Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca0010-il-50000-n5 Airfoil,naca0010-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,25.7191 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-naca0010-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.8297,0.07541,0.06782,-0.0232,1.0000,0.0595 -10.500,-0.8517,0.07046,0.06270,-0.0240,1.0000,0.0595 -10.250,-0.8713,0.06587,0.05785,-0.0235,1.0000,0.0596 -10.000,-0.8721,0.06242,0.05434,-0.0228,1.0000,0.0608 -9.750,-0.8666,0.05990,0.05175,-0.0220,1.0000,0.0629 -9.500,-0.8659,0.05668,0.04829,-0.0211,1.0000,0.0649 -9.250,-0.8657,0.05301,0.04425,-0.0199,1.0000,0.0668 -9.000,-0.8623,0.04925,0.04002,-0.0186,1.0000,0.0684 -8.750,-0.8549,0.04575,0.03595,-0.0172,1.0000,0.0704 -8.500,-0.8423,0.04300,0.03286,-0.0160,1.0000,0.0735 -8.250,-0.8250,0.04102,0.03076,-0.0151,1.0000,0.0771 -8.000,-0.8070,0.03866,0.02807,-0.0141,1.0000,0.0801 -7.750,-0.7872,0.03639,0.02534,-0.0131,1.0000,0.0834 -7.500,-0.7667,0.03458,0.02341,-0.0123,1.0000,0.0881 -7.250,-0.7454,0.03305,0.02176,-0.0114,1.0000,0.0935 -7.000,-0.7219,0.03138,0.01975,-0.0105,1.0000,0.0985 -6.750,-0.6997,0.02989,0.01831,-0.0096,1.0000,0.1037 -6.500,-0.6771,0.02859,0.01681,-0.0087,1.0000,0.1120 -6.250,-0.6563,0.02738,0.01565,-0.0077,1.0000,0.1232 -6.000,-0.6352,0.02617,0.01445,-0.0066,1.0000,0.1372 -5.750,-0.6141,0.02497,0.01327,-0.0056,1.0000,0.1563 -5.500,-0.5940,0.02382,0.01224,-0.0046,1.0000,0.1856 -5.250,-0.5744,0.02272,0.01140,-0.0035,1.0000,0.2264 -5.000,-0.5553,0.02172,0.01071,-0.0023,1.0000,0.2809 -4.750,-0.5365,0.02086,0.01016,-0.0009,1.0000,0.3432 -4.500,-0.5174,0.02016,0.00969,0.0007,1.0000,0.4043 -4.250,-0.4984,0.01959,0.00932,0.0026,1.0000,0.4613 -4.000,-0.4792,0.01912,0.00903,0.0045,1.0000,0.5163 -3.750,-0.4595,0.01872,0.00881,0.0066,1.0000,0.5689 -3.500,-0.4392,0.01840,0.00862,0.0088,1.0000,0.6193 -3.250,-0.4182,0.01816,0.00849,0.0109,1.0000,0.6669 -3.000,-0.3959,0.01799,0.00840,0.0130,1.0000,0.7117 -2.750,-0.3721,0.01790,0.00833,0.0147,1.0000,0.7542 -2.500,-0.3464,0.01786,0.00828,0.0161,1.0000,0.7953 -2.250,-0.3153,0.01789,0.00828,0.0164,1.0000,0.8324 -2.000,-0.2812,0.01794,0.00824,0.0159,1.0000,0.8677 -1.750,-0.2421,0.01800,0.00819,0.0142,1.0000,0.8996 -1.500,-0.1958,0.01804,0.00810,0.0108,1.0000,0.9266 -1.250,-0.1450,0.01803,0.00797,0.0062,1.0000,0.9505 -1.000,-0.0925,0.01794,0.00777,0.0009,1.0000,0.9724 -0.750,-0.0386,0.01776,0.00752,-0.0049,1.0000,0.9917 -0.500,-0.0110,0.01757,0.00732,-0.0060,1.0000,1.0000 -0.250,-0.0053,0.01745,0.00721,-0.0031,1.0000,1.0000 0.000,0.0000,0.01742,0.00718,0.0000,1.0000,1.0000 0.250,0.0053,0.01745,0.00721,0.0031,1.0000,1.0000 0.500,0.0110,0.01757,0.00731,0.0060,1.0000,1.0000 0.750,0.0386,0.01776,0.00752,0.0049,0.9917,1.0000 1.000,0.0925,0.01794,0.00777,-0.0009,0.9724,1.0000 1.250,0.1450,0.01803,0.00796,-0.0062,0.9505,1.0000 1.500,0.1958,0.01804,0.00810,-0.0108,0.9266,1.0000 1.750,0.2420,0.01800,0.00819,-0.0142,0.8996,1.0000 2.000,0.2811,0.01794,0.00824,-0.0159,0.8677,1.0000 2.250,0.3153,0.01789,0.00828,-0.0164,0.8324,1.0000 2.500,0.3463,0.01786,0.00828,-0.0161,0.7953,1.0000 2.750,0.3720,0.01790,0.00833,-0.0147,0.7542,1.0000 3.000,0.3959,0.01799,0.00840,-0.0130,0.7117,1.0000 3.250,0.4181,0.01816,0.00849,-0.0109,0.6669,1.0000 3.500,0.4392,0.01840,0.00862,-0.0088,0.6193,1.0000 3.750,0.4594,0.01872,0.00881,-0.0066,0.5689,1.0000 4.000,0.4791,0.01912,0.00903,-0.0045,0.5163,1.0000 4.250,0.4984,0.01959,0.00932,-0.0025,0.4614,1.0000 4.500,0.5173,0.02016,0.00969,-0.0007,0.4043,1.0000 4.750,0.5365,0.02086,0.01016,0.0009,0.3432,1.0000 5.000,0.5553,0.02172,0.01071,0.0023,0.2809,1.0000 5.250,0.5744,0.02271,0.01140,0.0035,0.2264,1.0000 5.500,0.5940,0.02382,0.01224,0.0046,0.1856,1.0000 5.750,0.6141,0.02497,0.01327,0.0056,0.1563,1.0000 6.000,0.6352,0.02617,0.01445,0.0066,0.1372,1.0000 6.250,0.6563,0.02738,0.01565,0.0077,0.1232,1.0000 6.500,0.6772,0.02859,0.01681,0.0087,0.1120,1.0000 6.750,0.6998,0.02989,0.01831,0.0096,0.1037,1.0000 7.000,0.7219,0.03138,0.01975,0.0105,0.0985,1.0000 7.250,0.7454,0.03305,0.02175,0.0114,0.0935,1.0000 7.500,0.7667,0.03458,0.02340,0.0123,0.0880,1.0000 7.750,0.7872,0.03638,0.02534,0.0131,0.0834,1.0000 8.000,0.8071,0.03866,0.02807,0.0141,0.0801,1.0000 8.250,0.8251,0.04102,0.03076,0.0151,0.0771,1.0000 8.500,0.8424,0.04300,0.03286,0.0160,0.0735,1.0000 8.750,0.8550,0.04575,0.03596,0.0172,0.0704,1.0000 9.000,0.8624,0.04926,0.04002,0.0186,0.0684,1.0000 9.250,0.8659,0.05301,0.04425,0.0199,0.0668,1.0000 9.500,0.8661,0.05668,0.04830,0.0210,0.0649,1.0000 9.750,0.8669,0.05990,0.05175,0.0220,0.0629,1.0000 10.000,0.8725,0.06241,0.05432,0.0228,0.0608,1.0000 10.250,0.8714,0.06590,0.05788,0.0234,0.0596,1.0000 10.500,0.8519,0.07050,0.06274,0.0239,0.0595,1.0000 10.750,0.8299,0.07546,0.06787,0.0231,0.0595,1.0000