Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-sc20010-il-200000 Airfoil,sc20010-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,39.4526 Max Cl/Cd alpha,3 Url,http://airfoiltools.com/polar/csv?polar=xf-sc20010-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.5702,0.08888,0.08535,-0.0097,1.0000,0.0779 -9.750,-0.5908,0.08117,0.07766,-0.0141,1.0000,0.0795 -9.500,-0.6295,0.07062,0.06711,-0.0217,1.0000,0.0798 -9.250,-0.8600,0.05430,0.04943,-0.0183,1.0000,0.0480 -9.000,-0.8590,0.04971,0.04461,-0.0171,1.0000,0.0471 -8.750,-0.8575,0.04482,0.03935,-0.0155,1.0000,0.0460 -8.500,-0.8565,0.03884,0.03276,-0.0133,1.0000,0.0441 -8.250,-0.8484,0.03384,0.02708,-0.0111,1.0000,0.0432 -8.000,-0.8307,0.03117,0.02407,-0.0099,1.0000,0.0436 -7.750,-0.8105,0.02902,0.02164,-0.0090,1.0000,0.0444 -7.500,-0.7889,0.02710,0.01945,-0.0081,1.0000,0.0456 -7.250,-0.7660,0.02558,0.01766,-0.0073,1.0000,0.0474 -7.000,-0.7428,0.02420,0.01597,-0.0065,1.0000,0.0495 -6.750,-0.7191,0.02242,0.01422,-0.0061,1.0000,0.0520 -6.500,-0.6947,0.02138,0.01311,-0.0055,1.0000,0.0549 -6.250,-0.6699,0.02047,0.01204,-0.0049,1.0000,0.0583 -6.000,-0.6466,0.01908,0.01070,-0.0043,1.0000,0.0628 -5.750,-0.6224,0.01849,0.01006,-0.0036,1.0000,0.0684 -5.500,-0.5996,0.01742,0.00902,-0.0028,1.0000,0.0740 -5.250,-0.5762,0.01689,0.00849,-0.0021,1.0000,0.0807 -5.000,-0.5544,0.01608,0.00773,-0.0011,1.0000,0.0873 -4.750,-0.5324,0.01562,0.00728,-0.0001,1.0000,0.0947 -4.500,-0.5125,0.01495,0.00669,0.0012,1.0000,0.1024 -4.250,-0.4924,0.01459,0.00631,0.0025,1.0000,0.1110 -4.000,-0.4754,0.01402,0.00585,0.0042,1.0000,0.1222 -3.750,-0.4589,0.01355,0.00549,0.0059,1.0000,0.1374 -3.500,-0.4423,0.01300,0.00515,0.0073,1.0000,0.1685 -3.250,-0.4258,0.01190,0.00478,0.0084,1.0000,0.2917 -3.000,-0.4036,0.01023,0.00473,0.0086,0.9975,0.6194 -2.750,-0.3681,0.01022,0.00491,0.0073,0.9925,0.7139 -2.500,-0.3320,0.01026,0.00499,0.0059,0.9868,0.7551 -2.250,-0.2954,0.01033,0.00509,0.0044,0.9824,0.7837 -2.000,-0.2623,0.01039,0.00516,0.0036,0.9762,0.8069 -1.750,-0.2263,0.01046,0.00525,0.0024,0.9720,0.8267 -1.500,-0.1934,0.01056,0.00538,0.0018,0.9669,0.8469 -1.250,-0.1625,0.01069,0.00553,0.0019,0.9611,0.8673 -1.000,-0.1302,0.01082,0.00569,0.0017,0.9571,0.8855 -0.750,-0.1013,0.01098,0.00586,0.0022,0.9515,0.9016 -0.500,-0.0699,0.01110,0.00598,0.0021,0.9454,0.9147 -0.250,-0.0342,0.01115,0.00603,0.0010,0.9408,0.9255 0.000,0.0000,0.01123,0.00612,0.0000,0.9341,0.9341 0.250,0.0342,0.01115,0.00603,-0.0010,0.9255,0.9408 0.500,0.0699,0.01110,0.00598,-0.0021,0.9147,0.9454 0.750,0.1013,0.01098,0.00586,-0.0022,0.9016,0.9515 1.000,0.1302,0.01082,0.00569,-0.0017,0.8855,0.9571 1.250,0.1625,0.01069,0.00553,-0.0019,0.8673,0.9611 1.500,0.1933,0.01056,0.00538,-0.0018,0.8469,0.9669 1.750,0.2263,0.01046,0.00525,-0.0024,0.8267,0.9721 2.000,0.2623,0.01039,0.00516,-0.0036,0.8069,0.9762 2.250,0.2954,0.01033,0.00509,-0.0044,0.7838,0.9824 2.500,0.3321,0.01026,0.00499,-0.0059,0.7551,0.9868 2.750,0.3681,0.01022,0.00491,-0.0073,0.7139,0.9926 3.000,0.4036,0.01023,0.00473,-0.0086,0.6195,0.9975 3.250,0.4257,0.01190,0.00478,-0.0083,0.2920,1.0000 3.500,0.4422,0.01300,0.00515,-0.0073,0.1685,1.0000 3.750,0.4588,0.01355,0.00549,-0.0058,0.1375,1.0000 4.000,0.4753,0.01402,0.00585,-0.0042,0.1222,1.0000 4.250,0.4924,0.01458,0.00631,-0.0025,0.1110,1.0000 4.500,0.5125,0.01495,0.00669,-0.0012,0.1025,1.0000 4.750,0.5324,0.01562,0.00728,0.0001,0.0947,1.0000 5.000,0.5544,0.01608,0.00772,0.0011,0.0873,1.0000 5.250,0.5762,0.01689,0.00849,0.0021,0.0807,1.0000 5.500,0.5996,0.01742,0.00902,0.0028,0.0740,1.0000 5.750,0.6224,0.01849,0.01006,0.0036,0.0684,1.0000 6.000,0.6466,0.01908,0.01070,0.0043,0.0628,1.0000 6.250,0.6699,0.02047,0.01204,0.0049,0.0583,1.0000 6.500,0.6947,0.02138,0.01312,0.0055,0.0549,1.0000 6.750,0.7191,0.02242,0.01422,0.0061,0.0520,1.0000 7.000,0.7428,0.02420,0.01598,0.0065,0.0495,1.0000 7.250,0.7660,0.02558,0.01766,0.0073,0.0475,1.0000 7.500,0.7889,0.02710,0.01945,0.0081,0.0456,1.0000 7.750,0.8105,0.02902,0.02163,0.0090,0.0444,1.0000 8.000,0.8308,0.03117,0.02406,0.0099,0.0436,1.0000 8.250,0.8484,0.03387,0.02711,0.0111,0.0432,1.0000 8.500,0.8566,0.03883,0.03275,0.0133,0.0441,1.0000 8.750,0.8575,0.04482,0.03935,0.0155,0.0459,1.0000 9.000,0.8591,0.04972,0.04461,0.0171,0.0471,1.0000 9.250,0.8602,0.05431,0.04943,0.0183,0.0480,1.0000 10.250,0.5593,0.09454,0.09098,0.0074,0.0763,1.0000 10.500,0.5544,0.09929,0.09572,0.0059,0.0748,1.0000