Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-mh22-il-50000-n5 Airfoil,mh22-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,35 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-mh22-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.4548,0.10683,0.10055,0.0007,1.0000,0.0388 -9.000,-0.4481,0.10250,0.09624,0.0007,1.0000,0.0373 -8.750,-0.5254,0.10469,0.09804,0.0032,1.0000,0.0374 -8.500,-0.5212,0.10067,0.09407,0.0019,1.0000,0.0361 -8.250,-0.5182,0.09673,0.09020,0.0001,1.0000,0.0349 -8.000,-0.5168,0.09258,0.08614,-0.0020,1.0000,0.0339 -7.750,-0.5161,0.08853,0.08217,-0.0045,1.0000,0.0330 -7.500,-0.5162,0.08432,0.07804,-0.0075,1.0000,0.0320 -7.250,-0.5137,0.07947,0.07324,-0.0114,1.0000,0.0311 -7.000,-0.5098,0.07411,0.06789,-0.0157,1.0000,0.0300 -6.750,-0.5038,0.06804,0.06175,-0.0203,1.0000,0.0287 -6.250,-0.4828,0.05783,0.05106,-0.0255,1.0000,0.0272 -6.000,-0.4712,0.05338,0.04640,-0.0266,1.0000,0.0270 -5.750,-0.4576,0.04895,0.04167,-0.0274,1.0000,0.0269 -5.500,-0.4419,0.04471,0.03705,-0.0279,1.0000,0.0269 -5.250,-0.4242,0.04071,0.03258,-0.0278,1.0000,0.0270 -5.000,-0.4045,0.03709,0.02845,-0.0275,1.0000,0.0272 -4.750,-0.3846,0.03352,0.02449,-0.0270,1.0000,0.0282 -4.500,-0.3638,0.03124,0.02199,-0.0265,1.0000,0.0322 -4.250,-0.3399,0.02891,0.01895,-0.0257,1.0000,0.0373 -4.000,-0.3153,0.02645,0.01607,-0.0246,1.0000,0.0406 -3.750,-0.2916,0.02439,0.01386,-0.0235,1.0000,0.0454 -3.500,-0.2674,0.02267,0.01197,-0.0224,1.0000,0.0572 -3.250,-0.2425,0.02107,0.01034,-0.0217,1.0000,0.0882 -3.000,-0.2194,0.01955,0.00908,-0.0210,1.0000,0.1524 -2.750,-0.1988,0.01828,0.00823,-0.0201,1.0000,0.2415 -2.500,-0.1810,0.01705,0.00761,-0.0187,1.0000,0.3699 -2.250,-0.1691,0.01561,0.00733,-0.0154,1.0000,0.6099 -2.000,-0.0738,0.01473,0.00638,-0.0262,1.0000,1.0000 -1.750,-0.0606,0.01482,0.00607,-0.0242,1.0000,1.0000 -1.500,-0.0494,0.01498,0.00598,-0.0220,1.0000,1.0000 -1.250,-0.0192,0.01516,0.00583,-0.0235,0.9879,1.0000 -1.000,0.0250,0.01532,0.00566,-0.0273,0.9701,1.0000 -0.750,0.0699,0.01546,0.00552,-0.0312,0.9543,1.0000 -0.500,0.1112,0.01559,0.00534,-0.0342,0.9372,1.0000 -0.250,0.1511,0.01573,0.00530,-0.0368,0.9204,1.0000 0.000,0.1892,0.01587,0.00529,-0.0389,0.9039,1.0000 0.250,0.2237,0.01602,0.00533,-0.0401,0.8871,1.0000 0.500,0.2541,0.01620,0.00542,-0.0406,0.8695,1.0000 0.750,0.2830,0.01640,0.00556,-0.0406,0.8527,1.0000 1.000,0.3105,0.01660,0.00569,-0.0403,0.8364,1.0000 1.250,0.3358,0.01683,0.00588,-0.0395,0.8196,1.0000 1.500,0.3604,0.01707,0.00609,-0.0386,0.8029,1.0000 1.750,0.3847,0.01732,0.00632,-0.0376,0.7865,1.0000 2.000,0.4089,0.01756,0.00657,-0.0365,0.7706,1.0000 2.250,0.4326,0.01782,0.00694,-0.0354,0.7537,1.0000 2.500,0.4561,0.01808,0.00725,-0.0342,0.7363,1.0000 2.750,0.4798,0.01833,0.00755,-0.0330,0.7193,1.0000 3.000,0.5034,0.01859,0.00787,-0.0318,0.7019,1.0000 3.250,0.5268,0.01886,0.00825,-0.0306,0.6828,1.0000 3.500,0.5504,0.01911,0.00858,-0.0293,0.6645,1.0000 3.750,0.5739,0.01939,0.00918,-0.0281,0.6435,1.0000 4.000,0.5977,0.01963,0.00955,-0.0268,0.6229,1.0000 4.250,0.6212,0.01989,0.00999,-0.0255,0.5997,1.0000 4.500,0.6446,0.02013,0.01042,-0.0242,0.5746,1.0000 4.750,0.6678,0.02036,0.01084,-0.0228,0.5477,1.0000 5.000,0.6908,0.02056,0.01120,-0.0212,0.5186,1.0000 5.250,0.7133,0.02083,0.01167,-0.0197,0.4843,1.0000 5.500,0.7352,0.02114,0.01209,-0.0180,0.4457,1.0000 5.750,0.7553,0.02158,0.01280,-0.0161,0.3946,1.0000 6.000,0.7716,0.02232,0.01333,-0.0140,0.3118,1.0000 6.250,0.7823,0.02421,0.01440,-0.0123,0.1691,1.0000 6.500,0.7898,0.02769,0.01696,-0.0107,0.0756,1.0000 6.750,0.8013,0.03041,0.01945,-0.0092,0.0482,1.0000 7.000,0.8164,0.03278,0.02203,-0.0071,0.0396,1.0000 7.250,0.8323,0.03515,0.02454,-0.0055,0.0326,1.0000 7.500,0.8472,0.03737,0.02689,-0.0044,0.0255,1.0000 7.750,0.8653,0.04034,0.03011,-0.0029,0.0236,1.0000 8.000,0.8840,0.04344,0.03367,-0.0015,0.0225,1.0000 8.250,0.8986,0.04691,0.03761,-0.0002,0.0218,1.0000 8.500,0.9083,0.05064,0.04181,0.0010,0.0214,1.0000 8.750,0.9127,0.05458,0.04619,0.0021,0.0212,1.0000 9.000,0.9118,0.05860,0.05060,0.0030,0.0211,1.0000 9.250,0.9061,0.06258,0.05489,0.0036,0.0211,1.0000 9.500,0.8940,0.06651,0.05906,0.0040,0.0212,1.0000 9.750,0.8796,0.07069,0.06342,0.0033,0.0213,1.0000 10.000,0.8653,0.07543,0.06830,0.0010,0.0215,1.0000 10.250,0.8507,0.08091,0.07391,-0.0024,0.0217,1.0000 10.500,0.8358,0.08731,0.08038,-0.0067,0.0219,1.0000 10.750,0.8229,0.09420,0.08732,-0.0115,0.0222,1.0000