Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rc1064c-il-500000 Airfoil,rc1064c-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,62.4057 Max Cl/Cd alpha,3.25 Url,http://airfoiltools.com/polar/csv?polar=xf-rc1064c-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.500,-0.4905,0.08491,0.08267,-0.0304,1.0000,0.0315 -10.250,-0.4987,0.07966,0.07743,-0.0321,1.0000,0.0318 -10.000,-0.5117,0.07348,0.07127,-0.0346,1.0000,0.0321 -9.750,-0.5550,0.06100,0.05880,-0.0437,1.0000,0.0317 -9.500,-0.6126,0.05177,0.04944,-0.0459,1.0000,0.0311 -9.250,-0.7867,0.04435,0.04110,-0.0315,1.0000,0.0223 -9.000,-0.8034,0.03962,0.03606,-0.0265,1.0000,0.0217 -8.750,-0.8179,0.03476,0.03076,-0.0210,1.0000,0.0213 -8.500,-0.8231,0.03078,0.02632,-0.0162,1.0000,0.0212 -8.250,-0.8188,0.02784,0.02301,-0.0126,1.0000,0.0213 -8.000,-0.8088,0.02559,0.02043,-0.0097,1.0000,0.0216 -7.750,-0.7945,0.02408,0.01865,-0.0075,1.0000,0.0222 -7.500,-0.7779,0.02306,0.01741,-0.0055,1.0000,0.0227 -7.250,-0.7603,0.02231,0.01647,-0.0036,1.0000,0.0231 -7.000,-0.7412,0.01966,0.01352,-0.0025,0.9996,0.0235 -6.750,-0.7116,0.01797,0.01170,-0.0033,0.9981,0.0243 -6.500,-0.6797,0.01703,0.01069,-0.0045,0.9964,0.0251 -6.250,-0.6468,0.01627,0.00986,-0.0059,0.9948,0.0260 -6.000,-0.6149,0.01564,0.00918,-0.0070,0.9927,0.0273 -5.750,-0.5828,0.01499,0.00846,-0.0081,0.9900,0.0284 -5.500,-0.5494,0.01440,0.00779,-0.0094,0.9876,0.0292 -5.250,-0.5173,0.01328,0.00661,-0.0107,0.9856,0.0308 -5.000,-0.4865,0.01268,0.00601,-0.0115,0.9814,0.0328 -4.750,-0.4526,0.01222,0.00553,-0.0130,0.9782,0.0353 -4.500,-0.4177,0.01171,0.00498,-0.0146,0.9759,0.0387 -4.250,-0.3862,0.01122,0.00452,-0.0155,0.9723,0.0444 -4.000,-0.3532,0.01074,0.00409,-0.0168,0.9693,0.0556 -3.750,-0.3186,0.01029,0.00372,-0.0184,0.9673,0.0762 -3.500,-0.2825,0.00989,0.00344,-0.0204,0.9657,0.1015 -3.250,-0.2475,0.00947,0.00319,-0.0222,0.9633,0.1378 -3.000,-0.2106,0.00940,0.00321,-0.0242,0.9606,0.1834 -2.750,-0.1739,0.00909,0.00292,-0.0263,0.9580,0.2006 -2.250,-0.1051,0.00804,0.00239,-0.0298,0.9498,0.3215 -2.000,-0.0783,0.00722,0.00225,-0.0301,0.9439,0.5132 -1.750,-0.0606,0.00676,0.00237,-0.0280,0.9352,0.6698 -1.500,-0.0397,0.00671,0.00256,-0.0262,0.9269,0.7380 -1.250,-0.0176,0.00674,0.00270,-0.0247,0.9187,0.7765 -1.000,0.0053,0.00669,0.00274,-0.0234,0.9102,0.8067 -0.750,0.0279,0.00655,0.00271,-0.0219,0.8993,0.8365 -0.500,0.0516,0.00643,0.00268,-0.0207,0.8857,0.8676 -0.250,0.0770,0.00633,0.00262,-0.0197,0.8763,0.8916 0.000,0.1034,0.00622,0.00253,-0.0188,0.8687,0.9082 0.250,0.1311,0.00608,0.00236,-0.0182,0.8614,0.9185 0.500,0.1593,0.00605,0.00224,-0.0179,0.8503,0.9255 0.750,0.1880,0.00615,0.00226,-0.0178,0.8355,0.9314 1.000,0.2134,0.00624,0.00230,-0.0170,0.8194,0.9389 1.250,0.2432,0.00632,0.00236,-0.0172,0.8037,0.9431 1.500,0.2713,0.00638,0.00239,-0.0171,0.7861,0.9487 1.750,0.2974,0.00645,0.00241,-0.0165,0.7661,0.9548 2.000,0.3295,0.00656,0.00247,-0.0172,0.7464,0.9580 2.250,0.3591,0.00671,0.00250,-0.0175,0.7139,0.9620 2.500,0.3844,0.00689,0.00255,-0.0167,0.6789,0.9677 2.750,0.4160,0.00708,0.00262,-0.0175,0.6417,0.9704 3.000,0.4489,0.00735,0.00271,-0.0187,0.5920,0.9725 3.250,0.4799,0.00769,0.00284,-0.0195,0.5353,0.9754 3.500,0.5071,0.00817,0.00299,-0.0195,0.4575,0.9795 3.750,0.5326,0.00886,0.00323,-0.0195,0.3505,0.9832 4.000,0.5624,0.00965,0.00353,-0.0206,0.2435,0.9854 4.250,0.5927,0.01033,0.00386,-0.0217,0.1668,0.9881 4.500,0.6231,0.01094,0.00419,-0.0227,0.1103,0.9912 4.750,0.6536,0.01155,0.00458,-0.0236,0.0753,0.9941 5.000,0.6873,0.01202,0.00499,-0.0252,0.0622,0.9961 5.250,0.7215,0.01237,0.00535,-0.0269,0.0563,0.9983 5.500,0.7513,0.01296,0.00593,-0.0276,0.0507,1.0000 5.750,0.7710,0.01322,0.00624,-0.0261,0.0485,1.0000 6.000,0.7897,0.01357,0.00662,-0.0244,0.0462,1.0000 6.250,0.8076,0.01398,0.00704,-0.0226,0.0441,1.0000 6.500,0.8223,0.01468,0.00776,-0.0202,0.0417,1.0000 6.750,0.8378,0.01533,0.00847,-0.0179,0.0402,1.0000 7.000,0.8561,0.01568,0.00887,-0.0161,0.0390,1.0000 7.250,0.8736,0.01613,0.00938,-0.0142,0.0376,1.0000 7.500,0.8909,0.01663,0.00992,-0.0123,0.0363,1.0000 7.750,0.9080,0.01716,0.01048,-0.0104,0.0350,1.0000 8.000,0.9244,0.01783,0.01116,-0.0084,0.0337,1.0000 8.250,0.9378,0.01949,0.01289,-0.0061,0.0320,1.0000 8.500,0.9569,0.01987,0.01336,-0.0045,0.0313,1.0000 8.750,0.9754,0.02049,0.01406,-0.0029,0.0305,1.0000 9.000,0.9939,0.02115,0.01481,-0.0014,0.0294,1.0000 9.250,1.0123,0.02173,0.01546,0.0001,0.0283,1.0000 9.500,1.0306,0.02226,0.01603,0.0015,0.0273,1.0000 9.750,1.0482,0.02306,0.01685,0.0029,0.0263,1.0000 10.000,1.0621,0.02573,0.01969,0.0045,0.0251,1.0000 10.250,1.0797,0.02612,0.02021,0.0060,0.0245,1.0000 10.500,1.0964,0.02682,0.02105,0.0076,0.0237,1.0000 10.750,1.1124,0.02760,0.02196,0.0091,0.0227,1.0000 11.000,1.1273,0.02842,0.02288,0.0107,0.0219,1.0000 11.250,1.1415,0.02918,0.02371,0.0124,0.0213,1.0000 11.500,1.1545,0.02998,0.02456,0.0141,0.0207,1.0000 11.750,1.1597,0.03208,0.02677,0.0166,0.0199,1.0000 12.000,1.1596,0.03407,0.02902,0.0199,0.0194,1.0000 12.250,1.1640,0.03518,0.03031,0.0225,0.0189,1.0000 12.500,1.1664,0.03666,0.03199,0.0249,0.0184,1.0000 12.750,1.1679,0.03827,0.03376,0.0271,0.0178,1.0000 13.000,1.1689,0.03997,0.03559,0.0290,0.0174,1.0000 13.250,1.1684,0.04185,0.03762,0.0305,0.0170,1.0000 13.500,1.1676,0.04388,0.03977,0.0316,0.0167,1.0000 13.750,1.1678,0.04592,0.04191,0.0323,0.0164,1.0000 14.000,1.1679,0.04812,0.04418,0.0326,0.0161,1.0000 14.250,1.1619,0.05127,0.04744,0.0325,0.0158,1.0000 14.500,1.1493,0.05554,0.05187,0.0317,0.0157,1.0000 14.750,1.1299,0.06118,0.05770,0.0298,0.0155,1.0000 15.000,1.1074,0.06788,0.06461,0.0265,0.0155,1.0000 15.250,1.0835,0.07561,0.07255,0.0220,0.0155,1.0000 15.500,1.0558,0.08512,0.08228,0.0157,0.0156,1.0000