Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-s6063-il-500000-n5 Airfoil,s6063-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,60.1908 Max Cl/Cd alpha,2 Url,http://airfoiltools.com/polar/csv?polar=xf-s6063-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.000,-0.5591,0.07473,0.07260,-0.0108,1.0000,0.0066 -7.750,-0.5634,0.06900,0.06690,-0.0168,1.0000,0.0063 -7.500,-0.5601,0.06246,0.06032,-0.0233,1.0000,0.0063 -7.250,-0.5545,0.05541,0.05315,-0.0286,1.0000,0.0063 -7.000,-0.5457,0.04878,0.04636,-0.0322,1.0000,0.0064 -6.000,-0.4882,0.02799,0.02431,-0.0351,1.0000,0.0067 -5.750,-0.4714,0.02402,0.01989,-0.0343,1.0000,0.0064 -5.500,-0.4523,0.02110,0.01658,-0.0333,0.9997,0.0063 -5.250,-0.4213,0.01834,0.01338,-0.0345,0.9931,0.0061 -5.000,-0.3897,0.01627,0.01093,-0.0355,0.9870,0.0061 -4.750,-0.3580,0.01465,0.00904,-0.0363,0.9810,0.0061 -4.500,-0.3267,0.01336,0.00754,-0.0371,0.9741,0.0061 -4.250,-0.2961,0.01231,0.00634,-0.0377,0.9666,0.0063 -4.000,-0.2659,0.01147,0.00539,-0.0381,0.9584,0.0065 -3.750,-0.2378,0.01083,0.00463,-0.0381,0.9484,0.0068 -3.500,-0.2103,0.01036,0.00409,-0.0379,0.9379,0.0071 -3.250,-0.1842,0.00968,0.00329,-0.0375,0.9270,0.0077 -3.000,-0.1582,0.00923,0.00275,-0.0370,0.9161,0.0095 -2.750,-0.1318,0.00896,0.00238,-0.0365,0.9047,0.0102 -2.500,-0.1052,0.00874,0.00206,-0.0361,0.8934,0.0109 -2.250,-0.0786,0.00856,0.00180,-0.0356,0.8816,0.0123 -2.000,-0.0522,0.00829,0.00157,-0.0352,0.8692,0.0351 -1.750,-0.0264,0.00782,0.00137,-0.0349,0.8561,0.1164 -1.500,-0.0007,0.00735,0.00122,-0.0347,0.8426,0.2213 -1.250,0.0251,0.00690,0.00112,-0.0344,0.8287,0.3366 -1.000,0.0491,0.00615,0.00106,-0.0340,0.8141,0.5450 -0.750,0.0747,0.00589,0.00102,-0.0335,0.7983,0.6296 -0.500,0.1000,0.00568,0.00099,-0.0328,0.7814,0.7047 -0.250,0.1249,0.00552,0.00098,-0.0320,0.7636,0.7711 0.000,0.1494,0.00542,0.00098,-0.0309,0.7450,0.8276 0.250,0.1733,0.00535,0.00098,-0.0297,0.7250,0.8795 0.500,0.1991,0.00535,0.00098,-0.0289,0.7035,0.9264 0.750,0.2323,0.00541,0.00096,-0.0298,0.6780,0.9609 1.000,0.2685,0.00551,0.00095,-0.0316,0.6491,0.9858 1.250,0.3013,0.00564,0.00095,-0.0328,0.6192,1.0000 1.500,0.3273,0.00580,0.00100,-0.0324,0.5902,1.0000 1.750,0.3534,0.00597,0.00105,-0.0320,0.5603,1.0000 2.000,0.3786,0.00629,0.00112,-0.0316,0.5020,1.0000 2.250,0.4027,0.00684,0.00123,-0.0311,0.4044,1.0000 2.500,0.4281,0.00722,0.00138,-0.0308,0.3451,1.0000 2.750,0.4537,0.00762,0.00154,-0.0306,0.2866,1.0000 3.000,0.4788,0.00812,0.00174,-0.0303,0.2173,1.0000 3.250,0.5033,0.00878,0.00201,-0.0300,0.1322,1.0000 3.500,0.5269,0.00966,0.00244,-0.0297,0.0360,1.0000 3.750,0.5529,0.01008,0.00275,-0.0294,0.0137,1.0000 4.000,0.5796,0.01033,0.00303,-0.0292,0.0120,1.0000 4.250,0.6061,0.01061,0.00336,-0.0290,0.0111,1.0000 4.500,0.6325,0.01094,0.00377,-0.0287,0.0105,1.0000 4.750,0.6587,0.01131,0.00421,-0.0284,0.0100,1.0000 5.000,0.6846,0.01174,0.00471,-0.0281,0.0097,1.0000 5.250,0.7101,0.01224,0.00528,-0.0277,0.0095,1.0000 5.500,0.7353,0.01281,0.00592,-0.0273,0.0092,1.0000 5.750,0.7600,0.01345,0.00665,-0.0269,0.0086,1.0000 6.000,0.7836,0.01430,0.00758,-0.0263,0.0080,1.0000 6.250,0.8065,0.01529,0.00866,-0.0256,0.0077,1.0000 6.500,0.8283,0.01660,0.01009,-0.0248,0.0075,1.0000 6.750,0.8499,0.01812,0.01175,-0.0239,0.0072,1.0000 7.000,0.8734,0.01909,0.01285,-0.0233,0.0071,1.0000 7.250,0.8966,0.02015,0.01405,-0.0227,0.0069,1.0000 7.500,0.9190,0.02145,0.01552,-0.0219,0.0068,1.0000 7.750,0.9404,0.02301,0.01731,-0.0211,0.0067,1.0000 8.000,0.9607,0.02481,0.01936,-0.0202,0.0066,1.0000 8.250,0.9793,0.02691,0.02173,-0.0192,0.0065,1.0000 8.500,0.9957,0.02932,0.02446,-0.0180,0.0065,1.0000 8.750,1.0092,0.03208,0.02756,-0.0167,0.0065,1.0000 9.000,1.0193,0.03514,0.03097,-0.0153,0.0065,1.0000 9.250,1.0280,0.03796,0.03409,-0.0139,0.0064,1.0000 9.500,1.0317,0.04121,0.03766,-0.0123,0.0063,1.0000 9.750,1.0323,0.04438,0.04110,-0.0107,0.0061,1.0000 10.000,1.0266,0.04767,0.04464,-0.0089,0.0059,1.0000 10.250,1.0098,0.05105,0.04822,-0.0066,0.0059,1.0000 10.500,0.9905,0.05516,0.05252,-0.0063,0.0060,1.0000 10.750,0.9698,0.06051,0.05803,-0.0087,0.0060,1.0000 11.000,0.9495,0.06745,0.06512,-0.0138,0.0061,1.0000 11.250,0.9245,0.07821,0.07604,-0.0229,0.0062,1.0000