Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m10-il-1000000-n5 Airfoil,m10-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,75.2667 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-m10-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.6382,0.09655,0.09505,0.0155,1.0000,0.0033 -9.000,-0.6412,0.09138,0.08991,0.0125,1.0000,0.0033 -8.750,-0.7898,0.02400,0.02080,-0.0265,1.0000,0.0030 -8.500,-0.7726,0.01976,0.01607,-0.0261,1.0000,0.0032 -8.250,-0.7500,0.01782,0.01382,-0.0259,1.0000,0.0033 -8.000,-0.7257,0.01651,0.01231,-0.0257,1.0000,0.0035 -7.750,-0.7006,0.01547,0.01112,-0.0255,1.0000,0.0037 -7.500,-0.6751,0.01455,0.01004,-0.0253,1.0000,0.0039 -7.250,-0.6492,0.01375,0.00910,-0.0252,1.0000,0.0042 -7.000,-0.6231,0.01305,0.00827,-0.0250,1.0000,0.0045 -6.750,-0.5966,0.01248,0.00759,-0.0249,1.0000,0.0047 -6.500,-0.5705,0.01164,0.00662,-0.0247,1.0000,0.0053 -6.250,-0.5439,0.01106,0.00597,-0.0246,1.0000,0.0058 -6.000,-0.5171,0.01058,0.00541,-0.0245,1.0000,0.0064 -5.750,-0.4902,0.01015,0.00488,-0.0243,1.0000,0.0070 -5.500,-0.4633,0.00973,0.00439,-0.0242,1.0000,0.0080 -5.250,-0.4365,0.00932,0.00399,-0.0240,1.0000,0.0099 -5.000,-0.4067,0.00903,0.00371,-0.0246,0.9941,0.0134 -4.750,-0.3742,0.00892,0.00365,-0.0257,0.9803,0.0174 -4.500,-0.3425,0.00880,0.00348,-0.0266,0.9620,0.0187 -4.250,-0.3150,0.00862,0.00323,-0.0264,0.9370,0.0200 -4.000,-0.2897,0.00853,0.00307,-0.0257,0.9098,0.0222 -3.750,-0.2638,0.00848,0.00294,-0.0252,0.8847,0.0240 -3.500,-0.2372,0.00844,0.00281,-0.0248,0.8618,0.0263 -3.250,-0.2102,0.00843,0.00270,-0.0246,0.8403,0.0282 -3.000,-0.1829,0.00839,0.00258,-0.0244,0.8196,0.0293 -2.750,-0.1555,0.00834,0.00244,-0.0243,0.8003,0.0299 -2.500,-0.1279,0.00827,0.00228,-0.0242,0.7822,0.0303 -2.250,-0.1003,0.00820,0.00213,-0.0242,0.7642,0.0305 -2.000,-0.0725,0.00811,0.00198,-0.0241,0.7469,0.0306 -1.750,-0.0449,0.00795,0.00172,-0.0241,0.7299,0.0310 -1.500,-0.0171,0.00782,0.00150,-0.0241,0.7136,0.0314 -1.250,0.0109,0.00772,0.00132,-0.0241,0.6973,0.0318 -1.000,0.0389,0.00764,0.00117,-0.0241,0.6820,0.0322 -0.750,0.0669,0.00758,0.00105,-0.0242,0.6671,0.0329 -0.500,0.0950,0.00753,0.00095,-0.0242,0.6521,0.0340 -0.250,0.1231,0.00750,0.00087,-0.0243,0.6376,0.0346 0.000,0.1513,0.00748,0.00081,-0.0243,0.6232,0.0362 0.250,0.1793,0.00747,0.00077,-0.0244,0.6048,0.0399 0.500,0.2071,0.00745,0.00076,-0.0244,0.5769,0.0700 0.750,0.2349,0.00738,0.00076,-0.0245,0.5499,0.1246 1.250,0.2895,0.00669,0.00082,-0.0250,0.5039,0.4563 1.500,0.3051,0.00533,0.00089,-0.0223,0.4756,0.9606 1.750,0.3465,0.00548,0.00093,-0.0255,0.4428,1.0000 2.000,0.3735,0.00564,0.00098,-0.0253,0.4151,1.0000 2.250,0.4006,0.00582,0.00106,-0.0253,0.3854,1.0000 2.500,0.4270,0.00621,0.00118,-0.0252,0.3188,1.0000 2.750,0.4535,0.00661,0.00133,-0.0252,0.2561,1.0000 3.000,0.4800,0.00704,0.00152,-0.0251,0.1942,1.0000 3.250,0.5059,0.00765,0.00178,-0.0251,0.1094,1.0000 3.500,0.5322,0.00817,0.00205,-0.0251,0.0489,1.0000 3.750,0.5594,0.00839,0.00223,-0.0250,0.0389,1.0000 4.000,0.5867,0.00861,0.00243,-0.0250,0.0344,1.0000 4.250,0.6139,0.00883,0.00266,-0.0250,0.0305,1.0000 4.500,0.6413,0.00899,0.00284,-0.0250,0.0293,1.0000 4.750,0.6686,0.00917,0.00304,-0.0250,0.0268,1.0000 5.000,0.6956,0.00943,0.00327,-0.0249,0.0188,1.0000 5.250,0.7225,0.00970,0.00352,-0.0249,0.0146,1.0000 5.500,0.7493,0.01003,0.00384,-0.0248,0.0104,1.0000 5.750,0.7760,0.01031,0.00416,-0.0247,0.0090,1.0000 6.000,0.8024,0.01069,0.00455,-0.0246,0.0073,1.0000 6.250,0.8287,0.01109,0.00500,-0.0245,0.0065,1.0000 6.500,0.8549,0.01147,0.00543,-0.0243,0.0059,1.0000 6.750,0.8809,0.01188,0.00588,-0.0242,0.0054,1.0000 7.000,0.9066,0.01233,0.00637,-0.0240,0.0049,1.0000 7.250,0.9311,0.01303,0.00717,-0.0236,0.0043,1.0000 7.500,0.9565,0.01349,0.00769,-0.0234,0.0041,1.0000 7.750,0.9816,0.01400,0.00827,-0.0231,0.0038,1.0000 8.000,1.0062,0.01459,0.00894,-0.0228,0.0036,1.0000 8.250,1.0304,0.01522,0.00964,-0.0224,0.0033,1.0000 8.500,1.0544,0.01585,0.01035,-0.0221,0.0031,1.0000 8.750,1.0780,0.01654,0.01111,-0.0216,0.0030,1.0000 9.000,1.1007,0.01739,0.01205,-0.0211,0.0028,1.0000 9.250,1.1203,0.01880,0.01364,-0.0202,0.0026,1.0000 9.500,1.1417,0.01982,0.01480,-0.0196,0.0026,1.0000 9.750,1.1627,0.02086,0.01604,-0.0189,0.0025,1.0000 10.000,1.1825,0.02207,0.01742,-0.0180,0.0024,1.0000 10.250,1.2008,0.02348,0.01903,-0.0171,0.0023,1.0000 10.500,1.2173,0.02511,0.02087,-0.0160,0.0022,1.0000 10.750,1.2317,0.02698,0.02299,-0.0147,0.0022,1.0000 11.000,1.2433,0.02916,0.02542,-0.0133,0.0021,1.0000 11.250,1.2512,0.03164,0.02819,-0.0116,0.0020,1.0000 11.500,1.2553,0.03437,0.03119,-0.0098,0.0020,1.0000 11.750,1.2539,0.03740,0.03450,-0.0077,0.0019,1.0000 12.000,1.2416,0.04060,0.03795,-0.0046,0.0019,1.0000 12.250,1.2264,0.04434,0.04191,-0.0031,0.0019,1.0000 12.500,1.2029,0.05006,0.04788,-0.0042,0.0019,1.0000 12.750,1.1687,0.05901,0.05712,-0.0092,0.0019,1.0000 13.000,1.1296,0.07126,0.06962,-0.0181,0.0020,1.0000 13.250,1.0640,0.09480,0.09341,-0.0336,0.0021,1.0000