Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rae100-il-200000 Airfoil,rae100-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,46.112 Max Cl/Cd alpha,4.75 Url,http://www.airfoiltools.com/polar/csv?polar=xf-rae100-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.500,-0.7609,0.10135,0.09757,-0.0020,1.0000,0.0414 -12.250,-0.7712,0.09463,0.09088,-0.0044,1.0000,0.0407 -12.000,-0.8118,0.08070,0.07690,-0.0140,1.0000,0.0393 -11.750,-0.8592,0.06815,0.06418,-0.0244,1.0000,0.0382 -11.500,-0.8993,0.05989,0.05569,-0.0301,1.0000,0.0372 -11.250,-0.9402,0.05374,0.04923,-0.0312,1.0000,0.0364 -11.000,-0.9708,0.04944,0.04461,-0.0285,1.0000,0.0360 -10.750,-0.9868,0.04528,0.04005,-0.0262,1.0000,0.0358 -10.500,-0.9864,0.04229,0.03677,-0.0244,1.0000,0.0362 -10.250,-0.9819,0.03948,0.03369,-0.0227,1.0000,0.0368 -10.000,-0.9739,0.03691,0.03082,-0.0211,1.0000,0.0376 -9.750,-0.9626,0.03473,0.02835,-0.0195,1.0000,0.0388 -9.500,-0.9495,0.03279,0.02605,-0.0180,1.0000,0.0404 -9.250,-0.9342,0.03124,0.02411,-0.0164,1.0000,0.0414 -9.000,-0.9182,0.02799,0.02069,-0.0153,1.0000,0.0430 -8.750,-0.8981,0.02652,0.01916,-0.0144,1.0000,0.0447 -8.500,-0.8775,0.02539,0.01791,-0.0134,1.0000,0.0472 -8.250,-0.8563,0.02437,0.01667,-0.0123,1.0000,0.0499 -8.000,-0.8360,0.02250,0.01471,-0.0113,1.0000,0.0526 -7.750,-0.8145,0.02143,0.01364,-0.0104,1.0000,0.0557 -7.500,-0.7922,0.02062,0.01271,-0.0094,1.0000,0.0598 -7.250,-0.7717,0.01932,0.01141,-0.0083,1.0000,0.0644 -7.000,-0.7498,0.01853,0.01061,-0.0073,1.0000,0.0696 -6.750,-0.7290,0.01754,0.00959,-0.0061,1.0000,0.0761 -6.500,-0.7068,0.01689,0.00891,-0.0050,1.0000,0.0841 -6.250,-0.6863,0.01601,0.00810,-0.0038,1.0000,0.0939 -6.000,-0.6653,0.01526,0.00740,-0.0026,1.0000,0.1066 -5.750,-0.6440,0.01457,0.00676,-0.0014,1.0000,0.1234 -5.500,-0.6233,0.01386,0.00618,-0.0002,1.0000,0.1453 -5.250,-0.6022,0.01322,0.00570,0.0009,1.0000,0.1736 -5.000,-0.5811,0.01264,0.00529,0.0021,1.0000,0.2077 -4.750,-0.5596,0.01214,0.00493,0.0032,1.0000,0.2454 -4.500,-0.5382,0.01168,0.00465,0.0043,1.0000,0.2842 -4.250,-0.5166,0.01129,0.00441,0.0055,1.0000,0.3232 -4.000,-0.4950,0.01094,0.00421,0.0067,1.0000,0.3616 -3.750,-0.4735,0.01063,0.00403,0.0079,1.0000,0.3990 -3.500,-0.4521,0.01036,0.00390,0.0092,1.0000,0.4354 -3.250,-0.4308,0.01012,0.00379,0.0105,1.0000,0.4711 -3.000,-0.4098,0.00992,0.00370,0.0118,1.0000,0.5058 -2.750,-0.3892,0.00973,0.00365,0.0133,1.0000,0.5393 -2.500,-0.3690,0.00958,0.00363,0.0148,1.0000,0.5724 -2.250,-0.3493,0.00947,0.00365,0.0163,1.0000,0.6054 -2.000,-0.3303,0.00939,0.00370,0.0180,1.0000,0.6379 -1.750,-0.2985,0.00934,0.00379,0.0170,0.9952,0.6746 -1.500,-0.2536,0.00923,0.00385,0.0137,0.9850,0.7126 -1.250,-0.2101,0.00911,0.00386,0.0107,0.9738,0.7496 -0.750,-0.1229,0.00884,0.00385,0.0054,0.9520,0.8184 -0.500,-0.0808,0.00873,0.00383,0.0033,0.9388,0.8494 -0.250,-0.0412,0.00866,0.00383,0.0018,0.9214,0.8776 0.000,0.0000,0.00864,0.00384,0.0000,0.9011,0.9010 0.250,0.0412,0.00866,0.00383,-0.0018,0.8777,0.9213 0.500,0.0808,0.00873,0.00384,-0.0033,0.8494,0.9389 0.750,0.1229,0.00884,0.00385,-0.0054,0.8183,0.9519 1.000,0.1672,0.00898,0.00386,-0.0081,0.7852,0.9625 1.250,0.2101,0.00911,0.00386,-0.0108,0.7496,0.9738 1.500,0.2536,0.00924,0.00385,-0.0137,0.7126,0.9849 1.750,0.2984,0.00934,0.00379,-0.0170,0.6745,0.9952 2.000,0.3304,0.00939,0.00370,-0.0180,0.6376,1.0000 2.250,0.3495,0.00947,0.00365,-0.0164,0.6052,1.0000 2.500,0.3692,0.00958,0.00363,-0.0148,0.5725,1.0000 2.750,0.3894,0.00973,0.00365,-0.0133,0.5394,1.0000 3.000,0.4100,0.00992,0.00370,-0.0119,0.5059,1.0000 3.250,0.4310,0.01012,0.00379,-0.0105,0.4712,1.0000 3.500,0.4523,0.01036,0.00390,-0.0092,0.4352,1.0000 3.750,0.4736,0.01063,0.00403,-0.0079,0.3989,1.0000 4.000,0.4952,0.01094,0.00421,-0.0067,0.3615,1.0000 4.250,0.5168,0.01129,0.00441,-0.0055,0.3231,1.0000 4.500,0.5384,0.01168,0.00465,-0.0044,0.2841,1.0000 4.750,0.5598,0.01214,0.00493,-0.0032,0.2454,1.0000 5.000,0.5813,0.01264,0.00529,-0.0021,0.2075,1.0000 5.250,0.6024,0.01322,0.00570,-0.0010,0.1736,1.0000 5.500,0.6234,0.01386,0.00619,0.0002,0.1452,1.0000 5.750,0.6442,0.01457,0.00676,0.0014,0.1234,1.0000 6.000,0.6654,0.01526,0.00740,0.0026,0.1065,1.0000 6.250,0.6864,0.01600,0.00810,0.0038,0.0938,1.0000 6.500,0.7068,0.01689,0.00891,0.0050,0.0841,1.0000 6.750,0.7290,0.01753,0.00959,0.0061,0.0760,1.0000 7.000,0.7497,0.01853,0.01061,0.0073,0.0696,1.0000 7.250,0.7716,0.01933,0.01142,0.0083,0.0644,1.0000 7.500,0.7921,0.02065,0.01274,0.0094,0.0599,1.0000 7.750,0.8144,0.02145,0.01365,0.0104,0.0558,1.0000 8.000,0.8358,0.02250,0.01471,0.0114,0.0526,1.0000 8.250,0.8562,0.02436,0.01666,0.0124,0.0499,1.0000 8.500,0.8774,0.02538,0.01790,0.0135,0.0472,1.0000 8.750,0.8979,0.02655,0.01919,0.0145,0.0448,1.0000 9.000,0.9180,0.02798,0.02068,0.0154,0.0430,1.0000 9.250,0.9340,0.03127,0.02414,0.0164,0.0415,1.0000 9.500,0.9494,0.03272,0.02598,0.0180,0.0403,1.0000 9.750,0.9623,0.03477,0.02839,0.0196,0.0390,1.0000 10.000,0.9734,0.03696,0.03088,0.0212,0.0377,1.0000 10.250,0.9820,0.03941,0.03361,0.0227,0.0367,1.0000 10.500,0.9851,0.04241,0.03692,0.0245,0.0364,1.0000 10.750,0.9868,0.04522,0.03999,0.0262,0.0358,1.0000 11.000,0.9761,0.04891,0.04400,0.0283,0.0358,1.0000 11.250,0.9404,0.05370,0.04918,0.0313,0.0364,1.0000 11.500,0.8979,0.06009,0.05590,0.0300,0.0375,1.0000 11.750,0.8590,0.06816,0.06419,0.0244,0.0381,1.0000 12.000,0.8112,0.08086,0.07707,0.0138,0.0393,1.0000 12.250,0.7723,0.09445,0.09070,0.0045,0.0407,1.0000 12.500,0.7612,0.10139,0.09761,0.0018,0.0414,1.0000