Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m24-il-50000-n5 Airfoil,m24-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,19.9087 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-m24-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.2515,0.11582,0.10963,-0.0264,0.7946,0.0960 -8.750,-0.2560,0.11474,0.10854,-0.0306,0.7875,0.0969 -8.500,-0.2610,0.11366,0.10746,-0.0346,0.7799,0.0972 -8.250,-0.2477,0.10837,0.10218,-0.0343,0.7733,0.0981 -8.000,-0.2284,0.10308,0.09683,-0.0323,0.7671,0.1002 -7.750,-0.2187,0.09982,0.09356,-0.0331,0.7598,0.1024 -7.500,-0.2149,0.09727,0.09097,-0.0336,0.7541,0.1046 -7.250,-0.2088,0.09479,0.08846,-0.0357,0.7473,0.1077 -7.000,-0.2063,0.09348,0.08707,-0.0396,0.7410,0.1116 -6.750,-0.2044,0.09382,0.08717,-0.0444,0.7359,0.1131 -6.500,-0.1883,0.08734,0.08085,-0.0424,0.7290,0.1153 -6.250,-0.1765,0.08404,0.07753,-0.0419,0.7233,0.1185 -6.000,-0.1656,0.08149,0.07489,-0.0426,0.7183,0.1222 -5.750,-0.1523,0.08047,0.07369,-0.0464,0.7114,0.1280 -5.500,-0.1394,0.07857,0.07160,-0.0482,0.7062,0.1297 -5.250,-0.1268,0.07432,0.06737,-0.0471,0.7012,0.1317 -5.000,-0.1117,0.07151,0.06454,-0.0474,0.6946,0.1350 -4.750,-0.0966,0.06936,0.06225,-0.0477,0.6896,0.1402 -4.500,-0.0789,0.06805,0.06064,-0.0492,0.6848,0.1465 -4.250,-0.0639,0.06487,0.05752,-0.0488,0.6782,0.1510 -3.750,-0.0304,0.06069,0.05302,-0.0484,0.6691,0.1673 -3.250,0.0071,0.05706,0.04912,-0.0487,0.6571,0.1829 -3.000,0.0493,0.05365,0.04484,-0.0502,0.6536,0.0948 -2.500,0.0963,0.04984,0.04038,-0.0500,0.6416,0.0811 -2.250,0.1183,0.04803,0.03833,-0.0491,0.6378,0.0804 -2.000,0.1408,0.04684,0.03690,-0.0490,0.6316,0.0807 -1.750,0.1639,0.04558,0.03538,-0.0485,0.6259,0.0808 -1.500,0.1882,0.04409,0.03359,-0.0477,0.6219,0.0804 -1.250,0.2116,0.04301,0.03228,-0.0473,0.6166,0.0796 -1.000,0.2350,0.04214,0.03119,-0.0470,0.6103,0.0790 -0.750,0.2613,0.04095,0.02968,-0.0464,0.6062,0.0786 -0.500,0.2889,0.03984,0.02824,-0.0459,0.6025,0.0786 -0.250,0.3120,0.03967,0.02790,-0.0462,0.5948,0.0792 0.000,0.3405,0.03892,0.02681,-0.0459,0.5905,0.0815 0.250,0.3727,0.03795,0.02562,-0.0461,0.5874,0.0846 0.500,0.4022,0.03832,0.02590,-0.0480,0.5792,0.0870 0.750,0.4409,0.03780,0.02514,-0.0498,0.5747,0.0899 1.000,0.4788,0.03706,0.02415,-0.0508,0.5716,0.0939 1.250,0.5002,0.03780,0.02485,-0.0512,0.5639,0.0985 1.500,0.5242,0.03781,0.02486,-0.0508,0.5590,0.1074 1.750,0.5495,0.03742,0.02438,-0.0499,0.5559,0.1183 2.000,0.5620,0.03847,0.02543,-0.0489,0.5487,0.1299 2.250,0.5785,0.03879,0.02583,-0.0476,0.5434,0.1559 2.500,0.5981,0.03834,0.02563,-0.0460,0.5402,0.2301 2.750,0.7287,0.03760,0.02607,-0.0661,0.5348,1.0000 3.000,0.7398,0.03906,0.02744,-0.0649,0.5281,1.0000 3.250,0.7606,0.03940,0.02762,-0.0637,0.5246,1.0000 3.500,0.7848,0.03942,0.02746,-0.0625,0.5222,1.0000 3.750,0.7749,0.04277,0.03091,-0.0606,0.5120,1.0000 4.000,0.7946,0.04320,0.03123,-0.0593,0.5087,1.0000 4.250,0.8049,0.04450,0.03247,-0.0577,0.5039,1.0000 4.500,0.7940,0.04757,0.03557,-0.0552,0.4951,1.0000 4.750,0.8149,0.04787,0.03579,-0.0539,0.4923,1.0000 5.000,0.8359,0.04821,0.03605,-0.0527,0.4898,1.0000 5.500,0.8184,0.05403,0.04189,-0.0482,0.4754,1.0000 6.000,0.7880,0.06047,0.04831,-0.0427,0.4609,1.0000 6.250,0.7988,0.06182,0.04962,-0.0414,0.4575,1.0000 6.500,0.7726,0.06633,0.05416,-0.0392,0.4482,1.0000 6.750,0.7903,0.06716,0.05497,-0.0381,0.4452,1.0000 7.000,0.8127,0.06761,0.05540,-0.0372,0.4433,1.0000 7.250,0.7778,0.07340,0.06122,-0.0357,0.4336,1.0000 7.500,0.7933,0.07455,0.06237,-0.0349,0.4303,1.0000 7.750,0.8151,0.07513,0.06294,-0.0341,0.4281,1.0000 8.000,0.7892,0.08034,0.06820,-0.0332,0.4198,1.0000 8.250,0.7992,0.08215,0.07003,-0.0326,0.4161,1.0000 8.500,0.8183,0.08308,0.07099,-0.0319,0.4134,1.0000 8.750,0.8065,0.08703,0.07498,-0.0314,0.4068,1.0000 9.000,0.8097,0.08960,0.07760,-0.0309,0.4021,1.0000 9.250,0.8253,0.09096,0.07899,-0.0303,0.3991,1.0000 9.500,0.8472,0.09168,0.07977,-0.0297,0.3968,1.0000 9.750,0.8242,0.09686,0.08501,-0.0297,0.3884,1.0000 10.000,0.8362,0.09861,0.08681,-0.0292,0.3847,1.0000 10.250,0.8565,0.09951,0.08778,-0.0287,0.3821,1.0000 10.500,0.8419,0.10394,0.09227,-0.0287,0.3747,1.0000 10.750,0.8504,0.10605,0.09445,-0.0285,0.3702,1.0000 11.000,0.8690,0.10714,0.09563,-0.0280,0.3672,1.0000 11.250,0.8615,0.11094,0.09950,-0.0281,0.3607,1.0000 11.500,0.8659,0.11351,0.10216,-0.0280,0.3556,1.0000 11.750,0.8827,0.11482,0.10356,-0.0277,0.3523,1.0000