GOE 226 (MVA H.36) AIRFOIL (goe226-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 226 (MVA H.36) AIRFOIL (goe226-il) Reynolds number: 50,000 Max Cl/Cd: 28.63 at α=3.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe226-il-50000-n5.txt Download as CSV file: xf-goe226-il-50000-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 = 0.050 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.000 -0.0462 0.11803 0.11098 -0.0802 0.9281 0.1331
-8.750 -0.0456 0.11720 0.11016 -0.0845 0.9216 0.1375
-8.500 -0.0533 0.11683 0.10982 -0.0861 0.9117 0.1382
-8.250 -0.0209 0.11081 0.10376 -0.0874 0.9097 0.1406
-8.000 0.0014 0.10719 0.10010 -0.0899 0.9066 0.1430
-7.750 -0.0009 0.10595 0.09890 -0.0882 0.8967 0.1444
-7.500 0.0107 0.10342 0.09635 -0.0901 0.8916 0.1460
-7.250 0.0085 0.10222 0.09519 -0.0891 0.8829 0.1481
-6.750 -0.0243 0.09699 0.08994 -0.0924 0.8619 0.1073
-6.500 -0.0080 0.09404 0.08697 -0.0930 0.8578 0.1059
-6.250 -0.0007 0.09170 0.08463 -0.0933 0.8522 0.1038
-6.000 -0.0071 0.09025 0.08322 -0.0917 0.8431 0.1019
-5.750 0.0082 0.08644 0.07936 -0.0964 0.8385 0.0992
-5.500 -0.0057 0.08502 0.07799 -0.0949 0.8277 0.0978
-5.250 0.0136 0.08171 0.07462 -0.0992 0.8227 0.0985
-5.000 0.0173 0.07961 0.07252 -0.1000 0.8139 0.0992
-4.750 0.0388 0.07598 0.06882 -0.1050 0.8068 0.0999
-4.500 0.0829 0.07004 0.06270 -0.1163 0.8030 0.0996
-4.250 0.0937 0.06690 0.05949 -0.1196 0.7911 0.1000
-4.000 0.1659 0.05793 0.05008 -0.1398 0.7875 0.1044
-3.750 0.2521 0.04845 0.03969 -0.1627 0.7837 0.1097
-3.500 0.2707 0.04783 0.03905 -0.1625 0.7746 0.1129
-3.250 0.3337 0.04382 0.03433 -0.1727 0.7716 0.1198
-3.000 0.3830 0.04174 0.03192 -0.1776 0.7688 0.1270
-2.750 0.3988 0.04153 0.03157 -0.1772 0.7586 0.1314
-2.500 0.4433 0.03992 0.02956 -0.1808 0.7546 0.1403
-2.250 0.4852 0.03881 0.02830 -0.1831 0.7516 0.1500
-2.000 0.5001 0.03901 0.02841 -0.1821 0.7408 0.1569
-1.750 0.5403 0.03811 0.02731 -0.1840 0.7368 0.1705
-1.500 0.5606 0.03831 0.02758 -0.1832 0.7281 0.1804
-1.250 0.5926 0.03794 0.02715 -0.1839 0.7219 0.1957
-1.000 0.6328 0.03722 0.02632 -0.1854 0.7183 0.2166
-0.750 0.6476 0.03781 0.02693 -0.1839 0.7072 0.2315
-0.500 0.6857 0.03721 0.02620 -0.1850 0.7028 0.2582
-0.250 0.7054 0.03759 0.02658 -0.1840 0.6931 0.2786
0.000 0.7372 0.03731 0.02632 -0.1842 0.6872 0.3062
0.250 0.7763 0.03661 0.02556 -0.1851 0.6837 0.3391
0.500 0.7885 0.03744 0.02641 -0.1832 0.6714 0.3595
0.750 0.8261 0.03685 0.02573 -0.1838 0.6673 0.3916
1.000 0.8391 0.03766 0.02658 -0.1819 0.6556 0.4117
1.250 0.8737 0.03724 0.02614 -0.1821 0.6508 0.4467
1.750 0.9191 0.03775 0.02670 -0.1802 0.6343 0.5021
2.000 0.9582 0.03697 0.02587 -0.1809 0.6308 0.5293
2.250 0.9645 0.03824 0.02719 -0.1784 0.6178 0.5457
2.500 1.0025 0.03756 0.02648 -0.1791 0.6138 0.5751
2.750 1.0070 0.03899 0.02800 -0.1765 0.6017 0.5947
3.000 1.0412 0.03853 0.02755 -0.1768 0.5971 0.6311
3.500 1.0751 0.03959 0.02885 -0.1741 0.5808 0.7211
3.750 1.1065 0.03865 0.02799 -0.1735 0.5772 1.0000
4.000 1.1010 0.04133 0.03066 -0.1707 0.5644 1.0000
4.250 1.1377 0.04098 0.03011 -0.1714 0.5609 1.0000
4.500 1.1307 0.04395 0.03309 -0.1686 0.5490 1.0000
4.750 1.1632 0.04374 0.03275 -0.1687 0.5450 1.0000
5.250 1.1838 0.04699 0.03594 -0.1658 0.5295 1.0000
5.500 1.2213 0.04623 0.03507 -0.1660 0.5267 1.0000
5.750 1.2022 0.05051 0.03944 -0.1629 0.5143 1.0000
6.000 1.2375 0.04977 0.03862 -0.1628 0.5112 1.0000
6.500 1.2520 0.05359 0.04247 -0.1597 0.4959 1.0000
6.750 1.2890 0.05258 0.04140 -0.1595 0.4932 1.0000
7.250 1.3007 0.05673 0.04563 -0.1564 0.4783 1.0000
7.750 1.3032 0.06216 0.05117 -0.1534 0.4628 1.0000
8.000 1.3419 0.06075 0.04973 -0.1530 0.4608 1.0000
8.500 1.2797 0.07448 0.06372 -0.1494 0.4361 1.0000
8.750 1.2907 0.07626 0.06556 -0.1483 0.4301 1.0000
9.000 1.3210 0.07548 0.06479 -0.1474 0.4276 1.0000
9.250 1.3572 0.07402 0.06335 -0.1465 0.4258 1.0000
9.750 1.3333 0.08375 0.07327 -0.1444 0.4080 1.0000
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Polar data table (+)
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