Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-usa22-il-50000-n5 Airfoil,usa22-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,37.264 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-usa22-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.3535,0.10966,0.10320,-0.0175,1.0000,0.0993 -8.250,-0.3596,0.10803,0.10170,-0.0208,1.0000,0.1003 -8.000,-0.3593,0.10502,0.09882,-0.0227,1.0000,0.1008 -7.750,-0.3415,0.09964,0.09343,-0.0205,1.0000,0.1028 -7.500,-0.3357,0.09636,0.09021,-0.0207,1.0000,0.1042 -7.250,-0.3328,0.09328,0.08722,-0.0219,1.0000,0.1046 -7.000,-0.3299,0.08601,0.07994,-0.0300,1.0000,0.0566 -6.750,-0.3237,0.08252,0.07651,-0.0302,1.0000,0.0548 -6.500,-0.3186,0.07896,0.07303,-0.0318,1.0000,0.0539 -6.250,-0.3133,0.07537,0.06949,-0.0338,1.0000,0.0536 -6.000,-0.3071,0.07168,0.06585,-0.0359,1.0000,0.0538 -5.750,-0.2996,0.06789,0.06208,-0.0381,1.0000,0.0541 -5.500,-0.2909,0.06398,0.05815,-0.0402,1.0000,0.0543 -5.250,-0.2805,0.05993,0.05406,-0.0422,1.0000,0.0542 -5.000,-0.2682,0.05573,0.04975,-0.0443,1.0000,0.0538 -4.750,-0.2531,0.05119,0.04504,-0.0466,1.0000,0.0536 -4.500,-0.2349,0.04641,0.03996,-0.0492,1.0000,0.0540 -4.250,-0.1851,0.03902,0.03144,-0.0580,0.9906,0.0581 -4.000,-0.1443,0.03547,0.02768,-0.0625,0.9794,0.0623 -3.750,-0.0994,0.03181,0.02319,-0.0670,0.9680,0.0700 -3.500,-0.0569,0.02900,0.01984,-0.0705,0.9559,0.0775 -3.250,-0.0146,0.02702,0.01737,-0.0735,0.9431,0.0893 -3.000,0.0281,0.02532,0.01526,-0.0761,0.9303,0.0982 -2.750,0.0687,0.02407,0.01379,-0.0783,0.9164,0.1088 -2.500,0.1077,0.02318,0.01268,-0.0800,0.9012,0.1251 -2.250,0.1464,0.02227,0.01157,-0.0815,0.8853,0.1404 -2.000,0.1826,0.02152,0.01080,-0.0826,0.8683,0.1719 -1.750,0.2160,0.02100,0.01045,-0.0832,0.8501,0.2293 -1.500,0.2464,0.02078,0.01017,-0.0831,0.8298,0.2918 -1.250,0.2763,0.02046,0.00978,-0.0831,0.8108,0.3516 -1.000,0.3040,0.01988,0.00931,-0.0827,0.7918,0.4182 -0.750,0.3300,0.01914,0.00889,-0.0819,0.7727,0.4805 -0.500,0.3644,0.01775,0.00847,-0.0817,0.7544,1.0000 -0.250,0.3931,0.01791,0.00819,-0.0813,0.7367,1.0000 0.000,0.4205,0.01811,0.00800,-0.0807,0.7189,1.0000 0.250,0.4472,0.01835,0.00793,-0.0801,0.7014,1.0000 0.500,0.4737,0.01861,0.00791,-0.0795,0.6848,1.0000 0.750,0.5000,0.01888,0.00793,-0.0789,0.6688,1.0000 1.000,0.5261,0.01918,0.00800,-0.0784,0.6537,1.0000 1.250,0.5522,0.01948,0.00811,-0.0778,0.6392,1.0000 1.500,0.5786,0.01980,0.00826,-0.0774,0.6253,1.0000 1.750,0.6049,0.02013,0.00844,-0.0769,0.6121,1.0000 2.000,0.6312,0.02046,0.00863,-0.0765,0.5993,1.0000 2.250,0.6576,0.02079,0.00883,-0.0760,0.5873,1.0000 2.500,0.6833,0.02116,0.00912,-0.0755,0.5744,1.0000 2.750,0.7089,0.02154,0.00943,-0.0750,0.5618,1.0000 3.000,0.7343,0.02192,0.00978,-0.0745,0.5495,1.0000 3.250,0.7597,0.02230,0.01011,-0.0740,0.5376,1.0000 3.500,0.7852,0.02268,0.01042,-0.0734,0.5261,1.0000 3.750,0.8107,0.02305,0.01078,-0.0729,0.5148,1.0000 4.000,0.8353,0.02351,0.01125,-0.0723,0.5025,1.0000 4.250,0.8599,0.02396,0.01174,-0.0718,0.4907,1.0000 4.500,0.8847,0.02442,0.01224,-0.0712,0.4795,1.0000 4.750,0.9098,0.02485,0.01267,-0.0706,0.4689,1.0000 5.000,0.9340,0.02537,0.01325,-0.0700,0.4574,1.0000 5.250,0.9578,0.02593,0.01392,-0.0694,0.4458,1.0000 5.500,0.9818,0.02650,0.01461,-0.0688,0.4351,1.0000 5.750,1.0065,0.02701,0.01516,-0.0682,0.4252,1.0000 6.000,1.0295,0.02767,0.01598,-0.0675,0.4138,1.0000 6.250,1.0523,0.02839,0.01687,-0.0668,0.4030,1.0000 6.500,1.0757,0.02904,0.01769,-0.0662,0.3930,1.0000 6.750,1.0989,0.02970,0.01849,-0.0655,0.3831,1.0000 7.000,1.1202,0.03060,0.01964,-0.0647,0.3727,1.0000 7.250,1.1430,0.03138,0.02059,-0.0640,0.3641,1.0000 7.500,1.1649,0.03222,0.02167,-0.0632,0.3549,1.0000 7.750,1.1843,0.03292,0.02266,-0.0621,0.3427,1.0000 8.000,1.2016,0.03268,0.02245,-0.0603,0.3226,1.0000 8.250,1.2137,0.03290,0.02283,-0.0582,0.2988,1.0000 8.500,1.2290,0.03340,0.02348,-0.0566,0.2821,1.0000 8.750,1.2417,0.03410,0.02434,-0.0548,0.2628,1.0000 9.000,1.2517,0.03497,0.02531,-0.0529,0.2402,1.0000 9.250,1.2582,0.03619,0.02658,-0.0509,0.2137,1.0000 9.500,1.2629,0.03775,0.02819,-0.0489,0.1869,1.0000 9.750,1.2621,0.03973,0.03016,-0.0467,0.1544,1.0000 10.000,1.2543,0.04253,0.03277,-0.0447,0.0952,1.0000 10.250,1.2325,0.04718,0.03696,-0.0438,0.0620,1.0000 10.500,1.2165,0.05194,0.04173,-0.0440,0.0503,1.0000 10.750,1.2045,0.05667,0.04653,-0.0447,0.0463,1.0000 11.000,1.1925,0.06169,0.05168,-0.0458,0.0437,1.0000 11.250,1.1811,0.06683,0.05696,-0.0472,0.0420,1.0000 11.500,1.1699,0.07211,0.06241,-0.0488,0.0405,1.0000 11.750,1.1584,0.07752,0.06799,-0.0504,0.0394,1.0000 12.000,1.1467,0.08302,0.07366,-0.0521,0.0384,1.0000 12.250,1.1352,0.08857,0.07934,-0.0538,0.0375,1.0000 12.500,1.1240,0.09409,0.08499,-0.0556,0.0367,1.0000