Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-nacam12-il-100000-n5 Airfoil,nacam12-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,48.8153 Max Cl/Cd alpha,6.25 Url,http://www.airfoiltools.com/polar/csv?polar=xf-nacam12-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.5441,0.09202,0.08665,-0.0279,1.0000,0.0483 -10.000,-0.5534,0.08546,0.08011,-0.0323,1.0000,0.0479 -9.750,-0.5734,0.07666,0.07132,-0.0399,1.0000,0.0473 -9.500,-0.6000,0.07012,0.06472,-0.0427,1.0000,0.0468 -9.250,-0.6223,0.06498,0.05944,-0.0425,1.0000,0.0465 -9.000,-0.6382,0.06008,0.05436,-0.0416,1.0000,0.0464 -8.750,-0.6484,0.05559,0.04962,-0.0399,1.0000,0.0464 -8.500,-0.6541,0.05149,0.04524,-0.0378,1.0000,0.0468 -8.250,-0.6575,0.04756,0.04099,-0.0352,1.0000,0.0476 -8.000,-0.6595,0.04360,0.03662,-0.0322,1.0000,0.0485 -7.750,-0.6581,0.04002,0.03261,-0.0291,1.0000,0.0491 -7.500,-0.6528,0.03701,0.02917,-0.0263,1.0000,0.0494 -7.250,-0.6446,0.03446,0.02621,-0.0236,1.0000,0.0498 -7.000,-0.6337,0.03233,0.02369,-0.0211,1.0000,0.0503 -6.750,-0.6205,0.03072,0.02190,-0.0190,1.0000,0.0509 -6.500,-0.6063,0.02965,0.02077,-0.0172,1.0000,0.0518 -6.250,-0.5806,0.02857,0.01956,-0.0175,0.9968,0.0534 -6.000,-0.5462,0.02718,0.01794,-0.0194,0.9912,0.0553 -5.750,-0.5115,0.02570,0.01621,-0.0211,0.9854,0.0567 -5.500,-0.4765,0.02439,0.01468,-0.0228,0.9794,0.0581 -5.250,-0.4407,0.02328,0.01339,-0.0246,0.9732,0.0596 -5.000,-0.4062,0.02228,0.01241,-0.0263,0.9667,0.0615 -4.750,-0.3708,0.02151,0.01166,-0.0281,0.9599,0.0647 -4.500,-0.3357,0.02076,0.01085,-0.0298,0.9532,0.0691 -4.250,-0.3027,0.02006,0.01021,-0.0310,0.9451,0.0734 -4.000,-0.2693,0.01951,0.00968,-0.0322,0.9373,0.0794 -3.750,-0.2354,0.01937,0.00966,-0.0335,0.9283,0.0869 -3.500,-0.2013,0.01953,0.00979,-0.0346,0.9192,0.0983 -3.250,-0.1670,0.01968,0.00962,-0.0355,0.9100,0.1237 -3.000,-0.1369,0.01962,0.00931,-0.0359,0.8996,0.1380 -2.750,-0.1049,0.01916,0.00873,-0.0366,0.8910,0.1495 -2.500,-0.0790,0.01836,0.00802,-0.0365,0.8796,0.1633 -2.250,-0.0528,0.01745,0.00723,-0.0362,0.8698,0.1767 -2.000,-0.0270,0.01686,0.00667,-0.0359,0.8589,0.1855 -1.750,-0.0010,0.01650,0.00633,-0.0354,0.8472,0.1925 -1.500,0.0264,0.01617,0.00603,-0.0352,0.8369,0.1996 -1.250,0.0529,0.01592,0.00589,-0.0348,0.8252,0.2085 -1.000,0.0788,0.01563,0.00584,-0.0344,0.8133,0.2729 -0.750,0.1069,0.01560,0.00573,-0.0341,0.8024,0.2905 -0.500,0.1343,0.01558,0.00563,-0.0338,0.7906,0.3015 -0.250,0.1613,0.01557,0.00558,-0.0334,0.7782,0.3098 0.000,0.1888,0.01556,0.00552,-0.0331,0.7666,0.3153 0.250,0.2162,0.01553,0.00545,-0.0327,0.7553,0.3233 0.500,0.2430,0.01557,0.00545,-0.0324,0.7422,0.3275 0.750,0.2701,0.01560,0.00544,-0.0320,0.7301,0.3319 1.000,0.2974,0.01561,0.00542,-0.0317,0.7185,0.3371 1.250,0.3243,0.01565,0.00545,-0.0314,0.7058,0.3435 1.500,0.3510,0.01568,0.00551,-0.0310,0.6929,0.3515 2.000,0.4031,0.01552,0.00557,-0.0301,0.6690,0.4145 2.250,0.4211,0.01451,0.00591,-0.0275,0.6564,0.7683 2.500,0.4551,0.01457,0.00613,-0.0283,0.6430,0.8370 2.750,0.4882,0.01468,0.00629,-0.0291,0.6300,0.8752 3.000,0.5192,0.01482,0.00642,-0.0296,0.6170,0.8976 3.250,0.5494,0.01497,0.00658,-0.0299,0.6032,0.9169 3.500,0.5793,0.01514,0.00676,-0.0303,0.5886,0.9338 3.750,0.6094,0.01531,0.00694,-0.0307,0.5735,0.9486 4.000,0.6397,0.01550,0.00711,-0.0311,0.5577,0.9618 4.250,0.6703,0.01570,0.00731,-0.0317,0.5415,0.9733 4.500,0.7011,0.01591,0.00753,-0.0324,0.5256,0.9834 4.750,0.7337,0.01614,0.00777,-0.0335,0.5097,0.9927 5.000,0.7659,0.01639,0.00804,-0.0345,0.4936,1.0000 5.250,0.7879,0.01664,0.00829,-0.0334,0.4786,1.0000 5.500,0.8096,0.01691,0.00856,-0.0322,0.4633,1.0000 5.750,0.8308,0.01718,0.00884,-0.0310,0.4461,1.0000 6.000,0.8507,0.01747,0.00912,-0.0295,0.4237,1.0000 6.250,0.8694,0.01781,0.00937,-0.0278,0.3966,1.0000 6.500,0.8873,0.01820,0.00966,-0.0261,0.3674,1.0000 6.750,0.9057,0.01863,0.01005,-0.0245,0.3391,1.0000 7.000,0.9236,0.01912,0.01046,-0.0229,0.3111,1.0000 7.250,0.9405,0.01968,0.01093,-0.0212,0.2817,1.0000 7.500,0.9567,0.02034,0.01147,-0.0194,0.2516,1.0000 7.750,0.9717,0.02109,0.01210,-0.0175,0.2212,1.0000 8.000,0.9861,0.02193,0.01283,-0.0157,0.1918,1.0000 8.250,0.9994,0.02286,0.01364,-0.0137,0.1638,1.0000 8.500,1.0117,0.02387,0.01453,-0.0117,0.1388,1.0000 8.750,1.0233,0.02492,0.01550,-0.0096,0.1188,1.0000 9.000,1.0341,0.02600,0.01653,-0.0074,0.1050,1.0000 9.250,1.0439,0.02711,0.01763,-0.0051,0.0953,1.0000 9.500,1.0517,0.02828,0.01877,-0.0027,0.0880,1.0000 9.750,1.0593,0.02937,0.01992,-0.0001,0.0823,1.0000 10.000,1.0659,0.03056,0.02115,0.0023,0.0777,1.0000 10.500,1.0790,0.03328,0.02396,0.0066,0.0709,1.0000 10.750,1.0869,0.03465,0.02543,0.0083,0.0674,1.0000 11.000,1.0933,0.03619,0.02701,0.0099,0.0646,1.0000 11.250,1.0993,0.03791,0.02872,0.0115,0.0622,1.0000 11.500,1.1088,0.03943,0.03040,0.0127,0.0596,1.0000 11.750,1.1169,0.04107,0.03216,0.0139,0.0570,1.0000 12.000,1.1239,0.04282,0.03397,0.0149,0.0547,1.0000 12.250,1.1305,0.04471,0.03588,0.0159,0.0529,1.0000 12.500,1.1382,0.04665,0.03794,0.0169,0.0510,1.0000 12.750,1.1442,0.04871,0.04021,0.0176,0.0489,1.0000 13.000,1.1492,0.05087,0.04252,0.0183,0.0471,1.0000 13.250,1.1537,0.05311,0.04486,0.0188,0.0455,1.0000 13.500,1.1582,0.05537,0.04716,0.0193,0.0442,1.0000 13.750,1.1631,0.05779,0.04960,0.0198,0.0428,1.0000 14.000,1.1605,0.06094,0.05305,0.0199,0.0416,1.0000 14.250,1.1569,0.06432,0.05670,0.0196,0.0404,1.0000 14.500,1.1524,0.06787,0.06046,0.0192,0.0393,1.0000 14.750,1.1473,0.07160,0.06438,0.0186,0.0384,1.0000 15.000,1.1410,0.07553,0.06848,0.0176,0.0377,1.0000 15.250,1.1346,0.07956,0.07265,0.0165,0.0369,1.0000 15.500,1.1290,0.08359,0.07679,0.0152,0.0363,1.0000 15.750,1.1256,0.08737,0.08062,0.0141,0.0356,1.0000 16.000,1.1121,0.09295,0.08638,0.0118,0.0351,1.0000 16.250,1.0910,0.10021,0.09391,0.0080,0.0349,1.0000 16.500,1.0674,0.10841,0.10236,0.0033,0.0348,1.0000 16.750,1.0406,0.11785,0.11204,-0.0023,0.0348,1.0000 17.000,1.0092,0.12913,0.12354,-0.0093,0.0350,1.0000 17.250,0.9693,0.14370,0.13826,-0.0184,0.0353,1.0000