HOBIESMO1.DAT (hobiesm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: HOBIESMO1.DAT (hobiesm-il) Reynolds number: 1,000,000 Max Cl/Cd: 118.23 at α=3.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-hobiesm-il-1000000-n5.txt Download as CSV file: xf-hobiesm-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: HOBIESMO1.DAT
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
------ -------- --------- --------- -------- -------- --------
-12.000 -0.6864 0.06941 0.06763 -0.0467 1.0000 0.0040
-11.750 -0.7629 0.05557 0.05374 -0.0565 1.0000 0.0036
-11.500 -0.8273 0.02872 0.02626 -0.0824 1.0000 0.0032
-11.250 -0.8052 0.02422 0.02137 -0.0873 0.9978 0.0034
-11.000 -0.7773 0.02190 0.01882 -0.0901 0.9950 0.0036
-10.750 -0.7501 0.02024 0.01696 -0.0918 0.9920 0.0038
-10.500 -0.7222 0.01889 0.01545 -0.0933 0.9883 0.0040
-10.250 -0.6925 0.01777 0.01418 -0.0947 0.9849 0.0042
-10.000 -0.6627 0.01679 0.01306 -0.0960 0.9815 0.0045
-9.750 -0.6342 0.01591 0.01205 -0.0969 0.9760 0.0047
-9.500 -0.6023 0.01510 0.01110 -0.0984 0.9718 0.0050
-9.250 -0.5705 0.01443 0.01030 -0.0997 0.9663 0.0052
-9.000 -0.5390 0.01345 0.00917 -0.1011 0.9586 0.0059
-8.750 -0.5066 0.01291 0.00857 -0.1025 0.9494 0.0065
-8.500 -0.4750 0.01245 0.00803 -0.1035 0.9377 0.0071
-8.250 -0.4461 0.01203 0.00749 -0.1039 0.9231 0.0077
-8.000 -0.4189 0.01168 0.00701 -0.1039 0.9085 0.0081
-7.750 -0.3926 0.01131 0.00652 -0.1036 0.8948 0.0086
-7.500 -0.3666 0.01092 0.00601 -0.1034 0.8823 0.0095
-7.250 -0.3401 0.01072 0.00575 -0.1031 0.8710 0.0104
-7.000 -0.3134 0.01052 0.00548 -0.1029 0.8606 0.0113
-6.750 -0.2866 0.01029 0.00516 -0.1027 0.8511 0.0121
-6.500 -0.2599 0.01008 0.00487 -0.1025 0.8420 0.0127
-6.250 -0.2329 0.00989 0.00460 -0.1023 0.8330 0.0130
-6.000 -0.2061 0.00957 0.00416 -0.1021 0.8247 0.0137
-5.750 -0.1795 0.00917 0.00364 -0.1019 0.8162 0.0151
-5.500 -0.1524 0.00890 0.00330 -0.1017 0.8081 0.0160
-5.250 -0.1253 0.00869 0.00302 -0.1016 0.8001 0.0168
-5.000 -0.0979 0.00849 0.00276 -0.1014 0.7918 0.0176
-4.750 -0.0706 0.00831 0.00250 -0.1012 0.7838 0.0181
-4.500 -0.0432 0.00815 0.00225 -0.1011 0.7752 0.0186
-4.250 -0.0157 0.00801 0.00204 -0.1009 0.7670 0.0192
-4.000 0.0117 0.00789 0.00185 -0.1008 0.7586 0.0199
-3.750 0.0393 0.00773 0.00166 -0.1006 0.7495 0.0242
-3.500 0.0666 0.00754 0.00147 -0.1005 0.7407 0.0354
-3.000 0.1211 0.00720 0.00121 -0.1002 0.7215 0.0760
-2.750 0.1486 0.00712 0.00112 -0.1001 0.7114 0.0870
-2.500 0.1760 0.00706 0.00104 -0.0999 0.7010 0.0962
-2.250 0.2034 0.00703 0.00097 -0.0998 0.6896 0.1039
-2.000 0.2309 0.00697 0.00091 -0.0997 0.6779 0.1151
-1.750 0.2583 0.00693 0.00086 -0.0995 0.6660 0.1273
-1.500 0.2856 0.00690 0.00082 -0.0994 0.6534 0.1390
-1.250 0.3129 0.00686 0.00079 -0.0992 0.6407 0.1590
-1.000 0.3400 0.00682 0.00077 -0.0991 0.6272 0.1805
-0.750 0.3673 0.00681 0.00076 -0.0989 0.6139 0.2007
-0.500 0.3944 0.00680 0.00076 -0.0987 0.6003 0.2196
-0.250 0.4216 0.00681 0.00077 -0.0986 0.5866 0.2379
0.000 0.4488 0.00684 0.00079 -0.0984 0.5730 0.2563
0.250 0.4759 0.00686 0.00081 -0.0982 0.5599 0.2745
0.500 0.5030 0.00689 0.00085 -0.0981 0.5470 0.2955
0.750 0.5301 0.00691 0.00090 -0.0979 0.5342 0.3199
1.000 0.5572 0.00695 0.00095 -0.0978 0.5216 0.3414
1.250 0.5843 0.00699 0.00101 -0.0976 0.5093 0.3627
1.500 0.6113 0.00701 0.00108 -0.0974 0.4973 0.3928
1.750 0.6380 0.00700 0.00116 -0.0973 0.4854 0.4401
2.000 0.6644 0.00693 0.00126 -0.0971 0.4733 0.5163
2.250 0.6901 0.00679 0.00138 -0.0967 0.4613 0.6319
2.750 0.7469 0.00636 0.00163 -0.0970 0.4239 1.0000
3.000 0.7731 0.00656 0.00175 -0.0967 0.4032 1.0000
3.250 0.7992 0.00676 0.00188 -0.0964 0.3839 1.0000
3.500 0.8242 0.00705 0.00205 -0.0959 0.3533 1.0000
3.750 0.8479 0.00750 0.00227 -0.0952 0.3054 1.0000
4.000 0.8697 0.00814 0.00259 -0.0943 0.2401 1.0000
4.250 0.8915 0.00880 0.00295 -0.0934 0.1791 1.0000
4.500 0.9058 0.01030 0.00378 -0.0914 0.0392 1.0000
4.750 0.9302 0.01068 0.00409 -0.0908 0.0227 1.0000
5.000 0.9552 0.01098 0.00436 -0.0903 0.0178 1.0000
5.250 0.9804 0.01125 0.00464 -0.0899 0.0145 1.0000
5.500 1.0051 0.01156 0.00493 -0.0894 0.0115 1.0000
5.750 1.0296 0.01190 0.00529 -0.0888 0.0095 1.0000
6.000 1.0542 0.01220 0.00562 -0.0883 0.0084 1.0000
6.250 1.0783 0.01255 0.00597 -0.0877 0.0075 1.0000
6.500 1.1017 0.01296 0.00640 -0.0870 0.0066 1.0000
6.750 1.1242 0.01348 0.00697 -0.0861 0.0059 1.0000
7.000 1.1477 0.01383 0.00736 -0.0854 0.0056 1.0000
7.250 1.1710 0.01421 0.00776 -0.0847 0.0051 1.0000
7.500 1.1933 0.01467 0.00828 -0.0839 0.0048 1.0000
7.750 1.2153 0.01513 0.00878 -0.0830 0.0044 1.0000
8.000 1.2368 0.01562 0.00931 -0.0820 0.0042 1.0000
8.250 1.2571 0.01620 0.00992 -0.0809 0.0039 1.0000
8.500 1.2745 0.01702 0.01082 -0.0793 0.0036 1.0000
8.750 1.2901 0.01793 0.01183 -0.0775 0.0034 1.0000
9.000 1.3089 0.01851 0.01247 -0.0761 0.0034 1.0000
9.250 1.3262 0.01918 0.01323 -0.0746 0.0033 1.0000
9.500 1.3413 0.01997 0.01410 -0.0727 0.0032 1.0000
9.750 1.3546 0.02077 0.01499 -0.0706 0.0030 1.0000
10.000 1.3652 0.02156 0.01586 -0.0680 0.0029 1.0000
10.250 1.3735 0.02248 0.01687 -0.0651 0.0028 1.0000
10.500 1.3828 0.02338 0.01784 -0.0625 0.0027 1.0000
10.750 1.3902 0.02444 0.01899 -0.0599 0.0026 1.0000
11.000 1.4001 0.02535 0.01997 -0.0578 0.0025 1.0000
11.250 1.4105 0.02627 0.02095 -0.0559 0.0024 1.0000
11.500 1.4181 0.02744 0.02221 -0.0539 0.0024 1.0000
11.750 1.4252 0.02872 0.02357 -0.0520 0.0023 1.0000
12.000 1.4304 0.03023 0.02520 -0.0501 0.0022 1.0000
12.250 1.4389 0.03149 0.02653 -0.0487 0.0022 1.0000
12.500 1.4425 0.03328 0.02842 -0.0471 0.0021 1.0000
12.750 1.4449 0.03529 0.03054 -0.0457 0.0021 1.0000
13.000 1.4443 0.03769 0.03306 -0.0443 0.0020 1.0000
13.250 1.4419 0.04041 0.03592 -0.0432 0.0020 1.0000
13.500 1.4378 0.04347 0.03914 -0.0423 0.0020 1.0000
13.750 1.4339 0.04666 0.04247 -0.0417 0.0019 1.0000
14.000 1.4206 0.05122 0.04724 -0.0414 0.0019 1.0000
14.250 1.4084 0.05589 0.05212 -0.0417 0.0019 1.0000
14.500 1.4026 0.05987 0.05624 -0.0423 0.0019 1.0000
14.750 1.3936 0.06456 0.06109 -0.0434 0.0019 1.0000
15.000 1.3849 0.06945 0.06614 -0.0448 0.0019 1.0000
15.250 1.3717 0.07533 0.07219 -0.0469 0.0019 1.0000
15.500 1.3633 0.08066 0.07766 -0.0491 0.0018 1.0000
15.750 1.3484 0.08744 0.08461 -0.0521 0.0018 1.0000
16.000 1.3323 0.09477 0.09210 -0.0556 0.0018 1.0000
16.250 1.3158 0.10256 0.10006 -0.0596 0.0018 1.0000
16.500 1.2990 0.11076 0.10841 -0.0641 0.0018 1.0000
16.750 1.2780 0.12027 0.11809 -0.0694 0.0018 1.0000
17.000 1.2558 0.13059 0.12857 -0.0755 0.0018 1.0000
17.250 1.2344 0.14123 0.13936 -0.0818 0.0019 1.0000
17.500 1.2029 0.15537 0.15368 -0.0904 0.0019 1.0000
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