Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe513-il-100000 Airfoil,goe513-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,44.498 Max Cl/Cd alpha,3 Url,http://airfoiltools.com/polar/csv?polar=xf-goe513-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.500,-0.2831,0.09759,0.09343,-0.0396,0.9649,0.1766 -7.250,-0.3261,0.09526,0.09110,-0.0439,0.9527,0.1842 -7.000,-0.3447,0.09130,0.08712,-0.0448,0.9404,0.1866 -6.750,-0.3078,0.08733,0.08316,-0.0459,0.9350,0.1890 -6.500,-0.4781,0.05724,0.05152,-0.0429,0.9156,0.1018 -6.250,-0.4554,0.05362,0.04774,-0.0433,0.9079,0.0990 -6.000,-0.4513,0.04973,0.04351,-0.0405,0.8970,0.0963 -5.750,-0.4380,0.04472,0.03773,-0.0389,0.8901,0.0937 -5.500,-0.4281,0.04228,0.03485,-0.0358,0.8779,0.0937 -5.250,-0.3910,0.03960,0.03166,-0.0372,0.8727,0.0940 -5.000,-0.3739,0.03787,0.02959,-0.0349,0.8596,0.0941 -4.750,-0.3461,0.03624,0.02765,-0.0344,0.8489,0.0946 -4.500,-0.3039,0.03448,0.02563,-0.0362,0.8418,0.0959 -4.250,-0.2744,0.03330,0.02426,-0.0359,0.8301,0.0976 -4.000,-0.2259,0.03181,0.02250,-0.0387,0.8243,0.1013 -3.750,-0.1948,0.03056,0.02137,-0.0389,0.8123,0.1046 -3.500,-0.1440,0.02903,0.01982,-0.0422,0.8072,0.1098 -3.250,-0.1132,0.02803,0.01881,-0.0420,0.7957,0.1150 -3.000,-0.0656,0.02653,0.01739,-0.0446,0.7906,0.1274 -2.750,-0.0100,0.02483,0.01614,-0.0486,0.7879,0.1690 -2.500,0.0035,0.02498,0.01644,-0.0447,0.7735,0.2405 -2.250,0.0254,0.02516,0.01651,-0.0423,0.7634,0.2810 -2.000,0.0626,0.02484,0.01603,-0.0430,0.7550,0.3086 -1.750,0.1273,0.02395,0.01510,-0.0493,0.7511,0.3380 -1.500,0.1485,0.02376,0.01488,-0.0476,0.7366,0.3559 -1.250,0.1846,0.02332,0.01439,-0.0488,0.7257,0.3792 -1.000,0.2347,0.02261,0.01356,-0.0527,0.7160,0.4012 -0.750,0.2664,0.02225,0.01320,-0.0533,0.7028,0.4109 -0.500,0.3212,0.02170,0.01244,-0.0582,0.6926,0.4206 -0.250,0.3606,0.02133,0.01209,-0.0604,0.6793,0.4285 0.000,0.3943,0.02117,0.01189,-0.0615,0.6662,0.4387 0.250,0.4511,0.02070,0.01140,-0.0671,0.6532,0.4529 0.500,0.4991,0.02030,0.01099,-0.0710,0.6406,0.4691 0.750,0.5202,0.02019,0.01098,-0.0696,0.6282,0.4876 1.000,0.7259,0.02037,0.01219,-0.1031,0.6059,0.9512 1.250,0.8768,0.02048,0.01180,-0.1274,0.5857,1.0000 1.500,0.8925,0.02078,0.01202,-0.1251,0.5745,1.0000 1.750,0.9152,0.02105,0.01210,-0.1242,0.5648,1.0000 2.000,0.9345,0.02134,0.01227,-0.1226,0.5541,1.0000 2.250,0.9534,0.02170,0.01252,-0.1210,0.5440,1.0000 2.500,0.9758,0.02203,0.01267,-0.1200,0.5339,1.0000 2.750,0.9906,0.02246,0.01306,-0.1176,0.5237,1.0000 3.000,1.0150,0.02281,0.01322,-0.1171,0.5139,1.0000 3.250,1.0259,0.02329,0.01373,-0.1140,0.5041,1.0000 3.500,1.0500,0.02367,0.01393,-0.1134,0.4948,1.0000 3.750,1.0591,0.02417,0.01449,-0.1100,0.4852,1.0000 4.000,1.0811,0.02454,0.01471,-0.1090,0.4761,1.0000 4.250,1.0900,0.02505,0.01527,-0.1056,0.4668,1.0000 4.500,1.1092,0.02539,0.01549,-0.1040,0.4578,1.0000 4.750,1.1191,0.02589,0.01603,-0.1008,0.4489,1.0000 5.000,1.1346,0.02624,0.01632,-0.0985,0.4404,1.0000 5.250,1.1491,0.02672,0.01677,-0.0962,0.4325,1.0000 5.500,1.1586,0.02718,0.01725,-0.0929,0.4244,1.0000 5.750,1.1852,0.02752,0.01741,-0.0928,0.4177,1.0000 6.000,1.1844,0.02819,0.01824,-0.0877,0.4100,1.0000 6.250,1.2035,0.02852,0.01849,-0.0862,0.4034,1.0000 6.500,1.2169,0.02910,0.01905,-0.0837,0.3970,1.0000 6.750,1.2222,0.02970,0.01974,-0.0798,0.3904,1.0000 7.000,1.2460,0.03000,0.01992,-0.0792,0.3847,1.0000 7.250,1.2558,0.03074,0.02071,-0.0762,0.3795,1.0000 7.500,1.2591,0.03154,0.02161,-0.0721,0.3741,1.0000 7.750,1.2768,0.03203,0.02208,-0.0705,0.3693,1.0000 8.000,1.3089,0.03251,0.02240,-0.0715,0.3649,1.0000 8.250,1.2983,0.03362,0.02375,-0.0651,0.3604,1.0000 8.500,1.3017,0.03445,0.02466,-0.0611,0.3559,1.0000 8.750,1.3210,0.03495,0.02514,-0.0599,0.3517,1.0000 9.000,1.3566,0.03548,0.02553,-0.0617,0.3478,1.0000 9.250,1.3386,0.03686,0.02716,-0.0542,0.3445,1.0000 9.500,1.3266,0.03805,0.02851,-0.0480,0.3412,1.0000 9.750,1.3258,0.03906,0.02960,-0.0436,0.3380,1.0000 10.000,1.3438,0.03972,0.03026,-0.0424,0.3346,1.0000 10.250,1.3925,0.04028,0.03069,-0.0464,0.3309,1.0000 10.500,1.3505,0.04204,0.03270,-0.0357,0.3286,1.0000 10.750,1.3134,0.04433,0.03523,-0.0270,0.3259,1.0000 11.000,1.2816,0.04702,0.03811,-0.0201,0.3232,1.0000 11.250,1.2636,0.04947,0.04069,-0.0154,0.3204,1.0000 11.500,1.2674,0.05107,0.04235,-0.0132,0.3179,1.0000 11.750,1.3270,0.05021,0.04138,-0.0166,0.3152,1.0000 12.000,0.6121,0.14373,0.13593,-0.0215,0.3508,1.0000 12.250,0.6389,0.14651,0.13873,-0.0214,0.3492,1.0000