Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-mh84-il-100000 Airfoil,mh84-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,40.3983 Max Cl/Cd alpha,5.5 Url,http://airfoiltools.com/polar/csv?polar=xf-mh84-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.2615,0.12289,0.11846,-0.0041,1.0000,0.0893 -9.750,-0.2687,0.12140,0.11705,-0.0088,1.0000,0.0921 -9.500,-0.2716,0.11877,0.11452,-0.0126,1.0000,0.0929 -9.250,-0.2421,0.11341,0.10919,-0.0104,1.0000,0.0947 -9.000,-0.2282,0.11028,0.10613,-0.0112,1.0000,0.0971 -8.750,-0.2198,0.10740,0.10333,-0.0134,1.0000,0.1004 -8.500,-0.2371,0.10647,0.10256,-0.0214,1.0000,0.1036 -8.250,-0.2190,0.10177,0.09795,-0.0219,1.0000,0.1048 -8.000,-0.1955,0.09813,0.09438,-0.0215,1.0000,0.1072 -7.750,-0.1764,0.09493,0.09125,-0.0256,0.9760,0.1109 -7.500,-0.1763,0.09148,0.08779,-0.0427,0.9363,0.1166 -7.250,-0.1394,0.08660,0.08285,-0.0392,0.9181,0.1186 -7.000,-0.1244,0.08403,0.08021,-0.0384,0.8938,0.1215 -6.750,-0.1216,0.08191,0.07807,-0.0388,0.8701,0.1256 -6.500,-0.1485,0.07995,0.07611,-0.0500,0.8473,0.1303 -6.250,-0.1319,0.07693,0.07307,-0.0436,0.8321,0.1317 -6.000,-0.1173,0.07473,0.07081,-0.0402,0.8173,0.1347 -5.500,-0.1258,0.03981,0.03428,-0.0822,0.8012,0.0654 -5.250,-0.1047,0.03597,0.02993,-0.0838,0.7872,0.0653 -5.000,-0.0820,0.03267,0.02600,-0.0844,0.7751,0.0657 -4.750,-0.0587,0.03039,0.02346,-0.0839,0.7630,0.0666 -4.500,-0.0329,0.02857,0.02141,-0.0837,0.7495,0.0681 -4.250,-0.0072,0.02685,0.01928,-0.0829,0.7385,0.0705 -4.000,0.0198,0.02537,0.01748,-0.0825,0.7253,0.0753 -3.750,0.0473,0.02442,0.01625,-0.0818,0.7130,0.0824 -3.500,0.0733,0.02335,0.01512,-0.0808,0.7020,0.0907 -3.250,0.1010,0.02249,0.01424,-0.0805,0.6888,0.1055 -3.000,0.1278,0.02185,0.01352,-0.0795,0.6788,0.1291 -2.750,0.1555,0.02140,0.01319,-0.0792,0.6654,0.1623 -2.500,0.1828,0.02126,0.01304,-0.0786,0.6540,0.1965 -2.250,0.2095,0.02109,0.01290,-0.0779,0.6427,0.2264 -2.000,0.2372,0.02092,0.01269,-0.0775,0.6303,0.2557 -1.750,0.2639,0.02064,0.01237,-0.0765,0.6207,0.2822 -1.500,0.2918,0.02047,0.01221,-0.0762,0.6077,0.3096 -1.250,0.3192,0.02021,0.01184,-0.0755,0.5980,0.3371 -1.000,0.3466,0.01998,0.01171,-0.0750,0.5859,0.3647 -0.750,0.3742,0.01984,0.01150,-0.0745,0.5754,0.3964 -0.500,0.4013,0.01958,0.01133,-0.0738,0.5647,0.4293 -0.250,0.4283,0.01945,0.01130,-0.0732,0.5539,0.4688 0.000,0.4548,0.01918,0.01111,-0.0723,0.5442,0.5202 0.250,0.4805,0.01899,0.01121,-0.0714,0.5332,0.5928 0.500,0.5023,0.01847,0.01105,-0.0690,0.5247,0.7202 0.750,0.5318,0.01802,0.01091,-0.0683,0.5133,1.0000 1.000,0.5619,0.01821,0.01069,-0.0683,0.5046,1.0000 1.250,0.5905,0.01859,0.01094,-0.0685,0.4933,1.0000 1.500,0.6195,0.01880,0.01082,-0.0681,0.4853,1.0000 1.750,0.6473,0.01922,0.01118,-0.0682,0.4740,1.0000 2.000,0.6760,0.01945,0.01110,-0.0678,0.4664,1.0000 2.250,0.7033,0.01992,0.01156,-0.0678,0.4556,1.0000 2.500,0.7319,0.02016,0.01152,-0.0674,0.4482,1.0000 2.750,0.7587,0.02068,0.01206,-0.0674,0.4379,1.0000 3.000,0.7870,0.02096,0.01211,-0.0670,0.4306,1.0000 3.250,0.8136,0.02153,0.01268,-0.0669,0.4212,1.0000 3.500,0.8414,0.02184,0.01282,-0.0666,0.4136,1.0000 3.750,0.8680,0.02243,0.01336,-0.0664,0.4055,1.0000 4.000,0.8949,0.02287,0.01374,-0.0662,0.3976,1.0000 4.250,0.9227,0.02332,0.01400,-0.0659,0.3912,1.0000 4.500,0.9478,0.02398,0.01475,-0.0657,0.3825,1.0000 4.750,0.9757,0.02432,0.01491,-0.0654,0.3765,1.0000 5.000,1.0003,0.02514,0.01580,-0.0652,0.3690,1.0000 5.250,1.0264,0.02566,0.01627,-0.0649,0.3621,1.0000 5.500,1.0548,0.02611,0.01650,-0.0647,0.3569,1.0000 5.750,1.0767,0.02708,0.01770,-0.0644,0.3492,1.0000 6.000,1.1032,0.02758,0.01811,-0.0641,0.3434,1.0000 6.250,1.1296,0.02826,0.01868,-0.0638,0.3383,1.0000 6.500,1.1508,0.02930,0.01992,-0.0634,0.3313,1.0000 6.750,1.1769,0.02982,0.02037,-0.0631,0.3261,1.0000 7.000,1.2033,0.03056,0.02099,-0.0629,0.3216,1.0000 7.250,1.2212,0.03190,0.02260,-0.0624,0.3152,1.0000 7.500,1.2457,0.03255,0.02323,-0.0620,0.3101,1.0000 7.750,1.2749,0.03301,0.02348,-0.0618,0.3062,1.0000 8.000,1.2877,0.03485,0.02568,-0.0611,0.3006,1.0000 8.250,1.3074,0.03600,0.02693,-0.0606,0.2956,1.0000 8.500,1.3340,0.03649,0.02732,-0.0603,0.2916,1.0000 8.750,1.3550,0.03774,0.02860,-0.0598,0.2876,1.0000 9.000,1.3611,0.04003,0.03123,-0.0588,0.2825,1.0000 9.250,1.3791,0.04129,0.03256,-0.0582,0.2784,1.0000 9.500,1.4065,0.04178,0.03296,-0.0579,0.2750,1.0000 9.750,1.4216,0.04354,0.03481,-0.0573,0.2715,1.0000 10.000,1.4020,0.04772,0.03945,-0.0553,0.2671,1.0000 10.250,1.3988,0.05046,0.04236,-0.0540,0.2633,1.0000 10.500,1.4275,0.05075,0.04259,-0.0537,0.2601,1.0000 10.750,1.4728,0.05033,0.04199,-0.0542,0.2574,1.0000 11.000,0.8381,0.15131,0.14435,-0.0994,0.2920,1.0000 11.250,0.8706,0.15456,0.14761,-0.0984,0.2901,1.0000