Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rae5213-il-100000-n5 Airfoil,rae5213-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,35.9473 Max Cl/Cd alpha,3 Url,http://airfoiltools.com/polar/csv?polar=xf-rae5213-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.5392,0.08990,0.08433,-0.0285,1.0000,0.0311 -9.750,-0.5412,0.08497,0.07944,-0.0310,1.0000,0.0309 -9.500,-0.5474,0.07872,0.07322,-0.0350,1.0000,0.0305 -9.250,-0.5604,0.07194,0.06644,-0.0401,1.0000,0.0300 -9.000,-0.5817,0.06584,0.06030,-0.0442,1.0000,0.0296 -8.750,-0.6014,0.06107,0.05542,-0.0462,1.0000,0.0293 -8.500,-0.6141,0.05632,0.05047,-0.0472,1.0000,0.0290 -8.250,-0.6210,0.05182,0.04571,-0.0474,1.0000,0.0288 -8.000,-0.6222,0.04770,0.04127,-0.0470,1.0000,0.0287 -7.750,-0.6188,0.04391,0.03713,-0.0462,1.0000,0.0289 -7.500,-0.6108,0.04069,0.03356,-0.0453,1.0000,0.0295 -7.250,-0.6007,0.03742,0.02980,-0.0443,1.0000,0.0305 -7.000,-0.5876,0.03453,0.02644,-0.0431,1.0000,0.0315 -6.750,-0.5704,0.03286,0.02464,-0.0422,1.0000,0.0323 -6.500,-0.5529,0.03086,0.02238,-0.0410,1.0000,0.0329 -6.250,-0.5343,0.02894,0.02018,-0.0398,1.0000,0.0337 -6.000,-0.5149,0.02715,0.01806,-0.0386,1.0000,0.0350 -5.750,-0.4951,0.02581,0.01655,-0.0374,1.0000,0.0367 -5.500,-0.4751,0.02476,0.01546,-0.0363,1.0000,0.0384 -5.250,-0.4546,0.02354,0.01408,-0.0351,1.0000,0.0399 -5.000,-0.4340,0.02243,0.01284,-0.0338,1.0000,0.0414 -4.750,-0.4141,0.02164,0.01210,-0.0327,1.0000,0.0436 -4.500,-0.3936,0.02085,0.01124,-0.0315,1.0000,0.0462 -4.250,-0.3735,0.02003,0.01044,-0.0303,1.0000,0.0481 -4.000,-0.3446,0.01934,0.00977,-0.0309,0.9969,0.0518 -3.750,-0.3104,0.01859,0.00903,-0.0325,0.9915,0.0558 -3.500,-0.2753,0.01794,0.00837,-0.0343,0.9860,0.0607 -3.250,-0.2414,0.01734,0.00777,-0.0359,0.9799,0.0692 -3.000,-0.2054,0.01670,0.00720,-0.0378,0.9746,0.0841 -2.750,-0.1732,0.01579,0.00666,-0.0393,0.9676,0.1426 -2.500,-0.1435,0.01403,0.00652,-0.0410,0.9626,0.4776 -2.250,-0.1146,0.01415,0.00695,-0.0407,0.9543,0.5977 -2.000,-0.0813,0.01455,0.00747,-0.0407,0.9487,0.6624 -1.750,-0.0556,0.01484,0.00783,-0.0392,0.9397,0.7011 -1.500,-0.0203,0.01490,0.00785,-0.0401,0.9345,0.7197 -1.250,0.0108,0.01483,0.00768,-0.0408,0.9255,0.7279 -1.000,0.0466,0.01474,0.00755,-0.0421,0.9194,0.7340 -0.750,0.0777,0.01467,0.00743,-0.0426,0.9100,0.7412 -0.500,0.1135,0.01457,0.00729,-0.0439,0.9031,0.7477 -0.250,0.1437,0.01451,0.00722,-0.0442,0.8936,0.7540 0.000,0.1786,0.01443,0.00710,-0.0454,0.8860,0.7610 0.250,0.2077,0.01436,0.00706,-0.0453,0.8758,0.7669 0.500,0.2417,0.01425,0.00695,-0.0461,0.8669,0.7733 0.750,0.2712,0.01414,0.00685,-0.0460,0.8522,0.7801 1.000,0.3016,0.01390,0.00661,-0.0455,0.8322,0.7859 1.250,0.3296,0.01365,0.00631,-0.0444,0.8013,0.7927 1.500,0.3571,0.01345,0.00602,-0.0432,0.7656,0.7992 1.750,0.3838,0.01335,0.00586,-0.0421,0.7337,0.8062 2.000,0.4109,0.01333,0.00579,-0.0414,0.7046,0.8139 2.250,0.4362,0.01333,0.00576,-0.0403,0.6697,0.8212 2.500,0.4615,0.01339,0.00573,-0.0392,0.6239,0.8304 2.750,0.4846,0.01353,0.00566,-0.0376,0.5538,0.8390 3.000,0.5047,0.01404,0.00564,-0.0357,0.4405,0.8495 3.250,0.5217,0.01498,0.00590,-0.0338,0.3036,0.8621 3.500,0.5410,0.01586,0.00629,-0.0325,0.2151,0.8778 4.000,0.5933,0.01699,0.00714,-0.0323,0.1565,0.9328 4.250,0.6230,0.01758,0.00765,-0.0331,0.1431,1.0000 4.500,0.6486,0.01820,0.00819,-0.0330,0.1331,1.0000 4.750,0.6740,0.01882,0.00876,-0.0329,0.1251,1.0000 5.000,0.6987,0.01949,0.00937,-0.0326,0.1180,1.0000 5.250,0.7237,0.02018,0.01005,-0.0323,0.1118,1.0000 5.500,0.7485,0.02088,0.01069,-0.0320,0.1056,1.0000 5.750,0.7730,0.02168,0.01147,-0.0316,0.1002,1.0000 6.000,0.7978,0.02239,0.01219,-0.0313,0.0942,1.0000 6.250,0.8218,0.02326,0.01298,-0.0309,0.0893,1.0000 6.500,0.8466,0.02402,0.01384,-0.0306,0.0839,1.0000 6.750,0.8703,0.02487,0.01462,-0.0302,0.0797,1.0000 7.000,0.8948,0.02578,0.01569,-0.0297,0.0751,1.0000 7.250,0.9183,0.02662,0.01653,-0.0293,0.0713,1.0000 7.500,0.9418,0.02767,0.01767,-0.0288,0.0679,1.0000 7.750,0.9650,0.02872,0.01885,-0.0283,0.0644,1.0000 8.000,0.9873,0.02959,0.01969,-0.0278,0.0620,1.0000 8.250,1.0095,0.03100,0.02136,-0.0271,0.0590,1.0000 8.500,1.0311,0.03233,0.02283,-0.0264,0.0568,1.0000 8.750,1.0521,0.03347,0.02402,-0.0258,0.0552,1.0000 9.000,1.0718,0.03511,0.02585,-0.0250,0.0535,1.0000 9.250,1.0890,0.03709,0.02817,-0.0240,0.0515,1.0000 9.500,1.1061,0.03862,0.02988,-0.0230,0.0499,1.0000 9.750,1.1233,0.03997,0.03133,-0.0221,0.0487,1.0000 10.000,1.1391,0.04168,0.03313,-0.0212,0.0479,1.0000 10.250,1.1438,0.04507,0.03707,-0.0193,0.0470,1.0000 10.500,1.1448,0.04848,0.04092,-0.0174,0.0462,1.0000 10.750,1.1412,0.05193,0.04475,-0.0153,0.0456,1.0000 11.000,1.1319,0.05533,0.04847,-0.0130,0.0451,1.0000 11.250,1.1166,0.05877,0.05219,-0.0106,0.0447,1.0000 11.500,1.0952,0.06294,0.05662,-0.0092,0.0445,1.0000 11.750,1.0651,0.06858,0.06254,-0.0097,0.0445,1.0000 12.000,1.0142,0.07841,0.07268,-0.0146,0.0449,1.0000