GOE 420 AIRFOIL (goe420-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 420 AIRFOIL (goe420-il) Reynolds number: 500,000 Max Cl/Cd: 83.51 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe420-il-500000-n5.txt Download as CSV file: xf-goe420-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 420 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.6574 0.11384 0.11026 -0.0710 1.0000 0.0273
-18.250 -0.6871 0.10496 0.10121 -0.0759 1.0000 0.0273
-18.000 -0.7074 0.09794 0.09404 -0.0799 1.0000 0.0275
-17.750 -0.7207 0.09233 0.08833 -0.0829 1.0000 0.0275
-17.500 -0.7315 0.08729 0.08319 -0.0856 1.0000 0.0276
-17.250 -0.7414 0.08249 0.07828 -0.0881 1.0000 0.0278
-17.000 -0.7481 0.07838 0.07410 -0.0902 1.0000 0.0278
-16.750 -0.7552 0.07428 0.06991 -0.0922 1.0000 0.0279
-16.500 -0.7600 0.07071 0.06626 -0.0938 1.0000 0.0279
-16.250 -0.7662 0.06702 0.06250 -0.0954 1.0000 0.0281
-16.000 -0.7722 0.06360 0.05900 -0.0967 1.0000 0.0282
-15.750 -0.7713 0.05979 0.05511 -0.0993 0.9918 0.0283
-15.500 -0.7645 0.05629 0.05151 -0.1030 0.9820 0.0284
-15.250 -0.7552 0.05291 0.04804 -0.1069 0.9713 0.0285
-15.000 -0.7421 0.04966 0.04469 -0.1114 0.9624 0.0287
-14.750 -0.7245 0.04665 0.04162 -0.1162 0.9547 0.0288
-14.500 -0.7029 0.04359 0.03850 -0.1218 0.9487 0.0291
-14.250 -0.6799 0.04065 0.03548 -0.1275 0.9411 0.0292
-13.750 -0.6318 0.03530 0.02993 -0.1384 0.9227 0.0296
-13.500 -0.6130 0.03298 0.02749 -0.1423 0.9112 0.0298
-13.250 -0.6010 0.03088 0.02527 -0.1445 0.8992 0.0301
-13.000 -0.5947 0.02896 0.02324 -0.1453 0.8879 0.0302
-12.500 -0.5844 0.02566 0.01974 -0.1455 0.8691 0.0306
-12.250 -0.5801 0.02422 0.01819 -0.1450 0.8607 0.0307
-12.000 -0.5764 0.02298 0.01687 -0.1438 0.8534 0.0309
-11.750 -0.5726 0.02194 0.01576 -0.1421 0.8457 0.0311
-11.500 -0.5679 0.02108 0.01478 -0.1401 0.8390 0.0313
-11.250 -0.5630 0.02034 0.01399 -0.1375 0.8322 0.0315
-11.000 -0.5575 0.01971 0.01328 -0.1347 0.8252 0.0317
-10.750 -0.5501 0.01923 0.01271 -0.1319 0.8195 0.0319
-10.500 -0.5374 0.01872 0.01215 -0.1299 0.8140 0.0321
-10.250 -0.5225 0.01824 0.01161 -0.1282 0.8084 0.0324
-10.000 -0.5065 0.01776 0.01106 -0.1267 0.8032 0.0327
-9.750 -0.4903 0.01724 0.01049 -0.1252 0.7983 0.0330
-9.500 -0.4724 0.01676 0.00999 -0.1239 0.7930 0.0334
-9.250 -0.4529 0.01634 0.00953 -0.1227 0.7875 0.0339
-9.000 -0.4321 0.01597 0.00909 -0.1217 0.7821 0.0344
-8.750 -0.4107 0.01561 0.00869 -0.1208 0.7766 0.0350
-8.500 -0.3888 0.01527 0.00831 -0.1199 0.7703 0.0357
-8.250 -0.3664 0.01495 0.00792 -0.1191 0.7641 0.0362
-8.000 -0.3434 0.01465 0.00756 -0.1184 0.7579 0.0368
-7.750 -0.3211 0.01428 0.00717 -0.1175 0.7504 0.0376
-7.500 -0.2979 0.01398 0.00681 -0.1168 0.7437 0.0385
-7.250 -0.2740 0.01370 0.00651 -0.1161 0.7370 0.0395
-7.000 -0.2498 0.01345 0.00620 -0.1155 0.7294 0.0407
-6.750 -0.2255 0.01321 0.00590 -0.1149 0.7225 0.0420
-6.500 -0.2011 0.01294 0.00563 -0.1143 0.7149 0.0439
-6.250 -0.1765 0.01274 0.00536 -0.1137 0.7070 0.0461
-6.000 -0.1518 0.01250 0.00511 -0.1131 0.6986 0.0493
-5.750 -0.1271 0.01229 0.00487 -0.1126 0.6908 0.0539
-5.500 -0.1020 0.01207 0.00464 -0.1121 0.6848 0.0599
-5.250 -0.0767 0.01183 0.00442 -0.1116 0.6787 0.0680
-5.000 -0.0517 0.01161 0.00420 -0.1111 0.6724 0.0782
-4.750 -0.0272 0.01133 0.00397 -0.1106 0.6667 0.0951
-4.500 -0.0021 0.01106 0.00381 -0.1101 0.6604 0.1215
-4.250 0.0235 0.01091 0.00367 -0.1097 0.6540 0.1362
-4.000 0.0497 0.01081 0.00355 -0.1093 0.6486 0.1472
-3.750 0.0761 0.01065 0.00342 -0.1090 0.6434 0.1579
-3.500 0.1022 0.01051 0.00330 -0.1087 0.6380 0.1699
-3.250 0.1278 0.01037 0.00319 -0.1083 0.6327 0.1869
-3.000 0.1535 0.01018 0.00310 -0.1079 0.6279 0.2159
-2.750 0.1798 0.01004 0.00306 -0.1076 0.6226 0.2455
-2.500 0.2058 0.00996 0.00303 -0.1072 0.6167 0.2697
-2.250 0.2319 0.00992 0.00301 -0.1068 0.6110 0.2899
-2.000 0.2590 0.00988 0.00299 -0.1066 0.6054 0.3024
-1.750 0.2856 0.00986 0.00298 -0.1062 0.5995 0.3136
-1.500 0.3119 0.00987 0.00295 -0.1058 0.5938 0.3207
-1.250 0.3388 0.00985 0.00294 -0.1056 0.5885 0.3274
-1.000 0.3655 0.00985 0.00293 -0.1052 0.5822 0.3337
-0.750 0.3915 0.00988 0.00292 -0.1048 0.5757 0.3396
-0.500 0.4178 0.00987 0.00293 -0.1044 0.5695 0.3472
-0.250 0.4438 0.00989 0.00293 -0.1039 0.5617 0.3552
0.000 0.4687 0.00992 0.00295 -0.1033 0.5540 0.3638
0.250 0.4944 0.00994 0.00297 -0.1028 0.5450 0.3728
0.500 0.5188 0.01001 0.00299 -0.1020 0.5362 0.3797
0.750 0.5440 0.01003 0.00303 -0.1014 0.5269 0.3879
1.000 0.5676 0.01011 0.00307 -0.1006 0.5176 0.3964
1.250 0.5917 0.01016 0.00313 -0.0998 0.5073 0.4059
1.500 0.6145 0.01025 0.00320 -0.0987 0.4972 0.4188
1.750 0.6368 0.01033 0.00328 -0.0976 0.4868 0.4318
2.000 0.6592 0.01043 0.00336 -0.0966 0.4778 0.4428
2.250 0.6812 0.01053 0.00346 -0.0954 0.4697 0.4554
2.500 0.7028 0.01064 0.00357 -0.0942 0.4626 0.4687
2.750 0.7241 0.01074 0.00368 -0.0929 0.4548 0.4829
3.000 0.7414 0.01088 0.00380 -0.0908 0.4468 0.4961
3.250 0.7619 0.01096 0.00391 -0.0894 0.4397 0.5102
3.500 0.7799 0.01109 0.00406 -0.0875 0.4323 0.5274
3.750 0.7988 0.01121 0.00423 -0.0859 0.4267 0.5492
4.000 0.8200 0.01129 0.00440 -0.0846 0.4224 0.5783
4.250 0.8402 0.01138 0.00460 -0.0832 0.4185 0.6121
4.500 0.8597 0.01152 0.00480 -0.0817 0.4146 0.6433
4.750 0.8785 0.01169 0.00502 -0.0800 0.4107 0.6690
5.000 0.8991 0.01180 0.00521 -0.0787 0.4073 0.6935
5.500 0.9356 0.01191 0.00564 -0.0751 0.3998 0.7766
5.750 0.9700 0.01188 0.00597 -0.0764 0.3959 0.9481
6.000 1.0074 0.01216 0.00623 -0.0788 0.3919 1.0000
6.250 1.0284 0.01236 0.00644 -0.0777 0.3891 1.0000
6.500 1.0496 0.01257 0.00666 -0.0767 0.3859 1.0000
6.750 1.0697 0.01281 0.00691 -0.0755 0.3823 1.0000
7.000 1.0882 0.01310 0.00718 -0.0740 0.3778 1.0000
7.250 1.1055 0.01345 0.00750 -0.0725 0.3735 1.0000
7.500 1.1252 0.01372 0.00779 -0.0713 0.3677 1.0000
7.750 1.1420 0.01409 0.00814 -0.0697 0.3600 1.0000
8.000 1.1574 0.01452 0.00853 -0.0680 0.3517 1.0000
8.250 1.1744 0.01492 0.00893 -0.0665 0.3436 1.0000
8.500 1.1893 0.01542 0.00939 -0.0648 0.3368 1.0000
8.750 1.2077 0.01580 0.00979 -0.0637 0.3301 1.0000
9.000 1.2221 0.01636 0.01032 -0.0620 0.3227 1.0000
9.250 1.2381 0.01687 0.01083 -0.0606 0.3141 1.0000
9.500 1.2497 0.01759 0.01151 -0.0587 0.3036 1.0000
9.750 1.2627 0.01829 0.01217 -0.0570 0.2921 1.0000
10.000 1.2730 0.01914 0.01298 -0.0552 0.2802 1.0000
10.250 1.2828 0.02006 0.01385 -0.0533 0.2692 1.0000
10.500 1.2925 0.02102 0.01477 -0.0515 0.2585 1.0000
10.750 1.3037 0.02192 0.01566 -0.0500 0.2500 1.0000
11.000 1.3128 0.02298 0.01669 -0.0483 0.2413 1.0000
11.250 1.3241 0.02394 0.01765 -0.0469 0.2338 1.0000
11.500 1.3328 0.02509 0.01878 -0.0453 0.2258 1.0000
11.750 1.3431 0.02618 0.01987 -0.0440 0.2188 1.0000
12.000 1.3516 0.02743 0.02110 -0.0425 0.2111 1.0000
12.250 1.3604 0.02869 0.02237 -0.0412 0.2039 1.0000
12.500 1.3683 0.03005 0.02372 -0.0400 0.1958 1.0000
12.750 1.3755 0.03151 0.02518 -0.0387 0.1875 1.0000
13.000 1.3792 0.03329 0.02693 -0.0374 0.1767 1.0000
13.250 1.3808 0.03529 0.02889 -0.0360 0.1629 1.0000
13.500 1.3775 0.03776 0.03128 -0.0346 0.1454 1.0000
13.750 1.3726 0.04046 0.03391 -0.0332 0.1303 1.0000
14.000 1.3699 0.04308 0.03649 -0.0321 0.1196 1.0000
14.250 1.3674 0.04573 0.03913 -0.0312 0.1111 1.0000
14.500 1.3653 0.04844 0.04183 -0.0303 0.1038 1.0000
14.750 1.3684 0.05069 0.04412 -0.0298 0.0996 1.0000
15.000 1.3687 0.05328 0.04673 -0.0292 0.0950 1.0000
15.250 1.3695 0.05586 0.04934 -0.0288 0.0919 1.0000
15.500 1.3725 0.05825 0.05177 -0.0285 0.0888 1.0000
15.750 1.3735 0.06091 0.05447 -0.0282 0.0862 1.0000
16.000 1.3726 0.06382 0.05742 -0.0280 0.0835 1.0000
16.250 1.3744 0.06646 0.06012 -0.0279 0.0813 1.0000
16.500 1.3757 0.06921 0.06292 -0.0279 0.0792 1.0000
16.750 1.3764 0.07206 0.06582 -0.0280 0.0773 1.0000
17.000 1.3745 0.07528 0.06909 -0.0281 0.0755 1.0000
17.250 1.3742 0.07836 0.07222 -0.0284 0.0739 1.0000
17.500 1.3762 0.08116 0.07508 -0.0286 0.0724 1.0000
17.750 1.3764 0.08421 0.07820 -0.0290 0.0710 1.0000
18.000 1.3766 0.08729 0.08134 -0.0294 0.0695 1.0000
18.250 1.3742 0.09076 0.08486 -0.0300 0.0681 1.0000
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