GOE 522 AIRFOIL (goe522-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 522 AIRFOIL (goe522-il) Reynolds number: 500,000 Max Cl/Cd: 73.66 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe522-il-500000.txt Download as CSV file: xf-goe522-il-500000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.750 -0.6577 0.11173 0.10816 -0.0792 0.9997 0.0371
-18.500 -0.6843 0.10222 0.09843 -0.0864 0.9989 0.0369
-18.250 -0.6993 0.09481 0.09085 -0.0924 0.9978 0.0368
-18.000 -0.7081 0.08856 0.08445 -0.0978 0.9964 0.0367
-17.750 -0.7130 0.08297 0.07872 -0.1028 0.9949 0.0367
-17.500 -0.7138 0.07804 0.07366 -0.1076 0.9934 0.0367
-17.250 -0.7090 0.07398 0.06949 -0.1118 0.9921 0.0367
-17.000 -0.7054 0.07023 0.06564 -0.1151 0.9901 0.0367
-16.750 -0.6995 0.06691 0.06224 -0.1181 0.9877 0.0367
-16.500 -0.6925 0.06359 0.05882 -0.1213 0.9855 0.0368
-16.250 -0.6818 0.06065 0.05581 -0.1245 0.9835 0.0368
-16.000 -0.6688 0.05789 0.05297 -0.1278 0.9818 0.0369
-15.750 -0.6541 0.05530 0.05030 -0.1310 0.9803 0.0369
-15.500 -0.6385 0.05271 0.04764 -0.1345 0.9791 0.0371
-15.250 -0.6218 0.05047 0.04534 -0.1374 0.9774 0.0372
-15.000 -0.6124 0.04851 0.04333 -0.1383 0.9724 0.0372
-14.750 -0.5953 0.04631 0.04108 -0.1411 0.9695 0.0373
-14.500 -0.5755 0.04425 0.03896 -0.1440 0.9674 0.0375
-14.250 -0.5530 0.04233 0.03700 -0.1470 0.9657 0.0375
-14.000 -0.5308 0.04022 0.03482 -0.1505 0.9643 0.0377
-13.750 -0.5060 0.03843 0.03300 -0.1537 0.9629 0.0378
-13.500 -0.4963 0.03672 0.03123 -0.1543 0.9557 0.0379
-13.250 -0.4735 0.03533 0.02985 -0.1560 0.9529 0.0382
-13.000 -0.4483 0.03368 0.02820 -0.1590 0.9504 0.0384
-12.750 -0.4197 0.03186 0.02637 -0.1630 0.9484 0.0387
-12.500 -0.3957 0.02998 0.02446 -0.1666 0.9443 0.0390
-12.250 -0.3812 0.02815 0.02260 -0.1685 0.9364 0.0393
-12.000 -0.3558 0.02624 0.02063 -0.1725 0.9312 0.0396
-11.750 -0.3429 0.02461 0.01894 -0.1738 0.9227 0.0398
-11.500 -0.3287 0.02303 0.01729 -0.1752 0.9140 0.0400
-11.250 -0.3219 0.02161 0.01579 -0.1750 0.9039 0.0403
-11.000 -0.3143 0.02043 0.01452 -0.1743 0.8941 0.0405
-10.750 -0.3126 0.01949 0.01350 -0.1721 0.8844 0.0406
-10.500 -0.3095 0.01870 0.01262 -0.1694 0.8753 0.0408
-10.250 -0.3057 0.01808 0.01192 -0.1663 0.8671 0.0411
-10.000 -0.3052 0.01764 0.01142 -0.1621 0.8580 0.0412
-9.750 -0.2909 0.01714 0.01083 -0.1604 0.8513 0.0415
-9.500 -0.2835 0.01676 0.01041 -0.1572 0.8430 0.0418
-9.250 -0.2681 0.01634 0.00991 -0.1553 0.8357 0.0420
-9.000 -0.2505 0.01590 0.00940 -0.1539 0.8294 0.0424
-8.750 -0.2384 0.01545 0.00893 -0.1513 0.8217 0.0429
-8.500 -0.2197 0.01504 0.00846 -0.1499 0.8149 0.0435
-8.250 -0.1996 0.01467 0.00802 -0.1487 0.8084 0.0442
-8.000 -0.1820 0.01434 0.00767 -0.1469 0.8005 0.0450
-7.750 -0.1597 0.01404 0.00728 -0.1459 0.7934 0.0460
-7.500 -0.1388 0.01375 0.00696 -0.1447 0.7863 0.0473
-7.250 -0.1193 0.01342 0.00662 -0.1432 0.7785 0.0499
-7.000 -0.0998 0.01290 0.00619 -0.1419 0.7713 0.0701
-6.750 -0.0795 0.01262 0.00597 -0.1405 0.7635 0.0848
-6.500 -0.0570 0.01241 0.00575 -0.1394 0.7550 0.0934
-6.250 -0.0336 0.01222 0.00555 -0.1385 0.7468 0.1015
-6.000 -0.0119 0.01204 0.00539 -0.1373 0.7373 0.1102
-5.750 0.0124 0.01191 0.00522 -0.1365 0.7285 0.1183
-5.500 0.0342 0.01178 0.00510 -0.1352 0.7187 0.1258
-5.250 0.0577 0.01168 0.00495 -0.1342 0.7087 0.1336
-5.000 0.0788 0.01154 0.00483 -0.1328 0.6975 0.1406
-4.750 0.1011 0.01149 0.00470 -0.1316 0.6856 0.1476
-4.500 0.1210 0.01135 0.00455 -0.1299 0.6719 0.1550
-4.250 0.1413 0.01127 0.00443 -0.1283 0.6576 0.1620
-4.000 0.1600 0.01118 0.00429 -0.1264 0.6423 0.1709
-3.750 0.1773 0.01109 0.00416 -0.1243 0.6262 0.1821
-3.500 0.1946 0.01097 0.00405 -0.1222 0.6101 0.1998
-3.250 0.2117 0.01085 0.00400 -0.1201 0.5957 0.2290
-3.000 0.2292 0.01086 0.00399 -0.1180 0.5828 0.2535
-2.750 0.2468 0.01088 0.00399 -0.1159 0.5713 0.2705
-2.500 0.2651 0.01091 0.00400 -0.1139 0.5617 0.2827
-2.250 0.2858 0.01099 0.00401 -0.1123 0.5533 0.2928
-2.000 0.3056 0.01106 0.00404 -0.1107 0.5457 0.3024
-1.750 0.3285 0.01111 0.00407 -0.1096 0.5398 0.3113
-1.500 0.3503 0.01114 0.00410 -0.1083 0.5339 0.3197
-1.250 0.3715 0.01125 0.00415 -0.1070 0.5276 0.3278
-1.000 0.3946 0.01135 0.00420 -0.1059 0.5220 0.3346
-0.750 0.4159 0.01136 0.00425 -0.1046 0.5162 0.3424
-0.500 0.4377 0.01145 0.00431 -0.1033 0.5106 0.3510
-0.250 0.4612 0.01160 0.00440 -0.1025 0.5054 0.3596
0.000 0.4844 0.01164 0.00449 -0.1015 0.5015 0.3691
0.250 0.5067 0.01172 0.00457 -0.1004 0.4972 0.3782
0.500 0.5284 0.01177 0.00465 -0.0991 0.4927 0.3876
0.750 0.5507 0.01188 0.00474 -0.0981 0.4883 0.3966
1.000 0.5751 0.01204 0.00484 -0.0974 0.4829 0.4053
1.250 0.5957 0.01206 0.00494 -0.0960 0.4796 0.4161
1.500 0.6167 0.01213 0.00504 -0.0946 0.4753 0.4273
1.750 0.6375 0.01220 0.00515 -0.0933 0.4711 0.4405
2.000 0.6587 0.01232 0.00526 -0.0920 0.4667 0.4542
2.250 0.6828 0.01247 0.00540 -0.0914 0.4625 0.4705
2.500 0.7034 0.01251 0.00554 -0.0900 0.4597 0.4884
2.750 0.7243 0.01258 0.00568 -0.0887 0.4563 0.5065
3.000 0.7451 0.01267 0.00583 -0.0874 0.4529 0.5261
3.250 0.7658 0.01279 0.00597 -0.0861 0.4493 0.5462
3.500 0.7867 0.01293 0.00614 -0.0849 0.4456 0.5663
3.750 0.8089 0.01306 0.00631 -0.0839 0.4420 0.5874
4.000 0.8280 0.01314 0.00650 -0.0823 0.4389 0.6081
4.250 0.8468 0.01324 0.00668 -0.0807 0.4352 0.6301
4.500 0.8650 0.01335 0.00686 -0.0791 0.4312 0.6547
4.750 0.8834 0.01348 0.00706 -0.0774 0.4275 0.6837
5.000 0.9025 0.01361 0.00727 -0.0759 0.4234 0.7214
5.250 0.9163 0.01362 0.00754 -0.0733 0.4203 0.7828
5.500 0.9738 0.01359 0.00791 -0.0797 0.4153 0.9239
5.750 1.0276 0.01395 0.00823 -0.0856 0.4100 1.0000
6.000 1.0465 0.01427 0.00847 -0.0844 0.4056 1.0000
6.250 1.0669 0.01452 0.00874 -0.0833 0.4018 1.0000
6.500 1.0869 0.01479 0.00901 -0.0823 0.3973 1.0000
6.750 1.1054 0.01512 0.00931 -0.0810 0.3925 1.0000
7.000 1.1227 0.01552 0.00965 -0.0796 0.3875 1.0000
7.250 1.1425 0.01585 0.00999 -0.0786 0.3829 1.0000
7.500 1.1612 0.01621 0.01036 -0.0775 0.3774 1.0000
7.750 1.1779 0.01668 0.01079 -0.0762 0.3716 1.0000
8.000 1.1952 0.01715 0.01123 -0.0750 0.3659 1.0000
8.250 1.2131 0.01760 0.01170 -0.0739 0.3593 1.0000
8.500 1.2276 0.01822 0.01227 -0.0724 0.3524 1.0000
8.750 1.2447 0.01876 0.01281 -0.0713 0.3450 1.0000
9.000 1.2583 0.01949 0.01350 -0.0699 0.3366 1.0000
9.250 1.2731 0.02019 0.01419 -0.0686 0.3281 1.0000
9.500 1.2838 0.02112 0.01507 -0.0670 0.3183 1.0000
9.750 1.2973 0.02196 0.01589 -0.0658 0.3087 1.0000
10.000 1.3054 0.02313 0.01699 -0.0640 0.2987 1.0000
10.250 1.3176 0.02411 0.01795 -0.0628 0.2898 1.0000
10.500 1.3257 0.02536 0.01916 -0.0612 0.2818 1.0000
10.750 1.3376 0.02643 0.02021 -0.0601 0.2750 1.0000
11.000 1.3450 0.02780 0.02153 -0.0586 0.2692 1.0000
11.250 1.3576 0.02887 0.02261 -0.0577 0.2645 1.0000
11.500 1.3692 0.03002 0.02378 -0.0567 0.2603 1.0000
11.750 1.3787 0.03133 0.02507 -0.0555 0.2565 1.0000
12.000 1.3861 0.03280 0.02650 -0.0543 0.2528 1.0000
12.250 1.3995 0.03389 0.02764 -0.0536 0.2503 1.0000
12.500 1.4129 0.03498 0.02877 -0.0530 0.2479 1.0000
12.750 1.4239 0.03626 0.03007 -0.0522 0.2454 1.0000
13.000 1.4343 0.03759 0.03142 -0.0513 0.2431 1.0000
13.250 1.4441 0.03897 0.03279 -0.0505 0.2409 1.0000
13.500 1.4532 0.04040 0.03421 -0.0497 0.2387 1.0000
13.750 1.4650 0.04161 0.03544 -0.0490 0.2366 1.0000
14.000 1.4774 0.04286 0.03676 -0.0485 0.2352 1.0000
14.250 1.4885 0.04422 0.03818 -0.0479 0.2337 1.0000
14.500 1.4997 0.04557 0.03957 -0.0474 0.2321 1.0000
14.750 1.5107 0.04693 0.04097 -0.0469 0.2305 1.0000
15.000 1.5207 0.04841 0.04248 -0.0464 0.2289 1.0000
15.250 1.5311 0.04982 0.04392 -0.0459 0.2275 1.0000
15.500 1.5419 0.05117 0.04528 -0.0454 0.2259 1.0000
15.750 1.5536 0.05238 0.04649 -0.0449 0.2242 1.0000
16.000 1.5699 0.05307 0.04715 -0.0444 0.2224 1.0000
16.250 1.5780 0.05481 0.04898 -0.0441 0.2214 1.0000
16.500 1.5867 0.05648 0.05074 -0.0438 0.2203 1.0000
16.750 1.5958 0.05810 0.05242 -0.0435 0.2192 1.0000
17.000 1.6046 0.05974 0.05413 -0.0432 0.2180 1.0000
17.250 1.6142 0.06130 0.05574 -0.0430 0.2168 1.0000
17.500 1.6222 0.06302 0.05752 -0.0427 0.2154 1.0000
17.750 1.6304 0.06471 0.05926 -0.0425 0.2140 1.0000
18.000 1.6391 0.06635 0.06093 -0.0423 0.2126 1.0000
18.250 1.6487 0.06783 0.06242 -0.0421 0.2108 1.0000
18.500 1.6641 0.06858 0.06315 -0.0418 0.2090 1.0000
18.750 1.6731 0.07013 0.06476 -0.0416 0.2074 1.0000
19.000 1.6718 0.07302 0.06777 -0.0417 0.2060 1.0000
19.250 1.6692 0.07607 0.07093 -0.0418 0.2041 1.0000
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