Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-fx61184-il-50000 Airfoil,fx61184-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,5.74049 Max Cl/Cd alpha,11.25 Url,http://airfoiltools.com/polar/csv?polar=xf-fx61184-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.4301,0.11585,0.10998,-0.0449,1.0000,0.1793 -10.500,-0.4646,0.10698,0.10123,-0.0476,1.0000,0.1516 -10.250,-0.4855,0.10196,0.09628,-0.0478,1.0000,0.1437 -10.000,-0.6307,0.09131,0.08577,-0.0534,1.0000,0.1343 -9.750,-0.6066,0.08773,0.08219,-0.0517,1.0000,0.1303 -9.500,-0.6437,0.08441,0.07889,-0.0500,1.0000,0.1286 -9.250,-0.6861,0.08183,0.07631,-0.0472,1.0000,0.1273 -9.000,-0.7275,0.07856,0.07296,-0.0453,1.0000,0.1255 -8.750,-0.7761,0.07406,0.06809,-0.0439,1.0000,0.1217 -8.500,-0.8027,0.07037,0.06383,-0.0427,1.0000,0.1182 -8.250,-0.8019,0.06655,0.05984,-0.0416,1.0000,0.1170 -8.000,-0.8007,0.06281,0.05583,-0.0407,1.0000,0.1154 -7.750,-0.7965,0.05920,0.05186,-0.0400,1.0000,0.1139 -7.500,-0.7884,0.05581,0.04807,-0.0395,1.0000,0.1130 -7.250,-0.7769,0.05286,0.04471,-0.0390,1.0000,0.1139 -7.000,-0.7625,0.05031,0.04172,-0.0385,1.0000,0.1156 -6.750,-0.7456,0.04806,0.03900,-0.0379,1.0000,0.1175 -6.500,-0.7269,0.04611,0.03661,-0.0371,1.0000,0.1190 -6.250,-0.7093,0.04405,0.03461,-0.0356,1.0000,0.1222 -6.000,-0.6918,0.04277,0.03332,-0.0341,1.0000,0.1275 -5.750,-0.6730,0.04176,0.03203,-0.0325,1.0000,0.1337 -5.500,-0.6576,0.04086,0.03141,-0.0295,1.0000,0.1405 -5.250,-0.6415,0.04029,0.03078,-0.0269,1.0000,0.1502 -5.000,-0.6278,0.03961,0.03023,-0.0242,1.0000,0.1641 -4.750,-0.6152,0.03862,0.02952,-0.0221,1.0000,0.1826 -4.500,-0.6002,0.03669,0.02818,-0.0219,1.0000,0.2261 -4.250,-0.6039,0.03847,0.03263,-0.0120,1.0000,0.5449 -4.000,-0.6064,0.04370,0.03765,0.0004,1.0000,0.6078 -3.750,-0.6059,0.04685,0.04065,0.0101,1.0000,0.6398 -3.500,-0.6020,0.04884,0.04246,0.0174,1.0000,0.6689 -3.250,-0.5989,0.05087,0.04438,0.0264,1.0000,0.6944 -3.000,-0.5944,0.05266,0.04606,0.0349,1.0000,0.7287 -2.750,-0.5331,0.05785,0.05096,0.0425,1.0000,0.8083 -2.500,-0.4840,0.05810,0.05087,0.0388,1.0000,0.8325 -2.250,-0.4980,0.05689,0.04959,0.0434,1.0000,0.8433 -2.000,-0.4780,0.05635,0.04884,0.0428,1.0000,0.8549 -1.750,-0.4553,0.05587,0.04818,0.0415,1.0000,0.8653 -1.500,-0.4790,0.05449,0.04674,0.0476,1.0000,0.8728 -1.250,-0.4466,0.05432,0.04636,0.0446,1.0000,0.8813 -1.000,-0.4633,0.05308,0.04506,0.0496,1.0000,0.8879 -0.750,-0.4369,0.05292,0.04473,0.0475,1.0000,0.8947 -0.500,-0.4388,0.05209,0.04380,0.0500,1.0000,0.9009 -0.250,-0.4290,0.05158,0.04318,0.0506,1.0000,0.9064 0.000,-0.4148,0.05129,0.04276,0.0503,1.0000,0.9120 0.250,-0.4169,0.05054,0.04192,0.0529,1.0000,0.9174 0.500,-0.3965,0.05053,0.04180,0.0515,1.0000,0.9222 0.750,-0.3833,0.05036,0.04153,0.0513,1.0000,0.9271 1.000,-0.3794,0.04993,0.04101,0.0528,1.0000,0.9323 1.250,-0.3571,0.05017,0.04114,0.0509,1.0000,0.9364 1.500,-0.3391,0.05035,0.04124,0.0497,1.0000,0.9410 1.750,-0.3243,0.05051,0.04131,0.0491,0.9990,0.9455 2.000,-0.2841,0.05207,0.04276,0.0434,0.9907,0.9492 2.250,-0.2448,0.05367,0.04428,0.0380,0.9811,0.9531 2.500,-0.2099,0.05517,0.04568,0.0334,0.9704,0.9571 2.750,-0.1706,0.05707,0.04752,0.0281,0.9588,0.9612 3.000,-0.1331,0.05839,0.04880,0.0230,0.9459,0.9646 3.250,-0.1020,0.05947,0.04983,0.0193,0.9329,0.9683 3.500,-0.0742,0.06060,0.05094,0.0162,0.9201,0.9722 3.750,-0.0370,0.06235,0.05266,0.0112,0.9082,0.9756 4.000,0.0067,0.06490,0.05519,0.0051,0.8973,0.9799 4.250,0.0383,0.06631,0.05661,0.0014,0.8835,0.9841 4.500,0.0640,0.06734,0.05766,-0.0015,0.8700,0.9880 4.750,0.0891,0.06866,0.05900,-0.0043,0.8574,0.9929 5.000,0.1186,0.07064,0.06100,-0.0078,0.8473,0.9999 5.250,0.1352,0.07194,0.06230,-0.0083,0.8348,1.0000 5.500,0.1340,0.07165,0.06202,-0.0061,0.8216,1.0000 5.750,0.1416,0.07233,0.06272,-0.0056,0.8105,1.0000 6.000,0.1728,0.07505,0.06544,-0.0090,0.8011,1.0000 6.250,0.1878,0.07590,0.06633,-0.0099,0.7876,1.0000 6.500,0.2005,0.07703,0.06750,-0.0109,0.7759,1.0000 6.750,0.2289,0.07970,0.07020,-0.0142,0.7671,1.0000 7.000,0.2586,0.08208,0.07265,-0.0175,0.7543,1.0000 7.250,0.2696,0.08328,0.07391,-0.0185,0.7420,1.0000 7.500,0.2917,0.08571,0.07640,-0.0212,0.7322,1.0000 7.750,0.3343,0.08964,0.08040,-0.0262,0.7203,1.0000 8.000,0.3446,0.09078,0.08163,-0.0273,0.7068,1.0000 8.250,0.3581,0.09276,0.08368,-0.0290,0.6948,1.0000 8.500,0.3820,0.09570,0.08671,-0.0320,0.6846,1.0000 8.750,0.4192,0.09947,0.09059,-0.0362,0.6720,1.0000 9.000,0.4322,0.10132,0.09253,-0.0378,0.6587,1.0000 9.250,0.4427,0.10353,0.09483,-0.0395,0.6466,1.0000 9.500,0.4613,0.10652,0.09791,-0.0420,0.6359,1.0000 9.750,0.4917,0.11024,0.10176,-0.0455,0.6243,1.0000 10.000,0.5219,0.11373,0.10536,-0.0488,0.6100,1.0000 10.250,0.5249,0.11556,0.10728,-0.0498,0.5975,1.0000 10.500,0.5355,0.11835,0.11018,-0.0517,0.5859,1.0000 11.000,0.6447,0.11957,0.11164,-0.0551,0.5012,1.0000 11.250,0.6853,0.11938,0.11160,-0.0558,0.4699,1.0000 11.500,0.6733,0.12470,0.11702,-0.0584,0.4715,1.0000 11.750,0.6748,0.12912,0.12153,-0.0608,0.4679,1.0000