Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-sd7062-il-50000 Airfoil,sd7062-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,12.0907 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-sd7062-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.2564,0.11919,0.11235,-0.0305,1.0000,0.2289 -9.500,-0.2373,0.11508,0.10827,-0.0295,1.0000,0.2361 -9.250,-0.2607,0.11580,0.10916,-0.0303,1.0000,0.2439 -9.000,-0.2381,0.11046,0.10386,-0.0291,1.0000,0.2490 -8.750,-0.2381,0.10865,0.10215,-0.0282,1.0000,0.2585 -8.500,-0.2513,0.10731,0.10098,-0.0276,1.0000,0.2638 -8.250,-0.2367,0.10411,0.09785,-0.0257,1.0000,0.2741 -8.000,-0.2791,0.10619,0.10018,-0.0234,1.0000,0.2792 -7.750,-0.2480,0.10088,0.09488,-0.0212,1.0000,0.2887 -7.500,-0.2800,0.10191,0.09611,-0.0175,1.0000,0.2955 -7.250,-0.2907,0.10031,0.09464,-0.0143,1.0000,0.3002 -7.000,-0.2915,0.09874,0.09315,-0.0110,1.0000,0.3089 -6.750,-0.3383,0.10069,0.09531,-0.0065,1.0000,0.3141 -6.500,-0.3241,0.09711,0.09177,-0.0044,1.0000,0.3213 -6.250,-0.3511,0.09742,0.09222,-0.0005,1.0000,0.3301 -6.000,-0.3832,0.09727,0.09223,0.0033,1.0000,0.3347 -5.750,-0.3703,0.09451,0.08950,0.0053,1.0000,0.3440 -5.500,-0.4210,0.09556,0.09074,0.0093,1.0000,0.3519 -5.250,-0.4031,0.09234,0.08753,0.0118,1.0000,0.3597 -5.000,-0.4320,0.09168,0.08700,0.0142,1.0000,0.3711 -4.750,-0.4509,0.06286,0.05685,-0.0352,0.9989,0.1589 -4.500,-0.4097,0.05494,0.04829,-0.0438,0.9909,0.1419 -4.250,-0.3675,0.05017,0.04311,-0.0497,0.9817,0.1363 -4.000,-0.3236,0.04540,0.03748,-0.0556,0.9723,0.1319 -3.750,-0.2845,0.04298,0.03461,-0.0592,0.9620,0.1345 -3.500,-0.2423,0.04097,0.03205,-0.0627,0.9516,0.1396 -3.250,-0.1965,0.03904,0.02959,-0.0663,0.9415,0.1452 -3.000,-0.1637,0.03798,0.02842,-0.0677,0.9299,0.1555 -2.750,-0.1247,0.03698,0.02728,-0.0698,0.9191,0.1735 -2.500,-0.0833,0.03598,0.02632,-0.0721,0.9086,0.2097 -2.250,-0.0563,0.03508,0.02592,-0.0723,0.8969,0.2715 -2.000,-0.0202,0.03413,0.02596,-0.0731,0.8870,0.4345 -1.750,-0.0015,0.03401,0.02652,-0.0702,0.8752,0.5731 -1.500,0.0116,0.03422,0.02708,-0.0660,0.8638,0.6723 -1.250,0.0313,0.03434,0.02745,-0.0617,0.8540,0.7719 -1.000,0.0323,0.03438,0.02768,-0.0556,0.8419,0.8520 -0.750,0.1248,0.03455,0.02753,-0.0674,0.8282,1.0000 -0.500,0.1732,0.03488,0.02736,-0.0729,0.8169,1.0000 -0.250,0.1930,0.03557,0.02773,-0.0734,0.8031,1.0000 0.000,0.2168,0.03638,0.02826,-0.0742,0.7904,1.0000 0.250,0.2584,0.03697,0.02854,-0.0767,0.7791,1.0000 0.500,0.2842,0.03776,0.02911,-0.0772,0.7667,1.0000 0.750,0.3027,0.03875,0.02991,-0.0768,0.7537,1.0000 1.000,0.3383,0.03941,0.03036,-0.0781,0.7425,1.0000 1.250,0.3672,0.04016,0.03095,-0.0787,0.7307,1.0000 1.500,0.3802,0.04140,0.03206,-0.0776,0.7177,1.0000 1.750,0.4131,0.04212,0.03263,-0.0784,0.7070,1.0000 2.000,0.4416,0.04287,0.03326,-0.0787,0.6954,1.0000 2.250,0.4501,0.04441,0.03470,-0.0773,0.6825,1.0000 2.500,0.4823,0.04513,0.03532,-0.0778,0.6722,1.0000 2.750,0.5075,0.04601,0.03611,-0.0777,0.6606,1.0000 3.000,0.5116,0.04793,0.03797,-0.0762,0.6481,1.0000 3.250,0.5515,0.04826,0.03821,-0.0770,0.6387,1.0000 3.500,0.5621,0.04989,0.03979,-0.0759,0.6264,1.0000 3.750,0.5652,0.05211,0.04197,-0.0747,0.6146,1.0000 4.000,0.6211,0.05137,0.04117,-0.0758,0.6063,1.0000 4.250,0.6040,0.05483,0.04461,-0.0738,0.5932,1.0000 4.500,0.6134,0.05689,0.04663,-0.0731,0.5826,1.0000 4.750,0.6515,0.05711,0.04683,-0.0732,0.5731,1.0000 5.000,0.6365,0.06083,0.05053,-0.0719,0.5616,1.0000 5.250,0.6769,0.06097,0.05065,-0.0719,0.5529,1.0000 5.500,0.6644,0.06468,0.05436,-0.0710,0.5419,1.0000 5.750,0.6744,0.06699,0.05666,-0.0706,0.5325,1.0000 6.000,0.6905,0.06886,0.05854,-0.0703,0.5232,1.0000 6.250,0.6861,0.07234,0.06202,-0.0699,0.5143,1.0000 6.500,0.7113,0.07363,0.06332,-0.0696,0.5053,1.0000 6.750,0.6995,0.07792,0.06761,-0.0696,0.4979,1.0000 7.000,0.7150,0.08004,0.06975,-0.0694,0.4892,1.0000 7.250,0.7148,0.08361,0.07333,-0.0695,0.4822,1.0000 7.500,0.7044,0.08806,0.07781,-0.0700,0.4775,1.0000 7.750,0.7364,0.08910,0.07888,-0.0695,0.4673,1.0000 8.000,0.7193,0.09437,0.08418,-0.0705,0.4652,1.0000 8.250,0.7127,0.09904,0.08890,-0.0716,0.4647,1.0000 8.500,0.7115,0.10354,0.09344,-0.0727,0.4658,1.0000 8.750,0.7260,0.10790,0.09786,-0.0742,0.4696,1.0000