Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-boe103-il-50000 Airfoil,boe103-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,32.583 Max Cl/Cd alpha,7.75 Url,http://airfoiltools.com/polar/csv?polar=xf-boe103-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.3430,0.10999,0.10301,-0.0267,1.0000,0.2656 -8.750,-0.3256,0.10581,0.09885,-0.0252,1.0000,0.2758 -8.500,-0.3641,0.10655,0.09983,-0.0246,1.0000,0.2834 -8.250,-0.3405,0.10212,0.09538,-0.0227,1.0000,0.2982 -8.000,-0.3279,0.09855,0.09186,-0.0210,1.0000,0.3088 -7.750,-0.3434,0.09701,0.09047,-0.0190,1.0000,0.3193 -7.500,-0.3599,0.09617,0.08977,-0.0160,1.0000,0.3321 -7.250,-0.3435,0.09256,0.08619,-0.0141,1.0000,0.3451 -7.000,-0.3464,0.09035,0.08408,-0.0113,1.0000,0.3574 -6.750,-0.3629,0.08905,0.08292,-0.0074,1.0000,0.3703 -6.500,-0.4039,0.08974,0.08381,-0.0014,1.0000,0.3823 -6.250,-0.4077,0.08773,0.08190,0.0023,1.0000,0.3986 -6.000,-0.4221,0.08639,0.08067,0.0064,1.0000,0.4158 -5.750,-0.3874,0.08252,0.07676,0.0088,1.0000,0.4443 -5.500,-0.4151,0.08214,0.07654,0.0146,1.0000,0.4652 -5.000,-0.4598,0.05374,0.04637,-0.0313,1.0000,0.1679 -4.750,-0.4432,0.05060,0.04303,-0.0313,1.0000,0.1640 -4.500,-0.4247,0.04736,0.03950,-0.0317,1.0000,0.1607 -4.250,-0.4023,0.04382,0.03537,-0.0328,1.0000,0.1552 -4.000,-0.3768,0.04110,0.03174,-0.0335,1.0000,0.1510 -3.750,-0.3542,0.03905,0.02935,-0.0335,1.0000,0.1512 -3.500,-0.3334,0.03745,0.02771,-0.0333,1.0000,0.1548 -3.250,-0.3113,0.03620,0.02626,-0.0331,1.0000,0.1594 -3.000,-0.2876,0.03500,0.02469,-0.0329,1.0000,0.1635 -2.750,-0.2637,0.03388,0.02325,-0.0327,1.0000,0.1680 -2.500,-0.2414,0.03297,0.02234,-0.0324,1.0000,0.1758 -2.250,-0.2184,0.03222,0.02152,-0.0321,1.0000,0.1887 -2.000,-0.1952,0.03150,0.02083,-0.0318,1.0000,0.2083 -1.750,-0.1682,0.03046,0.01997,-0.0318,1.0000,0.2534 -1.500,-0.1358,0.02854,0.01947,-0.0329,1.0000,0.4375 -1.250,-0.1300,0.02670,0.01966,-0.0263,1.0000,1.0000 -1.000,-0.1090,0.02731,0.01968,-0.0265,1.0000,1.0000 -0.750,-0.0614,0.02851,0.02033,-0.0316,0.9893,1.0000 -0.500,-0.0151,0.02969,0.02109,-0.0364,0.9771,1.0000 -0.250,0.0290,0.03078,0.02184,-0.0407,0.9639,1.0000 0.000,0.0718,0.03180,0.02258,-0.0446,0.9498,1.0000 0.250,0.1136,0.03275,0.02329,-0.0482,0.9350,1.0000 0.500,0.1540,0.03365,0.02399,-0.0514,0.9199,1.0000 0.750,0.1925,0.03450,0.02468,-0.0542,0.9048,1.0000 1.000,0.2297,0.03533,0.02535,-0.0566,0.8897,1.0000 1.250,0.2661,0.03612,0.02602,-0.0588,0.8746,1.0000 1.500,0.3021,0.03688,0.02668,-0.0608,0.8594,1.0000 1.750,0.3375,0.03759,0.02731,-0.0625,0.8439,1.0000 2.000,0.3723,0.03826,0.02792,-0.0641,0.8281,1.0000 2.250,0.4063,0.03889,0.02850,-0.0653,0.8121,1.0000 2.500,0.4395,0.03948,0.02906,-0.0663,0.7959,1.0000 2.750,0.4720,0.04004,0.02960,-0.0671,0.7795,1.0000 3.000,0.5035,0.04055,0.03010,-0.0676,0.7627,1.0000 3.250,0.5347,0.04104,0.03060,-0.0680,0.7462,1.0000 3.500,0.5659,0.04146,0.03103,-0.0682,0.7296,1.0000 3.750,0.5971,0.04184,0.03143,-0.0683,0.7134,1.0000 4.000,0.6291,0.04210,0.03173,-0.0683,0.6974,1.0000 4.250,0.6619,0.04224,0.03190,-0.0683,0.6821,1.0000 4.500,0.7224,0.04066,0.03039,-0.0702,0.6713,1.0000 4.750,0.7525,0.04066,0.03045,-0.0695,0.6556,1.0000 5.000,0.7831,0.04055,0.03040,-0.0687,0.6398,1.0000 5.250,0.8148,0.04030,0.03022,-0.0678,0.6240,1.0000 5.500,0.8496,0.03972,0.02969,-0.0670,0.6080,1.0000 5.750,0.8932,0.03830,0.02831,-0.0666,0.5913,1.0000 6.000,0.9267,0.03733,0.02739,-0.0652,0.5713,1.0000 6.250,0.9565,0.03655,0.02662,-0.0635,0.5496,1.0000 6.500,1.0011,0.03480,0.02482,-0.0631,0.5280,1.0000 6.750,1.0295,0.03441,0.02441,-0.0617,0.5064,1.0000 7.000,1.0520,0.03447,0.02448,-0.0599,0.4840,1.0000 7.250,1.0870,0.03384,0.02371,-0.0592,0.4609,1.0000 7.500,1.1022,0.03446,0.02437,-0.0567,0.4365,1.0000 7.750,1.1290,0.03465,0.02439,-0.0554,0.4114,1.0000 8.000,1.1493,0.03532,0.02495,-0.0536,0.3855,1.0000 8.250,1.1670,0.03639,0.02595,-0.0517,0.3611,1.0000 8.500,1.1870,0.03755,0.02699,-0.0502,0.3390,1.0000 8.750,1.2097,0.03895,0.02826,-0.0493,0.3206,1.0000 9.000,1.2242,0.04085,0.03026,-0.0476,0.3064,1.0000 9.250,1.2363,0.04300,0.03260,-0.0458,0.2951,1.0000 9.500,1.2578,0.04481,0.03440,-0.0451,0.2848,1.0000 9.750,1.2638,0.04708,0.03691,-0.0427,0.2761,1.0000 10.000,1.2775,0.04923,0.03916,-0.0413,0.2684,1.0000 10.250,1.2730,0.05219,0.04245,-0.0382,0.2628,1.0000 10.500,1.3038,0.05394,0.04416,-0.0387,0.2562,1.0000 10.750,1.2817,0.05791,0.04853,-0.0344,0.2536,1.0000 11.000,1.2465,0.06253,0.05350,-0.0296,0.2519,1.0000 11.250,1.1937,0.06870,0.05991,-0.0252,0.2520,1.0000 11.500,1.1090,0.08003,0.07138,-0.0245,0.2543,1.0000