Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe391-il-100000-n5 Airfoil,goe391-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,58.3511 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-goe391-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.750,-0.4075,0.09516,0.09027,-0.0229,1.0000,0.0267 -7.500,-0.4102,0.09287,0.08805,-0.0223,1.0000,0.0268 -7.250,-0.4133,0.09038,0.08564,-0.0218,1.0000,0.0274 -7.000,-0.4132,0.08769,0.08302,-0.0221,1.0000,0.0277 -6.750,-0.4123,0.08498,0.08035,-0.0226,1.0000,0.0280 -6.500,-0.4104,0.08220,0.07761,-0.0232,1.0000,0.0284 -6.250,-0.4070,0.07939,0.07483,-0.0239,1.0000,0.0287 -6.000,-0.4023,0.07641,0.07186,-0.0248,1.0000,0.0292 -5.750,-0.3958,0.07334,0.06879,-0.0258,1.0000,0.0296 -5.500,-0.3866,0.07020,0.06564,-0.0273,1.0000,0.0312 -5.250,-0.3664,0.06732,0.06262,-0.0317,1.0000,0.0337 -5.000,-0.3461,0.06438,0.05951,-0.0345,1.0000,0.0342 -4.750,-0.3276,0.06128,0.05621,-0.0360,1.0000,0.0344 -4.500,-0.3145,0.05714,0.05201,-0.0363,1.0000,0.0348 -4.250,-0.3065,0.05306,0.04794,-0.0356,1.0000,0.0356 -4.000,-0.2926,0.04975,0.04457,-0.0354,1.0000,0.0367 -3.750,-0.2734,0.04659,0.04125,-0.0359,1.0000,0.0373 -3.500,-0.2445,0.04257,0.03697,-0.0377,0.9984,0.0295 -3.250,-0.1971,0.03752,0.03123,-0.0410,0.9952,0.0244 -3.000,-0.1693,0.03464,0.02824,-0.0435,0.9912,0.0270 -2.750,-0.1334,0.03186,0.02508,-0.0456,0.9878,0.0301 -2.500,-0.0989,0.02884,0.02156,-0.0469,0.9841,0.0298 -2.250,-0.0638,0.02611,0.01827,-0.0479,0.9808,0.0306 -2.000,-0.0270,0.02404,0.01550,-0.0489,0.9780,0.0351 -1.750,0.0033,0.02221,0.01341,-0.0496,0.9738,0.0378 -1.500,0.0370,0.02108,0.01189,-0.0504,0.9700,0.0439 -1.250,0.0717,0.01965,0.01018,-0.0517,0.9673,0.0482 -1.000,0.1007,0.01892,0.00933,-0.0520,0.9619,0.0540 -0.750,0.1339,0.01829,0.00852,-0.0530,0.9576,0.0579 -0.500,0.1671,0.01763,0.00778,-0.0541,0.9537,0.0585 -0.250,0.1951,0.01710,0.00721,-0.0542,0.9475,0.0597 0.000,0.2294,0.01671,0.00676,-0.0555,0.9430,0.0624 0.250,0.2602,0.01648,0.00645,-0.0562,0.9367,0.0679 0.500,0.2957,0.01621,0.00614,-0.0577,0.9303,0.0827 0.750,0.3499,0.01392,0.00607,-0.0634,0.9293,1.0000 1.000,0.3823,0.01391,0.00593,-0.0642,0.9197,1.0000 1.250,0.4212,0.01385,0.00578,-0.0664,0.9126,1.0000 1.500,0.4542,0.01379,0.00569,-0.0672,0.9027,1.0000 1.750,0.4864,0.01374,0.00564,-0.0679,0.8923,1.0000 2.000,0.5204,0.01360,0.00552,-0.0688,0.8805,1.0000 2.250,0.5531,0.01346,0.00542,-0.0694,0.8675,1.0000 2.500,0.5842,0.01334,0.00535,-0.0696,0.8530,1.0000 2.750,0.6150,0.01322,0.00534,-0.0697,0.8366,1.0000 3.000,0.6468,0.01310,0.00530,-0.0700,0.8191,1.0000 3.250,0.6763,0.01296,0.00525,-0.0696,0.7917,1.0000 3.500,0.7060,0.01279,0.00511,-0.0690,0.7442,1.0000 3.750,0.7373,0.01276,0.00496,-0.0687,0.6793,1.0000 4.000,0.7644,0.01310,0.00493,-0.0677,0.5910,1.0000 4.250,0.7815,0.01394,0.00516,-0.0652,0.4637,1.0000 4.500,0.7958,0.01504,0.00563,-0.0627,0.3428,1.0000 4.750,0.8136,0.01599,0.00623,-0.0610,0.2600,1.0000 5.000,0.8303,0.01716,0.00691,-0.0593,0.1624,1.0000 5.250,0.8477,0.01839,0.00777,-0.0577,0.0901,1.0000 5.500,0.8666,0.01946,0.00877,-0.0561,0.0715,1.0000 5.750,0.8864,0.02038,0.00990,-0.0546,0.0649,1.0000 6.000,0.9052,0.02142,0.01107,-0.0530,0.0576,1.0000 6.250,0.9242,0.02243,0.01221,-0.0515,0.0485,1.0000 6.500,0.9408,0.02390,0.01378,-0.0497,0.0410,1.0000 6.750,0.9564,0.02580,0.01564,-0.0480,0.0337,1.0000 7.000,0.9774,0.02736,0.01751,-0.0465,0.0283,1.0000 7.250,0.9961,0.02950,0.01976,-0.0453,0.0241,1.0000 7.500,1.0183,0.03212,0.02272,-0.0441,0.0221,1.0000 7.750,1.0387,0.03448,0.02557,-0.0425,0.0192,1.0000 8.000,1.0559,0.03724,0.02878,-0.0407,0.0175,1.0000 8.250,1.0692,0.04051,0.03253,-0.0385,0.0166,1.0000 8.500,1.0784,0.04396,0.03647,-0.0360,0.0161,1.0000 8.750,1.0832,0.04763,0.04060,-0.0332,0.0157,1.0000 9.000,1.0842,0.05129,0.04469,-0.0304,0.0155,1.0000 9.250,1.0824,0.05462,0.04835,-0.0276,0.0149,1.0000 9.500,1.0760,0.05820,0.05226,-0.0248,0.0148,1.0000 9.750,1.0669,0.06112,0.05538,-0.0219,0.0143,1.0000 10.000,1.0531,0.06415,0.05857,-0.0191,0.0138,1.0000 10.250,1.0332,0.06859,0.06332,-0.0168,0.0144,1.0000 10.500,1.0151,0.07280,0.06771,-0.0163,0.0144,1.0000 10.750,0.9833,0.08069,0.07588,-0.0188,0.0155,1.0000 11.000,0.9574,0.08943,0.08475,-0.0243,0.0164,1.0000