Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e1212-il-100000 Airfoil,e1212-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,32.0847 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-e1212-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.250,-0.3620,0.14384,0.13831,-0.0144,1.0000,0.1568 -13.000,-0.3338,0.14060,0.13506,-0.0129,1.0000,0.1626 -12.750,-0.3587,0.13889,0.13339,-0.0167,1.0000,0.1687 -12.500,-0.3328,0.13391,0.12840,-0.0157,1.0000,0.1718 -12.250,-0.3188,0.13129,0.12579,-0.0156,1.0000,0.1785 -12.000,-0.3597,0.12962,0.12419,-0.0206,1.0000,0.1831 -11.750,-0.3141,0.12462,0.11916,-0.0177,1.0000,0.1874 -11.500,-0.3086,0.12228,0.11684,-0.0183,1.0000,0.1954 -11.250,-0.3594,0.12017,0.11481,-0.0240,1.0000,0.1985 -11.000,-0.2979,0.11565,0.11024,-0.0196,1.0000,0.2037 -10.750,-0.3008,0.11356,0.10818,-0.0207,1.0000,0.2124 -10.500,-0.3560,0.11093,0.10566,-0.0264,1.0000,0.2148 -10.250,-0.2847,0.10695,0.10161,-0.0212,1.0000,0.2203 -10.000,-0.2919,0.10505,0.09976,-0.0224,1.0000,0.2298 -9.750,-0.3265,0.10146,0.09627,-0.0258,1.0000,0.2327 -9.500,-0.2727,0.09867,0.09344,-0.0223,1.0000,0.2379 -9.250,-0.2748,0.09671,0.09152,-0.0228,1.0000,0.2469 -9.000,-0.3489,0.09388,0.08889,-0.0278,1.0000,0.2501 -8.750,-0.2643,0.09085,0.08577,-0.0228,1.0000,0.2560 -8.500,-0.2628,0.08900,0.08398,-0.0226,1.0000,0.2646 -8.250,-0.3714,0.08173,0.07702,-0.0281,1.0000,0.2505 -8.000,-0.3655,0.07948,0.07489,-0.0256,1.0000,0.2512 -7.750,-0.3393,0.07645,0.07188,-0.0277,0.9887,0.2525 -7.500,-0.4428,0.04467,0.03924,-0.0632,0.9387,0.2284 -7.250,-0.4088,0.04129,0.03562,-0.0680,0.9216,0.2356 -7.000,-0.3623,0.04084,0.03515,-0.0705,0.9041,0.2419 -6.750,-0.3542,0.03562,0.02913,-0.0740,0.8827,0.2506 -6.500,-0.3154,0.03565,0.02933,-0.0742,0.8628,0.2548 -6.250,-0.2885,0.03499,0.02855,-0.0739,0.8425,0.2601 -6.000,-0.2744,0.03287,0.02597,-0.0737,0.8232,0.2669 -5.750,-0.2549,0.03155,0.02442,-0.0729,0.8050,0.2717 -5.500,-0.2292,0.03129,0.02418,-0.0719,0.7876,0.2760 -5.250,-0.2071,0.03054,0.02323,-0.0710,0.7720,0.2816 -5.000,-0.1878,0.02931,0.02149,-0.0704,0.7578,0.2880 -4.750,-0.1650,0.02852,0.02069,-0.0695,0.7419,0.2922 -4.500,-0.1402,0.02817,0.02032,-0.0686,0.7278,0.2970 -4.250,-0.1159,0.02757,0.01946,-0.0679,0.7155,0.3029 -4.000,-0.0938,0.02688,0.01843,-0.0673,0.7011,0.3087 -3.750,-0.0687,0.02628,0.01784,-0.0666,0.6892,0.3133 -3.500,-0.0433,0.02594,0.01743,-0.0658,0.6766,0.3186 -3.250,-0.0185,0.02553,0.01684,-0.0653,0.6644,0.3245 -3.000,0.0072,0.02502,0.01604,-0.0648,0.6537,0.3303 -2.750,0.0322,0.02470,0.01578,-0.0641,0.6415,0.3354 -2.500,0.0591,0.02440,0.01532,-0.0636,0.6318,0.3415 -2.250,0.0842,0.02418,0.01496,-0.0631,0.6197,0.3480 -2.000,0.1113,0.02379,0.01444,-0.0626,0.6108,0.3538 -1.750,0.1363,0.02364,0.01435,-0.0620,0.5991,0.3599 -1.500,0.1640,0.02343,0.01392,-0.0616,0.5905,0.3673 -1.250,0.1892,0.02326,0.01376,-0.0611,0.5795,0.3740 -1.000,0.2165,0.02307,0.01352,-0.0606,0.5710,0.3813 -0.750,0.2423,0.02306,0.01344,-0.0601,0.5609,0.3894 -0.500,0.2692,0.02284,0.01320,-0.0597,0.5521,0.3973 -0.250,0.2955,0.02285,0.01320,-0.0592,0.5436,0.4068 0.000,0.3217,0.02277,0.01311,-0.0587,0.5344,0.4167 0.250,0.3500,0.02269,0.01294,-0.0583,0.5275,0.4277 0.500,0.3739,0.02274,0.01313,-0.0577,0.5175,0.4395 0.750,0.4017,0.02268,0.01299,-0.0573,0.5104,0.4549 1.000,0.4263,0.02277,0.01323,-0.0566,0.5022,0.4704 1.250,0.4520,0.02273,0.01329,-0.0559,0.4941,0.4895 1.500,0.4804,0.02266,0.01318,-0.0556,0.4882,0.5157 1.750,0.5020,0.02282,0.01367,-0.0545,0.4793,0.5463 2.000,0.5271,0.02268,0.01372,-0.0536,0.4726,0.5918 2.250,0.5511,0.02259,0.01389,-0.0522,0.4666,0.6633 2.500,0.5677,0.02251,0.01442,-0.0494,0.4588,0.7775 2.750,0.6463,0.02226,0.01423,-0.0574,0.4501,0.9977 3.000,0.6652,0.02289,0.01482,-0.0565,0.4428,1.0000 3.250,0.6875,0.02329,0.01510,-0.0556,0.4361,1.0000 3.500,0.7148,0.02355,0.01512,-0.0553,0.4310,1.0000 3.750,0.7338,0.02430,0.01591,-0.0541,0.4244,1.0000 4.000,0.7558,0.02483,0.01640,-0.0532,0.4179,1.0000 4.250,0.7832,0.02510,0.01648,-0.0529,0.4128,1.0000 4.500,0.8043,0.02583,0.01722,-0.0519,0.4070,1.0000 4.750,0.8239,0.02655,0.01798,-0.0509,0.4005,1.0000 5.000,0.8499,0.02694,0.01827,-0.0504,0.3956,1.0000 5.250,0.8788,0.02739,0.01852,-0.0503,0.3915,1.0000 5.500,0.8905,0.02858,0.01995,-0.0485,0.3847,1.0000 5.750,0.9133,0.02914,0.02049,-0.0478,0.3793,1.0000 6.000,0.9422,0.02942,0.02062,-0.0476,0.3751,1.0000 6.250,0.9594,0.03056,0.02183,-0.0465,0.3703,1.0000 6.500,0.9717,0.03188,0.02331,-0.0449,0.3647,1.0000 6.750,0.9951,0.03247,0.02387,-0.0442,0.3601,1.0000 7.000,1.0260,0.03270,0.02395,-0.0443,0.3564,1.0000 7.250,1.0345,0.03435,0.02577,-0.0424,0.3515,1.0000 7.500,1.0401,0.03610,0.02770,-0.0404,0.3462,1.0000 7.750,1.0611,0.03691,0.02851,-0.0397,0.3423,1.0000 8.000,1.0915,0.03721,0.02870,-0.0397,0.3391,1.0000 8.250,1.1047,0.03875,0.03031,-0.0384,0.3354,1.0000 8.500,1.0599,0.04359,0.03559,-0.0331,0.3296,1.0000 8.750,1.0541,0.04597,0.03806,-0.0307,0.3254,1.0000 9.000,1.1010,0.04515,0.03712,-0.0316,0.3226,1.0000 9.250,1.1481,0.04465,0.03647,-0.0327,0.3202,1.0000 10.000,0.5609,0.12501,0.11793,-0.0541,0.3458,1.0000 10.250,0.5781,0.12733,0.12024,-0.0542,0.3416,1.0000