Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-eiffel10-il-1000000-n5 Airfoil,eiffel10-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,45.2443 Max Cl/Cd alpha,2.25 Url,http://airfoiltools.com/polar/csv?polar=xf-eiffel10-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.250,-0.5480,0.16059,0.15875,0.0196,1.0000,0.0064 -13.000,-0.5404,0.15750,0.15567,0.0182,1.0000,0.0065 -12.750,-0.5329,0.15439,0.15256,0.0169,1.0000,0.0067 -12.500,-0.5252,0.15123,0.14940,0.0155,1.0000,0.0069 -12.250,-0.5176,0.14808,0.14625,0.0142,1.0000,0.0071 -12.000,-0.5101,0.14495,0.14312,0.0129,1.0000,0.0071 -11.750,-0.5023,0.14183,0.14000,0.0116,1.0000,0.0072 -11.500,-0.4945,0.13874,0.13692,0.0102,1.0000,0.0072 -11.250,-0.4867,0.13569,0.13387,0.0089,1.0000,0.0072 -11.000,-0.4788,0.13265,0.13083,0.0076,1.0000,0.0072 -10.750,-0.4708,0.12963,0.12782,0.0062,1.0000,0.0072 -10.500,-0.4626,0.12663,0.12483,0.0048,1.0000,0.0073 -10.250,-0.4544,0.12365,0.12185,0.0035,1.0000,0.0073 -10.000,-0.4462,0.12070,0.11891,0.0021,1.0000,0.0073 -9.750,-0.4379,0.11775,0.11597,0.0007,1.0000,0.0073 -9.500,-0.4295,0.11484,0.11306,-0.0007,1.0000,0.0073 -9.250,-0.4209,0.11193,0.11016,-0.0021,1.0000,0.0073 -9.000,-0.4122,0.10904,0.10729,-0.0036,1.0000,0.0073 -8.750,-0.4035,0.10619,0.10444,-0.0051,1.0000,0.0073 -8.500,-0.3948,0.10335,0.10162,-0.0067,1.0000,0.0073 -8.250,-0.3864,0.10058,0.09887,-0.0082,1.0000,0.0073 -8.000,-0.3775,0.09782,0.09613,-0.0100,1.0000,0.0073 -7.750,-0.3563,0.09402,0.09228,-0.0153,0.9467,0.0073 -7.500,-0.3493,0.09146,0.08948,-0.0153,0.8798,0.0074 -7.250,-0.3364,0.08876,0.08665,-0.0173,0.8462,0.0075 -7.000,-0.3208,0.08598,0.08377,-0.0201,0.8219,0.0075 -6.750,-0.3034,0.08317,0.08086,-0.0232,0.7974,0.0076 -6.500,-0.2848,0.08041,0.07792,-0.0265,0.7529,0.0078 -6.250,-0.2646,0.07765,0.07492,-0.0301,0.6948,0.0079 -6.000,-0.2454,0.07690,0.07235,-0.0339,0.0258,0.0081 -5.750,-0.2218,0.07390,0.06932,-0.0380,0.0225,0.0084 -5.500,-0.1965,0.07085,0.06625,-0.0423,0.0211,0.0086 -5.250,-0.1696,0.06777,0.06314,-0.0468,0.0200,0.0087 -5.000,-0.1408,0.06469,0.06004,-0.0515,0.0190,0.0088 -4.750,-0.1103,0.06160,0.05692,-0.0563,0.0187,0.0089 -4.500,-0.0778,0.05852,0.05379,-0.0613,0.0184,0.0089 -4.250,-0.0436,0.05544,0.05067,-0.0664,0.0182,0.0090 -4.000,-0.0075,0.05236,0.04753,-0.0716,0.0174,0.0090 -3.750,0.0310,0.04926,0.04435,-0.0770,0.0164,0.0091 -3.500,0.0732,0.04607,0.04106,-0.0829,0.0158,0.0091 -3.250,0.1141,0.04319,0.03808,-0.0879,0.0152,0.0091 -2.750,0.1778,0.03826,0.03304,-0.0939,0.0140,0.0093 -2.500,0.2119,0.03630,0.03102,-0.0968,0.0134,0.0096 -2.250,0.2484,0.03427,0.02891,-0.0999,0.0132,0.0098 -2.000,0.2856,0.03226,0.02680,-0.1029,0.0129,0.0100 -1.750,0.3226,0.03035,0.02480,-0.1055,0.0128,0.0102 -1.500,0.3596,0.02855,0.02288,-0.1078,0.0128,0.0105 -1.250,0.3977,0.02677,0.02097,-0.1099,0.0128,0.0109 -0.250,0.5416,0.02047,0.01398,-0.1149,0.0133,0.0111 0.250,0.6034,0.01883,0.01202,-0.1164,0.0126,0.0117 0.750,0.6620,0.01873,0.01144,-0.1160,0.0120,0.0134 1.000,0.6901,0.01907,0.01161,-0.1158,0.0119,0.0134 1.500,0.7498,0.01763,0.01002,-0.1159,0.0116,0.0109 1.750,0.7780,0.01768,0.01002,-0.1156,0.0113,0.0110 2.000,0.8060,0.01791,0.01024,-0.1152,0.0109,0.0113 2.250,0.8334,0.01842,0.01080,-0.1147,0.0104,0.0117 2.500,0.8607,0.01905,0.01147,-0.1143,0.0100,0.0122 2.750,0.8877,0.01981,0.01226,-0.1138,0.0098,0.0132 3.000,0.9148,0.02062,0.01313,-0.1134,0.0096,0.0137 3.250,0.9418,0.02167,0.01427,-0.1129,0.0096,0.0140 3.500,0.9686,0.02312,0.01586,-0.1122,0.0096,0.0144 3.750,0.9956,0.02557,0.01857,-0.1110,0.0101,0.0152 4.000,1.0211,0.02769,0.02089,-0.1100,0.0107,0.0159 4.250,1.0443,0.02993,0.02330,-0.1093,0.0115,0.0175 4.500,1.0656,0.03268,0.02614,-0.1088,0.0117,0.0183 4.750,1.0882,0.03484,0.02846,-0.1079,0.0118,0.0194 5.000,1.1101,0.03705,0.03084,-0.1068,0.0118,0.0208 5.250,1.1311,0.03937,0.03334,-0.1057,0.0118,0.0242 5.750,1.1690,0.04302,0.03883,-0.1034,0.0118,1.0000 7.500,1.1909,0.05773,0.05500,-0.0817,0.0117,1.0000 7.750,1.1900,0.06202,0.05945,-0.0792,0.0117,1.0000 8.000,1.1849,0.06633,0.06391,-0.0766,0.0117,1.0000 8.250,1.1744,0.07064,0.06837,-0.0737,0.0116,1.0000 8.500,1.1540,0.07438,0.07223,-0.0698,0.0116,1.0000 8.750,1.1254,0.07820,0.07615,-0.0663,0.0116,1.0000 9.000,1.0950,0.08302,0.08108,-0.0648,0.0116,1.0000 9.250,1.0642,0.08886,0.08702,-0.0652,0.0117,1.0000 9.500,1.0330,0.09585,0.09410,-0.0674,0.0117,1.0000