Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-nacam6-il-100000 Airfoil,nacam6-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,49.8864 Max Cl/Cd alpha,8 Url,http://airfoiltools.com/polar/csv?polar=xf-nacam6-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.3372,0.09748,0.09259,-0.0253,1.0000,0.1375 -9.500,-0.3433,0.09411,0.08926,-0.0267,1.0000,0.1432 -9.250,-0.3893,0.09014,0.08540,-0.0326,1.0000,0.1461 -9.000,-0.3606,0.08566,0.08092,-0.0296,1.0000,0.1493 -8.750,-0.3468,0.08262,0.07789,-0.0285,1.0000,0.1532 -8.500,-0.3543,0.07894,0.07426,-0.0296,1.0000,0.1585 -8.250,-0.4203,0.07405,0.06948,-0.0353,1.0000,0.1621 -8.000,-0.4734,0.07184,0.06729,-0.0320,1.0000,0.1627 -7.750,-0.3858,0.06641,0.06192,-0.0323,1.0000,0.1694 -7.500,-0.4044,0.06299,0.05856,-0.0316,1.0000,0.1737 -7.250,-0.4518,0.06088,0.05655,-0.0274,1.0000,0.1772 -7.000,-0.5098,0.06088,0.05657,-0.0199,1.0000,0.1787 -6.750,-0.5536,0.06128,0.05696,-0.0124,1.0000,0.1791 -6.500,-0.5765,0.06382,0.05910,-0.0105,1.0000,0.1819 -6.250,-0.5840,0.06222,0.05759,-0.0061,1.0000,0.1840 -6.000,-0.5969,0.06102,0.05641,-0.0013,1.0000,0.1869 -5.750,-0.5977,0.05852,0.05371,-0.0009,0.9940,0.1986 -5.500,-0.5711,0.05529,0.05029,-0.0037,0.9837,0.2146 -5.250,-0.5527,0.04282,0.03608,-0.0042,0.9712,0.1131 -5.000,-0.5303,0.03805,0.03042,-0.0031,0.9604,0.0997 -4.750,-0.4947,0.03465,0.02673,-0.0051,0.9534,0.0967 -4.500,-0.4633,0.03194,0.02358,-0.0058,0.9436,0.0941 -4.250,-0.4245,0.02956,0.02074,-0.0076,0.9364,0.0927 -4.000,-0.3850,0.02780,0.01864,-0.0096,0.9280,0.0937 -3.750,-0.3320,0.02614,0.01671,-0.0142,0.9238,0.0975 -3.500,-0.2946,0.02491,0.01524,-0.0158,0.9137,0.0997 -3.250,-0.2388,0.02305,0.01339,-0.0210,0.9091,0.1040 -3.000,-0.2003,0.02207,0.01245,-0.0229,0.8994,0.1105 -2.750,-0.1545,0.02089,0.01138,-0.0262,0.8927,0.1242 -2.500,-0.1253,0.02005,0.01064,-0.0262,0.8816,0.1437 -2.250,0.1733,0.01831,0.01184,-0.0713,0.9093,0.9840 -2.000,0.2465,0.01740,0.01067,-0.0806,0.8973,1.0000 -1.750,0.2748,0.01727,0.01037,-0.0810,0.8805,1.0000 -1.500,0.2990,0.01722,0.01017,-0.0806,0.8643,1.0000 -1.250,0.3201,0.01722,0.01004,-0.0795,0.8491,1.0000 -1.000,0.3400,0.01725,0.00995,-0.0781,0.8349,1.0000 -0.750,0.3599,0.01729,0.00987,-0.0766,0.8220,1.0000 -0.500,0.3795,0.01733,0.00980,-0.0751,0.8095,1.0000 -0.250,0.3984,0.01742,0.00982,-0.0736,0.7964,1.0000 0.000,0.4178,0.01752,0.00984,-0.0721,0.7845,1.0000 0.250,0.4384,0.01758,0.00979,-0.0706,0.7743,1.0000 0.500,0.4578,0.01771,0.00988,-0.0691,0.7621,1.0000 0.750,0.4775,0.01785,0.00998,-0.0677,0.7509,1.0000 1.000,0.4989,0.01792,0.00996,-0.0663,0.7417,1.0000 1.250,0.5182,0.01812,0.01015,-0.0649,0.7297,1.0000 1.500,0.5386,0.01829,0.01029,-0.0635,0.7196,1.0000 1.750,0.5599,0.01840,0.01035,-0.0621,0.7098,1.0000 2.000,0.5796,0.01864,0.01061,-0.0607,0.6986,1.0000 2.250,0.6013,0.01877,0.01067,-0.0594,0.6896,1.0000 2.500,0.6214,0.01897,0.01089,-0.0580,0.6784,1.0000 2.750,0.6416,0.01919,0.01113,-0.0566,0.6677,1.0000 3.000,0.6641,0.01924,0.01111,-0.0552,0.6585,1.0000 3.250,0.6833,0.01947,0.01140,-0.0536,0.6462,1.0000 3.500,0.7039,0.01964,0.01158,-0.0522,0.6352,1.0000 3.750,0.7266,0.01966,0.01156,-0.0508,0.6256,1.0000 4.000,0.7458,0.01991,0.01189,-0.0492,0.6133,1.0000 4.250,0.7666,0.02009,0.01209,-0.0478,0.6024,1.0000 4.500,0.7897,0.02011,0.01208,-0.0465,0.5927,1.0000 4.750,0.8087,0.02041,0.01248,-0.0449,0.5806,1.0000 5.000,0.8294,0.02059,0.01271,-0.0434,0.5695,1.0000 5.250,0.8530,0.02061,0.01271,-0.0422,0.5598,1.0000 5.500,0.8720,0.02084,0.01304,-0.0405,0.5466,1.0000 5.750,0.8920,0.02097,0.01322,-0.0389,0.5333,1.0000 6.000,0.9126,0.02097,0.01325,-0.0371,0.5193,1.0000 6.250,0.9332,0.02090,0.01320,-0.0354,0.5040,1.0000 6.500,0.9533,0.02084,0.01315,-0.0335,0.4877,1.0000 6.750,0.9724,0.02071,0.01302,-0.0314,0.4693,1.0000 7.000,0.9913,0.02057,0.01284,-0.0293,0.4496,1.0000 7.250,1.0091,0.02054,0.01280,-0.0272,0.4295,1.0000 7.500,1.0244,0.02068,0.01303,-0.0247,0.4077,1.0000 7.750,1.0401,0.02085,0.01320,-0.0224,0.3858,1.0000 8.000,1.0536,0.02112,0.01352,-0.0197,0.3612,1.0000 8.250,1.0652,0.02149,0.01387,-0.0168,0.3330,1.0000 8.500,1.0731,0.02205,0.01439,-0.0135,0.2972,1.0000 8.750,1.0747,0.02299,0.01513,-0.0093,0.2507,1.0000 9.000,1.0671,0.02459,0.01631,-0.0040,0.2002,1.0000 9.250,1.0584,0.02639,0.01777,0.0013,0.1638,1.0000 9.500,1.0520,0.02801,0.01915,0.0062,0.1424,1.0000 9.750,1.0465,0.02938,0.02040,0.0110,0.1289,1.0000 10.000,1.0442,0.03071,0.02168,0.0153,0.1187,1.0000 10.250,1.0452,0.03218,0.02302,0.0187,0.1105,1.0000 10.500,1.0505,0.03355,0.02436,0.0215,0.1030,1.0000 10.750,1.0637,0.03508,0.02584,0.0233,0.0968,1.0000 11.000,1.0765,0.03652,0.02725,0.0251,0.0908,1.0000 11.250,1.1009,0.03840,0.02910,0.0255,0.0853,1.0000 11.500,1.1156,0.04003,0.03089,0.0270,0.0814,1.0000 11.750,1.1624,0.04308,0.03375,0.0238,0.0756,1.0000 12.000,1.1584,0.04446,0.03543,0.0279,0.0738,1.0000 12.250,1.1628,0.04643,0.03767,0.0304,0.0719,1.0000 12.500,1.1686,0.04867,0.04014,0.0325,0.0703,1.0000 12.750,1.1744,0.05091,0.04254,0.0344,0.0685,1.0000 13.000,1.1794,0.05319,0.04492,0.0361,0.0668,1.0000 13.250,1.1936,0.05728,0.04906,0.0363,0.0646,1.0000 13.500,1.1776,0.05970,0.05176,0.0395,0.0643,1.0000 13.750,1.1584,0.06248,0.05482,0.0421,0.0639,1.0000 14.000,1.1430,0.06587,0.05846,0.0437,0.0638,1.0000 14.250,1.1231,0.06975,0.06259,0.0447,0.0637,1.0000 14.500,1.1026,0.07408,0.06716,0.0450,0.0638,1.0000 14.750,1.0815,0.07888,0.07216,0.0446,0.0640,1.0000 15.000,1.0559,0.08438,0.07787,0.0435,0.0641,1.0000 15.250,1.0330,0.09031,0.08397,0.0419,0.0644,1.0000 15.500,1.0102,0.09682,0.09061,0.0398,0.0647,1.0000 15.750,0.8392,0.13147,0.12577,0.0169,0.0752,1.0000