Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca001034a08cli02-il-50000 Airfoil,naca001034a08cli02-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,26.4877 Max Cl/Cd alpha,5.5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca001034a08cli02-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.500,-0.4998,0.12648,0.11950,-0.0164,1.0000,0.2251 -10.250,-0.5164,0.12532,0.11846,-0.0181,1.0000,0.2346 -10.000,-0.5073,0.12126,0.11442,-0.0173,1.0000,0.2480 -9.750,-0.5008,0.11748,0.11058,-0.0167,1.0000,0.2614 -9.500,-0.4976,0.11409,0.10724,-0.0163,1.0000,0.2752 -9.250,-0.5000,0.11126,0.10448,-0.0159,1.0000,0.2897 -9.000,-0.4805,0.10660,0.09981,-0.0140,1.0000,0.3098 -8.750,-0.4830,0.10411,0.09739,-0.0130,1.0000,0.3299 -8.500,-0.3775,0.09138,0.08526,-0.0177,1.0000,0.3600 -8.250,-0.3772,0.08796,0.08190,-0.0163,1.0000,0.3739 -8.000,-0.3616,0.08334,0.07727,-0.0155,1.0000,0.3828 -7.750,-0.3640,0.07985,0.07384,-0.0142,1.0000,0.3926 -6.000,-0.5979,0.05674,0.04990,-0.0260,1.0000,0.1754 -5.750,-0.5871,0.05103,0.04332,-0.0259,1.0000,0.1356 -5.500,-0.5727,0.04691,0.03865,-0.0243,1.0000,0.1210 -5.250,-0.5566,0.04371,0.03458,-0.0221,1.0000,0.1100 -5.000,-0.5379,0.04017,0.03079,-0.0207,1.0000,0.1067 -4.750,-0.5166,0.03705,0.02709,-0.0190,1.0000,0.1009 -4.500,-0.4925,0.03490,0.02417,-0.0171,1.0000,0.0964 -4.250,-0.4671,0.03229,0.02123,-0.0160,1.0000,0.0954 -4.000,-0.4402,0.03017,0.01874,-0.0147,1.0000,0.0961 -3.750,-0.1416,0.02356,0.01482,-0.0434,1.0000,1.0000 -3.500,-0.1426,0.02285,0.01391,-0.0407,1.0000,1.0000 -3.250,-0.1442,0.02224,0.01312,-0.0377,1.0000,1.0000 -3.000,-0.1459,0.02172,0.01242,-0.0343,1.0000,1.0000 -2.750,-0.1475,0.02127,0.01180,-0.0307,1.0000,1.0000 -2.500,-0.1485,0.02088,0.01125,-0.0270,1.0000,1.0000 -2.250,-0.1484,0.02056,0.01076,-0.0233,1.0000,1.0000 -2.000,-0.1463,0.02031,0.01027,-0.0198,1.0000,1.0000 -1.750,-0.1417,0.02013,0.00989,-0.0166,1.0000,1.0000 -1.500,-0.1343,0.02003,0.00958,-0.0138,1.0000,1.0000 -1.250,-0.1248,0.01999,0.00933,-0.0114,1.0000,1.0000 -1.000,-0.1131,0.02001,0.00916,-0.0093,1.0000,1.0000 -0.750,-0.0995,0.02008,0.00904,-0.0075,1.0000,1.0000 -0.500,-0.0844,0.02021,0.00896,-0.0060,1.0000,1.0000 -0.250,-0.0682,0.02038,0.00898,-0.0047,1.0000,1.0000 0.000,-0.0512,0.02059,0.00905,-0.0036,1.0000,1.0000 0.250,-0.0336,0.02084,0.00919,-0.0026,1.0000,1.0000 0.500,-0.0155,0.02113,0.00938,-0.0018,1.0000,1.0000 0.750,0.0028,0.02146,0.00960,-0.0010,1.0000,1.0000 1.000,0.0213,0.02182,0.00991,-0.0004,1.0000,1.0000 1.250,0.0398,0.02223,0.01027,0.0002,1.0000,1.0000 1.500,0.0584,0.02268,0.01070,0.0007,1.0000,1.0000 1.750,0.0770,0.02318,0.01119,0.0012,1.0000,1.0000 2.000,0.0954,0.02372,0.01174,0.0015,1.0000,1.0000 2.250,0.1137,0.02431,0.01235,0.0018,1.0000,1.0000 2.500,0.1317,0.02496,0.01304,0.0021,1.0000,1.0000 2.750,0.1495,0.02567,0.01380,0.0023,1.0000,1.0000 3.000,0.1669,0.02644,0.01467,0.0024,1.0000,1.0000 3.250,0.1840,0.02728,0.01559,0.0024,1.0000,1.0000 3.500,0.2006,0.02819,0.01661,0.0024,1.0000,1.0000 3.750,0.2372,0.02957,0.01816,-0.0016,0.9911,1.0000 4.000,0.2940,0.03126,0.02019,-0.0094,0.9702,1.0000 4.250,0.3444,0.03268,0.02192,-0.0155,0.9478,1.0000 4.500,0.3958,0.03395,0.02357,-0.0213,0.9246,1.0000 4.750,0.4483,0.03499,0.02511,-0.0268,0.9002,1.0000 5.000,0.4983,0.03570,0.02632,-0.0312,0.8740,1.0000 5.250,0.5416,0.03612,0.02729,-0.0339,0.8458,1.0000 5.500,0.6659,0.02514,0.01410,-0.0192,0.1829,1.0000 5.750,0.6775,0.02770,0.01612,-0.0163,0.1333,1.0000 6.000,0.7096,0.03013,0.01849,-0.0159,0.1098,1.0000 6.250,0.7590,0.03324,0.02165,-0.0178,0.0967,1.0000 6.500,0.7937,0.03638,0.02495,-0.0181,0.0875,1.0000 6.750,0.8241,0.03966,0.02870,-0.0173,0.0868,1.0000 7.000,0.8489,0.04328,0.03290,-0.0159,0.0879,1.0000 7.250,0.8707,0.04747,0.03741,-0.0145,0.0899,1.0000 7.500,0.8836,0.05045,0.04112,-0.0114,0.0928,1.0000 7.750,0.8891,0.05424,0.04565,-0.0079,0.0976,1.0000 8.000,0.8958,0.05850,0.05030,-0.0054,0.1009,1.0000 8.250,0.8999,0.06262,0.05491,-0.0027,0.1072,1.0000 8.500,0.8982,0.06779,0.06045,-0.0004,0.1156,1.0000 8.750,0.8983,0.07350,0.06658,0.0012,0.1322,1.0000 9.000,0.7763,0.06464,0.05839,0.0132,0.1262,1.0000 9.250,0.7577,0.06945,0.06332,0.0151,0.1338,1.0000 9.500,0.7160,0.07424,0.06820,0.0160,0.1359,1.0000 9.750,0.6814,0.08019,0.07405,0.0145,0.1379,1.0000 10.000,0.6600,0.08726,0.08114,0.0116,0.1472,1.0000 10.250,0.6229,0.09556,0.08935,0.0059,0.1508,1.0000 10.500,0.5948,0.10456,0.09828,0.0000,0.1776,1.0000