Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-whitcomb-il-200000 Airfoil,whitcomb-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,30.0954 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-whitcomb-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.000,-0.7429,0.08477,0.08039,-0.0499,1.0000,0.0558 -11.750,-0.7360,0.08195,0.07759,-0.0490,1.0000,0.0550 -11.500,-0.7532,0.07631,0.07192,-0.0508,1.0000,0.0544 -11.250,-0.7827,0.07013,0.06566,-0.0526,1.0000,0.0536 -11.000,-0.8194,0.06444,0.05984,-0.0529,1.0000,0.0528 -10.750,-0.9536,0.05229,0.04685,-0.0498,1.0000,0.0490 -10.500,-0.9621,0.04835,0.04259,-0.0494,1.0000,0.0489 -10.250,-0.9517,0.04632,0.04054,-0.0486,1.0000,0.0495 -10.000,-0.9400,0.04457,0.03875,-0.0479,1.0000,0.0503 -9.750,-0.9317,0.04181,0.03576,-0.0476,1.0000,0.0508 -9.500,-0.9207,0.03882,0.03245,-0.0477,1.0000,0.0512 -9.250,-0.9058,0.03596,0.02927,-0.0478,1.0000,0.0517 -9.000,-0.8876,0.03351,0.02652,-0.0479,1.0000,0.0524 -8.750,-0.8670,0.03136,0.02407,-0.0480,1.0000,0.0533 -8.500,-0.8446,0.02952,0.02191,-0.0481,1.0000,0.0545 -8.250,-0.8207,0.02795,0.02003,-0.0483,1.0000,0.0558 -8.000,-0.7988,0.02652,0.01868,-0.0478,1.0000,0.0576 -7.750,-0.7746,0.02561,0.01773,-0.0477,1.0000,0.0596 -7.500,-0.7497,0.02463,0.01663,-0.0475,1.0000,0.0618 -7.250,-0.7236,0.02377,0.01556,-0.0475,1.0000,0.0638 -7.000,-0.7009,0.02254,0.01443,-0.0468,1.0000,0.0664 -6.750,-0.6752,0.02191,0.01381,-0.0468,1.0000,0.0697 -6.500,-0.6483,0.02135,0.01312,-0.0469,1.0000,0.0733 -6.250,-0.6239,0.02038,0.01229,-0.0465,1.0000,0.0771 -6.000,-0.5968,0.01984,0.01174,-0.0467,1.0000,0.0819 -5.750,-0.5697,0.01910,0.01105,-0.0470,1.0000,0.0873 -5.500,-0.5412,0.01858,0.01057,-0.0475,1.0000,0.0940 -5.250,-0.5113,0.01789,0.00997,-0.0485,1.0000,0.1025 -5.000,-0.4798,0.01728,0.00943,-0.0498,1.0000,0.1141 -4.750,-0.4460,0.01665,0.00894,-0.0517,1.0000,0.1312 -4.500,-0.4102,0.01602,0.00846,-0.0541,1.0000,0.1580 -4.250,-0.3693,0.01524,0.00801,-0.0579,1.0000,0.2048 -4.000,-0.3152,0.01406,0.00744,-0.0652,1.0000,0.3114 -3.750,-0.2792,0.01362,0.00837,-0.0669,1.0000,0.5311 -3.500,-0.2871,0.01514,0.01018,-0.0569,1.0000,0.5807 -3.250,-0.2573,0.01566,0.01060,-0.0573,1.0000,0.6294 -3.000,-0.2282,0.01628,0.01111,-0.0574,1.0000,0.6555 -2.750,-0.2203,0.01722,0.01208,-0.0518,1.0000,0.6636 -2.500,-0.2035,0.01793,0.01278,-0.0487,1.0000,0.6752 -2.250,-0.1808,0.01848,0.01329,-0.0472,1.0000,0.6880 -2.000,-0.1727,0.01906,0.01391,-0.0419,1.0000,0.6922 -1.750,-0.1464,0.01944,0.01425,-0.0416,1.0000,0.7040 -1.500,-0.1383,0.01985,0.01471,-0.0363,1.0000,0.7081 -1.250,-0.1111,0.02021,0.01504,-0.0363,1.0000,0.7199 -1.000,-0.1068,0.02054,0.01543,-0.0302,1.0000,0.7248 -0.750,-0.0823,0.02088,0.01578,-0.0295,1.0000,0.7368 -0.500,-0.0760,0.02107,0.01602,-0.0241,1.0000,0.7424 -0.250,-0.0482,0.02132,0.01627,-0.0245,1.0000,0.7532 0.000,-0.0428,0.02144,0.01646,-0.0190,1.0000,0.7604 0.250,-0.0207,0.02172,0.01677,-0.0173,0.9978,0.7725 0.500,0.0297,0.02221,0.01729,-0.0206,0.9855,0.7866 0.750,0.0674,0.02220,0.01734,-0.0215,0.9747,0.7949 1.000,0.1318,0.02212,0.01727,-0.0289,0.9620,0.8006 1.250,0.1670,0.02150,0.01672,-0.0293,0.9502,0.8038 1.500,0.2101,0.02087,0.01615,-0.0314,0.9369,0.8071 1.750,0.2619,0.01990,0.01526,-0.0349,0.9198,0.8101 2.000,0.3045,0.01896,0.01439,-0.0369,0.8971,0.8127 2.250,0.3405,0.01819,0.01369,-0.0379,0.8625,0.8149 2.500,0.4428,0.01787,0.01161,-0.0489,0.4658,0.8175 2.750,0.4541,0.01862,0.01167,-0.0460,0.3292,0.8190 3.000,0.4737,0.01930,0.01181,-0.0450,0.2243,0.8200 3.250,0.4956,0.01991,0.01203,-0.0443,0.1638,0.8217 3.500,0.5217,0.02045,0.01234,-0.0444,0.1310,0.8225 3.750,0.5492,0.02101,0.01274,-0.0448,0.1125,0.8228 4.000,0.5767,0.02149,0.01315,-0.0451,0.1007,0.8240 4.250,0.6059,0.02194,0.01358,-0.0457,0.0921,0.8249 4.500,0.6352,0.02267,0.01422,-0.0464,0.0855,0.8251 4.750,0.6659,0.02309,0.01466,-0.0473,0.0796,0.8252 5.000,0.6964,0.02406,0.01552,-0.0483,0.0750,0.8256 5.250,0.7274,0.02462,0.01617,-0.0491,0.0713,0.8265 5.500,0.7581,0.02525,0.01676,-0.0500,0.0675,0.8269 5.750,0.7899,0.02645,0.01795,-0.0512,0.0646,0.8269 6.000,0.8212,0.02733,0.01899,-0.0520,0.0622,0.8269 6.250,0.8520,0.02831,0.02006,-0.0528,0.0601,0.8270 6.500,0.8822,0.02934,0.02109,-0.0537,0.0581,0.8275 6.750,0.9119,0.03114,0.02300,-0.0545,0.0563,0.8281 7.000,0.9390,0.03246,0.02466,-0.0546,0.0548,0.8283 7.250,0.9651,0.03426,0.02677,-0.0545,0.0538,0.8282 7.500,0.9891,0.03637,0.02921,-0.0542,0.0531,0.8282 7.750,1.0101,0.03896,0.03218,-0.0534,0.0527,0.8281 8.000,1.0263,0.04221,0.03589,-0.0521,0.0527,0.8280 8.250,1.0380,0.04593,0.04009,-0.0503,0.0528,0.8283 8.500,1.0428,0.05053,0.04519,-0.0480,0.0534,0.8287 8.750,1.0418,0.05577,0.05088,-0.0455,0.0548,0.8288 9.000,1.0492,0.05994,0.05521,-0.0444,0.0560,0.8287 9.250,0.8888,0.08767,0.08452,-0.0382,0.0845,0.8276 9.500,0.8441,0.09842,0.09544,-0.0472,0.0828,0.8271