Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rc10n1-il-100000 Airfoil,rc10n1-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,49.0032 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-rc10n1-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.5843,0.11013,0.10562,0.0045,1.0000,0.0762 -9.250,-0.5955,0.10537,0.10093,-0.0037,1.0000,0.0768 -9.000,-0.6098,0.10070,0.09626,-0.0105,1.0000,0.0770 -8.750,-0.5766,0.09641,0.09203,0.0001,1.0000,0.0811 -8.500,-0.5734,0.09243,0.08808,-0.0016,1.0000,0.0841 -8.250,-0.5774,0.08746,0.08317,-0.0068,1.0000,0.0866 -8.000,-0.5871,0.08262,0.07829,-0.0123,1.0000,0.0891 -7.750,-0.6074,0.07977,0.07505,-0.0183,1.0000,0.0913 -7.500,-0.5871,0.07332,0.06892,-0.0166,1.0000,0.0950 -7.250,-0.5798,0.06992,0.06545,-0.0175,1.0000,0.1023 -7.000,-0.5790,0.06544,0.06080,-0.0195,1.0000,0.1084 -6.500,-0.5565,0.05836,0.05363,-0.0200,1.0000,0.1265 -6.250,-0.5471,0.05488,0.05001,-0.0206,1.0000,0.1386 -6.000,-0.5360,0.05179,0.04684,-0.0205,1.0000,0.1530 -5.750,-0.5268,0.04912,0.04415,-0.0195,1.0000,0.1689 -5.500,-0.5290,0.04729,0.04230,-0.0165,1.0000,0.1836 -5.250,-0.5328,0.04568,0.04069,-0.0129,1.0000,0.1995 -4.500,-0.5071,0.03930,0.03446,-0.0072,0.9934,0.3005 -4.250,-0.4832,0.03706,0.03242,-0.0061,0.9866,0.3602 -4.000,-0.4187,0.03153,0.02511,-0.0157,0.9789,0.2387 -3.750,-0.3463,0.02711,0.01845,-0.0155,0.9744,0.0804 -3.500,-0.3015,0.02519,0.01612,-0.0179,0.9700,0.0746 -3.250,-0.2639,0.02333,0.01405,-0.0194,0.9635,0.0730 -3.000,-0.2206,0.02212,0.01256,-0.0220,0.9584,0.0766 -2.750,-0.1801,0.02036,0.01085,-0.0243,0.9537,0.0796 -2.500,-0.1474,0.01920,0.00981,-0.0253,0.9464,0.0845 -2.250,-0.1116,0.01822,0.00884,-0.0269,0.9408,0.0966 -2.000,-0.0855,0.01754,0.00813,-0.0266,0.9320,0.1166 -1.750,0.0844,0.01490,0.00832,-0.0460,0.9566,1.0000 -1.500,0.1145,0.01476,0.00800,-0.0479,0.9444,1.0000 -1.250,0.1408,0.01471,0.00780,-0.0489,0.9326,1.0000 -1.000,0.1650,0.01473,0.00768,-0.0493,0.9214,1.0000 -0.750,0.1888,0.01481,0.00763,-0.0492,0.9113,1.0000 -0.500,0.2108,0.01495,0.00767,-0.0488,0.9005,1.0000 -0.250,0.2327,0.01514,0.00777,-0.0483,0.8902,1.0000 0.000,0.2548,0.01535,0.00790,-0.0476,0.8808,1.0000 0.250,0.2763,0.01557,0.00805,-0.0467,0.8712,1.0000 0.500,0.2979,0.01585,0.00828,-0.0459,0.8612,1.0000 0.750,0.3192,0.01612,0.00850,-0.0448,0.8519,1.0000 1.000,0.3404,0.01637,0.00873,-0.0436,0.8424,1.0000 1.250,0.3619,0.01670,0.00903,-0.0427,0.8320,1.0000 1.500,0.3831,0.01699,0.00931,-0.0414,0.8226,1.0000 1.750,0.4042,0.01723,0.00953,-0.0399,0.8133,1.0000 2.000,0.4256,0.01756,0.00990,-0.0389,0.8023,1.0000 2.250,0.4468,0.01787,0.01022,-0.0376,0.7918,1.0000 2.500,0.4680,0.01805,0.01040,-0.0359,0.7829,1.0000 2.750,0.4895,0.01832,0.01071,-0.0346,0.7716,1.0000 3.000,0.5109,0.01861,0.01105,-0.0334,0.7598,1.0000 3.250,0.5323,0.01882,0.01134,-0.0319,0.7482,1.0000 3.500,0.5537,0.01892,0.01149,-0.0301,0.7366,1.0000 3.750,0.5746,0.01883,0.01144,-0.0278,0.7223,1.0000 4.000,0.5952,0.01855,0.01120,-0.0253,0.7056,1.0000 4.250,0.6164,0.01817,0.01089,-0.0227,0.6888,1.0000 4.500,0.6384,0.01781,0.01057,-0.0204,0.6725,1.0000 4.750,0.6610,0.01739,0.01019,-0.0182,0.6557,1.0000 5.000,0.6834,0.01704,0.00994,-0.0162,0.6349,1.0000 5.250,0.7063,0.01656,0.00953,-0.0141,0.6131,1.0000 5.500,0.7288,0.01618,0.00923,-0.0121,0.5852,1.0000 5.750,0.7509,0.01589,0.00900,-0.0102,0.5475,1.0000 6.000,0.7718,0.01575,0.00882,-0.0082,0.4919,1.0000 6.250,0.7879,0.01624,0.00883,-0.0056,0.3845,1.0000 6.500,0.7959,0.01822,0.00980,-0.0030,0.2440,1.0000 6.750,0.8074,0.02010,0.01110,-0.0010,0.1796,1.0000 7.000,0.8224,0.02169,0.01240,0.0007,0.1483,1.0000 7.250,0.8393,0.02322,0.01376,0.0022,0.1270,1.0000 7.500,0.8588,0.02479,0.01526,0.0035,0.1120,1.0000 7.750,0.8790,0.02637,0.01682,0.0045,0.0994,1.0000 8.000,0.9020,0.02850,0.01878,0.0052,0.0901,1.0000 8.250,0.9228,0.02988,0.02049,0.0064,0.0821,1.0000 8.500,0.9453,0.03237,0.02297,0.0070,0.0760,1.0000 8.750,0.9656,0.03459,0.02562,0.0083,0.0717,1.0000 9.000,0.9847,0.03655,0.02767,0.0091,0.0665,1.0000 9.250,1.0004,0.04014,0.03159,0.0102,0.0635,1.0000 9.500,1.0117,0.04336,0.03538,0.0121,0.0623,1.0000 9.750,1.0188,0.04697,0.03953,0.0140,0.0612,1.0000 10.000,1.0210,0.05055,0.04359,0.0159,0.0597,1.0000 10.250,1.0197,0.05415,0.04758,0.0177,0.0583,1.0000 10.500,1.0124,0.05825,0.05206,0.0195,0.0581,1.0000 10.750,0.9976,0.06278,0.05693,0.0212,0.0589,1.0000 11.000,0.9775,0.06697,0.06135,0.0228,0.0597,1.0000 11.250,0.9559,0.07155,0.06610,0.0229,0.0606,1.0000 11.500,0.9335,0.07673,0.07144,0.0216,0.0614,1.0000 11.750,0.9126,0.08252,0.07733,0.0195,0.0623,1.0000 12.000,0.8961,0.08873,0.08360,0.0170,0.0632,1.0000 12.250,0.8290,0.10700,0.10199,0.0037,0.0758,1.0000 12.500,0.8415,0.11061,0.10566,0.0054,0.0775,1.0000 12.750,0.7547,0.14308,0.13786,-0.0212,0.1339,1.0000 13.000,0.6171,0.13728,0.13233,-0.0030,0.1440,1.0000