Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m8-il-50000-n5 Airfoil,m8-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,26.4583 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-m8-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.1265,0.11210,0.10611,-0.0270,0.8297,0.1012 -8.750,-0.1247,0.11117,0.10516,-0.0289,0.8164,0.1022 -8.500,-0.1228,0.10982,0.10381,-0.0304,0.8050,0.1027 -8.250,-0.1012,0.10421,0.09815,-0.0287,0.7943,0.1065 -8.000,-0.0931,0.10209,0.09598,-0.0291,0.7841,0.1109 -7.750,-0.0913,0.10113,0.09504,-0.0310,0.7734,0.1142 -7.500,-0.0933,0.10065,0.09456,-0.0330,0.7638,0.1150 -7.250,-0.0733,0.09569,0.08956,-0.0317,0.7545,0.1177 -7.000,-0.0650,0.09353,0.08737,-0.0318,0.7453,0.1206 -6.750,-0.0596,0.09201,0.08584,-0.0332,0.7356,0.1245 -6.500,-0.0535,0.09068,0.08450,-0.0361,0.7266,0.1265 -6.250,-0.0390,0.08747,0.08125,-0.0346,0.7171,0.1317 -6.000,-0.0303,0.08653,0.08027,-0.0385,0.7084,0.1361 -5.750,-0.0165,0.08330,0.07704,-0.0376,0.6994,0.1389 -5.500,-0.0032,0.08120,0.07489,-0.0389,0.6915,0.1426 -5.250,0.0119,0.07957,0.07321,-0.0427,0.6828,0.1450 -5.000,0.0262,0.07682,0.07040,-0.0428,0.6762,0.1468 -4.500,0.0697,0.06888,0.06212,-0.0550,0.6614,0.1021 -4.250,0.0863,0.06620,0.05944,-0.0547,0.6536,0.0985 -4.000,0.1086,0.06331,0.05644,-0.0575,0.6462,0.0947 -3.750,0.1320,0.06073,0.05369,-0.0598,0.6403,0.0945 -3.500,0.1563,0.05853,0.05142,-0.0624,0.6314,0.0958 -3.250,0.1821,0.05594,0.04863,-0.0646,0.6253,0.0953 -3.000,0.2093,0.05338,0.04590,-0.0675,0.6177,0.0943 -2.750,0.2362,0.05106,0.04341,-0.0694,0.6106,0.0948 -2.500,0.2635,0.04892,0.04102,-0.0707,0.6057,0.0976 -2.250,0.2917,0.04682,0.03876,-0.0730,0.5970,0.0997 -2.000,0.3209,0.04425,0.03588,-0.0746,0.5910,0.1008 -1.750,0.3497,0.04192,0.03324,-0.0758,0.5851,0.1035 -1.500,0.3729,0.04165,0.03295,-0.0755,0.5765,0.1077 -1.250,0.4018,0.03976,0.03073,-0.0760,0.5711,0.1125 -1.000,0.4285,0.03867,0.02944,-0.0764,0.5638,0.1171 -0.750,0.4543,0.03818,0.02881,-0.0763,0.5566,0.1244 -0.500,0.4810,0.03760,0.02805,-0.0757,0.5518,0.1307 -0.250,0.5060,0.03760,0.02797,-0.0757,0.5445,0.1399 0.000,0.5321,0.03740,0.02762,-0.0755,0.5378,0.1500 0.250,0.5610,0.03699,0.02692,-0.0750,0.5331,0.1644 0.500,0.5865,0.03711,0.02685,-0.0750,0.5256,0.1796 0.750,0.6121,0.03702,0.02656,-0.0748,0.5189,0.1969 1.000,0.6390,0.03655,0.02583,-0.0743,0.5144,0.2179 1.250,0.6620,0.03664,0.02579,-0.0740,0.5083,0.2371 1.500,0.6840,0.03695,0.02598,-0.0736,0.5008,0.2547 1.750,0.7112,0.03652,0.02533,-0.0729,0.4955,0.2706 2.000,0.7333,0.03681,0.02558,-0.0727,0.4866,0.2857 2.250,0.7597,0.03662,0.02524,-0.0722,0.4789,0.3038 2.500,0.7888,0.03625,0.02468,-0.0719,0.4725,0.3147 2.750,0.8109,0.03685,0.02521,-0.0718,0.4629,0.3173 3.000,0.8421,0.03648,0.02460,-0.0714,0.4578,0.3172 3.250,0.8614,0.03749,0.02563,-0.0713,0.4490,0.3169 3.500,0.8882,0.03758,0.02560,-0.0710,0.4427,0.3174 3.750,0.9176,0.03741,0.02526,-0.0706,0.4379,0.3181 4.000,0.9325,0.03875,0.02670,-0.0703,0.4286,0.3181 4.250,0.9621,0.03847,0.02629,-0.0698,0.4235,0.3174 4.500,0.9776,0.03966,0.02753,-0.0693,0.4152,0.3167 4.750,1.0010,0.03994,0.02779,-0.0687,0.4087,0.3159 5.000,1.0332,0.03937,0.02706,-0.0681,0.4046,0.3151 5.250,1.0372,0.04153,0.02939,-0.0672,0.3945,0.3146 5.500,1.0660,0.04117,0.02893,-0.0664,0.3894,0.3139 5.750,1.0747,0.04272,0.03059,-0.0654,0.3812,0.3135 6.000,1.0930,0.04329,0.03115,-0.0644,0.3745,0.3136 6.250,1.1258,0.04255,0.03028,-0.0636,0.3704,0.3143 6.500,1.1130,0.04598,0.03393,-0.0621,0.3604,0.3143 6.750,1.1363,0.04609,0.03402,-0.0611,0.3553,0.3150 7.000,1.1724,0.04514,0.03295,-0.0603,0.3518,0.3157 7.250,1.1213,0.05172,0.03981,-0.0582,0.3400,0.3151 7.500,1.1513,0.05114,0.03918,-0.0571,0.3361,0.3156 7.750,1.1952,0.04954,0.03748,-0.0563,0.3333,0.3160 8.000,1.1042,0.06159,0.04983,-0.0568,0.3185,0.3153 8.250,1.1369,0.06039,0.04860,-0.0553,0.3162,0.3155 8.500,1.1751,0.05875,0.04690,-0.0537,0.3145,0.3157 9.000,1.0941,0.07587,0.06428,-0.0572,0.2965,0.3152 9.500,1.0328,0.09308,0.08165,-0.0622,0.2800,0.3149 10.000,0.9817,0.10962,0.09833,-0.0676,0.2671,0.3147 10.250,0.9928,0.11181,0.10055,-0.0675,0.2652,0.3148 10.500,1.0078,0.11337,0.10214,-0.0671,0.2637,0.3149 10.750,0.9689,0.12424,0.11310,-0.0716,0.2581,0.3147 11.000,0.9673,0.12855,0.11748,-0.0728,0.2546,0.3148