Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-b29root-il-50000-n5 Airfoil,b29root-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,8.54321 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-b29root-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -14.500,-0.4150,0.11908,0.11048,-0.0553,1.0000,0.1240 -14.250,-0.5667,0.08834,0.07947,-0.0709,1.0000,0.1270 -14.000,-0.6653,0.07349,0.06422,-0.0769,1.0000,0.1273 -13.750,-0.7102,0.06695,0.05738,-0.0779,1.0000,0.1280 -13.500,-0.7077,0.06464,0.05508,-0.0774,1.0000,0.1297 -13.250,-0.7017,0.06283,0.05330,-0.0768,1.0000,0.1318 -13.000,-0.7071,0.06033,0.05074,-0.0759,1.0000,0.1338 -12.750,-0.7168,0.05777,0.04807,-0.0747,1.0000,0.1358 -12.500,-0.7291,0.05536,0.04554,-0.0729,1.0000,0.1378 -12.250,-0.7437,0.05326,0.04330,-0.0704,1.0000,0.1397 -12.000,-0.7562,0.05183,0.04180,-0.0672,1.0000,0.1415 -11.750,-0.7576,0.05147,0.04160,-0.0640,1.0000,0.1434 -11.500,-0.7373,0.05016,0.04029,-0.0649,0.9875,0.1471 -11.250,-0.7133,0.04821,0.03814,-0.0673,0.9734,0.1521 -11.000,-0.6800,0.04668,0.03656,-0.0701,0.9626,0.1578 -10.750,-0.6476,0.04528,0.03512,-0.0726,0.9515,0.1641 -10.500,-0.6164,0.04376,0.03349,-0.0752,0.9414,0.1714 -10.250,-0.5823,0.04243,0.03217,-0.0779,0.9323,0.1797 -10.000,-0.5543,0.04115,0.03086,-0.0797,0.9210,0.1884 -9.750,-0.5255,0.03972,0.02933,-0.0820,0.9121,0.1999 -9.500,-0.5045,0.03868,0.02842,-0.0825,0.8998,0.2105 -9.250,-0.4832,0.03754,0.02731,-0.0832,0.8896,0.2234 -9.000,-0.4677,0.03654,0.02635,-0.0828,0.8779,0.2380 -8.750,-0.4553,0.03567,0.02552,-0.0817,0.8669,0.2541 -8.500,-0.4439,0.03488,0.02479,-0.0803,0.8565,0.2726 -8.250,-0.4367,0.03430,0.02427,-0.0780,0.8457,0.2916 -8.000,-0.4280,0.03377,0.02377,-0.0757,0.8359,0.3130 -7.750,-0.4231,0.03342,0.02344,-0.0726,0.8257,0.3332 -7.500,-0.4166,0.03310,0.02312,-0.0695,0.8165,0.3541 -7.250,-0.4106,0.03289,0.02290,-0.0662,0.8078,0.3739 -7.000,-0.4065,0.03279,0.02280,-0.0625,0.7982,0.3920 -6.750,-0.3953,0.03262,0.02257,-0.0597,0.7915,0.4113 -6.500,-0.3973,0.03272,0.02266,-0.0550,0.7815,0.4264 -6.250,-0.3916,0.03263,0.02249,-0.0513,0.7740,0.4435 -6.000,-0.3777,0.03263,0.02245,-0.0488,0.7675,0.4606 -5.750,-0.3658,0.03290,0.02276,-0.0460,0.7585,0.4754 -5.500,-0.3479,0.03290,0.02272,-0.0440,0.7522,0.4919 -5.250,-0.3352,0.03292,0.02266,-0.0414,0.7460,0.5079 -5.000,-0.3319,0.03314,0.02287,-0.0374,0.7372,0.5224 -4.750,-0.3055,0.03332,0.02306,-0.0365,0.7314,0.5394 -4.500,-0.2751,0.03345,0.02313,-0.0361,0.7271,0.5575 -4.250,-0.2760,0.03393,0.02366,-0.0316,0.7175,0.5712 -4.000,-0.2658,0.03394,0.02361,-0.0285,0.7113,0.5875 -3.750,-0.2198,0.03414,0.02375,-0.0306,0.7072,0.6008 -3.500,-0.2157,0.03445,0.02407,-0.0271,0.6991,0.6122 -3.250,-0.1987,0.03463,0.02420,-0.0253,0.6923,0.6243 -3.000,-0.1645,0.03464,0.02414,-0.0261,0.6878,0.6354 -2.750,-0.1551,0.03451,0.02392,-0.0231,0.6828,0.6494 -2.500,-0.1336,0.03529,0.02476,-0.0223,0.6743,0.6582 -2.250,-0.1215,0.03524,0.02464,-0.0198,0.6688,0.6719 -2.000,-0.0720,0.03540,0.02472,-0.0228,0.6653,0.6817 -1.750,-0.0748,0.03595,0.02529,-0.0184,0.6575,0.6948 -1.500,-0.0535,0.03644,0.02577,-0.0175,0.6509,0.7062 -1.250,-0.0205,0.03655,0.02582,-0.0182,0.6466,0.7179 -1.000,0.0107,0.03648,0.02564,-0.0183,0.6435,0.7315 -0.750,0.0130,0.03782,0.02708,-0.0153,0.6341,0.7417 -0.500,0.0266,0.03812,0.02735,-0.0131,0.6286,0.7563 -0.250,0.0792,0.03837,0.02752,-0.0168,0.6252,0.7651 0.000,0.1146,0.03827,0.02732,-0.0176,0.6225,0.7779 0.250,0.0894,0.04017,0.02936,-0.0110,0.6113,0.7930 0.500,0.1332,0.04059,0.02972,-0.0137,0.6073,0.8022 0.750,0.1609,0.04058,0.02964,-0.0134,0.6041,0.8166 1.250,0.1864,0.04326,0.03237,-0.0111,0.5896,0.8401 1.500,0.2314,0.04358,0.03264,-0.0140,0.5863,0.8493 1.750,0.2722,0.04357,0.03257,-0.0159,0.5837,0.8603 2.250,0.2790,0.04683,0.03590,-0.0122,0.5680,0.8876 2.500,0.3186,0.04693,0.03596,-0.0142,0.5653,0.8986 2.750,0.3696,0.04683,0.03581,-0.0179,0.5633,0.9073 3.250,0.3654,0.05087,0.03995,-0.0146,0.5465,0.9364 3.500,0.4097,0.05071,0.03975,-0.0172,0.5445,0.9464 4.000,0.4251,0.05532,0.04446,-0.0191,0.5280,0.9710 4.250,0.4715,0.05519,0.04431,-0.0223,0.5258,0.9796 5.250,0.4651,0.06305,0.05220,-0.0188,0.4984,1.0000 5.500,0.4568,0.06430,0.05341,-0.0155,0.4929,1.0000 5.750,0.4663,0.06462,0.05368,-0.0133,0.4895,1.0000 6.000,0.4841,0.06457,0.05360,-0.0116,0.4871,1.0000 6.250,0.4358,0.06847,0.05747,-0.0063,0.4768,1.0000 6.500,0.4413,0.06934,0.05831,-0.0042,0.4727,1.0000 6.750,0.4575,0.06960,0.05854,-0.0026,0.4697,1.0000 7.250,0.4333,0.07393,0.06282,0.0028,0.4566,1.0000 7.500,0.4453,0.07469,0.06357,0.0043,0.4530,1.0000 7.750,0.4650,0.07501,0.06387,0.0055,0.4504,1.0000 8.000,0.4394,0.07836,0.06722,0.0082,0.4415,1.0000 8.250,0.4457,0.07967,0.06852,0.0097,0.4367,1.0000 8.500,0.4631,0.08026,0.06910,0.0108,0.4333,1.0000 9.000,0.4554,0.08453,0.07339,0.0139,0.4204,1.0000 9.250,0.4708,0.08534,0.07421,0.0150,0.4163,1.0000 9.500,0.4953,0.08547,0.07434,0.0159,0.4135,1.0000 9.750,0.4724,0.08913,0.07802,0.0174,0.4032,1.0000 10.000,0.4886,0.08986,0.07877,0.0184,0.3986,1.0000 10.250,0.5150,0.08979,0.07871,0.0192,0.3955,1.0000 10.500,0.4937,0.09350,0.08246,0.0204,0.3846,1.0000 10.750,0.5137,0.09389,0.08287,0.0213,0.3801,1.0000 11.250,0.5189,0.09766,0.08671,0.0230,0.3652,1.0000 11.500,0.5440,0.09755,0.08662,0.0239,0.3614,1.0000 11.750,0.5299,0.10105,0.09016,0.0245,0.3508,1.0000 12.000,0.5498,0.10135,0.09051,0.0253,0.3457,1.0000 12.250,0.5457,0.10406,0.09326,0.0258,0.3367,1.0000 12.500,0.5590,0.10497,0.09422,0.0265,0.3301,1.0000 12.750,0.5773,0.10537,0.09465,0.0274,0.3249,1.0000 13.000,0.5711,0.10834,0.09767,0.0276,0.3142,1.0000 13.250,0.5982,0.10762,0.09700,0.0286,0.3103,1.0000 13.500,0.5846,0.11156,0.10099,0.0285,0.2981,1.0000 13.750,0.6116,0.11072,0.10020,0.0296,0.2940,1.0000