GOE 528 AIRFOIL (goe528-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 528 AIRFOIL (goe528-il) Reynolds number: 100,000 Max Cl/Cd: 46.58 at α=7.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe528-il-100000.txt Download as CSV file: xf-goe528-il-100000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 528 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.500 -0.2618 0.11825 0.11382 -0.0307 1.0000 0.0806
-9.250 -0.2761 0.11784 0.11351 -0.0282 1.0000 0.0817
-9.000 -0.2925 0.11766 0.11342 -0.0262 1.0000 0.0829
-8.750 -0.2997 0.11721 0.11302 -0.0362 0.9923 0.0847
-8.500 -0.2769 0.11083 0.10664 -0.0394 0.9874 0.0860
-8.250 -0.2402 0.10542 0.10117 -0.0401 0.9845 0.0893
-8.000 -0.2205 0.10187 0.09761 -0.0446 0.9770 0.0941
-7.750 -0.2209 0.10026 0.09603 -0.0540 0.9644 0.0982
-7.500 -0.2133 0.09590 0.09168 -0.0629 0.9526 0.0998
-7.250 -0.1761 0.09085 0.08660 -0.0597 0.9512 0.1031
-7.000 -0.1506 0.08706 0.08278 -0.0646 0.9448 0.1079
-6.750 -0.1492 0.08478 0.08033 -0.0853 0.9235 0.1143
-6.500 -0.1249 0.07929 0.07498 -0.0794 0.9205 0.1164
-6.250 -0.0922 0.07581 0.07148 -0.0801 0.9161 0.1232
-6.000 -0.0769 0.07160 0.06713 -0.0929 0.9024 0.1317
-5.750 -0.0426 0.06791 0.06347 -0.0921 0.8994 0.1364
-5.500 -0.0224 0.06425 0.05960 -0.1022 0.8867 0.1483
-5.250 0.0095 0.06083 0.05624 -0.1016 0.8825 0.1531
-5.000 0.0288 0.05777 0.05301 -0.1068 0.8706 0.1662
-4.750 0.0623 0.05465 0.04974 -0.1113 0.8643 0.1827
-4.500 0.0777 0.05268 0.04785 -0.1084 0.8538 0.1888
-4.250 0.1094 0.04970 0.04476 -0.1116 0.8472 0.2056
-4.000 0.1250 0.04780 0.04278 -0.1115 0.8351 0.2210
-3.750 0.1588 0.04557 0.04032 -0.1150 0.8290 0.2518
-3.500 0.1709 0.04389 0.03873 -0.1119 0.8168 0.2605
-3.250 0.2339 0.03369 0.02667 -0.1237 0.8118 0.1274
-3.000 0.2541 0.03126 0.02363 -0.1221 0.7997 0.1119
-2.750 0.2908 0.02882 0.02080 -0.1231 0.7948 0.1076
-2.500 0.3103 0.02775 0.01943 -0.1214 0.7827 0.1059
-2.250 0.3425 0.02653 0.01790 -0.1215 0.7759 0.1081
-2.000 0.3670 0.02571 0.01684 -0.1205 0.7658 0.1093
-1.750 0.3980 0.02473 0.01562 -0.1203 0.7586 0.1106
-1.500 0.4234 0.02413 0.01484 -0.1194 0.7491 0.1129
-1.250 0.4532 0.02323 0.01392 -0.1192 0.7420 0.1185
-1.000 0.4771 0.02285 0.01354 -0.1182 0.7326 0.1264
-0.750 0.5070 0.02209 0.01280 -0.1179 0.7262 0.1370
-0.500 0.5282 0.02178 0.01258 -0.1165 0.7165 0.1559
-0.250 0.5939 0.01848 0.01158 -0.1226 0.7118 1.0000
0.000 0.6118 0.01893 0.01183 -0.1208 0.7013 1.0000
0.250 0.6441 0.01887 0.01145 -0.1210 0.6955 1.0000
0.500 0.6619 0.01936 0.01183 -0.1192 0.6855 1.0000
0.750 0.6934 0.01933 0.01155 -0.1194 0.6795 1.0000
1.000 0.7119 0.01982 0.01197 -0.1178 0.6701 1.0000
1.250 0.7421 0.01985 0.01180 -0.1177 0.6639 1.0000
1.500 0.7620 0.02032 0.01219 -0.1164 0.6552 1.0000
1.750 0.7905 0.02042 0.01214 -0.1162 0.6484 1.0000
2.000 0.8129 0.02081 0.01247 -0.1151 0.6406 1.0000
2.250 0.8388 0.02102 0.01257 -0.1146 0.6331 1.0000
2.500 0.8649 0.02127 0.01272 -0.1141 0.6263 1.0000
2.750 0.8868 0.02166 0.01307 -0.1130 0.6181 1.0000
3.000 0.9189 0.02168 0.01294 -0.1133 0.6124 1.0000
3.250 0.9351 0.02231 0.01362 -0.1115 0.6031 1.0000
3.500 0.9683 0.02228 0.01342 -0.1120 0.5973 1.0000
3.750 0.9835 0.02297 0.01419 -0.1100 0.5880 1.0000
4.000 1.0155 0.02298 0.01407 -0.1104 0.5818 1.0000
4.250 1.0320 0.02364 0.01479 -0.1086 0.5729 1.0000
4.500 1.0624 0.02371 0.01477 -0.1087 0.5662 1.0000
4.750 1.0804 0.02433 0.01544 -0.1072 0.5576 1.0000
5.000 1.1090 0.02448 0.01552 -0.1070 0.5505 1.0000
5.250 1.1284 0.02506 0.01614 -0.1057 0.5422 1.0000
5.500 1.1549 0.02530 0.01634 -0.1053 0.5346 1.0000
5.750 1.1760 0.02583 0.01690 -0.1042 0.5268 1.0000
6.000 1.2001 0.02616 0.01724 -0.1035 0.5187 1.0000
6.250 1.2229 0.02663 0.01773 -0.1027 0.5112 1.0000
6.500 1.2438 0.02711 0.01824 -0.1016 0.5029 1.0000
6.750 1.2696 0.02749 0.01861 -0.1012 0.4958 1.0000
7.000 1.2860 0.02815 0.01938 -0.0995 0.4872 1.0000
7.250 1.3161 0.02836 0.01954 -0.0997 0.4806 1.0000
7.500 1.3271 0.02920 0.02053 -0.0973 0.4714 1.0000
7.750 1.3621 0.02924 0.02048 -0.0982 0.4652 1.0000
8.000 1.3664 0.03036 0.02183 -0.0949 0.4561 1.0000
8.250 1.4023 0.03037 0.02175 -0.0959 0.4500 1.0000
8.500 1.4038 0.03167 0.02328 -0.0923 0.4413 1.0000
8.750 1.4383 0.03159 0.02315 -0.0931 0.4346 1.0000
9.000 1.4412 0.03274 0.02450 -0.0897 0.4259 1.0000
9.250 1.4779 0.03240 0.02406 -0.0906 0.4185 1.0000
9.500 1.4775 0.03362 0.02550 -0.0868 0.4099 1.0000
9.750 1.5143 0.03330 0.02511 -0.0878 0.4026 1.0000
10.000 1.5113 0.03464 0.02668 -0.0837 0.3947 1.0000
10.250 1.5456 0.03437 0.02636 -0.0843 0.3873 1.0000
10.500 1.5429 0.03573 0.02794 -0.0804 0.3801 1.0000
10.750 1.5679 0.03585 0.02808 -0.0799 0.3729 1.0000
11.000 1.5736 0.03682 0.02919 -0.0770 0.3660 1.0000
11.250 1.5835 0.03745 0.02991 -0.0746 0.3590 1.0000
11.500 1.6031 0.03783 0.03035 -0.0734 0.3521 1.0000
11.750 1.5938 0.03915 0.03183 -0.0688 0.3456 1.0000
12.000 1.6267 0.03884 0.03149 -0.0692 0.3377 1.0000
12.250 1.6056 0.04080 0.03368 -0.0636 0.3318 1.0000
12.500 1.6417 0.04007 0.03287 -0.0642 0.3229 1.0000
12.750 1.6146 0.04256 0.03562 -0.0587 0.3173 1.0000
13.000 1.6495 0.04174 0.03473 -0.0589 0.3079 1.0000
13.250 1.6187 0.04478 0.03805 -0.0541 0.3027 1.0000
13.500 1.6439 0.04419 0.03740 -0.0533 0.2925 1.0000
13.750 1.6134 0.04767 0.04114 -0.0495 0.2868 1.0000
14.000 1.6236 0.04795 0.04141 -0.0479 0.2762 1.0000
14.250 1.6036 0.05100 0.04463 -0.0455 0.2683 1.0000
14.500 1.5945 0.05324 0.04695 -0.0438 0.2587 1.0000
14.750 1.5919 0.05486 0.04856 -0.0424 0.2472 1.0000
15.000 1.5669 0.05926 0.05315 -0.0413 0.2383 1.0000
15.250 1.5494 0.06315 0.05712 -0.0407 0.2277 1.0000
15.500 1.5350 0.06692 0.06092 -0.0404 0.2155 1.0000
15.750 1.5190 0.07120 0.06520 -0.0405 0.2026 1.0000
16.000 1.5015 0.07601 0.07001 -0.0410 0.1893 1.0000
16.250 1.4842 0.08110 0.07506 -0.0418 0.1758 1.0000
16.500 1.4689 0.08611 0.08002 -0.0427 0.1631 1.0000
16.750 1.4502 0.09204 0.08602 -0.0442 0.1521 1.0000
17.000 1.4358 0.09744 0.09144 -0.0456 0.1418 1.0000
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