Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-mh121-il-200000-n5 Airfoil,mh121-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,82.4167 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-mh121-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.4147,0.10977,0.10617,-0.0361,1.0000,0.0122 -9.500,-0.4163,0.10649,0.10293,-0.0360,1.0000,0.0106 -9.250,-0.4198,0.10300,0.09950,-0.0360,1.0000,0.0096 -9.000,-0.4250,0.09951,0.09606,-0.0359,1.0000,0.0087 -8.500,-0.4357,0.09103,0.08772,-0.0373,0.9992,0.0067 -8.250,-0.4220,0.08671,0.08340,-0.0417,0.9963,0.0064 -8.000,-0.4085,0.08296,0.07962,-0.0456,0.9933,0.0061 -7.750,-0.4045,0.07755,0.07423,-0.0505,0.9880,0.0059 -7.500,-0.3963,0.07151,0.06821,-0.0577,0.9823,0.0059 -7.250,-0.3877,0.06399,0.06069,-0.0679,0.9735,0.0056 -7.000,-0.3738,0.05588,0.05241,-0.0791,0.9667,0.0055 -6.750,-0.3607,0.04965,0.04595,-0.0852,0.9598,0.0055 -6.500,-0.3399,0.04343,0.03939,-0.0910,0.9561,0.0054 -6.250,-0.3255,0.03871,0.03433,-0.0928,0.9494,0.0053 -6.000,-0.3000,0.03378,0.02894,-0.0957,0.9463,0.0055 -5.750,-0.2703,0.02977,0.02442,-0.0981,0.9443,0.0058 -5.500,-0.2484,0.02641,0.02052,-0.0984,0.9394,0.0067 -5.250,-0.2230,0.02468,0.01856,-0.1000,0.9364,0.0095 -5.000,-0.1923,0.02217,0.01550,-0.1009,0.9345,0.0101 -4.750,-0.1606,0.01993,0.01287,-0.1017,0.9331,0.0100 -4.500,-0.1284,0.01812,0.01080,-0.1025,0.9319,0.0101 -4.250,-0.0960,0.01664,0.00914,-0.1035,0.9309,0.0103 -4.000,-0.0745,0.01571,0.00808,-0.1024,0.9259,0.0106 -3.750,-0.0444,0.01477,0.00697,-0.1031,0.9236,0.0115 -3.500,-0.0119,0.01404,0.00601,-0.1042,0.9218,0.0136 -3.250,0.0216,0.01292,0.00517,-0.1059,0.9204,0.0873 -3.000,0.0531,0.01134,0.00490,-0.1084,0.9193,0.4237 -2.750,0.0860,0.01117,0.00476,-0.1095,0.9181,0.4831 -2.500,0.1094,0.01118,0.00468,-0.1087,0.9135,0.5162 -2.250,0.1381,0.01112,0.00465,-0.1089,0.9107,0.5545 -2.000,0.1684,0.01106,0.00461,-0.1095,0.9086,0.5868 -1.750,0.2004,0.01099,0.00450,-0.1104,0.9069,0.6029 -1.500,0.2332,0.01092,0.00437,-0.1115,0.9055,0.6151 -1.250,0.2582,0.01095,0.00433,-0.1111,0.9015,0.6264 -1.000,0.2858,0.01095,0.00432,-0.1111,0.8981,0.6380 -0.750,0.3162,0.01091,0.00429,-0.1118,0.8957,0.6504 -0.500,0.3479,0.01086,0.00425,-0.1127,0.8938,0.6632 -0.250,0.3804,0.01079,0.00422,-0.1137,0.8921,0.6766 0.000,0.4029,0.01087,0.00437,-0.1127,0.8870,0.6903 0.250,0.4313,0.01085,0.00442,-0.1129,0.8836,0.7052 0.500,0.4623,0.01078,0.00443,-0.1136,0.8810,0.7214 0.750,0.4948,0.01069,0.00442,-0.1145,0.8788,0.7391 1.000,0.5160,0.01076,0.00459,-0.1132,0.8724,0.7583 1.250,0.5454,0.01067,0.00466,-0.1134,0.8685,0.7799 1.500,0.5754,0.01055,0.00466,-0.1136,0.8646,0.8039 1.750,0.5976,0.01051,0.00476,-0.1123,0.8573,0.8331 2.000,0.6275,0.01030,0.00468,-0.1122,0.8518,0.8685 2.250,0.6520,0.01013,0.00466,-0.1111,0.8423,0.9275 2.500,0.6850,0.00995,0.00456,-0.1119,0.8303,1.0000 2.750,0.7157,0.00975,0.00446,-0.1120,0.8128,1.0000 3.000,0.7408,0.00965,0.00440,-0.1110,0.7888,1.0000 3.250,0.7663,0.00961,0.00439,-0.1102,0.7617,1.0000 3.500,0.7912,0.00960,0.00434,-0.1091,0.7144,1.0000 3.750,0.8099,0.01012,0.00417,-0.1065,0.5710,1.0000 4.000,0.8134,0.01149,0.00469,-0.1017,0.4135,1.0000 4.250,0.8206,0.01287,0.00537,-0.0982,0.2736,1.0000 4.500,0.8276,0.01461,0.00619,-0.0951,0.1141,1.0000 4.750,0.8407,0.01605,0.00696,-0.0929,0.0257,1.0000 5.000,0.8595,0.01704,0.00797,-0.0913,0.0055,1.0000 5.250,0.8805,0.01783,0.00894,-0.0899,0.0046,1.0000 5.500,0.9006,0.01878,0.01009,-0.0884,0.0041,1.0000 5.750,0.9197,0.01989,0.01138,-0.0867,0.0038,1.0000 6.000,0.9384,0.02121,0.01286,-0.0850,0.0036,1.0000 6.250,0.9584,0.02278,0.01460,-0.0835,0.0035,1.0000 6.500,0.9809,0.02472,0.01675,-0.0824,0.0034,1.0000 6.750,1.0057,0.02699,0.01928,-0.0817,0.0034,1.0000 7.000,1.0303,0.02973,0.02238,-0.0808,0.0034,1.0000 7.250,1.0517,0.03292,0.02602,-0.0793,0.0035,1.0000 7.500,1.0683,0.03646,0.03004,-0.0771,0.0036,1.0000 7.750,1.0797,0.04032,0.03438,-0.0743,0.0037,1.0000 8.000,1.0863,0.04439,0.03892,-0.0711,0.0038,1.0000 8.250,1.0885,0.04862,0.04355,-0.0675,0.0039,1.0000 8.500,1.0865,0.05284,0.04814,-0.0638,0.0040,1.0000 8.750,1.0807,0.05698,0.05259,-0.0601,0.0041,1.0000 9.000,1.0699,0.06073,0.05660,-0.0561,0.0041,1.0000 9.250,1.0553,0.06436,0.06044,-0.0521,0.0042,1.0000 9.500,1.0388,0.06819,0.06446,-0.0489,0.0043,1.0000 9.750,1.0212,0.07231,0.06875,-0.0469,0.0043,1.0000 10.000,1.0024,0.07696,0.07357,-0.0460,0.0043,1.0000 10.250,0.9832,0.08225,0.07900,-0.0465,0.0043,1.0000 10.500,0.9645,0.08830,0.08518,-0.0487,0.0044,1.0000