Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n63212-il-100000 Airfoil,n63212-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,49.562 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-n63212-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.5387,0.09680,0.09190,-0.0211,1.0000,0.1584 -9.500,-0.5196,0.09404,0.08911,-0.0195,1.0000,0.1630 -9.250,-0.5495,0.08850,0.08372,-0.0253,1.0000,0.1728 -9.000,-0.5253,0.08601,0.08119,-0.0227,1.0000,0.1769 -8.750,-0.5541,0.08061,0.07593,-0.0278,1.0000,0.1880 -8.000,-0.6706,0.04786,0.04169,-0.0429,1.0000,0.0815 -7.750,-0.6700,0.04296,0.03595,-0.0403,1.0000,0.0704 -7.500,-0.6599,0.03939,0.03218,-0.0388,1.0000,0.0684 -7.250,-0.6502,0.03641,0.02889,-0.0367,1.0000,0.0664 -7.000,-0.6399,0.03379,0.02591,-0.0343,1.0000,0.0649 -6.750,-0.6283,0.03154,0.02331,-0.0319,1.0000,0.0642 -6.500,-0.6150,0.02965,0.02113,-0.0297,1.0000,0.0641 -6.250,-0.6001,0.02800,0.01926,-0.0278,1.0000,0.0647 -6.000,-0.5846,0.02671,0.01781,-0.0259,1.0000,0.0672 -5.750,-0.5681,0.02560,0.01648,-0.0242,1.0000,0.0700 -5.500,-0.5505,0.02422,0.01499,-0.0225,1.0000,0.0725 -5.250,-0.5334,0.02281,0.01370,-0.0211,1.0000,0.0762 -5.000,-0.5161,0.02182,0.01271,-0.0195,1.0000,0.0819 -4.750,-0.4996,0.02071,0.01169,-0.0181,1.0000,0.0903 -4.500,-0.4828,0.01971,0.01081,-0.0169,1.0000,0.1074 -4.250,-0.4574,0.01827,0.00971,-0.0177,0.9974,0.1537 -4.000,-0.4307,0.01578,0.00955,-0.0189,0.9907,0.5604 -3.750,-0.3928,0.01644,0.01017,-0.0201,0.9824,0.6256 -3.500,-0.3582,0.01706,0.01076,-0.0206,0.9734,0.6621 -3.250,-0.3272,0.01779,0.01148,-0.0200,0.9643,0.6962 -3.000,-0.2927,0.01861,0.01227,-0.0196,0.9568,0.7273 -2.750,-0.2669,0.01906,0.01266,-0.0183,0.9469,0.7507 -2.500,-0.2338,0.01949,0.01304,-0.0181,0.9395,0.7694 -2.250,-0.2034,0.01965,0.01310,-0.0182,0.9307,0.7846 -2.000,-0.1688,0.01972,0.01307,-0.0194,0.9231,0.7980 -1.750,-0.1339,0.01973,0.01298,-0.0208,0.9152,0.8110 -1.500,-0.1008,0.01980,0.01297,-0.0214,0.9077,0.8213 -1.250,-0.0677,0.01977,0.01288,-0.0223,0.8998,0.8321 -1.000,-0.0382,0.01975,0.01280,-0.0227,0.8915,0.8436 -0.750,-0.0047,0.01970,0.01269,-0.0236,0.8840,0.8547 -0.500,0.0218,0.01971,0.01267,-0.0233,0.8752,0.8650 -0.250,0.0557,0.01963,0.01255,-0.0242,0.8682,0.8756 0.000,0.0792,0.01964,0.01255,-0.0236,0.8586,0.8880 0.250,0.1162,0.01955,0.01243,-0.0249,0.8523,0.8981 0.500,0.1435,0.01959,0.01248,-0.0250,0.8429,0.9096 0.750,0.1828,0.01947,0.01234,-0.0269,0.8368,0.9200 1.000,0.2136,0.01953,0.01242,-0.0279,0.8274,0.9323 1.250,0.2616,0.01938,0.01229,-0.0314,0.8214,0.9409 1.500,0.3035,0.01942,0.01238,-0.0346,0.8124,0.9508 1.750,0.3508,0.01925,0.01223,-0.0381,0.8058,0.9599 2.000,0.4002,0.01925,0.01232,-0.0428,0.7964,0.9680 2.250,0.4507,0.01898,0.01210,-0.0469,0.7895,0.9759 2.500,0.4955,0.01898,0.01222,-0.0509,0.7785,0.9860 2.750,0.5426,0.01880,0.01212,-0.0548,0.7691,0.9957 3.000,0.5716,0.01868,0.01206,-0.0552,0.7590,1.0000 3.250,0.5826,0.01888,0.01234,-0.0529,0.7465,1.0000 3.500,0.5945,0.01896,0.01247,-0.0504,0.7344,1.0000 3.750,0.6083,0.01886,0.01240,-0.0476,0.7222,1.0000 4.000,0.6243,0.01860,0.01216,-0.0449,0.7093,1.0000 4.250,0.6410,0.01830,0.01191,-0.0422,0.6947,1.0000 4.500,0.6587,0.01803,0.01167,-0.0398,0.6768,1.0000 4.750,0.6812,0.01748,0.01113,-0.0376,0.6554,1.0000 5.000,0.7057,0.01686,0.01049,-0.0357,0.6311,1.0000 5.250,0.7303,0.01635,0.00997,-0.0340,0.6038,1.0000 5.500,0.7531,0.01608,0.00974,-0.0324,0.5710,1.0000 5.750,0.7750,0.01588,0.00954,-0.0306,0.5267,1.0000 6.000,0.7920,0.01598,0.00941,-0.0281,0.4372,1.0000 6.250,0.7862,0.01861,0.01035,-0.0236,0.1971,1.0000 6.500,0.7919,0.02099,0.01204,-0.0210,0.1313,1.0000 6.750,0.8066,0.02256,0.01341,-0.0193,0.1090,1.0000 7.000,0.8246,0.02410,0.01482,-0.0180,0.0966,1.0000 7.250,0.8460,0.02580,0.01630,-0.0173,0.0869,1.0000 7.500,0.8711,0.02718,0.01781,-0.0167,0.0800,1.0000 7.750,0.9003,0.02949,0.01993,-0.0170,0.0750,1.0000 8.000,0.9264,0.03122,0.02191,-0.0166,0.0712,1.0000 8.250,0.9516,0.03304,0.02389,-0.0162,0.0674,1.0000 8.500,0.9770,0.03535,0.02639,-0.0159,0.0655,1.0000 8.750,1.0006,0.03803,0.02928,-0.0155,0.0644,1.0000 9.000,1.0216,0.04111,0.03264,-0.0148,0.0637,1.0000 9.250,1.0388,0.04509,0.03689,-0.0142,0.0627,1.0000 9.500,1.0489,0.04872,0.04092,-0.0128,0.0620,1.0000 9.750,1.0579,0.05226,0.04485,-0.0114,0.0619,1.0000 10.000,1.0688,0.05580,0.04875,-0.0101,0.0628,1.0000 10.250,1.0400,0.06004,0.05401,-0.0054,0.0675,1.0000 10.500,1.0253,0.06500,0.05933,-0.0034,0.0702,1.0000 10.750,1.0170,0.06982,0.06431,-0.0022,0.0725,1.0000 11.000,0.8970,0.06592,0.06098,0.0041,0.0712,1.0000 11.250,0.8727,0.07169,0.06688,0.0036,0.0723,1.0000 11.500,0.8677,0.07743,0.07273,0.0030,0.0758,1.0000 11.750,0.8097,0.08586,0.08139,-0.0014,0.0763,1.0000 12.000,0.7379,0.10296,0.09865,-0.0113,0.0886,1.0000