Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m16-il-100000 Airfoil,m16-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,53.5629 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-m16-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.000,-0.4820,0.10608,0.10174,0.0163,1.0000,0.0464 -7.750,-0.4765,0.10282,0.09853,0.0138,1.0000,0.0481 -7.500,-0.4715,0.10000,0.09577,0.0098,1.0000,0.0499 -7.250,-0.4591,0.09833,0.09409,0.0006,1.0000,0.0513 -7.000,-0.4398,0.09693,0.09259,-0.0089,1.0000,0.0519 -6.750,-0.4364,0.08898,0.08478,-0.0055,1.0000,0.0532 -6.500,-0.4271,0.08420,0.08005,-0.0039,1.0000,0.0551 -6.250,-0.4131,0.08038,0.07623,-0.0059,1.0000,0.0576 -6.000,-0.3955,0.07668,0.07252,-0.0095,1.0000,0.0607 -5.750,-0.3577,0.07534,0.07090,-0.0204,1.0000,0.0654 -5.500,-0.3411,0.06985,0.06540,-0.0228,1.0000,0.0667 -5.250,-0.3306,0.06495,0.06063,-0.0218,1.0000,0.0692 -5.000,-0.3084,0.06161,0.05725,-0.0244,1.0000,0.0756 -4.750,-0.2783,0.05828,0.05374,-0.0300,1.0000,0.0816 -4.500,-0.2766,0.05584,0.05140,-0.0286,1.0000,0.0843 -4.250,-0.2243,0.05228,0.04744,-0.0373,0.9857,0.0951 -4.000,-0.1891,0.04776,0.04289,-0.0413,0.9718,0.1036 -3.750,-0.1493,0.04424,0.03913,-0.0460,0.9568,0.1169 -3.500,-0.1100,0.04222,0.03667,-0.0498,0.9402,0.1368 -3.250,-0.0840,0.03968,0.03396,-0.0506,0.9229,0.1510 -3.000,-0.0621,0.03720,0.03136,-0.0504,0.9069,0.1659 -2.750,-0.0417,0.03498,0.02905,-0.0497,0.8920,0.1827 -2.500,-0.0216,0.03317,0.02711,-0.0488,0.8782,0.2121 -2.250,-0.0022,0.03140,0.02522,-0.0479,0.8654,0.2516 -2.000,0.0172,0.03006,0.02374,-0.0466,0.8535,0.3034 -1.750,0.0352,0.02764,0.02134,-0.0449,0.8429,0.3427 -1.500,0.0575,0.02567,0.01930,-0.0440,0.8314,0.3804 -1.250,0.0855,0.02427,0.01768,-0.0439,0.8205,0.3974 -1.000,0.1546,0.02419,0.01577,-0.0458,0.8112,0.1326 -0.750,0.1828,0.02282,0.01400,-0.0446,0.8018,0.1162 -0.500,0.2124,0.02196,0.01271,-0.0440,0.7912,0.1068 -0.250,0.2393,0.02099,0.01162,-0.0434,0.7814,0.1043 0.000,0.2651,0.02026,0.01071,-0.0422,0.7729,0.1029 0.250,0.2929,0.01966,0.01003,-0.0420,0.7623,0.1032 0.500,0.3198,0.01920,0.00949,-0.0414,0.7525,0.1054 0.750,0.3445,0.01870,0.00897,-0.0402,0.7446,0.1107 1.000,0.3715,0.01845,0.00875,-0.0400,0.7339,0.1234 1.250,0.3979,0.01822,0.00851,-0.0394,0.7245,0.1363 1.500,0.4229,0.01780,0.00823,-0.0384,0.7166,0.1861 1.750,0.4657,0.01608,0.00802,-0.0410,0.7059,1.0000 2.000,0.4913,0.01637,0.00817,-0.0405,0.6965,1.0000 2.250,0.5159,0.01658,0.00824,-0.0395,0.6884,1.0000 2.500,0.5423,0.01691,0.00856,-0.0395,0.6779,1.0000 2.750,0.5680,0.01722,0.00883,-0.0391,0.6687,1.0000 3.000,0.5931,0.01746,0.00900,-0.0383,0.6605,1.0000 3.250,0.6195,0.01785,0.00942,-0.0383,0.6501,1.0000 3.500,0.6453,0.01818,0.00979,-0.0379,0.6412,1.0000 3.750,0.6709,0.01846,0.01007,-0.0373,0.6327,1.0000 4.000,0.6972,0.01889,0.01060,-0.0373,0.6224,1.0000 4.250,0.7230,0.01924,0.01099,-0.0368,0.6140,1.0000 4.500,0.7488,0.01957,0.01144,-0.0364,0.6048,1.0000 4.750,0.7751,0.02006,0.01209,-0.0364,0.5947,1.0000 5.000,0.8008,0.02038,0.01251,-0.0359,0.5861,1.0000 5.250,0.8250,0.02003,0.01222,-0.0342,0.5680,1.0000 5.500,0.8476,0.01873,0.01084,-0.0312,0.5394,1.0000 5.750,0.8714,0.01777,0.00992,-0.0290,0.5086,1.0000 6.000,0.8945,0.01670,0.00882,-0.0267,0.4460,1.0000 6.250,0.9031,0.01978,0.00972,-0.0255,0.0970,1.0000 6.500,0.9219,0.02191,0.01165,-0.0248,0.0670,1.0000 6.750,0.9421,0.02340,0.01333,-0.0240,0.0599,1.0000 7.000,0.9585,0.02520,0.01527,-0.0229,0.0547,1.0000 7.250,0.9761,0.02668,0.01686,-0.0217,0.0507,1.0000 7.500,0.9937,0.02836,0.01853,-0.0201,0.0490,1.0000 7.750,1.0144,0.03022,0.02035,-0.0186,0.0479,1.0000 8.000,1.0391,0.03235,0.02250,-0.0174,0.0476,1.0000 8.250,1.0653,0.03478,0.02503,-0.0164,0.0474,1.0000 8.500,1.0898,0.03807,0.02837,-0.0158,0.0457,1.0000 8.750,1.1128,0.04102,0.03166,-0.0148,0.0457,1.0000 9.000,1.1330,0.04374,0.03514,-0.0129,0.0496,1.0000 9.250,1.1509,0.04835,0.04020,-0.0116,0.0539,1.0000 9.500,1.1657,0.05257,0.04521,-0.0094,0.0633,1.0000 9.750,1.1741,0.05946,0.05316,-0.0070,0.0882,1.0000 10.750,1.0149,0.07074,0.06603,0.0042,0.1099,1.0000 11.000,0.9878,0.07619,0.07158,0.0034,0.1093,1.0000 11.250,0.9616,0.08224,0.07770,0.0018,0.1087,1.0000 11.500,0.9345,0.08897,0.08448,-0.0004,0.1082,1.0000 11.750,0.9068,0.09624,0.09174,-0.0032,0.1079,1.0000 12.000,0.8768,0.10422,0.09974,-0.0070,0.1076,1.0000