Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe382-il-100000-n5 Airfoil,goe382-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,39.7438 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe382-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.0596,0.09497,0.08944,-0.0953,0.8297,0.0552 -10.500,-0.0570,0.09156,0.08602,-0.0964,0.8184,0.0548 -10.000,-0.1467,0.06388,0.05810,-0.1168,0.8031,0.0503 -9.750,-0.1733,0.05774,0.05172,-0.1211,0.7928,0.0500 -9.500,-0.1983,0.05377,0.04753,-0.1212,0.7821,0.0498 -9.250,-0.2142,0.05022,0.04365,-0.1203,0.7737,0.0497 -9.000,-0.2223,0.04709,0.04018,-0.1191,0.7649,0.0496 -8.750,-0.2239,0.04426,0.03697,-0.1177,0.7571,0.0496 -8.500,-0.2199,0.04169,0.03398,-0.1162,0.7507,0.0498 -8.250,-0.2139,0.03943,0.03131,-0.1146,0.7425,0.0501 -8.000,-0.1993,0.03778,0.02938,-0.1136,0.7362,0.0507 -7.750,-0.1804,0.03668,0.02815,-0.1129,0.7298,0.0513 -7.500,-0.1626,0.03549,0.02679,-0.1119,0.7227,0.0519 -7.250,-0.1433,0.03415,0.02519,-0.1111,0.7169,0.0525 -7.000,-0.1235,0.03288,0.02365,-0.1102,0.7109,0.0529 -6.750,-0.1034,0.03172,0.02227,-0.1093,0.7042,0.0534 -6.500,-0.0809,0.03059,0.02088,-0.1086,0.6986,0.0539 -6.250,-0.0572,0.02956,0.01960,-0.1080,0.6935,0.0545 -6.000,-0.0351,0.02871,0.01858,-0.1072,0.6869,0.0551 -5.750,-0.0107,0.02793,0.01767,-0.1067,0.6813,0.0558 -5.500,0.0153,0.02725,0.01690,-0.1064,0.6767,0.0567 -5.250,0.0385,0.02676,0.01636,-0.1058,0.6709,0.0580 -5.000,0.0624,0.02625,0.01575,-0.1052,0.6650,0.0597 -4.750,0.0879,0.02571,0.01509,-0.1048,0.6601,0.0614 -4.500,0.1142,0.02518,0.01450,-0.1045,0.6558,0.0630 -4.250,0.1360,0.02482,0.01414,-0.1036,0.6497,0.0646 -4.000,0.1600,0.02443,0.01366,-0.1029,0.6442,0.0665 -3.750,0.1848,0.02396,0.01317,-0.1024,0.6395,0.0686 -3.500,0.2098,0.02359,0.01269,-0.1019,0.6351,0.0717 -3.250,0.2305,0.02329,0.01243,-0.1008,0.6290,0.0755 -3.000,0.2536,0.02292,0.01202,-0.1001,0.6237,0.0814 -2.750,0.2782,0.02242,0.01150,-0.0996,0.6193,0.0901 -2.500,0.3018,0.02199,0.01123,-0.0990,0.6148,0.1045 -2.250,0.3227,0.02183,0.01126,-0.0980,0.6086,0.1463 -2.000,0.3467,0.02159,0.01112,-0.0974,0.6033,0.1852 -1.750,0.3715,0.02116,0.01098,-0.0971,0.5990,0.2560 -1.500,0.3944,0.02092,0.01097,-0.0965,0.5941,0.3284 -1.250,0.4142,0.02073,0.01109,-0.0953,0.5880,0.3996 -1.000,0.4347,0.02031,0.01123,-0.0939,0.5829,0.5419 -0.750,0.4595,0.02010,0.01123,-0.0928,0.5787,0.6455 -0.500,0.4803,0.02015,0.01147,-0.0912,0.5733,0.7084 -0.250,0.5019,0.02028,0.01169,-0.0898,0.5674,0.7558 0.000,0.5289,0.02033,0.01174,-0.0892,0.5624,0.7980 0.250,0.5621,0.02035,0.01169,-0.0896,0.5583,0.8467 0.500,0.5911,0.02069,0.01208,-0.0898,0.5516,0.8915 0.750,0.6295,0.02091,0.01224,-0.0918,0.5458,0.9294 1.000,0.6777,0.02103,0.01219,-0.0957,0.5411,0.9593 1.250,0.7271,0.02132,0.01239,-0.1003,0.5350,0.9844 1.500,0.7717,0.02157,0.01255,-0.1043,0.5284,1.0000 1.750,0.7879,0.02167,0.01252,-0.1025,0.5240,1.0000 2.000,0.8064,0.02178,0.01249,-0.1010,0.5200,1.0000 2.250,0.8135,0.02218,0.01289,-0.0978,0.5140,1.0000 2.500,0.8284,0.02241,0.01304,-0.0958,0.5090,1.0000 2.750,0.8491,0.02252,0.01301,-0.0946,0.5048,1.0000 3.000,0.8643,0.02282,0.01325,-0.0927,0.5000,1.0000 3.250,0.8760,0.02324,0.01365,-0.0903,0.4944,1.0000 3.500,0.8951,0.02348,0.01381,-0.0890,0.4899,1.0000 3.750,0.9196,0.02362,0.01382,-0.0886,0.4863,1.0000 4.000,0.9323,0.02411,0.01430,-0.0864,0.4813,1.0000 4.250,0.9455,0.02458,0.01476,-0.0844,0.4761,1.0000 4.500,0.9661,0.02485,0.01495,-0.0834,0.4718,1.0000 4.750,0.9928,0.02498,0.01495,-0.0834,0.4683,1.0000 5.000,0.9995,0.02566,0.01566,-0.0805,0.4633,1.0000 5.250,1.0107,0.02626,0.01627,-0.0783,0.4587,1.0000 5.500,1.0305,0.02664,0.01660,-0.0773,0.4548,1.0000 5.750,1.0570,0.02682,0.01668,-0.0774,0.4515,1.0000 6.000,1.0677,0.02754,0.01742,-0.0753,0.4471,1.0000 6.250,1.0743,0.02846,0.01839,-0.0729,0.4421,1.0000 6.500,1.0920,0.02899,0.01890,-0.0719,0.4380,1.0000 6.750,1.1171,0.02927,0.01910,-0.0718,0.4349,1.0000 7.000,1.1426,0.02959,0.01935,-0.0718,0.4320,1.0000 7.250,1.1369,0.03120,0.02111,-0.0683,0.4269,1.0000 7.500,1.1460,0.03224,0.02218,-0.0666,0.4226,1.0000 7.750,1.1666,0.03272,0.02263,-0.0661,0.4191,1.0000 8.000,1.1958,0.03282,0.02266,-0.0665,0.4163,1.0000 8.250,1.1997,0.03421,0.02412,-0.0645,0.4123,1.0000 8.500,1.1892,0.03653,0.02658,-0.0614,0.4073,1.0000 8.750,1.1994,0.03773,0.02782,-0.0602,0.4036,1.0000 9.000,1.2223,0.03815,0.02822,-0.0601,0.4008,1.0000 9.250,1.2541,0.03803,0.02804,-0.0606,0.3984,1.0000 9.500,1.2213,0.04218,0.03240,-0.0566,0.3924,1.0000 9.750,1.1999,0.04599,0.03636,-0.0540,0.3865,1.0000 10.000,1.2200,0.04659,0.03695,-0.0537,0.3838,1.0000 10.250,1.2496,0.04644,0.03679,-0.0539,0.3819,1.0000 10.500,1.2853,0.04587,0.03617,-0.0545,0.3803,1.0000 10.750,1.1495,0.06102,0.05174,-0.0488,0.3653,1.0000 11.000,1.1826,0.06014,0.05085,-0.0488,0.3642,1.0000 11.250,1.2179,0.05911,0.04979,-0.0489,0.3632,1.0000 11.750,1.1188,0.07627,0.06724,-0.0467,0.3447,1.0000