Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rae102-il-100000-n5 Airfoil,rae102-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,36.6642 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-rae102-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.500,-0.7018,0.09215,0.08700,-0.0127,1.0000,0.0248 -11.250,-0.7174,0.08414,0.07897,-0.0182,1.0000,0.0246 -11.000,-0.7362,0.07681,0.07158,-0.0234,1.0000,0.0244 -10.750,-0.7545,0.07085,0.06552,-0.0272,1.0000,0.0242 -10.500,-0.7751,0.06563,0.06017,-0.0297,1.0000,0.0242 -10.250,-0.7938,0.06147,0.05585,-0.0302,1.0000,0.0241 -10.000,-0.8111,0.05795,0.05215,-0.0289,1.0000,0.0240 -9.750,-0.8255,0.05445,0.04839,-0.0268,1.0000,0.0240 -9.500,-0.8346,0.05068,0.04429,-0.0248,1.0000,0.0241 -9.250,-0.8375,0.04714,0.04037,-0.0227,1.0000,0.0243 -9.000,-0.8361,0.04369,0.03649,-0.0207,1.0000,0.0245 -8.750,-0.8302,0.04057,0.03288,-0.0187,1.0000,0.0248 -8.500,-0.8207,0.03733,0.02931,-0.0170,1.0000,0.0254 -8.250,-0.8068,0.03505,0.02685,-0.0158,1.0000,0.0264 -8.000,-0.7906,0.03343,0.02505,-0.0146,1.0000,0.0280 -7.750,-0.7731,0.03172,0.02309,-0.0134,1.0000,0.0300 -7.500,-0.7537,0.02969,0.02071,-0.0121,1.0000,0.0317 -7.250,-0.7328,0.02784,0.01857,-0.0109,1.0000,0.0330 -7.000,-0.7124,0.02599,0.01659,-0.0097,1.0000,0.0347 -6.750,-0.6932,0.02478,0.01538,-0.0087,1.0000,0.0379 -6.500,-0.6729,0.02366,0.01415,-0.0074,1.0000,0.0417 -6.250,-0.6527,0.02252,0.01284,-0.0060,1.0000,0.0445 -6.000,-0.6357,0.02129,0.01165,-0.0044,1.0000,0.0488 -5.750,-0.6165,0.02046,0.01074,-0.0030,1.0000,0.0554 -5.500,-0.5994,0.01946,0.00975,-0.0013,1.0000,0.0619 -5.250,-0.5813,0.01863,0.00891,0.0004,1.0000,0.0724 -5.000,-0.5635,0.01778,0.00813,0.0020,1.0000,0.0885 -4.750,-0.5461,0.01692,0.00738,0.0036,1.0000,0.1158 -4.500,-0.5298,0.01593,0.00671,0.0053,1.0000,0.1716 -4.250,-0.5160,0.01474,0.00612,0.0072,1.0000,0.2790 -4.000,-0.5038,0.01373,0.00587,0.0098,1.0000,0.4232 -3.750,-0.4870,0.01335,0.00578,0.0120,1.0000,0.5117 -3.500,-0.4688,0.01315,0.00566,0.0140,1.0000,0.5649 -3.250,-0.4504,0.01301,0.00559,0.0160,1.0000,0.6053 -3.000,-0.4321,0.01292,0.00555,0.0179,1.0000,0.6393 -2.750,-0.4008,0.01287,0.00554,0.0173,0.9926,0.6738 -2.500,-0.3644,0.01286,0.00551,0.0157,0.9825,0.7055 -2.250,-0.3286,0.01283,0.00549,0.0143,0.9719,0.7313 -2.000,-0.2928,0.01278,0.00540,0.0128,0.9610,0.7528 -1.750,-0.2552,0.01273,0.00531,0.0110,0.9511,0.7696 -1.500,-0.2165,0.01268,0.00522,0.0089,0.9415,0.7848 -1.250,-0.1808,0.01262,0.00514,0.0074,0.9294,0.7993 -1.000,-0.1447,0.01256,0.00505,0.0059,0.9172,0.8132 -0.750,-0.1084,0.01252,0.00499,0.0043,0.9049,0.8269 -0.500,-0.0722,0.01248,0.00494,0.0028,0.8926,0.8406 -0.250,-0.0362,0.01246,0.00490,0.0014,0.8799,0.8542 0.000,0.0000,0.01245,0.00489,0.0000,0.8672,0.8672 0.250,0.0362,0.01246,0.00490,-0.0014,0.8542,0.8800 0.500,0.0722,0.01248,0.00494,-0.0028,0.8406,0.8926 0.750,0.1084,0.01252,0.00499,-0.0043,0.8269,0.9050 1.000,0.1446,0.01256,0.00505,-0.0059,0.8132,0.9172 1.250,0.1807,0.01262,0.00513,-0.0074,0.7992,0.9294 1.500,0.2165,0.01268,0.00522,-0.0089,0.7848,0.9415 1.750,0.2551,0.01273,0.00531,-0.0110,0.7696,0.9512 2.000,0.2928,0.01278,0.00540,-0.0128,0.7528,0.9611 2.250,0.3286,0.01283,0.00548,-0.0143,0.7313,0.9720 2.500,0.3643,0.01286,0.00551,-0.0157,0.7057,0.9827 2.750,0.4008,0.01287,0.00554,-0.0173,0.6737,0.9928 3.000,0.4317,0.01292,0.00555,-0.0179,0.6393,1.0000 3.250,0.4500,0.01301,0.00559,-0.0159,0.6056,1.0000 3.500,0.4684,0.01315,0.00566,-0.0139,0.5654,1.0000 3.750,0.4865,0.01335,0.00577,-0.0119,0.5109,1.0000 4.000,0.5034,0.01373,0.00586,-0.0097,0.4235,1.0000 4.250,0.5157,0.01474,0.00611,-0.0072,0.2792,1.0000 4.500,0.5295,0.01592,0.00671,-0.0053,0.1723,1.0000 4.750,0.5458,0.01691,0.00737,-0.0036,0.1161,1.0000 5.000,0.5632,0.01778,0.00812,-0.0020,0.0885,1.0000 5.250,0.5811,0.01862,0.00890,-0.0003,0.0726,1.0000 5.500,0.5992,0.01946,0.00975,0.0013,0.0620,1.0000 5.750,0.6163,0.02046,0.01073,0.0030,0.0554,1.0000 6.000,0.6356,0.02128,0.01165,0.0044,0.0488,1.0000 6.250,0.6527,0.02252,0.01284,0.0060,0.0445,1.0000 6.500,0.6729,0.02366,0.01414,0.0074,0.0416,1.0000 6.750,0.6932,0.02477,0.01537,0.0086,0.0378,1.0000 7.000,0.7125,0.02600,0.01659,0.0097,0.0347,1.0000 7.250,0.7330,0.02784,0.01857,0.0108,0.0330,1.0000 7.500,0.7539,0.02971,0.02073,0.0120,0.0316,1.0000 7.750,0.7733,0.03172,0.02309,0.0133,0.0300,1.0000 8.000,0.7910,0.03342,0.02504,0.0145,0.0280,1.0000 8.250,0.8072,0.03501,0.02680,0.0157,0.0263,1.0000 8.500,0.8211,0.03735,0.02933,0.0169,0.0254,1.0000 8.750,0.8307,0.04060,0.03290,0.0185,0.0248,1.0000 9.000,0.8368,0.04372,0.03650,0.0205,0.0245,1.0000 9.250,0.8385,0.04712,0.04035,0.0226,0.0243,1.0000 9.500,0.8346,0.05080,0.04443,0.0247,0.0241,1.0000 9.750,0.8266,0.05445,0.04840,0.0266,0.0241,1.0000 10.000,0.8130,0.05794,0.05213,0.0286,0.0241,1.0000 10.250,0.7958,0.06144,0.05580,0.0300,0.0241,1.0000 10.500,0.7768,0.06562,0.06015,0.0296,0.0242,1.0000 10.750,0.7571,0.07070,0.06537,0.0272,0.0243,1.0000 11.000,0.7362,0.07708,0.07185,0.0230,0.0244,1.0000 11.250,0.7189,0.08414,0.07896,0.0180,0.0246,1.0000 11.500,0.7038,0.09201,0.08685,0.0127,0.0248,1.0000