Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-usa32-il-50000-n5 Airfoil,usa32-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,13.5141 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-usa32-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.0610,0.13280,0.12624,-0.0733,0.9115,0.1178 -9.000,-0.0682,0.13264,0.12612,-0.0766,0.9039,0.1201 -8.750,-0.0638,0.12979,0.12332,-0.0773,0.8967,0.1209 -8.500,-0.0421,0.12484,0.11835,-0.0768,0.8907,0.1233 -8.250,-0.0254,0.12150,0.11500,-0.0788,0.8859,0.1265 -8.000,-0.0259,0.11969,0.11323,-0.0780,0.8760,0.1291 -7.750,-0.0262,0.11812,0.11168,-0.0800,0.8686,0.1333 -7.500,-0.0482,0.11844,0.11207,-0.0787,0.8558,0.1345 -7.250,-0.0543,0.11687,0.11055,-0.0803,0.8490,0.1352 -7.000,-0.0186,0.11106,0.10469,-0.0787,0.8441,0.1402 -6.750,-0.0210,0.10939,0.10305,-0.0775,0.8348,0.1431 -6.500,-0.0316,0.10838,0.10208,-0.0758,0.8254,0.1462 -6.250,-0.0450,0.10771,0.10143,-0.0761,0.8155,0.1489 -6.000,-0.0629,0.10745,0.10118,-0.0749,0.8036,0.1497 -5.750,-0.0559,0.10459,0.09830,-0.0767,0.7977,0.1501 -5.250,-0.0576,0.09357,0.08704,-0.0794,0.7820,0.0927 -5.000,-0.0388,0.09038,0.08384,-0.0784,0.7789,0.0899 -4.750,-0.0494,0.08923,0.08271,-0.0752,0.7681,0.0890 -4.500,-0.0338,0.08567,0.07906,-0.0770,0.7636,0.0871 -4.000,-0.0202,0.07821,0.07125,-0.0802,0.7488,0.0803 -3.750,0.0030,0.07494,0.06786,-0.0814,0.7456,0.0792 -3.500,-0.0008,0.07382,0.06669,-0.0786,0.7353,0.0786 -3.250,0.0221,0.07035,0.06303,-0.0800,0.7313,0.0774 -3.000,0.0300,0.06825,0.06079,-0.0791,0.7235,0.0771 -2.750,0.0485,0.06515,0.05745,-0.0796,0.7178,0.0776 -2.500,0.0763,0.06073,0.05264,-0.0814,0.7144,0.0780 -2.250,0.0834,0.05840,0.05000,-0.0798,0.7062,0.0777 -2.000,0.1057,0.05512,0.04624,-0.0798,0.7013,0.0772 -1.750,0.1361,0.05166,0.04211,-0.0803,0.6981,0.0774 -1.500,0.1448,0.05082,0.04088,-0.0779,0.6894,0.0777 -1.250,0.1727,0.04910,0.03860,-0.0778,0.6846,0.0795 -1.000,0.2090,0.04749,0.03661,-0.0786,0.6814,0.0820 -0.750,0.2176,0.04780,0.03682,-0.0763,0.6718,0.0837 -0.500,0.2498,0.04687,0.03565,-0.0767,0.6672,0.0860 -0.250,0.3000,0.04569,0.03408,-0.0798,0.6644,0.0894 0.000,0.3174,0.04638,0.03456,-0.0792,0.6543,0.0917 0.250,0.3616,0.04577,0.03388,-0.0818,0.6500,0.0989 0.500,0.4127,0.04481,0.03286,-0.0852,0.6473,0.1112 1.000,0.4595,0.04555,0.03401,-0.0844,0.6321,0.1581 1.250,0.4912,0.04525,0.03356,-0.0837,0.6291,0.2231 1.750,0.5020,0.04731,0.03557,-0.0765,0.6123,0.2788 2.000,0.5272,0.04702,0.03515,-0.0747,0.6096,0.3118 2.500,0.5485,0.04897,0.03697,-0.0704,0.5923,0.3495 2.750,0.5960,0.04811,0.03587,-0.0730,0.5903,0.3613 3.250,0.6289,0.05019,0.03778,-0.0717,0.5728,0.3719 3.750,0.6571,0.05262,0.04005,-0.0700,0.5556,0.3813 4.000,0.7003,0.05182,0.03912,-0.0718,0.5534,0.3886 4.500,0.7172,0.05494,0.04220,-0.0691,0.5363,0.4000 5.000,0.7303,0.05839,0.04564,-0.0661,0.5197,0.4110 5.500,0.7393,0.06242,0.04968,-0.0633,0.5037,0.4218 5.750,0.7684,0.06200,0.04925,-0.0631,0.5015,0.4326 6.250,0.7708,0.06665,0.05398,-0.0600,0.4858,0.4474 6.750,0.7688,0.07205,0.05953,-0.0573,0.4712,0.4655 7.000,0.7928,0.07209,0.05972,-0.0569,0.4687,0.4913 8.000,0.8446,0.08588,0.07430,-0.0652,0.4419,1.0000 8.250,0.8566,0.08749,0.07587,-0.0644,0.4377,1.0000 8.500,0.8780,0.08805,0.07636,-0.0637,0.4351,1.0000 9.000,0.8615,0.09607,0.08445,-0.0619,0.4218,1.0000 9.250,0.8789,0.09709,0.08542,-0.0612,0.4186,1.0000 9.500,0.9029,0.09733,0.08561,-0.0606,0.4164,1.0000 10.000,0.8868,0.10516,0.09354,-0.0591,0.4020,1.0000 10.250,0.9128,0.10498,0.09331,-0.0583,0.3992,1.0000 10.500,0.8894,0.11046,0.09887,-0.0576,0.3881,1.0000 10.750,0.9100,0.11075,0.09914,-0.0568,0.3838,1.0000 11.000,0.9383,0.11011,0.09848,-0.0560,0.3810,1.0000 11.250,0.9118,0.11611,0.10457,-0.0557,0.3692,1.0000 11.500,0.9320,0.11647,0.10493,-0.0549,0.3654,1.0000 11.750,0.9581,0.11612,0.10457,-0.0541,0.3630,1.0000 12.000,0.9305,0.12248,0.11103,-0.0542,0.3508,1.0000 12.250,0.9511,0.12274,0.11132,-0.0535,0.3472,1.0000