GOE 424 AIRFOIL (goe424-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 424 AIRFOIL (goe424-il) Reynolds number: 1,000,000 Max Cl/Cd: 124.15 at α=7.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe424-il-1000000.txt Download as CSV file: xf-goe424-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 424 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.8208 0.09476 0.09208 -0.0771 1.0000 0.0185
-19.250 -0.8582 0.08499 0.08214 -0.0828 1.0000 0.0186
-19.000 -0.8826 0.07764 0.07466 -0.0871 1.0000 0.0187
-18.750 -0.8985 0.07181 0.06873 -0.0905 1.0000 0.0189
-18.500 -0.9093 0.06684 0.06367 -0.0934 1.0000 0.0190
-18.250 -0.9166 0.06251 0.05927 -0.0958 1.0000 0.0192
-18.000 -0.9204 0.05878 0.05547 -0.0979 1.0000 0.0193
-17.750 -0.9227 0.05535 0.05199 -0.0996 1.0000 0.0195
-17.500 -0.9242 0.05221 0.04878 -0.1011 1.0000 0.0197
-17.250 -0.9258 0.04933 0.04584 -0.1022 1.0000 0.0199
-17.000 -0.9289 0.04663 0.04307 -0.1028 1.0000 0.0200
-16.750 -0.9345 0.04418 0.04056 -0.1026 1.0000 0.0202
-16.500 -0.9427 0.04199 0.03830 -0.1015 1.0000 0.0204
-16.250 -0.9464 0.03984 0.03607 -0.1010 0.9996 0.0206
-16.000 -0.9320 0.03746 0.03359 -0.1036 0.9980 0.0209
-15.750 -0.9159 0.03528 0.03130 -0.1061 0.9961 0.0212
-15.500 -0.8965 0.03338 0.02929 -0.1087 0.9944 0.0215
-15.250 -0.8816 0.03106 0.02685 -0.1111 0.9927 0.0218
-15.000 -0.8663 0.02924 0.02499 -0.1127 0.9892 0.0222
-14.750 -0.8457 0.02803 0.02376 -0.1142 0.9857 0.0225
-14.500 -0.8231 0.02701 0.02270 -0.1156 0.9823 0.0228
-14.250 -0.8060 0.02612 0.02178 -0.1158 0.9763 0.0231
-14.000 -0.7892 0.02531 0.02092 -0.1157 0.9699 0.0235
-13.750 -0.7757 0.02456 0.02012 -0.1147 0.9621 0.0238
-13.500 -0.7631 0.02383 0.01930 -0.1134 0.9541 0.0242
-13.250 -0.7502 0.02313 0.01852 -0.1121 0.9451 0.0246
-13.000 -0.7366 0.02250 0.01780 -0.1106 0.9362 0.0249
-12.750 -0.7217 0.02195 0.01715 -0.1092 0.9254 0.0252
-12.500 -0.7114 0.02076 0.01586 -0.1074 0.9140 0.0257
-12.250 -0.6955 0.02022 0.01528 -0.1060 0.9006 0.0261
-12.000 -0.6783 0.01985 0.01484 -0.1047 0.8835 0.0264
-11.750 -0.6607 0.01955 0.01445 -0.1032 0.8626 0.0267
-11.500 -0.6440 0.01932 0.01409 -0.1016 0.8397 0.0271
-11.250 -0.6251 0.01910 0.01373 -0.1003 0.8172 0.0276
-11.000 -0.6051 0.01883 0.01333 -0.0992 0.7942 0.0281
-10.750 -0.5848 0.01857 0.01291 -0.0982 0.7697 0.0286
-10.500 -0.5640 0.01834 0.01251 -0.0971 0.7408 0.0290
-10.250 -0.5447 0.01788 0.01185 -0.0960 0.7060 0.0294
-10.000 -0.5261 0.01735 0.01117 -0.0948 0.6723 0.0300
-9.750 -0.5045 0.01719 0.01090 -0.0939 0.6473 0.0304
-9.500 -0.4817 0.01708 0.01070 -0.0932 0.6302 0.0309
-9.250 -0.4583 0.01694 0.01048 -0.0926 0.6176 0.0314
-9.000 -0.4351 0.01674 0.01019 -0.0919 0.6071 0.0320
-8.750 -0.4114 0.01645 0.00983 -0.0914 0.5987 0.0326
-8.500 -0.3879 0.01621 0.00949 -0.0907 0.5905 0.0331
-8.250 -0.3630 0.01600 0.00923 -0.0903 0.5847 0.0336
-8.000 -0.3416 0.01534 0.00852 -0.0894 0.5787 0.0343
-7.750 -0.3181 0.01507 0.00822 -0.0888 0.5726 0.0349
-7.500 -0.2931 0.01483 0.00797 -0.0884 0.5684 0.0355
-7.250 -0.2682 0.01461 0.00771 -0.0880 0.5636 0.0361
-7.000 -0.2437 0.01439 0.00744 -0.0875 0.5588 0.0367
-6.750 -0.2190 0.01420 0.00720 -0.0870 0.5542 0.0374
-6.500 -0.1932 0.01400 0.00698 -0.0867 0.5512 0.0381
-6.250 -0.1672 0.01385 0.00678 -0.0864 0.5478 0.0386
-6.000 -0.1455 0.01331 0.00622 -0.0855 0.5445 0.0393
-5.750 -0.1221 0.01300 0.00589 -0.0848 0.5411 0.0400
-5.500 -0.0977 0.01283 0.00569 -0.0842 0.5371 0.0407
-5.250 -0.0716 0.01264 0.00550 -0.0840 0.5350 0.0416
-5.000 -0.0456 0.01247 0.00532 -0.0837 0.5326 0.0425
-4.750 -0.0198 0.01228 0.00511 -0.0834 0.5299 0.0432
-4.500 0.0061 0.01214 0.00494 -0.0831 0.5270 0.0439
-4.250 0.0323 0.01205 0.00482 -0.0828 0.5242 0.0444
-4.000 0.0545 0.01167 0.00439 -0.0819 0.5213 0.0456
-3.750 0.0801 0.01152 0.00423 -0.0815 0.5187 0.0468
-3.500 0.1067 0.01137 0.00409 -0.0814 0.5171 0.0480
-3.250 0.1334 0.01124 0.00395 -0.0812 0.5153 0.0491
-3.000 0.1602 0.01113 0.00382 -0.0810 0.5132 0.0501
-2.750 0.1872 0.01105 0.00373 -0.0809 0.5109 0.0508
-2.500 0.2125 0.01083 0.00348 -0.0805 0.5087 0.0528
-2.250 0.2387 0.01074 0.00337 -0.0803 0.5064 0.0546
-2.000 0.2652 0.01070 0.00330 -0.0801 0.5038 0.0565
-1.750 0.2922 0.01068 0.00326 -0.0800 0.5015 0.0579
-1.500 0.3192 0.01055 0.00315 -0.0799 0.5003 0.0612
-1.250 0.3464 0.01046 0.00306 -0.0799 0.4986 0.0648
-1.000 0.3729 0.01031 0.00299 -0.0798 0.4968 0.0840
-0.750 0.3897 0.00926 0.00277 -0.0783 0.4951 0.3402
-0.500 0.4141 0.00896 0.00276 -0.0779 0.4934 0.4299
-0.250 0.4396 0.00879 0.00277 -0.0776 0.4915 0.4864
0.000 0.4653 0.00867 0.00280 -0.0773 0.4895 0.5388
0.250 0.4915 0.00864 0.00285 -0.0772 0.4871 0.5782
0.500 0.5184 0.00866 0.00294 -0.0771 0.4846 0.6092
0.750 0.5458 0.00861 0.00297 -0.0772 0.4834 0.6343
1.000 0.5729 0.00857 0.00301 -0.0771 0.4820 0.6591
1.250 0.5999 0.00853 0.00306 -0.0771 0.4803 0.6875
1.500 0.6267 0.00849 0.00311 -0.0770 0.4785 0.7154
1.750 0.6537 0.00848 0.00317 -0.0770 0.4766 0.7392
2.000 0.6804 0.00847 0.00323 -0.0769 0.4746 0.7648
2.250 0.7066 0.00848 0.00331 -0.0766 0.4726 0.7916
2.500 0.7327 0.00854 0.00341 -0.0764 0.4699 0.8181
2.750 0.7584 0.00858 0.00354 -0.0761 0.4672 0.8487
3.000 0.7840 0.00855 0.00360 -0.0757 0.4650 0.8744
3.250 0.8097 0.00855 0.00366 -0.0753 0.4621 0.8942
3.500 0.8353 0.00858 0.00373 -0.0749 0.4593 0.9113
3.750 0.8606 0.00865 0.00382 -0.0745 0.4568 0.9268
4.000 0.8861 0.00875 0.00393 -0.0741 0.4544 0.9421
4.250 0.9130 0.00892 0.00408 -0.0741 0.4516 0.9565
4.500 0.9424 0.00902 0.00420 -0.0746 0.4500 0.9684
4.750 0.9752 0.00911 0.00432 -0.0759 0.4481 0.9765
5.000 1.0088 0.00921 0.00443 -0.0775 0.4457 0.9826
5.250 1.0448 0.00932 0.00455 -0.0796 0.4429 0.9865
5.500 1.0804 0.00947 0.00467 -0.0816 0.4401 0.9903
5.750 1.1162 0.00965 0.00483 -0.0837 0.4370 0.9935
6.000 1.1551 0.00983 0.00500 -0.0866 0.4340 0.9958
6.250 1.1946 0.00993 0.00513 -0.0895 0.4310 0.9983
6.500 1.2268 0.01002 0.00525 -0.0908 0.4275 1.0000
6.750 1.2304 0.01003 0.00526 -0.0861 0.4245 1.0000
7.000 1.2388 0.01011 0.00532 -0.0825 0.4214 1.0000
7.250 1.2535 0.01024 0.00544 -0.0802 0.4179 1.0000
7.500 1.2744 0.01030 0.00555 -0.0791 0.4143 1.0000
7.750 1.2949 0.01043 0.00568 -0.0781 0.4097 1.0000
8.000 1.3142 0.01062 0.00586 -0.0768 0.4051 1.0000
8.250 1.3359 0.01080 0.00604 -0.0761 0.4010 1.0000
8.500 1.3588 0.01095 0.00622 -0.0756 0.3963 1.0000
8.750 1.3792 0.01118 0.00645 -0.0747 0.3907 1.0000
9.000 1.3999 0.01143 0.00670 -0.0739 0.3848 1.0000
9.250 1.4208 0.01169 0.00696 -0.0732 0.3773 1.0000
9.500 1.4391 0.01204 0.00729 -0.0720 0.3694 1.0000
9.750 1.4566 0.01245 0.00767 -0.0708 0.3587 1.0000
10.000 1.4730 0.01291 0.00810 -0.0695 0.3467 1.0000
10.250 1.4877 0.01347 0.00862 -0.0680 0.3347 1.0000
10.500 1.5006 0.01414 0.00924 -0.0663 0.3225 1.0000
10.750 1.5121 0.01489 0.00995 -0.0644 0.3102 1.0000
11.000 1.5253 0.01560 0.01063 -0.0629 0.2993 1.0000
11.250 1.5371 0.01640 0.01141 -0.0613 0.2894 1.0000
11.500 1.5457 0.01740 0.01237 -0.0594 0.2787 1.0000
11.750 1.5553 0.01839 0.01335 -0.0577 0.2682 1.0000
12.000 1.5639 0.01949 0.01444 -0.0561 0.2591 1.0000
12.250 1.5698 0.02080 0.01573 -0.0543 0.2503 1.0000
12.500 1.5795 0.02194 0.01688 -0.0530 0.2435 1.0000
12.750 1.5843 0.02345 0.01839 -0.0514 0.2362 1.0000
13.000 1.5916 0.02486 0.01983 -0.0502 0.2297 1.0000
13.250 1.5947 0.02663 0.02161 -0.0487 0.2227 1.0000
13.500 1.5980 0.02848 0.02347 -0.0475 0.2162 1.0000
13.750 1.6001 0.03052 0.02552 -0.0463 0.2095 1.0000
14.000 1.5988 0.03291 0.02793 -0.0451 0.2036 1.0000
14.250 1.6024 0.03495 0.03002 -0.0443 0.1982 1.0000
14.500 1.5987 0.03772 0.03281 -0.0432 0.1924 1.0000
14.750 1.5991 0.04017 0.03530 -0.0425 0.1876 1.0000
15.000 1.5991 0.04268 0.03786 -0.0418 0.1824 1.0000
15.250 1.5920 0.04589 0.04108 -0.0409 0.1767 1.0000
15.500 1.5907 0.04857 0.04380 -0.0403 0.1710 1.0000
15.750 1.5817 0.05203 0.04727 -0.0395 0.1638 1.0000
16.000 1.5761 0.05517 0.05044 -0.0389 0.1568 1.0000
16.250 1.5642 0.05900 0.05425 -0.0382 0.1487 1.0000
16.500 1.5559 0.06250 0.05775 -0.0377 0.1397 1.0000
16.750 1.5456 0.06623 0.06147 -0.0372 0.1315 1.0000
17.000 1.5321 0.07037 0.06560 -0.0367 0.1229 1.0000
17.250 1.5216 0.07426 0.06949 -0.0364 0.1149 1.0000
17.500 1.5137 0.07789 0.07312 -0.0362 0.1076 1.0000
18.000 1.4964 0.08543 0.08065 -0.0361 0.0934 1.0000
18.250 1.4852 0.08962 0.08483 -0.0362 0.0843 1.0000
18.500 1.4610 0.09537 0.09047 -0.0363 0.0657 1.0000
18.750 1.4338 0.10162 0.09662 -0.0367 0.0495 1.0000
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