Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-usa32-il-1000000-n5 Airfoil,usa32-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,67.929 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-usa32-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.250,0.2317,0.08879,0.08606,-0.1726,0.8516,0.0129 -12.000,0.2447,0.08718,0.08443,-0.1738,0.8475,0.0131 -11.750,0.2523,0.08474,0.08199,-0.1749,0.8438,0.0132 -10.750,0.2670,0.07165,0.06883,-0.1815,0.8249,0.0157 -10.500,0.2798,0.07022,0.06739,-0.1824,0.8200,0.0159 -10.250,0.2933,0.06881,0.06595,-0.1835,0.8145,0.0161 -9.750,0.0014,0.02829,0.02493,-0.1923,0.7957,0.0195 -9.500,-0.0011,0.02515,0.02160,-0.1904,0.7902,0.0197 -9.250,0.0025,0.02276,0.01902,-0.1882,0.7830,0.0199 -9.000,0.0152,0.02159,0.01771,-0.1864,0.7745,0.0201 -8.750,0.0213,0.02016,0.01607,-0.1832,0.7628,0.0204 -8.500,0.0232,0.01928,0.01500,-0.1785,0.7452,0.0207 -8.250,-0.0041,0.01912,0.01450,-0.1671,0.6798,0.0207 -8.000,-0.0111,0.01863,0.01374,-0.1603,0.6489,0.0209 -7.750,-0.0069,0.01783,0.01274,-0.1558,0.6379,0.0212 -7.250,0.0146,0.01655,0.01113,-0.1492,0.6248,0.0216 -7.000,0.0307,0.01613,0.01058,-0.1468,0.6202,0.0218 -6.750,0.0447,0.01573,0.01005,-0.1440,0.6146,0.0220 -6.250,0.0741,0.01478,0.00893,-0.1387,0.6054,0.0224 -6.000,0.0922,0.01447,0.00855,-0.1366,0.6009,0.0225 -5.750,0.1100,0.01420,0.00822,-0.1345,0.5964,0.0227 -5.500,0.1273,0.01397,0.00791,-0.1323,0.5921,0.0228 -5.250,0.1462,0.01373,0.00761,-0.1303,0.5889,0.0230 -5.000,0.1673,0.01352,0.00736,-0.1288,0.5866,0.0233 -4.750,0.1878,0.01326,0.00704,-0.1272,0.5840,0.0234 -4.500,0.2087,0.01307,0.00680,-0.1256,0.5812,0.0237 -4.250,0.2292,0.01293,0.00660,-0.1240,0.5778,0.0240 -4.000,0.2493,0.01276,0.00637,-0.1223,0.5750,0.0243 -3.750,0.2691,0.01262,0.00617,-0.1205,0.5719,0.0245 -3.500,0.2906,0.01244,0.00595,-0.1191,0.5695,0.0248 -3.250,0.3125,0.01227,0.00575,-0.1177,0.5673,0.0250 -3.000,0.3343,0.01212,0.00556,-0.1164,0.5649,0.0252 -2.750,0.3560,0.01199,0.00540,-0.1150,0.5621,0.0253 -2.500,0.3772,0.01190,0.00527,-0.1135,0.5587,0.0255 -2.250,0.3977,0.01183,0.00515,-0.1119,0.5552,0.0256 -2.000,0.4188,0.01174,0.00503,-0.1104,0.5523,0.0257 -1.750,0.4410,0.01153,0.00481,-0.1092,0.5499,0.0261 -1.500,0.4632,0.01142,0.00468,-0.1079,0.5469,0.0263 -1.250,0.4850,0.01134,0.00459,-0.1066,0.5434,0.0266 -1.000,0.5063,0.01132,0.00456,-0.1052,0.5394,0.0269 -0.750,0.5262,0.01132,0.00452,-0.1036,0.5347,0.0273 -0.500,0.5496,0.01127,0.00447,-0.1026,0.5306,0.0278 -0.250,0.5718,0.01125,0.00443,-0.1014,0.5255,0.0281 0.000,0.5914,0.01128,0.00443,-0.0998,0.5197,0.0284 0.250,0.6125,0.01131,0.00443,-0.0984,0.5146,0.0288 0.500,0.6337,0.01134,0.00444,-0.0971,0.5076,0.0292 0.750,0.6528,0.01142,0.00448,-0.0953,0.5001,0.0294 1.000,0.6723,0.01152,0.00454,-0.0937,0.4889,0.0297 1.250,0.6905,0.01164,0.00461,-0.0919,0.4800,0.0302 1.500,0.7086,0.01177,0.00469,-0.0901,0.4699,0.0305 1.750,0.7263,0.01193,0.00480,-0.0882,0.4579,0.0314 2.000,0.7443,0.01212,0.00493,-0.0864,0.4486,0.0319 2.250,0.7633,0.01228,0.00506,-0.0848,0.4397,0.0327 2.500,0.7809,0.01249,0.00523,-0.0829,0.4315,0.0340 3.000,0.8188,0.01287,0.00555,-0.0798,0.4170,0.0368 3.500,0.8585,0.01296,0.00590,-0.0772,0.4055,0.1613 3.750,0.8757,0.01321,0.00618,-0.0755,0.3988,0.1884 4.000,0.8960,0.01341,0.00639,-0.0743,0.3932,0.1983 4.250,0.9154,0.01364,0.00662,-0.0730,0.3869,0.2061 4.500,0.9336,0.01393,0.00689,-0.0715,0.3802,0.2161 4.750,0.9545,0.01414,0.00710,-0.0705,0.3750,0.2215 5.000,0.9741,0.01438,0.00736,-0.0693,0.3705,0.2298 5.250,0.9914,0.01474,0.00769,-0.0678,0.3636,0.2352 5.750,1.0332,0.01521,0.00819,-0.0660,0.3564,0.2468 6.250,1.0725,0.01581,0.00883,-0.0639,0.3480,0.2663 6.500,1.0915,0.01615,0.00917,-0.0628,0.3443,0.2726 6.750,1.1123,0.01643,0.00947,-0.0621,0.3407,0.2799 7.000,1.1330,0.01672,0.00980,-0.0613,0.3376,0.2891 7.250,1.1529,0.01706,0.01014,-0.0604,0.3342,0.2959 7.500,1.1717,0.01745,0.01055,-0.0594,0.3304,0.3038 7.750,1.1901,0.01787,0.01099,-0.0584,0.3269,0.3113 8.000,1.2107,0.01821,0.01135,-0.0578,0.3235,0.3169 8.250,1.2304,0.01859,0.01176,-0.0570,0.3195,0.3238 8.500,1.2502,0.01898,0.01216,-0.0563,0.3170,0.3295 8.750,1.2677,0.01947,0.01266,-0.0553,0.3134,0.3333 9.000,1.2855,0.01998,0.01319,-0.0544,0.3100,0.3377 9.250,1.3051,0.02041,0.01364,-0.0538,0.3052,0.3420 9.500,1.3237,0.02089,0.01414,-0.0531,0.3012,0.3461 9.750,1.3420,0.02140,0.01467,-0.0524,0.2985,0.3497 10.000,1.3588,0.02202,0.01531,-0.0515,0.2953,0.3533 10.250,1.3768,0.02257,0.01589,-0.0508,0.2911,0.3573 10.500,1.3957,0.02308,0.01644,-0.0503,0.2879,0.3626 10.750,1.4110,0.02380,0.01716,-0.0493,0.2817,0.3655 11.000,1.4256,0.02461,0.01798,-0.0484,0.2763,0.3693 11.250,1.4433,0.02524,0.01864,-0.0478,0.2716,0.3732 11.500,1.4559,0.02618,0.01957,-0.0467,0.2639,0.3763 11.750,1.4685,0.02715,0.02054,-0.0457,0.2550,0.3799 12.000,1.4791,0.02832,0.02169,-0.0446,0.2443,0.3844 12.250,1.4818,0.03007,0.02336,-0.0429,0.2245,0.3886 12.500,1.4862,0.03177,0.02500,-0.0413,0.2088,0.3933 12.750,1.4748,0.03472,0.02780,-0.0386,0.1812,0.3993 13.000,1.4809,0.03643,0.02952,-0.0376,0.1730,0.4074 13.250,1.4794,0.03882,0.03188,-0.0361,0.1604,0.4165 13.500,1.4906,0.04040,0.03354,-0.0360,0.1561,0.4454 14.000,1.6003,0.04583,0.03999,-0.0567,0.1377,0.9996 14.250,1.6087,0.04824,0.04241,-0.0572,0.1319,1.0000 14.500,1.6062,0.05076,0.04492,-0.0557,0.1223,1.0000 14.750,1.6081,0.05290,0.04709,-0.0546,0.1187,1.0000 15.000,1.5991,0.05614,0.05029,-0.0530,0.1066,1.0000 15.250,1.5952,0.05893,0.05309,-0.0518,0.0997,1.0000 15.500,1.5858,0.06230,0.05645,-0.0504,0.0912,1.0000 16.000,1.5658,0.06937,0.06351,-0.0480,0.0762,1.0000 16.250,1.5653,0.07198,0.06618,-0.0473,0.0751,1.0000 16.500,1.5564,0.07553,0.06975,-0.0464,0.0683,1.0000 16.750,1.5528,0.07855,0.07281,-0.0458,0.0656,1.0000 17.000,1.5433,0.08232,0.07660,-0.0452,0.0600,1.0000 17.250,1.5386,0.08557,0.07989,-0.0448,0.0572,1.0000 17.500,1.5255,0.08989,0.08421,-0.0444,0.0500,1.0000 17.750,1.5169,0.09371,0.08807,-0.0442,0.0458,1.0000 18.000,1.4895,0.10000,0.09433,-0.0440,0.0319,1.0000 18.250,1.4689,0.10558,0.09992,-0.0441,0.0206,1.0000