Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-sa7035-il-100000-n5 Airfoil,sa7035-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,53.3273 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-sa7035-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.4102,0.08661,0.08177,-0.0347,1.0000,0.0247 -8.250,-0.4091,0.08341,0.07861,-0.0344,1.0000,0.0240 -8.000,-0.4124,0.07959,0.07488,-0.0359,1.0000,0.0239 -7.750,-0.4164,0.07650,0.07187,-0.0363,1.0000,0.0233 -7.500,-0.4232,0.07267,0.06813,-0.0380,1.0000,0.0229 -7.250,-0.4283,0.06831,0.06380,-0.0406,1.0000,0.0227 -7.000,-0.4324,0.06437,0.05987,-0.0417,1.0000,0.0220 -6.750,-0.4371,0.05996,0.05542,-0.0427,1.0000,0.0217 -6.500,-0.4400,0.05567,0.05103,-0.0430,1.0000,0.0212 -6.250,-0.4404,0.05134,0.04653,-0.0430,1.0000,0.0209 -6.000,-0.4381,0.04677,0.04171,-0.0427,1.0000,0.0203 -5.750,-0.4318,0.04232,0.03691,-0.0423,1.0000,0.0197 -5.500,-0.4217,0.03795,0.03208,-0.0417,1.0000,0.0192 -5.250,-0.3918,0.03303,0.02642,-0.0442,0.9953,0.0188 -5.000,-0.3597,0.02948,0.02225,-0.0461,0.9901,0.0188 -4.750,-0.3258,0.02672,0.01896,-0.0479,0.9853,0.0190 -4.500,-0.2924,0.02453,0.01637,-0.0492,0.9804,0.0195 -4.250,-0.2585,0.02269,0.01418,-0.0504,0.9750,0.0205 -4.000,-0.2218,0.02117,0.01241,-0.0522,0.9707,0.0220 -3.750,-0.1901,0.02002,0.01108,-0.0529,0.9637,0.0255 -3.500,-0.1543,0.01889,0.00991,-0.0547,0.9585,0.0299 -3.250,-0.1218,0.01787,0.00873,-0.0556,0.9515,0.0368 -3.000,-0.0863,0.01681,0.00776,-0.0572,0.9456,0.0670 -2.750,-0.0543,0.01556,0.00717,-0.0586,0.9390,0.1914 -2.500,-0.0228,0.01458,0.00687,-0.0598,0.9319,0.3634 -2.250,0.0066,0.01394,0.00669,-0.0601,0.9238,0.5050 -2.000,0.0368,0.01346,0.00655,-0.0599,0.9163,0.6355 -1.750,0.0619,0.01314,0.00645,-0.0584,0.9065,0.7374 -1.500,0.0926,0.01287,0.00630,-0.0577,0.8991,0.8296 -1.250,0.1329,0.01269,0.00608,-0.0592,0.8907,0.9120 -1.000,0.1889,0.01249,0.00571,-0.0645,0.8848,0.9759 -0.750,0.2293,0.01237,0.00541,-0.0670,0.8743,1.0000 -0.500,0.2558,0.01233,0.00520,-0.0666,0.8611,1.0000 -0.250,0.2823,0.01229,0.00502,-0.0662,0.8476,1.0000 0.000,0.3090,0.01226,0.00486,-0.0657,0.8336,1.0000 0.250,0.3356,0.01224,0.00471,-0.0653,0.8190,1.0000 0.500,0.3623,0.01222,0.00459,-0.0647,0.8040,1.0000 0.750,0.3891,0.01222,0.00448,-0.0642,0.7885,1.0000 1.000,0.4152,0.01225,0.00441,-0.0636,0.7716,1.0000 1.250,0.4413,0.01229,0.00437,-0.0630,0.7539,1.0000 1.500,0.4676,0.01234,0.00432,-0.0624,0.7359,1.0000 1.750,0.4940,0.01241,0.00429,-0.0618,0.7177,1.0000 2.000,0.5196,0.01252,0.00432,-0.0611,0.6978,1.0000 2.250,0.5455,0.01265,0.00437,-0.0604,0.6781,1.0000 2.500,0.5712,0.01280,0.00444,-0.0598,0.6580,1.0000 2.750,0.5967,0.01297,0.00453,-0.0592,0.6371,1.0000 3.000,0.6222,0.01316,0.00465,-0.0585,0.6166,1.0000 3.250,0.6474,0.01337,0.00483,-0.0579,0.5949,1.0000 3.500,0.6725,0.01361,0.00499,-0.0572,0.5734,1.0000 3.750,0.6973,0.01386,0.00519,-0.0565,0.5507,1.0000 4.000,0.7220,0.01413,0.00541,-0.0558,0.5280,1.0000 4.250,0.7465,0.01444,0.00568,-0.0551,0.5058,1.0000 4.500,0.7710,0.01475,0.00597,-0.0545,0.4831,1.0000 4.750,0.7952,0.01509,0.00627,-0.0538,0.4610,1.0000 5.000,0.8192,0.01545,0.00661,-0.0531,0.4382,1.0000 5.250,0.8429,0.01583,0.00701,-0.0524,0.4153,1.0000 5.500,0.8662,0.01626,0.00739,-0.0516,0.3925,1.0000 5.750,0.8895,0.01668,0.00783,-0.0509,0.3689,1.0000 6.000,0.9124,0.01715,0.00829,-0.0501,0.3460,1.0000 6.250,0.9349,0.01765,0.00881,-0.0493,0.3233,1.0000 6.500,0.9573,0.01817,0.00936,-0.0485,0.3009,1.0000 6.750,0.9789,0.01876,0.00993,-0.0476,0.2789,1.0000 7.000,1.0004,0.01935,0.01055,-0.0468,0.2557,1.0000 7.250,1.0212,0.02000,0.01121,-0.0458,0.2324,1.0000 7.500,1.0410,0.02073,0.01191,-0.0448,0.2096,1.0000 7.750,1.0610,0.02146,0.01272,-0.0439,0.1866,1.0000 8.000,1.0800,0.02228,0.01355,-0.0428,0.1655,1.0000 8.250,1.0981,0.02317,0.01445,-0.0417,0.1447,1.0000 8.500,1.1155,0.02413,0.01544,-0.0404,0.1258,1.0000 8.750,1.1319,0.02518,0.01652,-0.0391,0.1068,1.0000 9.000,1.1463,0.02638,0.01771,-0.0376,0.0911,1.0000 9.250,1.1592,0.02768,0.01905,-0.0360,0.0771,1.0000 9.500,1.1706,0.02908,0.02047,-0.0343,0.0654,1.0000 9.750,1.1816,0.03045,0.02197,-0.0324,0.0552,1.0000 10.000,1.1898,0.03193,0.02357,-0.0303,0.0480,1.0000 10.250,1.1922,0.03367,0.02530,-0.0277,0.0426,1.0000 10.500,1.1984,0.03529,0.02715,-0.0255,0.0377,1.0000 10.750,1.2006,0.03719,0.02918,-0.0233,0.0346,1.0000 11.000,1.1988,0.03956,0.03161,-0.0212,0.0320,1.0000 11.250,1.2025,0.04164,0.03395,-0.0197,0.0290,1.0000 11.500,1.2034,0.04394,0.03641,-0.0184,0.0267,1.0000 11.750,1.2017,0.04660,0.03920,-0.0173,0.0250,1.0000 12.000,1.1979,0.04974,0.04244,-0.0165,0.0239,1.0000 12.250,1.1963,0.05297,0.04586,-0.0159,0.0230,1.0000 12.500,1.1938,0.05639,0.04963,-0.0156,0.0217,1.0000 12.750,1.1891,0.06011,0.05361,-0.0160,0.0206,1.0000 13.000,1.1825,0.06417,0.05788,-0.0169,0.0195,1.0000 13.250,1.1753,0.06853,0.06244,-0.0181,0.0189,1.0000 13.500,1.1665,0.07333,0.06742,-0.0200,0.0183,1.0000 13.750,1.1564,0.07851,0.07277,-0.0223,0.0178,1.0000 14.000,1.1450,0.08421,0.07864,-0.0250,0.0175,1.0000 14.250,1.1325,0.09044,0.08505,-0.0282,0.0173,1.0000 14.500,1.1186,0.09730,0.09211,-0.0319,0.0173,1.0000 14.750,1.1029,0.10493,0.09993,-0.0363,0.0172,1.0000 15.000,1.0844,0.11371,0.10892,-0.0417,0.0173,1.0000 15.250,1.0584,0.12524,0.12069,-0.0489,0.0179,1.0000 15.500,1.0110,0.14445,0.14008,-0.0603,0.0205,1.0000