MH 94 16.03% (mh94-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: MH 94 16.03% (mh94-il) Reynolds number: 200,000 Max Cl/Cd: 45.87 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-mh94-il-200000-n5.txt Download as CSV file: xf-mh94-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: MH 94 16.03%
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.750 -0.6610 0.11895 0.11421 -0.0469 1.0000 0.0147
-16.500 -0.7018 0.10613 0.10116 -0.0541 1.0000 0.0146
-16.250 -0.7336 0.09620 0.09099 -0.0595 1.0000 0.0146
-16.000 -0.7527 0.08936 0.08398 -0.0629 1.0000 0.0145
-15.750 -0.7713 0.08302 0.07746 -0.0659 1.0000 0.0144
-15.500 -0.7859 0.07766 0.07193 -0.0682 1.0000 0.0144
-15.250 -0.8006 0.07258 0.06667 -0.0700 1.0000 0.0144
-15.000 -0.8115 0.06832 0.06225 -0.0712 1.0000 0.0144
-14.750 -0.8223 0.06431 0.05806 -0.0721 1.0000 0.0146
-14.500 -0.8302 0.06086 0.05445 -0.0724 1.0000 0.0147
-14.250 -0.8369 0.05772 0.05115 -0.0724 1.0000 0.0148
-14.000 -0.8414 0.05495 0.04824 -0.0721 1.0000 0.0148
-13.750 -0.8444 0.05245 0.04560 -0.0715 1.0000 0.0149
-13.500 -0.8463 0.05014 0.04315 -0.0706 1.0000 0.0150
-13.250 -0.8472 0.04802 0.04090 -0.0695 1.0000 0.0151
-13.000 -0.8473 0.04604 0.03882 -0.0683 1.0000 0.0152
-12.750 -0.8461 0.04430 0.03703 -0.0668 1.0000 0.0153
-12.500 -0.8450 0.04264 0.03533 -0.0653 1.0000 0.0155
-12.250 -0.8440 0.04107 0.03372 -0.0636 1.0000 0.0156
-12.000 -0.8431 0.03957 0.03217 -0.0617 1.0000 0.0158
-11.750 -0.8425 0.03815 0.03070 -0.0597 1.0000 0.0160
-11.500 -0.8417 0.03682 0.02932 -0.0575 1.0000 0.0161
-11.250 -0.8420 0.03550 0.02796 -0.0550 1.0000 0.0164
-11.000 -0.8422 0.03430 0.02669 -0.0524 1.0000 0.0165
-10.750 -0.8435 0.03314 0.02548 -0.0494 1.0000 0.0167
-10.500 -0.8460 0.03202 0.02431 -0.0462 1.0000 0.0171
-10.250 -0.8496 0.03099 0.02322 -0.0427 1.0000 0.0173
-10.000 -0.8549 0.03005 0.02221 -0.0387 1.0000 0.0176
-9.750 -0.8390 0.02889 0.02097 -0.0387 0.9969 0.0179
-9.500 -0.8205 0.02779 0.01981 -0.0392 0.9933 0.0184
-9.250 -0.8053 0.02684 0.01883 -0.0386 0.9885 0.0190
-9.000 -0.7841 0.02594 0.01787 -0.0389 0.9846 0.0198
-8.750 -0.7619 0.02505 0.01691 -0.0392 0.9810 0.0207
-8.500 -0.7429 0.02420 0.01601 -0.0387 0.9759 0.0217
-8.250 -0.7174 0.02344 0.01522 -0.0393 0.9724 0.0233
-8.000 -0.6935 0.02270 0.01443 -0.0395 0.9686 0.0254
-7.750 -0.6735 0.02201 0.01372 -0.0388 0.9630 0.0277
-7.500 -0.6471 0.02126 0.01294 -0.0393 0.9594 0.0309
-7.250 -0.6173 0.02054 0.01221 -0.0405 0.9569 0.0355
-7.000 -0.6025 0.01994 0.01161 -0.0384 0.9495 0.0409
-6.750 -0.5759 0.01923 0.01096 -0.0389 0.9456 0.0517
-6.500 -0.5463 0.01847 0.01030 -0.0399 0.9430 0.0711
-6.250 -0.5320 0.01778 0.00976 -0.0378 0.9352 0.0955
-6.000 -0.5078 0.01682 0.00911 -0.0380 0.9308 0.1484
-5.750 -0.4798 0.01586 0.00850 -0.0390 0.9280 0.2167
-5.500 -0.4656 0.01519 0.00810 -0.0368 0.9197 0.2710
-5.250 -0.4383 0.01455 0.00772 -0.0371 0.9155 0.3279
-5.000 -0.4062 0.01407 0.00741 -0.0382 0.9127 0.3747
-4.750 -0.3855 0.01377 0.00722 -0.0368 0.9054 0.4088
-4.500 -0.3568 0.01346 0.00702 -0.0370 0.9005 0.4452
-4.250 -0.3236 0.01318 0.00682 -0.0379 0.8974 0.4795
-4.000 -0.2875 0.01293 0.00662 -0.0394 0.8952 0.5025
-3.500 -0.2341 0.01261 0.00628 -0.0385 0.8816 0.5299
-3.250 -0.1959 0.01239 0.00606 -0.0403 0.8787 0.5425
-3.000 -0.1743 0.01230 0.00592 -0.0389 0.8688 0.5540
-2.750 -0.1384 0.01210 0.00575 -0.0402 0.8640 0.5653
-2.500 -0.1062 0.01196 0.00558 -0.0408 0.8573 0.5764
-2.250 -0.0764 0.01182 0.00544 -0.0409 0.8486 0.5876
-2.000 -0.0371 0.01163 0.00524 -0.0429 0.8432 0.5979
-1.750 -0.0106 0.01155 0.00513 -0.0424 0.8313 0.6080
-1.500 0.0246 0.01141 0.00499 -0.0435 0.8223 0.6166
-1.250 0.0571 0.01130 0.00484 -0.0442 0.8106 0.6262
-1.000 0.0881 0.01121 0.00475 -0.0445 0.7975 0.6342
-0.750 0.1209 0.01114 0.00463 -0.0452 0.7835 0.6430
-0.500 0.1530 0.01108 0.00452 -0.0458 0.7680 0.6511
-0.250 0.1835 0.01106 0.00445 -0.0460 0.7509 0.6590
0.000 0.2130 0.01106 0.00437 -0.0461 0.7328 0.6677
0.250 0.2409 0.01109 0.00436 -0.0458 0.7136 0.6747
0.500 0.2682 0.01114 0.00434 -0.0454 0.6937 0.6829
0.750 0.2946 0.01121 0.00434 -0.0449 0.6730 0.6903
1.000 0.3202 0.01130 0.00437 -0.0442 0.6513 0.6978
1.250 0.3455 0.01141 0.00438 -0.0435 0.6288 0.7064
1.500 0.3694 0.01154 0.00445 -0.0425 0.6053 0.7128
1.750 0.3928 0.01169 0.00450 -0.0414 0.5799 0.7209
2.000 0.4152 0.01186 0.00456 -0.0402 0.5515 0.7282
2.250 0.4362 0.01207 0.00466 -0.0387 0.5204 0.7353
2.500 0.4567 0.01231 0.00474 -0.0372 0.4886 0.7435
2.750 0.4767 0.01255 0.00487 -0.0355 0.4575 0.7503
3.000 0.4971 0.01280 0.00502 -0.0340 0.4293 0.7579
3.250 0.5176 0.01307 0.00515 -0.0326 0.4021 0.7660
3.500 0.5373 0.01333 0.00535 -0.0309 0.3772 0.7729
3.750 0.5579 0.01360 0.00552 -0.0296 0.3532 0.7811
4.000 0.5779 0.01387 0.00572 -0.0281 0.3308 0.7885
4.250 0.5975 0.01415 0.00593 -0.0265 0.3101 0.7964
4.500 0.6178 0.01444 0.00615 -0.0252 0.2909 0.8048
4.750 0.6367 0.01473 0.00639 -0.0235 0.2725 0.8124
5.000 0.6564 0.01503 0.00662 -0.0220 0.2552 0.8216
5.250 0.6742 0.01531 0.00688 -0.0201 0.2387 0.8295
5.500 0.6928 0.01559 0.00713 -0.0185 0.2239 0.8390
5.750 0.7103 0.01587 0.00740 -0.0165 0.2103 0.8478
6.000 0.7281 0.01619 0.00768 -0.0148 0.1972 0.8580
6.250 0.7445 0.01653 0.00800 -0.0127 0.1850 0.8681
6.500 0.7615 0.01688 0.00833 -0.0108 0.1733 0.8796
6.750 0.7784 0.01721 0.00866 -0.0089 0.1629 0.8918
7.000 0.7948 0.01758 0.00903 -0.0069 0.1543 0.9057
7.250 0.8127 0.01795 0.00940 -0.0053 0.1462 0.9214
7.500 0.8334 0.01836 0.00983 -0.0044 0.1392 0.9402
7.750 0.8606 0.01885 0.01032 -0.0049 0.1320 0.9624
8.000 0.8872 0.01934 0.01080 -0.0055 0.1264 1.0000
8.250 0.9062 0.01983 0.01128 -0.0045 0.1219 1.0000
8.500 0.9236 0.02039 0.01181 -0.0033 0.1181 1.0000
8.750 0.9408 0.02097 0.01238 -0.0021 0.1150 1.0000
9.000 0.9592 0.02150 0.01295 -0.0011 0.1119 1.0000
9.250 0.9764 0.02209 0.01355 0.0001 0.1089 1.0000
9.500 0.9921 0.02276 0.01420 0.0014 0.1064 1.0000
9.750 1.0067 0.02352 0.01493 0.0028 0.1042 1.0000
10.000 1.0239 0.02414 0.01562 0.0039 0.1022 1.0000
10.250 1.0401 0.02483 0.01636 0.0051 0.1002 1.0000
10.500 1.0556 0.02556 0.01713 0.0063 0.0984 1.0000
10.750 1.0704 0.02634 0.01793 0.0075 0.0967 1.0000
11.000 1.0839 0.02721 0.01881 0.0087 0.0952 1.0000
11.250 1.0965 0.02821 0.01977 0.0100 0.0936 1.0000
11.500 1.1117 0.02902 0.02068 0.0111 0.0922 1.0000
11.750 1.1261 0.02990 0.02165 0.0121 0.0908 1.0000
12.000 1.1398 0.03084 0.02266 0.0131 0.0894 1.0000
12.250 1.1530 0.03184 0.02372 0.0142 0.0882 1.0000
12.500 1.1656 0.03289 0.02481 0.0152 0.0871 1.0000
12.750 1.1776 0.03399 0.02596 0.0161 0.0860 1.0000
13.000 1.1890 0.03517 0.02717 0.0170 0.0849 1.0000
13.250 1.2006 0.03644 0.02842 0.0179 0.0838 1.0000
13.500 1.2117 0.03769 0.02979 0.0187 0.0828 1.0000
13.750 1.2222 0.03900 0.03123 0.0195 0.0819 1.0000
14.000 1.2319 0.04041 0.03275 0.0202 0.0808 1.0000
14.250 1.2411 0.04189 0.03433 0.0208 0.0799 1.0000
14.500 1.2498 0.04343 0.03597 0.0214 0.0790 1.0000
14.750 1.2578 0.04506 0.03768 0.0219 0.0782 1.0000
15.000 1.2651 0.04675 0.03945 0.0223 0.0773 1.0000
15.250 1.2724 0.04850 0.04126 0.0226 0.0765 1.0000
15.500 1.2793 0.05031 0.04313 0.0228 0.0757 1.0000
15.750 1.2879 0.05208 0.04491 0.0230 0.0749 1.0000
16.000 1.2913 0.05436 0.04733 0.0231 0.0743 1.0000
16.250 1.2919 0.05697 0.05013 0.0229 0.0736 1.0000
16.500 1.2917 0.05977 0.05310 0.0225 0.0730 1.0000
16.750 1.2898 0.06282 0.05632 0.0220 0.0722 1.0000
17.000 1.2877 0.06602 0.05968 0.0212 0.0715 1.0000
17.250 1.2842 0.06947 0.06327 0.0201 0.0708 1.0000
17.500 1.2804 0.07307 0.06701 0.0189 0.0701 1.0000
17.750 1.2765 0.07680 0.07087 0.0174 0.0694 1.0000
18.000 1.2728 0.08059 0.07477 0.0158 0.0688 1.0000
18.250 1.2694 0.08442 0.07871 0.0141 0.0682 1.0000
18.500 1.2668 0.08821 0.08258 0.0124 0.0677 1.0000
18.750 1.2675 0.09152 0.08595 0.0109 0.0671 1.0000
19.000 1.2604 0.09616 0.09070 0.0086 0.0665 1.0000
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