GOE 522 AIRFOIL (goe522-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 522 AIRFOIL (goe522-il) Reynolds number: 500,000 Max Cl/Cd: 63.53 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe522-il-500000-n5.txt Download as CSV file: xf-goe522-il-500000-n5.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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.6162 0.11869 0.11459 -0.0845 0.9974 0.0274
-19.500 -0.6185 0.11336 0.10916 -0.0887 0.9963 0.0275
-19.250 -0.6174 0.10866 0.10437 -0.0925 0.9949 0.0275
-19.000 -0.6156 0.10415 0.09978 -0.0962 0.9932 0.0276
-18.750 -0.6140 0.09985 0.09539 -0.0996 0.9912 0.0277
-18.500 -0.6108 0.09614 0.09162 -0.1022 0.9894 0.0277
-18.250 -0.6066 0.09256 0.08798 -0.1050 0.9875 0.0278
-18.000 -0.6035 0.08872 0.08406 -0.1080 0.9855 0.0279
-17.750 -0.5972 0.08534 0.08061 -0.1109 0.9836 0.0280
-17.500 -0.5941 0.08141 0.07659 -0.1143 0.9818 0.0281
-17.250 -0.5869 0.07809 0.07321 -0.1173 0.9803 0.0282
-17.000 -0.5779 0.07496 0.07002 -0.1203 0.9788 0.0283
-16.750 -0.5690 0.07214 0.06715 -0.1228 0.9768 0.0283
-16.500 -0.5624 0.06957 0.06454 -0.1244 0.9729 0.0284
-16.250 -0.5548 0.06668 0.06159 -0.1268 0.9699 0.0284
-16.000 -0.5441 0.06415 0.05902 -0.1291 0.9675 0.0285
-15.750 -0.5295 0.06205 0.05689 -0.1312 0.9654 0.0286
-15.500 -0.5128 0.06004 0.05488 -0.1335 0.9635 0.0287
-15.250 -0.5021 0.05789 0.05271 -0.1352 0.9590 0.0288
-15.000 -0.4900 0.05557 0.05036 -0.1374 0.9541 0.0289
-14.750 -0.4742 0.05328 0.04804 -0.1402 0.9506 0.0290
-14.500 -0.4564 0.05086 0.04559 -0.1437 0.9475 0.0291
-14.250 -0.4427 0.04846 0.04315 -0.1466 0.9428 0.0292
-14.000 -0.4284 0.04617 0.04082 -0.1495 0.9371 0.0293
-13.750 -0.4086 0.04369 0.03829 -0.1537 0.9326 0.0294
-13.500 -0.3851 0.04123 0.03577 -0.1586 0.9289 0.0295
-13.250 -0.3713 0.03893 0.03341 -0.1615 0.9218 0.0296
-13.000 -0.3538 0.03660 0.03101 -0.1652 0.9141 0.0298
-12.750 -0.3357 0.03436 0.02870 -0.1688 0.9061 0.0299
-12.500 -0.3255 0.03233 0.02659 -0.1706 0.8962 0.0300
-12.250 -0.3117 0.03032 0.02449 -0.1730 0.8881 0.0301
-12.000 -0.3078 0.02844 0.02253 -0.1734 0.8773 0.0302
-11.750 -0.2995 0.02662 0.02062 -0.1744 0.8677 0.0303
-11.500 -0.2969 0.02497 0.01888 -0.1740 0.8561 0.0305
-11.250 -0.2913 0.02348 0.01728 -0.1739 0.8463 0.0305
-11.000 -0.2898 0.02210 0.01582 -0.1727 0.8350 0.0306
-10.750 -0.2869 0.02095 0.01457 -0.1713 0.8245 0.0307
-10.500 -0.2868 0.01996 0.01349 -0.1690 0.8136 0.0309
-10.250 -0.2857 0.01916 0.01260 -0.1662 0.8042 0.0310
-10.000 -0.2843 0.01855 0.01192 -0.1628 0.7946 0.0311
-9.750 -0.2806 0.01813 0.01140 -0.1593 0.7864 0.0313
-9.500 -0.2740 0.01772 0.01095 -0.1561 0.7781 0.0314
-9.250 -0.2625 0.01732 0.01047 -0.1538 0.7699 0.0316
-9.000 -0.2478 0.01698 0.01006 -0.1518 0.7622 0.0318
-8.750 -0.2327 0.01664 0.00966 -0.1498 0.7533 0.0320
-8.500 -0.2185 0.01623 0.00917 -0.1478 0.7450 0.0322
-8.250 -0.2029 0.01581 0.00872 -0.1459 0.7366 0.0325
-8.000 -0.1857 0.01548 0.00832 -0.1442 0.7282 0.0328
-7.750 -0.1668 0.01518 0.00796 -0.1427 0.7206 0.0330
-7.500 -0.1477 0.01489 0.00762 -0.1412 0.7114 0.0333
-7.250 -0.1283 0.01465 0.00730 -0.1398 0.7024 0.0336
-7.000 -0.1080 0.01441 0.00702 -0.1384 0.6923 0.0339
-6.750 -0.0883 0.01423 0.00675 -0.1369 0.6819 0.0343
-6.500 -0.0674 0.01403 0.00650 -0.1356 0.6710 0.0347
-6.250 -0.0474 0.01387 0.00627 -0.1341 0.6599 0.0351
-6.000 -0.0269 0.01372 0.00605 -0.1326 0.6470 0.0355
-5.750 -0.0073 0.01358 0.00583 -0.1310 0.6332 0.0360
-5.500 0.0107 0.01345 0.00561 -0.1291 0.6174 0.0367
-5.250 0.0281 0.01336 0.00542 -0.1270 0.6000 0.0374
-5.000 0.0459 0.01328 0.00525 -0.1250 0.5829 0.0382
-4.750 0.0640 0.01319 0.00508 -0.1231 0.5686 0.0395
-4.500 0.0810 0.01306 0.00489 -0.1210 0.5570 0.0429
-4.250 0.0972 0.01270 0.00464 -0.1189 0.5470 0.0768
-4.000 0.1141 0.01263 0.00454 -0.1167 0.5382 0.0846
-3.750 0.1332 0.01251 0.00442 -0.1149 0.5305 0.0925
-3.500 0.1508 0.01240 0.00432 -0.1129 0.5231 0.1023
-3.250 0.1692 0.01231 0.00425 -0.1111 0.5166 0.1145
-3.000 0.1907 0.01221 0.00418 -0.1098 0.5114 0.1257
-2.750 0.2116 0.01216 0.00414 -0.1084 0.5063 0.1345
-2.500 0.2321 0.01214 0.00410 -0.1069 0.5015 0.1422
-2.000 0.2752 0.01206 0.00404 -0.1044 0.4932 0.1595
-1.750 0.2974 0.01199 0.00400 -0.1032 0.4889 0.1715
-1.500 0.3183 0.01194 0.00400 -0.1019 0.4838 0.1876
-1.250 0.3375 0.01187 0.00403 -0.1003 0.4786 0.2245
-1.000 0.3583 0.01188 0.00411 -0.0990 0.4744 0.2535
-0.750 0.3819 0.01188 0.00417 -0.0981 0.4710 0.2676
-0.500 0.4052 0.01193 0.00422 -0.0972 0.4672 0.2796
-0.250 0.4273 0.01198 0.00430 -0.0960 0.4631 0.2918
0.000 0.4491 0.01207 0.00438 -0.0948 0.4593 0.3023
0.250 0.4696 0.01217 0.00448 -0.0934 0.4549 0.3116
0.500 0.4925 0.01224 0.00456 -0.0925 0.4512 0.3199
0.750 0.5153 0.01229 0.00463 -0.0915 0.4471 0.3286
1.000 0.5373 0.01236 0.00473 -0.0904 0.4430 0.3397
1.250 0.5587 0.01247 0.00483 -0.0891 0.4392 0.3478
1.500 0.5786 0.01259 0.00495 -0.0877 0.4351 0.3555
1.750 0.6005 0.01269 0.00506 -0.0866 0.4313 0.3630
2.000 0.6230 0.01278 0.00517 -0.0856 0.4270 0.3711
2.250 0.6441 0.01288 0.00530 -0.0844 0.4225 0.3818
2.500 0.6645 0.01302 0.00544 -0.0831 0.4185 0.3915
2.750 0.6840 0.01317 0.00561 -0.0817 0.4149 0.4041
3.250 0.7277 0.01339 0.00592 -0.0796 0.4086 0.4312
3.500 0.7486 0.01352 0.00609 -0.0784 0.4044 0.4467
3.750 0.7684 0.01369 0.00629 -0.0771 0.4005 0.4629
4.000 0.7862 0.01390 0.00652 -0.0754 0.3959 0.4812
4.250 0.8067 0.01406 0.00673 -0.0743 0.3923 0.4956
4.500 0.8279 0.01422 0.00693 -0.0732 0.3882 0.5107
4.750 0.8473 0.01441 0.00717 -0.0719 0.3838 0.5263
5.000 0.8650 0.01466 0.00744 -0.0703 0.3793 0.5421
5.250 0.8830 0.01492 0.00772 -0.0688 0.3753 0.5602
5.500 0.9033 0.01510 0.00798 -0.0677 0.3710 0.5780
5.750 0.9218 0.01534 0.00827 -0.0663 0.3660 0.5961
6.000 0.9376 0.01567 0.00863 -0.0646 0.3607 0.6154
6.250 0.9549 0.01595 0.00896 -0.0631 0.3561 0.6380
6.500 0.9727 0.01620 0.00930 -0.0616 0.3503 0.6647
6.750 0.9867 0.01654 0.00974 -0.0596 0.3441 0.6994
7.250 1.0940 0.01722 0.01098 -0.0721 0.3258 0.9507
7.500 1.1155 0.01781 0.01154 -0.0717 0.3184 1.0000
7.750 1.1309 0.01845 0.01212 -0.0704 0.3097 1.0000
8.000 1.1469 0.01908 0.01272 -0.0692 0.3013 1.0000
8.250 1.1604 0.01987 0.01345 -0.0678 0.2922 1.0000
8.500 1.1756 0.02059 0.01414 -0.0666 0.2833 1.0000
8.750 1.1878 0.02150 0.01500 -0.0652 0.2750 1.0000
9.000 1.2021 0.02234 0.01579 -0.0640 0.2666 1.0000
9.250 1.2130 0.02339 0.01680 -0.0626 0.2593 1.0000
9.500 1.2283 0.02420 0.01761 -0.0616 0.2540 1.0000
9.750 1.2408 0.02522 0.01860 -0.0605 0.2484 1.0000
10.000 1.2523 0.02632 0.01968 -0.0593 0.2439 1.0000
10.250 1.2671 0.02723 0.02061 -0.0585 0.2399 1.0000
10.500 1.2805 0.02826 0.02164 -0.0576 0.2365 1.0000
10.750 1.2918 0.02944 0.02282 -0.0566 0.2325 1.0000
11.000 1.3016 0.03077 0.02413 -0.0555 0.2292 1.0000
11.250 1.3151 0.03184 0.02523 -0.0548 0.2269 1.0000
11.500 1.3282 0.03297 0.02638 -0.0540 0.2243 1.0000
11.750 1.3410 0.03413 0.02757 -0.0533 0.2226 1.0000
12.000 1.3524 0.03542 0.02888 -0.0526 0.2203 1.0000
12.250 1.3618 0.03688 0.03036 -0.0518 0.2181 1.0000
12.500 1.3717 0.03831 0.03181 -0.0510 0.2162 1.0000
12.750 1.3796 0.03994 0.03346 -0.0502 0.2143 1.0000
13.000 1.3889 0.04146 0.03500 -0.0495 0.2127 1.0000
13.250 1.4007 0.04281 0.03641 -0.0490 0.2117 1.0000
13.500 1.4123 0.04419 0.03783 -0.0485 0.2108 1.0000
13.750 1.4234 0.04560 0.03929 -0.0480 0.2096 1.0000
14.000 1.4330 0.04717 0.04091 -0.0476 0.2085 1.0000
14.250 1.4427 0.04874 0.04252 -0.0471 0.2070 1.0000
14.500 1.4512 0.05044 0.04427 -0.0466 0.2058 1.0000
14.750 1.4589 0.05222 0.04609 -0.0462 0.2043 1.0000
15.000 1.4661 0.05408 0.04798 -0.0458 0.2029 1.0000
15.250 1.4722 0.05603 0.04996 -0.0454 0.2015 1.0000
15.500 1.4784 0.05798 0.05194 -0.0450 0.2001 1.0000
15.750 1.4838 0.06002 0.05402 -0.0446 0.1987 1.0000
16.000 1.4921 0.06177 0.05581 -0.0444 0.1976 1.0000
16.250 1.5009 0.06352 0.05763 -0.0442 0.1969 1.0000
16.500 1.5093 0.06533 0.05950 -0.0440 0.1959 1.0000
16.750 1.5181 0.06708 0.06131 -0.0439 0.1949 1.0000
17.000 1.5250 0.06903 0.06333 -0.0438 0.1938 1.0000
17.250 1.5315 0.07103 0.06539 -0.0437 0.1924 1.0000
17.500 1.5390 0.07290 0.06732 -0.0436 0.1913 1.0000
17.750 1.5448 0.07498 0.06945 -0.0436 0.1902 1.0000
18.000 1.5500 0.07712 0.07163 -0.0435 0.1888 1.0000
18.250 1.5558 0.07918 0.07373 -0.0435 0.1876 1.0000
18.500 1.5591 0.08151 0.07609 -0.0435 0.1860 1.0000
18.750 1.5631 0.08373 0.07832 -0.0435 0.1842 1.0000
19.000 1.5690 0.08583 0.08051 -0.0437 0.1830 1.0000
19.250 1.5727 0.08822 0.08299 -0.0439 0.1812 1.0000
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