Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n64108-il-200000-n5 Airfoil,n64108-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,43.4871 Max Cl/Cd alpha,2.75 Url,http://airfoiltools.com/polar/csv?polar=xf-n64108-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.6240,0.08622,0.08276,-0.0063,1.0000,0.0118 -9.000,-0.6294,0.08020,0.07679,-0.0107,1.0000,0.0117 -8.750,-0.6397,0.07303,0.06965,-0.0175,1.0000,0.0116 -8.500,-0.6531,0.06764,0.06425,-0.0213,1.0000,0.0114 -8.250,-0.6608,0.06218,0.05867,-0.0237,1.0000,0.0111 -8.000,-0.6640,0.05679,0.05310,-0.0252,1.0000,0.0112 -7.750,-0.6631,0.05143,0.04750,-0.0260,1.0000,0.0112 -7.500,-0.6578,0.04636,0.04213,-0.0261,1.0000,0.0112 -7.250,-0.6471,0.04208,0.03749,-0.0259,1.0000,0.0121 -7.000,-0.6338,0.03767,0.03265,-0.0253,1.0000,0.0132 -6.750,-0.6187,0.03348,0.02799,-0.0244,1.0000,0.0137 -6.500,-0.6014,0.02978,0.02379,-0.0234,1.0000,0.0140 -6.250,-0.5813,0.02696,0.02049,-0.0225,1.0000,0.0144 -6.000,-0.5614,0.02366,0.01671,-0.0216,1.0000,0.0151 -5.750,-0.5399,0.02175,0.01461,-0.0211,1.0000,0.0165 -5.500,-0.5166,0.02093,0.01367,-0.0207,1.0000,0.0185 -5.250,-0.4932,0.01944,0.01196,-0.0199,1.0000,0.0198 -5.000,-0.4700,0.01804,0.01038,-0.0189,1.0000,0.0209 -4.750,-0.4473,0.01690,0.00907,-0.0180,1.0000,0.0221 -4.500,-0.4245,0.01635,0.00841,-0.0171,1.0000,0.0238 -4.250,-0.4044,0.01505,0.00707,-0.0159,1.0000,0.0255 -4.000,-0.3816,0.01409,0.00608,-0.0153,0.9984,0.0271 -3.750,-0.3477,0.01331,0.00524,-0.0169,0.9902,0.0300 -3.500,-0.3134,0.01271,0.00450,-0.0186,0.9823,0.0342 -3.250,-0.2791,0.01213,0.00388,-0.0202,0.9742,0.0425 -3.000,-0.2453,0.01163,0.00339,-0.0218,0.9657,0.0605 -2.750,-0.2152,0.01039,0.00288,-0.0233,0.9557,0.2245 -2.500,-0.1885,0.00902,0.00261,-0.0240,0.9453,0.5097 -2.250,-0.1587,0.00870,0.00256,-0.0244,0.9355,0.5998 -2.000,-0.1332,0.00846,0.00273,-0.0233,0.9248,0.7075 -1.750,-0.1078,0.00842,0.00281,-0.0222,0.9132,0.7582 -1.500,-0.0802,0.00839,0.00272,-0.0220,0.9020,0.7734 -1.000,-0.0256,0.00833,0.00257,-0.0213,0.8800,0.7961 -0.750,0.0011,0.00831,0.00252,-0.0208,0.8693,0.8071 -0.500,0.0273,0.00830,0.00247,-0.0203,0.8579,0.8185 -0.250,0.0536,0.00829,0.00245,-0.0198,0.8469,0.8300 0.000,0.0797,0.00829,0.00243,-0.0192,0.8362,0.8419 0.250,0.1056,0.00829,0.00243,-0.0186,0.8257,0.8538 0.500,0.1314,0.00829,0.00245,-0.0180,0.8151,0.8656 0.750,0.1573,0.00830,0.00248,-0.0173,0.8042,0.8779 1.000,0.1834,0.00831,0.00251,-0.0168,0.7937,0.8906 1.250,0.2100,0.00833,0.00256,-0.0163,0.7839,0.9037 1.500,0.2374,0.00835,0.00263,-0.0160,0.7733,0.9172 1.750,0.2659,0.00837,0.00270,-0.0160,0.7616,0.9309 2.000,0.2953,0.00840,0.00273,-0.0161,0.7444,0.9448 2.250,0.3251,0.00842,0.00268,-0.0161,0.7048,0.9586 2.500,0.3546,0.00861,0.00257,-0.0161,0.6209,0.9734 2.750,0.3866,0.00889,0.00260,-0.0170,0.5464,0.9902 3.000,0.4105,0.00952,0.00272,-0.0166,0.4116,1.0000 3.250,0.4252,0.01137,0.00328,-0.0155,0.1354,1.0000 3.500,0.4476,0.01230,0.00382,-0.0150,0.0563,1.0000 3.750,0.4724,0.01285,0.00432,-0.0147,0.0413,1.0000 4.000,0.4976,0.01340,0.00495,-0.0144,0.0355,1.0000 4.250,0.5224,0.01401,0.00564,-0.0140,0.0314,1.0000 4.500,0.5461,0.01485,0.00652,-0.0135,0.0284,1.0000 4.750,0.5693,0.01582,0.00754,-0.0129,0.0258,1.0000 5.000,0.5940,0.01655,0.00840,-0.0125,0.0238,1.0000 5.250,0.6181,0.01758,0.00952,-0.0119,0.0224,1.0000 5.500,0.6424,0.01876,0.01081,-0.0113,0.0211,1.0000 5.750,0.6669,0.02011,0.01229,-0.0107,0.0200,1.0000 6.000,0.6914,0.02126,0.01355,-0.0104,0.0185,1.0000 6.250,0.7132,0.02380,0.01626,-0.0098,0.0165,1.0000 6.500,0.7373,0.02540,0.01821,-0.0092,0.0159,1.0000 6.750,0.7598,0.02765,0.02087,-0.0084,0.0153,1.0000 7.000,0.7800,0.03063,0.02432,-0.0073,0.0147,1.0000 7.250,0.7988,0.03353,0.02766,-0.0062,0.0134,1.0000 7.500,0.8171,0.03569,0.03013,-0.0055,0.0120,1.0000 7.750,0.8313,0.03887,0.03367,-0.0045,0.0115,1.0000 8.000,0.8420,0.04245,0.03761,-0.0035,0.0111,1.0000 8.250,0.8491,0.04633,0.04182,-0.0026,0.0108,1.0000 8.500,0.8508,0.05093,0.04675,-0.0016,0.0107,1.0000 8.750,0.8474,0.05581,0.05193,-0.0008,0.0106,1.0000 9.000,0.8384,0.06112,0.05749,-0.0004,0.0107,1.0000 9.250,0.8220,0.06614,0.06269,0.0000,0.0108,1.0000 9.500,0.7951,0.07328,0.06998,-0.0026,0.0112,1.0000 9.750,0.7736,0.08190,0.07867,-0.0093,0.0115,1.0000