Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-dsma523b-il-200000 Airfoil,dsma523b-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,29.7512 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-dsma523b-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.6224,0.09817,0.09405,-0.0262,1.0000,0.0891 -10.000,-0.8806,0.05190,0.04593,-0.0549,1.0000,0.0572 -9.750,-0.8626,0.04908,0.04326,-0.0536,1.0000,0.0565 -9.500,-0.8491,0.04516,0.03909,-0.0547,1.0000,0.0562 -9.250,-0.8316,0.04128,0.03479,-0.0567,1.0000,0.0562 -9.000,-0.8089,0.03784,0.03086,-0.0589,1.0000,0.0564 -8.750,-0.7829,0.03504,0.02761,-0.0608,1.0000,0.0566 -8.500,-0.7540,0.03300,0.02507,-0.0627,1.0000,0.0571 -8.250,-0.7306,0.03045,0.02248,-0.0628,1.0000,0.0579 -8.000,-0.7071,0.02894,0.02101,-0.0625,1.0000,0.0590 -7.750,-0.6810,0.02770,0.01968,-0.0628,1.0000,0.0608 -7.500,-0.6521,0.02655,0.01825,-0.0636,1.0000,0.0627 -7.250,-0.6246,0.02515,0.01667,-0.0640,1.0000,0.0643 -7.000,-0.5996,0.02393,0.01551,-0.0636,1.0000,0.0660 -6.750,-0.5730,0.02302,0.01460,-0.0635,1.0000,0.0680 -6.500,-0.5444,0.02234,0.01378,-0.0638,1.0000,0.0704 -6.250,-0.5192,0.02124,0.01288,-0.0634,1.0000,0.0734 -6.000,-0.4911,0.02060,0.01226,-0.0637,1.0000,0.0766 -5.750,-0.4621,0.01984,0.01158,-0.0641,1.0000,0.0797 -5.500,-0.4316,0.01933,0.01116,-0.0651,1.0000,0.0842 -5.250,-0.3994,0.01879,0.01070,-0.0664,1.0000,0.0893 -5.000,-0.3673,0.01843,0.01038,-0.0677,1.0000,0.0951 -4.750,-0.3328,0.01798,0.01003,-0.0696,1.0000,0.1025 -4.500,-0.2982,0.01762,0.00972,-0.0714,1.0000,0.1118 -4.250,-0.2617,0.01724,0.00945,-0.0738,1.0000,0.1258 -4.000,-0.2188,0.01663,0.00917,-0.0779,1.0000,0.1690 -3.750,-0.1409,0.01494,0.00890,-0.0911,1.0000,0.4412 -3.500,-0.1374,0.01580,0.01053,-0.0841,1.0000,0.5588 -3.250,-0.1134,0.01629,0.01101,-0.0830,1.0000,0.6113 -3.000,-0.0892,0.01678,0.01146,-0.0819,1.0000,0.6328 -2.750,-0.0656,0.01733,0.01195,-0.0806,1.0000,0.6495 -2.500,-0.0510,0.01792,0.01258,-0.0770,1.0000,0.6558 -2.250,-0.0218,0.01826,0.01286,-0.0773,1.0000,0.6677 -2.000,-0.0073,0.01876,0.01341,-0.0737,1.0000,0.6720 -1.750,0.0123,0.01919,0.01386,-0.0716,1.0000,0.6788 -1.500,0.0393,0.01950,0.01415,-0.0714,1.0000,0.6875 -1.250,0.0530,0.01994,0.01467,-0.0678,1.0000,0.6920 -1.000,0.0739,0.02039,0.01515,-0.0660,1.0000,0.7015 -0.750,0.0848,0.02091,0.01575,-0.0616,1.0000,0.7100 -0.500,0.1018,0.02154,0.01644,-0.0588,1.0000,0.7250 -0.250,0.1042,0.02197,0.01698,-0.0523,1.0000,0.7330 0.000,0.1363,0.02231,0.01735,-0.0531,0.9977,0.7448 0.250,0.1963,0.02203,0.01714,-0.0580,0.9826,0.7508 0.500,0.2674,0.02139,0.01654,-0.0658,0.9672,0.7584 0.750,0.3050,0.02059,0.01582,-0.0668,0.9490,0.7648 1.000,0.3426,0.01937,0.01469,-0.0667,0.9302,0.7723 1.250,0.4669,0.01777,0.01154,-0.0820,0.5268,0.7841 1.500,0.4688,0.01948,0.01190,-0.0767,0.2555,0.7884 1.750,0.4898,0.02058,0.01232,-0.0756,0.1430,0.7939 2.000,0.5235,0.02127,0.01282,-0.0774,0.1206,0.7995 2.250,0.5389,0.02147,0.01294,-0.0743,0.1111,0.8029 2.500,0.5642,0.02173,0.01320,-0.0737,0.1043,0.8052 2.750,0.5917,0.02235,0.01371,-0.0738,0.0975,0.8065 3.000,0.6220,0.02283,0.01419,-0.0745,0.0926,0.8074 3.250,0.6519,0.02333,0.01467,-0.0751,0.0883,0.8091 3.500,0.6827,0.02407,0.01533,-0.0759,0.0845,0.8106 3.750,0.7153,0.02509,0.01633,-0.0772,0.0809,0.8113 4.000,0.7478,0.02565,0.01695,-0.0782,0.0778,0.8118 4.250,0.7804,0.02642,0.01775,-0.0794,0.0751,0.8128 4.500,0.8131,0.02733,0.01861,-0.0807,0.0723,0.8140 4.750,0.8462,0.02897,0.02029,-0.0821,0.0696,0.8146 5.000,0.8775,0.02976,0.02127,-0.0828,0.0677,0.8148 5.250,0.9088,0.03094,0.02264,-0.0836,0.0659,0.8152 5.500,0.9404,0.03233,0.02418,-0.0845,0.0643,0.8162 5.750,0.9710,0.03378,0.02575,-0.0853,0.0631,0.8168 6.000,0.9988,0.03518,0.02722,-0.0857,0.0617,0.8170 6.250,1.0235,0.03832,0.03050,-0.0858,0.0603,0.8172 6.500,1.0453,0.03984,0.03244,-0.0846,0.0593,0.8174 6.750,1.0656,0.04242,0.03541,-0.0834,0.0591,0.8176 7.000,1.0828,0.04551,0.03891,-0.0819,0.0591,0.8179 7.250,1.0973,0.04896,0.04273,-0.0802,0.0592,0.8181 7.500,1.1086,0.05265,0.04679,-0.0781,0.0593,0.8183 7.750,1.1190,0.05714,0.05152,-0.0765,0.0598,0.8186 8.000,1.0575,0.07538,0.07142,-0.0662,0.0845,0.8184 8.250,1.0735,0.07892,0.07490,-0.0660,0.0836,0.8191 8.500,1.0665,0.08852,0.08452,-0.0658,0.0823,0.8196 8.750,1.0444,0.09186,0.08820,-0.0624,0.0820,0.8199 9.000,0.9955,0.09564,0.09231,-0.0582,0.0815,0.8197