Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-hq358-il-100000-n5 Airfoil,hq358-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,63.5038 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-hq358-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.500,-0.3501,0.09173,0.08718,-0.0317,1.0000,0.0343 -7.250,-0.3580,0.09002,0.08557,-0.0297,1.0000,0.0360 -7.000,-0.3700,0.08850,0.08414,-0.0274,1.0000,0.0357 -6.750,-0.3791,0.08665,0.08238,-0.0260,1.0000,0.0361 -6.500,-0.3860,0.08447,0.08028,-0.0254,1.0000,0.0369 -6.250,-0.3807,0.08114,0.07699,-0.0292,0.9978,0.0397 -6.000,-0.3432,0.07489,0.07061,-0.0461,0.9897,0.0422 -5.750,-0.3053,0.06969,0.06505,-0.0593,0.9824,0.0430 -5.500,-0.2906,0.06333,0.05880,-0.0613,0.9781,0.0442 -5.250,-0.2667,0.05874,0.05418,-0.0647,0.9744,0.0454 -5.000,-0.2416,0.05433,0.04962,-0.0689,0.9682,0.0461 -4.750,-0.2029,0.04807,0.04299,-0.0745,0.9638,0.0278 -4.500,-0.1697,0.04310,0.03774,-0.0793,0.9600,0.0247 -4.250,-0.1376,0.03858,0.03282,-0.0825,0.9542,0.0225 -4.000,-0.0978,0.03374,0.02734,-0.0860,0.9506,0.0203 -3.750,-0.0581,0.03020,0.02318,-0.0887,0.9481,0.0194 -3.500,-0.0279,0.02771,0.02022,-0.0894,0.9426,0.0191 -3.250,0.0064,0.02515,0.01719,-0.0910,0.9388,0.0194 -3.000,0.0418,0.02356,0.01529,-0.0930,0.9359,0.0226 -2.750,0.0739,0.02206,0.01348,-0.0936,0.9315,0.0254 -2.500,0.1054,0.02054,0.01170,-0.0940,0.9269,0.0264 -2.250,0.1402,0.01921,0.01019,-0.0950,0.9236,0.0282 -2.000,0.1766,0.01813,0.00897,-0.0965,0.9211,0.0308 -1.750,0.2030,0.01748,0.00821,-0.0963,0.9140,0.0381 -1.500,0.2377,0.01660,0.00749,-0.0978,0.9102,0.1019 -1.250,0.2627,0.01462,0.00762,-0.0974,0.9069,0.7081 -1.000,0.2802,0.01436,0.00752,-0.0943,0.8991,0.8128 -0.750,0.3179,0.01383,0.00706,-0.0953,0.8955,1.0000 -0.500,0.3479,0.01390,0.00690,-0.0960,0.8882,1.0000 -0.250,0.3828,0.01390,0.00664,-0.0974,0.8827,1.0000 0.000,0.4128,0.01395,0.00652,-0.0979,0.8747,1.0000 0.250,0.4472,0.01391,0.00633,-0.0991,0.8685,1.0000 0.500,0.4760,0.01393,0.00625,-0.0992,0.8590,1.0000 0.750,0.5078,0.01385,0.00606,-0.0997,0.8499,1.0000 1.000,0.5408,0.01370,0.00581,-0.1002,0.8403,1.0000 1.250,0.5696,0.01361,0.00566,-0.1000,0.8274,1.0000 1.500,0.5979,0.01354,0.00553,-0.0997,0.8142,1.0000 1.750,0.6257,0.01352,0.00550,-0.0994,0.8013,1.0000 2.000,0.6531,0.01355,0.00551,-0.0992,0.7892,1.0000 2.250,0.6807,0.01358,0.00553,-0.0989,0.7767,1.0000 2.500,0.7084,0.01361,0.00556,-0.0986,0.7635,1.0000 2.750,0.7360,0.01364,0.00565,-0.0983,0.7490,1.0000 3.000,0.7637,0.01367,0.00569,-0.0980,0.7335,1.0000 3.250,0.7903,0.01374,0.00579,-0.0975,0.7153,1.0000 3.500,0.8169,0.01381,0.00589,-0.0970,0.6952,1.0000 3.750,0.8432,0.01391,0.00600,-0.0964,0.6722,1.0000 4.000,0.8691,0.01404,0.00621,-0.0957,0.6456,1.0000 4.250,0.8944,0.01422,0.00637,-0.0949,0.6134,1.0000 4.500,0.9189,0.01447,0.00657,-0.0939,0.5745,1.0000 4.750,0.9422,0.01484,0.00680,-0.0928,0.5289,1.0000 5.000,0.9640,0.01535,0.00714,-0.0915,0.4796,1.0000 5.250,0.9849,0.01598,0.00759,-0.0902,0.4336,1.0000 5.500,1.0057,0.01666,0.00823,-0.0890,0.3936,1.0000 5.750,1.0268,0.01733,0.00885,-0.0879,0.3594,1.0000 6.000,1.0477,0.01803,0.00951,-0.0868,0.3291,1.0000 6.250,1.0684,0.01875,0.01022,-0.0857,0.3016,1.0000 6.500,1.0870,0.01959,0.01095,-0.0844,0.2651,1.0000 6.750,1.1055,0.02044,0.01173,-0.0831,0.2262,1.0000 7.000,1.1218,0.02149,0.01249,-0.0817,0.1580,1.0000 7.250,1.1299,0.02380,0.01396,-0.0796,0.0527,1.0000 7.500,1.1416,0.02594,0.01589,-0.0773,0.0216,1.0000 7.750,1.1547,0.02777,0.01788,-0.0751,0.0166,1.0000 8.000,1.1682,0.02935,0.01971,-0.0730,0.0140,1.0000 8.250,1.1813,0.03083,0.02141,-0.0710,0.0118,1.0000 8.500,1.1921,0.03245,0.02325,-0.0689,0.0105,1.0000 8.750,1.1998,0.03429,0.02531,-0.0663,0.0100,1.0000 9.000,1.2048,0.03630,0.02751,-0.0635,0.0095,1.0000 9.250,1.2097,0.03852,0.02993,-0.0608,0.0092,1.0000 9.500,1.2152,0.04102,0.03263,-0.0583,0.0090,1.0000 9.750,1.2214,0.04388,0.03572,-0.0562,0.0088,1.0000 10.000,1.2273,0.04705,0.03916,-0.0541,0.0086,1.0000 10.250,1.2304,0.05044,0.04286,-0.0521,0.0085,1.0000 10.500,1.2296,0.05397,0.04671,-0.0500,0.0085,1.0000 10.750,1.2252,0.05762,0.05068,-0.0481,0.0085,1.0000 11.000,1.2176,0.06141,0.05477,-0.0465,0.0085,1.0000 11.250,1.2078,0.06542,0.05907,-0.0454,0.0085,1.0000 11.500,1.1961,0.06973,0.06366,-0.0450,0.0085,1.0000 11.750,1.1834,0.07433,0.06851,-0.0452,0.0085,1.0000 12.000,1.1693,0.07939,0.07382,-0.0463,0.0085,1.0000 12.250,1.1550,0.08488,0.07954,-0.0483,0.0085,1.0000 12.500,1.1403,0.09088,0.08576,-0.0511,0.0086,1.0000 12.750,1.1256,0.09743,0.09251,-0.0547,0.0086,1.0000