Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ui1720-il-100000-n5 Airfoil,ui1720-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,29.0838 Max Cl/Cd alpha,4.5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-ui1720-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.3179,0.11311,0.10638,-0.0120,0.3948,0.0446 -9.750,-0.3160,0.10885,0.10208,-0.0142,0.3873,0.0450 -9.500,-0.3139,0.10479,0.09801,-0.0165,0.3805,0.0461 -9.250,-0.3026,0.10257,0.09572,-0.0172,0.3706,0.0478 -9.000,-0.2995,0.09868,0.09182,-0.0194,0.3659,0.0491 -8.750,-0.3001,0.09388,0.08703,-0.0224,0.3627,0.0500 -8.500,-0.3022,0.08869,0.08187,-0.0259,0.3602,0.0512 -8.250,-0.2887,0.08706,0.08019,-0.0262,0.3535,0.0528 -8.000,-0.2859,0.08298,0.07609,-0.0291,0.3506,0.0545 -7.000,-0.2752,0.05036,0.04313,-0.0678,0.3463,0.0637 -6.500,-0.2371,0.03850,0.03022,-0.0798,0.3390,0.0709 -6.250,-0.2125,0.03759,0.02916,-0.0801,0.3342,0.0731 -6.000,-0.1881,0.03319,0.02379,-0.0834,0.3310,0.0776 -5.750,-0.1624,0.03262,0.02322,-0.0832,0.3271,0.0794 -5.500,-0.1362,0.03168,0.02211,-0.0833,0.3234,0.0819 -5.250,-0.1092,0.02986,0.01975,-0.0841,0.3203,0.0853 -5.000,-0.0825,0.02883,0.01846,-0.0842,0.3176,0.0876 -4.750,-0.0557,0.02821,0.01769,-0.0841,0.3152,0.0899 -4.500,-0.0284,0.02743,0.01662,-0.0841,0.3131,0.0924 -4.250,-0.0005,0.02661,0.01538,-0.0841,0.3113,0.0953 -4.000,0.0271,0.02591,0.01456,-0.0840,0.3095,0.0973 -3.750,0.0547,0.02544,0.01402,-0.0838,0.3077,0.0994 -3.500,0.0825,0.02501,0.01348,-0.0836,0.3060,0.1021 -3.250,0.1106,0.02457,0.01284,-0.0834,0.3044,0.1049 -3.000,0.1388,0.02416,0.01225,-0.0831,0.3029,0.1071 -2.750,0.1662,0.02384,0.01195,-0.0828,0.3014,0.1097 -2.500,0.1939,0.02363,0.01169,-0.0826,0.3001,0.1131 -2.250,0.2218,0.02344,0.01139,-0.0823,0.2989,0.1167 -2.000,0.2496,0.02325,0.01111,-0.0819,0.2978,0.1200 -1.750,0.2771,0.02312,0.01099,-0.0817,0.2967,0.1242 -1.500,0.3049,0.02309,0.01090,-0.0814,0.2957,0.1300 -1.250,0.3325,0.02306,0.01084,-0.0811,0.2949,0.1361 -1.000,0.3602,0.02312,0.01086,-0.0808,0.2939,0.1438 -0.750,0.3877,0.02317,0.01094,-0.0806,0.2930,0.1540 -0.500,0.4152,0.02320,0.01106,-0.0803,0.2920,0.1687 -0.250,0.4427,0.02325,0.01123,-0.0800,0.2910,0.1896 0.000,0.4700,0.02333,0.01145,-0.0798,0.2899,0.2216 0.250,0.4970,0.02342,0.01175,-0.0795,0.2890,0.2684 0.500,0.5241,0.02355,0.01211,-0.0793,0.2882,0.3320 0.750,0.5510,0.02369,0.01252,-0.0790,0.2874,0.4135 1.000,0.5769,0.02379,0.01299,-0.0785,0.2867,0.5194 1.250,0.5997,0.02375,0.01345,-0.0771,0.2860,0.6658 1.500,0.6252,0.02356,0.01376,-0.0757,0.2853,0.9996 1.750,0.6523,0.02413,0.01423,-0.0755,0.2846,0.9996 2.000,0.6791,0.02472,0.01475,-0.0753,0.2840,0.9996 2.250,0.7057,0.02535,0.01531,-0.0750,0.2834,0.9996 2.500,0.7320,0.02600,0.01592,-0.0747,0.2828,0.9996 2.750,0.7580,0.02668,0.01657,-0.0744,0.2822,0.9996 3.000,0.7837,0.02740,0.01726,-0.0741,0.2817,0.9996 3.250,0.8091,0.02815,0.01800,-0.0738,0.2812,0.9996 3.500,0.8343,0.02894,0.01879,-0.0734,0.2807,0.9996 3.750,0.8592,0.02973,0.01957,-0.0730,0.2800,0.9996 4.000,0.8841,0.03049,0.02033,-0.0726,0.2793,0.9996 4.250,0.9088,0.03127,0.02108,-0.0723,0.2786,0.9996 4.500,0.9333,0.03209,0.02188,-0.0719,0.2779,0.9996 4.750,0.9574,0.03299,0.02280,-0.0715,0.2773,0.9996 5.000,0.9808,0.03400,0.02383,-0.0710,0.2769,0.9996 5.250,1.0039,0.03508,0.02494,-0.0706,0.2764,0.9996 5.500,1.0264,0.03627,0.02616,-0.0702,0.2760,0.9996 5.750,1.0465,0.03769,0.02769,-0.0696,0.2755,0.9996 6.000,1.0635,0.03942,0.02962,-0.0690,0.2750,0.9996 6.250,1.0780,0.04145,0.03187,-0.0683,0.2743,0.9996 6.500,1.0873,0.04406,0.03477,-0.0675,0.2730,0.9996 6.750,1.0913,0.04729,0.03830,-0.0669,0.2714,0.9996 7.000,1.0878,0.05148,0.04278,-0.0665,0.2699,0.9996 7.250,1.0732,0.05674,0.04833,-0.0665,0.2672,0.9996 7.500,1.0547,0.06233,0.05412,-0.0672,0.2646,0.9996 7.750,1.0480,0.06609,0.05795,-0.0673,0.2626,0.9996 8.000,1.0537,0.06846,0.06035,-0.0671,0.2614,0.9996 8.250,1.0634,0.07046,0.06235,-0.0668,0.2604,0.9996 8.500,1.0757,0.07222,0.06412,-0.0663,0.2597,0.9996 8.750,1.0880,0.07404,0.06594,-0.0658,0.2590,0.9996 11.750,0.7458,0.13759,0.13067,-0.0735,0.2107,0.9996 12.000,0.7425,0.14014,0.13327,-0.0740,0.2080,0.9996