Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-s4096-il-200000-n5 Airfoil,s4096-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,48.2857 Max Cl/Cd alpha,7.75 Url,http://airfoiltools.com/polar/csv?polar=xf-s4096-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.7035,0.10396,0.10053,0.0075,1.0011,0.0179 -9.500,-0.7713,0.07419,0.07055,-0.0129,1.0011,0.0167 -9.250,-0.7861,0.06224,0.05802,-0.0191,1.0011,0.0168 -9.000,-0.7818,0.05390,0.04903,-0.0224,1.0011,0.0170 -8.750,-0.7657,0.04812,0.04272,-0.0244,1.0011,0.0171 -8.500,-0.7441,0.04361,0.03773,-0.0260,1.0011,0.0173 -8.250,-0.7194,0.04020,0.03391,-0.0274,1.0011,0.0175 -8.000,-0.6929,0.03742,0.03078,-0.0285,1.0011,0.0178 -7.750,-0.6653,0.03505,0.02808,-0.0295,1.0011,0.0182 -7.500,-0.6370,0.03298,0.02571,-0.0304,1.0011,0.0185 -7.250,-0.6083,0.03127,0.02374,-0.0312,1.0011,0.0191 -7.000,-0.5793,0.02987,0.02211,-0.0319,1.0011,0.0200 -6.750,-0.5499,0.02844,0.02044,-0.0326,1.0011,0.0208 -6.500,-0.5204,0.02707,0.01886,-0.0332,1.0011,0.0212 -6.250,-0.4910,0.02587,0.01749,-0.0338,1.0011,0.0215 -6.000,-0.4614,0.02484,0.01634,-0.0344,1.0011,0.0219 -5.750,-0.4322,0.02364,0.01511,-0.0351,1.0011,0.0225 -5.500,-0.4026,0.02276,0.01420,-0.0358,1.0011,0.0232 -5.250,-0.3729,0.02206,0.01346,-0.0365,1.0011,0.0241 -5.000,-0.3430,0.02147,0.01283,-0.0373,1.0011,0.0254 -4.750,-0.3130,0.02096,0.01228,-0.0380,1.0011,0.0272 -4.500,-0.2828,0.02042,0.01169,-0.0387,1.0011,0.0288 -4.250,-0.2526,0.01994,0.01119,-0.0395,1.0011,0.0309 -4.000,-0.2223,0.01956,0.01077,-0.0403,1.0011,0.0341 -3.750,-0.1920,0.01916,0.01040,-0.0410,1.0011,0.0419 -3.500,-0.1617,0.01869,0.01009,-0.0419,1.0011,0.0726 -3.250,-0.1316,0.01818,0.00990,-0.0430,1.0011,0.1391 -3.000,-0.1016,0.01769,0.00983,-0.0441,1.0011,0.2278 -2.750,-0.0716,0.01737,0.00983,-0.0451,1.0011,0.3069 -2.500,-0.0388,0.01728,0.01005,-0.0467,0.9884,0.3918 -2.250,-0.0035,0.01691,0.01021,-0.0489,0.9578,0.5191 -2.000,0.0284,0.01661,0.01036,-0.0497,0.9258,0.6400 -1.750,0.0535,0.01637,0.01046,-0.0486,0.8943,0.7497 -1.500,0.0714,0.01603,0.01036,-0.0451,0.8659,0.8780 -1.250,0.1006,0.01518,0.00942,-0.0449,0.8368,0.9989 -1.000,0.1292,0.01526,0.00930,-0.0449,0.8123,0.9989 -0.750,0.1580,0.01535,0.00919,-0.0451,0.7902,0.9989 -0.500,0.1871,0.01544,0.00911,-0.0454,0.7691,0.9989 -0.250,0.2164,0.01554,0.00904,-0.0458,0.7495,0.9989 0.000,0.2459,0.01565,0.00898,-0.0462,0.7312,0.9989 0.250,0.2756,0.01576,0.00895,-0.0467,0.7134,0.9989 0.500,0.3053,0.01587,0.00893,-0.0472,0.6962,0.9989 0.750,0.3350,0.01598,0.00892,-0.0477,0.6796,0.9989 1.000,0.3648,0.01610,0.00893,-0.0483,0.6636,0.9989 1.250,0.3946,0.01623,0.00895,-0.0489,0.6479,0.9989 1.500,0.4244,0.01636,0.00898,-0.0494,0.6324,0.9989 1.750,0.4542,0.01649,0.00903,-0.0500,0.6169,0.9989 2.000,0.4840,0.01663,0.00908,-0.0506,0.6013,0.9989 2.250,0.5138,0.01678,0.00916,-0.0512,0.5856,0.9989 2.500,0.5435,0.01694,0.00924,-0.0518,0.5696,0.9989 2.750,0.5732,0.01710,0.00933,-0.0524,0.5535,0.9989 3.000,0.6028,0.01727,0.00944,-0.0530,0.5367,0.9989 3.250,0.6325,0.01744,0.00956,-0.0536,0.5191,0.9989 3.500,0.6621,0.01762,0.00968,-0.0542,0.5005,0.9989 3.750,0.6916,0.01782,0.00984,-0.0548,0.4811,0.9989 4.000,0.7210,0.01805,0.00999,-0.0554,0.4612,0.9989 4.250,0.7504,0.01828,0.01016,-0.0560,0.4402,0.9989 4.500,0.7796,0.01855,0.01036,-0.0565,0.4188,0.9989 4.750,0.8088,0.01883,0.01059,-0.0571,0.3981,0.9989 5.000,0.8378,0.01913,0.01083,-0.0577,0.3773,0.9989 5.250,0.8668,0.01947,0.01109,-0.0583,0.3567,0.9989 5.500,0.8957,0.01979,0.01140,-0.0589,0.3362,0.9989 5.750,0.9244,0.02016,0.01171,-0.0595,0.3158,0.9989 6.000,0.9531,0.02054,0.01204,-0.0601,0.2964,0.9989 6.250,0.9816,0.02093,0.01240,-0.0606,0.2766,0.9989 6.500,1.0099,0.02136,0.01280,-0.0612,0.2579,0.9989 6.750,1.0381,0.02181,0.01321,-0.0617,0.2402,0.9989 7.000,1.0663,0.02226,0.01364,-0.0623,0.2227,0.9989 7.250,1.0942,0.02274,0.01412,-0.0628,0.2053,0.9989 7.500,1.1218,0.02325,0.01461,-0.0633,0.1888,0.9989 7.750,1.1492,0.02380,0.01514,-0.0637,0.1725,0.9989 8.000,1.1764,0.02439,0.01571,-0.0642,0.1570,0.9989 8.250,1.2032,0.02499,0.01632,-0.0646,0.1425,0.9989 8.500,1.2299,0.02561,0.01694,-0.0649,0.1295,0.9989 8.750,1.2564,0.02624,0.01761,-0.0652,0.1180,0.9989 9.000,1.2825,0.02691,0.01832,-0.0655,0.1073,0.9989 9.250,1.3082,0.02763,0.01909,-0.0657,0.0973,0.9989 9.500,1.3332,0.02843,0.01991,-0.0659,0.0880,0.9989 9.750,1.3579,0.02923,0.02075,-0.0660,0.0787,0.9989 10.000,1.3822,0.03005,0.02161,-0.0660,0.0693,0.9989 10.250,1.4057,0.03094,0.02253,-0.0660,0.0603,0.9989 10.500,1.4283,0.03192,0.02353,-0.0659,0.0525,0.9989 10.750,1.4504,0.03290,0.02456,-0.0657,0.0456,0.9989 11.000,1.4721,0.03388,0.02564,-0.0654,0.0407,0.9989 11.250,1.4918,0.03506,0.02688,-0.0648,0.0358,0.9989 11.500,1.5116,0.03615,0.02809,-0.0643,0.0310,0.9989 11.750,1.5286,0.03751,0.02952,-0.0634,0.0263,0.9989 12.000,1.5431,0.03906,0.03115,-0.0622,0.0218,0.9989 12.250,1.5560,0.04064,0.03287,-0.0608,0.0181,0.9989 12.500,1.5643,0.04257,0.03491,-0.0588,0.0157,0.9989 12.750,1.5689,0.04464,0.03714,-0.0563,0.0140,0.9989 13.000,1.5628,0.04720,0.03984,-0.0524,0.0131,0.9989 13.250,1.5527,0.05030,0.04310,-0.0487,0.0125,0.9989 13.500,1.5452,0.05371,0.04671,-0.0464,0.0120,0.9989 13.750,1.5374,0.05758,0.05078,-0.0450,0.0115,0.9989 14.000,1.5291,0.06189,0.05528,-0.0445,0.0111,0.9989 14.250,1.5196,0.06668,0.06025,-0.0446,0.0108,0.9989 14.500,1.5087,0.07194,0.06570,-0.0453,0.0105,0.9989 14.750,1.4961,0.07768,0.07163,-0.0465,0.0103,0.9989 15.000,1.4814,0.08391,0.07805,-0.0482,0.0101,0.9989 15.250,1.4653,0.09056,0.08488,-0.0503,0.0100,0.9989 15.500,1.4480,0.09761,0.09211,-0.0528,0.0099,0.9989 15.750,1.4302,0.10495,0.09963,-0.0558,0.0099,0.9989