Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca65410-il-500000 Airfoil,naca65410-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,97.8393 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-naca65410-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.4435,0.09342,0.09111,-0.0427,1.0000,0.0168 -9.750,-0.4428,0.09010,0.08781,-0.0432,1.0000,0.0170 -9.500,-0.4429,0.08650,0.08423,-0.0445,1.0000,0.0171 -9.250,-0.4432,0.08326,0.08102,-0.0453,1.0000,0.0174 -9.000,-0.4457,0.07969,0.07748,-0.0465,1.0000,0.0175 -8.750,-0.4518,0.07588,0.07372,-0.0479,1.0000,0.0177 -8.500,-0.4695,0.07146,0.06937,-0.0498,1.0000,0.0176 -8.250,-0.4973,0.06720,0.06513,-0.0516,0.9983,0.0174 -8.000,-0.4807,0.06106,0.05887,-0.0599,0.9930,0.0177 -7.750,-0.4634,0.05580,0.05347,-0.0661,0.9874,0.0182 -7.500,-0.4415,0.05057,0.04806,-0.0719,0.9837,0.0190 -7.250,-0.4213,0.04564,0.04289,-0.0757,0.9772,0.0205 -7.000,-0.3866,0.04247,0.03923,-0.0786,0.9733,0.0227 -6.750,-0.3592,0.03812,0.03449,-0.0820,0.9705,0.0228 -6.500,-0.3479,0.02991,0.02587,-0.0841,0.9622,0.0241 -6.250,-0.3193,0.02832,0.02426,-0.0860,0.9582,0.0257 -6.000,-0.2922,0.02650,0.02223,-0.0869,0.9524,0.0281 -5.750,-0.2672,0.02052,0.01545,-0.0857,0.9449,0.0215 -5.500,-0.2406,0.01807,0.01264,-0.0856,0.9387,0.0215 -5.250,-0.2146,0.01655,0.01088,-0.0852,0.9313,0.0220 -5.000,-0.1882,0.01498,0.00905,-0.0850,0.9250,0.0237 -4.750,-0.1635,0.01362,0.00761,-0.0845,0.9173,0.0250 -4.500,-0.1371,0.01280,0.00672,-0.0843,0.9110,0.0260 -4.250,-0.1117,0.01214,0.00600,-0.0839,0.9032,0.0274 -4.000,-0.0852,0.01166,0.00545,-0.0836,0.8967,0.0296 -3.750,-0.0592,0.01122,0.00494,-0.0833,0.8889,0.0311 -3.500,-0.0330,0.01068,0.00432,-0.0830,0.8825,0.0323 -3.250,-0.0078,0.00986,0.00344,-0.0828,0.8749,0.0355 -3.000,0.0194,0.00955,0.00309,-0.0828,0.8688,0.0397 -2.750,0.0464,0.00930,0.00277,-0.0827,0.8613,0.0431 -2.500,0.0740,0.00894,0.00236,-0.0827,0.8553,0.0524 -2.250,0.0995,0.00778,0.00198,-0.0832,0.8479,0.2792 -2.000,0.1244,0.00659,0.00188,-0.0835,0.8420,0.6186 -1.750,0.1515,0.00651,0.00189,-0.0833,0.8350,0.6646 -1.500,0.1785,0.00650,0.00193,-0.0830,0.8289,0.7054 -1.250,0.2049,0.00654,0.00204,-0.0825,0.8224,0.7418 -1.000,0.2320,0.00658,0.00207,-0.0822,0.8161,0.7611 -0.750,0.2591,0.00663,0.00211,-0.0819,0.8102,0.7762 -0.500,0.2863,0.00665,0.00213,-0.0818,0.8036,0.7869 -0.250,0.3143,0.00667,0.00212,-0.0818,0.7982,0.7933 0.000,0.3420,0.00668,0.00213,-0.0818,0.7915,0.8004 0.250,0.3699,0.00671,0.00213,-0.0818,0.7859,0.8071 0.500,0.3975,0.00673,0.00217,-0.0818,0.7797,0.8142 0.750,0.4252,0.00675,0.00220,-0.0818,0.7737,0.8211 1.000,0.4529,0.00680,0.00225,-0.0818,0.7682,0.8284 1.250,0.4803,0.00682,0.00230,-0.0817,0.7619,0.8356 1.500,0.5079,0.00687,0.00235,-0.0817,0.7564,0.8431 1.750,0.5347,0.00688,0.00242,-0.0814,0.7481,0.8505 2.000,0.5611,0.00690,0.00244,-0.0811,0.7368,0.8588 2.250,0.5867,0.00690,0.00246,-0.0805,0.7241,0.8663 2.500,0.6126,0.00692,0.00247,-0.0800,0.7085,0.8751 2.750,0.6364,0.00694,0.00249,-0.0789,0.6870,0.8831 3.000,0.6603,0.00700,0.00251,-0.0780,0.6606,0.8923 3.250,0.6843,0.00709,0.00259,-0.0771,0.6374,0.9019 3.500,0.7064,0.00722,0.00267,-0.0758,0.6034,0.9114 3.750,0.7255,0.00751,0.00278,-0.0739,0.5420,0.9228 4.000,0.7311,0.00875,0.00320,-0.0699,0.3594,0.9387 4.250,0.7326,0.01052,0.00393,-0.0656,0.1381,0.9619 4.500,0.7552,0.01166,0.00459,-0.0653,0.0452,1.0000 4.750,0.7817,0.01216,0.00511,-0.0655,0.0373,1.0000 5.000,0.8044,0.01302,0.00601,-0.0649,0.0313,1.0000 5.250,0.8303,0.01343,0.00646,-0.0648,0.0290,1.0000 5.500,0.8543,0.01400,0.00706,-0.0644,0.0266,1.0000 5.750,0.8766,0.01471,0.00779,-0.0637,0.0247,1.0000 6.000,0.8946,0.01590,0.00904,-0.0623,0.0232,1.0000 6.250,0.9125,0.01740,0.01063,-0.0608,0.0222,1.0000 6.500,0.9361,0.01813,0.01141,-0.0603,0.0216,1.0000 6.750,0.9598,0.01887,0.01222,-0.0597,0.0206,1.0000 7.000,0.9833,0.01983,0.01324,-0.0592,0.0196,1.0000 7.250,1.0073,0.02101,0.01450,-0.0587,0.0190,1.0000 7.500,1.0318,0.02234,0.01593,-0.0584,0.0184,1.0000 7.750,1.0562,0.02378,0.01747,-0.0580,0.0178,1.0000 8.000,1.0798,0.02533,0.01914,-0.0576,0.0173,1.0000 8.250,1.1020,0.02728,0.02118,-0.0572,0.0164,1.0000 8.500,1.1203,0.03266,0.02697,-0.0563,0.0159,1.0000 8.750,1.1355,0.03597,0.03059,-0.0548,0.0159,1.0000 9.000,1.1498,0.03862,0.03352,-0.0531,0.0160,1.0000 9.250,1.1634,0.04083,0.03598,-0.0513,0.0161,1.0000 9.500,1.0633,0.05164,0.04820,-0.0388,0.0223,1.0000 9.750,1.0524,0.05559,0.05237,-0.0355,0.0223,1.0000 10.000,1.0341,0.05875,0.05570,-0.0314,0.0223,1.0000 10.250,1.0126,0.06211,0.05922,-0.0280,0.0223,1.0000 10.500,0.9891,0.06592,0.06319,-0.0256,0.0222,1.0000 10.750,0.9655,0.07055,0.06796,-0.0244,0.0223,1.0000 11.000,0.9396,0.07589,0.07345,-0.0242,0.0223,1.0000 11.250,0.9150,0.08154,0.07923,-0.0251,0.0223,1.0000 11.500,0.8896,0.08789,0.08570,-0.0271,0.0223,1.0000 11.750,0.8633,0.09473,0.09266,-0.0302,0.0223,1.0000 12.000,0.8371,0.10198,0.10002,-0.0343,0.0223,1.0000 12.250,0.8118,0.10944,0.10758,-0.0393,0.0224,1.0000