Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-mh44-il-50000 Airfoil,mh44-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,29.1187 Max Cl/Cd alpha,6.75 Url,http://www.airfoiltools.com/polar/csv?polar=xf-mh44-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.000,-0.5037,0.09644,0.09026,0.0042,1.0000,0.2839 -7.750,-0.4781,0.09114,0.08495,0.0053,1.0000,0.2922 -7.000,-0.5557,0.06222,0.05569,-0.0287,1.0000,0.1143 -6.750,-0.5569,0.05569,0.04875,-0.0301,1.0000,0.1036 -6.500,-0.5453,0.05128,0.04413,-0.0297,1.0000,0.0986 -6.250,-0.5371,0.04660,0.03906,-0.0290,1.0000,0.0942 -6.000,-0.5299,0.04234,0.03371,-0.0272,1.0000,0.0889 -5.750,-0.5149,0.03889,0.02991,-0.0255,1.0000,0.0885 -5.500,-0.4998,0.03577,0.02650,-0.0238,1.0000,0.0902 -5.250,-0.4829,0.03346,0.02416,-0.0221,1.0000,0.0958 -5.000,-0.4651,0.03103,0.02126,-0.0200,1.0000,0.0997 -4.750,-0.4450,0.02860,0.01852,-0.0180,1.0000,0.1043 -4.500,-0.4255,0.02676,0.01660,-0.0162,1.0000,0.1177 -4.250,-0.4057,0.02494,0.01486,-0.0142,1.0000,0.1394 -4.000,-0.3873,0.02303,0.01324,-0.0120,1.0000,0.1895 -3.750,-0.3775,0.02062,0.01202,-0.0083,1.0000,0.3614 -3.500,-0.3724,0.01990,0.01184,-0.0034,1.0000,0.4782 -3.250,-0.3645,0.01937,0.01168,0.0013,1.0000,0.5707 -3.000,-0.3525,0.01869,0.01138,0.0057,1.0000,0.6597 -2.750,-0.3340,0.01796,0.01106,0.0098,1.0000,0.7717 -2.500,-0.0731,0.01785,0.00956,-0.0289,1.0000,1.0000 -2.250,-0.0973,0.01747,0.00915,-0.0233,1.0000,1.0000 -2.000,-0.1051,0.01739,0.00884,-0.0191,1.0000,1.0000 -1.750,-0.1035,0.01745,0.00866,-0.0159,1.0000,1.0000 -1.500,-0.0977,0.01759,0.00858,-0.0133,1.0000,1.0000 -1.250,-0.0898,0.01779,0.00858,-0.0110,1.0000,1.0000 -1.000,-0.0804,0.01805,0.00864,-0.0089,1.0000,1.0000 -0.750,-0.0698,0.01836,0.00878,-0.0071,1.0000,1.0000 -0.500,-0.0583,0.01872,0.00895,-0.0056,1.0000,1.0000 -0.250,-0.0460,0.01914,0.00922,-0.0042,1.0000,1.0000 0.000,-0.0334,0.01961,0.00956,-0.0031,1.0000,1.0000 0.250,-0.0204,0.02014,0.00997,-0.0021,1.0000,1.0000 0.500,0.0252,0.02107,0.01079,-0.0074,0.9874,1.0000 0.750,0.0884,0.02219,0.01180,-0.0157,0.9678,1.0000 1.000,0.1456,0.02309,0.01267,-0.0225,0.9467,1.0000 1.250,0.2048,0.02391,0.01348,-0.0293,0.9260,1.0000 1.500,0.2587,0.02457,0.01418,-0.0348,0.9040,1.0000 1.750,0.3156,0.02509,0.01478,-0.0404,0.8824,1.0000 2.000,0.3687,0.02543,0.01521,-0.0448,0.8605,1.0000 2.250,0.4082,0.02580,0.01565,-0.0465,0.8378,1.0000 2.500,0.4520,0.02591,0.01589,-0.0482,0.8166,1.0000 2.750,0.4784,0.02626,0.01631,-0.0473,0.7930,1.0000 3.000,0.5127,0.02623,0.01636,-0.0468,0.7721,1.0000 3.250,0.5360,0.02646,0.01665,-0.0449,0.7486,1.0000 3.500,0.5612,0.02653,0.01684,-0.0430,0.7263,1.0000 3.750,0.5874,0.02640,0.01678,-0.0408,0.7045,1.0000 4.000,0.6094,0.02652,0.01697,-0.0384,0.6807,1.0000 4.250,0.6351,0.02627,0.01679,-0.0357,0.6591,1.0000 4.500,0.6571,0.02635,0.01693,-0.0332,0.6341,1.0000 4.750,0.6791,0.02648,0.01712,-0.0307,0.6084,1.0000 5.000,0.7016,0.02658,0.01726,-0.0282,0.5822,1.0000 5.250,0.7242,0.02671,0.01741,-0.0257,0.5552,1.0000 5.500,0.7466,0.02693,0.01768,-0.0233,0.5271,1.0000 5.750,0.7686,0.02725,0.01801,-0.0210,0.4979,1.0000 6.000,0.7905,0.02767,0.01841,-0.0188,0.4679,1.0000 6.250,0.8123,0.02817,0.01890,-0.0167,0.4377,1.0000 6.500,0.8341,0.02873,0.01944,-0.0147,0.4073,1.0000 6.750,0.8558,0.02939,0.02000,-0.0128,0.3771,1.0000 7.000,0.8757,0.03035,0.02097,-0.0110,0.3470,1.0000 7.250,0.8952,0.03144,0.02208,-0.0092,0.3175,1.0000 7.500,0.9145,0.03263,0.02326,-0.0075,0.2893,1.0000 7.750,0.9344,0.03398,0.02454,-0.0059,0.2631,1.0000 8.000,0.9524,0.03542,0.02605,-0.0042,0.2376,1.0000 8.250,0.9677,0.03765,0.02853,-0.0026,0.2167,1.0000 8.500,0.9881,0.03919,0.02986,-0.0012,0.1948,1.0000 8.750,1.0009,0.04193,0.03292,0.0005,0.1793,1.0000 9.000,1.0122,0.04458,0.03583,0.0022,0.1646,1.0000 9.250,1.0245,0.04737,0.03877,0.0037,0.1520,1.0000 9.500,1.0234,0.05150,0.04348,0.0057,0.1457,1.0000 9.750,1.0301,0.05484,0.04698,0.0072,0.1374,1.0000 10.000,1.0175,0.05929,0.05189,0.0089,0.1339,1.0000 10.250,1.0317,0.06232,0.05487,0.0100,0.1258,1.0000 10.500,1.0138,0.06728,0.06016,0.0113,0.1256,1.0000 10.750,0.9923,0.07229,0.06539,0.0121,0.1259,1.0000 11.000,0.9705,0.07725,0.07044,0.0126,0.1264,1.0000 11.250,0.8147,0.10518,0.09806,-0.0103,0.1660,1.0000 11.500,0.8061,0.11250,0.10536,-0.0133,0.1677,1.0000