Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe494-il-1000000-n5 Airfoil,goe494-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,112.281 Max Cl/Cd alpha,1.5 Url,http://airfoiltools.com/polar/csv?polar=xf-goe494-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.2947,0.08724,0.08562,-0.0479,0.9857,0.0032 -8.000,-0.2842,0.08314,0.08153,-0.0514,0.9798,0.0033 -7.750,-0.2737,0.07795,0.07634,-0.0563,0.9724,0.0035 -7.500,-0.2531,0.07311,0.07150,-0.0634,0.9673,0.0037 -7.250,-0.2278,0.06798,0.06635,-0.0719,0.9613,0.0039 -7.000,-0.1967,0.06230,0.06063,-0.0823,0.9551,0.0042 -6.750,-0.1653,0.05492,0.05320,-0.0950,0.9438,0.0049 -6.500,-0.1294,0.04303,0.04116,-0.1145,0.9277,0.0055 -6.250,-0.0751,0.01140,0.00737,-0.1477,0.9126,0.0059 -5.750,-0.0204,0.00964,0.00524,-0.1482,0.9014,0.0081 -5.500,0.0072,0.00929,0.00480,-0.1482,0.8961,0.0100 -5.250,0.0349,0.01020,0.00588,-0.1479,0.8901,0.0117 -5.000,0.0623,0.00992,0.00551,-0.1479,0.8843,0.0144 -4.750,0.0898,0.01016,0.00573,-0.1477,0.8775,0.0171 -4.500,0.1171,0.01018,0.00567,-0.1475,0.8706,0.0195 -4.250,0.1444,0.01033,0.00577,-0.1474,0.8629,0.0214 -4.000,0.1716,0.01049,0.00588,-0.1472,0.8553,0.0224 -3.500,0.2258,0.01010,0.00525,-0.1470,0.8340,0.0244 -3.250,0.2525,0.00942,0.00446,-0.1471,0.8206,0.0260 -3.000,0.2793,0.00916,0.00410,-0.1469,0.8061,0.0270 -2.750,0.3062,0.00882,0.00364,-0.1467,0.7927,0.0273 -2.500,0.3331,0.00849,0.00318,-0.1465,0.7804,0.0274 -2.250,0.3601,0.00825,0.00286,-0.1464,0.7695,0.0279 -2.000,0.3871,0.00796,0.00247,-0.1462,0.7597,0.0276 -1.750,0.4146,0.00767,0.00210,-0.1461,0.7519,0.0270 -1.500,0.4419,0.00745,0.00180,-0.1460,0.7458,0.0265 -1.250,0.4696,0.00727,0.00158,-0.1459,0.7405,0.0261 -1.000,0.4972,0.00713,0.00140,-0.1459,0.7354,0.0257 -0.750,0.5247,0.00702,0.00126,-0.1458,0.7312,0.0254 -0.500,0.5524,0.00692,0.00114,-0.1457,0.7269,0.0252 -0.250,0.5799,0.00685,0.00104,-0.1456,0.7210,0.0250 0.000,0.6072,0.00679,0.00097,-0.1455,0.7144,0.0248 0.250,0.6346,0.00674,0.00090,-0.1454,0.7075,0.0247 0.500,0.6618,0.00671,0.00084,-0.1452,0.7005,0.0247 0.750,0.6889,0.00669,0.00080,-0.1450,0.6906,0.0249 1.000,0.7154,0.00672,0.00076,-0.1447,0.6739,0.0255 1.250,0.7419,0.00675,0.00074,-0.1443,0.6513,0.0286 1.500,0.7680,0.00684,0.00078,-0.1439,0.6249,0.0331 1.750,0.7920,0.00712,0.00087,-0.1431,0.5696,0.0423 2.000,0.8156,0.00729,0.00108,-0.1425,0.5136,0.1823 2.250,0.8393,0.00762,0.00131,-0.1419,0.4565,0.2424 2.500,0.8589,0.00844,0.00172,-0.1406,0.3298,0.3085 2.750,0.8798,0.00916,0.00216,-0.1397,0.2286,0.3766 3.000,0.9022,0.00960,0.00255,-0.1390,0.1552,0.4979 3.500,0.9450,0.00996,0.00334,-0.1369,0.0366,1.0000 3.750,0.9703,0.01023,0.00360,-0.1364,0.0271,1.0000 4.000,0.9953,0.01055,0.00387,-0.1359,0.0170,1.0000 4.250,1.0204,0.01085,0.00416,-0.1354,0.0115,1.0000 4.500,1.0454,0.01115,0.00446,-0.1349,0.0095,1.0000 4.750,1.0696,0.01156,0.00487,-0.1342,0.0071,1.0000 5.000,1.0944,0.01188,0.00524,-0.1336,0.0064,1.0000 5.250,1.1187,0.01225,0.00564,-0.1330,0.0057,1.0000 5.500,1.1426,0.01268,0.00608,-0.1323,0.0050,1.0000 5.750,1.1648,0.01334,0.00682,-0.1313,0.0044,1.0000 6.000,1.1884,0.01378,0.00730,-0.1305,0.0041,1.0000 6.250,1.2117,0.01424,0.00783,-0.1297,0.0037,1.0000 6.500,1.2347,0.01473,0.00836,-0.1289,0.0034,1.0000 6.750,1.2571,0.01528,0.00895,-0.1280,0.0031,1.0000 7.000,1.2788,0.01592,0.00964,-0.1270,0.0029,1.0000 7.250,1.2971,0.01704,0.01088,-0.1254,0.0026,1.0000 7.500,1.3177,0.01785,0.01178,-0.1242,0.0026,1.0000 7.750,1.3380,0.01868,0.01271,-0.1230,0.0024,1.0000 8.000,1.3574,0.01968,0.01384,-0.1216,0.0023,1.0000 8.250,1.3761,0.02086,0.01519,-0.1201,0.0022,1.0000 8.500,1.3942,0.02221,0.01670,-0.1185,0.0020,1.0000 8.750,1.4119,0.02374,0.01842,-0.1169,0.0019,1.0000 9.000,1.4286,0.02555,0.02044,-0.1152,0.0018,1.0000 9.250,1.4438,0.02780,0.02296,-0.1133,0.0018,1.0000 9.500,1.4579,0.03005,0.02547,-0.1114,0.0017,1.0000 9.750,1.4717,0.03190,0.02753,-0.1095,0.0016,1.0000 10.000,1.4841,0.03367,0.02949,-0.1075,0.0016,1.0000 10.250,1.4929,0.03595,0.03200,-0.1050,0.0015,1.0000 10.500,1.4854,0.04151,0.03806,-0.1006,0.0015,1.0000 10.750,1.4117,0.05654,0.05395,-0.0887,0.0014,1.0000 11.000,1.3854,0.06128,0.05892,-0.0841,0.0014,1.0000 11.250,1.3583,0.06653,0.06438,-0.0811,0.0014,1.0000 11.500,1.3335,0.07200,0.07004,-0.0797,0.0014,1.0000 11.750,1.3084,0.07818,0.07638,-0.0799,0.0014,1.0000 12.000,1.2825,0.08527,0.08362,-0.0818,0.0015,1.0000 12.250,1.2515,0.09449,0.09301,-0.0859,0.0015,1.0000 12.500,1.2088,0.10944,0.10815,-0.0954,0.0015,1.0000