GOE 226 (MVA H.36) AIRFOIL (goe226-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 226 (MVA H.36) AIRFOIL (goe226-il) Reynolds number: 1,000,000 Max Cl/Cd: 125.89 at α=7.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe226-il-1000000-n5.txt Download as CSV file: xf-goe226-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 226 (MVA H.36) AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.250 -0.4712 0.06912 0.06629 -0.1005 0.8335 0.0259
-13.000 -0.5191 0.05704 0.05403 -0.1118 0.8273 0.0260
-12.750 -0.5444 0.04697 0.04379 -0.1252 0.8210 0.0262
-12.500 -0.5405 0.03567 0.03227 -0.1465 0.8158 0.0265
-12.250 -0.5104 0.02726 0.02363 -0.1647 0.8109 0.0269
-12.000 -0.4737 0.02235 0.01852 -0.1759 0.8065 0.0273
-11.750 -0.4370 0.01942 0.01538 -0.1830 0.8025 0.0277
-11.500 -0.4049 0.01815 0.01400 -0.1859 0.7983 0.0281
-11.250 -0.3739 0.01719 0.01293 -0.1880 0.7921 0.0284
-11.000 -0.3436 0.01641 0.01201 -0.1895 0.7854 0.0288
-10.750 -0.3131 0.01575 0.01125 -0.1908 0.7788 0.0292
-10.500 -0.2831 0.01518 0.01057 -0.1919 0.7720 0.0295
-10.250 -0.2531 0.01465 0.00994 -0.1929 0.7655 0.0298
-10.000 -0.2230 0.01413 0.00931 -0.1938 0.7576 0.0300
-9.750 -0.1929 0.01354 0.00862 -0.1948 0.7499 0.0305
-9.500 -0.1628 0.01308 0.00809 -0.1956 0.7417 0.0310
-9.250 -0.1331 0.01272 0.00764 -0.1962 0.7332 0.0314
-9.000 -0.1032 0.01239 0.00723 -0.1968 0.7242 0.0318
-8.750 -0.0735 0.01210 0.00685 -0.1972 0.7157 0.0323
-8.500 -0.0438 0.01183 0.00650 -0.1977 0.7062 0.0328
-8.250 -0.0142 0.01160 0.00618 -0.1981 0.6974 0.0333
-8.000 0.0156 0.01137 0.00587 -0.1985 0.6887 0.0338
-7.750 0.0452 0.01117 0.00557 -0.1989 0.6816 0.0342
-7.500 0.0753 0.01089 0.00523 -0.1994 0.6748 0.0348
-7.250 0.1050 0.01066 0.00494 -0.1998 0.6679 0.0354
-7.000 0.1349 0.01048 0.00470 -0.2002 0.6617 0.0361
-6.750 0.1646 0.01031 0.00448 -0.2005 0.6548 0.0368
-6.250 0.2241 0.01004 0.00409 -0.2011 0.6434 0.0383
-6.000 0.2538 0.00992 0.00391 -0.2014 0.6374 0.0389
-5.750 0.2834 0.00978 0.00371 -0.2017 0.6317 0.0400
-5.500 0.3133 0.00964 0.00355 -0.2020 0.6277 0.0412
-5.250 0.3431 0.00952 0.00341 -0.2023 0.6236 0.0423
-5.000 0.3728 0.00943 0.00328 -0.2026 0.6186 0.0434
-4.750 0.4022 0.00938 0.00316 -0.2028 0.6138 0.0443
-4.500 0.4321 0.00926 0.00302 -0.2031 0.6104 0.0457
-4.250 0.4620 0.00915 0.00290 -0.2034 0.6067 0.0473
-4.000 0.4916 0.00908 0.00281 -0.2036 0.6023 0.0489
-3.750 0.5209 0.00905 0.00273 -0.2038 0.5969 0.0504
-3.500 0.5505 0.00898 0.00263 -0.2040 0.5920 0.0525
-3.250 0.5802 0.00891 0.00255 -0.2043 0.5868 0.0547
-3.000 0.6094 0.00889 0.00249 -0.2045 0.5803 0.0569
-2.750 0.6387 0.00885 0.00243 -0.2047 0.5746 0.0598
-2.500 0.6681 0.00881 0.00239 -0.2049 0.5678 0.0638
-2.250 0.6970 0.00880 0.00236 -0.2050 0.5603 0.0699
-2.000 0.7263 0.00877 0.00235 -0.2052 0.5525 0.0782
-1.750 0.7548 0.00881 0.00235 -0.2053 0.5417 0.0855
-1.500 0.7831 0.00888 0.00237 -0.2053 0.5263 0.0923
-1.250 0.8103 0.00905 0.00242 -0.2051 0.5007 0.0959
-1.000 0.8364 0.00930 0.00252 -0.2048 0.4701 0.1008
-0.750 0.8631 0.00951 0.00262 -0.2046 0.4509 0.1050
-0.500 0.8903 0.00967 0.00271 -0.2045 0.4389 0.1075
-0.250 0.9179 0.00979 0.00279 -0.2044 0.4297 0.1119
0.000 0.9457 0.00989 0.00286 -0.2044 0.4229 0.1173
0.250 0.9737 0.00997 0.00293 -0.2043 0.4180 0.1221
0.500 1.0015 0.01005 0.00301 -0.2043 0.4129 0.1326
0.750 1.0292 0.01010 0.00311 -0.2044 0.4075 0.1673
1.000 1.0575 0.01010 0.00321 -0.2045 0.4042 0.2054
1.250 1.0854 0.01016 0.00331 -0.2045 0.4005 0.2269
1.500 1.1128 0.01027 0.00343 -0.2044 0.3961 0.2426
1.750 1.1397 0.01041 0.00356 -0.2043 0.3915 0.2560
2.000 1.1670 0.01052 0.00369 -0.2042 0.3880 0.2683
2.250 1.1946 0.01060 0.00379 -0.2041 0.3854 0.2783
2.500 1.2219 0.01069 0.00391 -0.2040 0.3821 0.2893
2.750 1.2490 0.01080 0.00404 -0.2039 0.3792 0.3017
3.000 1.2758 0.01093 0.00418 -0.2037 0.3766 0.3146
3.250 1.3023 0.01106 0.00433 -0.2035 0.3740 0.3285
3.500 1.3285 0.01121 0.00450 -0.2033 0.3712 0.3397
3.750 1.3554 0.01131 0.00463 -0.2031 0.3695 0.3524
4.000 1.3821 0.01140 0.00478 -0.2030 0.3674 0.3670
4.250 1.4085 0.01152 0.00494 -0.2028 0.3648 0.3835
4.500 1.4346 0.01165 0.00512 -0.2025 0.3622 0.4026
4.750 1.4602 0.01179 0.00531 -0.2022 0.3596 0.4255
5.000 1.4853 0.01196 0.00551 -0.2018 0.3569 0.4488
5.250 1.5100 0.01214 0.00573 -0.2013 0.3541 0.4678
5.500 1.5354 0.01228 0.00592 -0.2009 0.3518 0.4844
5.750 1.5605 0.01242 0.00611 -0.2005 0.3483 0.5028
6.000 1.5848 0.01259 0.00634 -0.2000 0.3446 0.5227
6.250 1.6081 0.01280 0.00659 -0.1993 0.3404 0.5474
6.750 1.6541 0.01317 0.00714 -0.1979 0.3316 0.6439
7.000 1.6741 0.01338 0.00742 -0.1966 0.3264 0.6831
7.250 1.6944 0.01357 0.00779 -0.1955 0.3209 0.7834
7.500 1.7121 0.01360 0.00805 -0.1937 0.3161 1.0000
7.750 1.7305 0.01401 0.00844 -0.1922 0.3077 1.0000
8.000 1.7479 0.01447 0.00886 -0.1907 0.2981 1.0000
8.250 1.7629 0.01508 0.00941 -0.1888 0.2861 1.0000
8.500 1.7773 0.01574 0.01002 -0.1869 0.2751 1.0000
8.750 1.7908 0.01649 0.01072 -0.1850 0.2624 1.0000
9.000 1.8025 0.01736 0.01153 -0.1828 0.2494 1.0000
9.250 1.8139 0.01828 0.01239 -0.1807 0.2376 1.0000
9.500 1.8243 0.01929 0.01335 -0.1786 0.2268 1.0000
9.750 1.8367 0.02020 0.01424 -0.1768 0.2179 1.0000
10.000 1.8483 0.02118 0.01520 -0.1749 0.2098 1.0000
10.250 1.8575 0.02234 0.01632 -0.1728 0.1999 1.0000
10.500 1.8685 0.02339 0.01736 -0.1710 0.1911 1.0000
10.750 1.8753 0.02477 0.01869 -0.1688 0.1793 1.0000
11.000 1.8783 0.02645 0.02029 -0.1662 0.1628 1.0000
11.250 1.8715 0.02891 0.02259 -0.1628 0.1376 1.0000
11.500 1.8589 0.03192 0.02545 -0.1590 0.1118 1.0000
11.750 1.8514 0.03468 0.02813 -0.1560 0.0948 1.0000
12.000 1.8336 0.03850 0.03181 -0.1525 0.0678 1.0000
12.250 1.8132 0.04285 0.03605 -0.1492 0.0428 1.0000
12.500 1.8112 0.04559 0.03880 -0.1475 0.0361 1.0000
12.750 1.8134 0.04796 0.04121 -0.1461 0.0332 1.0000
13.000 1.8163 0.05032 0.04361 -0.1448 0.0311 1.0000
13.250 1.8197 0.05268 0.04602 -0.1437 0.0298 1.0000
13.500 1.8215 0.05526 0.04866 -0.1425 0.0284 1.0000
13.750 1.8228 0.05791 0.05135 -0.1414 0.0272 1.0000
14.000 1.8255 0.06043 0.05394 -0.1405 0.0264 1.0000
14.250 1.8271 0.06313 0.05671 -0.1396 0.0257 1.0000
14.500 1.8282 0.06591 0.05954 -0.1387 0.0249 1.0000
14.750 1.8273 0.06896 0.06266 -0.1379 0.0241 1.0000
15.000 1.8250 0.07221 0.06597 -0.1371 0.0233 1.0000
15.250 1.8242 0.07529 0.06911 -0.1364 0.0227 1.0000
15.500 1.8230 0.07847 0.07237 -0.1358 0.0221 1.0000
15.750 1.8208 0.08183 0.07580 -0.1353 0.0215 1.0000
16.000 1.8183 0.08524 0.07928 -0.1348 0.0208 1.0000
16.250 1.8137 0.08897 0.08309 -0.1345 0.0202 1.0000
16.500 1.8080 0.09288 0.08707 -0.1342 0.0197 1.0000
16.750 1.8029 0.09677 0.09104 -0.1341 0.0192 1.0000
17.000 1.7994 0.10047 0.09482 -0.1340 0.0187 1.0000
17.250 1.7948 0.10436 0.09879 -0.1341 0.0182 1.0000
17.500 1.7892 0.10843 0.10294 -0.1343 0.0177 1.0000
17.750 1.7830 0.11258 0.10716 -0.1347 0.0171 1.0000
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