Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe682-il-50000 Airfoil,goe682-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,25.4484 Max Cl/Cd alpha,8 Url,http://airfoiltools.com/polar/csv?polar=xf-goe682-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.3056,0.11101,0.10395,-0.0302,1.0000,0.2135 -8.750,-0.3022,0.10857,0.10156,-0.0293,1.0000,0.2217 -8.500,-0.3305,0.10982,0.10303,-0.0293,1.0000,0.2256 -8.250,-0.3018,0.10354,0.09669,-0.0276,1.0000,0.2327 -8.000,-0.3142,0.10272,0.09601,-0.0265,1.0000,0.2399 -7.750,-0.3532,0.10447,0.09802,-0.0242,1.0000,0.2419 -7.500,-0.3135,0.09756,0.09102,-0.0231,1.0000,0.2514 -7.250,-0.3436,0.09811,0.09177,-0.0201,1.0000,0.2569 -7.000,-0.3411,0.09497,0.08870,-0.0179,1.0000,0.2620 -6.750,-0.3493,0.09355,0.08738,-0.0148,1.0000,0.2701 -6.500,-0.3889,0.09448,0.08852,-0.0120,1.0000,0.2737 -6.250,-0.3727,0.09048,0.08454,-0.0086,1.0000,0.2832 -6.000,-0.4053,0.09069,0.08491,-0.0075,1.0000,0.2897 -5.750,-0.3950,0.08728,0.08154,-0.0036,1.0000,0.2994 -5.500,-0.4209,0.08656,0.08096,-0.0036,1.0000,0.3077 -5.250,-0.4165,0.08402,0.07845,0.0000,1.0000,0.3196 -5.000,-0.4200,0.08164,0.07613,0.0023,1.0000,0.3290 -4.750,-0.4286,0.07974,0.07429,0.0031,1.0000,0.3420 -4.500,-0.4328,0.07769,0.07229,0.0044,1.0000,0.3572 -4.250,-0.4337,0.07546,0.07010,0.0065,1.0000,0.3735 -4.000,-0.4329,0.07316,0.06786,0.0092,1.0000,0.3911 -3.750,-0.4316,0.07101,0.06575,0.0121,1.0000,0.4110 -3.500,-0.4331,0.06902,0.06381,0.0153,1.0000,0.4398 -3.250,-0.4341,0.06713,0.06199,0.0203,1.0000,0.4733 -3.000,-0.4366,0.06555,0.06048,0.0260,1.0000,0.5140 -2.750,-0.4387,0.06365,0.05866,0.0337,1.0000,0.5571 -2.500,-0.4432,0.06184,0.05693,0.0402,1.0000,0.6009 -2.250,-0.2142,0.04094,0.03201,-0.0429,1.0000,0.1775 -2.000,-0.1939,0.03931,0.03022,-0.0430,1.0000,0.1792 -1.750,-0.1718,0.03787,0.02846,-0.0432,1.0000,0.1798 -1.500,-0.1280,0.03683,0.02710,-0.0470,0.9912,0.1841 -1.250,-0.0814,0.03614,0.02591,-0.0511,0.9807,0.1950 -1.000,-0.0349,0.03565,0.02519,-0.0550,0.9699,0.2072 -0.750,0.0032,0.03527,0.02464,-0.0575,0.9584,0.2271 -0.500,0.0405,0.03493,0.02430,-0.0596,0.9470,0.2535 -0.250,0.0844,0.03450,0.02397,-0.0627,0.9360,0.3119 0.000,0.1299,0.03267,0.02356,-0.0657,0.9271,0.5348 0.250,0.1738,0.03199,0.02335,-0.0685,0.9144,1.0000 0.500,0.2075,0.03287,0.02381,-0.0703,0.9015,1.0000 0.750,0.2419,0.03377,0.02441,-0.0722,0.8889,1.0000 1.000,0.2797,0.03468,0.02505,-0.0746,0.8767,1.0000 1.250,0.3143,0.03554,0.02570,-0.0764,0.8641,1.0000 1.500,0.3392,0.03640,0.02641,-0.0768,0.8508,1.0000 1.750,0.3658,0.03730,0.02718,-0.0774,0.8377,1.0000 2.000,0.3949,0.03818,0.02795,-0.0782,0.8246,1.0000 2.250,0.4271,0.03902,0.02868,-0.0794,0.8117,1.0000 2.500,0.4637,0.03972,0.02929,-0.0809,0.7984,1.0000 2.750,0.5020,0.04022,0.02973,-0.0823,0.7840,1.0000 3.000,0.5373,0.04061,0.03007,-0.0831,0.7685,1.0000 3.250,0.5720,0.04089,0.03033,-0.0836,0.7527,1.0000 3.500,0.6058,0.04114,0.03057,-0.0839,0.7373,1.0000 3.750,0.6359,0.04149,0.03091,-0.0838,0.7220,1.0000 4.000,0.6652,0.04183,0.03128,-0.0835,0.7069,1.0000 4.250,0.6945,0.04214,0.03161,-0.0831,0.6917,1.0000 4.500,0.7239,0.04240,0.03191,-0.0826,0.6766,1.0000 4.750,0.7560,0.04242,0.03199,-0.0822,0.6614,1.0000 5.000,0.7882,0.04241,0.03204,-0.0817,0.6462,1.0000 5.250,0.8226,0.04222,0.03192,-0.0813,0.6308,1.0000 5.500,0.8567,0.04193,0.03172,-0.0807,0.6153,1.0000 5.750,0.8896,0.04171,0.03158,-0.0799,0.5997,1.0000 6.000,0.9237,0.04136,0.03133,-0.0792,0.5839,1.0000 6.250,0.9565,0.04112,0.03116,-0.0784,0.5680,1.0000 6.500,0.9855,0.04123,0.03135,-0.0774,0.5525,1.0000 6.750,1.0129,0.04147,0.03169,-0.0764,0.5370,1.0000 7.000,1.0361,0.04206,0.03236,-0.0751,0.5220,1.0000 7.250,1.0527,0.04325,0.03363,-0.0735,0.5080,1.0000 7.500,1.0680,0.04465,0.03512,-0.0719,0.4952,1.0000 7.750,1.1028,0.04465,0.03523,-0.0717,0.4835,1.0000 8.000,1.1378,0.04471,0.03538,-0.0715,0.4721,1.0000 8.250,1.0912,0.05087,0.04166,-0.0664,0.4610,1.0000 8.500,1.0933,0.05355,0.04442,-0.0645,0.4516,1.0000 8.750,1.1605,0.05114,0.04221,-0.0658,0.4410,1.0000 9.000,0.9311,0.07775,0.06833,-0.0636,0.4344,1.0000 9.250,0.9328,0.08150,0.07216,-0.0636,0.4275,1.0000 9.500,0.9253,0.08649,0.07718,-0.0640,0.4220,1.0000 9.750,0.8943,0.09397,0.08465,-0.0656,0.4185,1.0000 10.000,0.9287,0.09409,0.08496,-0.0642,0.4077,1.0000 10.250,0.8976,0.10170,0.09253,-0.0662,0.4055,1.0000 10.500,0.8818,0.10742,0.09828,-0.0675,0.4018,1.0000