Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca65410-il-100000-n5 Airfoil,naca65410-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,52.6393 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-naca65410-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.500,-0.4457,0.11242,0.10724,-0.0422,1.0000,0.0401 -10.250,-0.4293,0.10825,0.10305,-0.0369,1.0000,0.0440 -10.000,-0.4265,0.10492,0.09976,-0.0379,1.0000,0.0452 -9.750,-0.4254,0.10160,0.09645,-0.0390,1.0000,0.0481 -9.500,-0.4271,0.09792,0.09284,-0.0409,1.0000,0.0500 -9.000,-0.3567,0.07804,0.07341,-0.0455,1.0000,0.0362 -8.750,-0.3639,0.07374,0.06918,-0.0461,1.0000,0.0346 -8.500,-0.4453,0.08055,0.07577,-0.0474,1.0000,0.0362 -8.250,-0.4575,0.07671,0.07203,-0.0485,1.0000,0.0348 -8.000,-0.4757,0.07330,0.06871,-0.0488,1.0000,0.0339 -7.750,-0.4933,0.06961,0.06504,-0.0484,1.0000,0.0325 -7.500,-0.5194,0.06462,0.05970,-0.0482,1.0000,0.0282 -7.250,-0.5231,0.06135,0.05642,-0.0463,0.9998,0.0274 -7.000,-0.5060,0.05557,0.05039,-0.0507,0.9930,0.0269 -6.750,-0.4858,0.05006,0.04451,-0.0546,0.9863,0.0267 -6.500,-0.4642,0.04514,0.03915,-0.0573,0.9793,0.0266 -6.000,-0.4148,0.03711,0.03015,-0.0619,0.9672,0.0302 -5.750,-0.3838,0.03371,0.02626,-0.0640,0.9632,0.0308 -5.500,-0.3575,0.03098,0.02308,-0.0646,0.9565,0.0313 -5.250,-0.3252,0.02850,0.02015,-0.0661,0.9524,0.0323 -5.000,-0.2932,0.02678,0.01809,-0.0674,0.9481,0.0354 -4.750,-0.2632,0.02516,0.01607,-0.0679,0.9424,0.0375 -4.500,-0.2290,0.02352,0.01411,-0.0691,0.9388,0.0387 -4.250,-0.1935,0.02220,0.01255,-0.0705,0.9360,0.0400 -4.000,-0.1688,0.02083,0.01124,-0.0704,0.9290,0.0439 -3.750,-0.1368,0.01989,0.01026,-0.0714,0.9248,0.0477 -3.500,-0.1064,0.01903,0.00929,-0.0720,0.9201,0.0506 -3.250,-0.0787,0.01837,0.00853,-0.0722,0.9137,0.0538 -3.000,-0.0462,0.01768,0.00780,-0.0735,0.9096,0.0636 -2.750,-0.0188,0.01713,0.00722,-0.0736,0.9032,0.0750 -2.500,0.0106,0.01621,0.00662,-0.0745,0.8979,0.1466 -2.250,0.0272,0.01436,0.00697,-0.0724,0.8934,0.6818 -2.000,0.0442,0.01456,0.00727,-0.0691,0.8855,0.7518 -1.750,0.0631,0.01479,0.00755,-0.0655,0.8807,0.8045 -1.500,0.0775,0.01498,0.00772,-0.0617,0.8728,0.8367 -1.250,0.1054,0.01494,0.00753,-0.0614,0.8681,0.8481 -1.000,0.1323,0.01491,0.00738,-0.0613,0.8623,0.8569 -0.750,0.1593,0.01488,0.00726,-0.0612,0.8563,0.8662 -0.500,0.1899,0.01481,0.00708,-0.0617,0.8523,0.8740 -0.250,0.2134,0.01484,0.00707,-0.0610,0.8451,0.8839 0.000,0.2423,0.01480,0.00697,-0.0612,0.8403,0.8931 0.250,0.2703,0.01477,0.00691,-0.0613,0.8351,0.9023 0.500,0.2963,0.01479,0.00692,-0.0610,0.8287,0.9130 0.750,0.3274,0.01474,0.00684,-0.0617,0.8245,0.9234 1.000,0.3551,0.01478,0.00690,-0.0619,0.8181,0.9346 1.250,0.3876,0.01477,0.00692,-0.0630,0.8129,0.9453 1.500,0.4245,0.01472,0.00689,-0.0649,0.8093,0.9553 1.750,0.4577,0.01482,0.00707,-0.0666,0.8023,0.9677 2.000,0.4966,0.01482,0.00712,-0.0691,0.7976,0.9794 2.250,0.5335,0.01487,0.00728,-0.0713,0.7922,0.9996 2.500,0.5563,0.01503,0.00749,-0.0708,0.7850,1.0000 2.750,0.5845,0.01511,0.00764,-0.0711,0.7797,1.0000 3.000,0.6084,0.01532,0.00794,-0.0708,0.7714,1.0000 3.250,0.6373,0.01539,0.00813,-0.0711,0.7645,1.0000 3.500,0.6641,0.01548,0.00834,-0.0710,0.7552,1.0000 3.750,0.6925,0.01526,0.00820,-0.0704,0.7397,1.0000 4.000,0.7169,0.01474,0.00770,-0.0685,0.7054,1.0000 4.250,0.7380,0.01424,0.00703,-0.0656,0.6391,1.0000 4.500,0.7559,0.01436,0.00680,-0.0629,0.5374,1.0000 4.750,0.7628,0.01573,0.00702,-0.0591,0.3346,1.0000 5.000,0.7638,0.01822,0.00820,-0.0557,0.1210,1.0000 5.250,0.7781,0.01967,0.00922,-0.0540,0.0674,1.0000 5.500,0.7972,0.02064,0.01024,-0.0527,0.0561,1.0000 5.750,0.8156,0.02165,0.01129,-0.0514,0.0496,1.0000 6.000,0.8345,0.02257,0.01228,-0.0503,0.0437,1.0000 6.250,0.8496,0.02392,0.01363,-0.0487,0.0403,1.0000 6.500,0.8686,0.02503,0.01488,-0.0474,0.0387,1.0000 6.750,0.8890,0.02633,0.01627,-0.0464,0.0371,1.0000 7.000,0.9122,0.02780,0.01788,-0.0458,0.0356,1.0000 7.250,0.9373,0.02932,0.01949,-0.0455,0.0338,1.0000 7.500,0.9613,0.03080,0.02106,-0.0453,0.0316,1.0000 7.750,0.9864,0.03286,0.02317,-0.0453,0.0296,1.0000 8.000,1.0146,0.03598,0.02650,-0.0457,0.0288,1.0000 8.250,1.0374,0.03835,0.02921,-0.0451,0.0284,1.0000 8.500,1.0571,0.04083,0.03207,-0.0442,0.0281,1.0000 8.750,1.0736,0.04357,0.03521,-0.0429,0.0278,1.0000 9.000,1.0865,0.04654,0.03861,-0.0412,0.0277,1.0000 9.250,1.0954,0.04975,0.04224,-0.0393,0.0276,1.0000 9.500,1.1004,0.05313,0.04602,-0.0371,0.0275,1.0000 9.750,1.1010,0.05639,0.04968,-0.0347,0.0272,1.0000 10.000,1.0969,0.05962,0.05328,-0.0319,0.0268,1.0000 10.250,1.0871,0.06271,0.05670,-0.0288,0.0263,1.0000 10.500,1.0734,0.06598,0.06025,-0.0259,0.0260,1.0000 10.750,1.0574,0.06960,0.06411,-0.0238,0.0259,1.0000 11.000,1.0394,0.07366,0.06839,-0.0226,0.0258,1.0000 11.250,1.0198,0.07828,0.07322,-0.0225,0.0258,1.0000 11.500,0.9989,0.08356,0.07868,-0.0236,0.0259,1.0000 11.750,0.9774,0.08961,0.08489,-0.0260,0.0261,1.0000