GOE 434 AIRFOIL (goe434-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 434 AIRFOIL (goe434-il) Reynolds number: 200,000 Max Cl/Cd: 62.83 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe434-il-200000-n5.txt Download as CSV file: xf-goe434-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 434 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.750 -0.6892 0.08400 0.07788 -0.0898 1.0000 0.0709
-16.500 -0.7097 0.07802 0.07171 -0.0934 1.0000 0.0716
-16.250 -0.6993 0.07656 0.07030 -0.0936 1.0000 0.0721
-16.000 -0.6944 0.07444 0.06820 -0.0943 1.0000 0.0726
-15.750 -0.6929 0.07204 0.06580 -0.0951 1.0000 0.0732
-15.500 -0.6938 0.06952 0.06326 -0.0958 0.9998 0.0738
-15.250 -0.6855 0.06609 0.05974 -0.0995 0.9914 0.0747
-15.000 -0.6782 0.06266 0.05621 -0.1031 0.9819 0.0756
-14.750 -0.6719 0.05908 0.05249 -0.1070 0.9720 0.0766
-14.500 -0.6658 0.05566 0.04890 -0.1106 0.9605 0.0774
-14.250 -0.6553 0.05338 0.04655 -0.1125 0.9465 0.0782
-14.000 -0.6382 0.05222 0.04543 -0.1129 0.9308 0.0789
-13.750 -0.6255 0.05078 0.04398 -0.1133 0.9113 0.0797
-13.500 -0.6154 0.04918 0.04233 -0.1136 0.8884 0.0805
-13.250 -0.6076 0.04746 0.04050 -0.1137 0.8644 0.0813
-13.000 -0.6008 0.04569 0.03860 -0.1139 0.8419 0.0822
-12.750 -0.5935 0.04393 0.03669 -0.1143 0.8223 0.0831
-12.500 -0.5862 0.04212 0.03471 -0.1148 0.8054 0.0840
-12.250 -0.5779 0.04038 0.03279 -0.1155 0.7903 0.0849
-12.000 -0.5633 0.03945 0.03188 -0.1152 0.7769 0.0858
-11.750 -0.5512 0.03820 0.03057 -0.1153 0.7649 0.0866
-11.500 -0.5394 0.03678 0.02911 -0.1159 0.7541 0.0876
-11.250 -0.5278 0.03535 0.02760 -0.1164 0.7439 0.0886
-11.000 -0.5158 0.03387 0.02604 -0.1172 0.7354 0.0898
-10.750 -0.5031 0.03240 0.02450 -0.1180 0.7266 0.0909
-10.500 -0.4902 0.03098 0.02296 -0.1189 0.7186 0.0920
-10.250 -0.4804 0.02960 0.02154 -0.1194 0.7118 0.0930
-10.000 -0.4672 0.02806 0.02000 -0.1209 0.7053 0.0942
-9.750 -0.4500 0.02657 0.01846 -0.1229 0.6994 0.0955
-9.500 -0.4296 0.02524 0.01703 -0.1251 0.6940 0.0971
-9.250 -0.4072 0.02419 0.01586 -0.1268 0.6895 0.0989
-9.000 -0.3843 0.02327 0.01491 -0.1281 0.6852 0.1007
-8.750 -0.3608 0.02241 0.01404 -0.1292 0.6807 0.1028
-8.500 -0.3361 0.02171 0.01331 -0.1301 0.6761 0.1051
-8.250 -0.3106 0.02112 0.01266 -0.1307 0.6717 0.1079
-8.000 -0.2848 0.02052 0.01204 -0.1315 0.6679 0.1115
-7.500 -0.2309 0.01955 0.01105 -0.1327 0.6616 0.1226
-7.250 -0.2035 0.01911 0.01063 -0.1333 0.6582 0.1306
-7.000 -0.1757 0.01873 0.01025 -0.1337 0.6546 0.1401
-6.750 -0.1477 0.01838 0.00989 -0.1342 0.6510 0.1502
-6.500 -0.1193 0.01808 0.00955 -0.1346 0.6477 0.1601
-6.250 -0.0909 0.01774 0.00921 -0.1350 0.6448 0.1696
-6.000 -0.0622 0.01746 0.00890 -0.1355 0.6419 0.1787
-5.750 -0.0331 0.01724 0.00865 -0.1359 0.6390 0.1886
-5.500 -0.0045 0.01699 0.00847 -0.1363 0.6361 0.1998
-5.250 0.0244 0.01679 0.00834 -0.1366 0.6330 0.2124
-5.000 0.0535 0.01666 0.00826 -0.1369 0.6297 0.2256
-4.750 0.0827 0.01657 0.00819 -0.1372 0.6264 0.2390
-4.500 0.1121 0.01652 0.00813 -0.1374 0.6232 0.2504
-4.250 0.1419 0.01650 0.00804 -0.1376 0.6202 0.2609
-4.000 0.1717 0.01651 0.00804 -0.1379 0.6173 0.2703
-3.750 0.2019 0.01656 0.00798 -0.1382 0.6145 0.2791
-3.500 0.2307 0.01656 0.00805 -0.1382 0.6117 0.2862
-3.250 0.2599 0.01657 0.00805 -0.1383 0.6087 0.2934
-3.000 0.2891 0.01658 0.00804 -0.1385 0.6057 0.2995
-2.750 0.3182 0.01661 0.00811 -0.1386 0.6026 0.3056
-2.500 0.3476 0.01664 0.00811 -0.1387 0.5995 0.3121
-2.250 0.3773 0.01667 0.00805 -0.1388 0.5965 0.3177
-2.000 0.4069 0.01669 0.00807 -0.1390 0.5938 0.3224
-1.750 0.4370 0.01676 0.00812 -0.1392 0.5913 0.3274
-1.500 0.4659 0.01684 0.00820 -0.1393 0.5886 0.3332
-1.250 0.4943 0.01690 0.00826 -0.1393 0.5854 0.3391
-1.000 0.5227 0.01692 0.00832 -0.1392 0.5819 0.3442
-0.750 0.5512 0.01695 0.00841 -0.1392 0.5786 0.3491
-0.500 0.5800 0.01700 0.00845 -0.1392 0.5753 0.3539
-0.250 0.6092 0.01702 0.00844 -0.1393 0.5719 0.3588
0.000 0.6393 0.01707 0.00839 -0.1395 0.5683 0.3635
0.250 0.6666 0.01709 0.00843 -0.1393 0.5638 0.3672
0.500 0.6935 0.01707 0.00851 -0.1390 0.5586 0.3711
0.750 0.7212 0.01708 0.00856 -0.1388 0.5541 0.3756
1.000 0.7496 0.01710 0.00856 -0.1387 0.5500 0.3804
1.250 0.7789 0.01713 0.00852 -0.1388 0.5463 0.3856
1.500 0.8058 0.01721 0.00862 -0.1385 0.5417 0.3902
1.750 0.8321 0.01723 0.00873 -0.1382 0.5365 0.3949
2.000 0.8590 0.01724 0.00879 -0.1379 0.5314 0.3996
2.250 0.8869 0.01725 0.00877 -0.1377 0.5267 0.4043
2.500 0.9135 0.01732 0.00886 -0.1374 0.5218 0.4090
2.750 0.9392 0.01742 0.00901 -0.1369 0.5161 0.4137
3.000 0.9653 0.01745 0.00904 -0.1365 0.5100 0.4183
3.250 0.9912 0.01747 0.00908 -0.1360 0.5040 0.4238
3.500 1.0152 0.01758 0.00928 -0.1353 0.4964 0.4300
3.750 1.0400 0.01766 0.00935 -0.1347 0.4896 0.4369
4.000 1.0645 0.01780 0.00948 -0.1340 0.4834 0.4434
4.250 1.0880 0.01793 0.00970 -0.1333 0.4764 0.4500
4.500 1.1113 0.01806 0.00983 -0.1324 0.4697 0.4578
4.750 1.1335 0.01826 0.01007 -0.1314 0.4619 0.4661
5.000 1.1546 0.01846 0.01028 -0.1303 0.4537 0.4741
5.250 1.1742 0.01869 0.01055 -0.1289 0.4456 0.4834
5.500 1.1913 0.01897 0.01084 -0.1271 0.4367 0.4939
5.750 1.2086 0.01929 0.01118 -0.1254 0.4284 0.5043
6.000 1.2259 0.01969 0.01162 -0.1239 0.4189 0.5163
6.250 1.2423 0.02017 0.01209 -0.1222 0.4095 0.5280
6.500 1.2569 0.02072 0.01266 -0.1204 0.3986 0.5401
6.750 1.2708 0.02136 0.01330 -0.1186 0.3873 0.5523
7.000 1.2815 0.02214 0.01407 -0.1165 0.3749 0.5642
7.250 1.2910 0.02305 0.01497 -0.1144 0.3605 0.5767
7.500 1.2985 0.02411 0.01604 -0.1123 0.3447 0.5889
7.750 1.3031 0.02544 0.01732 -0.1100 0.3274 0.6021
8.000 1.3051 0.02701 0.01887 -0.1077 0.3095 0.6147
8.500 1.3054 0.03081 0.02262 -0.1036 0.2772 0.6418
8.750 1.3064 0.03283 0.02463 -0.1019 0.2653 0.6563
9.000 1.3069 0.03498 0.02678 -0.1004 0.2559 0.6721
9.250 1.3113 0.03685 0.02869 -0.0991 0.2482 0.6892
9.500 1.3133 0.03895 0.03080 -0.0977 0.2416 0.7077
9.750 1.3198 0.04071 0.03261 -0.0966 0.2364 0.7301
10.000 1.3260 0.04248 0.03445 -0.0955 0.2315 0.7553
10.250 1.3307 0.04437 0.03639 -0.0943 0.2271 0.7845
10.500 1.3360 0.04611 0.03820 -0.0930 0.2233 0.8241
10.750 1.3390 0.04737 0.03963 -0.0911 0.2198 1.0000
11.000 1.3483 0.04910 0.04135 -0.0905 0.2161 1.0000
11.250 1.3564 0.05093 0.04316 -0.0898 0.2128 1.0000
11.500 1.3643 0.05278 0.04496 -0.0892 0.2099 1.0000
11.750 1.3742 0.05443 0.04658 -0.0886 0.2076 1.0000
12.000 1.3865 0.05591 0.04810 -0.0881 0.2053 1.0000
12.250 1.3974 0.05751 0.04974 -0.0876 0.2030 1.0000
12.500 1.4079 0.05917 0.05142 -0.0871 0.2006 1.0000
12.750 1.4181 0.06084 0.05309 -0.0866 0.1983 1.0000
13.250 1.4364 0.06433 0.05651 -0.0856 0.1932 1.0000
13.500 1.4460 0.06612 0.05834 -0.0852 0.1909 1.0000
13.750 1.4558 0.06792 0.06020 -0.0849 0.1885 1.0000
14.000 1.4658 0.06968 0.06201 -0.0845 0.1863 1.0000
14.250 1.4751 0.07149 0.06385 -0.0842 0.1841 1.0000
14.500 1.4832 0.07345 0.06582 -0.0839 0.1819 1.0000
14.750 1.4912 0.07539 0.06774 -0.0836 0.1796 1.0000
15.000 1.5001 0.07720 0.06954 -0.0832 0.1774 1.0000
15.250 1.5083 0.07923 0.07167 -0.0831 0.1754 1.0000
15.500 1.5156 0.08136 0.07388 -0.0829 0.1732 1.0000
15.750 1.5225 0.08352 0.07610 -0.0828 0.1710 1.0000
16.000 1.5295 0.08568 0.07830 -0.0827 0.1689 1.0000
16.250 1.5358 0.08789 0.08053 -0.0827 0.1668 1.0000
16.500 1.5427 0.08998 0.08260 -0.0825 0.1648 1.0000
16.750 1.5482 0.09236 0.08506 -0.0826 0.1627 1.0000
17.000 1.5528 0.09490 0.08771 -0.0828 0.1603 1.0000
17.250 1.5560 0.09761 0.09051 -0.0830 0.1578 1.0000
17.500 1.5598 0.10022 0.09317 -0.0832 0.1554 1.0000
17.750 1.5635 0.10282 0.09578 -0.0835 0.1531 1.0000
18.000 1.5663 0.10557 0.09858 -0.0839 0.1507 1.0000
18.250 1.5677 0.10862 0.10176 -0.0844 0.1478 1.0000
18.500 1.5677 0.11184 0.10506 -0.0851 0.1448 1.0000
18.750 1.5687 0.11487 0.10812 -0.0858 0.1420 1.0000
19.000 1.5687 0.11809 0.11138 -0.0866 0.1392 1.0000
19.250 1.5675 0.12155 0.11498 -0.0875 0.1357 1.0000
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