.00491,0.00111,-0.1242,0.7392,0.8960 1.000,0.6316,0.00487,0.00115,-0.1237,0.7360,0.9159 1.250,0.6581,0.00486,0.00116,-0.1235,0.7326,0.9282 1.500,0.6855,0.00486,0.00117,-0.1236,0.7294,0.9358 1.750,0.7137,0.00487,0.00121,-0.1238,0.7261,0.9441 2.000,0.7444,0.00487,0.00125,-0.1247,0.7218,0.9535 2.250,0.7773,0.00488,0.00131,-0.1261,0.7140,0.9634 2.500,0.8110,0.00493,0.00132,-0.1276,0.6903,0.9740 2.750,0.8427,0.00518,0.00138,-0.1288,0.6420,0.9932 3.250,0.8646,0.00649,0.00195,-0.1221,0.4786,1.0000 3.500,0.8610,0.00811,0.00268,-0.1162,0.2905,1.0000 3.750,0.8539,0.01009,0.00359,-0.1099,0.0522,1.0000 4.000,0.8727,0.01059,0.00393,-0.1083,0.0157,1.0000 4.250,0.8948,0.01087,0.00421,-0.1074,0.0087,1.0000 4.500,0.9157,0.01124,0.00461,-0.1062,0.0037,1.0000 4.750,0.9371,0.01158,0.00498,-0.1052,0.0028,1.0000 5.000,0.9573,0.01199,0.00546,-0.1038,0.0025,1.0000 5.250,0.9746,0.01260,0.00617,-0.1018,0.0022,1.0000 5.500,0.9909,0.01324,0.00691,-0.0997,0.0022,1.0000 5.750,1.0028,0.01407,0.00785,-0.0967,0.0022,1.0000 6.000,1.0138,0.01502,0.00892,-0.0936,0.0022,1.0000 6.250,1.0250,0.01616,0.01016,-0.0906,0.0022,1.0000 6.500,1.0378,0.01763,0.01174,-0.0879,0.0022,1.0000 6.750,1.0597,0.01945,0.01368,-0.0869,0.0023,1.0000 7.000,1.0975,0.02227,0.01669,-0.0886,0.0025,1.0000 7.250,1.1305,0.02546,0.02018,-0.0892,0.0027,1.0000 7.500,1.1549,0.02866,0.02367,-0.0883,0.0028,1.0000 7.750,1.1746,0.03136,0.02660,-0.0866,0.0027,1.0000 8.000,1.1925,0.03287,0.02827,-0.0852,0.0022,1.0000 8.250,1.2060,0.03604,0.03171,-0.0826,0.0022,1.0000 8.500,1.2164,0.03922,0.03516,-0.0796,0.0021,1.0000 8.750,1.2267,0.04101,0.03711,-0.0774,0.0019,1.0000 9.000,1.2296,0.04497,0.04135,-0.0735,0.0019,1.0000 9.250,1.2357,0.04639,0.04290,-0.0710,0.0017,1.0000 9.500,1.2333,0.05006,0.04681,-0.0669,0.0017,1.0000 9.750,1.2308,0.05235,0.04927,-0.0633,0.0016,1.0000 10.000,1.2255,0.05402,0.05106,-0.0595,0.0015,1.0000 10.250,1.2158,0.05616,0.05334,-0.0554,0.0014,1.0000 10.500,1.2014,0.05900,0.05634,-0.0513,0.0014,1.0000 10.750,1.1852,0.06191,0.05939,-0.0478,0.0014,1.0000 11.000,1.1678,0.06603,0.06368,-0.0446,0.0014,1.0000 11.250,1.1489,0.06915,0.06693,-0.0426,0.0013,1.0000 11.500,1.1300,0.07381,0.07173,-0.0407,0.0014,1.0000 11.750,1.1084,0.07815,0.07620,-0.0400,0.0013,1.0000 12.000,1.0878,0.08405,0.08223,-0.0397,0.0014,1.0000 12.250,1.0679,0.08902,0.08730,-0.0408,0.0013,1.0000 12.500,1.0428,0.09580,0.09419,-0.0434,0.0013,1.0000 12.750,1.0234,0.10379,0.10229,-0.0467,0.0014,1.0000