MH 92 15.49% (mh92-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: MH 92 15.49% (mh92-il) Reynolds number: 1,000,000 Max Cl/Cd: 90.09 at α=10.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mh92-il-1000000-n5.txt Download as CSV file: xf-mh92-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: MH 92 15.49%
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
------ -------- --------- --------- -------- -------- --------
-18.750 -1.0057 0.13140 0.12879 0.0240 1.0000 0.0045
-18.500 -1.0391 0.11941 0.11663 0.0167 1.0000 0.0045
-18.250 -1.0673 0.10891 0.10596 0.0103 1.0000 0.0045
-18.000 -1.0962 0.09870 0.09557 0.0041 1.0000 0.0045
-17.750 -1.1196 0.08990 0.08663 -0.0012 1.0000 0.0045
-17.500 -1.1415 0.08173 0.07829 -0.0060 1.0000 0.0045
-17.250 -1.1587 0.07469 0.07112 -0.0100 1.0000 0.0045
-17.000 -1.1708 0.06879 0.06509 -0.0132 1.0000 0.0045
-16.750 -1.1863 0.06268 0.05881 -0.0164 1.0000 0.0044
-16.500 -1.1948 0.05790 0.05392 -0.0186 1.0000 0.0044
-16.250 -1.2030 0.05344 0.04934 -0.0204 1.0000 0.0044
-16.000 -1.2051 0.04998 0.04579 -0.0216 1.0000 0.0045
-15.750 -1.2120 0.04617 0.04185 -0.0225 1.0000 0.0045
-15.500 -1.2145 0.04311 0.03869 -0.0229 1.0000 0.0045
-15.250 -1.2156 0.04037 0.03585 -0.0230 1.0000 0.0045
-15.000 -1.2132 0.03812 0.03353 -0.0227 1.0000 0.0046
-14.750 -1.2127 0.03583 0.03114 -0.0222 1.0000 0.0046
-14.500 -1.2104 0.03381 0.02904 -0.0214 1.0000 0.0046
-14.250 -1.2058 0.03209 0.02724 -0.0204 1.0000 0.0047
-14.000 -1.2014 0.03042 0.02549 -0.0192 1.0000 0.0046
-13.750 -1.1923 0.02919 0.02420 -0.0180 1.0000 0.0048
-13.500 -1.1865 0.02775 0.02269 -0.0165 1.0000 0.0048
-13.250 -1.1786 0.02652 0.02139 -0.0149 1.0000 0.0048
-13.000 -1.1689 0.02545 0.02026 -0.0134 1.0000 0.0049
-12.750 -1.1591 0.02443 0.01918 -0.0117 1.0000 0.0049
-12.500 -1.1484 0.02348 0.01817 -0.0100 1.0000 0.0049
-12.250 -1.1373 0.02259 0.01721 -0.0082 1.0000 0.0050
-12.000 -1.1247 0.02180 0.01638 -0.0064 1.0000 0.0051
-11.750 -1.1110 0.02109 0.01562 -0.0047 1.0000 0.0052
-11.500 -1.0930 0.02031 0.01478 -0.0039 0.9504 0.0052
-11.250 -1.0817 0.01988 0.01415 -0.0012 0.8886 0.0053
-11.000 -1.0702 0.01938 0.01351 0.0014 0.8609 0.0054
-10.750 -1.0577 0.01883 0.01285 0.0039 0.8393 0.0054
-10.500 -1.0430 0.01838 0.01230 0.0061 0.8209 0.0055
-10.250 -1.0276 0.01791 0.01174 0.0081 0.8049 0.0056
-10.000 -1.0088 0.01748 0.01121 0.0096 0.7900 0.0056
-9.750 -0.9890 0.01704 0.01070 0.0109 0.7754 0.0057
-9.500 -0.9681 0.01665 0.01024 0.0121 0.7622 0.0058
-9.250 -0.9474 0.01621 0.00972 0.0133 0.7498 0.0058
-9.000 -0.9272 0.01570 0.00913 0.0145 0.7372 0.0060
-8.750 -0.9053 0.01527 0.00865 0.0156 0.7252 0.0062
-8.500 -0.8828 0.01489 0.00821 0.0165 0.7133 0.0064
-8.250 -0.8595 0.01455 0.00781 0.0173 0.7013 0.0064
-8.000 -0.8358 0.01422 0.00744 0.0181 0.6900 0.0067
-7.750 -0.8118 0.01391 0.00707 0.0188 0.6788 0.0069
-7.500 -0.7874 0.01361 0.00672 0.0194 0.6668 0.0071
-7.250 -0.7627 0.01333 0.00639 0.0200 0.6557 0.0073
-7.000 -0.7377 0.01306 0.00606 0.0206 0.6446 0.0076
-6.750 -0.7122 0.01281 0.00577 0.0211 0.6335 0.0078
-6.500 -0.6872 0.01253 0.00544 0.0217 0.6225 0.0083
-6.250 -0.6617 0.01228 0.00516 0.0222 0.6110 0.0088
-6.000 -0.6357 0.01206 0.00490 0.0226 0.6000 0.0095
-5.750 -0.6096 0.01186 0.00465 0.0230 0.5888 0.0101
-5.500 -0.5835 0.01163 0.00440 0.0234 0.5776 0.0114
-5.250 -0.5571 0.01143 0.00417 0.0237 0.5670 0.0130
-5.000 -0.5307 0.01124 0.00395 0.0241 0.5558 0.0156
-4.750 -0.5043 0.01103 0.00374 0.0244 0.5455 0.0197
-4.500 -0.4778 0.01084 0.00353 0.0248 0.5348 0.0253
-4.000 -0.4251 0.01039 0.00314 0.0254 0.5148 0.0468
-3.750 -0.3990 0.01014 0.00294 0.0258 0.5039 0.0658
-3.500 -0.3736 0.00981 0.00273 0.0262 0.4938 0.0974
-3.250 -0.3492 0.00940 0.00250 0.0268 0.4838 0.1481
-3.000 -0.3247 0.00898 0.00229 0.0273 0.4745 0.2050
-2.750 -0.3006 0.00855 0.00211 0.0279 0.4644 0.2714
-2.500 -0.2756 0.00820 0.00196 0.0284 0.4544 0.3293
-2.000 -0.2246 0.00763 0.00173 0.0292 0.4359 0.4350
-1.750 -0.1982 0.00744 0.00165 0.0295 0.4262 0.4788
-1.500 -0.1709 0.00733 0.00159 0.0297 0.4161 0.5070
-1.250 -0.1433 0.00724 0.00155 0.0298 0.4075 0.5322
-1.000 -0.1156 0.00719 0.00151 0.0299 0.3973 0.5555
-0.750 -0.0879 0.00711 0.00148 0.0300 0.3884 0.5794
-0.250 -0.0328 0.00697 0.00144 0.0303 0.3710 0.6316
0.000 -0.0051 0.00695 0.00144 0.0304 0.3614 0.6546
0.250 0.0230 0.00693 0.00144 0.0304 0.3540 0.6755
0.750 0.0794 0.00695 0.00149 0.0305 0.3375 0.7111
1.000 0.1076 0.00698 0.00152 0.0305 0.3292 0.7255
1.250 0.1361 0.00701 0.00156 0.0305 0.3225 0.7386
1.500 0.1646 0.00708 0.00160 0.0304 0.3142 0.7502
1.750 0.1931 0.00713 0.00166 0.0304 0.3078 0.7615
2.000 0.2217 0.00718 0.00171 0.0303 0.3015 0.7707
2.250 0.2502 0.00727 0.00177 0.0302 0.2947 0.7803
2.500 0.2788 0.00732 0.00184 0.0302 0.2888 0.7887
2.750 0.3072 0.00741 0.00191 0.0301 0.2819 0.7981
3.000 0.3355 0.00749 0.00199 0.0301 0.2767 0.8072
3.250 0.3640 0.00757 0.00207 0.0300 0.2717 0.8162
3.500 0.3923 0.00767 0.00216 0.0299 0.2656 0.8229
3.750 0.4206 0.00777 0.00226 0.0299 0.2603 0.8291
4.000 0.4491 0.00786 0.00235 0.0297 0.2548 0.8348
4.250 0.4774 0.00798 0.00244 0.0297 0.2496 0.8397
4.500 0.5055 0.00809 0.00256 0.0296 0.2449 0.8448
4.750 0.5337 0.00819 0.00266 0.0295 0.2400 0.8501
5.000 0.5619 0.00833 0.00277 0.0294 0.2342 0.8548
5.250 0.5896 0.00846 0.00290 0.0294 0.2295 0.8594
5.500 0.6176 0.00856 0.00303 0.0294 0.2255 0.8643
5.750 0.6452 0.00871 0.00316 0.0293 0.2200 0.8695
6.000 0.6728 0.00887 0.00331 0.0293 0.2147 0.8743
6.250 0.7001 0.00899 0.00346 0.0293 0.2109 0.8797
6.500 0.7272 0.00914 0.00361 0.0294 0.2057 0.8856
6.750 0.7542 0.00934 0.00378 0.0294 0.2004 0.8908
7.000 0.7813 0.00947 0.00395 0.0295 0.1962 0.8950
7.250 0.8077 0.00966 0.00413 0.0296 0.1902 0.8995
7.500 0.8340 0.00986 0.00432 0.0297 0.1847 0.9041
7.750 0.8609 0.01003 0.00450 0.0298 0.1806 0.9082
8.000 0.8868 0.01023 0.00470 0.0300 0.1759 0.9122
8.250 0.9122 0.01044 0.00493 0.0302 0.1713 0.9167
8.500 0.9382 0.01062 0.00513 0.0304 0.1677 0.9213
8.750 0.9638 0.01085 0.00535 0.0306 0.1632 0.9255
9.250 1.0129 0.01129 0.00583 0.0313 0.1552 0.9352
9.500 1.0375 0.01152 0.00607 0.0317 0.1513 0.9403
9.750 1.0608 0.01181 0.00636 0.0322 0.1463 0.9453
10.000 1.0845 0.01204 0.00663 0.0327 0.1429 0.9513
10.250 1.1081 0.01230 0.00690 0.0331 0.1390 0.9575
10.500 1.1322 0.01263 0.00724 0.0334 0.1342 0.9637
11.000 1.1852 0.01329 0.00793 0.0327 0.1252 0.9754
11.250 1.2126 0.01374 0.00837 0.0320 0.1199 0.9816
11.500 1.2427 0.01413 0.00878 0.0308 0.1151 0.9858
11.750 1.2711 0.01467 0.00929 0.0296 0.1092 0.9909
12.000 1.2991 0.01513 0.00978 0.0287 0.1048 0.9981
12.250 1.3146 0.01566 0.01029 0.0300 0.0997 1.0000
12.500 1.3237 0.01614 0.01079 0.0325 0.0962 1.0000
12.750 1.3313 0.01670 0.01137 0.0350 0.0926 1.0000
13.000 1.3376 0.01749 0.01216 0.0372 0.0883 1.0000
13.250 1.3462 0.01832 0.01300 0.0388 0.0841 1.0000
13.500 1.3540 0.01930 0.01399 0.0402 0.0806 1.0000
13.750 1.3610 0.02044 0.01515 0.0414 0.0769 1.0000
14.000 1.3706 0.02150 0.01625 0.0423 0.0748 1.0000
14.250 1.3774 0.02282 0.01761 0.0431 0.0720 1.0000
14.500 1.3828 0.02435 0.01916 0.0437 0.0695 1.0000
14.750 1.3897 0.02584 0.02071 0.0441 0.0675 1.0000
15.000 1.3954 0.02750 0.02241 0.0444 0.0653 1.0000
15.250 1.3983 0.02946 0.02441 0.0446 0.0632 1.0000
15.500 1.3978 0.03181 0.02681 0.0446 0.0604 1.0000
15.750 1.4012 0.03389 0.02895 0.0445 0.0590 1.0000
16.000 1.4031 0.03616 0.03129 0.0442 0.0578 1.0000
16.250 1.4002 0.03897 0.03416 0.0438 0.0558 1.0000
16.500 1.3957 0.04202 0.03726 0.0432 0.0543 1.0000
16.750 1.3912 0.04516 0.04047 0.0425 0.0526 1.0000
17.000 1.3873 0.04834 0.04373 0.0416 0.0514 1.0000
17.250 1.3815 0.05185 0.04732 0.0405 0.0501 1.0000
17.500 1.3732 0.05574 0.05128 0.0392 0.0489 1.0000
17.750 1.3622 0.06004 0.05565 0.0377 0.0475 1.0000
18.000 1.3512 0.06446 0.06014 0.0361 0.0465 1.0000
18.250 1.3428 0.06861 0.06438 0.0345 0.0456 1.0000
18.500 1.3329 0.07305 0.06891 0.0328 0.0446 1.0000
18.750 1.3210 0.07786 0.07380 0.0308 0.0436 1.0000
19.000 1.3075 0.08295 0.07897 0.0286 0.0425 1.0000
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