Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca24112-jf-100000-n5 Airfoil,naca24112-jf Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,43.4623 Max Cl/Cd alpha,9 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca24112-jf-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.5962,0.08244,0.07727,-0.0205,1.0000,0.0383 -9.750,-0.6094,0.07689,0.07167,-0.0236,1.0000,0.0381 -9.500,-0.6249,0.07207,0.06678,-0.0246,1.0000,0.0380 -9.250,-0.6388,0.06758,0.06217,-0.0244,1.0000,0.0379 -9.000,-0.6491,0.06284,0.05725,-0.0238,1.0000,0.0378 -8.750,-0.6568,0.05798,0.05213,-0.0227,1.0000,0.0378 -8.500,-0.6625,0.05295,0.04676,-0.0211,1.0000,0.0379 -8.250,-0.6664,0.04779,0.04112,-0.0189,1.0000,0.0382 -8.000,-0.6571,0.04517,0.03831,-0.0174,1.0000,0.0389 -7.750,-0.6410,0.04397,0.03709,-0.0163,1.0000,0.0399 -7.500,-0.6286,0.04176,0.03468,-0.0147,1.0000,0.0411 -7.250,-0.6177,0.03886,0.03141,-0.0127,1.0000,0.0422 -7.000,-0.6059,0.03582,0.02794,-0.0105,1.0000,0.0431 -6.750,-0.5923,0.03295,0.02458,-0.0083,1.0000,0.0441 -6.500,-0.5759,0.03095,0.02226,-0.0065,1.0000,0.0456 -6.250,-0.5570,0.03002,0.02131,-0.0052,1.0000,0.0471 -6.000,-0.5384,0.02880,0.01995,-0.0036,1.0000,0.0489 -5.750,-0.5192,0.02726,0.01816,-0.0020,1.0000,0.0505 -5.500,-0.4994,0.02579,0.01636,-0.0004,1.0000,0.0524 -5.250,-0.4803,0.02487,0.01547,0.0010,1.0000,0.0544 -5.000,-0.4547,0.02405,0.01461,0.0011,0.9968,0.0570 -4.750,-0.4126,0.02276,0.01313,-0.0017,0.9855,0.0604 -4.500,-0.3722,0.02171,0.01207,-0.0043,0.9728,0.0644 -4.250,-0.3337,0.02086,0.01119,-0.0064,0.9575,0.0690 -4.000,-0.2967,0.01996,0.01024,-0.0081,0.9406,0.0738 -3.750,-0.2624,0.01925,0.00959,-0.0093,0.9205,0.0795 -3.500,-0.2299,0.01857,0.00885,-0.0099,0.8980,0.0857 -3.250,-0.1996,0.01797,0.00829,-0.0101,0.8741,0.0932 -3.000,-0.1725,0.01744,0.00770,-0.0096,0.8474,0.1013 -2.750,-0.1463,0.01703,0.00721,-0.0088,0.8207,0.1120 -2.500,-0.1219,0.01660,0.00675,-0.0077,0.7929,0.1248 -2.250,-0.0978,0.01622,0.00632,-0.0066,0.7653,0.1433 -2.000,-0.0742,0.01575,0.00590,-0.0054,0.7386,0.1773 -1.750,-0.0628,0.01370,0.00555,-0.0026,0.7146,0.5615 -1.500,-0.0339,0.01334,0.00593,-0.0005,0.6888,0.7909 -1.250,0.0021,0.01366,0.00618,-0.0004,0.6617,0.8626 -1.000,0.0384,0.01404,0.00633,-0.0008,0.6359,0.9007 -0.750,0.0767,0.01441,0.00648,-0.0019,0.6098,0.9285 -0.500,0.1284,0.01483,0.00662,-0.0057,0.5836,0.9530 -0.250,0.1822,0.01510,0.00663,-0.0105,0.5579,0.9723 0.000,0.2221,0.01519,0.00649,-0.0130,0.5369,0.9813 0.250,0.2591,0.01523,0.00633,-0.0150,0.5181,0.9870 0.500,0.2952,0.01530,0.00622,-0.0169,0.5008,0.9933 0.750,0.3325,0.01534,0.00610,-0.0191,0.4849,0.9984 1.000,0.3603,0.01540,0.00604,-0.0194,0.4714,1.0000 1.250,0.3842,0.01548,0.00602,-0.0189,0.4593,1.0000 1.500,0.4080,0.01559,0.00601,-0.0183,0.4485,1.0000 1.750,0.4316,0.01571,0.00603,-0.0177,0.4382,1.0000 2.000,0.4553,0.01584,0.00610,-0.0171,0.4283,1.0000 2.250,0.4786,0.01601,0.00615,-0.0164,0.4197,1.0000 2.500,0.5022,0.01616,0.00628,-0.0157,0.4104,1.0000 2.750,0.5255,0.01637,0.00637,-0.0150,0.4029,1.0000 3.000,0.5490,0.01655,0.00657,-0.0143,0.3942,1.0000 3.250,0.5721,0.01677,0.00670,-0.0135,0.3871,1.0000 3.500,0.5955,0.01699,0.00694,-0.0128,0.3792,1.0000 3.750,0.6185,0.01723,0.00713,-0.0120,0.3723,1.0000 4.000,0.6417,0.01749,0.00739,-0.0113,0.3652,1.0000 4.250,0.6647,0.01775,0.00764,-0.0105,0.3582,1.0000 4.500,0.6876,0.01804,0.00791,-0.0096,0.3521,1.0000 4.750,0.7105,0.01833,0.00824,-0.0088,0.3449,1.0000 5.000,0.7332,0.01863,0.00851,-0.0080,0.3388,1.0000 5.250,0.7560,0.01896,0.00890,-0.0071,0.3322,1.0000 5.500,0.7786,0.01927,0.00924,-0.0063,0.3256,1.0000 5.750,0.8012,0.01962,0.00957,-0.0054,0.3199,1.0000 6.000,0.8235,0.01997,0.01003,-0.0046,0.3129,1.0000 6.250,0.8459,0.02031,0.01037,-0.0037,0.3070,1.0000 6.500,0.8680,0.02070,0.01085,-0.0028,0.3004,1.0000 6.750,0.8901,0.02107,0.01128,-0.0019,0.2939,1.0000 7.000,0.9121,0.02145,0.01168,-0.0009,0.2881,1.0000 7.250,0.9335,0.02186,0.01224,0.0000,0.2810,1.0000 7.500,0.9553,0.02222,0.01259,0.0010,0.2750,1.0000 7.750,0.9762,0.02268,0.01321,0.0020,0.2677,1.0000 8.000,0.9974,0.02305,0.01364,0.0029,0.2610,1.0000 8.250,1.0180,0.02351,0.01421,0.0040,0.2539,1.0000 8.500,1.0385,0.02392,0.01469,0.0050,0.2465,1.0000 8.750,1.0586,0.02438,0.01528,0.0060,0.2390,1.0000 9.000,1.0783,0.02481,0.01579,0.0071,0.2311,1.0000 9.250,1.0974,0.02532,0.01643,0.0082,0.2228,1.0000 9.500,1.1160,0.02576,0.01692,0.0094,0.2148,1.0000 9.750,1.1338,0.02635,0.01768,0.0106,0.2054,1.0000 10.000,1.1508,0.02691,0.01829,0.0118,0.1968,1.0000 10.250,1.1667,0.02754,0.01903,0.0131,0.1873,1.0000 10.500,1.1817,0.02827,0.01991,0.0145,0.1776,1.0000 10.750,1.1949,0.02905,0.02075,0.0160,0.1684,1.0000 11.000,1.2062,0.02994,0.02171,0.0176,0.1587,1.0000 11.250,1.2160,0.03096,0.02287,0.0193,0.1490,1.0000 11.500,1.2219,0.03211,0.02408,0.0213,0.1403,1.0000 11.750,1.2234,0.03345,0.02548,0.0236,0.1323,1.0000 12.000,1.2245,0.03506,0.02721,0.0253,0.1244,1.0000 12.250,1.2215,0.03711,0.02928,0.0267,0.1179,1.0000 12.500,1.2196,0.03947,0.03180,0.0272,0.1108,1.0000 12.750,1.2124,0.04252,0.03487,0.0272,0.1057,1.0000 13.000,1.2069,0.04585,0.03838,0.0265,0.0999,1.0000 13.250,1.1969,0.04993,0.04252,0.0252,0.0956,1.0000 13.500,1.1867,0.05429,0.04698,0.0236,0.0917,1.0000 13.750,1.1755,0.05899,0.05182,0.0217,0.0878,1.0000 14.000,1.1622,0.06404,0.05693,0.0196,0.0847,1.0000 14.250,1.1496,0.06902,0.06196,0.0176,0.0818,1.0000 14.500,1.1372,0.07417,0.06727,0.0155,0.0786,1.0000 14.750,1.1246,0.07933,0.07251,0.0134,0.0757,1.0000 15.000,1.1142,0.08414,0.07733,0.0115,0.0732,1.0000 15.250,1.1045,0.08907,0.08234,0.0096,0.0705,1.0000