Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-giiim-il-50000-n5 Airfoil,giiim-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,31.2628 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-giiim-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.5347,0.11462,0.10725,0.0092,1.0000,0.1058 -9.000,-0.5412,0.11177,0.10449,0.0049,1.0000,0.1098 -8.750,-0.5566,0.10898,0.10179,-0.0026,1.0000,0.1110 -8.500,-0.5352,0.10373,0.09657,0.0016,1.0000,0.1138 -8.250,-0.5249,0.10011,0.09297,0.0021,1.0000,0.1178 -8.000,-0.5247,0.09661,0.08952,-0.0006,1.0000,0.1224 -7.750,-0.5474,0.09368,0.08657,-0.0117,1.0000,0.1268 -7.500,-0.5260,0.08860,0.08163,-0.0072,1.0000,0.1304 -7.250,-0.5171,0.08513,0.07819,-0.0075,1.0000,0.1360 -7.000,-0.5228,0.08129,0.07430,-0.0131,1.0000,0.1446 -6.750,-0.5076,0.07774,0.07083,-0.0111,1.0000,0.1510 -6.500,-0.5038,0.07417,0.06726,-0.0128,1.0000,0.1638 -6.000,-0.4878,0.06797,0.06114,-0.0123,1.0000,0.2001 -5.000,-0.4037,0.05051,0.04183,-0.0216,1.0000,0.0810 -4.750,-0.3866,0.04734,0.03858,-0.0210,1.0000,0.0787 -4.500,-0.3685,0.04469,0.03570,-0.0203,1.0000,0.0779 -4.250,-0.3500,0.04224,0.03299,-0.0194,1.0000,0.0773 -4.000,-0.3307,0.03987,0.03034,-0.0184,1.0000,0.0756 -3.750,-0.3106,0.03765,0.02778,-0.0172,1.0000,0.0735 -3.500,-0.2900,0.03572,0.02550,-0.0159,1.0000,0.0724 -3.250,-0.2701,0.03401,0.02362,-0.0149,1.0000,0.0737 -3.000,-0.2497,0.03248,0.02190,-0.0137,1.0000,0.0753 -2.750,-0.2286,0.03102,0.02021,-0.0125,1.0000,0.0757 -2.500,-0.2070,0.02966,0.01864,-0.0114,1.0000,0.0757 -2.250,-0.1853,0.02846,0.01726,-0.0103,1.0000,0.0763 -2.000,-0.1637,0.02749,0.01613,-0.0092,1.0000,0.0786 -1.750,-0.1419,0.02666,0.01511,-0.0082,1.0000,0.0806 -1.500,-0.1121,0.02576,0.01406,-0.0086,0.9959,0.0816 -1.250,-0.0684,0.02458,0.01287,-0.0114,0.9848,0.0837 -1.000,-0.0253,0.02364,0.01198,-0.0143,0.9728,0.0888 -0.750,0.0178,0.02293,0.01121,-0.0170,0.9599,0.0926 -0.500,0.0609,0.02232,0.01052,-0.0197,0.9465,0.0967 -0.250,0.1004,0.02162,0.00990,-0.0221,0.9314,0.1045 0.000,0.1390,0.02120,0.00940,-0.0240,0.9149,0.1113 0.250,0.1755,0.02070,0.00896,-0.0256,0.8980,0.1245 0.500,0.2104,0.02021,0.00862,-0.0267,0.8806,0.1465 0.750,0.2758,0.01744,0.00856,-0.0318,0.8688,1.0000 1.000,0.3075,0.01756,0.00843,-0.0319,0.8479,1.0000 1.250,0.3337,0.01769,0.00839,-0.0310,0.8233,1.0000 1.500,0.3594,0.01776,0.00828,-0.0296,0.7974,1.0000 1.750,0.3819,0.01786,0.00823,-0.0278,0.7687,1.0000 2.000,0.4047,0.01795,0.00817,-0.0259,0.7415,1.0000 2.250,0.4273,0.01807,0.00819,-0.0242,0.7152,1.0000 2.500,0.4502,0.01822,0.00823,-0.0227,0.6906,1.0000 2.750,0.4732,0.01837,0.00828,-0.0211,0.6656,1.0000 3.000,0.4961,0.01855,0.00836,-0.0195,0.6391,1.0000 3.250,0.5188,0.01874,0.00841,-0.0178,0.6113,1.0000 3.500,0.5411,0.01897,0.00852,-0.0161,0.5803,1.0000 3.750,0.5632,0.01924,0.00866,-0.0145,0.5471,1.0000 4.000,0.5851,0.01956,0.00885,-0.0129,0.5118,1.0000 4.250,0.6071,0.01994,0.00912,-0.0115,0.4722,1.0000 4.500,0.6287,0.02036,0.00940,-0.0101,0.4295,1.0000 4.750,0.6501,0.02085,0.00976,-0.0088,0.3816,1.0000 5.000,0.6709,0.02146,0.01013,-0.0075,0.3334,1.0000 5.250,0.6915,0.02227,0.01064,-0.0064,0.2935,1.0000 5.500,0.7124,0.02321,0.01134,-0.0055,0.2607,1.0000 5.750,0.7332,0.02423,0.01217,-0.0046,0.2355,1.0000 6.000,0.7548,0.02524,0.01311,-0.0038,0.2133,1.0000 6.250,0.7765,0.02629,0.01410,-0.0030,0.1953,1.0000 6.500,0.7984,0.02735,0.01515,-0.0022,0.1799,1.0000 6.750,0.8203,0.02844,0.01622,-0.0015,0.1671,1.0000 7.000,0.8418,0.02954,0.01723,-0.0007,0.1560,1.0000 7.250,0.8640,0.03070,0.01853,0.0000,0.1454,1.0000 7.500,0.8857,0.03195,0.01986,0.0007,0.1365,1.0000 7.750,0.9071,0.03318,0.02110,0.0014,0.1289,1.0000 8.000,0.9284,0.03468,0.02278,0.0022,0.1216,1.0000 8.250,0.9490,0.03605,0.02420,0.0028,0.1153,1.0000 8.500,0.9694,0.03781,0.02613,0.0035,0.1103,1.0000 8.750,0.9878,0.03962,0.02821,0.0043,0.1048,1.0000 9.000,1.0072,0.04115,0.02974,0.0049,0.1005,1.0000 9.250,1.0231,0.04360,0.03253,0.0058,0.0971,1.0000 9.500,1.0356,0.04621,0.03556,0.0067,0.0935,1.0000 9.750,1.0487,0.04841,0.03796,0.0075,0.0901,1.0000 10.000,1.0644,0.05027,0.03983,0.0081,0.0874,1.0000 10.250,1.0681,0.05373,0.04369,0.0091,0.0856,1.0000 10.500,1.0631,0.05785,0.04830,0.0101,0.0841,1.0000 10.750,1.0517,0.06222,0.05307,0.0108,0.0829,1.0000 11.000,1.0316,0.06688,0.05802,0.0112,0.0823,1.0000 11.250,1.0022,0.07284,0.06424,0.0097,0.0822,1.0000 11.500,0.9608,0.08191,0.07352,0.0041,0.0829,1.0000 11.750,0.9104,0.09564,0.08736,-0.0059,0.0839,1.0000