WORTMANN FX 08-S-176 AIRFOIL (fx08s176-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 08-S-176 AIRFOIL (fx08s176-il) Reynolds number: 1,000,000 Max Cl/Cd: 139.29 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx08s176-il-1000000-n5.txt Download as CSV file: xf-fx08s176-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 08-S-176 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
------ -------- --------- --------- -------- -------- --------
-14.000 -0.6743 0.03540 0.03133 -0.1177 0.5681 0.0049
-13.750 -0.6893 0.03246 0.02820 -0.1155 0.5674 0.0049
-13.500 -0.6986 0.03011 0.02566 -0.1128 0.5667 0.0049
-13.250 -0.6984 0.02849 0.02391 -0.1105 0.5659 0.0050
-13.000 -0.6985 0.02690 0.02216 -0.1078 0.5650 0.0052
-12.750 -0.6948 0.02571 0.02083 -0.1051 0.5642 0.0053
-12.500 -0.6911 0.02466 0.01965 -0.1021 0.5634 0.0053
-12.250 -0.6819 0.02360 0.01845 -0.0999 0.5625 0.0054
-12.000 -0.6686 0.02270 0.01740 -0.0982 0.5616 0.0055
-11.750 -0.6543 0.02178 0.01635 -0.0967 0.5607 0.0056
-11.500 -0.6385 0.02088 0.01534 -0.0953 0.5602 0.0058
-11.250 -0.6205 0.02014 0.01449 -0.0942 0.5596 0.0060
-11.000 -0.6006 0.01951 0.01380 -0.0933 0.5590 0.0063
-10.750 -0.5790 0.01905 0.01330 -0.0926 0.5581 0.0066
-10.500 -0.5568 0.01862 0.01282 -0.0919 0.5573 0.0069
-10.250 -0.5342 0.01821 0.01236 -0.0913 0.5564 0.0073
-10.000 -0.5125 0.01766 0.01171 -0.0906 0.5555 0.0075
-9.750 -0.4894 0.01725 0.01122 -0.0901 0.5547 0.0079
-9.500 -0.4664 0.01679 0.01068 -0.0895 0.5539 0.0081
-9.250 -0.4435 0.01629 0.01010 -0.0889 0.5531 0.0084
-9.000 -0.4195 0.01591 0.00968 -0.0885 0.5522 0.0088
-8.750 -0.3947 0.01564 0.00938 -0.0882 0.5514 0.0092
-8.500 -0.3692 0.01545 0.00915 -0.0880 0.5506 0.0096
-8.250 -0.3443 0.01516 0.00881 -0.0876 0.5498 0.0099
-8.000 -0.3190 0.01491 0.00852 -0.0874 0.5490 0.0104
-7.750 -0.2938 0.01463 0.00817 -0.0871 0.5480 0.0108
-7.500 -0.2684 0.01438 0.00786 -0.0869 0.5470 0.0113
-7.250 -0.2425 0.01417 0.00759 -0.0867 0.5461 0.0116
-7.000 -0.2159 0.01401 0.00740 -0.0866 0.5455 0.0118
-6.750 -0.1920 0.01344 0.00678 -0.0862 0.5449 0.0125
-6.500 -0.1660 0.01319 0.00652 -0.0860 0.5442 0.0129
-6.250 -0.1396 0.01297 0.00628 -0.0860 0.5435 0.0134
-6.000 -0.1131 0.01278 0.00606 -0.0859 0.5428 0.0139
-5.750 -0.0866 0.01257 0.00582 -0.0858 0.5421 0.0145
-5.500 -0.0599 0.01237 0.00559 -0.0858 0.5413 0.0152
-5.250 -0.0336 0.01213 0.00531 -0.0857 0.5405 0.0156
-5.000 -0.0069 0.01192 0.00507 -0.0856 0.5397 0.0160
-4.750 0.0201 0.01176 0.00488 -0.0856 0.5389 0.0163
-4.500 0.0468 0.01156 0.00465 -0.0856 0.5380 0.0165
-4.250 0.0721 0.01116 0.00419 -0.0854 0.5370 0.0172
-4.000 0.0984 0.01089 0.00389 -0.0853 0.5361 0.0179
-3.750 0.1254 0.01071 0.00368 -0.0853 0.5353 0.0185
-3.500 0.1525 0.01055 0.00350 -0.0853 0.5345 0.0192
-3.250 0.1798 0.01042 0.00335 -0.0854 0.5336 0.0200
-3.000 0.2073 0.01031 0.00321 -0.0856 0.5327 0.0208
-2.750 0.2350 0.01021 0.00308 -0.0857 0.5319 0.0215
-2.500 0.2630 0.01010 0.00296 -0.0860 0.5313 0.0220
-2.250 0.2910 0.00999 0.00285 -0.0862 0.5306 0.0227
-2.000 0.3191 0.00988 0.00273 -0.0864 0.5297 0.0245
-1.750 0.3472 0.00978 0.00265 -0.0867 0.5288 0.0273
-1.500 0.3753 0.00967 0.00258 -0.0870 0.5278 0.0360
-1.250 0.4034 0.00953 0.00253 -0.0873 0.5267 0.0582
-1.000 0.4317 0.00946 0.00247 -0.0877 0.5253 0.0681
-0.750 0.4601 0.00938 0.00241 -0.0880 0.5238 0.0789
-0.500 0.4883 0.00927 0.00236 -0.0884 0.5224 0.0990
-0.250 0.5159 0.00900 0.00231 -0.0888 0.5209 0.1842
0.000 0.5419 0.00767 0.00219 -0.0899 0.5195 0.6048
0.250 0.5711 0.00729 0.00219 -0.0907 0.5180 0.7249
0.500 0.5985 0.00725 0.00238 -0.0906 0.5169 0.7991
0.750 0.6270 0.00734 0.00249 -0.0909 0.5154 0.8210
1.000 0.6566 0.00741 0.00255 -0.0914 0.5137 0.8317
1.250 0.6847 0.00748 0.00262 -0.0916 0.5120 0.8366
1.500 0.7136 0.00755 0.00268 -0.0921 0.5105 0.8411
1.750 0.7429 0.00761 0.00272 -0.0926 0.5091 0.8452
2.000 0.7719 0.00766 0.00274 -0.0931 0.5077 0.8471
2.250 0.7999 0.00773 0.00280 -0.0934 0.5062 0.8494
2.500 0.8273 0.00783 0.00290 -0.0935 0.5045 0.8535
2.750 0.8563 0.00788 0.00296 -0.0940 0.5032 0.8555
3.000 0.8854 0.00793 0.00302 -0.0946 0.5017 0.8570
3.250 0.9145 0.00799 0.00308 -0.0952 0.5001 0.8588
3.500 0.9436 0.00804 0.00314 -0.0958 0.4983 0.8602
3.750 0.9726 0.00810 0.00319 -0.0964 0.4965 0.8611
4.000 1.0009 0.00814 0.00325 -0.0969 0.4946 0.8620
4.250 1.0290 0.00820 0.00331 -0.0973 0.4927 0.8629
4.500 1.0566 0.00828 0.00338 -0.0976 0.4908 0.8641
4.750 1.0849 0.00834 0.00348 -0.0981 0.4890 0.8652
5.000 1.1131 0.00840 0.00358 -0.0986 0.4868 0.8662
5.250 1.1411 0.00846 0.00366 -0.0990 0.4831 0.8672
5.500 1.1678 0.00855 0.00374 -0.0992 0.4766 0.8682
5.750 1.1954 0.00863 0.00384 -0.0996 0.4701 0.8692
6.000 1.2216 0.00877 0.00395 -0.0997 0.4634 0.8704
6.250 1.2456 0.00900 0.00412 -0.0995 0.4434 0.8717
6.500 1.2615 0.00965 0.00456 -0.0979 0.4050 0.8733
6.750 1.2766 0.01035 0.00510 -0.0963 0.3738 0.8746
7.000 1.2895 0.01111 0.00571 -0.0943 0.3454 0.8759
7.250 1.2997 0.01185 0.00634 -0.0918 0.3209 0.8775
7.500 1.3032 0.01275 0.00709 -0.0882 0.2911 0.8792
7.750 1.2817 0.01410 0.00824 -0.0803 0.2477 0.8820
8.000 1.2465 0.01625 0.01024 -0.0715 0.2099 0.8851
8.250 1.2173 0.01927 0.01322 -0.0662 0.1861 0.8881
8.500 1.1876 0.02346 0.01735 -0.0626 0.1582 0.8904
8.750 1.1668 0.02697 0.02079 -0.0596 0.1341 0.8923
9.000 1.1339 0.03124 0.02495 -0.0558 0.0985 0.8943
9.250 1.1196 0.03425 0.02788 -0.0534 0.0752 0.8958
9.500 1.0974 0.03792 0.03143 -0.0507 0.0399 0.8975
9.750 1.0896 0.04071 0.03415 -0.0492 0.0174 0.8988
10.000 1.0913 0.04290 0.03633 -0.0483 0.0077 0.8998
10.250 1.1001 0.04453 0.03800 -0.0479 0.0066 0.9006
10.500 1.1100 0.04609 0.03960 -0.0476 0.0059 0.9015
10.750 1.1192 0.04776 0.04130 -0.0474 0.0056 0.9023
11.000 1.1283 0.04947 0.04306 -0.0471 0.0054 0.9031
11.250 1.1375 0.05120 0.04482 -0.0469 0.0050 0.9038
11.500 1.1467 0.05295 0.04662 -0.0468 0.0048 0.9045
12.000 1.1615 0.05688 0.05065 -0.0464 0.0042 0.9061
12.250 1.1688 0.05889 0.05271 -0.0463 0.0041 0.9070
12.500 1.1721 0.06139 0.05528 -0.0461 0.0037 0.9078
12.750 1.1817 0.06322 0.05715 -0.0462 0.0036 0.9087
13.000 1.1890 0.06534 0.05932 -0.0462 0.0035 0.9097
13.250 1.1954 0.06759 0.06163 -0.0463 0.0033 0.9107
13.500 1.2024 0.06980 0.06389 -0.0464 0.0033 0.9117
13.750 1.2086 0.07215 0.06630 -0.0466 0.0031 0.9126
14.000 1.2136 0.07472 0.06894 -0.0468 0.0030 0.9135
14.250 1.2205 0.07706 0.07132 -0.0471 0.0029 0.9143
14.500 1.2252 0.07972 0.07404 -0.0475 0.0028 0.9151
14.750 1.2298 0.08242 0.07680 -0.0479 0.0027 0.9159
15.000 1.2352 0.08505 0.07949 -0.0484 0.0027 0.9167
15.250 1.2395 0.08790 0.08239 -0.0489 0.0026 0.9174
15.500 1.2445 0.09064 0.08518 -0.0495 0.0025 0.9181
16.000 1.2494 0.09694 0.09161 -0.0509 0.0024 0.9196
16.250 1.2476 0.10076 0.09552 -0.0517 0.0023 0.9203
16.500 1.2467 0.10447 0.09932 -0.0526 0.0022 0.9211
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