Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca651212a06-il-200000-n5 Airfoil,naca651212a06-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,56.6546 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-naca651212a06-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.000,-0.5422,0.08996,0.08643,-0.0349,1.0000,0.0188 -10.750,-0.5552,0.08122,0.07774,-0.0408,1.0000,0.0187 -10.500,-0.5776,0.07089,0.06738,-0.0491,1.0000,0.0184 -10.250,-0.6001,0.06419,0.06058,-0.0537,1.0000,0.0181 -10.000,-0.6225,0.05902,0.05530,-0.0559,1.0000,0.0179 -9.750,-0.6448,0.05482,0.05095,-0.0553,1.0000,0.0179 -9.500,-0.6558,0.05028,0.04616,-0.0554,0.9729,0.0179 -9.250,-0.6555,0.04506,0.04050,-0.0566,0.9520,0.0181 -9.000,-0.6539,0.04075,0.03575,-0.0557,0.9363,0.0184 -8.750,-0.6504,0.03711,0.03163,-0.0539,0.9228,0.0188 -8.500,-0.6429,0.03410,0.02809,-0.0518,0.9115,0.0197 -8.250,-0.6320,0.03165,0.02516,-0.0500,0.9024,0.0205 -8.000,-0.6160,0.02966,0.02296,-0.0489,0.8940,0.0210 -7.750,-0.5980,0.02806,0.02113,-0.0479,0.8869,0.0215 -7.500,-0.5784,0.02661,0.01944,-0.0469,0.8794,0.0221 -7.250,-0.5579,0.02524,0.01783,-0.0459,0.8736,0.0226 -7.000,-0.5354,0.02397,0.01636,-0.0453,0.8669,0.0234 -6.750,-0.5128,0.02297,0.01516,-0.0445,0.8611,0.0246 -6.500,-0.4892,0.02199,0.01397,-0.0439,0.8555,0.0258 -6.250,-0.4650,0.02096,0.01275,-0.0433,0.8496,0.0264 -6.000,-0.4410,0.02009,0.01173,-0.0426,0.8448,0.0269 -5.750,-0.4184,0.01871,0.01031,-0.0420,0.8396,0.0280 -5.500,-0.3955,0.01788,0.00945,-0.0414,0.8339,0.0290 -5.250,-0.3724,0.01727,0.00877,-0.0407,0.8293,0.0307 -5.000,-0.3486,0.01673,0.00818,-0.0402,0.8245,0.0328 -4.750,-0.3249,0.01617,0.00755,-0.0396,0.8193,0.0344 -4.500,-0.3013,0.01566,0.00694,-0.0389,0.8149,0.0357 -4.250,-0.2787,0.01502,0.00623,-0.0382,0.8105,0.0380 -4.000,-0.2543,0.01458,0.00576,-0.0378,0.8053,0.0415 -3.750,-0.2292,0.01425,0.00535,-0.0374,0.8010,0.0464 -3.500,-0.2046,0.01384,0.00491,-0.0369,0.7975,0.0540 -3.250,-0.1797,0.01343,0.00456,-0.0366,0.7929,0.0740 -3.000,-0.1599,0.01237,0.00413,-0.0359,0.7881,0.2173 -2.750,-0.1447,0.01100,0.00381,-0.0343,0.7840,0.4687 -2.500,-0.1225,0.01069,0.00386,-0.0332,0.7805,0.5863 -2.250,-0.0992,0.01060,0.00401,-0.0320,0.7760,0.6571 -2.000,-0.0750,0.01063,0.00413,-0.0310,0.7719,0.7003 -1.750,-0.0495,0.01068,0.00418,-0.0302,0.7683,0.7237 -1.500,-0.0227,0.01069,0.00414,-0.0299,0.7649,0.7361 -1.250,0.0051,0.01070,0.00408,-0.0300,0.7606,0.7436 -1.000,0.0327,0.01068,0.00403,-0.0300,0.7568,0.7497 -0.750,0.0605,0.01067,0.00395,-0.0300,0.7533,0.7569 -0.500,0.0883,0.01065,0.00387,-0.0301,0.7502,0.7634 -0.250,0.1159,0.01066,0.00386,-0.0302,0.7458,0.7710 0.000,0.1435,0.01064,0.00383,-0.0303,0.7419,0.7777 0.250,0.1713,0.01062,0.00378,-0.0303,0.7384,0.7855 0.500,0.1991,0.01057,0.00373,-0.0303,0.7355,0.7921 0.750,0.2266,0.01056,0.00377,-0.0304,0.7311,0.8000 1.000,0.2539,0.01053,0.00382,-0.0304,0.7270,0.8072 1.250,0.2813,0.01052,0.00386,-0.0302,0.7234,0.8148 1.500,0.3086,0.01054,0.00395,-0.0300,0.7205,0.8229 1.750,0.3349,0.01063,0.00419,-0.0295,0.7161,0.8312 2.000,0.3616,0.01075,0.00442,-0.0291,0.7119,0.8400 2.250,0.3893,0.01085,0.00462,-0.0287,0.7082,0.8499 2.750,0.4360,0.01116,0.00497,-0.0273,0.7000,0.9066 3.000,0.4620,0.01119,0.00507,-0.0269,0.6948,0.9160 3.250,0.4895,0.01115,0.00506,-0.0267,0.6897,0.9241 3.500,0.5158,0.01110,0.00511,-0.0263,0.6787,0.9325 3.750,0.5451,0.01086,0.00486,-0.0261,0.6583,0.9396 4.000,0.5730,0.01066,0.00463,-0.0258,0.6189,0.9475 4.250,0.6029,0.01066,0.00451,-0.0261,0.5652,0.9543 4.500,0.6283,0.01109,0.00451,-0.0258,0.4635,0.9617 4.750,0.6429,0.01280,0.00522,-0.0248,0.2712,0.9717 5.000,0.6608,0.01458,0.00618,-0.0248,0.1127,0.9817 5.250,0.6852,0.01565,0.00693,-0.0253,0.0570,0.9913 5.500,0.7104,0.01635,0.00759,-0.0255,0.0441,1.0000 5.750,0.7238,0.01691,0.00815,-0.0232,0.0387,1.0000 6.000,0.7385,0.01742,0.00872,-0.0211,0.0357,1.0000 6.250,0.7526,0.01803,0.00936,-0.0190,0.0331,1.0000 6.500,0.7638,0.01886,0.01024,-0.0166,0.0307,1.0000 6.750,0.7787,0.01950,0.01093,-0.0147,0.0292,1.0000 7.000,0.7940,0.02014,0.01163,-0.0130,0.0273,1.0000 7.250,0.8076,0.02089,0.01242,-0.0110,0.0261,1.0000 7.500,0.8205,0.02168,0.01326,-0.0090,0.0252,1.0000 7.750,0.8339,0.02255,0.01417,-0.0071,0.0243,1.0000 8.000,0.8482,0.02357,0.01520,-0.0054,0.0235,1.0000 8.250,0.8650,0.02491,0.01656,-0.0042,0.0228,1.0000 8.500,0.8858,0.02611,0.01784,-0.0034,0.0222,1.0000 8.750,0.9082,0.02729,0.01913,-0.0029,0.0218,1.0000 9.000,0.9302,0.02847,0.02047,-0.0023,0.0212,1.0000 9.250,0.9509,0.02970,0.02185,-0.0017,0.0203,1.0000 9.500,0.9704,0.03098,0.02328,-0.0009,0.0196,1.0000 9.750,0.9887,0.03240,0.02486,0.0000,0.0189,1.0000 10.000,1.0064,0.03405,0.02669,0.0009,0.0186,1.0000 10.250,1.0211,0.03574,0.02857,0.0021,0.0182,1.0000 10.500,1.0328,0.03745,0.03048,0.0035,0.0179,1.0000 10.750,1.0424,0.03934,0.03255,0.0051,0.0176,1.0000 11.000,1.0495,0.04137,0.03475,0.0067,0.0173,1.0000 11.250,1.0534,0.04373,0.03734,0.0085,0.0172,1.0000 11.500,1.0534,0.04659,0.04040,0.0103,0.0169,1.0000 11.750,1.0478,0.04952,0.04358,0.0123,0.0168,1.0000 12.000,1.0382,0.05227,0.04663,0.0143,0.0166,1.0000 12.250,1.0254,0.05556,0.05023,0.0159,0.0164,1.0000 12.500,1.0099,0.05930,0.05427,0.0169,0.0161,1.0000 12.750,0.9938,0.06353,0.05873,0.0173,0.0161,1.0000 13.000,0.9736,0.06844,0.06390,0.0168,0.0159,1.0000 13.250,0.9531,0.07381,0.06950,0.0155,0.0159,1.0000 13.500,0.9315,0.07985,0.07573,0.0132,0.0159,1.0000 13.750,0.9063,0.08718,0.08325,0.0096,0.0160,1.0000 14.000,0.8807,0.09572,0.09195,0.0046,0.0161,1.0000