Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rc10n1-il-50000-n5 Airfoil,rc10n1-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,33.3392 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-rc10n1-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.5727,0.10547,0.09918,0.0046,1.0000,0.1376 -8.750,-0.5816,0.10119,0.09501,0.0005,1.0000,0.1443 -8.250,-0.5844,0.09287,0.08683,-0.0041,1.0000,0.1589 -7.750,-0.5820,0.07637,0.06991,-0.0181,1.0000,0.0672 -7.500,-0.5880,0.07118,0.06417,-0.0207,1.0000,0.0569 -7.250,-0.5752,0.06654,0.05962,-0.0207,1.0000,0.0549 -7.000,-0.5669,0.06245,0.05538,-0.0210,1.0000,0.0534 -6.750,-0.5577,0.05859,0.05128,-0.0210,1.0000,0.0530 -6.500,-0.5466,0.05499,0.04739,-0.0208,1.0000,0.0533 -6.250,-0.5338,0.05160,0.04367,-0.0203,1.0000,0.0536 -6.000,-0.5194,0.04836,0.04010,-0.0196,1.0000,0.0534 -5.750,-0.5042,0.04528,0.03665,-0.0187,1.0000,0.0526 -5.500,-0.4890,0.04248,0.03351,-0.0175,1.0000,0.0518 -5.250,-0.4752,0.04005,0.03074,-0.0157,1.0000,0.0513 -5.000,-0.4635,0.03799,0.02835,-0.0135,1.0000,0.0510 -4.750,-0.4518,0.03613,0.02618,-0.0111,1.0000,0.0508 -4.500,-0.4363,0.03432,0.02404,-0.0093,0.9988,0.0509 -4.250,-0.4007,0.03211,0.02138,-0.0109,0.9887,0.0521 -4.000,-0.3640,0.03037,0.01918,-0.0125,0.9797,0.0555 -3.750,-0.3249,0.02862,0.01706,-0.0144,0.9723,0.0579 -3.500,-0.2875,0.02683,0.01521,-0.0161,0.9649,0.0602 -3.250,-0.2486,0.02549,0.01375,-0.0179,0.9584,0.0640 -3.000,-0.2137,0.02454,0.01258,-0.0193,0.9499,0.0718 -2.750,-0.1792,0.02343,0.01134,-0.0209,0.9425,0.0799 -2.500,-0.1489,0.02255,0.01034,-0.0217,0.9333,0.0917 -2.250,-0.1194,0.02156,0.00943,-0.0225,0.9247,0.1226 -2.000,0.0210,0.01881,0.00962,-0.0370,0.9472,1.0000 -1.750,0.0514,0.01868,0.00918,-0.0388,0.9342,1.0000 -1.500,0.0799,0.01862,0.00884,-0.0400,0.9219,1.0000 -1.250,0.1068,0.01862,0.00861,-0.0408,0.9105,1.0000 -1.000,0.1332,0.01866,0.00845,-0.0412,0.8999,1.0000 -0.750,0.1569,0.01877,0.00840,-0.0411,0.8889,1.0000 -0.500,0.1800,0.01893,0.00839,-0.0409,0.8785,1.0000 -0.250,0.2036,0.01910,0.00843,-0.0406,0.8690,1.0000 0.000,0.2267,0.01930,0.00852,-0.0401,0.8596,1.0000 0.250,0.2487,0.01954,0.00868,-0.0395,0.8496,1.0000 0.500,0.2715,0.01979,0.00884,-0.0388,0.8406,1.0000 0.750,0.2940,0.02005,0.00904,-0.0381,0.8313,1.0000 1.000,0.3156,0.02036,0.00931,-0.0373,0.8214,1.0000 1.250,0.3381,0.02064,0.00957,-0.0365,0.8124,1.0000 1.500,0.3603,0.02094,0.00986,-0.0356,0.8029,1.0000 1.750,0.3817,0.02129,0.01021,-0.0346,0.7924,1.0000 2.000,0.4042,0.02160,0.01053,-0.0337,0.7827,1.0000 2.250,0.4272,0.02186,0.01082,-0.0327,0.7733,1.0000 2.500,0.4484,0.02223,0.01125,-0.0317,0.7619,1.0000 2.750,0.4700,0.02257,0.01165,-0.0306,0.7508,1.0000 3.000,0.4921,0.02286,0.01201,-0.0295,0.7400,1.0000 3.250,0.5151,0.02306,0.01228,-0.0281,0.7299,1.0000 3.500,0.5363,0.02337,0.01273,-0.0269,0.7172,1.0000 3.750,0.5577,0.02365,0.01313,-0.0256,0.7043,1.0000 4.000,0.5793,0.02388,0.01349,-0.0242,0.6910,1.0000 4.250,0.6011,0.02403,0.01377,-0.0227,0.6767,1.0000 4.500,0.6231,0.02400,0.01392,-0.0209,0.6608,1.0000 4.750,0.6440,0.02386,0.01391,-0.0187,0.6402,1.0000 5.000,0.6658,0.02344,0.01361,-0.0162,0.6172,1.0000 5.250,0.6863,0.02315,0.01345,-0.0138,0.5899,1.0000 5.500,0.7072,0.02286,0.01333,-0.0115,0.5597,1.0000 5.750,0.7270,0.02277,0.01336,-0.0094,0.5209,1.0000 6.000,0.7464,0.02271,0.01332,-0.0070,0.4717,1.0000 6.250,0.7638,0.02291,0.01329,-0.0044,0.4030,1.0000 6.500,0.7772,0.02380,0.01371,-0.0020,0.3207,1.0000 6.750,0.7874,0.02533,0.01479,0.0001,0.2467,1.0000 7.000,0.7971,0.02705,0.01612,0.0019,0.1945,1.0000 7.250,0.8081,0.02873,0.01756,0.0036,0.1624,1.0000 7.500,0.8201,0.03035,0.01903,0.0051,0.1385,1.0000 7.750,0.8338,0.03194,0.02055,0.0067,0.1227,1.0000 8.000,0.8495,0.03348,0.02210,0.0081,0.1090,1.0000 8.250,0.8659,0.03500,0.02370,0.0093,0.0965,1.0000 8.500,0.8880,0.03661,0.02555,0.0105,0.0873,1.0000 8.750,0.9087,0.03841,0.02746,0.0115,0.0793,1.0000 9.000,0.9262,0.04012,0.02926,0.0124,0.0718,1.0000 9.250,0.9486,0.04259,0.03202,0.0133,0.0671,1.0000 9.500,0.9654,0.04504,0.03482,0.0144,0.0625,1.0000 9.750,0.9800,0.04721,0.03697,0.0151,0.0581,1.0000 10.000,0.9879,0.05029,0.04065,0.0166,0.0551,1.0000 10.250,0.9932,0.05378,0.04461,0.0179,0.0533,1.0000 10.500,0.9935,0.05739,0.04861,0.0193,0.0519,1.0000 10.750,0.9888,0.06098,0.05254,0.0207,0.0509,1.0000 11.000,0.9790,0.06441,0.05623,0.0220,0.0500,1.0000 11.250,0.9670,0.06809,0.06011,0.0226,0.0492,1.0000 11.500,0.9526,0.07224,0.06446,0.0223,0.0487,1.0000 11.750,0.9288,0.07782,0.07027,0.0206,0.0490,1.0000 12.000,0.8950,0.08565,0.07832,0.0165,0.0504,1.0000 12.250,0.8628,0.09473,0.08752,0.0108,0.0518,1.0000