Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-mh33-il-50000 Airfoil,mh33-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,32.2979 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-mh33-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.5223,0.10041,0.09369,0.0014,1.0000,0.2551 -8.000,-0.5283,0.09783,0.09122,0.0008,1.0000,0.2665 -7.500,-0.5320,0.09194,0.08550,0.0013,1.0000,0.2927 -7.250,-0.5323,0.08889,0.08254,0.0020,1.0000,0.3061 -6.500,-0.5115,0.07779,0.07161,0.0058,1.0000,0.3507 -5.750,-0.5189,0.05112,0.04361,-0.0294,1.0000,0.1155 -5.500,-0.5045,0.04599,0.03789,-0.0292,1.0000,0.1026 -5.250,-0.4881,0.04175,0.03335,-0.0282,1.0000,0.0968 -5.000,-0.4690,0.03785,0.02847,-0.0269,1.0000,0.0902 -4.750,-0.4483,0.03438,0.02462,-0.0256,1.0000,0.0890 -4.500,-0.4256,0.03136,0.02109,-0.0241,1.0000,0.0894 -4.250,-0.4030,0.02867,0.01819,-0.0228,1.0000,0.0962 -4.000,-0.3796,0.02651,0.01582,-0.0215,1.0000,0.1108 -3.750,-0.3531,0.02404,0.01311,-0.0197,1.0000,0.1310 -3.500,-0.3291,0.02158,0.01104,-0.0182,1.0000,0.1980 -3.250,-0.3142,0.01822,0.00941,-0.0153,1.0000,0.4263 -3.000,-0.1572,0.01671,0.00836,-0.0303,1.0000,1.0000 -2.750,-0.1522,0.01623,0.00762,-0.0278,1.0000,1.0000 -2.500,-0.1426,0.01593,0.00703,-0.0255,1.0000,1.0000 -2.250,-0.1304,0.01574,0.00656,-0.0233,1.0000,1.0000 -2.000,-0.1167,0.01560,0.00616,-0.0212,1.0000,1.0000 -1.750,-0.1021,0.01551,0.00583,-0.0192,1.0000,1.0000 -1.500,-0.0869,0.01546,0.00556,-0.0172,1.0000,1.0000 -1.250,-0.0709,0.01544,0.00528,-0.0154,1.0000,1.0000 -1.000,-0.0543,0.01545,0.00512,-0.0136,1.0000,1.0000 -0.750,-0.0371,0.01549,0.00500,-0.0120,1.0000,1.0000 -0.500,-0.0194,0.01555,0.00493,-0.0105,1.0000,1.0000 -0.250,-0.0013,0.01564,0.00490,-0.0090,1.0000,1.0000 0.000,0.0170,0.01576,0.00493,-0.0077,1.0000,1.0000 0.250,0.0354,0.01591,0.00496,-0.0064,1.0000,1.0000 0.500,0.0539,0.01609,0.00508,-0.0053,1.0000,1.0000 0.750,0.0723,0.01630,0.00526,-0.0042,1.0000,1.0000 1.000,0.0906,0.01655,0.00549,-0.0031,1.0000,1.0000 1.250,0.1086,0.01685,0.00579,-0.0021,1.0000,1.0000 1.500,0.1263,0.01720,0.00616,-0.0012,1.0000,1.0000 1.750,0.1434,0.01760,0.00660,-0.0004,1.0000,1.0000 2.000,0.1600,0.01808,0.00712,0.0004,1.0000,1.0000 2.250,0.1758,0.01864,0.00773,0.0010,1.0000,1.0000 2.500,0.1908,0.01930,0.00847,0.0015,1.0000,1.0000 2.750,0.2048,0.02008,0.00933,0.0018,1.0000,1.0000 3.000,0.2693,0.02152,0.01110,-0.0076,0.9746,1.0000 3.250,0.3611,0.02248,0.01252,-0.0204,0.9312,1.0000 3.500,0.4520,0.02229,0.01299,-0.0308,0.8820,1.0000 3.750,0.5334,0.02102,0.01234,-0.0368,0.8267,1.0000 4.000,0.5841,0.01983,0.01147,-0.0362,0.7629,1.0000 4.250,0.6145,0.01937,0.01109,-0.0325,0.6873,1.0000 4.500,0.6353,0.01967,0.01113,-0.0283,0.6021,1.0000 4.750,0.6533,0.02047,0.01154,-0.0245,0.5140,1.0000 5.000,0.6708,0.02164,0.01223,-0.0213,0.4299,1.0000 5.250,0.6883,0.02307,0.01329,-0.0186,0.3525,1.0000 5.500,0.7068,0.02469,0.01458,-0.0164,0.2865,1.0000 5.750,0.7275,0.02665,0.01633,-0.0145,0.2339,1.0000 6.000,0.7480,0.02868,0.01822,-0.0129,0.1915,1.0000 6.250,0.7700,0.03110,0.02050,-0.0115,0.1607,1.0000 6.500,0.7908,0.03362,0.02334,-0.0099,0.1382,1.0000 6.750,0.8118,0.03707,0.02741,-0.0083,0.1271,1.0000 7.000,0.8288,0.03987,0.03052,-0.0067,0.1130,1.0000 7.250,0.8445,0.04354,0.03454,-0.0051,0.1059,1.0000 7.500,0.8551,0.04802,0.03969,-0.0032,0.1044,1.0000 7.750,0.8612,0.05294,0.04519,-0.0016,0.1045,1.0000 8.000,0.8643,0.05813,0.05081,-0.0003,0.1058,1.0000 8.250,0.8681,0.06350,0.05644,0.0005,0.1075,1.0000 8.500,0.7802,0.06142,0.05537,0.0033,0.1151,1.0000 8.750,0.7629,0.06741,0.06146,0.0031,0.1183,1.0000 9.000,0.7717,0.07355,0.06763,0.0035,0.1217,1.0000 9.250,0.6979,0.08175,0.07579,-0.0039,0.1294,1.0000 9.500,0.7034,0.08778,0.08186,-0.0042,0.1353,1.0000