Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-oaf102-il-200000 Airfoil,oaf102-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,82.2222 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-oaf102-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.5526,0.07181,0.06843,-0.0411,1.0000,0.0408 -9.000,-0.5711,0.06190,0.05855,-0.0498,1.0000,0.0396 -8.750,-0.5795,0.04031,0.03611,-0.0838,1.0000,0.0375 -8.500,-0.5568,0.03333,0.02838,-0.0917,1.0000,0.0378 -8.250,-0.5288,0.02923,0.02368,-0.0957,1.0000,0.0390 -8.000,-0.4993,0.02732,0.02125,-0.0979,1.0000,0.0410 -7.750,-0.4731,0.02405,0.01780,-0.0999,1.0000,0.0436 -7.500,-0.4487,0.02268,0.01628,-0.1003,1.0000,0.0460 -7.250,-0.4270,0.02149,0.01491,-0.1000,1.0000,0.0486 -7.000,-0.4076,0.02057,0.01376,-0.0993,1.0000,0.0515 -6.750,-0.3886,0.01936,0.01259,-0.0989,1.0000,0.0552 -6.500,-0.3541,0.01842,0.01150,-0.1009,0.9975,0.0604 -6.250,-0.3126,0.01717,0.01021,-0.1044,0.9945,0.0684 -6.000,-0.2714,0.01611,0.00909,-0.1077,0.9904,0.0784 -5.750,-0.2293,0.01525,0.00824,-0.1111,0.9867,0.0934 -5.500,-0.1858,0.01443,0.00741,-0.1148,0.9840,0.1164 -5.250,-0.1449,0.01376,0.00684,-0.1180,0.9789,0.1472 -5.000,-0.1042,0.01339,0.00650,-0.1210,0.9736,0.1795 -4.750,-0.0651,0.01311,0.00623,-0.1235,0.9678,0.2076 -4.500,-0.0287,0.01294,0.00602,-0.1254,0.9598,0.2326 -4.250,0.0047,0.01282,0.00592,-0.1266,0.9511,0.2540 -4.000,0.0363,0.01279,0.00583,-0.1272,0.9424,0.2745 -3.750,0.0646,0.01276,0.00580,-0.1272,0.9315,0.2926 -3.500,0.0922,0.01275,0.00579,-0.1269,0.9217,0.3094 -3.250,0.1190,0.01275,0.00577,-0.1264,0.9127,0.3256 -3.000,0.1463,0.01274,0.00576,-0.1261,0.9025,0.3415 -2.750,0.1730,0.01273,0.00573,-0.1256,0.8937,0.3572 -2.500,0.2000,0.01271,0.00570,-0.1252,0.8844,0.3730 -2.250,0.2277,0.01270,0.00569,-0.1249,0.8757,0.3889 -2.000,0.2550,0.01269,0.00566,-0.1246,0.8679,0.4048 -1.750,0.2833,0.01269,0.00567,-0.1245,0.8597,0.4210 -1.500,0.3109,0.01268,0.00566,-0.1242,0.8525,0.4370 -1.250,0.3395,0.01269,0.00569,-0.1243,0.8447,0.4533 -1.000,0.3676,0.01268,0.00569,-0.1241,0.8379,0.4696 -0.750,0.3962,0.01269,0.00573,-0.1242,0.8305,0.4858 -0.500,0.4245,0.01268,0.00574,-0.1241,0.8234,0.5015 -0.250,0.4531,0.01268,0.00578,-0.1241,0.8165,0.5169 0.000,0.4818,0.01267,0.00581,-0.1242,0.8093,0.5327 0.250,0.5102,0.01268,0.00585,-0.1241,0.8028,0.5499 0.500,0.5389,0.01266,0.00592,-0.1242,0.7949,0.5680 0.750,0.5668,0.01264,0.00597,-0.1240,0.7886,0.5870 1.000,0.5957,0.01262,0.00607,-0.1242,0.7805,0.6088 1.250,0.6235,0.01258,0.00613,-0.1239,0.7747,0.6346 1.500,0.6522,0.01253,0.00630,-0.1241,0.7664,0.6704 1.750,0.6785,0.01237,0.00638,-0.1234,0.7602,0.7284 2.000,0.6943,0.01179,0.00627,-0.1201,0.7522,1.0000 2.250,0.7242,0.01194,0.00635,-0.1204,0.7456,1.0000 2.500,0.7540,0.01212,0.00654,-0.1208,0.7376,1.0000 2.750,0.7831,0.01227,0.00666,-0.1209,0.7307,1.0000 3.000,0.8123,0.01245,0.00689,-0.1212,0.7222,1.0000 3.250,0.8402,0.01249,0.00690,-0.1207,0.7108,1.0000 3.500,0.8668,0.01232,0.00668,-0.1198,0.6904,1.0000 3.750,0.8931,0.01216,0.00641,-0.1187,0.6684,1.0000 4.000,0.9206,0.01212,0.00640,-0.1182,0.6467,1.0000 4.250,0.9482,0.01216,0.00644,-0.1179,0.6274,1.0000 4.500,0.9756,0.01221,0.00650,-0.1174,0.6039,1.0000 4.750,1.0027,0.01230,0.00657,-0.1170,0.5730,1.0000 5.000,1.0286,0.01251,0.00666,-0.1163,0.5229,1.0000 5.250,1.0495,0.01349,0.00697,-0.1151,0.3914,1.0000 5.500,1.0562,0.01716,0.00886,-0.1133,0.1182,1.0000 5.750,1.0761,0.01864,0.01010,-0.1123,0.0847,1.0000 6.000,1.0974,0.01978,0.01120,-0.1114,0.0717,1.0000 6.250,1.1175,0.02100,0.01243,-0.1103,0.0641,1.0000 6.500,1.1376,0.02216,0.01356,-0.1091,0.0583,1.0000 6.750,1.1564,0.02354,0.01498,-0.1077,0.0538,1.0000 7.000,1.1774,0.02461,0.01610,-0.1066,0.0501,1.0000 7.250,1.1972,0.02596,0.01741,-0.1054,0.0472,1.0000 7.500,1.2174,0.02806,0.01951,-0.1041,0.0446,1.0000 7.750,1.2402,0.02909,0.02068,-0.1032,0.0422,1.0000 8.000,1.2631,0.03050,0.02220,-0.1023,0.0402,1.0000 8.250,1.2860,0.03209,0.02387,-0.1015,0.0386,1.0000 8.500,1.3094,0.03404,0.02586,-0.1009,0.0372,1.0000 8.750,1.3335,0.03781,0.02979,-0.1005,0.0356,1.0000 9.000,1.3517,0.03916,0.03147,-0.0989,0.0344,1.0000 9.250,1.3700,0.04176,0.03442,-0.0974,0.0337,1.0000 9.500,1.3853,0.04494,0.03798,-0.0956,0.0334,1.0000 9.750,1.3965,0.04867,0.04210,-0.0934,0.0333,1.0000 10.000,1.4024,0.05290,0.04674,-0.0908,0.0337,1.0000 10.250,1.4032,0.05723,0.05145,-0.0880,0.0340,1.0000 10.500,1.3992,0.06154,0.05611,-0.0849,0.0342,1.0000 10.750,1.3904,0.06568,0.06057,-0.0815,0.0343,1.0000 11.000,1.3765,0.06983,0.06499,-0.0780,0.0346,1.0000 11.250,1.3584,0.07406,0.06942,-0.0744,0.0349,1.0000 11.500,1.2536,0.07205,0.06754,-0.0588,0.0361,1.0000 11.750,1.2294,0.07485,0.07057,-0.0557,0.0364,1.0000