Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m22-il-200000 Airfoil,m22-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,74.8987 Max Cl/Cd alpha,6.5 Url,http://airfoiltools.com/polar/csv?polar=xf-m22-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr 0.250,0.3035,0.02488,0.01759,-0.0243,0.5873,0.0948 0.500,0.3331,0.02400,0.01653,-0.0245,0.5820,0.1052 0.750,0.3621,0.02332,0.01567,-0.0245,0.5768,0.1179 1.000,0.3895,0.02253,0.01469,-0.0244,0.5729,0.1315 1.250,0.4172,0.02151,0.01366,-0.0248,0.5676,0.1463 2.000,0.5095,0.01869,0.01004,-0.0236,0.5538,0.0871 2.250,0.5392,0.01774,0.00893,-0.0234,0.5489,0.0735 2.500,0.5670,0.01701,0.00810,-0.0232,0.5450,0.0699 2.750,0.5951,0.01656,0.00761,-0.0231,0.5400,0.0673 3.000,0.6225,0.01619,0.00725,-0.0230,0.5348,0.0664 3.250,0.6492,0.01592,0.00694,-0.0227,0.5308,0.0672 3.500,0.6764,0.01580,0.00690,-0.0227,0.5262,0.0698 3.750,0.7034,0.01572,0.00684,-0.0226,0.5209,0.0744 4.000,0.7300,0.01563,0.00672,-0.0223,0.5168,0.0885 4.250,0.8034,0.01432,0.00707,-0.0325,0.5101,1.0000 4.500,0.8295,0.01450,0.00724,-0.0323,0.5054,1.0000 4.750,0.8551,0.01468,0.00733,-0.0318,0.5017,1.0000 5.000,0.8815,0.01495,0.00769,-0.0319,0.4963,1.0000 5.250,0.9066,0.01478,0.00741,-0.0312,0.4877,1.0000 5.500,0.9317,0.01435,0.00691,-0.0304,0.4725,1.0000 5.750,0.9578,0.01431,0.00699,-0.0303,0.4619,1.0000 6.000,0.9837,0.01427,0.00701,-0.0300,0.4510,1.0000 6.250,1.0093,0.01388,0.00660,-0.0295,0.4244,1.0000 6.500,1.0351,0.01382,0.00651,-0.0293,0.3906,1.0000 6.750,1.0596,0.01442,0.00681,-0.0294,0.3118,1.0000 7.000,1.0675,0.01928,0.01000,-0.0311,0.0396,1.0000 7.250,1.0877,0.02040,0.01123,-0.0307,0.0323,1.0000 7.500,1.1075,0.02142,0.01244,-0.0302,0.0307,1.0000 7.750,1.1247,0.02268,0.01391,-0.0295,0.0295,1.0000 8.000,1.1380,0.02423,0.01566,-0.0288,0.0288,1.0000 8.250,1.1466,0.02609,0.01771,-0.0279,0.0282,1.0000 8.500,1.1507,0.02830,0.02004,-0.0273,0.0271,1.0000 8.750,1.1480,0.03071,0.02252,-0.0262,0.0261,1.0000 9.000,1.1456,0.03318,0.02505,-0.0249,0.0253,1.0000 9.250,1.1461,0.03551,0.02743,-0.0236,0.0250,1.0000 9.500,1.1496,0.03755,0.02951,-0.0220,0.0249,1.0000 9.750,1.1576,0.03916,0.03115,-0.0200,0.0250,1.0000