GOE 410 AIRFOIL (goe410-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 410 AIRFOIL (goe410-il) Reynolds number: 500,000 Max Cl/Cd: 65.15 at α=9.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe410-il-500000-n5.txt Download as CSV file: xf-goe410-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 410 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 -1.2202 0.10801 0.10361 -0.0049 1.0000 0.0354
-19.500 -1.2349 0.10188 0.09739 -0.0082 1.0000 0.0358
-19.250 -1.2499 0.09584 0.09126 -0.0113 1.0000 0.0364
-19.000 -1.2619 0.09041 0.08573 -0.0140 1.0000 0.0369
-18.750 -1.2723 0.08533 0.08056 -0.0165 1.0000 0.0376
-18.500 -1.2805 0.08070 0.07585 -0.0186 1.0000 0.0382
-18.250 -1.2874 0.07635 0.07140 -0.0205 1.0000 0.0390
-18.000 -1.2927 0.07231 0.06727 -0.0222 1.0000 0.0396
-17.750 -1.3008 0.06798 0.06287 -0.0240 1.0000 0.0404
-17.500 -1.3082 0.06385 0.05867 -0.0257 1.0000 0.0414
-17.250 -1.3128 0.06018 0.05494 -0.0270 1.0000 0.0424
-17.000 -1.3166 0.05674 0.05142 -0.0282 1.0000 0.0436
-16.500 -1.3222 0.05034 0.04490 -0.0301 1.0000 0.0460
-16.250 -1.3239 0.04740 0.04190 -0.0308 1.0000 0.0475
-16.000 -1.3235 0.04471 0.03916 -0.0314 1.0000 0.0494
-15.750 -1.3225 0.04211 0.03651 -0.0319 1.0000 0.0512
-15.500 -1.3202 0.03969 0.03405 -0.0323 1.0000 0.0532
-15.250 -1.3154 0.03757 0.03187 -0.0325 1.0000 0.0554
-15.000 -1.3108 0.03546 0.02971 -0.0327 1.0000 0.0571
-14.750 -1.3053 0.03349 0.02770 -0.0328 1.0000 0.0589
-14.500 -1.2976 0.03179 0.02594 -0.0327 1.0000 0.0609
-14.250 -1.2882 0.03029 0.02436 -0.0325 1.0000 0.0626
-14.000 -1.2814 0.02862 0.02267 -0.0322 1.0000 0.0641
-13.750 -1.2728 0.02719 0.02120 -0.0318 1.0000 0.0659
-13.500 -1.2626 0.02594 0.01990 -0.0312 1.0000 0.0676
-13.250 -1.2508 0.02489 0.01878 -0.0305 1.0000 0.0693
-13.000 -1.2406 0.02379 0.01763 -0.0296 1.0000 0.0705
-12.750 -1.2320 0.02269 0.01650 -0.0284 1.0000 0.0719
-12.500 -1.2220 0.02179 0.01557 -0.0271 1.0000 0.0732
-12.250 -1.2108 0.02102 0.01476 -0.0255 1.0000 0.0747
-12.000 -1.1988 0.02037 0.01407 -0.0238 1.0000 0.0760
-11.750 -1.1857 0.01983 0.01347 -0.0220 1.0000 0.0773
-11.500 -1.1728 0.01933 0.01292 -0.0200 1.0000 0.0785
-11.250 -1.1611 0.01875 0.01233 -0.0178 1.0000 0.0799
-11.000 -1.1447 0.01823 0.01181 -0.0163 1.0000 0.0814
-10.750 -1.1265 0.01777 0.01133 -0.0149 1.0000 0.0828
-10.500 -1.1071 0.01735 0.01088 -0.0138 1.0000 0.0842
-10.250 -1.0868 0.01695 0.01045 -0.0127 1.0000 0.0856
-10.000 -1.0656 0.01659 0.01005 -0.0117 1.0000 0.0869
-9.750 -1.0453 0.01616 0.00962 -0.0106 1.0000 0.0886
-9.500 -1.0244 0.01575 0.00922 -0.0096 1.0000 0.0907
-9.250 -1.0025 0.01539 0.00887 -0.0087 1.0000 0.0930
-9.000 -0.9801 0.01507 0.00853 -0.0078 1.0000 0.0951
-8.750 -0.9573 0.01477 0.00821 -0.0069 1.0000 0.0969
-8.500 -0.9229 0.01434 0.00781 -0.0086 0.9701 0.1000
-8.250 -0.8802 0.01397 0.00743 -0.0118 0.9308 0.1038
-8.000 -0.8502 0.01377 0.00710 -0.0121 0.8797 0.1068
-7.750 -0.8275 0.01359 0.00680 -0.0110 0.8437 0.1092
-7.500 -0.8042 0.01338 0.00651 -0.0101 0.8196 0.1122
-7.250 -0.7800 0.01319 0.00624 -0.0093 0.7992 0.1153
-7.000 -0.7550 0.01302 0.00600 -0.0086 0.7800 0.1184
-6.750 -0.7301 0.01284 0.00574 -0.0080 0.7612 0.1215
-6.500 -0.7050 0.01263 0.00549 -0.0074 0.7432 0.1254
-6.250 -0.6793 0.01246 0.00526 -0.0069 0.7243 0.1292
-6.000 -0.6531 0.01234 0.00505 -0.0064 0.7043 0.1326
-5.750 -0.6276 0.01213 0.00480 -0.0059 0.6843 0.1371
-5.500 -0.6017 0.01197 0.00457 -0.0055 0.6647 0.1415
-5.000 -0.5486 0.01172 0.00417 -0.0047 0.6272 0.1491
-4.500 -0.4956 0.01140 0.00377 -0.0039 0.5959 0.1595
-4.250 -0.4687 0.01125 0.00359 -0.0036 0.5833 0.1653
-3.750 -0.4158 0.01081 0.00319 -0.0030 0.5618 0.1899
-3.500 -0.3912 0.01037 0.00293 -0.0025 0.5526 0.2374
-3.250 -0.3652 0.01006 0.00277 -0.0021 0.5444 0.2773
-3.000 -0.3382 0.00988 0.00266 -0.0019 0.5366 0.3027
-2.750 -0.3108 0.00976 0.00257 -0.0016 0.5301 0.3215
-2.500 -0.2830 0.00963 0.00250 -0.0014 0.5231 0.3387
-2.250 -0.2552 0.00956 0.00244 -0.0012 0.5145 0.3529
-2.000 -0.2273 0.00948 0.00238 -0.0010 0.5060 0.3683
-1.750 -0.1992 0.00942 0.00234 -0.0009 0.4980 0.3832
-1.500 -0.1711 0.00939 0.00232 -0.0007 0.4915 0.3970
-1.250 -0.1427 0.00933 0.00230 -0.0006 0.4861 0.4093
-1.000 -0.1142 0.00930 0.00228 -0.0005 0.4796 0.4194
-0.750 -0.0859 0.00930 0.00227 -0.0003 0.4724 0.4289
-0.500 -0.0571 0.00928 0.00226 -0.0002 0.4641 0.4364
-0.250 -0.0288 0.00928 0.00225 -0.0001 0.4560 0.4434
0.000 0.0000 0.00928 0.00225 0.0000 0.4501 0.4501
0.250 0.0288 0.00928 0.00225 0.0001 0.4434 0.4560
0.500 0.0571 0.00928 0.00226 0.0002 0.4364 0.4641
0.750 0.0859 0.00930 0.00227 0.0003 0.4290 0.4725
1.000 0.1142 0.00930 0.00228 0.0005 0.4194 0.4796
1.250 0.1427 0.00933 0.00230 0.0006 0.4093 0.4861
1.500 0.1711 0.00939 0.00232 0.0007 0.3971 0.4916
1.750 0.1992 0.00942 0.00234 0.0009 0.3830 0.4981
2.000 0.2273 0.00949 0.00238 0.0010 0.3680 0.5058
2.250 0.2552 0.00956 0.00244 0.0012 0.3529 0.5141
2.500 0.2830 0.00964 0.00250 0.0014 0.3385 0.5230
2.750 0.3108 0.00976 0.00257 0.0016 0.3213 0.5301
3.000 0.3382 0.00988 0.00266 0.0019 0.3026 0.5366
3.250 0.3651 0.01007 0.00277 0.0021 0.2771 0.5445
3.500 0.3912 0.01037 0.00293 0.0025 0.2379 0.5526
3.750 0.4158 0.01081 0.00319 0.0030 0.1900 0.5618
4.250 0.4687 0.01125 0.00359 0.0036 0.1653 0.5832
4.500 0.4956 0.01140 0.00377 0.0039 0.1595 0.5959
5.000 0.5486 0.01172 0.00417 0.0047 0.1491 0.6273
5.250 0.5752 0.01184 0.00437 0.0050 0.1454 0.6454
5.500 0.6017 0.01197 0.00457 0.0055 0.1415 0.6649
5.750 0.6276 0.01213 0.00480 0.0059 0.1370 0.6844
6.000 0.6531 0.01234 0.00505 0.0064 0.1326 0.7043
6.250 0.6793 0.01246 0.00526 0.0069 0.1292 0.7242
6.500 0.7050 0.01263 0.00549 0.0074 0.1253 0.7432
6.750 0.7301 0.01284 0.00574 0.0080 0.1215 0.7613
7.000 0.7550 0.01302 0.00600 0.0086 0.1184 0.7801
7.250 0.7800 0.01319 0.00624 0.0093 0.1153 0.7993
7.500 0.8042 0.01338 0.00651 0.0101 0.1122 0.8196
7.750 0.8275 0.01359 0.00679 0.0110 0.1092 0.8436
8.000 0.8502 0.01377 0.00710 0.0121 0.1068 0.8797
8.250 0.8801 0.01397 0.00743 0.0118 0.1039 0.9303
8.500 0.9229 0.01434 0.00781 0.0086 0.1000 0.9701
8.750 0.9573 0.01477 0.00821 0.0069 0.0969 1.0000
9.000 0.9802 0.01506 0.00853 0.0078 0.0951 1.0000
9.250 1.0026 0.01539 0.00887 0.0087 0.0930 1.0000
9.500 1.0244 0.01575 0.00922 0.0096 0.0906 1.0000
9.750 1.0454 0.01616 0.00962 0.0106 0.0885 1.0000
10.000 1.0657 0.01659 0.01005 0.0117 0.0868 1.0000
10.250 1.0870 0.01695 0.01045 0.0127 0.0856 1.0000
10.500 1.1073 0.01734 0.01088 0.0137 0.0842 1.0000
10.750 1.1266 0.01777 0.01133 0.0149 0.0828 1.0000
11.000 1.1449 0.01823 0.01180 0.0162 0.0813 1.0000
11.250 1.1613 0.01875 0.01233 0.0177 0.0799 1.0000
11.500 1.1731 0.01933 0.01292 0.0199 0.0785 1.0000
11.750 1.1862 0.01982 0.01346 0.0219 0.0773 1.0000
12.000 1.1992 0.02037 0.01406 0.0237 0.0760 1.0000
12.250 1.2114 0.02101 0.01475 0.0254 0.0746 1.0000
12.500 1.2225 0.02177 0.01555 0.0270 0.0732 1.0000
12.750 1.2326 0.02268 0.01649 0.0284 0.0718 1.0000
13.000 1.2412 0.02378 0.01761 0.0296 0.0705 1.0000
13.250 1.2520 0.02484 0.01873 0.0304 0.0692 1.0000
13.500 1.2633 0.02593 0.01988 0.0311 0.0677 1.0000
13.750 1.2738 0.02715 0.02116 0.0317 0.0659 1.0000
14.000 1.2824 0.02859 0.02264 0.0321 0.0642 1.0000
14.250 1.2892 0.03026 0.02433 0.0324 0.0626 1.0000
14.500 1.2987 0.03175 0.02590 0.0326 0.0609 1.0000
14.750 1.3065 0.03345 0.02766 0.0327 0.0589 1.0000
15.000 1.3122 0.03540 0.02965 0.0326 0.0570 1.0000
15.250 1.3172 0.03748 0.03177 0.0324 0.0551 1.0000
15.500 1.3218 0.03963 0.03398 0.0321 0.0531 1.0000
15.750 1.3241 0.04207 0.03646 0.0317 0.0510 1.0000
16.000 1.3253 0.04464 0.03908 0.0312 0.0493 1.0000
16.250 1.3258 0.04731 0.04181 0.0306 0.0474 1.0000
16.500 1.3242 0.05026 0.04482 0.0299 0.0459 1.0000
16.750 1.3202 0.05354 0.04814 0.0289 0.0445 1.0000
17.000 1.3188 0.05663 0.05131 0.0280 0.0435 1.0000
17.250 1.3154 0.06004 0.05479 0.0268 0.0424 1.0000
17.500 1.3102 0.06377 0.05859 0.0255 0.0413 1.0000
17.750 1.3029 0.06790 0.06279 0.0238 0.0404 1.0000
18.000 1.2949 0.07220 0.06716 0.0220 0.0397 1.0000
18.250 1.2899 0.07621 0.07126 0.0203 0.0389 1.0000
18.500 1.2830 0.08058 0.07571 0.0184 0.0381 1.0000
18.750 1.2745 0.08523 0.08046 0.0163 0.0375 1.0000
19.000 1.2639 0.09036 0.08567 0.0138 0.0368 1.0000
19.250 1.2516 0.09584 0.09125 0.0111 0.0362 1.0000
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