GOE 522 AIRFOIL (goe522-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 522 AIRFOIL (goe522-il) Reynolds number: 200,000 Max Cl/Cd: 51.56 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe522-il-200000-n5.txt Download as CSV file: xf-goe522-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.750 -0.5426 0.11490 0.10962 -0.0802 0.9969 0.0371
-17.500 -0.5587 0.10690 0.10142 -0.0861 0.9950 0.0371
-17.250 -0.5640 0.10094 0.09532 -0.0907 0.9930 0.0372
-17.000 -0.5645 0.09602 0.09027 -0.0947 0.9908 0.0372
-16.750 -0.5620 0.09189 0.08604 -0.0979 0.9882 0.0373
-16.500 -0.5579 0.08799 0.08206 -0.1011 0.9856 0.0374
-16.250 -0.5513 0.08451 0.07850 -0.1041 0.9832 0.0375
-16.000 -0.5430 0.08117 0.07509 -0.1072 0.9810 0.0377
-15.750 -0.5321 0.07808 0.07193 -0.1104 0.9790 0.0378
-15.500 -0.5219 0.07525 0.06905 -0.1129 0.9764 0.0379
-15.250 -0.5142 0.07257 0.06632 -0.1148 0.9722 0.0380
-15.000 -0.5036 0.06991 0.06361 -0.1172 0.9690 0.0382
-14.750 -0.4906 0.06742 0.06107 -0.1198 0.9664 0.0383
-14.500 -0.4768 0.06486 0.05846 -0.1226 0.9644 0.0385
-14.250 -0.4614 0.06234 0.05589 -0.1256 0.9626 0.0387
-14.000 -0.4559 0.06018 0.05370 -0.1264 0.9561 0.0388
-13.750 -0.4435 0.05781 0.05129 -0.1287 0.9524 0.0389
-13.500 -0.4285 0.05534 0.04877 -0.1317 0.9494 0.0391
-13.250 -0.4117 0.05277 0.04614 -0.1351 0.9470 0.0393
-13.000 -0.4047 0.05044 0.04375 -0.1366 0.9405 0.0395
-12.750 -0.3939 0.04803 0.04134 -0.1389 0.9351 0.0398
-12.500 -0.3791 0.04526 0.03854 -0.1426 0.9314 0.0400
-12.250 -0.3609 0.04221 0.03544 -0.1475 0.9285 0.0404
-12.000 -0.3603 0.03969 0.03285 -0.1486 0.9193 0.0406
-11.750 -0.3484 0.03694 0.03002 -0.1520 0.9133 0.0408
-11.500 -0.3308 0.03406 0.02704 -0.1567 0.9090 0.0413
-11.250 -0.3340 0.03208 0.02498 -0.1563 0.8976 0.0414
-11.000 -0.3198 0.02979 0.02256 -0.1592 0.8909 0.0418
-10.750 -0.3205 0.02815 0.02083 -0.1584 0.8801 0.0420
-10.500 -0.3118 0.02650 0.01905 -0.1590 0.8715 0.0423
-10.250 -0.3141 0.02538 0.01784 -0.1567 0.8608 0.0425
-10.000 -0.3097 0.02441 0.01676 -0.1547 0.8523 0.0427
-9.750 -0.3078 0.02372 0.01597 -0.1516 0.8442 0.0431
-9.500 -0.3043 0.02317 0.01534 -0.1484 0.8354 0.0434
-9.250 -0.2888 0.02240 0.01448 -0.1474 0.8296 0.0439
-9.000 -0.2823 0.02189 0.01392 -0.1443 0.8211 0.0444
-8.750 -0.2682 0.02131 0.01327 -0.1425 0.8135 0.0451
-8.500 -0.2453 0.02069 0.01255 -0.1422 0.8078 0.0460
-8.250 -0.2360 0.02030 0.01213 -0.1393 0.7987 0.0469
-8.000 -0.2164 0.01976 0.01155 -0.1382 0.7915 0.0485
-7.750 -0.1964 0.01923 0.01100 -0.1372 0.7850 0.0512
-7.500 -0.1848 0.01862 0.01055 -0.1348 0.7764 0.0667
-7.250 -0.1605 0.01823 0.01012 -0.1343 0.7693 0.0811
-7.000 -0.1402 0.01793 0.00980 -0.1330 0.7612 0.0882
-6.750 -0.1191 0.01764 0.00948 -0.1319 0.7523 0.0952
-6.500 -0.0935 0.01732 0.00913 -0.1315 0.7446 0.1039
-6.250 -0.0745 0.01711 0.00892 -0.1299 0.7351 0.1103
-6.000 -0.0490 0.01688 0.00862 -0.1294 0.7267 0.1168
-5.750 -0.0282 0.01669 0.00841 -0.1281 0.7171 0.1224
-5.500 -0.0042 0.01652 0.00816 -0.1273 0.7070 0.1290
-5.250 0.0171 0.01633 0.00794 -0.1261 0.6965 0.1348
-5.000 0.0407 0.01619 0.00771 -0.1251 0.6854 0.1401
-4.750 0.0614 0.01602 0.00751 -0.1238 0.6743 0.1458
-4.500 0.0846 0.01589 0.00729 -0.1228 0.6631 0.1521
-4.250 0.1045 0.01571 0.00710 -0.1213 0.6510 0.1592
-4.000 0.1262 0.01557 0.00689 -0.1200 0.6390 0.1677
-3.750 0.1457 0.01541 0.00671 -0.1185 0.6258 0.1776
-3.500 0.1658 0.01526 0.00655 -0.1170 0.6134 0.1900
-3.250 0.1856 0.01513 0.00643 -0.1155 0.6016 0.2084
-3.000 0.2055 0.01503 0.00639 -0.1140 0.5907 0.2329
-2.500 0.2478 0.01503 0.00632 -0.1113 0.5720 0.2696
-2.250 0.2691 0.01507 0.00629 -0.1099 0.5634 0.2832
-2.000 0.2903 0.01511 0.00628 -0.1086 0.5559 0.2965
-1.750 0.3111 0.01514 0.00629 -0.1072 0.5486 0.3080
-1.500 0.3331 0.01521 0.00628 -0.1060 0.5421 0.3201
-1.250 0.3557 0.01525 0.00632 -0.1050 0.5368 0.3321
-1.000 0.3781 0.01532 0.00636 -0.1039 0.5314 0.3438
-0.750 0.4001 0.01536 0.00641 -0.1027 0.5261 0.3542
-0.500 0.4235 0.01545 0.00645 -0.1018 0.5211 0.3640
-0.250 0.4475 0.01554 0.00649 -0.1011 0.5166 0.3730
0.000 0.4689 0.01559 0.00658 -0.0998 0.5119 0.3815
0.250 0.4914 0.01568 0.00665 -0.0988 0.5073 0.3894
0.500 0.5139 0.01576 0.00673 -0.0978 0.5027 0.3977
0.750 0.5377 0.01589 0.00680 -0.0970 0.4980 0.4072
1.000 0.5598 0.01600 0.00691 -0.0959 0.4934 0.4164
1.250 0.5789 0.01609 0.00707 -0.0943 0.4881 0.4269
1.750 0.6211 0.01635 0.00732 -0.0918 0.4783 0.4517
2.000 0.6453 0.01651 0.00744 -0.0911 0.4744 0.4651
2.250 0.6634 0.01661 0.00764 -0.0894 0.4699 0.4790
2.500 0.6818 0.01675 0.00783 -0.0877 0.4648 0.4928
2.750 0.7005 0.01690 0.00799 -0.0860 0.4594 0.5074
3.000 0.7213 0.01706 0.00813 -0.0848 0.4548 0.5223
3.250 0.7400 0.01722 0.00834 -0.0832 0.4503 0.5384
3.500 0.7586 0.01736 0.00858 -0.0816 0.4463 0.5559
3.750 0.7773 0.01752 0.00880 -0.0801 0.4421 0.5734
4.000 0.7967 0.01769 0.00900 -0.0787 0.4383 0.5916
4.250 0.8170 0.01787 0.00919 -0.0774 0.4347 0.6115
4.500 0.8360 0.01804 0.00945 -0.0760 0.4311 0.6330
4.750 0.8534 0.01822 0.00975 -0.0743 0.4270 0.6570
5.000 0.8707 0.01839 0.01004 -0.0726 0.4229 0.6850
5.250 0.8883 0.01855 0.01032 -0.0709 0.4188 0.7216
5.500 0.9101 0.01869 0.01061 -0.0700 0.4149 0.7825
5.750 0.9670 0.01888 0.01110 -0.0763 0.4093 0.9160
6.000 0.9905 0.01921 0.01144 -0.0762 0.4039 1.0000
6.250 1.0071 0.01958 0.01176 -0.0747 0.3991 1.0000
6.500 1.0238 0.01997 0.01206 -0.0733 0.3946 1.0000
6.750 1.0400 0.02039 0.01252 -0.0718 0.3895 1.0000
7.000 1.0556 0.02084 0.01296 -0.0703 0.3840 1.0000
7.250 1.0702 0.02132 0.01339 -0.0686 0.3787 1.0000
7.500 1.0857 0.02182 0.01387 -0.0672 0.3738 1.0000
7.750 1.1003 0.02237 0.01444 -0.0657 0.3678 1.0000
8.000 1.1136 0.02296 0.01501 -0.0641 0.3619 1.0000
8.250 1.1274 0.02358 0.01559 -0.0625 0.3564 1.0000
8.500 1.1404 0.02426 0.01629 -0.0610 0.3497 1.0000
8.750 1.1521 0.02501 0.01700 -0.0594 0.3435 1.0000
9.000 1.1643 0.02579 0.01779 -0.0579 0.3370 1.0000
9.250 1.1753 0.02664 0.01863 -0.0563 0.3299 1.0000
9.500 1.1850 0.02759 0.01954 -0.0547 0.3235 1.0000
9.750 1.1959 0.02855 0.02052 -0.0533 0.3161 1.0000
10.000 1.2041 0.02966 0.02159 -0.0517 0.3095 1.0000
10.250 1.2144 0.03073 0.02267 -0.0504 0.3031 1.0000
10.500 1.2229 0.03194 0.02387 -0.0490 0.2966 1.0000
10.750 1.2303 0.03324 0.02514 -0.0476 0.2907 1.0000
11.000 1.2396 0.03450 0.02642 -0.0465 0.2850 1.0000
11.250 1.2469 0.03591 0.02781 -0.0453 0.2795 1.0000
11.500 1.2541 0.03736 0.02922 -0.0441 0.2749 1.0000
11.750 1.2642 0.03868 0.03058 -0.0432 0.2707 1.0000
12.000 1.2727 0.04011 0.03203 -0.0423 0.2667 1.0000
12.250 1.2812 0.04158 0.03348 -0.0414 0.2632 1.0000
12.500 1.2902 0.04299 0.03485 -0.0406 0.2603 1.0000
12.750 1.3008 0.04437 0.03628 -0.0399 0.2577 1.0000
13.000 1.3109 0.04579 0.03775 -0.0393 0.2550 1.0000
13.250 1.3199 0.04732 0.03932 -0.0387 0.2521 1.0000
13.500 1.3289 0.04886 0.04088 -0.0381 0.2495 1.0000
13.750 1.3377 0.05040 0.04240 -0.0374 0.2466 1.0000
14.000 1.3490 0.05169 0.04365 -0.0369 0.2443 1.0000
14.250 1.3581 0.05331 0.04534 -0.0365 0.2424 1.0000
14.500 1.3665 0.05501 0.04712 -0.0361 0.2402 1.0000
14.750 1.3751 0.05669 0.04886 -0.0357 0.2382 1.0000
15.000 1.3840 0.05835 0.05059 -0.0354 0.2365 1.0000
15.250 1.3929 0.06002 0.05229 -0.0351 0.2346 1.0000
15.500 1.4018 0.06165 0.05396 -0.0348 0.2327 1.0000
15.750 1.4123 0.06310 0.05541 -0.0345 0.2307 1.0000
16.000 1.4268 0.06410 0.05636 -0.0342 0.2287 1.0000
16.250 1.4328 0.06613 0.05848 -0.0340 0.2270 1.0000
16.500 1.4366 0.06843 0.06090 -0.0339 0.2255 1.0000
16.750 1.4415 0.07062 0.06319 -0.0338 0.2240 1.0000
17.000 1.4454 0.07293 0.06560 -0.0337 0.2225 1.0000
17.250 1.4501 0.07514 0.06790 -0.0337 0.2210 1.0000
17.500 1.4550 0.07733 0.07017 -0.0337 0.2196 1.0000
17.750 1.4597 0.07955 0.07246 -0.0338 0.2180 1.0000
18.000 1.4674 0.08140 0.07435 -0.0338 0.2162 1.0000
18.250 1.4801 0.08261 0.07555 -0.0338 0.2145 1.0000
18.500 1.4985 0.08308 0.07599 -0.0336 0.2129 1.0000
18.750 1.4868 0.08738 0.08048 -0.0341 0.2112 1.0000
19.000 1.4737 0.09190 0.08519 -0.0348 0.2093 1.0000
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