Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca64a010-il-50000-n5 Airfoil,naca64a010-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,26.2473 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-naca64a010-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.500,-0.6879,0.08881,0.08145,-0.0273,1.0000,0.0464 -10.250,-0.6984,0.08400,0.07661,-0.0292,1.0000,0.0462 -10.000,-0.7121,0.07964,0.07220,-0.0303,1.0000,0.0460 -9.750,-0.7262,0.07569,0.06817,-0.0302,1.0000,0.0458 -9.500,-0.7387,0.07209,0.06447,-0.0291,1.0000,0.0457 -9.250,-0.7485,0.06834,0.06055,-0.0281,1.0000,0.0455 -9.000,-0.7553,0.06456,0.05656,-0.0268,1.0000,0.0454 -8.750,-0.7586,0.06087,0.05261,-0.0253,1.0000,0.0453 -8.500,-0.7591,0.05724,0.04867,-0.0236,1.0000,0.0452 -8.250,-0.7567,0.05370,0.04477,-0.0218,1.0000,0.0453 -8.000,-0.7512,0.05028,0.04094,-0.0199,1.0000,0.0455 -7.750,-0.7425,0.04707,0.03727,-0.0180,1.0000,0.0458 -7.500,-0.7313,0.04409,0.03384,-0.0160,1.0000,0.0466 -7.250,-0.7166,0.04132,0.03097,-0.0150,1.0000,0.0490 -7.000,-0.6996,0.03912,0.02856,-0.0137,1.0000,0.0516 -6.750,-0.6803,0.03674,0.02578,-0.0124,1.0000,0.0537 -6.500,-0.6577,0.03443,0.02310,-0.0113,1.0000,0.0554 -6.250,-0.6324,0.03238,0.02068,-0.0103,1.0000,0.0579 -6.000,-0.6085,0.03056,0.01888,-0.0096,1.0000,0.0627 -5.750,-0.5844,0.02914,0.01730,-0.0086,1.0000,0.0689 -5.500,-0.5609,0.02769,0.01573,-0.0073,1.0000,0.0735 -5.250,-0.5425,0.02645,0.01443,-0.0057,1.0000,0.0820 -5.000,-0.5262,0.02524,0.01321,-0.0039,1.0000,0.0934 -4.750,-0.5114,0.02399,0.01198,-0.0017,1.0000,0.1068 -4.500,-0.4985,0.02259,0.01079,0.0005,1.0000,0.1379 -4.250,-0.4918,0.02037,0.00952,0.0030,1.0000,0.2528 -4.000,-0.4923,0.01876,0.00957,0.0087,1.0000,0.5412 -3.750,-0.4808,0.01874,0.00979,0.0135,1.0000,0.6521 -3.500,-0.4690,0.01910,0.01028,0.0189,1.0000,0.7334 -3.250,-0.4488,0.02006,0.01129,0.0244,1.0000,0.8052 -3.000,-0.4155,0.02055,0.01155,0.0255,1.0000,0.8381 -2.750,-0.3859,0.02048,0.01122,0.0253,1.0000,0.8544 -2.500,-0.3568,0.02036,0.01090,0.0250,1.0000,0.8691 -2.250,-0.3275,0.02023,0.01057,0.0243,1.0000,0.8827 -2.000,-0.2977,0.02009,0.01027,0.0234,1.0000,0.8959 -1.750,-0.2667,0.01998,0.00999,0.0221,1.0000,0.9090 -1.500,-0.2320,0.01989,0.00976,0.0201,1.0000,0.9211 -1.250,-0.1928,0.01982,0.00957,0.0170,1.0000,0.9320 -1.000,-0.1557,0.01975,0.00939,0.0142,1.0000,0.9439 -0.750,-0.1194,0.01969,0.00926,0.0114,1.0000,0.9566 -0.500,-0.0827,0.01965,0.00918,0.0083,1.0000,0.9699 -0.250,-0.0453,0.01963,0.00912,0.0049,1.0000,0.9840 0.000,0.0000,0.01961,0.00910,0.0000,0.9953,0.9953 0.250,0.0452,0.01963,0.00912,-0.0049,0.9840,1.0000 0.500,0.0827,0.01965,0.00917,-0.0083,0.9699,1.0000 0.750,0.1194,0.01969,0.00926,-0.0114,0.9566,1.0000 1.000,0.1557,0.01975,0.00939,-0.0142,0.9438,1.0000 1.250,0.1928,0.01982,0.00957,-0.0170,0.9320,1.0000 1.500,0.2319,0.01989,0.00976,-0.0200,0.9210,1.0000 1.750,0.2668,0.01998,0.00998,-0.0222,0.9090,1.0000 2.000,0.2977,0.02009,0.01027,-0.0234,0.8959,1.0000 2.250,0.3275,0.02023,0.01057,-0.0243,0.8827,1.0000 2.500,0.3568,0.02036,0.01089,-0.0250,0.8690,1.0000 2.750,0.3859,0.02048,0.01122,-0.0253,0.8544,1.0000 3.000,0.4154,0.02055,0.01155,-0.0255,0.8381,1.0000 3.250,0.4488,0.02006,0.01129,-0.0244,0.8051,1.0000 3.500,0.4691,0.01909,0.01028,-0.0189,0.7332,1.0000 3.750,0.4809,0.01874,0.00979,-0.0135,0.6527,1.0000 4.000,0.4924,0.01876,0.00957,-0.0087,0.5421,1.0000 4.250,0.4917,0.02039,0.00953,-0.0030,0.2510,1.0000 4.500,0.4985,0.02259,0.01080,-0.0005,0.1378,1.0000 4.750,0.5114,0.02400,0.01198,0.0017,0.1067,1.0000 5.000,0.5262,0.02524,0.01322,0.0039,0.0933,1.0000 5.250,0.5425,0.02645,0.01444,0.0057,0.0819,1.0000 5.500,0.5609,0.02769,0.01572,0.0073,0.0736,1.0000 5.750,0.5845,0.02915,0.01732,0.0086,0.0687,1.0000 6.000,0.6086,0.03058,0.01889,0.0096,0.0627,1.0000 6.250,0.6324,0.03238,0.02069,0.0103,0.0579,1.0000 6.500,0.6577,0.03443,0.02310,0.0113,0.0555,1.0000 6.750,0.6803,0.03675,0.02583,0.0124,0.0537,1.0000 7.000,0.6996,0.03912,0.02856,0.0138,0.0515,1.0000 7.250,0.7165,0.04130,0.03095,0.0150,0.0489,1.0000 7.500,0.7311,0.04417,0.03391,0.0160,0.0465,1.0000 7.750,0.7426,0.04705,0.03725,0.0179,0.0458,1.0000 8.000,0.7512,0.05028,0.04094,0.0199,0.0455,1.0000 8.250,0.7568,0.05369,0.04476,0.0218,0.0453,1.0000 8.500,0.7592,0.05724,0.04867,0.0236,0.0452,1.0000 8.750,0.7586,0.06087,0.05261,0.0253,0.0453,1.0000 9.000,0.7552,0.06458,0.05658,0.0268,0.0454,1.0000 9.250,0.7491,0.06832,0.06053,0.0281,0.0456,1.0000 9.500,0.7384,0.07212,0.06451,0.0291,0.0456,1.0000 9.750,0.7266,0.07568,0.06816,0.0302,0.0459,1.0000 10.000,0.7119,0.07964,0.07219,0.0303,0.0460,1.0000 10.250,0.7006,0.08398,0.07658,0.0293,0.0463,1.0000