Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-mh80-il-200000-n5 Airfoil,mh80-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,58.2887 Max Cl/Cd alpha,9 Url,http://airfoiltools.com/polar/csv?polar=xf-mh80-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.5169,0.09255,0.08950,0.0144,1.0000,0.0134 -9.250,-0.5170,0.08812,0.08512,0.0118,1.0000,0.0133 -9.000,-0.5210,0.08275,0.07980,0.0083,1.0000,0.0131 -8.750,-0.5257,0.07664,0.07364,0.0031,0.8728,0.0129 -8.500,-0.5421,0.06970,0.06656,-0.0028,0.8215,0.0126 -8.250,-0.5650,0.06262,0.05928,-0.0060,0.7931,0.0124 -7.750,-0.6330,0.03864,0.03360,-0.0067,0.7689,0.0108 -7.500,-0.6239,0.03552,0.03002,-0.0052,0.7482,0.0108 -7.250,-0.6110,0.03268,0.02669,-0.0038,0.7293,0.0108 -7.000,-0.5953,0.03007,0.02360,-0.0024,0.7112,0.0108 -6.750,-0.5763,0.02809,0.02125,-0.0013,0.6936,0.0109 -6.500,-0.5554,0.02645,0.01932,-0.0003,0.6769,0.0111 -6.250,-0.5330,0.02496,0.01752,0.0006,0.6607,0.0112 -6.000,-0.5096,0.02369,0.01598,0.0014,0.6452,0.0114 -5.500,-0.4607,0.02143,0.01326,0.0029,0.6152,0.0120 -5.250,-0.4356,0.02041,0.01203,0.0036,0.6011,0.0125 -5.000,-0.4102,0.01948,0.01091,0.0043,0.5875,0.0130 -4.750,-0.3847,0.01869,0.00992,0.0050,0.5745,0.0135 -4.500,-0.3594,0.01804,0.00919,0.0055,0.5617,0.0142 -4.250,-0.3332,0.01755,0.00861,0.0060,0.5488,0.0157 -4.000,-0.3072,0.01699,0.00794,0.0065,0.5368,0.0171 -3.750,-0.2812,0.01649,0.00735,0.0070,0.5253,0.0186 -3.500,-0.2548,0.01599,0.00673,0.0075,0.5136,0.0202 -3.250,-0.2282,0.01554,0.00619,0.0080,0.5026,0.0225 -3.000,-0.2015,0.01514,0.00570,0.0084,0.4922,0.0270 -2.750,-0.1750,0.01468,0.00524,0.0089,0.4813,0.0372 -2.500,-0.1491,0.01414,0.00482,0.0093,0.4714,0.0674 -2.250,-0.1236,0.01360,0.00454,0.0097,0.4619,0.1338 -2.000,-0.0980,0.01312,0.00433,0.0101,0.4525,0.2081 -1.750,-0.0731,0.01263,0.00413,0.0105,0.4434,0.2959 -1.500,-0.0498,0.01199,0.00397,0.0113,0.4343,0.4215 -1.250,-0.0303,0.01118,0.00385,0.0130,0.4265,0.6026 -1.000,-0.0088,0.01068,0.00398,0.0154,0.4185,0.7692 -0.750,0.0217,0.01076,0.00411,0.0159,0.4103,0.8511 -0.500,0.0527,0.01088,0.00415,0.0160,0.4016,0.8880 -0.250,0.0834,0.01103,0.00415,0.0160,0.3935,0.9115 0.000,0.1163,0.01116,0.00417,0.0155,0.3853,0.9287 0.250,0.1493,0.01131,0.00417,0.0149,0.3779,0.9432 0.500,0.1878,0.01146,0.00421,0.0131,0.3702,0.9561 0.750,0.2363,0.01165,0.00423,0.0093,0.3618,0.9685 1.000,0.2853,0.01177,0.00423,0.0053,0.3536,0.9788 1.250,0.3285,0.01187,0.00420,0.0023,0.3465,0.9866 1.500,0.3689,0.01195,0.00418,-0.0002,0.3402,0.9928 1.750,0.4078,0.01201,0.00415,-0.0025,0.3333,0.9977 2.250,0.4639,0.01221,0.00421,-0.0027,0.3227,1.0000 2.500,0.4885,0.01233,0.00428,-0.0022,0.3179,1.0000 2.750,0.5128,0.01249,0.00435,-0.0015,0.3135,1.0000 3.000,0.5373,0.01263,0.00446,-0.0009,0.3091,1.0000 3.250,0.5617,0.01277,0.00458,-0.0003,0.3042,1.0000 3.500,0.5860,0.01294,0.00470,0.0003,0.2998,1.0000 3.750,0.6100,0.01315,0.00483,0.0009,0.2963,1.0000 4.000,0.6344,0.01331,0.00501,0.0016,0.2923,1.0000 4.250,0.6586,0.01350,0.00519,0.0022,0.2880,1.0000 4.500,0.6825,0.01370,0.00537,0.0029,0.2841,1.0000 4.750,0.7062,0.01395,0.00554,0.0035,0.2807,1.0000 5.000,0.7303,0.01415,0.00579,0.0042,0.2770,1.0000 5.250,0.7544,0.01437,0.00603,0.0048,0.2733,1.0000 5.500,0.7782,0.01461,0.00627,0.0055,0.2698,1.0000 5.750,0.8018,0.01488,0.00649,0.0061,0.2665,1.0000 6.000,0.8256,0.01514,0.00677,0.0068,0.2631,1.0000 6.250,0.8496,0.01540,0.00709,0.0074,0.2596,1.0000 6.500,0.8735,0.01567,0.00738,0.0080,0.2563,1.0000 6.750,0.8971,0.01596,0.00766,0.0086,0.2531,1.0000 7.000,0.9205,0.01630,0.00796,0.0092,0.2500,1.0000 7.250,0.9445,0.01658,0.00835,0.0097,0.2466,1.0000 7.500,0.9683,0.01690,0.00872,0.0103,0.2434,1.0000 7.750,0.9922,0.01722,0.00909,0.0108,0.2403,1.0000 8.000,1.0158,0.01756,0.00943,0.0113,0.2373,1.0000 8.250,1.0394,0.01794,0.00982,0.0117,0.2343,1.0000 8.500,1.0632,0.01830,0.01030,0.0121,0.2309,1.0000 8.750,1.0869,0.01867,0.01076,0.0126,0.2278,1.0000 9.000,1.1104,0.01905,0.01118,0.0130,0.2248,1.0000 9.250,1.1335,0.01946,0.01159,0.0134,0.2218,1.0000 9.500,1.1565,0.01990,0.01212,0.0138,0.2187,1.0000 9.750,1.1794,0.02035,0.01270,0.0142,0.2154,1.0000 10.000,1.2019,0.02079,0.01323,0.0146,0.2121,1.0000 10.250,1.2239,0.02123,0.01371,0.0151,0.2090,1.0000 10.500,1.2455,0.02174,0.01424,0.0155,0.2061,1.0000 10.750,1.2665,0.02227,0.01495,0.0160,0.2026,1.0000 11.000,1.2870,0.02281,0.01561,0.0165,0.1990,1.0000 11.250,1.3068,0.02334,0.01620,0.0171,0.1958,1.0000 11.500,1.3258,0.02392,0.01679,0.0177,0.1928,1.0000 11.750,1.3433,0.02460,0.01767,0.0184,0.1892,1.0000 12.000,1.3597,0.02529,0.01849,0.0191,0.1856,1.0000 12.250,1.3745,0.02600,0.01927,0.0200,0.1822,1.0000 12.500,1.3871,0.02677,0.02006,0.0210,0.1793,1.0000 12.750,1.3942,0.02777,0.02126,0.0224,0.1759,1.0000 13.000,1.3999,0.02896,0.02258,0.0235,0.1725,1.0000 13.250,1.4053,0.03031,0.02401,0.0241,0.1694,1.0000 13.500,1.4104,0.03180,0.02553,0.0245,0.1666,1.0000 13.750,1.4133,0.03374,0.02764,0.0244,0.1632,1.0000 14.000,1.4148,0.03591,0.02997,0.0241,0.1597,1.0000 14.250,1.4148,0.03829,0.03244,0.0236,0.1563,1.0000 14.500,1.4150,0.04071,0.03487,0.0230,0.1534,1.0000 14.750,1.4103,0.04392,0.03829,0.0219,0.1500,1.0000 15.000,1.4041,0.04736,0.04186,0.0206,0.1465,1.0000 15.250,1.3974,0.05091,0.04547,0.0192,0.1432,1.0000 15.500,1.3904,0.05452,0.04914,0.0178,0.1403,1.0000 15.750,1.3758,0.05937,0.05418,0.0157,0.1369,1.0000 16.000,1.3614,0.06431,0.05923,0.0135,0.1335,1.0000 16.250,1.3514,0.06874,0.06370,0.0115,0.1303,1.0000 16.500,1.3368,0.07410,0.06917,0.0089,0.1271,1.0000 16.750,1.3136,0.08103,0.07626,0.0054,0.1235,1.0000 17.000,1.2986,0.08678,0.08208,0.0025,0.1200,1.0000 17.250,1.2913,0.09133,0.08664,0.0003,0.1165,1.0000 17.500,1.2604,0.10011,0.09560,-0.0042,0.1129,1.0000