Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-sc20610-il-200000-n5 Airfoil,sc20610-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,43.1234 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-sc20610-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.750,-0.7273,0.08578,0.08161,-0.0357,1.0000,0.0228 -12.500,-0.8075,0.06322,0.05872,-0.0529,1.0000,0.0221 -12.250,-0.8398,0.05583,0.05107,-0.0569,1.0000,0.0220 -12.000,-0.8652,0.05065,0.04566,-0.0580,1.0000,0.0220 -11.750,-0.8875,0.04692,0.04172,-0.0567,1.0000,0.0220 -11.500,-0.9040,0.04348,0.03803,-0.0555,1.0000,0.0222 -11.250,-0.9101,0.03996,0.03417,-0.0552,1.0000,0.0224 -11.000,-0.9084,0.03687,0.03070,-0.0545,1.0000,0.0227 -10.750,-0.9006,0.03417,0.02763,-0.0539,1.0000,0.0230 -10.500,-0.8881,0.03190,0.02501,-0.0533,1.0000,0.0234 -10.250,-0.8724,0.03018,0.02316,-0.0528,1.0000,0.0238 -10.000,-0.8545,0.02889,0.02176,-0.0524,1.0000,0.0243 -9.750,-0.8354,0.02771,0.02049,-0.0520,1.0000,0.0248 -9.500,-0.8154,0.02655,0.01921,-0.0516,1.0000,0.0255 -9.250,-0.7946,0.02547,0.01798,-0.0512,1.0000,0.0264 -9.000,-0.7731,0.02441,0.01674,-0.0509,1.0000,0.0276 -8.750,-0.7510,0.02338,0.01552,-0.0505,1.0000,0.0286 -8.500,-0.7287,0.02242,0.01456,-0.0503,1.0000,0.0297 -8.250,-0.7054,0.02164,0.01375,-0.0502,1.0000,0.0308 -8.000,-0.6817,0.02086,0.01289,-0.0500,1.0000,0.0322 -7.750,-0.6573,0.02009,0.01202,-0.0499,1.0000,0.0339 -7.500,-0.6323,0.01930,0.01119,-0.0501,1.0000,0.0356 -7.250,-0.6069,0.01877,0.01067,-0.0503,1.0000,0.0379 -7.000,-0.5811,0.01827,0.01010,-0.0504,1.0000,0.0409 -6.750,-0.5544,0.01766,0.00948,-0.0509,1.0000,0.0439 -6.500,-0.5276,0.01721,0.00902,-0.0512,1.0000,0.0473 -6.250,-0.5005,0.01680,0.00855,-0.0516,1.0000,0.0512 -6.000,-0.4723,0.01631,0.00810,-0.0523,1.0000,0.0559 -5.750,-0.4443,0.01600,0.00773,-0.0528,1.0000,0.0610 -5.500,-0.4145,0.01553,0.00732,-0.0539,1.0000,0.0672 -5.250,-0.3818,0.01518,0.00694,-0.0554,0.9991,0.0746 -5.000,-0.3476,0.01479,0.00660,-0.0572,0.9980,0.0842 -4.750,-0.3131,0.01443,0.00629,-0.0591,0.9969,0.0977 -4.500,-0.2777,0.01404,0.00599,-0.0613,0.9958,0.1178 -4.000,-0.2029,0.01290,0.00546,-0.0670,0.9947,0.2471 -3.750,-0.1612,0.01192,0.00521,-0.0713,0.9953,0.4087 -3.500,-0.1260,0.01158,0.00558,-0.0731,0.9947,0.5619 -3.250,-0.0937,0.01169,0.00574,-0.0739,0.9924,0.6089 -3.000,-0.0621,0.01181,0.00587,-0.0746,0.9897,0.6324 -2.750,-0.0306,0.01198,0.00607,-0.0752,0.9871,0.6524 -2.500,0.0024,0.01221,0.00628,-0.0762,0.9849,0.6738 -2.250,0.0324,0.01247,0.00658,-0.0763,0.9818,0.6875 -2.000,0.0597,0.01272,0.00687,-0.0758,0.9778,0.6975 -1.750,0.0916,0.01289,0.00703,-0.0765,0.9751,0.7074 -1.500,0.1228,0.01306,0.00724,-0.0769,0.9726,0.7129 -1.250,0.1560,0.01311,0.00730,-0.0781,0.9694,0.7188 -1.000,0.1895,0.01308,0.00728,-0.0792,0.9638,0.7235 -0.750,0.2295,0.01297,0.00722,-0.0814,0.9589,0.7260 -0.500,0.2679,0.01273,0.00701,-0.0832,0.9490,0.7284 -0.250,0.3127,0.01232,0.00664,-0.0861,0.9381,0.7308 0.000,0.3527,0.01190,0.00624,-0.0879,0.9205,0.7333 0.250,0.3926,0.01150,0.00583,-0.0897,0.8938,0.7361 0.500,0.4295,0.01126,0.00556,-0.0910,0.8621,0.7392 0.750,0.4620,0.01115,0.00541,-0.0913,0.8154,0.7408 1.000,0.4904,0.01139,0.00515,-0.0903,0.6851,0.7426 1.250,0.5058,0.01262,0.00536,-0.0874,0.4802,0.7446 1.500,0.5256,0.01366,0.00571,-0.0861,0.3304,0.7470 1.750,0.5490,0.01446,0.00603,-0.0855,0.2259,0.7497 2.000,0.5749,0.01509,0.00631,-0.0855,0.1565,0.7525 2.250,0.6026,0.01559,0.00659,-0.0858,0.1194,0.7553 2.500,0.6282,0.01600,0.00692,-0.0853,0.0997,0.7570 2.750,0.6540,0.01638,0.00728,-0.0849,0.0865,0.7589 3.000,0.6801,0.01676,0.00766,-0.0845,0.0771,0.7610 3.250,0.7061,0.01722,0.00807,-0.0842,0.0695,0.7634 3.500,0.7331,0.01759,0.00849,-0.0840,0.0632,0.7661 3.750,0.7597,0.01812,0.00897,-0.0840,0.0578,0.7688 4.000,0.7877,0.01851,0.00940,-0.0841,0.0528,0.7715 4.250,0.8122,0.01907,0.00994,-0.0835,0.0485,0.7730 4.500,0.8377,0.01950,0.01047,-0.0830,0.0449,0.7748 4.750,0.8629,0.02001,0.01102,-0.0825,0.0419,0.7768 5.000,0.8874,0.02069,0.01170,-0.0819,0.0393,0.7792 5.250,0.9130,0.02127,0.01238,-0.0815,0.0365,0.7819 5.500,0.9389,0.02182,0.01295,-0.0813,0.0342,0.7848 5.750,0.9640,0.02264,0.01379,-0.0810,0.0325,0.7874 6.000,0.9878,0.02345,0.01474,-0.0801,0.0310,0.7892 6.250,1.0116,0.02429,0.01570,-0.0794,0.0296,0.7912 6.500,1.0354,0.02512,0.01660,-0.0787,0.0285,0.7935 6.750,1.0590,0.02603,0.01756,-0.0781,0.0276,0.7960 7.000,1.0824,0.02723,0.01887,-0.0775,0.0268,0.7987 7.250,1.1065,0.02844,0.02031,-0.0770,0.0257,0.8015 7.500,1.1287,0.02961,0.02169,-0.0761,0.0247,0.8037 7.750,1.1498,0.03073,0.02298,-0.0751,0.0239,0.8058 8.000,1.1703,0.03195,0.02438,-0.0740,0.0233,0.8082 8.250,1.1902,0.03321,0.02578,-0.0729,0.0228,0.8110 8.500,1.2092,0.03466,0.02736,-0.0719,0.0224,0.8141 8.750,1.2259,0.03671,0.02965,-0.0706,0.0221,0.8171 9.000,1.2377,0.03927,0.03268,-0.0684,0.0217,0.8193 9.250,1.2448,0.04235,0.03625,-0.0658,0.0214,0.8216 9.500,1.2457,0.04602,0.04044,-0.0627,0.0211,0.8240 9.750,1.2389,0.05029,0.04521,-0.0591,0.0208,0.8266 10.000,1.2233,0.05500,0.05039,-0.0551,0.0206,0.8294 10.250,1.1967,0.05958,0.05534,-0.0503,0.0205,0.8325 10.500,1.1641,0.06514,0.06125,-0.0471,0.0205,0.8348 10.750,1.1239,0.07264,0.06910,-0.0469,0.0206,0.8370