Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m10-il-1000000 Airfoil,m10-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,80.9354 Max Cl/Cd alpha,3 Url,http://airfoiltools.com/polar/csv?polar=xf-m10-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.000,-0.5992,0.08650,0.08499,0.0080,1.0000,0.0119 -7.750,-0.5938,0.08138,0.07987,0.0022,1.0000,0.0125 -7.250,-0.6386,0.02449,0.02149,-0.0251,1.0000,0.0092 -7.000,-0.6266,0.01606,0.01189,-0.0241,1.0000,0.0098 -6.750,-0.6031,0.01389,0.00934,-0.0237,1.0000,0.0108 -6.500,-0.5761,0.01365,0.00907,-0.0237,1.0000,0.0115 -6.250,-0.5490,0.01332,0.00869,-0.0236,1.0000,0.0123 -6.000,-0.5222,0.01283,0.00810,-0.0234,1.0000,0.0132 -5.750,-0.4948,0.01265,0.00786,-0.0233,1.0000,0.0138 -5.500,-0.4687,0.01179,0.00691,-0.0232,1.0000,0.0155 -5.250,-0.4409,0.01202,0.00718,-0.0232,1.0000,0.0166 -5.000,-0.4136,0.01185,0.00698,-0.0231,1.0000,0.0179 -4.750,-0.3861,0.01183,0.00693,-0.0230,1.0000,0.0190 -4.500,-0.3605,0.01069,0.00565,-0.0227,1.0000,0.0208 -4.250,-0.3336,0.01062,0.00560,-0.0226,1.0000,0.0223 -4.000,-0.3069,0.01055,0.00553,-0.0224,1.0000,0.0239 -3.750,-0.2809,0.01026,0.00521,-0.0220,1.0000,0.0253 -3.500,-0.2532,0.01000,0.00492,-0.0220,0.9989,0.0265 -3.250,-0.2172,0.01010,0.00501,-0.0239,0.9931,0.0275 -3.000,-0.1845,0.00869,0.00348,-0.0251,0.9837,0.0300 -2.750,-0.1519,0.00830,0.00307,-0.0262,0.9688,0.0317 -2.500,-0.1238,0.00803,0.00276,-0.0261,0.9456,0.0328 -2.250,-0.0988,0.00781,0.00244,-0.0252,0.9196,0.0335 -2.000,-0.0736,0.00762,0.00215,-0.0244,0.8941,0.0342 -1.750,-0.0476,0.00747,0.00189,-0.0239,0.8702,0.0351 -1.500,-0.0208,0.00736,0.00169,-0.0235,0.8473,0.0366 -1.250,0.0063,0.00727,0.00150,-0.0232,0.8263,0.0380 -1.000,0.0337,0.00721,0.00135,-0.0231,0.8060,0.0390 -0.750,0.0613,0.00710,0.00114,-0.0229,0.7869,0.0428 -0.500,0.0891,0.00703,0.00104,-0.0228,0.7686,0.0480 -0.250,0.1168,0.00686,0.00097,-0.0228,0.7509,0.0907 0.000,0.1441,0.00647,0.00093,-0.0229,0.7338,0.2291 0.250,0.1664,0.00479,0.00090,-0.0226,0.7177,0.7847 0.500,0.1863,0.00436,0.00094,-0.0202,0.7020,0.9690 0.750,0.2353,0.00443,0.00095,-0.0249,0.6844,1.0000 1.000,0.2616,0.00453,0.00093,-0.0246,0.6597,1.0000 1.250,0.2880,0.00464,0.00093,-0.0242,0.6320,1.0000 1.500,0.3146,0.00474,0.00094,-0.0240,0.6084,1.0000 1.750,0.3415,0.00485,0.00097,-0.0237,0.5883,1.0000 2.000,0.3685,0.00497,0.00100,-0.0236,0.5638,1.0000 2.500,0.4223,0.00534,0.00111,-0.0233,0.4926,1.0000 2.750,0.4492,0.00557,0.00119,-0.0232,0.4498,1.0000 3.000,0.4759,0.00588,0.00130,-0.0231,0.3951,1.0000 3.250,0.5021,0.00636,0.00147,-0.0230,0.3158,1.0000 3.500,0.5270,0.00725,0.00178,-0.0230,0.1804,1.0000 3.750,0.5517,0.00828,0.00224,-0.0229,0.0490,1.0000 4.000,0.5788,0.00858,0.00250,-0.0228,0.0384,1.0000 4.250,0.6061,0.00880,0.00274,-0.0228,0.0347,1.0000 4.500,0.6330,0.00918,0.00312,-0.0226,0.0290,1.0000 4.750,0.6601,0.00944,0.00343,-0.0226,0.0266,1.0000 5.000,0.6872,0.00966,0.00365,-0.0225,0.0235,1.0000 5.250,0.7131,0.01029,0.00432,-0.0223,0.0189,1.0000 5.500,0.7403,0.01047,0.00451,-0.0222,0.0177,1.0000 5.750,0.7671,0.01076,0.00483,-0.0221,0.0159,1.0000 6.000,0.7934,0.01118,0.00526,-0.0220,0.0142,1.0000 6.250,0.8177,0.01210,0.00628,-0.0215,0.0127,1.0000 6.500,0.8442,0.01238,0.00660,-0.0214,0.0119,1.0000 6.750,0.8698,0.01287,0.00713,-0.0211,0.0110,1.0000 7.000,0.8952,0.01337,0.00769,-0.0208,0.0102,1.0000 7.250,0.9200,0.01401,0.00836,-0.0205,0.0096,1.0000 7.500,0.9383,0.01626,0.01083,-0.0192,0.0087,1.0000 7.750,0.9626,0.01701,0.01169,-0.0187,0.0085,1.0000 8.000,0.9866,0.01782,0.01260,-0.0183,0.0081,1.0000 8.250,1.0097,0.01884,0.01375,-0.0177,0.0077,1.0000 8.500,1.0331,0.01967,0.01470,-0.0172,0.0072,1.0000 8.750,1.0559,0.02055,0.01568,-0.0167,0.0068,1.0000 9.000,1.0773,0.02173,0.01701,-0.0160,0.0065,1.0000 9.250,1.0978,0.02301,0.01844,-0.0153,0.0063,1.0000 9.500,1.1160,0.02474,0.02036,-0.0144,0.0061,1.0000 9.750,1.1294,0.02739,0.02330,-0.0130,0.0060,1.0000 10.000,1.1338,0.03160,0.02796,-0.0110,0.0058,1.0000 10.250,1.1262,0.03729,0.03419,-0.0083,0.0058,1.0000 10.500,1.1106,0.04312,0.04046,-0.0057,0.0057,1.0000 10.750,1.0912,0.04776,0.04539,-0.0031,0.0057,1.0000 11.000,1.0713,0.05199,0.04981,-0.0021,0.0058,1.0000 11.250,1.0507,0.05758,0.05559,-0.0044,0.0058,1.0000 11.500,1.0345,0.06394,0.06211,-0.0089,0.0058,1.0000 11.750,1.0180,0.07188,0.07019,-0.0152,0.0059,1.0000