GOE 434 AIRFOIL (goe434-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 434 AIRFOIL (goe434-il) Reynolds number: 500,000 Max Cl/Cd: 83.2 at α=4.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe434-il-500000-n5.txt Download as CSV file: xf-goe434-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.8065 0.11040 0.10601 -0.0696 1.0000 0.0542
-19.500 -0.8120 0.10603 0.10154 -0.0722 1.0000 0.0547
-19.250 -0.8072 0.10329 0.09881 -0.0737 1.0000 0.0552
-19.000 -0.8048 0.10020 0.09570 -0.0755 1.0000 0.0557
-18.750 -0.8038 0.09690 0.09238 -0.0773 1.0000 0.0561
-18.500 -0.8015 0.09380 0.08925 -0.0790 1.0000 0.0566
-18.250 -0.8006 0.09053 0.08594 -0.0808 1.0000 0.0571
-18.000 -0.7984 0.08749 0.08287 -0.0825 1.0000 0.0577
-17.750 -0.7955 0.08458 0.07991 -0.0841 1.0000 0.0582
-17.500 -0.7939 0.08150 0.07678 -0.0857 1.0000 0.0587
-17.250 -0.7902 0.07876 0.07399 -0.0871 1.0000 0.0593
-17.000 -0.7859 0.07604 0.07121 -0.0887 0.9972 0.0597
-16.750 -0.7778 0.07320 0.06834 -0.0912 0.9856 0.0602
-16.500 -0.7678 0.07049 0.06561 -0.0937 0.9755 0.0607
-16.250 -0.7598 0.06789 0.06299 -0.0956 0.9637 0.0613
-16.000 -0.7545 0.06523 0.06029 -0.0971 0.9509 0.0618
-15.750 -0.7500 0.06280 0.05779 -0.0981 0.9360 0.0624
-15.500 -0.7457 0.06055 0.05547 -0.0987 0.9171 0.0629
-15.250 -0.7430 0.05826 0.05306 -0.0991 0.8895 0.0635
-15.000 -0.7400 0.05608 0.05071 -0.0993 0.8559 0.0641
-14.750 -0.7343 0.05405 0.04850 -0.0999 0.8269 0.0646
-14.500 -0.7282 0.05195 0.04622 -0.1008 0.8043 0.0651
-14.250 -0.7220 0.04982 0.04396 -0.1018 0.7856 0.0656
-14.000 -0.7159 0.04773 0.04179 -0.1028 0.7687 0.0661
-13.750 -0.7108 0.04551 0.03949 -0.1040 0.7544 0.0666
-13.500 -0.7051 0.04339 0.03727 -0.1051 0.7403 0.0671
-13.250 -0.6983 0.04130 0.03511 -0.1063 0.7285 0.0677
-13.000 -0.6914 0.03923 0.03294 -0.1075 0.7167 0.0683
-12.750 -0.6832 0.03725 0.03088 -0.1087 0.7071 0.0689
-12.500 -0.6744 0.03529 0.02883 -0.1100 0.6975 0.0696
-12.250 -0.6648 0.03340 0.02684 -0.1112 0.6888 0.0702
-12.000 -0.6533 0.03161 0.02497 -0.1125 0.6816 0.0708
-11.750 -0.6409 0.02988 0.02316 -0.1138 0.6741 0.0714
-11.500 -0.6318 0.02784 0.02105 -0.1154 0.6670 0.0720
-11.250 -0.6227 0.02589 0.01905 -0.1171 0.6615 0.0725
-11.000 -0.6052 0.02409 0.01720 -0.1198 0.6566 0.0732
-10.750 -0.5835 0.02254 0.01558 -0.1226 0.6518 0.0741
-10.500 -0.5588 0.02125 0.01420 -0.1253 0.6471 0.0750
-10.250 -0.5328 0.02029 0.01316 -0.1273 0.6427 0.0759
-10.000 -0.5067 0.01962 0.01241 -0.1284 0.6389 0.0768
-9.750 -0.4799 0.01905 0.01179 -0.1293 0.6361 0.0775
-9.500 -0.4534 0.01844 0.01114 -0.1302 0.6329 0.0783
-9.250 -0.4270 0.01780 0.01048 -0.1310 0.6294 0.0794
-9.000 -0.3999 0.01730 0.00994 -0.1317 0.6259 0.0805
-8.750 -0.3723 0.01688 0.00948 -0.1322 0.6228 0.0816
-8.500 -0.3443 0.01651 0.00907 -0.1327 0.6198 0.0826
-8.250 -0.3161 0.01620 0.00869 -0.1331 0.6169 0.0837
-8.000 -0.2876 0.01593 0.00837 -0.1334 0.6143 0.0847
-7.750 -0.2591 0.01549 0.00794 -0.1340 0.6124 0.0861
-7.500 -0.2303 0.01512 0.00756 -0.1345 0.6100 0.0876
-7.250 -0.2013 0.01480 0.00724 -0.1349 0.6076 0.0891
-7.000 -0.1721 0.01454 0.00695 -0.1353 0.6053 0.0907
-6.750 -0.1428 0.01429 0.00668 -0.1356 0.6028 0.0924
-6.500 -0.1138 0.01399 0.00638 -0.1360 0.6002 0.0952
-6.250 -0.0846 0.01373 0.00611 -0.1363 0.5976 0.0986
-6.000 -0.0555 0.01346 0.00584 -0.1367 0.5949 0.1043
-5.750 -0.0265 0.01315 0.00559 -0.1371 0.5918 0.1187
-5.500 0.0030 0.01290 0.00541 -0.1375 0.5894 0.1371
-5.250 0.0329 0.01270 0.00525 -0.1378 0.5874 0.1481
-5.000 0.0628 0.01252 0.00510 -0.1382 0.5851 0.1570
-4.750 0.0928 0.01234 0.00494 -0.1385 0.5827 0.1643
-4.500 0.1227 0.01221 0.00482 -0.1388 0.5804 0.1711
-4.250 0.1526 0.01206 0.00469 -0.1391 0.5780 0.1780
-3.500 0.2419 0.01162 0.00436 -0.1400 0.5705 0.2184
-3.250 0.2718 0.01155 0.00433 -0.1403 0.5681 0.2350
-3.000 0.3020 0.01150 0.00432 -0.1405 0.5661 0.2475
-2.750 0.3322 0.01145 0.00430 -0.1408 0.5641 0.2584
-2.500 0.3624 0.01140 0.00430 -0.1410 0.5617 0.2673
-2.250 0.3925 0.01139 0.00430 -0.1412 0.5591 0.2754
-2.000 0.4225 0.01137 0.00429 -0.1414 0.5561 0.2817
-1.750 0.4523 0.01136 0.00429 -0.1415 0.5528 0.2876
-1.500 0.4818 0.01138 0.00427 -0.1416 0.5493 0.2924
-1.250 0.5110 0.01144 0.00427 -0.1417 0.5454 0.2963
-1.000 0.5409 0.01140 0.00428 -0.1418 0.5419 0.3005
-0.750 0.5707 0.01139 0.00430 -0.1420 0.5380 0.3054
-0.500 0.6002 0.01140 0.00432 -0.1421 0.5342 0.3101
-0.250 0.6295 0.01142 0.00433 -0.1421 0.5305 0.3141
0.000 0.6584 0.01148 0.00434 -0.1421 0.5264 0.3179
0.250 0.6877 0.01149 0.00438 -0.1422 0.5224 0.3231
0.500 0.7171 0.01149 0.00443 -0.1423 0.5180 0.3282
0.750 0.7460 0.01152 0.00447 -0.1423 0.5132 0.3328
1.000 0.7743 0.01158 0.00450 -0.1422 0.5079 0.3367
1.250 0.8029 0.01164 0.00454 -0.1421 0.5026 0.3396
1.500 0.8314 0.01169 0.00459 -0.1421 0.4961 0.3423
1.750 0.8592 0.01174 0.00464 -0.1419 0.4898 0.3469
2.000 0.8871 0.01181 0.00472 -0.1418 0.4844 0.3514
2.250 0.9149 0.01188 0.00480 -0.1417 0.4769 0.3556
2.500 0.9408 0.01202 0.00489 -0.1412 0.4679 0.3596
2.750 0.9676 0.01214 0.00500 -0.1409 0.4583 0.3633
3.000 0.9926 0.01232 0.00513 -0.1403 0.4485 0.3675
3.250 1.0181 0.01247 0.00528 -0.1398 0.4379 0.3734
3.500 1.0428 0.01266 0.00545 -0.1392 0.4295 0.3789
3.750 1.0675 0.01286 0.00563 -0.1385 0.4198 0.3838
4.000 1.0906 0.01311 0.00584 -0.1377 0.4100 0.3881
4.250 1.1131 0.01338 0.00607 -0.1367 0.3989 0.3924
4.500 1.1349 0.01364 0.00632 -0.1356 0.3886 0.3986
4.750 1.1525 0.01397 0.00662 -0.1339 0.3771 0.4051
5.000 1.1716 0.01429 0.00692 -0.1324 0.3645 0.4116
5.500 1.2036 0.01538 0.00787 -0.1288 0.3290 0.4247
5.750 1.2145 0.01620 0.00858 -0.1264 0.3052 0.4319
6.000 1.2229 0.01716 0.00943 -0.1239 0.2793 0.4389
6.250 1.2307 0.01822 0.01037 -0.1214 0.2585 0.4454
6.500 1.2409 0.01919 0.01131 -0.1194 0.2440 0.4544
6.750 1.2529 0.02012 0.01223 -0.1176 0.2340 0.4639
7.000 1.2647 0.02111 0.01321 -0.1160 0.2258 0.4727
7.250 1.2785 0.02203 0.01416 -0.1147 0.2201 0.4842
7.500 1.2919 0.02301 0.01516 -0.1134 0.2150 0.4962
7.750 1.3040 0.02413 0.01632 -0.1122 0.2103 0.5088
8.000 1.3170 0.02522 0.01745 -0.1110 0.2068 0.5223
8.250 1.3311 0.02628 0.01857 -0.1101 0.2037 0.5352
8.500 1.3441 0.02744 0.01977 -0.1091 0.2004 0.5480
8.750 1.3548 0.02880 0.02119 -0.1080 0.1972 0.5591
9.000 1.3638 0.03034 0.02275 -0.1069 0.1938 0.5711
9.250 1.3759 0.03165 0.02411 -0.1060 0.1911 0.5821
9.500 1.3884 0.03296 0.02549 -0.1053 0.1887 0.5947
9.750 1.4001 0.03433 0.02693 -0.1044 0.1864 0.6069
10.000 1.4102 0.03587 0.02853 -0.1036 0.1842 0.6212
10.250 1.4198 0.03746 0.03019 -0.1028 0.1822 0.6353
10.500 1.4277 0.03924 0.03203 -0.1019 0.1801 0.6510
10.750 1.4359 0.04098 0.03384 -0.1011 0.1782 0.6683
11.000 1.4471 0.04249 0.03545 -0.1004 0.1769 0.6877
11.250 1.4584 0.04397 0.03703 -0.0997 0.1754 0.7101
11.500 1.4694 0.04546 0.03863 -0.0991 0.1738 0.7356
11.750 1.4786 0.04716 0.04043 -0.0984 0.1721 0.7637
12.000 1.4878 0.04883 0.04222 -0.0977 0.1704 0.7959
12.250 1.4955 0.05046 0.04401 -0.0967 0.1685 0.8561
12.500 1.4978 0.05237 0.04603 -0.0954 0.1664 1.0000
12.750 1.5042 0.05442 0.04809 -0.0948 0.1643 1.0000
13.000 1.5157 0.05599 0.04970 -0.0943 0.1629 1.0000
13.250 1.5249 0.05781 0.05156 -0.0939 0.1615 1.0000
13.500 1.5344 0.05960 0.05338 -0.0934 0.1598 1.0000
13.750 1.5434 0.06141 0.05522 -0.0929 0.1580 1.0000
14.000 1.5509 0.06342 0.05725 -0.0925 0.1563 1.0000
14.250 1.5567 0.06562 0.05947 -0.0920 0.1544 1.0000
14.500 1.5623 0.06785 0.06170 -0.0916 0.1524 1.0000
14.750 1.5713 0.06972 0.06361 -0.0912 0.1504 1.0000
15.000 1.5791 0.07174 0.06567 -0.0909 0.1484 1.0000
15.250 1.5866 0.07377 0.06773 -0.0906 0.1462 1.0000
15.500 1.5930 0.07593 0.06991 -0.0903 0.1438 1.0000
15.750 1.5960 0.07853 0.07253 -0.0900 0.1414 1.0000
16.000 1.6019 0.08078 0.07481 -0.0898 0.1394 1.0000
16.250 1.6098 0.08279 0.07686 -0.0896 0.1370 1.0000
16.500 1.6149 0.08515 0.07926 -0.0894 0.1342 1.0000
16.750 1.6175 0.08782 0.08195 -0.0893 0.1313 1.0000
17.000 1.6216 0.09029 0.08444 -0.0892 0.1286 1.0000
17.250 1.6257 0.09282 0.08701 -0.0892 0.1252 1.0000
17.500 1.6269 0.09569 0.08990 -0.0892 0.1214 1.0000
17.750 1.6294 0.09839 0.09262 -0.0893 0.1176 1.0000
18.000 1.6284 0.10157 0.09582 -0.0895 0.1128 1.0000
18.250 1.6281 0.10463 0.09889 -0.0897 0.1080 1.0000
18.750 1.6216 0.11163 0.10590 -0.0905 0.0977 1.0000
19.000 1.6168 0.11538 0.10967 -0.0911 0.0936 1.0000
19.250 1.6144 0.11880 0.11311 -0.0917 0.0903 1.0000
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