GOE 365 AIRFOIL (goe365-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 365 AIRFOIL (goe365-il) Reynolds number: 500,000 Max Cl/Cd: 107.16 at α=2.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe365-il-500000.txt Download as CSV file: xf-goe365-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 365 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.250 -0.2042 0.09275 0.09056 -0.0587 0.9852 0.0227
-9.000 -0.1960 0.08663 0.08446 -0.0684 0.9741 0.0229
-8.750 -0.1847 0.08123 0.07905 -0.0744 0.9623 0.0230
-8.500 -0.1663 0.07760 0.07541 -0.0763 0.9549 0.0233
-8.250 -0.1411 0.07429 0.07209 -0.0800 0.9469 0.0236
-8.000 -0.1107 0.06991 0.06767 -0.0881 0.9374 0.0242
-7.750 -0.0789 0.06471 0.06239 -0.0991 0.9221 0.0251
-7.500 -0.0553 0.05910 0.05661 -0.1097 0.8986 0.0266
-7.250 -0.0563 0.05147 0.04852 -0.1177 0.8680 0.0275
-7.000 -0.0528 0.04764 0.04462 -0.1173 0.8540 0.0278
-6.750 -0.0420 0.04562 0.04252 -0.1167 0.8427 0.0281
-6.500 -0.0293 0.04381 0.04062 -0.1162 0.8332 0.0284
-6.250 -0.0165 0.04179 0.03851 -0.1157 0.8238 0.0290
-6.000 -0.0026 0.03959 0.03617 -0.1153 0.8155 0.0298
-5.750 0.0131 0.03635 0.03232 -0.1139 0.8070 0.0329
-5.500 0.0220 0.03215 0.02798 -0.1129 0.7996 0.0336
-5.250 0.0399 0.03054 0.02631 -0.1123 0.7924 0.0341
-5.000 0.0591 0.02915 0.02483 -0.1116 0.7864 0.0348
-4.750 0.0787 0.02769 0.02325 -0.1108 0.7806 0.0360
-4.500 0.1038 0.02755 0.02256 -0.1089 0.7754 0.0396
-4.250 0.1183 0.02364 0.01849 -0.1080 0.7708 0.0409
-4.000 0.1401 0.02248 0.01732 -0.1074 0.7656 0.0420
-3.750 0.1633 0.02153 0.01627 -0.1068 0.7610 0.0439
-3.500 0.1921 0.02265 0.01700 -0.1057 0.7564 0.0480
-3.250 0.2094 0.01911 0.01337 -0.1048 0.7518 0.0503
-3.000 0.2336 0.01826 0.01247 -0.1043 0.7471 0.0522
-2.750 0.2598 0.01790 0.01194 -0.1037 0.7427 0.0563
-2.500 0.2832 0.01669 0.01058 -0.1030 0.7383 0.0617
-2.250 0.3083 0.01608 0.00995 -0.1025 0.7332 0.0657
-2.000 0.3333 0.01541 0.00911 -0.1019 0.7286 0.0743
-1.750 0.3595 0.01479 0.00847 -0.1016 0.7239 0.0788
-1.500 0.3897 0.01287 0.00613 -0.0999 0.7188 0.0458
-1.250 0.4157 0.01228 0.00546 -0.0993 0.7126 0.0455
-1.000 0.4414 0.01172 0.00485 -0.0986 0.7061 0.0447
-0.750 0.4660 0.01126 0.00436 -0.0977 0.6986 0.0442
-0.500 0.4912 0.01093 0.00397 -0.0970 0.6917 0.0444
-0.250 0.5151 0.01061 0.00366 -0.0960 0.6830 0.0447
0.000 0.5396 0.01038 0.00338 -0.0951 0.6747 0.0453
0.250 0.5639 0.01017 0.00318 -0.0942 0.6659 0.0465
0.500 0.5890 0.01003 0.00301 -0.0935 0.6582 0.0475
0.750 0.6136 0.00987 0.00283 -0.0927 0.6492 0.0483
1.000 0.6380 0.00967 0.00262 -0.0919 0.6401 0.0501
1.250 0.6626 0.00958 0.00249 -0.0911 0.6305 0.0530
1.500 0.6874 0.00952 0.00241 -0.0903 0.6189 0.0570
1.750 0.7926 0.00754 0.00268 -0.1077 0.5995 1.0000
2.000 0.8129 0.00763 0.00267 -0.1061 0.5818 1.0000
2.250 0.8326 0.00777 0.00269 -0.1043 0.5625 1.0000
2.500 0.8511 0.00796 0.00274 -0.1024 0.5411 1.0000
2.750 0.8694 0.00818 0.00283 -0.1004 0.5185 1.0000
3.000 0.8878 0.00842 0.00294 -0.0985 0.4976 1.0000
3.250 0.9064 0.00867 0.00306 -0.0966 0.4789 1.0000
3.500 0.9256 0.00890 0.00320 -0.0949 0.4625 1.0000
4.250 0.9832 0.00963 0.00368 -0.0898 0.4150 1.0000
4.500 1.0023 0.00988 0.00385 -0.0881 0.3991 1.0000
4.750 1.0212 0.01014 0.00405 -0.0864 0.3826 1.0000
5.000 1.0398 0.01041 0.00424 -0.0847 0.3660 1.0000
5.250 1.0580 0.01070 0.00446 -0.0828 0.3485 1.0000
5.500 1.0754 0.01101 0.00469 -0.0809 0.3301 1.0000
5.750 1.0919 0.01137 0.00495 -0.0788 0.3109 1.0000
6.000 1.1074 0.01176 0.00523 -0.0766 0.2925 1.0000
6.250 1.1233 0.01213 0.00552 -0.0744 0.2757 1.0000
6.500 1.1374 0.01252 0.00584 -0.0719 0.2615 1.0000
6.750 1.1513 0.01289 0.00615 -0.0694 0.2494 1.0000
7.000 1.1664 0.01323 0.00647 -0.0671 0.2401 1.0000
7.250 1.1804 0.01364 0.00683 -0.0647 0.2319 1.0000
7.500 1.1971 0.01397 0.00717 -0.0629 0.2252 1.0000
7.750 1.2117 0.01440 0.00757 -0.0607 0.2194 1.0000
8.000 1.2286 0.01475 0.00794 -0.0590 0.2148 1.0000
8.250 1.2455 0.01512 0.00833 -0.0573 0.2105 1.0000
8.500 1.2602 0.01559 0.00879 -0.0553 0.2056 1.0000
8.750 1.2767 0.01600 0.00922 -0.0537 0.2007 1.0000
9.000 1.2936 0.01640 0.00964 -0.0522 0.1956 1.0000
9.250 1.3076 0.01695 0.01017 -0.0503 0.1906 1.0000
9.500 1.3240 0.01740 0.01068 -0.0488 0.1868 1.0000
9.750 1.3412 0.01783 0.01115 -0.0475 0.1824 1.0000
10.000 1.3556 0.01841 0.01173 -0.0459 0.1776 1.0000
10.250 1.3701 0.01901 0.01235 -0.0444 0.1731 1.0000
10.500 1.3872 0.01948 0.01289 -0.0432 0.1681 1.0000
10.750 1.4005 0.02018 0.01359 -0.0417 0.1626 1.0000
11.000 1.4159 0.02078 0.01424 -0.0404 0.1573 1.0000
11.250 1.4306 0.02145 0.01493 -0.0392 0.1509 1.0000
11.500 1.4437 0.02223 0.01574 -0.0378 0.1441 1.0000
11.750 1.4561 0.02309 0.01659 -0.0365 0.1343 1.0000
12.000 1.4656 0.02418 0.01761 -0.0350 0.1151 1.0000
12.250 1.4650 0.02602 0.01927 -0.0328 0.0930 1.0000
12.500 1.4668 0.02778 0.02099 -0.0309 0.0822 1.0000
12.750 1.4680 0.02964 0.02284 -0.0291 0.0701 1.0000
13.000 1.4553 0.03272 0.02568 -0.0266 0.0366 1.0000
13.250 1.4471 0.03558 0.02853 -0.0247 0.0275 1.0000
13.500 1.4461 0.03793 0.03096 -0.0234 0.0247 1.0000
13.750 1.4451 0.04035 0.03346 -0.0222 0.0228 1.0000
14.000 1.4472 0.04254 0.03577 -0.0214 0.0216 1.0000
14.250 1.4469 0.04504 0.03838 -0.0206 0.0206 1.0000
14.500 1.4437 0.04793 0.04136 -0.0200 0.0198 1.0000
14.750 1.4377 0.05124 0.04478 -0.0195 0.0191 1.0000
15.000 1.4283 0.05511 0.04878 -0.0193 0.0185 1.0000
15.250 1.4267 0.05820 0.05199 -0.0192 0.0180 1.0000
15.500 1.4227 0.06165 0.05556 -0.0194 0.0176 1.0000
15.750 1.4157 0.06564 0.05967 -0.0198 0.0171 1.0000
16.000 1.4077 0.06987 0.06401 -0.0205 0.0168 1.0000
16.250 1.3978 0.07450 0.06876 -0.0214 0.0165 1.0000
16.500 1.3865 0.07942 0.07380 -0.0225 0.0162 1.0000
16.750 1.3756 0.08442 0.07892 -0.0237 0.0161 1.0000
17.000 1.3608 0.09010 0.08472 -0.0253 0.0158 1.0000
17.250 1.3484 0.09549 0.09023 -0.0269 0.0158 1.0000
17.500 1.3337 0.10134 0.09618 -0.0288 0.0155 1.0000
17.750 1.3167 0.10768 0.10263 -0.0310 0.0153 1.0000
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