Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-fx69h083-il-50000 Airfoil,fx69h083-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,36.3167 Max Cl/Cd alpha,6.75 Url,http://airfoiltools.com/polar/csv?polar=xf-fx69h083-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.4969,0.10319,0.09698,-0.0019,1.0000,0.2055 -8.000,-0.5028,0.10081,0.09469,-0.0043,1.0000,0.2160 -7.750,-0.4945,0.09677,0.09069,-0.0040,1.0000,0.2291 -7.500,-0.4906,0.09318,0.08717,-0.0042,1.0000,0.2427 -7.250,-0.4912,0.08998,0.08404,-0.0056,1.0000,0.2574 -7.000,-0.4878,0.08629,0.08043,-0.0060,1.0000,0.2739 -6.750,-0.4774,0.08275,0.07693,-0.0040,1.0000,0.2980 -6.500,-0.4740,0.07967,0.07392,-0.0028,1.0000,0.3268 -6.250,-0.4622,0.07635,0.07065,0.0017,1.0000,0.3668 -6.000,-0.4623,0.07396,0.06830,0.0050,1.0000,0.4117 -5.750,-0.4366,0.07027,0.06463,0.0126,1.0000,0.4721 -5.500,-0.4011,0.06672,0.06100,0.0198,1.0000,0.5609 -5.000,-0.2403,0.05435,0.04818,0.0207,1.0000,0.8484 -4.750,-0.2851,0.05422,0.04828,0.0245,1.0000,0.7775 -4.500,-0.3467,0.05374,0.04819,0.0256,1.0000,0.6812 -4.250,-0.3904,0.04563,0.03856,-0.0233,1.0000,0.2301 -4.000,-0.3573,0.04039,0.03241,-0.0249,1.0000,0.1563 -3.750,-0.3323,0.03724,0.02834,-0.0240,1.0000,0.1323 -3.500,-0.3113,0.03429,0.02509,-0.0230,1.0000,0.1254 -3.250,-0.2890,0.03208,0.02242,-0.0220,1.0000,0.1252 -3.000,-0.2655,0.03011,0.02004,-0.0211,1.0000,0.1268 -2.750,-0.2399,0.02821,0.01772,-0.0202,1.0000,0.1258 -2.500,-0.2137,0.02659,0.01574,-0.0194,1.0000,0.1276 -2.250,-0.1865,0.02527,0.01402,-0.0187,1.0000,0.1325 -2.000,-0.1588,0.02400,0.01274,-0.0184,1.0000,0.1501 -1.750,-0.1309,0.02288,0.01156,-0.0180,1.0000,0.1740 -1.500,-0.0694,0.01811,0.00953,-0.0213,1.0000,1.0000 -1.250,-0.0539,0.01836,0.00929,-0.0197,1.0000,1.0000 -1.000,-0.0380,0.01865,0.00917,-0.0184,1.0000,1.0000 -0.750,-0.0215,0.01898,0.00920,-0.0173,1.0000,1.0000 -0.500,-0.0046,0.01934,0.00930,-0.0164,1.0000,1.0000 -0.250,0.0126,0.01976,0.00949,-0.0157,1.0000,1.0000 0.000,0.0299,0.02022,0.00974,-0.0151,1.0000,1.0000 0.250,0.0474,0.02072,0.01007,-0.0146,1.0000,1.0000 0.500,0.0650,0.02128,0.01044,-0.0142,1.0000,1.0000 0.750,0.0826,0.02189,0.01092,-0.0140,1.0000,1.0000 1.000,0.1104,0.02266,0.01157,-0.0158,0.9960,1.0000 1.250,0.1651,0.02376,0.01254,-0.0226,0.9816,1.0000 1.500,0.2134,0.02475,0.01345,-0.0280,0.9659,1.0000 1.750,0.2590,0.02571,0.01438,-0.0328,0.9499,1.0000 2.000,0.3034,0.02664,0.01532,-0.0372,0.9336,1.0000 2.250,0.3479,0.02755,0.01628,-0.0414,0.9173,1.0000 2.500,0.3936,0.02841,0.01722,-0.0456,0.9013,1.0000 2.750,0.4241,0.02923,0.01812,-0.0470,0.8832,1.0000 3.000,0.4609,0.03001,0.01901,-0.0493,0.8654,1.0000 3.250,0.5040,0.03067,0.01988,-0.0523,0.8482,1.0000 3.500,0.5403,0.03132,0.02069,-0.0541,0.8303,1.0000 3.750,0.5682,0.03204,0.02156,-0.0543,0.8116,1.0000 4.000,0.6021,0.03259,0.02237,-0.0552,0.7945,1.0000 4.250,0.6362,0.03307,0.02307,-0.0558,0.7783,1.0000 4.500,0.6597,0.03379,0.02399,-0.0551,0.7599,1.0000 4.750,0.6869,0.03423,0.02466,-0.0543,0.7409,1.0000 5.000,0.7234,0.03394,0.02468,-0.0536,0.7230,1.0000 5.250,0.7459,0.03418,0.02524,-0.0516,0.7007,1.0000 5.500,0.7833,0.03296,0.02436,-0.0493,0.6799,1.0000 5.750,0.8148,0.03155,0.02328,-0.0457,0.6541,1.0000 6.000,0.8435,0.03026,0.02232,-0.0420,0.6267,1.0000 6.250,0.8687,0.02899,0.02146,-0.0378,0.5931,1.0000 6.500,0.8895,0.02491,0.01730,-0.0287,0.5152,1.0000 6.750,0.8854,0.02438,0.01604,-0.0204,0.3461,1.0000 7.000,0.8715,0.02866,0.01826,-0.0149,0.1684,1.0000 7.250,0.8826,0.03206,0.02113,-0.0121,0.1247,1.0000 7.500,0.9062,0.03454,0.02351,-0.0105,0.1030,1.0000 7.750,0.9400,0.03768,0.02663,-0.0098,0.0933,1.0000 8.000,0.9674,0.04075,0.02988,-0.0090,0.0858,1.0000 8.250,0.9888,0.04434,0.03390,-0.0079,0.0809,1.0000 8.500,1.0066,0.04797,0.03809,-0.0063,0.0795,1.0000 8.750,1.0206,0.05206,0.04269,-0.0047,0.0798,1.0000 9.000,1.0307,0.05645,0.04753,-0.0032,0.0807,1.0000 9.250,1.0390,0.06122,0.05265,-0.0018,0.0820,1.0000 9.500,1.0444,0.06575,0.05758,-0.0003,0.0840,1.0000 9.750,1.0204,0.06979,0.06240,0.0021,0.0873,1.0000 10.000,1.0002,0.07457,0.06753,0.0032,0.0897,1.0000 10.250,0.9795,0.07912,0.07226,0.0040,0.0915,1.0000 10.500,0.9602,0.08405,0.07731,0.0036,0.0931,1.0000 10.750,0.9646,0.08967,0.08299,0.0034,0.0969,1.0000 11.000,0.9242,0.09578,0.08921,-0.0009,0.0976,1.0000 11.250,0.8729,0.10734,0.10076,-0.0119,0.1004,1.0000 11.500,0.8573,0.11687,0.11015,-0.0177,0.1062,1.0000 11.750,0.8371,0.12745,0.12062,-0.0252,0.1169,1.0000