GOE 522 AIRFOIL (goe522-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 522 AIRFOIL (goe522-il) Reynolds number: 1,000,000 Max Cl/Cd: 89.39 at α=6.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe522-il-1000000.txt Download as CSV file: xf-goe522-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 522 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
------ -------- --------- --------- -------- -------- --------
-19.750 -0.7054 0.10566 0.10243 -0.0904 0.9981 0.0284
-19.500 -0.7069 0.10064 0.09733 -0.0946 0.9973 0.0286
-19.250 -0.7073 0.09596 0.09256 -0.0986 0.9965 0.0286
-19.000 -0.7069 0.09147 0.08800 -0.1024 0.9955 0.0287
-18.750 -0.7037 0.08740 0.08384 -0.1060 0.9945 0.0288
-18.500 -0.6985 0.08363 0.08001 -0.1095 0.9935 0.0288
-18.250 -0.6918 0.08012 0.07643 -0.1128 0.9925 0.0288
-18.000 -0.6842 0.07679 0.07304 -0.1160 0.9916 0.0289
-17.750 -0.6812 0.07341 0.06961 -0.1184 0.9895 0.0289
-17.500 -0.6749 0.07024 0.06638 -0.1211 0.9877 0.0291
-17.250 -0.6654 0.06750 0.06360 -0.1235 0.9860 0.0291
-17.000 -0.6554 0.06469 0.06073 -0.1263 0.9844 0.0291
-16.750 -0.6426 0.06211 0.05811 -0.1290 0.9829 0.0291
-16.500 -0.6316 0.05913 0.05507 -0.1323 0.9814 0.0293
-16.250 -0.6177 0.05660 0.05250 -0.1352 0.9802 0.0293
-16.000 -0.6026 0.05408 0.04994 -0.1383 0.9790 0.0294
-15.750 -0.5903 0.05162 0.04743 -0.1408 0.9769 0.0295
-15.500 -0.5822 0.04928 0.04504 -0.1425 0.9725 0.0296
-15.250 -0.5696 0.04699 0.04271 -0.1448 0.9694 0.0296
-15.000 -0.5546 0.04487 0.04054 -0.1473 0.9667 0.0297
-14.750 -0.5374 0.04253 0.03815 -0.1507 0.9644 0.0298
-14.500 -0.5235 0.04043 0.03600 -0.1530 0.9593 0.0299
-14.250 -0.5078 0.03853 0.03406 -0.1553 0.9537 0.0299
-14.000 -0.4861 0.03628 0.03173 -0.1594 0.9496 0.0300
-13.750 -0.4597 0.03462 0.03004 -0.1631 0.9464 0.0301
-13.500 -0.4478 0.03283 0.02824 -0.1646 0.9389 0.0303
-13.250 -0.4235 0.03047 0.02584 -0.1697 0.9338 0.0306
-13.000 -0.3940 0.02834 0.02364 -0.1752 0.9285 0.0308
-12.750 -0.3825 0.02647 0.02171 -0.1769 0.9185 0.0309
-12.500 -0.3598 0.02457 0.01971 -0.1807 0.9102 0.0310
-12.250 -0.3556 0.02288 0.01798 -0.1807 0.8998 0.0312
-12.000 -0.3438 0.02130 0.01629 -0.1819 0.8903 0.0315
-11.750 -0.3423 0.01994 0.01486 -0.1807 0.8793 0.0315
-11.500 -0.3366 0.01881 0.01363 -0.1797 0.8691 0.0317
-11.250 -0.3362 0.01781 0.01256 -0.1773 0.8583 0.0319
-11.000 -0.3334 0.01705 0.01170 -0.1748 0.8488 0.0320
-10.750 -0.3331 0.01638 0.01097 -0.1713 0.8392 0.0320
-10.500 -0.3299 0.01588 0.01039 -0.1678 0.8301 0.0322
-10.250 -0.3269 0.01550 0.00997 -0.1639 0.8217 0.0324
-10.000 -0.3187 0.01515 0.00953 -0.1608 0.8134 0.0325
-9.750 -0.3059 0.01478 0.00911 -0.1585 0.8062 0.0327
-9.500 -0.2910 0.01444 0.00872 -0.1564 0.7982 0.0329
-9.250 -0.2752 0.01412 0.00833 -0.1544 0.7902 0.0330
-9.000 -0.2575 0.01380 0.00798 -0.1528 0.7830 0.0332
-8.750 -0.2393 0.01352 0.00763 -0.1512 0.7750 0.0334
-8.500 -0.2199 0.01326 0.00731 -0.1497 0.7679 0.0336
-8.250 -0.1995 0.01299 0.00702 -0.1484 0.7607 0.0337
-8.000 -0.1799 0.01273 0.00668 -0.1470 0.7528 0.0340
-7.750 -0.1605 0.01240 0.00630 -0.1455 0.7455 0.0343
-7.500 -0.1404 0.01209 0.00595 -0.1441 0.7373 0.0348
-7.250 -0.1200 0.01187 0.00566 -0.1427 0.7286 0.0352
-7.000 -0.0977 0.01162 0.00539 -0.1417 0.7210 0.0357
-6.750 -0.0761 0.01144 0.00515 -0.1404 0.7122 0.0362
-6.500 -0.0536 0.01127 0.00493 -0.1393 0.7040 0.0367
-6.250 -0.0312 0.01111 0.00473 -0.1382 0.6944 0.0372
-6.000 -0.0092 0.01098 0.00455 -0.1370 0.6843 0.0377
-5.750 0.0126 0.01084 0.00436 -0.1357 0.6723 0.0386
-5.500 0.0336 0.01069 0.00415 -0.1343 0.6598 0.0402
-5.250 0.0533 0.01059 0.00398 -0.1326 0.6449 0.0420
-5.000 0.0706 0.01031 0.00372 -0.1306 0.6284 0.0577
-4.750 0.0882 0.01011 0.00356 -0.1285 0.6102 0.0822
-4.500 0.1059 0.01004 0.00345 -0.1265 0.5911 0.0923
-4.250 0.1236 0.00998 0.00336 -0.1244 0.5735 0.1033
-4.000 0.1414 0.00991 0.00329 -0.1224 0.5589 0.1164
-3.750 0.1573 0.00988 0.00324 -0.1199 0.5460 0.1274
-3.500 0.1769 0.00981 0.00318 -0.1182 0.5372 0.1376
-3.250 0.1953 0.00979 0.00313 -0.1162 0.5286 0.1460
-3.000 0.2157 0.00973 0.00308 -0.1146 0.5220 0.1554
-2.750 0.2377 0.00967 0.00303 -0.1134 0.5163 0.1644
-2.500 0.2575 0.00963 0.00299 -0.1117 0.5101 0.1754
-2.250 0.2759 0.00956 0.00296 -0.1098 0.5035 0.1948
-2.000 0.2978 0.00938 0.00294 -0.1087 0.4994 0.2355
-1.750 0.3197 0.00934 0.00297 -0.1075 0.4940 0.2586
-1.500 0.3415 0.00940 0.00303 -0.1062 0.4891 0.2727
-1.250 0.3619 0.00948 0.00311 -0.1046 0.4834 0.2844
-1.000 0.3868 0.00951 0.00315 -0.1039 0.4808 0.2922
-0.750 0.4105 0.00952 0.00318 -0.1030 0.4770 0.3001
-0.500 0.4335 0.00958 0.00324 -0.1020 0.4728 0.3074
-0.250 0.4555 0.00969 0.00331 -0.1008 0.4684 0.3122
0.000 0.4763 0.00981 0.00340 -0.0993 0.4633 0.3182
0.250 0.5005 0.00982 0.00346 -0.0985 0.4608 0.3269
0.500 0.5246 0.00986 0.00351 -0.0977 0.4578 0.3335
0.750 0.5473 0.00991 0.00358 -0.0967 0.4540 0.3435
1.000 0.5688 0.00999 0.00367 -0.0954 0.4496 0.3517
1.250 0.5896 0.01013 0.00377 -0.0941 0.4449 0.3573
1.500 0.6120 0.01018 0.00386 -0.0930 0.4415 0.3677
1.750 0.6358 0.01023 0.00393 -0.0922 0.4390 0.3768
2.000 0.6583 0.01027 0.00403 -0.0912 0.4358 0.3906
2.250 0.6804 0.01036 0.00413 -0.0901 0.4325 0.4020
2.500 0.7010 0.01045 0.00426 -0.0887 0.4287 0.4185
2.750 0.7206 0.01060 0.00441 -0.0872 0.4244 0.4332
3.250 0.7660 0.01073 0.00466 -0.0853 0.4187 0.4678
3.500 0.7876 0.01082 0.00480 -0.0842 0.4152 0.4863
3.750 0.8083 0.01094 0.00495 -0.0830 0.4115 0.5043
4.000 0.8279 0.01111 0.00514 -0.0816 0.4075 0.5225
4.250 0.8476 0.01127 0.00533 -0.0801 0.4038 0.5416
4.500 0.8699 0.01135 0.00549 -0.0792 0.4010 0.5605
4.750 0.8911 0.01147 0.00566 -0.0781 0.3975 0.5785
5.000 0.9113 0.01163 0.00586 -0.0768 0.3935 0.5982
5.250 0.9296 0.01183 0.00609 -0.0753 0.3890 0.6189
5.500 0.9482 0.01202 0.00633 -0.0738 0.3851 0.6429
5.750 0.9687 0.01212 0.00654 -0.0726 0.3816 0.6719
6.000 0.9873 0.01226 0.00678 -0.0710 0.3773 0.7096
6.250 1.0016 0.01238 0.00709 -0.0687 0.3726 0.7752
6.500 1.1020 0.01246 0.00756 -0.0843 0.3645 0.9420
6.750 1.1478 0.01284 0.00793 -0.0885 0.3577 1.0000
7.000 1.1664 0.01327 0.00829 -0.0873 0.3509 1.0000
7.250 1.1889 0.01354 0.00856 -0.0867 0.3454 1.0000
7.500 1.2079 0.01397 0.00894 -0.0857 0.3379 1.0000
7.750 1.2264 0.01443 0.00936 -0.0846 0.3304 1.0000
8.000 1.2451 0.01490 0.00979 -0.0836 0.3214 1.0000
8.250 1.2622 0.01544 0.01029 -0.0824 0.3118 1.0000
8.500 1.2758 0.01617 0.01094 -0.0808 0.2995 1.0000
8.750 1.2911 0.01684 0.01154 -0.0794 0.2874 1.0000
9.000 1.3044 0.01762 0.01226 -0.0779 0.2757 1.0000
9.250 1.3170 0.01847 0.01305 -0.0763 0.2658 1.0000
9.500 1.3314 0.01924 0.01378 -0.0751 0.2577 1.0000
9.750 1.3440 0.02013 0.01463 -0.0736 0.2507 1.0000
10.000 1.3591 0.02089 0.01538 -0.0725 0.2451 1.0000
10.250 1.3716 0.02183 0.01629 -0.0712 0.2402 1.0000
10.500 1.3855 0.02272 0.01717 -0.0701 0.2358 1.0000
10.750 1.4019 0.02346 0.01792 -0.0693 0.2332 1.0000
11.000 1.4157 0.02438 0.01885 -0.0682 0.2303 1.0000
11.250 1.4289 0.02535 0.01982 -0.0672 0.2276 1.0000
11.500 1.4398 0.02649 0.02096 -0.0660 0.2248 1.0000
11.750 1.4506 0.02767 0.02215 -0.0648 0.2222 1.0000
12.000 1.4666 0.02851 0.02303 -0.0642 0.2213 1.0000
12.250 1.4812 0.02947 0.02402 -0.0634 0.2201 1.0000
12.500 1.4956 0.03044 0.02502 -0.0627 0.2186 1.0000
12.750 1.5083 0.03154 0.02615 -0.0619 0.2170 1.0000
13.000 1.5195 0.03279 0.02742 -0.0611 0.2153 1.0000
13.250 1.5304 0.03405 0.02871 -0.0602 0.2138 1.0000
13.500 1.5391 0.03553 0.03022 -0.0593 0.2124 1.0000
13.750 1.5452 0.03721 0.03190 -0.0582 0.2099 1.0000
14.000 1.5508 0.03897 0.03368 -0.0572 0.2083 1.0000
14.250 1.5632 0.04018 0.03495 -0.0566 0.2075 1.0000
14.500 1.5745 0.04153 0.03635 -0.0561 0.2068 1.0000
14.750 1.5859 0.04288 0.03774 -0.0556 0.2060 1.0000
15.000 1.5969 0.04426 0.03917 -0.0550 0.2051 1.0000
15.250 1.6058 0.04584 0.04081 -0.0545 0.2043 1.0000
15.500 1.6158 0.04732 0.04233 -0.0540 0.2032 1.0000
15.750 1.6233 0.04905 0.04410 -0.0534 0.2021 1.0000
16.000 1.6309 0.05079 0.04588 -0.0529 0.2009 1.0000
16.250 1.6373 0.05265 0.04779 -0.0524 0.1998 1.0000
16.500 1.6420 0.05470 0.04987 -0.0519 0.1986 1.0000
16.750 1.6468 0.05671 0.05191 -0.0514 0.1974 1.0000
17.000 1.6494 0.05892 0.05415 -0.0509 0.1956 1.0000
17.250 1.6557 0.06075 0.05601 -0.0505 0.1940 1.0000
17.500 1.6628 0.06268 0.05801 -0.0503 0.1932 1.0000
17.750 1.6709 0.06450 0.05990 -0.0502 0.1921 1.0000
18.000 1.6766 0.06660 0.06205 -0.0501 0.1902 1.0000
18.250 1.6826 0.06860 0.06411 -0.0500 0.1889 1.0000
18.500 1.6875 0.07072 0.06628 -0.0499 0.1873 1.0000
18.750 1.6888 0.07324 0.06883 -0.0498 0.1856 1.0000
19.000 1.6913 0.07560 0.07121 -0.0496 0.1840 1.0000
19.250 1.6911 0.07824 0.07388 -0.0495 0.1820 1.0000
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