GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL (goe303-il) Xfoil prediction polar at RE=100,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 303 (FRIEDRICHSHAFEN G03) AIRFOIL (goe303-il) Reynolds number: 100,000 Max Cl/Cd: 58.29 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe303-il-100000.txt Download as CSV file: xf-goe303-il-100000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 303 (FRIEDRICHSHAFEN G03) 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
------ -------- --------- --------- -------- -------- --------
-7.500 -0.2838 0.09995 0.09606 -0.0174 1.0000 0.0788
-7.250 -0.3541 0.10302 0.09877 -0.0202 1.0000 0.0766
-7.000 -0.3558 0.10067 0.09648 -0.0175 1.0000 0.0778
-6.750 -0.3617 0.09891 0.09479 -0.0155 1.0000 0.0790
-6.500 -0.3684 0.09728 0.09322 -0.0141 1.0000 0.0802
-6.250 -0.3577 0.09434 0.09029 -0.0173 0.9969 0.0828
-6.000 -0.2933 0.08962 0.08530 -0.0472 0.9839 0.0891
-5.750 -0.2847 0.08414 0.07994 -0.0416 0.9790 0.0907
-5.500 -0.2591 0.08029 0.07609 -0.0429 0.9732 0.0946
-5.250 -0.1934 0.07652 0.07190 -0.0663 0.9610 0.1043
-5.000 -0.1785 0.07113 0.06665 -0.0641 0.9557 0.1059
-4.750 -0.1547 0.06770 0.06323 -0.0650 0.9478 0.1094
-4.500 -0.1016 0.06375 0.05894 -0.0785 0.9385 0.1211
-4.250 -0.0784 0.06009 0.05537 -0.0783 0.9322 0.1250
-4.000 -0.0303 0.05674 0.05170 -0.0878 0.9234 0.1377
-3.750 -0.0018 0.05336 0.04838 -0.0890 0.9169 0.1425
-3.500 0.0425 0.05011 0.04490 -0.0955 0.9102 0.1559
-3.250 0.0794 0.04749 0.04213 -0.0994 0.9018 0.1716
-3.000 0.1251 0.04440 0.03894 -0.1044 0.8983 0.1891
-2.750 0.1595 0.04358 0.03781 -0.1072 0.8870 0.2161
-2.500 0.2001 0.03978 0.03406 -0.1108 0.8835 0.2353
-1.750 0.3567 0.02942 0.02165 -0.1236 0.8662 0.1161
-1.500 0.3862 0.02780 0.01971 -0.1236 0.8554 0.1108
-1.250 0.4298 0.02602 0.01757 -0.1257 0.8507 0.1104
-1.000 0.4579 0.02524 0.01658 -0.1254 0.8399 0.1136
-0.750 0.4985 0.02388 0.01497 -0.1268 0.8346 0.1163
-0.500 0.5254 0.02333 0.01422 -0.1261 0.8236 0.1198
-0.250 0.5632 0.02213 0.01307 -0.1272 0.8182 0.1315
0.000 0.5880 0.02167 0.01268 -0.1264 0.8068 0.1454
0.250 0.6201 0.02079 0.01190 -0.1264 0.7996 0.1790
0.500 0.6489 0.01990 0.01131 -0.1262 0.7899 0.2663
0.750 0.6814 0.01800 0.01084 -0.1261 0.7804 1.0000
1.000 0.7147 0.01769 0.01023 -0.1260 0.7714 1.0000
1.250 0.7410 0.01765 0.01000 -0.1251 0.7580 1.0000
1.500 0.7681 0.01759 0.00977 -0.1242 0.7448 1.0000
1.750 0.7959 0.01758 0.00961 -0.1235 0.7330 1.0000
2.000 0.8262 0.01755 0.00942 -0.1234 0.7237 1.0000
2.250 0.8507 0.01784 0.00963 -0.1226 0.7119 1.0000
2.500 0.8773 0.01805 0.00975 -0.1221 0.7014 1.0000
2.750 0.9066 0.01812 0.00970 -0.1218 0.6917 1.0000
3.000 0.9307 0.01842 0.00997 -0.1210 0.6795 1.0000
3.250 0.9565 0.01866 0.01015 -0.1203 0.6681 1.0000
3.500 0.9851 0.01878 0.01017 -0.1200 0.6579 1.0000
3.750 1.0095 0.01906 0.01043 -0.1192 0.6456 1.0000
4.000 1.0341 0.01935 0.01071 -0.1184 0.6334 1.0000
4.250 1.0600 0.01957 0.01090 -0.1177 0.6214 1.0000
4.500 1.0872 0.01971 0.01097 -0.1172 0.6094 1.0000
4.750 1.1122 0.01992 0.01114 -0.1164 0.5957 1.0000
5.000 1.1359 0.02016 0.01138 -0.1154 0.5810 1.0000
5.250 1.1599 0.02041 0.01163 -0.1144 0.5660 1.0000
5.500 1.1838 0.02067 0.01187 -0.1134 0.5505 1.0000
5.750 1.2077 0.02094 0.01211 -0.1124 0.5343 1.0000
6.000 1.2314 0.02123 0.01237 -0.1114 0.5174 1.0000
6.250 1.2549 0.02155 0.01262 -0.1104 0.5000 1.0000
6.500 1.2782 0.02193 0.01293 -0.1093 0.4827 1.0000
6.750 1.2996 0.02242 0.01344 -0.1081 0.4655 1.0000
7.000 1.3222 0.02295 0.01393 -0.1071 0.4499 1.0000
7.250 1.3455 0.02349 0.01442 -0.1063 0.4358 1.0000
7.500 1.3664 0.02410 0.01507 -0.1052 0.4220 1.0000
7.750 1.3872 0.02473 0.01578 -0.1040 0.4091 1.0000
8.000 1.4079 0.02531 0.01638 -0.1028 0.3965 1.0000
8.250 1.4284 0.02582 0.01688 -0.1016 0.3838 1.0000
8.500 1.4495 0.02632 0.01734 -0.1005 0.3717 1.0000
8.750 1.4690 0.02693 0.01802 -0.0992 0.3604 1.0000
9.000 1.4875 0.02767 0.01888 -0.0978 0.3502 1.0000
9.250 1.5096 0.02834 0.01954 -0.0970 0.3408 1.0000
9.500 1.5274 0.02906 0.02040 -0.0955 0.3308 1.0000
9.750 1.5446 0.02985 0.02131 -0.0940 0.3211 1.0000
10.000 1.5664 0.03056 0.02197 -0.0932 0.3112 1.0000
10.250 1.5789 0.03137 0.02298 -0.0910 0.3008 1.0000
10.500 1.5925 0.03222 0.02398 -0.0889 0.2901 1.0000
10.750 1.6077 0.03303 0.02480 -0.0871 0.2787 1.0000
11.000 1.6213 0.03383 0.02557 -0.0852 0.2660 1.0000
11.250 1.6225 0.03473 0.02665 -0.0813 0.2534 1.0000
11.500 1.6200 0.03570 0.02775 -0.0770 0.2408 1.0000
11.750 1.6155 0.03678 0.02890 -0.0726 0.2282 1.0000
12.000 1.6102 0.03800 0.03018 -0.0685 0.2158 1.0000
12.250 1.6043 0.03939 0.03159 -0.0647 0.2036 1.0000
12.500 1.5958 0.04110 0.03339 -0.0612 0.1919 1.0000
12.750 1.5866 0.04319 0.03566 -0.0581 0.1801 1.0000
13.000 1.5792 0.04547 0.03805 -0.0557 0.1690 1.0000
13.250 1.5721 0.04793 0.04057 -0.0536 0.1589 1.0000
13.500 1.5647 0.05060 0.04324 -0.0520 0.1494 1.0000
13.750 1.5562 0.05375 0.04653 -0.0507 0.1395 1.0000
14.000 1.5473 0.05709 0.04992 -0.0497 0.1304 1.0000
14.250 1.5377 0.06061 0.05338 -0.0488 0.1221 1.0000
14.500 1.5267 0.06457 0.05746 -0.0483 0.1136 1.0000
14.750 1.5154 0.06873 0.06165 -0.0479 0.1052 1.0000
15.000 1.5051 0.07279 0.06562 -0.0474 0.0969 1.0000
15.250 1.4931 0.07734 0.07026 -0.0475 0.0893 1.0000
15.500 1.4835 0.08165 0.07461 -0.0473 0.0821 1.0000
15.750 1.4839 0.08440 0.07715 -0.0461 0.0745 1.0000
16.000 1.4725 0.08940 0.08245 -0.0468 0.0708 1.0000
16.250 1.4712 0.09268 0.08572 -0.0466 0.0663 1.0000
16.500 1.4716 0.09587 0.08896 -0.0461 0.0625 1.0000
16.750 1.4610 0.10094 0.09430 -0.0474 0.0603 1.0000
17.000 1.4555 0.10522 0.09874 -0.0484 0.0579 1.0000
17.250 1.4755 0.10543 0.09872 -0.0458 0.0543 1.0000
17.500 1.4606 0.11132 0.10493 -0.0480 0.0536 1.0000
17.750 1.4449 0.11762 0.11153 -0.0507 0.0530 1.0000
18.000 1.4274 0.12450 0.11869 -0.0540 0.0526 1.0000
18.250 1.4076 0.13213 0.12659 -0.0581 0.0523 1.0000
18.500 1.3848 0.14079 0.13551 -0.0633 0.0523 1.0000
18.750 1.3578 0.15091 0.14588 -0.0699 0.0527 1.0000
19.000 1.3272 0.16271 0.15787 -0.0779 0.0534 1.0000
19.250 1.2940 0.17623 0.17154 -0.0871 0.0541 1.0000
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Polar data table (+)
Polar graphs
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