Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe458-il-100000-n5 Airfoil,goe458-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,64.6226 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe458-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.750,-0.3081,0.10186,0.09750,-0.0309,1.0000,0.0357 -7.500,-0.3152,0.10044,0.09616,-0.0288,1.0000,0.0361 -7.250,-0.3230,0.09903,0.09482,-0.0267,0.9997,0.0368 -7.000,-0.3071,0.09535,0.09116,-0.0316,0.9932,0.0389 -6.750,-0.2873,0.09196,0.08779,-0.0416,0.9830,0.0415 -6.500,-0.2574,0.08808,0.08387,-0.0551,0.9731,0.0424 -6.250,-0.2417,0.08243,0.07825,-0.0572,0.9688,0.0432 -6.000,-0.2272,0.07846,0.07427,-0.0576,0.9627,0.0444 -5.750,-0.2042,0.07431,0.07006,-0.0617,0.9572,0.0458 -5.500,-0.1828,0.07060,0.06632,-0.0660,0.9497,0.0484 -5.250,-0.1272,0.06496,0.06045,-0.0853,0.9425,0.0550 -5.000,-0.1157,0.06055,0.05609,-0.0851,0.9352,0.0566 -4.750,-0.0830,0.05409,0.04947,-0.0899,0.9305,0.0307 -4.250,-0.0039,0.04113,0.03596,-0.1048,0.9184,0.0224 -4.000,0.0366,0.03563,0.03006,-0.1108,0.9150,0.0213 -3.750,0.0664,0.03129,0.02522,-0.1133,0.9068,0.0207 -3.500,0.1049,0.02710,0.02030,-0.1165,0.9027,0.0202 -3.250,0.1363,0.02435,0.01690,-0.1174,0.8962,0.0202 -3.000,0.1698,0.02216,0.01411,-0.1183,0.8907,0.0208 -2.750,0.2062,0.02072,0.01217,-0.1194,0.8867,0.0233 -2.500,0.2324,0.01923,0.01051,-0.1191,0.8784,0.0254 -2.250,0.2671,0.01812,0.00918,-0.1201,0.8739,0.0285 -2.000,0.2940,0.01740,0.00827,-0.1197,0.8652,0.0365 -1.750,0.3282,0.01621,0.00721,-0.1206,0.8603,0.0771 -1.500,0.3549,0.01606,0.00731,-0.1205,0.8512,0.2124 -1.250,0.3863,0.01590,0.00703,-0.1211,0.8448,0.2497 -1.000,0.4137,0.01569,0.00668,-0.1208,0.8361,0.2643 -0.750,0.4431,0.01548,0.00637,-0.1209,0.8282,0.2839 -0.500,0.4734,0.01524,0.00608,-0.1213,0.8206,0.3110 -0.250,0.5009,0.01502,0.00589,-0.1212,0.8115,0.3543 0.000,0.5302,0.01429,0.00571,-0.1215,0.8049,0.5277 0.500,0.5936,0.01358,0.00542,-0.1225,0.7875,1.0000 0.750,0.6212,0.01366,0.00536,-0.1223,0.7785,1.0000 1.000,0.6476,0.01378,0.00537,-0.1220,0.7692,1.0000 1.250,0.6769,0.01383,0.00532,-0.1221,0.7618,1.0000 1.500,0.7022,0.01399,0.00542,-0.1217,0.7517,1.0000 1.750,0.7291,0.01412,0.00550,-0.1214,0.7432,1.0000 2.000,0.7567,0.01424,0.00559,-0.1213,0.7350,1.0000 2.250,0.7823,0.01439,0.00574,-0.1208,0.7248,1.0000 2.500,0.8087,0.01450,0.00582,-0.1204,0.7140,1.0000 2.750,0.8349,0.01457,0.00588,-0.1198,0.7015,1.0000 3.000,0.8606,0.01466,0.00599,-0.1192,0.6875,1.0000 3.250,0.8858,0.01477,0.00610,-0.1184,0.6725,1.0000 3.500,0.9108,0.01490,0.00625,-0.1176,0.6571,1.0000 3.750,0.9359,0.01506,0.00650,-0.1169,0.6431,1.0000 4.000,0.9616,0.01526,0.00678,-0.1164,0.6319,1.0000 4.250,0.9869,0.01549,0.00712,-0.1158,0.6204,1.0000 4.500,1.0108,0.01571,0.00745,-0.1148,0.6039,1.0000 4.750,1.0275,0.01590,0.00753,-0.1121,0.5545,1.0000 5.000,1.0396,0.01636,0.00771,-0.1087,0.4705,1.0000 5.250,1.0396,0.01804,0.00825,-0.1038,0.2943,1.0000 5.500,1.0416,0.02025,0.00954,-0.1001,0.1630,1.0000 5.750,1.0404,0.02282,0.01121,-0.0959,0.0282,1.0000 6.000,1.0558,0.02389,0.01245,-0.0937,0.0221,1.0000 6.250,1.0695,0.02517,0.01397,-0.0913,0.0199,1.0000 6.500,1.0841,0.02630,0.01533,-0.0891,0.0187,1.0000 6.750,1.0970,0.02749,0.01681,-0.0867,0.0169,1.0000 7.000,1.1060,0.02883,0.01835,-0.0838,0.0154,1.0000 7.250,1.1121,0.03031,0.02000,-0.0806,0.0148,1.0000 7.500,1.1173,0.03191,0.02174,-0.0774,0.0145,1.0000 7.750,1.1235,0.03366,0.02359,-0.0744,0.0142,1.0000 8.000,1.1341,0.03555,0.02554,-0.0721,0.0139,1.0000 8.250,1.1545,0.03769,0.02770,-0.0709,0.0136,1.0000 8.750,1.2331,0.04548,0.03572,-0.0742,0.0115,1.0000 9.000,1.2589,0.04923,0.03975,-0.0740,0.0116,1.0000 9.250,1.2810,0.05341,0.04434,-0.0734,0.0119,1.0000 9.500,1.2904,0.05548,0.04674,-0.0709,0.0121,1.0000 9.750,1.2964,0.05736,0.04896,-0.0680,0.0124,1.0000 10.000,1.2980,0.05928,0.05128,-0.0645,0.0129,1.0000 10.250,1.2895,0.06138,0.05382,-0.0599,0.0135,1.0000 10.500,1.2798,0.06422,0.05708,-0.0560,0.0142,1.0000 10.750,1.2698,0.06750,0.06071,-0.0528,0.0148,1.0000 11.000,1.2581,0.07109,0.06460,-0.0503,0.0154,1.0000 11.250,1.2446,0.07496,0.06874,-0.0485,0.0159,1.0000 11.500,1.2294,0.07906,0.07309,-0.0473,0.0162,1.0000 11.750,1.2132,0.08350,0.07777,-0.0468,0.0165,1.0000 12.000,1.1960,0.08833,0.08283,-0.0471,0.0168,1.0000 12.250,1.1782,0.09356,0.08826,-0.0482,0.0170,1.0000 12.500,1.1604,0.09912,0.09402,-0.0502,0.0171,1.0000 12.750,1.1421,0.10522,0.10030,-0.0529,0.0171,1.0000 13.000,1.1239,0.11180,0.10705,-0.0565,0.0171,1.0000