Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-sc20710-il-100000 Airfoil,sc20710-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,32.3289 Max Cl/Cd alpha,3 Url,http://airfoiltools.com/polar/csv?polar=xf-sc20710-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.5548,0.10018,0.09471,-0.0281,1.0000,0.1510 -10.000,-0.5415,0.09774,0.09227,-0.0262,1.0000,0.1563 -9.750,-0.5938,0.09314,0.08787,-0.0319,1.0000,0.1632 -9.500,-0.5674,0.08982,0.08453,-0.0284,1.0000,0.1672 -9.250,-0.5599,0.08723,0.08195,-0.0267,1.0000,0.1720 -9.000,-0.6431,0.08106,0.07599,-0.0349,1.0000,0.1792 -8.750,-0.6085,0.07923,0.07420,-0.0275,1.0000,0.1833 -8.500,-0.6886,0.04997,0.04340,-0.0526,1.0000,0.0911 -8.250,-0.6715,0.04493,0.03796,-0.0537,1.0000,0.0849 -8.000,-0.6507,0.03986,0.03236,-0.0555,1.0000,0.0819 -7.750,-0.6252,0.03569,0.02761,-0.0572,1.0000,0.0810 -7.500,-0.5988,0.03308,0.02458,-0.0582,1.0000,0.0836 -7.250,-0.5702,0.03078,0.02177,-0.0592,1.0000,0.0871 -7.000,-0.5415,0.02845,0.01901,-0.0599,1.0000,0.0896 -6.750,-0.5165,0.02672,0.01734,-0.0600,1.0000,0.0950 -6.500,-0.4888,0.02547,0.01581,-0.0601,1.0000,0.1012 -6.250,-0.4627,0.02389,0.01424,-0.0601,1.0000,0.1076 -6.000,-0.4356,0.02291,0.01316,-0.0600,1.0000,0.1157 -5.750,-0.4094,0.02171,0.01208,-0.0598,1.0000,0.1244 -5.500,-0.3818,0.02074,0.01112,-0.0598,1.0000,0.1358 -5.250,-0.3533,0.01981,0.01035,-0.0601,1.0000,0.1513 -5.000,-0.3225,0.01887,0.00962,-0.0611,1.0000,0.1788 -4.750,-0.2717,0.01605,0.00914,-0.0675,1.0000,0.4973 -4.500,-0.2619,0.01718,0.01056,-0.0616,1.0000,0.6322 -4.250,-0.2516,0.01826,0.01160,-0.0561,1.0000,0.6668 -4.000,-0.2383,0.01922,0.01248,-0.0517,1.0000,0.6942 -3.750,-0.2293,0.02003,0.01326,-0.0462,1.0000,0.7119 -3.500,-0.2187,0.02068,0.01387,-0.0412,1.0000,0.7290 -3.250,-0.2080,0.02119,0.01435,-0.0364,1.0000,0.7458 -3.000,-0.1983,0.02158,0.01472,-0.0314,1.0000,0.7628 -2.750,-0.1886,0.02184,0.01496,-0.0266,1.0000,0.7806 -2.500,-0.1786,0.02198,0.01508,-0.0220,1.0000,0.7995 -2.250,-0.1652,0.02206,0.01512,-0.0183,1.0000,0.8209 -2.000,-0.1584,0.02181,0.01487,-0.0131,1.0000,0.8390 -1.750,-0.1463,0.02151,0.01455,-0.0096,1.0000,0.8560 -1.500,-0.1289,0.02119,0.01421,-0.0075,1.0000,0.8700 -1.250,-0.1066,0.02096,0.01393,-0.0069,1.0000,0.8815 -1.000,-0.0844,0.02070,0.01366,-0.0063,1.0000,0.8912 -0.750,-0.0620,0.02042,0.01337,-0.0058,1.0000,0.8992 -0.500,-0.0340,0.02036,0.01330,-0.0067,1.0000,0.9062 -0.250,-0.0106,0.02015,0.01309,-0.0066,1.0000,0.9125 0.000,0.0166,0.02012,0.01308,-0.0074,1.0000,0.9184 0.250,0.0438,0.02010,0.01310,-0.0083,1.0000,0.9234 0.500,0.0695,0.02009,0.01312,-0.0088,1.0000,0.9285 0.750,0.0987,0.02024,0.01333,-0.0102,1.0000,0.9329 1.000,0.1264,0.02038,0.01354,-0.0113,1.0000,0.9370 1.250,0.1534,0.02056,0.01380,-0.0124,1.0000,0.9410 1.500,0.1816,0.02085,0.01419,-0.0138,1.0000,0.9453 1.750,0.2276,0.02121,0.01469,-0.0184,0.9900,0.9486 2.000,0.3128,0.02089,0.01456,-0.0287,0.9556,0.9500 2.250,0.3775,0.01986,0.01374,-0.0342,0.9249,0.9523 2.500,0.4327,0.01845,0.01255,-0.0372,0.8934,0.9549 2.750,0.4792,0.01656,0.01090,-0.0375,0.8476,0.9579 3.000,0.5386,0.01666,0.00844,-0.0376,0.2980,0.9581 3.250,0.5558,0.01848,0.00929,-0.0362,0.1843,0.9619 3.500,0.5800,0.01955,0.01011,-0.0358,0.1557,0.9657 3.750,0.6080,0.02057,0.01102,-0.0361,0.1375,0.9694 4.250,0.6707,0.02284,0.01317,-0.0379,0.1140,0.9774 4.500,0.7048,0.02436,0.01475,-0.0391,0.1059,0.9825 4.750,0.7392,0.02596,0.01628,-0.0408,0.0974,0.9885 5.000,0.7722,0.02771,0.01837,-0.0417,0.0922,1.0000 5.250,0.8029,0.02929,0.02009,-0.0426,0.0861,1.0000 5.500,0.8339,0.03258,0.02345,-0.0440,0.0827,1.0000 5.750,0.8611,0.03491,0.02634,-0.0438,0.0813,1.0000 6.000,0.8859,0.03760,0.02960,-0.0435,0.0793,1.0000 6.250,0.9081,0.04081,0.03335,-0.0430,0.0780,1.0000 6.500,0.9278,0.04498,0.03800,-0.0424,0.0794,1.0000 6.750,0.9464,0.04978,0.04308,-0.0423,0.0815,1.0000 7.000,0.8966,0.07201,0.06791,-0.0400,0.1799,1.0000 7.250,0.9197,0.07584,0.07169,-0.0401,0.1741,1.0000 7.500,0.8913,0.08115,0.07728,-0.0415,0.1649,1.0000 7.750,0.9080,0.08479,0.08094,-0.0415,0.1593,1.0000 8.000,0.9037,0.09045,0.08664,-0.0423,0.1550,1.0000 8.250,0.8517,0.09781,0.09413,-0.0496,0.1509,1.0000 8.500,0.8475,0.10359,0.09990,-0.0540,0.1459,1.0000 8.750,0.8934,0.10527,0.10156,-0.0462,0.1405,1.0000 9.000,0.8401,0.11564,0.11192,-0.0615,0.1384,1.0000 9.250,0.8310,0.12150,0.11775,-0.0671,0.1322,1.0000