Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-dsma523b-il-50000-n5 Airfoil,dsma523b-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,20.6334 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-dsma523b-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.7782,0.07377,0.06479,-0.0466,1.0000,0.0704 -10.000,-0.7980,0.06841,0.05921,-0.0486,1.0000,0.0704 -9.750,-0.8061,0.06375,0.05430,-0.0501,1.0000,0.0708 -9.500,-0.7964,0.06131,0.05182,-0.0498,1.0000,0.0719 -9.250,-0.7899,0.05806,0.04839,-0.0505,1.0000,0.0731 -9.000,-0.7814,0.05453,0.04457,-0.0516,1.0000,0.0744 -8.750,-0.7692,0.05083,0.04047,-0.0529,1.0000,0.0756 -8.500,-0.7526,0.04728,0.03647,-0.0542,1.0000,0.0767 -8.250,-0.7325,0.04406,0.03275,-0.0553,1.0000,0.0779 -8.000,-0.7116,0.04224,0.03088,-0.0552,1.0000,0.0798 -7.750,-0.6896,0.04058,0.02911,-0.0552,1.0000,0.0824 -7.500,-0.6662,0.03864,0.02688,-0.0554,1.0000,0.0854 -7.250,-0.6433,0.03699,0.02508,-0.0550,1.0000,0.0877 -7.000,-0.6208,0.03572,0.02377,-0.0543,1.0000,0.0902 -6.750,-0.5976,0.03453,0.02245,-0.0536,1.0000,0.0942 -6.500,-0.5751,0.03345,0.02129,-0.0526,1.0000,0.0983 -6.250,-0.5534,0.03255,0.02043,-0.0513,1.0000,0.1023 -6.000,-0.5315,0.03177,0.01950,-0.0497,1.0000,0.1073 -5.750,-0.5100,0.03100,0.01881,-0.0484,1.0000,0.1130 -5.500,-0.4878,0.03029,0.01809,-0.0471,1.0000,0.1197 -5.250,-0.4651,0.02956,0.01742,-0.0462,1.0000,0.1275 -5.000,-0.4413,0.02887,0.01672,-0.0456,1.0000,0.1383 -4.750,-0.4161,0.02805,0.01608,-0.0456,1.0000,0.1524 -4.500,-0.3889,0.02716,0.01538,-0.0462,1.0000,0.1741 -4.250,-0.3580,0.02598,0.01465,-0.0481,1.0000,0.2195 -4.000,-0.3230,0.02460,0.01405,-0.0514,1.0000,0.3209 -3.750,-0.3107,0.02461,0.01498,-0.0467,1.0000,0.4347 -3.500,-0.3142,0.02594,0.01677,-0.0365,1.0000,0.5025 -3.250,-0.2936,0.02683,0.01763,-0.0337,1.0000,0.5787 -3.000,-0.2551,0.02729,0.01783,-0.0368,1.0000,0.6336 -2.750,-0.2301,0.02784,0.01825,-0.0358,1.0000,0.6602 -2.500,-0.2043,0.02839,0.01869,-0.0351,1.0000,0.6862 -2.250,-0.1877,0.02882,0.01908,-0.0318,1.0000,0.7057 -2.000,-0.1709,0.02912,0.01936,-0.0287,1.0000,0.7243 -1.750,-0.1567,0.02929,0.01952,-0.0249,1.0000,0.7417 -1.500,-0.1436,0.02937,0.01961,-0.0210,1.0000,0.7599 -1.250,-0.1306,0.02933,0.01959,-0.0171,1.0000,0.7780 -1.000,-0.1170,0.02916,0.01944,-0.0136,1.0000,0.7937 -0.750,-0.1000,0.02895,0.01923,-0.0111,1.0000,0.8070 -0.500,-0.0760,0.02886,0.01913,-0.0107,1.0000,0.8182 -0.250,-0.0561,0.02860,0.01889,-0.0093,1.0000,0.8257 0.000,-0.0280,0.02856,0.01886,-0.0101,1.0000,0.8314 0.250,-0.0007,0.02851,0.01885,-0.0107,1.0000,0.8358 0.500,0.0238,0.02841,0.01880,-0.0106,1.0000,0.8399 0.750,0.0506,0.02843,0.01889,-0.0111,1.0000,0.8439 1.000,0.0796,0.02855,0.01909,-0.0123,1.0000,0.8471 1.250,0.1099,0.02875,0.01939,-0.0138,1.0000,0.8500 1.500,0.1362,0.02886,0.01965,-0.0143,1.0000,0.8525 1.750,0.1626,0.02905,0.01999,-0.0149,1.0000,0.8547 2.000,0.2514,0.02848,0.01965,-0.0262,0.9524,0.8557 2.250,0.3084,0.02663,0.01800,-0.0296,0.8782,0.8571 2.500,0.3346,0.02588,0.01743,-0.0281,0.7987,0.8589 2.750,0.4382,0.02650,0.01522,-0.0381,0.2733,0.8590 3.000,0.4651,0.02771,0.01584,-0.0386,0.1955,0.8606 3.250,0.4955,0.02867,0.01651,-0.0396,0.1648,0.8623 3.500,0.5281,0.02956,0.01726,-0.0409,0.1469,0.8639 3.750,0.5631,0.03037,0.01810,-0.0425,0.1339,0.8651 4.000,0.6006,0.03130,0.01903,-0.0445,0.1238,0.8659 4.250,0.6364,0.03223,0.02000,-0.0461,0.1166,0.8667 4.500,0.6710,0.03336,0.02106,-0.0476,0.1103,0.8678 4.750,0.7039,0.03441,0.02229,-0.0485,0.1044,0.8692 5.000,0.7362,0.03568,0.02366,-0.0494,0.1005,0.8708 5.250,0.7675,0.03721,0.02513,-0.0505,0.0968,0.8723 5.500,0.7974,0.03874,0.02699,-0.0510,0.0928,0.8736 5.750,0.8264,0.04044,0.02901,-0.0514,0.0894,0.8747 6.000,0.8546,0.04238,0.03120,-0.0518,0.0872,0.8756 6.250,0.8810,0.04428,0.03328,-0.0522,0.0848,0.8765 6.500,0.9066,0.04652,0.03553,-0.0527,0.0824,0.8774 6.750,0.9257,0.04902,0.03870,-0.0517,0.0801,0.8785 7.000,0.9432,0.05193,0.04213,-0.0507,0.0785,0.8798 7.250,0.9564,0.05501,0.04569,-0.0492,0.0776,0.8811 7.500,0.9665,0.05829,0.04942,-0.0475,0.0767,0.8825 7.750,0.9738,0.06167,0.05321,-0.0459,0.0756,0.8839 8.000,0.9795,0.06502,0.05691,-0.0443,0.0744,0.8851 8.250,0.9850,0.06821,0.06036,-0.0430,0.0731,0.8862 8.500,0.9906,0.07138,0.06375,-0.0420,0.0720,0.8871 8.750,0.9972,0.07453,0.06703,-0.0411,0.0711,0.8880 9.000,0.9911,0.07875,0.07153,-0.0397,0.0709,0.8888 9.250,0.9601,0.08429,0.07749,-0.0373,0.0713,0.8894 9.500,0.9123,0.09252,0.08610,-0.0378,0.0725,0.8898 9.750,0.8656,0.10456,0.09839,-0.0454,0.0742,0.8900