GOE 776 AIRFOIL (goe776-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 776 AIRFOIL (goe776-il) Reynolds number: 200,000 Max Cl/Cd: 35.06 at α=10° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe776-il-200000-n5.txt Download as CSV file: xf-goe776-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.0546 0.09833 0.09157 -0.0463 1.0000 0.1122
-19.000 -1.0590 0.09458 0.08773 -0.0477 1.0000 0.1144
-18.750 -1.0635 0.09080 0.08382 -0.0490 1.0000 0.1167
-18.500 -1.0617 0.08802 0.08104 -0.0498 1.0000 0.1186
-18.250 -1.0612 0.08508 0.07809 -0.0507 1.0000 0.1206
-18.000 -1.0630 0.08181 0.07476 -0.0517 1.0000 0.1229
-17.750 -1.0640 0.07865 0.07150 -0.0525 1.0000 0.1253
-17.500 -1.0637 0.07571 0.06850 -0.0533 1.0000 0.1275
-17.250 -1.0620 0.07306 0.06587 -0.0538 1.0000 0.1296
-17.000 -1.0617 0.07021 0.06298 -0.0544 1.0000 0.1320
-16.750 -1.0607 0.06745 0.06014 -0.0550 1.0000 0.1345
-16.500 -1.0587 0.06484 0.05742 -0.0554 1.0000 0.1371
-16.250 -1.0566 0.06238 0.05499 -0.0557 1.0000 0.1393
-16.000 -1.0546 0.05991 0.05250 -0.0559 1.0000 0.1418
-15.750 -1.0523 0.05749 0.05003 -0.0561 1.0000 0.1446
-15.500 -1.0480 0.05531 0.04776 -0.0562 1.0000 0.1475
-15.250 -1.0451 0.05311 0.04556 -0.0561 1.0000 0.1499
-15.000 -1.0422 0.05094 0.04339 -0.0560 1.0000 0.1527
-14.750 -1.0383 0.04891 0.04131 -0.0558 1.0000 0.1558
-14.500 -1.0327 0.04708 0.03940 -0.0555 1.0000 0.1590
-14.250 -1.0288 0.04521 0.03754 -0.0550 1.0000 0.1618
-14.000 -1.0257 0.04335 0.03569 -0.0544 1.0000 0.1649
-13.750 -1.0208 0.04171 0.03401 -0.0536 1.0000 0.1684
-13.500 -1.0144 0.04026 0.03248 -0.0528 1.0000 0.1719
-13.250 -1.0121 0.03867 0.03092 -0.0516 1.0000 0.1750
-13.000 -1.0093 0.03723 0.02949 -0.0501 1.0000 0.1785
-12.750 -1.0056 0.03597 0.02820 -0.0485 1.0000 0.1823
-12.500 -1.0018 0.03487 0.02706 -0.0467 1.0000 0.1859
-12.250 -1.0025 0.03367 0.02590 -0.0443 1.0000 0.1892
-12.000 -1.0030 0.03263 0.02486 -0.0416 1.0000 0.1929
-11.750 -1.0026 0.03178 0.02398 -0.0388 1.0000 0.1967
-11.500 -1.0040 0.03099 0.02317 -0.0356 1.0000 0.2000
-11.250 -1.0024 0.03003 0.02224 -0.0331 0.9989 0.2038
-11.000 -0.9783 0.02896 0.02115 -0.0346 0.9946 0.2093
-10.750 -0.9520 0.02803 0.02018 -0.0362 0.9910 0.2147
-10.500 -0.9303 0.02699 0.01918 -0.0370 0.9853 0.2199
-10.250 -0.9043 0.02613 0.01830 -0.0383 0.9802 0.2259
-10.000 -0.8761 0.02530 0.01745 -0.0399 0.9763 0.2316
-9.750 -0.8546 0.02448 0.01666 -0.0402 0.9688 0.2373
-9.500 -0.8275 0.02380 0.01594 -0.0413 0.9626 0.2435
-9.250 -0.8033 0.02307 0.01523 -0.0418 0.9560 0.2492
-9.000 -0.7819 0.02242 0.01459 -0.0416 0.9466 0.2554
-8.500 -0.7371 0.02126 0.01343 -0.0412 0.9282 0.2673
-8.250 -0.7125 0.02070 0.01285 -0.0413 0.9200 0.2739
-8.000 -0.6938 0.02028 0.01239 -0.0401 0.9073 0.2799
-7.750 -0.6738 0.01976 0.01189 -0.0391 0.8968 0.2860
-7.500 -0.6551 0.01935 0.01146 -0.0377 0.8839 0.2925
-7.250 -0.6348 0.01896 0.01103 -0.0366 0.8722 0.2986
-7.000 -0.6168 0.01856 0.01064 -0.0350 0.8593 0.3049
-6.750 -0.5976 0.01824 0.01027 -0.0336 0.8465 0.3118
-6.500 -0.5777 0.01790 0.00990 -0.0322 0.8342 0.3182
-6.250 -0.5601 0.01760 0.00960 -0.0305 0.8208 0.3250
-6.000 -0.5395 0.01735 0.00927 -0.0291 0.8088 0.3322
-5.750 -0.5221 0.01712 0.00904 -0.0273 0.7953 0.3386
-5.500 -0.5038 0.01691 0.00879 -0.0255 0.7832 0.3457
-5.250 -0.4843 0.01676 0.00858 -0.0239 0.7700 0.3528
-5.000 -0.4646 0.01655 0.00837 -0.0223 0.7582 0.3594
-4.750 -0.4443 0.01639 0.00818 -0.0209 0.7453 0.3667
-4.250 -0.4014 0.01608 0.00781 -0.0185 0.7214 0.3809
-4.000 -0.3794 0.01596 0.00764 -0.0173 0.7101 0.3886
-3.750 -0.3570 0.01585 0.00749 -0.0162 0.6979 0.3959
-3.500 -0.3352 0.01571 0.00735 -0.0150 0.6870 0.4034
-3.250 -0.3128 0.01562 0.00722 -0.0139 0.6751 0.4113
-3.000 -0.2898 0.01553 0.00708 -0.0129 0.6646 0.4189
-2.750 -0.2677 0.01542 0.00700 -0.0118 0.6531 0.4268
-2.500 -0.2443 0.01536 0.00687 -0.0109 0.6426 0.4352
-2.250 -0.2217 0.01526 0.00680 -0.0098 0.6318 0.4430
-2.000 -0.1989 0.01520 0.00671 -0.0088 0.6210 0.4517
-1.750 -0.1754 0.01515 0.00664 -0.0079 0.6107 0.4602
-1.500 -0.1528 0.01508 0.00659 -0.0068 0.6000 0.4689
-1.250 -0.1293 0.01505 0.00653 -0.0058 0.5901 0.4783
-1.000 -0.1063 0.01500 0.00650 -0.0048 0.5792 0.4870
-0.750 -0.0832 0.01498 0.00645 -0.0038 0.5695 0.4969
-0.500 -0.0598 0.01495 0.00643 -0.0029 0.5589 0.5061
-0.250 -0.0369 0.01494 0.00641 -0.0018 0.5490 0.5160
0.000 -0.0133 0.01493 0.00640 -0.0009 0.5388 0.5260
0.250 0.0096 0.01492 0.00641 0.0001 0.5287 0.5357
0.500 0.0331 0.01494 0.00641 0.0011 0.5191 0.5463
0.750 0.0561 0.01494 0.00643 0.0021 0.5089 0.5559
1.000 0.0793 0.01498 0.00644 0.0031 0.4999 0.5666
1.250 0.1027 0.01499 0.00649 0.0040 0.4900 0.5764
1.750 0.1490 0.01507 0.00657 0.0060 0.4719 0.5973
2.000 0.1718 0.01512 0.00663 0.0070 0.4629 0.6078
2.250 0.1950 0.01520 0.00669 0.0080 0.4546 0.6186
2.500 0.2182 0.01524 0.00679 0.0090 0.4458 0.6290
2.750 0.2405 0.01535 0.00684 0.0101 0.4378 0.6401
3.000 0.2640 0.01539 0.00697 0.0110 0.4297 0.6504
3.250 0.2864 0.01549 0.00706 0.0121 0.4215 0.6619
3.500 0.3089 0.01560 0.00718 0.0132 0.4141 0.6725
3.750 0.3317 0.01568 0.00732 0.0142 0.4061 0.6844
4.000 0.3537 0.01581 0.00745 0.0153 0.3985 0.6954
4.250 0.3758 0.01593 0.00760 0.0165 0.3913 0.7074
4.500 0.3980 0.01605 0.00777 0.0176 0.3836 0.7188
4.750 0.4189 0.01621 0.00793 0.0189 0.3764 0.7312
5.000 0.4408 0.01635 0.00812 0.0201 0.3695 0.7429
5.250 0.4619 0.01650 0.00833 0.0214 0.3621 0.7556
5.500 0.4814 0.01671 0.00853 0.0229 0.3553 0.7676
5.750 0.5013 0.01687 0.00875 0.0244 0.3484 0.7806
6.000 0.5200 0.01706 0.00898 0.0261 0.3413 0.7928
6.500 0.5576 0.01754 0.00953 0.0294 0.3279 0.8183
6.750 0.5754 0.01781 0.00981 0.0312 0.3210 0.8322
7.000 0.5947 0.01817 0.01019 0.0326 0.3147 0.8441
7.250 0.6142 0.01846 0.01053 0.0340 0.3079 0.8573
7.500 0.6334 0.01886 0.01094 0.0354 0.3011 0.8697
7.750 0.6519 0.01926 0.01135 0.0369 0.2952 0.8821
8.000 0.6724 0.01966 0.01179 0.0379 0.2886 0.8943
8.250 0.6918 0.02013 0.01226 0.0390 0.2823 0.9055
8.500 0.7110 0.02061 0.01274 0.0401 0.2766 0.9176
8.750 0.7346 0.02112 0.01329 0.0403 0.2699 0.9267
9.000 0.7533 0.02169 0.01383 0.0412 0.2640 0.9380
9.250 0.7787 0.02228 0.01444 0.0409 0.2580 0.9455
9.500 0.8022 0.02289 0.01507 0.0407 0.2517 0.9543
9.750 0.8242 0.02363 0.01576 0.0406 0.2459 0.9620
10.000 0.8520 0.02430 0.01647 0.0394 0.2398 0.9678
10.250 0.8737 0.02506 0.01723 0.0392 0.2340 0.9759
10.500 0.9010 0.02595 0.01809 0.0376 0.2283 0.9797
10.750 0.9283 0.02675 0.01894 0.0361 0.2223 0.9846
11.000 0.9507 0.02773 0.01990 0.0353 0.2168 0.9905
11.250 0.9760 0.02871 0.02089 0.0338 0.2116 0.9942
11.500 1.0012 0.02972 0.02193 0.0323 0.2060 0.9984
11.750 1.0063 0.03067 0.02287 0.0342 0.2018 1.0000
12.000 1.0025 0.03152 0.02369 0.0377 0.1987 1.0000
12.250 1.0037 0.03232 0.02454 0.0405 0.1949 1.0000
12.500 1.0041 0.03331 0.02553 0.0431 0.1911 1.0000
12.750 1.0042 0.03444 0.02665 0.0455 0.1876 1.0000
13.000 1.0060 0.03564 0.02783 0.0475 0.1842 1.0000
13.250 1.0107 0.03681 0.02906 0.0491 0.1804 1.0000
13.500 1.0144 0.03818 0.03044 0.0505 0.1767 1.0000
13.750 1.0169 0.03976 0.03199 0.0517 0.1735 1.0000
14.000 1.0225 0.04125 0.03352 0.0526 0.1701 1.0000
14.250 1.0282 0.04283 0.03515 0.0533 0.1665 1.0000
14.500 1.0321 0.04462 0.03696 0.0539 0.1633 1.0000
14.750 1.0352 0.04653 0.03884 0.0545 0.1604 1.0000
15.000 1.0409 0.04835 0.04072 0.0548 0.1573 1.0000
15.250 1.0457 0.05030 0.04273 0.0550 0.1541 1.0000
15.500 1.0488 0.05245 0.04490 0.0551 0.1512 1.0000
15.750 1.0513 0.05467 0.04710 0.0552 0.1487 1.0000
16.000 1.0557 0.05683 0.04934 0.0551 0.1459 1.0000
16.250 1.0587 0.05919 0.05176 0.0549 0.1430 1.0000
16.500 1.0609 0.06164 0.05424 0.0547 0.1404 1.0000
16.750 1.0627 0.06416 0.05675 0.0544 0.1381 1.0000
17.000 1.0652 0.06667 0.05933 0.0540 0.1356 1.0000
17.250 1.0663 0.06943 0.06218 0.0535 0.1330 1.0000
17.500 1.0668 0.07226 0.06505 0.0529 0.1305 1.0000
17.750 1.0677 0.07504 0.06783 0.0523 0.1283 1.0000
18.000 1.0692 0.07778 0.07059 0.0516 0.1262 1.0000
18.250 1.0680 0.08098 0.07391 0.0507 0.1238 1.0000
18.500 1.0664 0.08423 0.07723 0.0498 0.1214 1.0000
18.750 1.0662 0.08729 0.08031 0.0489 0.1193 1.0000
19.000 1.0693 0.08986 0.08284 0.0481 0.1174 1.0000
19.250 1.0647 0.09366 0.08678 0.0468 0.1151 1.0000
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