Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-usa46-il-1000000 Airfoil,usa46-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,97.2523 Max Cl/Cd alpha,2.25 Url,http://airfoiltools.com/polar/csv?polar=xf-usa46-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.7109,0.02778,0.02533,-0.0583,1.0000,0.0065 -8.750,-0.6949,0.02441,0.02160,-0.0591,1.0000,0.0067 -8.500,-0.6762,0.02192,0.01879,-0.0592,1.0000,0.0069 -8.250,-0.6548,0.02043,0.01708,-0.0589,1.0000,0.0071 -8.000,-0.6323,0.01932,0.01580,-0.0585,1.0000,0.0072 -7.750,-0.6139,0.01622,0.01223,-0.0582,1.0000,0.0075 -7.500,-0.5933,0.01404,0.00972,-0.0576,1.0000,0.0079 -7.250,-0.5700,0.01310,0.00865,-0.0570,1.0000,0.0084 -7.000,-0.5461,0.01246,0.00792,-0.0564,1.0000,0.0090 -6.750,-0.5219,0.01198,0.00737,-0.0558,1.0000,0.0097 -6.500,-0.4977,0.01149,0.00679,-0.0551,1.0000,0.0104 -6.250,-0.4734,0.01107,0.00630,-0.0544,1.0000,0.0109 -6.000,-0.4500,0.01005,0.00510,-0.0536,1.0000,0.0118 -5.750,-0.4261,0.00946,0.00444,-0.0528,1.0000,0.0133 -5.500,-0.4021,0.00913,0.00406,-0.0520,1.0000,0.0147 -5.250,-0.3730,0.00885,0.00373,-0.0523,0.9993,0.0161 -5.000,-0.3389,0.00834,0.00321,-0.0537,0.9975,0.0213 -4.750,-0.3043,0.00802,0.00290,-0.0552,0.9955,0.0282 -4.500,-0.2696,0.00792,0.00279,-0.0567,0.9935,0.0325 -4.250,-0.2367,0.00759,0.00247,-0.0578,0.9905,0.0392 -4.000,-0.2027,0.00746,0.00233,-0.0591,0.9875,0.0433 -3.750,-0.1676,0.00719,0.00205,-0.0606,0.9847,0.0492 -3.500,-0.1332,0.00699,0.00185,-0.0620,0.9805,0.0551 -3.250,-0.0993,0.00673,0.00163,-0.0632,0.9739,0.0663 -3.000,-0.0639,0.00648,0.00143,-0.0648,0.9672,0.0821 -2.750,-0.0292,0.00621,0.00129,-0.0663,0.9575,0.1133 -2.500,0.0056,0.00608,0.00118,-0.0677,0.9439,0.1333 -2.250,0.0379,0.00599,0.00108,-0.0685,0.9249,0.1449 -2.000,0.0666,0.00597,0.00100,-0.0684,0.9046,0.1543 -1.750,0.0938,0.00596,0.00092,-0.0681,0.8850,0.1626 -1.500,0.1205,0.00594,0.00086,-0.0676,0.8649,0.1703 -1.250,0.1470,0.00596,0.00080,-0.0671,0.8435,0.1778 -1.000,0.1736,0.00593,0.00075,-0.0667,0.8228,0.1898 -0.750,0.2003,0.00590,0.00071,-0.0663,0.8032,0.2056 -0.500,0.2267,0.00581,0.00067,-0.0659,0.7818,0.2427 -0.250,0.2521,0.00548,0.00065,-0.0655,0.7580,0.3777 0.000,0.2767,0.00505,0.00068,-0.0650,0.7328,0.5632 0.250,0.3012,0.00485,0.00074,-0.0642,0.7055,0.6844 0.500,0.3265,0.00488,0.00079,-0.0635,0.6738,0.7423 0.750,0.3524,0.00497,0.00083,-0.0629,0.6429,0.7726 1.000,0.3783,0.00505,0.00087,-0.0623,0.6138,0.7955 1.250,0.4041,0.00512,0.00091,-0.0617,0.5860,0.8184 1.500,0.4292,0.00513,0.00095,-0.0610,0.5620,0.8507 1.750,0.4668,0.00502,0.00099,-0.0631,0.5299,1.0000 2.000,0.4936,0.00518,0.00106,-0.0627,0.5062,1.0000 2.250,0.5203,0.00535,0.00114,-0.0624,0.4783,1.0000 2.500,0.5459,0.00566,0.00123,-0.0620,0.4190,1.0000 2.750,0.5705,0.00612,0.00137,-0.0614,0.3465,1.0000 3.000,0.5963,0.00645,0.00153,-0.0610,0.3079,1.0000 3.250,0.6225,0.00672,0.00169,-0.0607,0.2765,1.0000 3.500,0.6486,0.00699,0.00184,-0.0604,0.2441,1.0000 3.750,0.6740,0.00739,0.00203,-0.0599,0.1967,1.0000 4.000,0.6953,0.00845,0.00251,-0.0591,0.0727,1.0000 4.250,0.7192,0.00918,0.00298,-0.0583,0.0198,1.0000 4.500,0.7451,0.00954,0.00334,-0.0579,0.0161,1.0000 4.750,0.7705,0.01004,0.00394,-0.0572,0.0138,1.0000 5.000,0.7965,0.01037,0.00431,-0.0568,0.0132,1.0000 5.250,0.8221,0.01075,0.00472,-0.0563,0.0119,1.0000 5.500,0.8474,0.01119,0.00520,-0.0558,0.0109,1.0000 5.750,0.8717,0.01180,0.00586,-0.0551,0.0101,1.0000 6.000,0.8931,0.01295,0.00714,-0.0539,0.0093,1.0000 6.250,0.9152,0.01396,0.00824,-0.0528,0.0089,1.0000 6.500,0.9398,0.01447,0.00881,-0.0522,0.0085,1.0000 6.750,0.9633,0.01525,0.00966,-0.0514,0.0081,1.0000 7.000,0.9856,0.01631,0.01083,-0.0504,0.0077,1.0000 7.250,1.0081,0.01733,0.01193,-0.0494,0.0073,1.0000 7.500,1.0310,0.01819,0.01286,-0.0487,0.0070,1.0000 7.750,1.0537,0.01903,0.01378,-0.0479,0.0066,1.0000 8.000,1.0751,0.02026,0.01512,-0.0470,0.0065,1.0000 8.250,1.0956,0.02169,0.01667,-0.0459,0.0063,1.0000 8.500,1.1145,0.02353,0.01870,-0.0447,0.0062,1.0000 8.750,1.1311,0.02584,0.02122,-0.0433,0.0061,1.0000 9.000,1.1435,0.02902,0.02469,-0.0415,0.0060,1.0000 9.250,1.1489,0.03332,0.02941,-0.0392,0.0059,1.0000 9.500,1.1433,0.03902,0.03559,-0.0361,0.0058,1.0000 9.750,1.1403,0.04310,0.03999,-0.0335,0.0058,1.0000 10.000,1.1394,0.04606,0.04316,-0.0313,0.0058,1.0000 10.250,1.1303,0.04923,0.04655,-0.0285,0.0059,1.0000 10.500,1.1227,0.05107,0.04851,-0.0254,0.0059,1.0000 10.750,0.9061,0.07024,0.06848,-0.0305,0.0090,1.0000 11.000,0.8853,0.07842,0.07676,-0.0355,0.0090,1.0000