Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rae100-il-100000-n5 Airfoil,rae100-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,35.235 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-rae100-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.750,-0.7911,0.09882,0.09340,-0.0011,1.0000,0.0333 -12.500,-0.8322,0.08482,0.07932,-0.0107,1.0000,0.0328 -12.250,-0.8675,0.07390,0.06826,-0.0191,1.0000,0.0323 -12.000,-0.8957,0.06595,0.06013,-0.0251,1.0000,0.0321 -11.750,-0.9205,0.05982,0.05378,-0.0288,1.0000,0.0320 -11.500,-0.9406,0.05520,0.04892,-0.0301,1.0000,0.0320 -11.250,-0.9584,0.05143,0.04488,-0.0294,1.0000,0.0322 -11.000,-0.9716,0.04826,0.04142,-0.0274,1.0000,0.0326 -10.750,-0.9770,0.04512,0.03790,-0.0256,1.0000,0.0330 -10.500,-0.9771,0.04222,0.03459,-0.0239,1.0000,0.0339 -10.250,-0.9661,0.04044,0.03278,-0.0228,1.0000,0.0351 -10.000,-0.9545,0.03878,0.03100,-0.0217,1.0000,0.0364 -9.750,-0.9424,0.03686,0.02885,-0.0204,1.0000,0.0379 -9.500,-0.9287,0.03478,0.02646,-0.0191,1.0000,0.0395 -9.250,-0.9129,0.03280,0.02413,-0.0178,1.0000,0.0411 -9.000,-0.8962,0.03120,0.02247,-0.0168,1.0000,0.0431 -8.750,-0.8781,0.02998,0.02119,-0.0159,1.0000,0.0455 -8.500,-0.8591,0.02862,0.01964,-0.0148,1.0000,0.0484 -8.250,-0.8395,0.02722,0.01804,-0.0137,1.0000,0.0511 -8.000,-0.8207,0.02606,0.01690,-0.0127,1.0000,0.0544 -7.750,-0.8005,0.02502,0.01574,-0.0117,1.0000,0.0587 -7.500,-0.7807,0.02388,0.01452,-0.0105,1.0000,0.0628 -7.250,-0.7605,0.02296,0.01357,-0.0095,1.0000,0.0682 -7.000,-0.7400,0.02201,0.01256,-0.0084,1.0000,0.0745 -6.750,-0.7193,0.02116,0.01167,-0.0074,1.0000,0.0821 -6.500,-0.6987,0.02031,0.01083,-0.0063,1.0000,0.0911 -6.250,-0.6777,0.01953,0.01005,-0.0052,1.0000,0.1023 -6.000,-0.6565,0.01879,0.00934,-0.0042,1.0000,0.1163 -5.750,-0.6352,0.01809,0.00868,-0.0032,1.0000,0.1335 -5.500,-0.6135,0.01745,0.00809,-0.0022,1.0000,0.1550 -5.250,-0.5922,0.01681,0.00757,-0.0012,1.0000,0.1803 -5.000,-0.5707,0.01623,0.00711,-0.0002,1.0000,0.2089 -4.750,-0.5491,0.01571,0.00669,0.0009,1.0000,0.2412 -4.500,-0.5274,0.01523,0.00633,0.0019,1.0000,0.2749 -4.250,-0.5059,0.01478,0.00602,0.0031,1.0000,0.3099 -4.000,-0.4842,0.01438,0.00574,0.0042,1.0000,0.3455 -3.750,-0.4625,0.01403,0.00550,0.0054,1.0000,0.3811 -3.500,-0.4409,0.01370,0.00530,0.0066,1.0000,0.4160 -3.250,-0.4193,0.01341,0.00514,0.0078,1.0000,0.4503 -3.000,-0.3978,0.01315,0.00499,0.0091,1.0000,0.4843 -2.750,-0.3764,0.01292,0.00487,0.0104,1.0000,0.5175 -2.500,-0.3552,0.01272,0.00479,0.0118,1.0000,0.5500 -2.250,-0.3343,0.01255,0.00474,0.0132,1.0000,0.5820 -2.000,-0.3137,0.01241,0.00470,0.0147,1.0000,0.6136 -1.750,-0.2795,0.01229,0.00472,0.0134,0.9908,0.6489 -1.500,-0.2399,0.01219,0.00473,0.0112,0.9774,0.6850 -1.250,-0.2002,0.01210,0.00474,0.0091,0.9634,0.7199 -0.750,-0.1217,0.01193,0.00476,0.0055,0.9321,0.7859 -0.500,-0.0820,0.01188,0.00478,0.0038,0.9139,0.8168 -0.250,-0.0408,0.01184,0.00479,0.0018,0.8944,0.8453 0.000,0.0000,0.01183,0.00481,0.0000,0.8709,0.8709 0.250,0.0408,0.01184,0.00480,-0.0018,0.8453,0.8944 0.500,0.0820,0.01188,0.00478,-0.0038,0.8168,0.9139 0.750,0.1217,0.01193,0.00476,-0.0055,0.7860,0.9320 1.250,0.2002,0.01210,0.00474,-0.0091,0.7200,0.9634 1.500,0.2399,0.01219,0.00473,-0.0112,0.6849,0.9774 1.750,0.2795,0.01229,0.00472,-0.0134,0.6490,0.9908 2.000,0.3138,0.01241,0.00470,-0.0147,0.6137,1.0000 2.250,0.3344,0.01255,0.00472,-0.0132,0.5820,1.0000 2.500,0.3554,0.01272,0.00479,-0.0118,0.5500,1.0000 2.750,0.3765,0.01292,0.00487,-0.0105,0.5174,1.0000 3.000,0.3979,0.01315,0.00499,-0.0092,0.4843,1.0000 3.250,0.4194,0.01341,0.00514,-0.0079,0.4503,1.0000 3.500,0.4410,0.01370,0.00530,-0.0066,0.4158,1.0000 3.750,0.4626,0.01403,0.00550,-0.0054,0.3811,1.0000 4.000,0.4844,0.01438,0.00574,-0.0042,0.3455,1.0000 4.250,0.5060,0.01478,0.00602,-0.0031,0.3098,1.0000 4.500,0.5275,0.01523,0.00633,-0.0020,0.2750,1.0000 4.750,0.5492,0.01571,0.00669,-0.0009,0.2412,1.0000 5.000,0.5708,0.01623,0.00711,0.0001,0.2090,1.0000 5.250,0.5923,0.01681,0.00757,0.0012,0.1802,1.0000 5.500,0.6136,0.01745,0.00809,0.0022,0.1549,1.0000 5.750,0.6353,0.01809,0.00868,0.0032,0.1336,1.0000 6.000,0.6565,0.01879,0.00934,0.0042,0.1162,1.0000 6.250,0.6777,0.01953,0.01005,0.0052,0.1023,1.0000 6.500,0.6987,0.02031,0.01083,0.0063,0.0911,1.0000 6.750,0.7193,0.02116,0.01167,0.0074,0.0820,1.0000 7.000,0.7399,0.02201,0.01256,0.0084,0.0745,1.0000 7.250,0.7604,0.02296,0.01357,0.0095,0.0682,1.0000 7.500,0.7806,0.02388,0.01451,0.0105,0.0628,1.0000 7.750,0.8004,0.02502,0.01573,0.0117,0.0587,1.0000 8.000,0.8206,0.02605,0.01690,0.0127,0.0543,1.0000 8.250,0.8393,0.02721,0.01803,0.0137,0.0510,1.0000 8.500,0.8589,0.02862,0.01964,0.0148,0.0484,1.0000 8.750,0.8779,0.02999,0.02120,0.0159,0.0457,1.0000 9.000,0.8959,0.03120,0.02248,0.0169,0.0431,1.0000 9.250,0.9127,0.03280,0.02412,0.0179,0.0412,1.0000 9.500,0.9285,0.03477,0.02644,0.0192,0.0396,1.0000 9.750,0.9421,0.03687,0.02885,0.0205,0.0380,1.0000 10.000,0.9542,0.03880,0.03102,0.0217,0.0365,1.0000 10.250,0.9660,0.04039,0.03273,0.0229,0.0350,1.0000 10.500,0.9766,0.04223,0.03462,0.0240,0.0340,1.0000 10.750,0.9771,0.04508,0.03785,0.0256,0.0331,1.0000 11.000,0.9713,0.04826,0.04141,0.0274,0.0325,1.0000 11.250,0.9587,0.05139,0.04484,0.0295,0.0323,1.0000 11.500,0.9416,0.05509,0.04880,0.0301,0.0321,1.0000 11.750,0.9205,0.05980,0.05376,0.0288,0.0320,1.0000 12.000,0.8961,0.06589,0.06008,0.0251,0.0321,1.0000 12.250,0.8690,0.07366,0.06801,0.0193,0.0324,1.0000 12.500,0.8351,0.08426,0.07876,0.0112,0.0328,1.0000 12.750,0.7937,0.09825,0.09283,0.0015,0.0333,1.0000