Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m11-il-200000 Airfoil,m11-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,65.6991 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-m11-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.5194,0.09565,0.09204,-0.0226,1.0000,0.0477 -9.000,-0.5268,0.09130,0.08773,-0.0273,1.0000,0.0479 -8.750,-0.5360,0.08748,0.08389,-0.0293,1.0000,0.0480 -8.500,-0.5277,0.08181,0.07831,-0.0260,1.0000,0.0495 -8.250,-0.5219,0.07922,0.07572,-0.0246,1.0000,0.0505 -8.000,-0.5206,0.07633,0.07284,-0.0244,1.0000,0.0519 -7.750,-0.5204,0.07285,0.06936,-0.0255,1.0000,0.0537 -7.500,-0.5204,0.06903,0.06550,-0.0269,1.0000,0.0555 -7.250,-0.5275,0.06477,0.06085,-0.0307,1.0000,0.0599 -7.000,-0.5328,0.05932,0.05520,-0.0300,1.0000,0.0609 -6.750,-0.5201,0.05606,0.05216,-0.0287,1.0000,0.0627 -6.500,-0.5095,0.05416,0.05029,-0.0271,1.0000,0.0654 -6.250,-0.5052,0.05334,0.04882,-0.0252,1.0000,0.0734 -6.000,-0.5026,0.04725,0.04280,-0.0240,1.0000,0.0751 -5.750,-0.4911,0.04482,0.04046,-0.0224,1.0000,0.0769 -5.500,-0.4808,0.04290,0.03851,-0.0203,1.0000,0.0803 -5.250,-0.4784,0.04055,0.03565,-0.0168,1.0000,0.0889 -5.000,-0.4676,0.03822,0.03344,-0.0150,1.0000,0.0912 -4.750,-0.4577,0.03689,0.03206,-0.0124,1.0000,0.0974 -4.500,-0.4526,0.03475,0.02967,-0.0093,1.0000,0.1049 -4.250,-0.4427,0.03321,0.02812,-0.0069,1.0000,0.1087 -4.000,-0.4155,0.03097,0.02562,-0.0079,0.9960,0.1205 -3.750,-0.3756,0.02393,0.01722,-0.0069,0.9909,0.0705 -3.500,-0.3373,0.02081,0.01333,-0.0077,0.9858,0.0613 -3.250,-0.2972,0.01986,0.01215,-0.0099,0.9800,0.0604 -3.000,-0.2589,0.01818,0.01027,-0.0119,0.9741,0.0607 -2.750,-0.2177,0.01649,0.00851,-0.0147,0.9702,0.0625 -2.500,-0.1810,0.01549,0.00746,-0.0164,0.9623,0.0630 -2.250,-0.1391,0.01457,0.00657,-0.0192,0.9574,0.0645 -2.000,-0.1012,0.01386,0.00589,-0.0211,0.9498,0.0668 -1.750,-0.0606,0.01322,0.00524,-0.0236,0.9434,0.0699 -1.500,-0.0253,0.01269,0.00474,-0.0250,0.9339,0.0754 -1.250,0.0129,0.01214,0.00422,-0.0268,0.9264,0.0855 -1.000,0.0401,0.01130,0.00380,-0.0265,0.9134,0.1734 -0.750,0.2016,0.00924,0.00431,-0.0532,0.9400,1.0000 -0.500,0.2391,0.00909,0.00404,-0.0551,0.9206,1.0000 -0.250,0.2709,0.00898,0.00382,-0.0557,0.9000,1.0000 0.000,0.2966,0.00893,0.00367,-0.0550,0.8788,1.0000 0.250,0.3193,0.00893,0.00356,-0.0537,0.8577,1.0000 0.500,0.3417,0.00895,0.00346,-0.0523,0.8385,1.0000 0.750,0.3635,0.00899,0.00341,-0.0509,0.8192,1.0000 1.000,0.3855,0.00904,0.00339,-0.0495,0.8006,1.0000 1.250,0.4078,0.00911,0.00337,-0.0482,0.7828,1.0000 1.500,0.4304,0.00919,0.00336,-0.0469,0.7658,1.0000 1.750,0.4532,0.00928,0.00338,-0.0456,0.7490,1.0000 2.000,0.4760,0.00937,0.00343,-0.0445,0.7318,1.0000 2.250,0.4989,0.00947,0.00348,-0.0433,0.7143,1.0000 2.500,0.5219,0.00958,0.00355,-0.0421,0.6969,1.0000 2.750,0.5446,0.00969,0.00362,-0.0409,0.6780,1.0000 3.000,0.5672,0.00980,0.00368,-0.0396,0.6573,1.0000 3.250,0.5897,0.00991,0.00375,-0.0383,0.6351,1.0000 3.500,0.6118,0.01002,0.00380,-0.0369,0.6092,1.0000 3.750,0.6338,0.01016,0.00388,-0.0354,0.5816,1.0000 4.000,0.6559,0.01033,0.00399,-0.0341,0.5549,1.0000 4.250,0.6779,0.01053,0.00412,-0.0328,0.5272,1.0000 4.500,0.6999,0.01075,0.00429,-0.0315,0.4979,1.0000 4.750,0.7216,0.01099,0.00451,-0.0302,0.4651,1.0000 5.000,0.7424,0.01130,0.00471,-0.0287,0.4247,1.0000 5.250,0.7622,0.01171,0.00497,-0.0272,0.3722,1.0000 5.500,0.7792,0.01240,0.00533,-0.0253,0.2957,1.0000 5.750,0.7903,0.01385,0.00603,-0.0228,0.1634,1.0000 6.000,0.8036,0.01521,0.00700,-0.0206,0.1044,1.0000 6.250,0.8195,0.01627,0.00792,-0.0186,0.0838,1.0000 6.500,0.8361,0.01726,0.00887,-0.0167,0.0710,1.0000 6.750,0.8533,0.01819,0.00980,-0.0148,0.0621,1.0000 7.000,0.8700,0.01925,0.01092,-0.0129,0.0552,1.0000 7.250,0.8860,0.02044,0.01208,-0.0110,0.0494,1.0000 7.500,0.9036,0.02183,0.01354,-0.0092,0.0461,1.0000 7.750,0.9229,0.02289,0.01469,-0.0077,0.0425,1.0000 8.000,0.9413,0.02410,0.01589,-0.0063,0.0394,1.0000 8.250,0.9603,0.02644,0.01835,-0.0050,0.0371,1.0000 8.500,0.9799,0.02798,0.02015,-0.0035,0.0357,1.0000 8.750,0.9982,0.02990,0.02232,-0.0019,0.0344,1.0000 9.000,1.0149,0.03165,0.02429,-0.0002,0.0328,1.0000 9.250,1.0305,0.03328,0.02607,0.0014,0.0314,1.0000 9.500,1.0444,0.03528,0.02818,0.0029,0.0301,1.0000 9.750,1.0539,0.03865,0.03183,0.0049,0.0295,1.0000 10.000,1.0592,0.04208,0.03560,0.0073,0.0294,1.0000 10.250,1.0608,0.04547,0.03936,0.0101,0.0294,1.0000 10.500,1.0604,0.04829,0.04253,0.0131,0.0298,1.0000 10.750,1.0140,0.05499,0.05012,0.0201,0.0330,1.0000 11.000,0.9900,0.05883,0.05420,0.0237,0.0340,1.0000 11.250,0.9672,0.06291,0.05846,0.0252,0.0347,1.0000 11.500,0.9438,0.06757,0.06330,0.0250,0.0352,1.0000 11.750,0.9233,0.07272,0.06856,0.0234,0.0360,1.0000 12.000,0.9019,0.07865,0.07460,0.0205,0.0365,1.0000 12.250,0.7783,0.07805,0.07431,0.0207,0.0350,1.0000 12.500,0.7456,0.08763,0.08398,0.0155,0.0356,1.0000