Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rc410-il-100000 Airfoil,rc410-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,39.1208 Max Cl/Cd alpha,3.25 Url,http://airfoiltools.com/polar/csv?polar=xf-rc410-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.5157,0.10604,0.10135,0.0066,1.0000,0.1057 -8.750,-0.5386,0.10234,0.09776,-0.0042,1.0000,0.1078 -8.500,-0.5628,0.09845,0.09380,-0.0140,1.0000,0.1083 -8.250,-0.5160,0.09313,0.08862,-0.0025,1.0000,0.1111 -8.000,-0.5046,0.08980,0.08531,-0.0022,1.0000,0.1141 -7.750,-0.5034,0.08578,0.08135,-0.0058,1.0000,0.1173 -7.500,-0.5199,0.08121,0.07665,-0.0174,1.0000,0.1225 -7.250,-0.5200,0.07602,0.07136,-0.0211,1.0000,0.1241 -7.000,-0.5011,0.07156,0.06703,-0.0199,1.0000,0.1258 -6.750,-0.4866,0.06808,0.06359,-0.0201,1.0000,0.1285 -6.500,-0.4754,0.06458,0.06005,-0.0218,1.0000,0.1327 -6.250,-0.4867,0.06287,0.05782,-0.0241,1.0000,0.1394 -6.000,-0.4881,0.05943,0.05453,-0.0212,1.0000,0.1404 -5.750,-0.4901,0.05706,0.05223,-0.0181,1.0000,0.1417 -5.500,-0.4904,0.05495,0.05012,-0.0154,1.0000,0.1436 -5.250,-0.4629,0.04351,0.03740,-0.0200,0.9922,0.0960 -5.000,-0.4308,0.03909,0.03259,-0.0222,0.9856,0.0914 -4.750,-0.3991,0.03482,0.02781,-0.0241,0.9793,0.0900 -4.500,-0.3657,0.03124,0.02350,-0.0254,0.9730,0.0930 -4.250,-0.3301,0.02948,0.02166,-0.0278,0.9680,0.0997 -4.000,-0.2969,0.02761,0.01912,-0.0285,0.9614,0.1081 -3.750,-0.2578,0.02622,0.01770,-0.0312,0.9569,0.1206 -3.500,-0.2250,0.02512,0.01649,-0.0326,0.9507,0.1340 -3.250,-0.1912,0.02412,0.01534,-0.0340,0.9448,0.1486 -3.000,-0.1532,0.02310,0.01417,-0.0361,0.9407,0.1630 -2.750,-0.1253,0.02238,0.01331,-0.0363,0.9340,0.1742 -2.500,-0.0913,0.02187,0.01264,-0.0375,0.9284,0.1861 -2.250,-0.0535,0.02094,0.01181,-0.0395,0.9244,0.1976 -2.000,-0.0291,0.02050,0.01138,-0.0391,0.9174,0.2068 -1.750,0.0028,0.02012,0.01099,-0.0399,0.9123,0.2178 -1.500,0.0355,0.01956,0.01061,-0.0408,0.9074,0.2307 -1.250,0.0604,0.01921,0.01038,-0.0401,0.8981,0.2425 -1.000,0.0889,0.01882,0.01009,-0.0396,0.8883,0.2607 -0.750,0.1169,0.01833,0.00974,-0.0387,0.8772,0.2879 -0.500,0.2441,0.01564,0.00929,-0.0532,0.8664,1.0000 -0.250,0.2640,0.01579,0.00927,-0.0512,0.8547,1.0000 0.000,0.2833,0.01590,0.00922,-0.0489,0.8439,1.0000 0.250,0.3034,0.01602,0.00924,-0.0471,0.8311,1.0000 0.500,0.3231,0.01613,0.00925,-0.0450,0.8184,1.0000 0.750,0.3425,0.01619,0.00922,-0.0427,0.8054,1.0000 1.000,0.3616,0.01618,0.00911,-0.0401,0.7919,1.0000 1.250,0.3810,0.01612,0.00896,-0.0374,0.7791,1.0000 1.500,0.4018,0.01610,0.00888,-0.0353,0.7654,1.0000 1.750,0.4227,0.01602,0.00876,-0.0332,0.7506,1.0000 2.000,0.4435,0.01586,0.00855,-0.0309,0.7348,1.0000 2.250,0.4645,0.01562,0.00825,-0.0284,0.7176,1.0000 2.500,0.4856,0.01527,0.00785,-0.0258,0.6978,1.0000 2.750,0.5069,0.01485,0.00741,-0.0234,0.6697,1.0000 3.000,0.5280,0.01434,0.00683,-0.0207,0.6264,1.0000 3.250,0.5473,0.01399,0.00611,-0.0176,0.5203,1.0000 3.500,0.5628,0.01498,0.00598,-0.0150,0.3817,1.0000 3.750,0.5831,0.01593,0.00649,-0.0138,0.3425,1.0000 4.000,0.6050,0.01672,0.00699,-0.0128,0.3204,1.0000 4.250,0.6280,0.01745,0.00752,-0.0118,0.3046,1.0000 4.500,0.6517,0.01815,0.00808,-0.0110,0.2917,1.0000 4.750,0.6756,0.01890,0.00868,-0.0103,0.2807,1.0000 5.000,0.6997,0.01963,0.00930,-0.0096,0.2705,1.0000 5.250,0.7242,0.02038,0.01004,-0.0090,0.2621,1.0000 5.500,0.7488,0.02118,0.01073,-0.0084,0.2543,1.0000 5.750,0.7732,0.02199,0.01158,-0.0079,0.2469,1.0000 6.000,0.7976,0.02277,0.01235,-0.0073,0.2395,1.0000 6.250,0.8223,0.02379,0.01333,-0.0068,0.2337,1.0000 6.500,0.8463,0.02463,0.01432,-0.0062,0.2275,1.0000 6.750,0.8706,0.02557,0.01523,-0.0057,0.2217,1.0000 7.000,0.8939,0.02667,0.01646,-0.0051,0.2162,1.0000 7.250,0.9172,0.02767,0.01761,-0.0045,0.2107,1.0000 7.500,0.9410,0.02875,0.01870,-0.0040,0.2060,1.0000 7.750,0.9632,0.03016,0.02027,-0.0035,0.2013,1.0000 8.000,0.9843,0.03133,0.02170,-0.0027,0.1959,1.0000 8.250,1.0071,0.03250,0.02294,-0.0021,0.1915,1.0000 8.500,1.0299,0.03430,0.02470,-0.0018,0.1876,1.0000 8.750,1.0459,0.03586,0.02676,-0.0006,0.1832,1.0000 9.000,1.0645,0.03735,0.02848,0.0002,0.1784,1.0000 9.250,1.0868,0.03868,0.02981,0.0007,0.1746,1.0000 9.500,1.1042,0.04097,0.03225,0.0014,0.1712,1.0000 9.750,1.1115,0.04348,0.03532,0.0029,0.1673,1.0000 10.000,1.1231,0.04565,0.03777,0.0040,0.1632,1.0000 10.250,1.1440,0.04701,0.03913,0.0046,0.1597,1.0000 10.500,1.1608,0.04947,0.04160,0.0050,0.1565,1.0000 10.750,1.1488,0.05355,0.04633,0.0072,0.1539,1.0000 11.000,1.1334,0.05804,0.05125,0.0089,0.1516,1.0000 11.250,1.1098,0.06307,0.05659,0.0103,0.1502,1.0000 11.500,1.0535,0.07059,0.06438,0.0109,0.1513,1.0000 11.750,0.9760,0.08369,0.07762,0.0051,0.1545,1.0000 12.000,0.9246,0.09797,0.09194,-0.0028,0.1578,1.0000 12.250,0.9262,0.10301,0.09700,-0.0034,0.1569,1.0000