GOE 424 AIRFOIL (goe424-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 424 AIRFOIL (goe424-il) Reynolds number: 1,000,000 Max Cl/Cd: 117.47 at α=6.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe424-il-1000000-n5.txt Download as CSV file: xf-goe424-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9788 0.07421 0.07086 -0.0889 1.0000 0.0134
-19.500 -0.9966 0.06830 0.06484 -0.0922 1.0000 0.0136
-19.250 -1.0100 0.06320 0.05964 -0.0950 1.0000 0.0137
-19.000 -1.0209 0.05859 0.05494 -0.0974 1.0000 0.0139
-18.750 -1.0283 0.05456 0.05082 -0.0995 1.0000 0.0141
-18.500 -1.0339 0.05090 0.04707 -0.1012 1.0000 0.0143
-18.250 -1.0375 0.04763 0.04373 -0.1025 1.0000 0.0145
-18.000 -1.0396 0.04468 0.04071 -0.1036 1.0000 0.0148
-17.750 -1.0412 0.04199 0.03795 -0.1043 1.0000 0.0150
-17.500 -1.0349 0.03942 0.03530 -0.1060 0.9967 0.0153
-17.250 -1.0249 0.03701 0.03281 -0.1080 0.9931 0.0156
-17.000 -1.0153 0.03484 0.03055 -0.1095 0.9880 0.0159
-16.750 -1.0035 0.03285 0.02848 -0.1109 0.9833 0.0161
-16.500 -0.9928 0.03101 0.02657 -0.1119 0.9772 0.0165
-16.250 -0.9813 0.02939 0.02490 -0.1125 0.9707 0.0168
-16.000 -0.9706 0.02797 0.02343 -0.1125 0.9638 0.0172
-15.750 -0.9598 0.02670 0.02209 -0.1122 0.9560 0.0175
-15.500 -0.9489 0.02554 0.02087 -0.1116 0.9471 0.0179
-15.250 -0.9376 0.02448 0.01973 -0.1108 0.9379 0.0183
-15.000 -0.9257 0.02349 0.01866 -0.1100 0.9270 0.0187
-14.750 -0.9127 0.02258 0.01766 -0.1092 0.9165 0.0190
-14.500 -0.8994 0.02175 0.01674 -0.1082 0.9036 0.0193
-14.250 -0.8847 0.02105 0.01597 -0.1072 0.8857 0.0198
-14.000 -0.8692 0.02047 0.01528 -0.1061 0.8627 0.0202
-13.750 -0.8528 0.01997 0.01466 -0.1050 0.8385 0.0207
-13.500 -0.8359 0.01949 0.01405 -0.1039 0.8158 0.0212
-13.250 -0.8186 0.01903 0.01346 -0.1029 0.7940 0.0216
-13.000 -0.8012 0.01860 0.01288 -0.1017 0.7717 0.0220
-12.750 -0.7834 0.01819 0.01232 -0.1006 0.7460 0.0224
-12.500 -0.7659 0.01783 0.01182 -0.0993 0.7143 0.0228
-12.250 -0.7483 0.01758 0.01143 -0.0979 0.6798 0.0232
-12.000 -0.7303 0.01740 0.01113 -0.0965 0.6528 0.0236
-11.750 -0.7101 0.01720 0.01083 -0.0955 0.6333 0.0241
-11.500 -0.6886 0.01697 0.01051 -0.0947 0.6192 0.0246
-11.250 -0.6669 0.01671 0.01017 -0.0938 0.6080 0.0251
-11.000 -0.6450 0.01643 0.00982 -0.0931 0.5985 0.0255
-10.750 -0.6228 0.01616 0.00946 -0.0923 0.5906 0.0259
-10.500 -0.6004 0.01587 0.00911 -0.0916 0.5836 0.0263
-10.250 -0.5777 0.01561 0.00881 -0.0909 0.5764 0.0268
-10.000 -0.5537 0.01540 0.00857 -0.0903 0.5706 0.0272
-9.750 -0.5296 0.01519 0.00833 -0.0898 0.5645 0.0277
-9.500 -0.5055 0.01500 0.00808 -0.0893 0.5585 0.0282
-9.250 -0.4811 0.01479 0.00784 -0.0888 0.5541 0.0287
-9.000 -0.4564 0.01458 0.00758 -0.0883 0.5500 0.0292
-8.750 -0.4320 0.01436 0.00731 -0.0879 0.5457 0.0296
-8.500 -0.4073 0.01417 0.00706 -0.0874 0.5415 0.0300
-8.250 -0.3837 0.01390 0.00675 -0.0868 0.5376 0.0305
-8.000 -0.3588 0.01367 0.00652 -0.0863 0.5348 0.0310
-7.750 -0.3334 0.01348 0.00631 -0.0860 0.5316 0.0314
-7.500 -0.3078 0.01332 0.00613 -0.0856 0.5283 0.0320
-7.250 -0.2823 0.01316 0.00594 -0.0853 0.5250 0.0325
-7.000 -0.2571 0.01299 0.00572 -0.0849 0.5216 0.0330
-6.750 -0.2317 0.01282 0.00551 -0.0845 0.5187 0.0334
-6.500 -0.2058 0.01264 0.00530 -0.0842 0.5162 0.0339
-6.250 -0.1797 0.01249 0.00512 -0.0839 0.5135 0.0343
-6.000 -0.1545 0.01228 0.00489 -0.0835 0.5110 0.0349
-5.750 -0.1289 0.01211 0.00471 -0.0832 0.5085 0.0355
-5.500 -0.1029 0.01197 0.00455 -0.0829 0.5059 0.0360
-5.250 -0.0769 0.01186 0.00441 -0.0826 0.5034 0.0365
-5.000 -0.0506 0.01174 0.00427 -0.0824 0.5013 0.0371
-4.750 -0.0240 0.01160 0.00413 -0.0822 0.4997 0.0377
-4.500 0.0028 0.01149 0.00400 -0.0820 0.4978 0.0384
-4.250 0.0296 0.01139 0.00388 -0.0819 0.4955 0.0390
-4.000 0.0560 0.01126 0.00373 -0.0817 0.4933 0.0397
-3.750 0.0824 0.01114 0.00361 -0.0815 0.4911 0.0405
-3.500 0.1089 0.01105 0.00351 -0.0813 0.4891 0.0413
-3.250 0.1356 0.01098 0.00342 -0.0811 0.4871 0.0421
-3.000 0.1621 0.01092 0.00334 -0.0809 0.4849 0.0430
-2.750 0.1893 0.01085 0.00326 -0.0809 0.4835 0.0439
-2.500 0.2167 0.01078 0.00320 -0.0809 0.4820 0.0446
-2.250 0.2436 0.01068 0.00310 -0.0807 0.4803 0.0461
-2.000 0.2707 0.01061 0.00304 -0.0807 0.4785 0.0474
-1.750 0.2979 0.01055 0.00298 -0.0806 0.4768 0.0487
-1.500 0.3251 0.01051 0.00293 -0.0806 0.4751 0.0499
-1.250 0.3521 0.01047 0.00289 -0.0805 0.4732 0.0512
-1.000 0.3788 0.01043 0.00284 -0.0804 0.4713 0.0534
-0.750 0.4055 0.01041 0.00281 -0.0803 0.4691 0.0560
-0.500 0.4322 0.01040 0.00279 -0.0802 0.4671 0.0591
-0.250 0.4596 0.01033 0.00277 -0.0802 0.4661 0.0664
0.000 0.4828 0.00984 0.00268 -0.0797 0.4648 0.2064
0.250 0.5064 0.00942 0.00261 -0.0792 0.4632 0.3187
0.500 0.5314 0.00917 0.00262 -0.0790 0.4615 0.4003
0.750 0.5582 0.00910 0.00264 -0.0789 0.4597 0.4311
1.000 0.5849 0.00904 0.00267 -0.0789 0.4579 0.4609
1.250 0.6111 0.00897 0.00271 -0.0788 0.4559 0.4976
1.500 0.6372 0.00892 0.00276 -0.0786 0.4538 0.5377
1.750 0.6632 0.00890 0.00283 -0.0785 0.4517 0.5703
2.000 0.6897 0.00887 0.00289 -0.0784 0.4499 0.6036
2.250 0.7169 0.00884 0.00295 -0.0785 0.4483 0.6322
2.500 0.7441 0.00884 0.00301 -0.0785 0.4459 0.6527
2.750 0.7708 0.00884 0.00308 -0.0785 0.4428 0.6744
3.000 0.7967 0.00884 0.00315 -0.0783 0.4391 0.7004
3.250 0.8218 0.00888 0.00324 -0.0780 0.4351 0.7279
3.500 0.8483 0.00889 0.00332 -0.0780 0.4322 0.7505
3.750 0.8747 0.00890 0.00341 -0.0779 0.4294 0.7747
4.000 0.9003 0.00892 0.00351 -0.0776 0.4266 0.7999
4.250 0.9250 0.00895 0.00362 -0.0772 0.4238 0.8261
4.500 0.9488 0.00899 0.00374 -0.0766 0.4212 0.8526
4.750 0.9721 0.00907 0.00387 -0.0758 0.4185 0.8770
5.000 0.9971 0.00913 0.00399 -0.0755 0.4164 0.8962
5.250 1.0221 0.00920 0.00412 -0.0751 0.4139 0.9137
5.500 1.0468 0.00930 0.00426 -0.0747 0.4106 0.9314
5.750 1.0716 0.00943 0.00442 -0.0743 0.4067 0.9502
6.000 1.0989 0.00962 0.00460 -0.0746 0.4024 0.9683
6.250 1.1317 0.00976 0.00476 -0.0760 0.3981 0.9816
6.500 1.1644 0.00996 0.00494 -0.0776 0.3912 0.9914
6.750 1.1970 0.01019 0.00514 -0.0792 0.3836 0.9988
7.000 1.2169 0.01038 0.00531 -0.0781 0.3758 1.0000
7.250 1.2351 0.01060 0.00551 -0.0766 0.3695 1.0000
7.500 1.2556 0.01081 0.00570 -0.0757 0.3629 1.0000
7.750 1.2742 0.01111 0.00597 -0.0744 0.3557 1.0000
8.000 1.2947 0.01137 0.00622 -0.0735 0.3483 1.0000
8.250 1.3128 0.01173 0.00655 -0.0723 0.3396 1.0000
8.500 1.3309 0.01212 0.00690 -0.0711 0.3294 1.0000
8.750 1.3477 0.01258 0.00732 -0.0698 0.3182 1.0000
9.000 1.3630 0.01311 0.00780 -0.0683 0.3073 1.0000
9.250 1.3792 0.01362 0.00829 -0.0669 0.2974 1.0000
9.500 1.3958 0.01413 0.00878 -0.0657 0.2894 1.0000
9.750 1.4097 0.01478 0.00940 -0.0642 0.2799 1.0000
10.000 1.4231 0.01547 0.01006 -0.0627 0.2688 1.0000
10.250 1.4331 0.01637 0.01090 -0.0608 0.2558 1.0000
10.500 1.4429 0.01731 0.01180 -0.0590 0.2452 1.0000
10.750 1.4540 0.01821 0.01269 -0.0574 0.2363 1.0000
11.000 1.4642 0.01922 0.01368 -0.0559 0.2283 1.0000
11.250 1.4734 0.02033 0.01478 -0.0544 0.2203 1.0000
11.500 1.4833 0.02143 0.01589 -0.0531 0.2145 1.0000
11.750 1.4939 0.02255 0.01702 -0.0520 0.2087 1.0000
12.000 1.5003 0.02400 0.01847 -0.0505 0.2027 1.0000
12.250 1.5102 0.02526 0.01976 -0.0496 0.1985 1.0000
12.500 1.5184 0.02669 0.02122 -0.0485 0.1936 1.0000
12.750 1.5222 0.02852 0.02307 -0.0473 0.1883 1.0000
13.000 1.5277 0.03030 0.02487 -0.0464 0.1829 1.0000
13.250 1.5281 0.03257 0.02715 -0.0453 0.1756 1.0000
13.500 1.5277 0.03499 0.02960 -0.0442 0.1690 1.0000
13.750 1.5251 0.03769 0.03230 -0.0433 0.1612 1.0000
14.000 1.5216 0.04054 0.03517 -0.0424 0.1537 1.0000
14.250 1.5123 0.04397 0.03859 -0.0413 0.1448 1.0000
14.500 1.5025 0.04750 0.04212 -0.0404 0.1350 1.0000
14.750 1.4931 0.05103 0.04566 -0.0396 0.1266 1.0000
15.000 1.4830 0.05464 0.04927 -0.0388 0.1192 1.0000
15.250 1.4758 0.05803 0.05267 -0.0381 0.1126 1.0000
15.500 1.4702 0.06127 0.05592 -0.0376 0.1070 1.0000
15.750 1.4648 0.06456 0.05923 -0.0373 0.1017 1.0000
16.000 1.4589 0.06791 0.06259 -0.0369 0.0966 1.0000
16.250 1.4561 0.07097 0.06568 -0.0367 0.0910 1.0000
16.500 1.4494 0.07450 0.06921 -0.0365 0.0852 1.0000
16.750 1.4417 0.07816 0.07285 -0.0363 0.0756 1.0000
17.000 1.4142 0.08413 0.07870 -0.0360 0.0547 1.0000
17.250 1.3983 0.08893 0.08349 -0.0360 0.0452 1.0000
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