Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca65410-il-50000-n5 Airfoil,naca65410-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,35.3759 Max Cl/Cd alpha,5.5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca65410-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.4435,0.09016,0.08327,-0.0446,1.0000,0.0666 -8.250,-0.4730,0.08113,0.07444,-0.0498,1.0000,0.0572 -8.000,-0.4782,0.07773,0.07111,-0.0495,1.0000,0.0558 -7.750,-0.4865,0.07436,0.06776,-0.0492,1.0000,0.0545 -7.500,-0.4957,0.07095,0.06436,-0.0487,1.0000,0.0533 -7.250,-0.5043,0.06756,0.06092,-0.0479,1.0000,0.0520 -7.000,-0.5111,0.06407,0.05732,-0.0470,1.0000,0.0507 -6.750,-0.5156,0.06037,0.05341,-0.0461,1.0000,0.0493 -6.500,-0.5163,0.05652,0.04923,-0.0453,1.0000,0.0479 -6.250,-0.5118,0.05325,0.04567,-0.0443,1.0000,0.0479 -6.000,-0.5041,0.05054,0.04279,-0.0433,1.0000,0.0494 -5.750,-0.4940,0.04779,0.03976,-0.0425,1.0000,0.0510 -5.500,-0.4810,0.04487,0.03647,-0.0419,1.0000,0.0520 -5.250,-0.4651,0.04191,0.03302,-0.0413,1.0000,0.0520 -5.000,-0.4467,0.03915,0.02980,-0.0408,1.0000,0.0521 -4.750,-0.4246,0.03662,0.02679,-0.0406,0.9994,0.0526 -4.500,-0.3902,0.03427,0.02386,-0.0424,0.9947,0.0559 -4.250,-0.3558,0.03241,0.02135,-0.0437,0.9898,0.0589 -4.000,-0.3228,0.03029,0.01903,-0.0449,0.9858,0.0608 -3.750,-0.2920,0.02883,0.01738,-0.0454,0.9807,0.0633 -3.500,-0.2593,0.02782,0.01618,-0.0463,0.9763,0.0700 -3.250,-0.2306,0.02680,0.01502,-0.0463,0.9708,0.0751 -3.000,-0.1987,0.02591,0.01400,-0.0473,0.9659,0.0808 -2.750,-0.1695,0.02513,0.01305,-0.0481,0.9600,0.0908 -2.500,-0.1374,0.02431,0.01221,-0.0497,0.9546,0.1107 -2.250,-0.1034,0.02250,0.01123,-0.0525,0.9506,0.2390 -2.000,-0.1051,0.02138,0.01233,-0.0444,0.9432,0.7483 -1.750,-0.0959,0.02175,0.01276,-0.0377,0.9368,0.8487 -1.500,-0.0282,0.02207,0.01277,-0.0410,0.9385,0.9729 -1.250,0.0180,0.02205,0.01241,-0.0457,0.9336,0.9845 -1.000,0.0629,0.02205,0.01212,-0.0503,0.9285,0.9983 -0.750,0.0902,0.02210,0.01198,-0.0515,0.9218,1.0000 -0.500,0.1075,0.02216,0.01190,-0.0509,0.9127,1.0000 -0.250,0.1283,0.02227,0.01187,-0.0508,0.9051,1.0000 0.000,0.1530,0.02243,0.01188,-0.0513,0.8979,1.0000 0.250,0.1781,0.02263,0.01196,-0.0519,0.8910,1.0000 0.500,0.2048,0.02286,0.01210,-0.0526,0.8843,1.0000 0.750,0.2360,0.02312,0.01226,-0.0541,0.8788,1.0000 1.000,0.2595,0.02343,0.01251,-0.0542,0.8712,1.0000 1.250,0.2950,0.02369,0.01273,-0.0563,0.8667,1.0000 1.500,0.3154,0.02409,0.01310,-0.0559,0.8583,1.0000 1.750,0.3496,0.02438,0.01341,-0.0576,0.8533,1.0000 2.000,0.3718,0.02482,0.01386,-0.0574,0.8454,1.0000 2.250,0.4042,0.02515,0.01423,-0.0588,0.8398,1.0000 2.500,0.4282,0.02561,0.01474,-0.0589,0.8322,1.0000 2.750,0.4592,0.02597,0.01521,-0.0600,0.8259,1.0000 3.000,0.4842,0.02643,0.01577,-0.0601,0.8182,1.0000 3.250,0.5153,0.02679,0.01626,-0.0611,0.8114,1.0000 3.500,0.5393,0.02727,0.01691,-0.0609,0.8026,1.0000 3.750,0.5743,0.02750,0.01734,-0.0623,0.7959,1.0000 4.000,0.5969,0.02797,0.01799,-0.0618,0.7853,1.0000 4.250,0.6269,0.02825,0.01850,-0.0622,0.7762,1.0000 4.500,0.6603,0.02836,0.01894,-0.0628,0.7671,1.0000 4.750,0.6864,0.02859,0.01945,-0.0624,0.7545,1.0000 5.000,0.7336,0.02621,0.01745,-0.0608,0.7193,1.0000 5.250,0.7621,0.02247,0.01367,-0.0534,0.6060,1.0000 5.500,0.7811,0.02208,0.01241,-0.0486,0.3928,1.0000 5.750,0.7716,0.02510,0.01371,-0.0437,0.1720,1.0000 6.000,0.7754,0.02745,0.01540,-0.0411,0.1104,1.0000 6.250,0.7869,0.02912,0.01698,-0.0392,0.0917,1.0000 6.500,0.7996,0.03069,0.01856,-0.0373,0.0827,1.0000 6.750,0.8155,0.03211,0.02007,-0.0358,0.0741,1.0000 7.000,0.8359,0.03359,0.02170,-0.0348,0.0668,1.0000 7.250,0.8678,0.03520,0.02347,-0.0349,0.0618,1.0000 7.500,0.9099,0.03735,0.02566,-0.0363,0.0573,1.0000 7.750,0.9439,0.03935,0.02800,-0.0368,0.0524,1.0000 8.000,0.9760,0.04186,0.03082,-0.0373,0.0498,1.0000 8.250,1.0041,0.04477,0.03400,-0.0374,0.0482,1.0000 8.500,1.0277,0.04811,0.03764,-0.0371,0.0472,1.0000 8.750,1.0455,0.05185,0.04171,-0.0363,0.0462,1.0000 9.000,1.0544,0.05486,0.04533,-0.0342,0.0451,1.0000 9.250,1.0591,0.05813,0.04915,-0.0320,0.0438,1.0000 9.500,1.0600,0.06165,0.05313,-0.0298,0.0429,1.0000 9.750,1.0573,0.06537,0.05725,-0.0276,0.0426,1.0000 10.000,1.0503,0.06915,0.06138,-0.0254,0.0426,1.0000 10.250,1.0382,0.07276,0.06527,-0.0230,0.0427,1.0000 10.500,1.0231,0.07654,0.06929,-0.0211,0.0428,1.0000 10.750,1.0057,0.08066,0.07362,-0.0201,0.0430,1.0000 11.000,0.9865,0.08526,0.07841,-0.0201,0.0432,1.0000 11.250,0.9664,0.09042,0.08374,-0.0213,0.0435,1.0000 11.500,0.9463,0.09626,0.08970,-0.0236,0.0438,1.0000