Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ah93w300-il-100000-n5 Airfoil,ah93w300-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,27.3342 Max Cl/Cd alpha,6.5 Url,http://airfoiltools.com/polar/csv?polar=xf-ah93w300-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -15.000,-0.4649,0.11657,0.10902,-0.0464,1.0000,0.1970 -14.750,-0.4518,0.11545,0.10794,-0.0466,1.0000,0.2005 -14.250,-0.4865,0.10437,0.09680,-0.0492,1.0000,0.2193 -14.000,-0.4625,0.10508,0.09757,-0.0487,1.0000,0.2204 -13.750,-0.4410,0.10551,0.09807,-0.0481,1.0000,0.2219 -13.500,-0.4248,0.10529,0.09791,-0.0476,1.0000,0.2244 -13.000,-0.4808,0.09316,0.08573,-0.0490,1.0000,0.2461 -12.750,-0.4609,0.09418,0.08685,-0.0476,1.0000,0.2470 -12.250,-0.4537,0.08726,0.07992,-0.0515,0.9842,0.2605 -12.000,-0.3739,0.09206,0.08480,-0.0535,0.9704,0.2549 -11.250,-0.3468,0.08045,0.07300,-0.0633,0.9312,0.2765 -7.250,-0.2732,0.04229,0.03362,-0.0689,0.7321,0.3741 -7.000,-0.2384,0.04317,0.03455,-0.0686,0.7215,0.3749 -6.750,-0.2060,0.04385,0.03523,-0.0682,0.7113,0.3760 -6.500,-0.1754,0.04433,0.03564,-0.0677,0.7025,0.3773 -6.250,-0.1489,0.04455,0.03586,-0.0673,0.6930,0.3792 -5.500,-0.2602,0.03182,0.02263,-0.0609,0.6721,0.4122 -5.250,-0.2281,0.03227,0.02313,-0.0607,0.6635,0.4141 -5.000,-0.1992,0.03254,0.02345,-0.0603,0.6543,0.4163 -4.750,-0.1745,0.03244,0.02330,-0.0599,0.6464,0.4194 -4.500,-0.1620,0.03138,0.02208,-0.0595,0.6399,0.4253 -4.250,-0.1556,0.02994,0.02051,-0.0590,0.6318,0.4321 -4.000,-0.1265,0.03019,0.02080,-0.0586,0.6234,0.4342 -3.750,-0.0974,0.03032,0.02091,-0.0584,0.6162,0.4367 -3.500,-0.0713,0.03029,0.02085,-0.0582,0.6092,0.4399 -3.250,-0.0506,0.02990,0.02044,-0.0580,0.6011,0.4446 -3.000,-0.0340,0.02863,0.01894,-0.0587,0.5940,0.4520 -2.750,-0.0042,0.02879,0.01909,-0.0584,0.5875,0.4540 -2.500,0.0232,0.02899,0.01933,-0.0581,0.5805,0.4564 -2.250,0.0489,0.02910,0.01949,-0.0576,0.5727,0.4594 -2.000,0.0750,0.02899,0.01935,-0.0576,0.5659,0.4631 -1.750,0.1018,0.02859,0.01879,-0.0582,0.5600,0.4680 -1.500,0.1262,0.02796,0.01802,-0.0591,0.5533,0.4740 -1.250,0.1520,0.02815,0.01830,-0.0585,0.5459,0.4763 -1.000,0.1790,0.02829,0.01846,-0.0581,0.5394,0.4789 -0.750,0.2079,0.02833,0.01845,-0.0581,0.5339,0.4819 -0.500,0.2333,0.02835,0.01848,-0.0580,0.5273,0.4855 -0.250,0.2588,0.02822,0.01834,-0.0581,0.5204,0.4901 0.000,0.2871,0.02783,0.01779,-0.0593,0.5142,0.4960 0.250,0.3160,0.02782,0.01772,-0.0594,0.5090,0.4990 0.500,0.3411,0.02801,0.01799,-0.0589,0.5030,0.5015 0.750,0.3654,0.02818,0.01824,-0.0583,0.4964,0.5044 1.000,0.3917,0.02827,0.01834,-0.0580,0.4905,0.5079 1.250,0.4207,0.02826,0.01824,-0.0584,0.4853,0.5121 1.500,0.4484,0.02823,0.01815,-0.0589,0.4798,0.5169 1.750,0.4749,0.02814,0.01801,-0.0597,0.4734,0.5220 2.000,0.4994,0.02828,0.01821,-0.0590,0.4675,0.5246 2.250,0.5261,0.02841,0.01834,-0.0586,0.4624,0.5275 2.500,0.5527,0.02861,0.01853,-0.0584,0.4574,0.5308 2.750,0.5738,0.02886,0.01888,-0.0575,0.4510,0.5343 3.000,0.5982,0.02898,0.01901,-0.0572,0.4451,0.5383 3.250,0.6265,0.02901,0.01896,-0.0576,0.4399,0.5429 3.500,0.6571,0.02904,0.01885,-0.0586,0.4349,0.5480 3.750,0.6754,0.02932,0.01927,-0.0574,0.4286,0.5512 4.000,0.6961,0.02958,0.01960,-0.0562,0.4229,0.5541 4.250,0.7203,0.02976,0.01977,-0.0556,0.4178,0.5573 4.500,0.7471,0.02994,0.01991,-0.0555,0.4131,0.5609 4.750,0.7618,0.03036,0.02046,-0.0538,0.4070,0.5649 5.000,0.7818,0.03064,0.02076,-0.0530,0.4012,0.5694 5.250,0.8071,0.03079,0.02084,-0.0530,0.3962,0.5743 5.500,0.8337,0.03098,0.02094,-0.0533,0.3914,0.5785 5.750,0.8403,0.03150,0.02163,-0.0503,0.3855,0.5813 6.000,0.8519,0.03190,0.02212,-0.0480,0.3801,0.5844 6.250,0.8705,0.03219,0.02241,-0.0467,0.3754,0.5881 6.500,0.8900,0.03256,0.02276,-0.0457,0.3707,0.5923 6.750,0.8964,0.03345,0.02379,-0.0435,0.3649,0.5965 7.000,0.9121,0.03408,0.02445,-0.0425,0.3594,0.6010 7.250,0.9360,0.03440,0.02469,-0.0425,0.3547,0.6057 7.500,0.9502,0.03520,0.02552,-0.0416,0.3496,0.6096 7.750,0.9547,0.03635,0.02682,-0.0395,0.3439,0.6129 8.000,0.9677,0.03713,0.02766,-0.0383,0.3388,0.6166 8.250,0.9910,0.03742,0.02790,-0.0379,0.3345,0.6211 8.500,0.9909,0.03909,0.02973,-0.0361,0.3289,0.6251 8.750,0.9968,0.04052,0.03124,-0.0349,0.3233,0.6295 9.000,1.0140,0.04128,0.03196,-0.0346,0.3186,0.6342 9.250,1.0301,0.04224,0.03289,-0.0344,0.3140,0.6390 9.500,1.0248,0.04460,0.03544,-0.0331,0.3081,0.6425 9.750,1.0322,0.04601,0.03692,-0.0321,0.3031,0.6464 10.000,1.0543,0.04636,0.03722,-0.0317,0.2991,0.6512 10.250,1.0431,0.04948,0.04055,-0.0307,0.2933,0.6550 10.500,1.0426,0.05187,0.04303,-0.0302,0.2878,0.6595 10.750,1.0606,0.05269,0.04380,-0.0301,0.2835,0.6649 11.000,1.0593,0.05538,0.04657,-0.0300,0.2784,0.6694 11.250,1.0483,0.05910,0.05042,-0.0299,0.2725,0.6732 11.500,1.0611,0.06025,0.05161,-0.0295,0.2682,0.6778 11.750,1.0700,0.06192,0.05330,-0.0292,0.2640,0.6827 12.000,1.0403,0.06795,0.05958,-0.0296,0.2573,0.6858 12.250,1.0533,0.06936,0.06098,-0.0296,0.2531,0.6917 12.500,1.0805,0.06926,0.06077,-0.0296,0.2499,0.6987 12.750,1.0233,0.07915,0.07101,-0.0313,0.2416,0.7000 13.000,1.0412,0.08003,0.07187,-0.0314,0.2380,0.7058 13.250,1.0732,0.07894,0.07072,-0.0307,0.2356,0.7128 13.500,0.9932,0.09256,0.08473,-0.0340,0.2256,0.7121 13.750,1.0214,0.09197,0.08409,-0.0336,0.2232,0.7201 14.250,0.9706,0.10594,0.09833,-0.0378,0.2103,0.7276 14.500,1.0054,0.10432,0.09665,-0.0371,0.2089,0.7364 15.000,0.9572,0.11832,0.11092,-0.0418,0.1961,0.7436 15.250,0.9919,0.11655,0.10910,-0.0410,0.1952,0.7539 15.750,0.9518,0.13011,0.12288,-0.0466,0.1830,0.7632