Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-v13006-il-500000 Airfoil,v13006-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,54.7299 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-v13006-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.6439,0.09463,0.09240,0.0196,1.0000,0.0163 -8.250,-0.6424,0.09035,0.08813,0.0166,1.0000,0.0167 -8.000,-0.6419,0.08569,0.08350,0.0124,1.0000,0.0172 -7.750,-0.6375,0.07991,0.07771,0.0051,1.0000,0.0177 -7.500,-0.6253,0.07314,0.07086,-0.0034,1.0000,0.0183 -7.250,-0.6115,0.06755,0.06513,-0.0082,1.0000,0.0186 -7.000,-0.5983,0.06263,0.06008,-0.0108,1.0000,0.0187 -6.750,-0.5845,0.05788,0.05516,-0.0126,1.0000,0.0187 -6.500,-0.5700,0.05329,0.05036,-0.0137,1.0000,0.0188 -6.250,-0.5664,0.04566,0.04257,-0.0152,1.0000,0.0195 -6.000,-0.5500,0.04279,0.03960,-0.0154,1.0000,0.0199 -5.750,-0.5317,0.04014,0.03683,-0.0156,1.0000,0.0205 -5.500,-0.5117,0.03732,0.03385,-0.0156,1.0000,0.0215 -5.250,-0.4900,0.03434,0.03066,-0.0153,1.0000,0.0231 -5.000,-0.4603,0.03372,0.02964,-0.0140,1.0000,0.0256 -4.750,-0.4451,0.02720,0.02261,-0.0134,1.0000,0.0267 -4.500,-0.4236,0.02484,0.02019,-0.0131,1.0000,0.0278 -4.250,-0.4005,0.02335,0.01861,-0.0127,1.0000,0.0293 -4.000,-0.3762,0.02203,0.01712,-0.0121,1.0000,0.0321 -3.750,-0.3481,0.02303,0.01791,-0.0109,1.0000,0.0353 -3.500,-0.3278,0.01833,0.01281,-0.0101,1.0000,0.0377 -3.250,-0.3006,0.01398,0.00799,-0.0080,1.0000,0.0221 -3.000,-0.2755,0.01262,0.00647,-0.0070,1.0000,0.0220 -2.750,-0.2507,0.01169,0.00547,-0.0062,1.0000,0.0225 -2.500,-0.2260,0.01101,0.00476,-0.0054,1.0000,0.0235 -2.250,-0.2011,0.01058,0.00431,-0.0047,1.0000,0.0250 -2.000,-0.1764,0.01006,0.00376,-0.0039,1.0000,0.0256 -1.750,-0.1523,0.00909,0.00275,-0.0031,1.0000,0.0277 -1.500,-0.1273,0.00869,0.00236,-0.0025,1.0000,0.0309 -1.250,-0.1021,0.00846,0.00213,-0.0020,1.0000,0.0352 -1.000,-0.0676,0.00797,0.00167,-0.0034,0.9969,0.0541 -0.750,-0.0354,0.00566,0.00143,-0.0057,0.9921,0.6337 -0.500,-0.0071,0.00477,0.00158,-0.0047,0.9853,0.9355 -0.250,0.0564,0.00478,0.00156,-0.0121,0.9843,1.0000 0.000,0.0954,0.00475,0.00148,-0.0144,0.9661,1.0000 0.250,0.1305,0.00472,0.00140,-0.0158,0.9399,1.0000 0.500,0.1580,0.00472,0.00132,-0.0154,0.9037,1.0000 0.750,0.1821,0.00479,0.00124,-0.0141,0.8593,1.0000 1.000,0.2061,0.00493,0.00119,-0.0130,0.8083,1.0000 1.250,0.2303,0.00514,0.00116,-0.0119,0.7522,1.0000 1.500,0.2547,0.00540,0.00117,-0.0110,0.6884,1.0000 1.750,0.2793,0.00570,0.00119,-0.0103,0.6228,1.0000 2.000,0.3038,0.00608,0.00124,-0.0096,0.5421,1.0000 2.250,0.3280,0.00655,0.00131,-0.0090,0.4455,1.0000 2.500,0.3531,0.00695,0.00142,-0.0086,0.3732,1.0000 2.750,0.3786,0.00731,0.00154,-0.0082,0.3162,1.0000 3.000,0.4041,0.00769,0.00168,-0.0079,0.2630,1.0000 3.250,0.4301,0.00797,0.00183,-0.0076,0.2256,1.0000 3.500,0.4559,0.00833,0.00201,-0.0073,0.1804,1.0000 3.750,0.4802,0.00910,0.00233,-0.0070,0.0811,1.0000 4.000,0.5048,0.01001,0.00299,-0.0064,0.0275,1.0000 4.250,0.5310,0.01045,0.00350,-0.0060,0.0247,1.0000 4.500,0.5571,0.01087,0.00398,-0.0056,0.0231,1.0000 4.750,0.5831,0.01129,0.00443,-0.0053,0.0215,1.0000 5.000,0.6087,0.01185,0.00503,-0.0049,0.0205,1.0000 5.250,0.6335,0.01263,0.00586,-0.0044,0.0198,1.0000 5.500,0.6571,0.01379,0.00712,-0.0037,0.0191,1.0000 5.750,0.6804,0.01516,0.00856,-0.0029,0.0188,1.0000 6.000,0.7050,0.01624,0.00972,-0.0023,0.0187,1.0000 6.250,0.7291,0.01769,0.01129,-0.0016,0.0186,1.0000 6.500,0.7522,0.02007,0.01382,-0.0008,0.0189,1.0000 6.750,0.7765,0.02152,0.01542,-0.0003,0.0190,1.0000 7.000,0.7991,0.02368,0.01781,0.0004,0.0190,1.0000 7.250,0.8236,0.02464,0.01893,0.0010,0.0193,1.0000 7.500,0.7992,0.01964,0.01564,0.0075,0.0310,1.0000 7.750,0.8129,0.02266,0.01893,0.0084,0.0297,1.0000 8.000,0.8253,0.02576,0.02222,0.0092,0.0287,1.0000 8.250,0.8366,0.02895,0.02558,0.0099,0.0280,1.0000 8.500,0.8479,0.03241,0.02908,0.0104,0.0273,1.0000 8.750,0.8407,0.03981,0.03668,0.0108,0.0264,1.0000