GOE 222 (MVA H.33) AIRFOIL (goe222-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 222 (MVA H.33) AIRFOIL (goe222-il) Reynolds number: 200,000 Max Cl/Cd: 67.16 at α=2.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe222-il-200000-n5.txt Download as CSV file: xf-goe222-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 222 (MVA H.33) 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
------ -------- --------- --------- -------- -------- --------
-13.250 -0.2784 0.06777 0.06307 -0.1446 0.9416 0.0343
-13.000 -0.3088 0.06053 0.05562 -0.1500 0.9321 0.0344
-12.750 -0.3256 0.05449 0.04933 -0.1557 0.9252 0.0346
-12.500 -0.3410 0.05003 0.04468 -0.1590 0.9141 0.0348
-12.250 -0.3507 0.04579 0.04020 -0.1629 0.9048 0.0350
-12.000 -0.3590 0.04217 0.03634 -0.1661 0.8937 0.0353
-11.750 -0.3580 0.04005 0.03415 -0.1666 0.8830 0.0357
-11.500 -0.3440 0.03813 0.03215 -0.1685 0.8764 0.0362
-11.250 -0.3333 0.03624 0.03018 -0.1704 0.8660 0.0366
-11.000 -0.3137 0.03415 0.02793 -0.1738 0.8595 0.0372
-10.750 -0.2976 0.03245 0.02609 -0.1757 0.8498 0.0377
-10.500 -0.2751 0.03086 0.02432 -0.1778 0.8442 0.0383
-10.250 -0.2557 0.02959 0.02290 -0.1788 0.8363 0.0390
-10.000 -0.2317 0.02833 0.02145 -0.1803 0.8305 0.0398
-9.750 -0.2072 0.02722 0.02014 -0.1816 0.8250 0.0406
-9.500 -0.1838 0.02624 0.01905 -0.1822 0.8190 0.0412
-9.250 -0.1588 0.02530 0.01810 -0.1827 0.8144 0.0418
-9.000 -0.1327 0.02445 0.01721 -0.1834 0.8103 0.0425
-8.750 -0.1086 0.02372 0.01644 -0.1838 0.8049 0.0432
-8.500 -0.0822 0.02298 0.01563 -0.1846 0.8002 0.0440
-8.250 -0.0539 0.02227 0.01482 -0.1856 0.7965 0.0451
-8.000 -0.0263 0.02165 0.01410 -0.1865 0.7929 0.0462
-7.750 0.0004 0.02111 0.01348 -0.1872 0.7889 0.0471
-7.500 0.0277 0.02042 0.01277 -0.1881 0.7854 0.0480
-7.250 0.0568 0.01973 0.01204 -0.1894 0.7820 0.0490
-7.000 0.0879 0.01911 0.01133 -0.1909 0.7786 0.0503
-6.750 0.1157 0.01862 0.01077 -0.1917 0.7736 0.0517
-6.500 0.1444 0.01817 0.01023 -0.1925 0.7685 0.0535
-6.250 0.1752 0.01767 0.00962 -0.1938 0.7642 0.0555
-6.000 0.2074 0.01715 0.00897 -0.1953 0.7605 0.0583
-5.750 0.2351 0.01680 0.00856 -0.1958 0.7554 0.0612
-5.500 0.2645 0.01640 0.00811 -0.1966 0.7505 0.0661
-5.250 0.2960 0.01584 0.00759 -0.1980 0.7459 0.0852
-5.000 0.3277 0.01517 0.00707 -0.1996 0.7415 0.1435
-4.750 0.3562 0.01472 0.00689 -0.2005 0.7365 0.2121
-4.500 0.3852 0.01467 0.00688 -0.2009 0.7326 0.2452
-4.250 0.4150 0.01469 0.00685 -0.2014 0.7294 0.2642
-4.000 0.4457 0.01473 0.00680 -0.2020 0.7264 0.2789
-3.750 0.4750 0.01480 0.00680 -0.2023 0.7231 0.2906
-3.500 0.5022 0.01488 0.00688 -0.2022 0.7190 0.2997
-3.250 0.5304 0.01496 0.00686 -0.2023 0.7149 0.3105
-3.000 0.5591 0.01509 0.00699 -0.2025 0.7110 0.3205
-2.750 0.5896 0.01522 0.00703 -0.2030 0.7076 0.3317
-2.500 0.6173 0.01537 0.00718 -0.2030 0.7039 0.3404
-2.250 0.6441 0.01543 0.00718 -0.2029 0.6996 0.3466
-2.000 0.6714 0.01546 0.00722 -0.2028 0.6953 0.3505
-1.750 0.7003 0.01548 0.00720 -0.2031 0.6913 0.3545
-1.500 0.7303 0.01550 0.00712 -0.2035 0.6874 0.3587
-1.250 0.7550 0.01554 0.00715 -0.2030 0.6820 0.3624
-1.000 0.7815 0.01554 0.00713 -0.2029 0.6765 0.3654
-0.750 0.8099 0.01553 0.00709 -0.2030 0.6717 0.3684
-0.500 0.8358 0.01558 0.00715 -0.2027 0.6662 0.3721
-0.250 0.8606 0.01562 0.00720 -0.2022 0.6599 0.3762
0.000 0.8880 0.01564 0.00715 -0.2022 0.6542 0.3802
0.250 0.9130 0.01568 0.00720 -0.2017 0.6478 0.3835
0.500 0.9373 0.01571 0.00727 -0.2011 0.6404 0.3866
0.750 0.9630 0.01574 0.00728 -0.2008 0.6336 0.3903
1.000 0.9853 0.01583 0.00739 -0.1998 0.6246 0.3945
1.250 1.0094 0.01589 0.00741 -0.1991 0.6160 0.3991
1.500 1.0311 0.01596 0.00750 -0.1981 0.6048 0.4029
1.750 1.0523 0.01605 0.00758 -0.1968 0.5920 0.4067
2.000 1.0729 0.01616 0.00765 -0.1955 0.5783 0.4108
2.250 1.0919 0.01631 0.00772 -0.1939 0.5642 0.4152
2.500 1.1091 0.01652 0.00783 -0.1919 0.5507 0.4195
2.750 1.1263 0.01677 0.00803 -0.1901 0.5380 0.4237
3.000 1.1452 0.01707 0.00829 -0.1886 0.5267 0.4288
3.250 1.1648 0.01741 0.00856 -0.1873 0.5170 0.4344
3.500 1.1849 0.01775 0.00887 -0.1861 0.5081 0.4395
3.750 1.2053 0.01810 0.00920 -0.1850 0.5006 0.4446
4.000 1.2256 0.01846 0.00956 -0.1839 0.4928 0.4506
4.500 1.2658 0.01923 0.01033 -0.1817 0.4788 0.4638
4.750 1.2863 0.01962 0.01073 -0.1807 0.4728 0.4720
5.000 1.3076 0.02001 0.01111 -0.1799 0.4682 0.4800
5.250 1.3285 0.02038 0.01155 -0.1790 0.4635 0.4890
5.500 1.3488 0.02078 0.01200 -0.1780 0.4584 0.4984
5.750 1.3685 0.02122 0.01246 -0.1770 0.4533 0.5096
6.000 1.3885 0.02166 0.01293 -0.1760 0.4485 0.5220
6.250 1.4069 0.02212 0.01349 -0.1748 0.4430 0.5358
6.500 1.4250 0.02262 0.01404 -0.1736 0.4374 0.5510
6.750 1.4438 0.02312 0.01455 -0.1725 0.4328 0.5669
7.000 1.4627 0.02360 0.01513 -0.1714 0.4287 0.5840
7.500 1.4992 0.02458 0.01633 -0.1692 0.4203 0.6267
7.750 1.5172 0.02508 0.01693 -0.1680 0.4163 0.6593
8.000 1.5315 0.02526 0.01750 -0.1659 0.4126 0.8165
8.250 1.5425 0.02573 0.01810 -0.1636 0.4084 1.0000
8.500 1.5585 0.02642 0.01883 -0.1623 0.4038 1.0000
8.750 1.5740 0.02715 0.01956 -0.1609 0.3993 1.0000
9.000 1.5895 0.02789 0.02031 -0.1596 0.3947 1.0000
9.250 1.6026 0.02875 0.02127 -0.1580 0.3892 1.0000
9.500 1.6151 0.02964 0.02220 -0.1564 0.3835 1.0000
9.750 1.6279 0.03055 0.02310 -0.1549 0.3785 1.0000
10.000 1.6396 0.03155 0.02423 -0.1533 0.3725 1.0000
10.250 1.6500 0.03264 0.02537 -0.1516 0.3663 1.0000
10.500 1.6599 0.03378 0.02654 -0.1499 0.3601 1.0000
10.750 1.6685 0.03507 0.02794 -0.1482 0.3522 1.0000
11.000 1.6751 0.03651 0.02939 -0.1464 0.3444 1.0000
11.250 1.6813 0.03809 0.03105 -0.1447 0.3341 1.0000
11.500 1.6857 0.03985 0.03284 -0.1428 0.3230 1.0000
11.750 1.6871 0.04190 0.03489 -0.1409 0.3097 1.0000
12.000 1.6859 0.04425 0.03722 -0.1389 0.2949 1.0000
12.250 1.6829 0.04684 0.03976 -0.1369 0.2809 1.0000
12.750 1.6775 0.05218 0.04503 -0.1332 0.2580 1.0000
13.000 1.6756 0.05484 0.04767 -0.1316 0.2494 1.0000
13.250 1.6753 0.05741 0.05025 -0.1301 0.2416 1.0000
13.500 1.6742 0.06009 0.05292 -0.1286 0.2354 1.0000
13.750 1.6779 0.06233 0.05524 -0.1275 0.2298 1.0000
14.000 1.6786 0.06488 0.05782 -0.1264 0.2243 1.0000
14.250 1.6781 0.06758 0.06052 -0.1252 0.2194 1.0000
14.500 1.6821 0.06991 0.06294 -0.1243 0.2144 1.0000
14.750 1.6833 0.07254 0.06563 -0.1234 0.2094 1.0000
15.000 1.6830 0.07535 0.06847 -0.1225 0.2050 1.0000
15.250 1.6858 0.07785 0.07106 -0.1218 0.2010 1.0000
15.500 1.6879 0.08050 0.07382 -0.1212 0.1963 1.0000
15.750 1.6870 0.08353 0.07690 -0.1206 0.1912 1.0000
16.000 1.6852 0.08667 0.08008 -0.1200 0.1867 1.0000
16.250 1.6872 0.08948 0.08302 -0.1197 0.1817 1.0000
16.500 1.6861 0.09266 0.08629 -0.1195 0.1765 1.0000
16.750 1.6828 0.09613 0.08983 -0.1192 0.1715 1.0000
17.000 1.6816 0.09943 0.09324 -0.1192 0.1646 1.0000
17.250 1.6756 0.10337 0.09723 -0.1193 0.1576 1.0000
17.500 1.6717 0.10707 0.10101 -0.1195 0.1489 1.0000
17.750 1.6639 0.11134 0.10532 -0.1199 0.1393 1.0000
18.000 1.6537 0.11599 0.10999 -0.1205 0.1290 1.0000
18.250 1.6412 0.12101 0.11499 -0.1213 0.1177 1.0000
18.500 1.6277 0.12620 0.12016 -0.1223 0.1054 1.0000
18.750 1.6096 0.13216 0.12607 -0.1238 0.0852 1.0000
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