Marsden (marsden-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: Marsden (marsden-il) Reynolds number: 1,000,000 Max Cl/Cd: 70.22 at α=4.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-marsden-il-1000000.txt Download as CSV file: xf-marsden-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: Marsden
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.250 -0.1003 0.05490 0.04911 -0.1826 0.4405 0.0414
-15.000 -0.1205 0.04952 0.04360 -0.1866 0.4404 0.0414
-14.750 -0.1281 0.04593 0.03991 -0.1891 0.4403 0.0415
-14.500 -0.1305 0.04309 0.03699 -0.1909 0.4402 0.0416
-14.250 -0.1295 0.04076 0.03458 -0.1922 0.4401 0.0417
-14.000 -0.1267 0.03873 0.03249 -0.1931 0.4400 0.0418
-13.750 -0.1222 0.03696 0.03066 -0.1938 0.4399 0.0419
-13.500 -0.1154 0.03546 0.02911 -0.1941 0.4397 0.0420
-13.250 -0.1076 0.03414 0.02775 -0.1942 0.4396 0.0422
-13.000 -0.0993 0.03291 0.02647 -0.1942 0.4394 0.0423
-12.750 -0.0894 0.03183 0.02535 -0.1940 0.4393 0.0425
-12.500 -0.0789 0.03086 0.02434 -0.1937 0.4391 0.0426
-12.250 -0.0675 0.02998 0.02343 -0.1933 0.4389 0.0428
-12.000 -0.0557 0.02915 0.02256 -0.1928 0.4388 0.0430
-11.750 -0.0438 0.02837 0.02174 -0.1922 0.4386 0.0432
-11.500 -0.0310 0.02762 0.02096 -0.1914 0.4384 0.0434
-11.250 -0.0180 0.02691 0.02021 -0.1906 0.4382 0.0435
-11.000 -0.0045 0.02628 0.01955 -0.1897 0.4380 0.0436
-10.750 0.0096 0.02568 0.01893 -0.1887 0.4378 0.0438
-10.500 0.0236 0.02513 0.01835 -0.1876 0.4376 0.0439
-10.250 0.0374 0.02462 0.01781 -0.1864 0.4374 0.0440
-10.000 0.0516 0.02415 0.01732 -0.1851 0.4372 0.0441
-9.750 0.0648 0.02373 0.01689 -0.1835 0.4370 0.0442
-9.500 0.0761 0.02337 0.01651 -0.1816 0.4368 0.0443
-9.250 0.0855 0.02310 0.01622 -0.1793 0.4366 0.0444
-9.000 0.0971 0.02281 0.01592 -0.1773 0.4363 0.0445
-8.750 0.1128 0.02249 0.01559 -0.1760 0.4361 0.0445
-8.500 0.1300 0.02218 0.01526 -0.1749 0.4358 0.0446
-8.250 0.1466 0.02171 0.01478 -0.1736 0.4354 0.0448
-8.000 0.1629 0.02122 0.01429 -0.1721 0.4351 0.0450
-7.750 0.1807 0.02082 0.01389 -0.1710 0.4348 0.0453
-7.500 0.2004 0.02046 0.01354 -0.1703 0.4346 0.0455
-7.250 0.2222 0.02016 0.01324 -0.1700 0.4343 0.0458
-7.000 0.2457 0.01988 0.01298 -0.1699 0.4340 0.0461
-6.750 0.2708 0.01964 0.01274 -0.1701 0.4338 0.0464
-6.500 0.2972 0.01941 0.01251 -0.1704 0.4335 0.0467
-6.250 0.3247 0.01920 0.01231 -0.1710 0.4332 0.0470
-6.000 0.3533 0.01901 0.01212 -0.1717 0.4329 0.0473
-5.750 0.3828 0.01883 0.01194 -0.1726 0.4326 0.0477
-5.500 0.4131 0.01868 0.01179 -0.1735 0.4323 0.0482
-5.250 0.4441 0.01854 0.01164 -0.1746 0.4320 0.0486
-5.000 0.4752 0.01844 0.01154 -0.1756 0.4316 0.0491
-4.750 0.5063 0.01836 0.01146 -0.1766 0.4313 0.0495
-4.500 0.5373 0.01829 0.01138 -0.1775 0.4309 0.0498
-4.250 0.5719 0.01799 0.01107 -0.1794 0.4305 0.0506
-4.000 0.6058 0.01781 0.01090 -0.1810 0.4300 0.0514
-3.750 0.6391 0.01772 0.01080 -0.1824 0.4296 0.0521
-3.500 0.6724 0.01766 0.01075 -0.1837 0.4292 0.0528
-3.250 0.7059 0.01761 0.01070 -0.1851 0.4288 0.0536
-3.000 0.7395 0.01761 0.01069 -0.1865 0.4284 0.0545
-2.750 0.7728 0.01765 0.01073 -0.1878 0.4281 0.0553
-2.500 0.8093 0.01762 0.01071 -0.1899 0.4278 0.0570
-2.250 0.8441 0.01767 0.01076 -0.1915 0.4274 0.0588
-2.000 0.8780 0.01776 0.01086 -0.1930 0.4271 0.0609
-1.750 0.9139 0.01783 0.01096 -0.1949 0.4267 0.0644
-1.500 0.9494 0.01796 0.01111 -0.1968 0.4263 0.0699
-1.250 0.9868 0.01811 0.01133 -0.1991 0.4259 0.0826
-1.000 1.0344 0.01823 0.01168 -0.2038 0.4253 0.1439
-0.750 1.0743 0.01981 0.01362 -0.2079 0.4232 0.2216
-0.500 1.1245 0.01965 0.01370 -0.2130 0.4231 0.3032
-0.250 1.1870 0.01942 0.01380 -0.2208 0.4229 0.4289
0.000 1.2410 0.01940 0.01406 -0.2265 0.4228 0.5465
0.250 1.2722 0.01956 0.01429 -0.2274 0.4226 0.5744
0.500 1.3008 0.01975 0.01449 -0.2278 0.4225 0.5900
0.750 1.3282 0.01994 0.01471 -0.2279 0.4223 0.6027
1.000 1.3554 0.02015 0.01492 -0.2280 0.4221 0.6120
1.250 1.3798 0.02039 0.01521 -0.2275 0.4218 0.6223
1.500 1.4039 0.02067 0.01549 -0.2270 0.4216 0.6319
1.750 1.4281 0.02089 0.01575 -0.2265 0.4213 0.6383
2.000 1.4509 0.02114 0.01603 -0.2258 0.4210 0.6425
2.250 1.4743 0.02138 0.01629 -0.2253 0.4207 0.6455
2.500 1.4975 0.02164 0.01656 -0.2247 0.4204 0.6489
2.750 1.5205 0.02190 0.01684 -0.2242 0.4200 0.6523
3.000 1.5426 0.02219 0.01714 -0.2235 0.4197 0.6556
3.250 1.5650 0.02244 0.01741 -0.2229 0.4193 0.6592
3.500 1.5841 0.02266 0.01766 -0.2217 0.4189 0.6625
3.750 1.6032 0.02291 0.01795 -0.2205 0.4184 0.6646
4.000 1.6239 0.02318 0.01824 -0.2196 0.4180 0.6663
4.250 1.6452 0.02345 0.01853 -0.2190 0.4175 0.6678
4.500 1.6664 0.02373 0.01883 -0.2183 0.4171 0.6693
4.750 1.6867 0.02403 0.01915 -0.2175 0.4166 0.6709
5.000 1.7060 0.02433 0.01947 -0.2166 0.4162 0.6724
5.250 1.7249 0.02464 0.01980 -0.2156 0.4157 0.6741
5.500 1.7435 0.02496 0.02015 -0.2146 0.4152 0.6758
5.750 1.7622 0.02528 0.02048 -0.2137 0.4148 0.6773
6.000 1.7805 0.02558 0.02079 -0.2127 0.4143 0.6785
6.250 1.7990 0.02586 0.02109 -0.2118 0.4139 0.6795
6.500 1.8182 0.02611 0.02135 -0.2110 0.4134 0.6804
6.750 1.8371 0.02640 0.02165 -0.2102 0.4130 0.6811
7.000 1.8589 0.02665 0.02191 -0.2100 0.4126 0.6833
7.250 1.8790 0.02694 0.02222 -0.2095 0.4122 0.6850
7.500 1.8978 0.02727 0.02257 -0.2088 0.4118 0.6866
7.750 1.9169 0.02758 0.02290 -0.2082 0.4114 0.6882
8.000 1.9363 0.02792 0.02325 -0.2076 0.4110 0.6896
8.250 1.9555 0.02829 0.02364 -0.2071 0.4106 0.6910
8.500 1.9750 0.02869 0.02406 -0.2067 0.4101 0.6923
8.750 1.9940 0.02916 0.02454 -0.2062 0.4096 0.6936
9.000 2.0064 0.03011 0.02552 -0.2050 0.4087 0.6949
9.250 1.4029 0.08464 0.08119 -0.1750 0.3795 0.6918
9.500 1.4321 0.08423 0.08077 -0.1754 0.3798 0.6931
9.750 1.4611 0.08383 0.08036 -0.1759 0.3799 0.6944
10.000 1.4902 0.08342 0.07995 -0.1764 0.3801 0.6957
10.250 1.6668 0.06691 0.06330 -0.1801 0.3922 0.6985
10.500 1.7001 0.06608 0.06245 -0.1807 0.3924 0.6998
10.750 1.7342 0.06516 0.06151 -0.1813 0.3925 0.7010
11.000 1.7701 0.06406 0.06039 -0.1819 0.3927 0.7023
11.250 1.8063 0.06291 0.05921 -0.1826 0.3929 0.7034
11.500 1.8446 0.06155 0.05783 -0.1833 0.3931 0.7043
11.750 1.8863 0.06002 0.05628 -0.1843 0.3933 0.7065
12.000 1.9302 0.05821 0.05444 -0.1853 0.3935 0.7085
12.250 1.4168 0.11809 0.11482 -0.1753 0.3446 0.7029
12.500 1.4398 0.11823 0.11495 -0.1757 0.3444 0.7038
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