GOE 776 AIRFOIL (goe776-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 776 AIRFOIL (goe776-il) Reynolds number: 500,000 Max Cl/Cd: 48.52 at α=9° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe776-il-500000-n5.txt Download as CSV file: xf-goe776-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 776 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
------ -------- --------- --------- -------- -------- --------
-19.500 -1.1566 0.09063 0.08519 -0.0439 1.0000 0.0899
-19.250 -1.1557 0.08769 0.08219 -0.0448 1.0000 0.0914
-19.000 -1.1604 0.08408 0.07855 -0.0458 1.0000 0.0930
-18.750 -1.1643 0.08058 0.07500 -0.0468 1.0000 0.0947
-18.500 -1.1651 0.07750 0.07187 -0.0475 1.0000 0.0964
-18.250 -1.1653 0.07450 0.06881 -0.0482 1.0000 0.0981
-18.000 -1.1628 0.07186 0.06611 -0.0488 1.0000 0.0997
-17.750 -1.1669 0.06847 0.06269 -0.0495 1.0000 0.1014
-17.500 -1.1677 0.06552 0.05970 -0.0500 1.0000 0.1032
-17.250 -1.1670 0.06274 0.05687 -0.0505 1.0000 0.1051
-17.000 -1.1640 0.06025 0.05433 -0.0508 1.0000 0.1069
-16.750 -1.1611 0.05778 0.05181 -0.0511 1.0000 0.1085
-16.500 -1.1622 0.05493 0.04893 -0.0514 1.0000 0.1104
-16.250 -1.1600 0.05247 0.04644 -0.0515 1.0000 0.1124
-16.000 -1.1565 0.05018 0.04410 -0.0516 1.0000 0.1145
-15.750 -1.1506 0.04816 0.04204 -0.0516 1.0000 0.1164
-15.500 -1.1468 0.04598 0.03982 -0.0515 1.0000 0.1183
-15.250 -1.1443 0.04372 0.03754 -0.0513 1.0000 0.1204
-15.000 -1.1389 0.04180 0.03559 -0.0510 1.0000 0.1228
-14.750 -1.1322 0.04003 0.03379 -0.0507 1.0000 0.1251
-14.500 -1.1246 0.03842 0.03213 -0.0502 1.0000 0.1272
-14.250 -1.1203 0.03659 0.03029 -0.0496 1.0000 0.1296
-14.000 -1.1149 0.03493 0.02862 -0.0488 1.0000 0.1322
-13.750 -1.1074 0.03355 0.02721 -0.0479 1.0000 0.1349
-13.500 -1.0995 0.03231 0.02594 -0.0468 1.0000 0.1372
-13.250 -1.0969 0.03088 0.02451 -0.0452 1.0000 0.1398
-13.000 -1.0939 0.02968 0.02330 -0.0432 1.0000 0.1426
-12.750 -1.0911 0.02864 0.02225 -0.0410 1.0000 0.1454
-12.500 -1.0766 0.02761 0.02119 -0.0406 0.9983 0.1484
-12.250 -1.0570 0.02631 0.01990 -0.0416 0.9951 0.1523
-12.000 -1.0342 0.02523 0.01881 -0.0428 0.9924 0.1566
-11.750 -1.0106 0.02428 0.01785 -0.0439 0.9892 0.1606
-11.500 -0.9916 0.02322 0.01681 -0.0442 0.9833 0.1651
-11.250 -0.9682 0.02236 0.01594 -0.0450 0.9782 0.1700
-11.000 -0.9472 0.02152 0.01510 -0.0453 0.9717 0.1744
-10.750 -0.9273 0.02069 0.01429 -0.0453 0.9638 0.1794
-10.500 -0.9053 0.02004 0.01362 -0.0453 0.9563 0.1841
-10.250 -0.8882 0.01931 0.01289 -0.0445 0.9456 0.1886
-10.000 -0.8704 0.01868 0.01226 -0.0436 0.9353 0.1936
-9.750 -0.8519 0.01816 0.01170 -0.0426 0.9235 0.1981
-9.500 -0.8358 0.01759 0.01112 -0.0412 0.9110 0.2028
-9.250 -0.8189 0.01708 0.01058 -0.0398 0.8984 0.2078
-9.000 -0.8001 0.01667 0.01013 -0.0386 0.8844 0.2124
-8.750 -0.7828 0.01621 0.00965 -0.0373 0.8708 0.2174
-8.500 -0.7649 0.01580 0.00919 -0.0359 0.8560 0.2229
-8.250 -0.7445 0.01548 0.00883 -0.0349 0.8415 0.2280
-8.000 -0.7259 0.01511 0.00842 -0.0336 0.8273 0.2330
-7.750 -0.7066 0.01479 0.00806 -0.0324 0.8124 0.2387
-7.500 -0.6851 0.01453 0.00775 -0.0315 0.7987 0.2442
-7.250 -0.6659 0.01423 0.00741 -0.0302 0.7845 0.2500
-7.000 -0.6452 0.01396 0.00712 -0.0291 0.7705 0.2561
-6.750 -0.6229 0.01377 0.00686 -0.0282 0.7573 0.2613
-6.500 -0.6028 0.01351 0.00658 -0.0270 0.7433 0.2673
-6.250 -0.5814 0.01330 0.00634 -0.0260 0.7306 0.2740
-6.000 -0.5589 0.01314 0.00613 -0.0251 0.7173 0.2796
-5.750 -0.5383 0.01292 0.00589 -0.0238 0.7053 0.2860
-5.500 -0.5166 0.01276 0.00570 -0.0228 0.6925 0.2926
-5.250 -0.4943 0.01262 0.00553 -0.0218 0.6812 0.2987
-5.000 -0.4748 0.01246 0.00536 -0.0202 0.6691 0.3057
-4.750 -0.4536 0.01236 0.00523 -0.0190 0.6583 0.3128
-4.500 -0.4338 0.01226 0.00510 -0.0174 0.6469 0.3193
-4.250 -0.4138 0.01215 0.00499 -0.0159 0.6367 0.3266
-4.000 -0.3909 0.01209 0.00489 -0.0149 0.6256 0.3331
-3.750 -0.3693 0.01199 0.00478 -0.0137 0.6159 0.3399
-3.500 -0.3463 0.01189 0.00468 -0.0128 0.6056 0.3473
-3.000 -0.2999 0.01175 0.00451 -0.0109 0.5855 0.3608
-2.750 -0.2766 0.01170 0.00444 -0.0100 0.5752 0.3683
-2.500 -0.2521 0.01166 0.00437 -0.0093 0.5654 0.3748
-2.250 -0.2294 0.01158 0.00430 -0.0082 0.5548 0.3824
-2.000 -0.2055 0.01155 0.00425 -0.0074 0.5454 0.3900
-1.750 -0.1809 0.01151 0.00420 -0.0067 0.5350 0.3968
-1.500 -0.1583 0.01148 0.00415 -0.0056 0.5247 0.4048
-1.250 -0.1333 0.01144 0.00411 -0.0050 0.5149 0.4126
-1.000 -0.1099 0.01143 0.00408 -0.0041 0.5046 0.4199
-0.750 -0.0858 0.01139 0.00405 -0.0033 0.4951 0.4286
-0.500 -0.0614 0.01141 0.00404 -0.0025 0.4847 0.4364
-0.250 -0.0380 0.01137 0.00402 -0.0016 0.4757 0.4450
0.000 -0.0138 0.01137 0.00401 -0.0008 0.4658 0.4542
0.250 0.0098 0.01138 0.00401 0.0001 0.4569 0.4627
0.500 0.0340 0.01136 0.00401 0.0009 0.4480 0.4728
0.750 0.0578 0.01141 0.00403 0.0017 0.4390 0.4818
1.000 0.0817 0.01139 0.00404 0.0025 0.4314 0.4920
1.250 0.1062 0.01142 0.00407 0.0033 0.4228 0.5019
1.500 0.1290 0.01144 0.00411 0.0043 0.4149 0.5119
1.750 0.1541 0.01146 0.00414 0.0049 0.4076 0.5221
2.000 0.1774 0.01149 0.00418 0.0059 0.3995 0.5320
2.250 0.2011 0.01154 0.00424 0.0067 0.3924 0.5427
2.500 0.2256 0.01157 0.00429 0.0074 0.3851 0.5520
2.750 0.2485 0.01163 0.00435 0.0084 0.3774 0.5627
3.000 0.2726 0.01170 0.00442 0.0092 0.3706 0.5724
3.250 0.2961 0.01173 0.00449 0.0101 0.3635 0.5829
3.500 0.3190 0.01183 0.00458 0.0111 0.3560 0.5926
3.750 0.3424 0.01188 0.00466 0.0120 0.3498 0.6028
4.000 0.3657 0.01195 0.00475 0.0129 0.3427 0.6136
4.250 0.3872 0.01207 0.00486 0.0141 0.3354 0.6230
4.500 0.4102 0.01213 0.00496 0.0151 0.3293 0.6341
4.750 0.4312 0.01223 0.00507 0.0164 0.3221 0.6444
5.000 0.4498 0.01234 0.00520 0.0182 0.3153 0.6556
5.500 0.4919 0.01256 0.00548 0.0207 0.3017 0.6786
6.000 0.5352 0.01286 0.00585 0.0229 0.2888 0.7026
6.250 0.5564 0.01308 0.00606 0.0240 0.2822 0.7149
6.500 0.5780 0.01325 0.00629 0.0251 0.2766 0.7279
6.750 0.6002 0.01344 0.00652 0.0260 0.2703 0.7407
7.000 0.6203 0.01370 0.00679 0.0272 0.2638 0.7547
7.250 0.6421 0.01391 0.00705 0.0282 0.2585 0.7677
7.500 0.6634 0.01415 0.00733 0.0292 0.2526 0.7822
7.750 0.6826 0.01446 0.00767 0.0304 0.2466 0.7960
8.000 0.7040 0.01472 0.00798 0.0314 0.2412 0.8100
8.250 0.7239 0.01502 0.00833 0.0325 0.2354 0.8246
8.500 0.7421 0.01540 0.00874 0.0338 0.2300 0.8388
8.750 0.7626 0.01572 0.00910 0.0349 0.2252 0.8537
9.000 0.7812 0.01610 0.00953 0.0361 0.2197 0.8681
9.250 0.7979 0.01658 0.01003 0.0376 0.2143 0.8821
9.500 0.8169 0.01697 0.01047 0.0387 0.2099 0.8962
9.750 0.8346 0.01745 0.01098 0.0400 0.2049 0.9087
10.000 0.8501 0.01804 0.01157 0.0415 0.1999 0.9218
10.250 0.8687 0.01855 0.01213 0.0425 0.1955 0.9333
10.500 0.8867 0.01914 0.01272 0.0434 0.1906 0.9441
10.750 0.9037 0.01989 0.01346 0.0442 0.1859 0.9547
11.000 0.9251 0.02052 0.01412 0.0443 0.1813 0.9629
11.250 0.9464 0.02129 0.01488 0.0442 0.1763 0.9705
11.500 0.9656 0.02219 0.01576 0.0442 0.1718 0.9776
11.750 0.9902 0.02298 0.01656 0.0432 0.1671 0.9826
12.000 1.0103 0.02397 0.01754 0.0428 0.1625 0.9885
12.250 1.0324 0.02499 0.01856 0.0419 0.1585 0.9922
12.500 1.0563 0.02601 0.01960 0.0407 0.1543 0.9948
12.750 1.0771 0.02720 0.02079 0.0396 0.1502 0.9980
13.000 1.0909 0.02836 0.02196 0.0398 0.1471 1.0000
13.250 1.0947 0.02933 0.02295 0.0421 0.1443 1.0000
13.500 1.0986 0.03046 0.02409 0.0440 0.1415 1.0000
13.750 1.1020 0.03183 0.02546 0.0456 0.1387 1.0000
14.000 1.1083 0.03317 0.02681 0.0468 0.1363 1.0000
14.250 1.1164 0.03451 0.02819 0.0477 0.1336 1.0000
14.500 1.1231 0.03605 0.02975 0.0484 0.1310 1.0000
14.750 1.1284 0.03779 0.03150 0.0490 0.1284 1.0000
15.000 1.1340 0.03959 0.03332 0.0495 0.1262 1.0000
15.250 1.1419 0.04123 0.03501 0.0499 0.1240 1.0000
15.500 1.1477 0.04313 0.03694 0.0501 0.1216 1.0000
15.750 1.1512 0.04528 0.03911 0.0503 0.1193 1.0000
16.000 1.1537 0.04757 0.04143 0.0504 0.1172 1.0000
16.250 1.1599 0.04957 0.04348 0.0504 0.1153 1.0000
16.500 1.1645 0.05174 0.04569 0.0504 0.1132 1.0000
16.750 1.1668 0.05420 0.04819 0.0502 0.1111 1.0000
17.000 1.1665 0.05697 0.05099 0.0500 0.1092 1.0000
17.250 1.1687 0.05950 0.05355 0.0497 0.1075 1.0000
17.500 1.1716 0.06201 0.05612 0.0493 0.1057 1.0000
17.750 1.1733 0.06467 0.05883 0.0489 0.1038 1.0000
18.000 1.1722 0.06767 0.06187 0.0484 0.1019 1.0000
18.250 1.1688 0.07098 0.06521 0.0477 0.1002 1.0000
18.500 1.1704 0.07372 0.06800 0.0471 0.0986 1.0000
18.750 1.1706 0.07668 0.07103 0.0464 0.0968 1.0000
19.000 1.1703 0.07970 0.07410 0.0457 0.0951 1.0000
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