Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-c141d-il-100000-n5 Airfoil,c141d-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,44.5207 Max Cl/Cd alpha,4 Url,http://www.airfoiltools.com/polar/csv?polar=xf-c141d-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.5246,0.09258,0.08695,-0.0419,1.0000,0.0333 -10.000,-0.5370,0.08663,0.08107,-0.0446,1.0000,0.0333 -9.750,-0.5554,0.07959,0.07410,-0.0486,1.0000,0.0330 -9.500,-0.5881,0.07175,0.06627,-0.0526,1.0000,0.0323 -9.250,-0.6283,0.06661,0.06108,-0.0504,1.0000,0.0317 -9.000,-0.6588,0.06171,0.05605,-0.0475,1.0000,0.0315 -8.750,-0.6786,0.05773,0.05189,-0.0443,1.0000,0.0316 -8.500,-0.6918,0.05411,0.04806,-0.0411,1.0000,0.0320 -8.250,-0.7010,0.05046,0.04415,-0.0380,1.0000,0.0324 -8.000,-0.7071,0.04666,0.03999,-0.0348,1.0000,0.0330 -7.750,-0.7097,0.04275,0.03562,-0.0317,1.0000,0.0336 -7.500,-0.7077,0.03895,0.03128,-0.0288,1.0000,0.0341 -7.250,-0.7011,0.03533,0.02700,-0.0261,1.0000,0.0349 -7.000,-0.6872,0.03356,0.02504,-0.0244,1.0000,0.0356 -6.750,-0.6713,0.03217,0.02349,-0.0228,1.0000,0.0366 -6.500,-0.6545,0.03080,0.02188,-0.0213,1.0000,0.0383 -6.250,-0.6363,0.02891,0.01951,-0.0198,1.0000,0.0408 -6.000,-0.6175,0.02811,0.01871,-0.0187,1.0000,0.0426 -5.500,-0.5615,0.02564,0.01581,-0.0194,0.9961,0.0484 -5.250,-0.5307,0.02495,0.01504,-0.0205,0.9936,0.0526 -5.000,-0.5010,0.02412,0.01412,-0.0212,0.9907,0.0570 -4.750,-0.4700,0.02348,0.01332,-0.0221,0.9877,0.0627 -4.500,-0.4384,0.02287,0.01275,-0.0233,0.9850,0.0683 -4.250,-0.4082,0.02224,0.01201,-0.0240,0.9820,0.0747 -4.000,-0.3789,0.02166,0.01145,-0.0247,0.9783,0.0812 -3.750,-0.3479,0.02106,0.01085,-0.0256,0.9752,0.0885 -3.500,-0.3151,0.02059,0.01034,-0.0269,0.9725,0.0974 -3.250,-0.2880,0.02007,0.00989,-0.0271,0.9680,0.1065 -3.000,-0.2583,0.01964,0.00951,-0.0278,0.9640,0.1187 -2.750,-0.2256,0.01925,0.00917,-0.0291,0.9607,0.1366 -2.500,-0.1951,0.01881,0.00887,-0.0300,0.9570,0.1658 -2.250,-0.1688,0.01817,0.00862,-0.0302,0.9519,0.2380 -2.000,-0.1428,0.01679,0.00853,-0.0305,0.9487,0.5130 -1.750,-0.1157,0.01629,0.00880,-0.0295,0.9457,0.7170 -1.500,-0.0900,0.01626,0.00900,-0.0280,0.9409,0.8057 -1.250,-0.0570,0.01641,0.00921,-0.0282,0.9367,0.8713 -1.000,-0.0094,0.01671,0.00950,-0.0313,0.9351,0.9337 -0.750,0.0727,0.01716,0.00986,-0.0419,0.9394,0.9858 -0.500,0.1320,0.01723,0.00983,-0.0487,0.9385,1.0000 -0.250,0.1629,0.01717,0.00970,-0.0498,0.9327,1.0000 0.000,0.1891,0.01713,0.00962,-0.0500,0.9255,1.0000 0.250,0.2174,0.01710,0.00954,-0.0505,0.9185,1.0000 0.500,0.2552,0.01704,0.00946,-0.0527,0.9147,1.0000 0.750,0.2731,0.01706,0.00945,-0.0510,0.9042,1.0000 1.000,0.3104,0.01699,0.00938,-0.0530,0.8998,1.0000 1.250,0.3306,0.01701,0.00941,-0.0517,0.8897,1.0000 1.750,0.3930,0.01673,0.00918,-0.0527,0.8727,1.0000 2.000,0.4300,0.01619,0.00867,-0.0536,0.8575,1.0000 2.250,0.4675,0.01553,0.00803,-0.0543,0.8383,1.0000 2.500,0.4979,0.01505,0.00756,-0.0538,0.8149,1.0000 2.750,0.5257,0.01469,0.00719,-0.0528,0.7872,1.0000 3.000,0.5501,0.01452,0.00701,-0.0515,0.7592,1.0000 3.250,0.5782,0.01434,0.00682,-0.0509,0.7267,1.0000 3.500,0.6071,0.01423,0.00661,-0.0503,0.6819,1.0000 3.750,0.6345,0.01429,0.00643,-0.0495,0.6147,1.0000 4.000,0.6549,0.01471,0.00638,-0.0474,0.5167,1.0000 4.250,0.6659,0.01558,0.00659,-0.0440,0.3994,1.0000 4.500,0.6758,0.01658,0.00701,-0.0407,0.3039,1.0000 4.750,0.6890,0.01745,0.00749,-0.0382,0.2388,1.0000 5.000,0.7043,0.01821,0.00801,-0.0361,0.1966,1.0000 5.250,0.7212,0.01889,0.00852,-0.0342,0.1688,1.0000 5.500,0.7386,0.01955,0.00906,-0.0324,0.1500,1.0000 5.750,0.7566,0.02018,0.00963,-0.0307,0.1361,1.0000 6.000,0.7748,0.02083,0.01025,-0.0290,0.1255,1.0000 6.250,0.7924,0.02155,0.01088,-0.0273,0.1166,1.0000 6.500,0.8118,0.02218,0.01156,-0.0259,0.1084,1.0000 6.750,0.8299,0.02296,0.01229,-0.0243,0.1016,1.0000 7.000,0.8496,0.02365,0.01304,-0.0230,0.0948,1.0000 7.250,0.8681,0.02451,0.01385,-0.0216,0.0892,1.0000 7.500,0.8885,0.02528,0.01471,-0.0204,0.0834,1.0000 7.750,0.9071,0.02618,0.01556,-0.0192,0.0786,1.0000 8.000,0.9281,0.02705,0.01658,-0.0181,0.0735,1.0000 8.250,0.9471,0.02791,0.01745,-0.0169,0.0692,1.0000 8.500,0.9673,0.02897,0.01860,-0.0159,0.0652,1.0000 8.750,0.9866,0.02992,0.01966,-0.0147,0.0612,1.0000 9.000,1.0047,0.03094,0.02061,-0.0136,0.0583,1.0000 9.250,1.0246,0.03218,0.02213,-0.0124,0.0548,1.0000 9.500,1.0417,0.03319,0.02324,-0.0111,0.0520,1.0000 9.750,1.0588,0.03439,0.02444,-0.0099,0.0499,1.0000 10.000,1.0762,0.03606,0.02644,-0.0085,0.0475,1.0000 10.250,1.0910,0.03741,0.02794,-0.0070,0.0454,1.0000 10.500,1.1046,0.03851,0.02908,-0.0054,0.0439,1.0000 10.750,1.1158,0.04031,0.03113,-0.0035,0.0423,1.0000 11.000,1.1237,0.04239,0.03355,-0.0011,0.0408,1.0000 11.250,1.1298,0.04440,0.03580,0.0013,0.0397,1.0000 11.500,1.1343,0.04632,0.03793,0.0037,0.0388,1.0000 11.750,1.1383,0.04810,0.03984,0.0060,0.0381,1.0000 12.000,1.1425,0.04985,0.04167,0.0080,0.0375,1.0000 12.250,1.1342,0.05284,0.04500,0.0109,0.0369,1.0000 12.500,1.1186,0.05647,0.04904,0.0137,0.0363,1.0000 12.750,1.1002,0.06045,0.05336,0.0158,0.0359,1.0000 13.000,1.0788,0.06497,0.05819,0.0169,0.0356,1.0000 13.250,1.0536,0.07034,0.06386,0.0168,0.0355,1.0000 13.500,1.0233,0.07708,0.07088,0.0149,0.0355,1.0000 13.750,0.9864,0.08603,0.08008,0.0104,0.0358,1.0000 14.000,0.9423,0.09853,0.09279,0.0023,0.0365,1.0000