MH 150 23.89% (mh150-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: MH 150 23.89% (mh150-il) Reynolds number: 200,000 Max Cl/Cd: 56.27 at α=7° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-mh150-il-200000.txt Download as CSV file: xf-mh150-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: MH 150 23.89%
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -0.6070 0.12383 0.11922 -0.0636 1.0001 0.0408
-19.000 -0.6447 0.11323 0.10832 -0.0702 1.0001 0.0410
-18.750 -0.6686 0.10533 0.10017 -0.0753 1.0001 0.0413
-18.500 -0.6466 0.10535 0.10034 -0.0750 1.0001 0.0424
-18.250 -0.6413 0.10247 0.09747 -0.0768 1.0001 0.0432
-18.000 -0.6433 0.09840 0.09332 -0.0793 1.0001 0.0441
-17.750 -0.6490 0.09376 0.08855 -0.0823 1.0001 0.0450
-17.500 -0.6558 0.08900 0.08362 -0.0853 1.0001 0.0459
-17.250 -0.6393 0.08812 0.08286 -0.0856 1.0001 0.0472
-17.000 -0.6295 0.08609 0.08088 -0.0869 1.0001 0.0486
-16.750 -0.6281 0.08280 0.07752 -0.0891 1.0001 0.0500
-16.500 -0.6271 0.07968 0.07434 -0.0910 1.0001 0.0515
-16.250 -0.6170 0.07866 0.07346 -0.0913 1.0001 0.0533
-16.000 -0.6218 0.07684 0.07165 -0.0916 0.9982 0.0549
-15.750 -0.6071 0.07336 0.06812 -0.0961 0.9925 0.0577
-15.500 -0.5924 0.07007 0.06483 -0.1004 0.9852 0.0610
-15.250 -0.5778 0.06678 0.06156 -0.1048 0.9784 0.0647
-15.000 -0.5722 0.06296 0.05762 -0.1087 0.9669 0.0688
-14.750 -0.5640 0.06048 0.05523 -0.1107 0.9541 0.0728
-14.500 -0.5642 0.05766 0.05238 -0.1119 0.9406 0.0770
-14.250 -0.5676 0.05491 0.04959 -0.1124 0.9271 0.0813
-14.000 -0.5695 0.05234 0.04702 -0.1130 0.9143 0.0858
-13.750 -0.5750 0.04940 0.04396 -0.1136 0.9036 0.0910
-13.500 -0.5758 0.04690 0.04151 -0.1145 0.8920 0.0960
-13.250 -0.5785 0.04432 0.03886 -0.1152 0.8825 0.1016
-13.000 -0.5791 0.04159 0.03605 -0.1168 0.8718 0.1079
-12.750 -0.5801 0.03932 0.03377 -0.1173 0.8634 0.1137
-12.500 -0.5774 0.03695 0.03136 -0.1189 0.8532 0.1205
-12.250 -0.5755 0.03476 0.02909 -0.1200 0.8446 0.1273
-12.000 -0.5705 0.03282 0.02715 -0.1212 0.8362 0.1341
-11.750 -0.5641 0.03087 0.02510 -0.1226 0.8271 0.1419
-11.500 -0.5566 0.02920 0.02339 -0.1235 0.8199 0.1495
-11.250 -0.5464 0.02770 0.02190 -0.1248 0.8111 0.1575
-11.000 -0.5390 0.02636 0.02043 -0.1255 0.8029 0.1659
-10.750 -0.5245 0.02524 0.01932 -0.1266 0.7967 0.1745
-10.500 -0.5063 0.02420 0.01827 -0.1286 0.7883 0.1841
-10.250 -0.4835 0.02316 0.01709 -0.1313 0.7809 0.1949
-10.000 -0.4572 0.02248 0.01640 -0.1333 0.7752 0.2052
-9.750 -0.4296 0.02194 0.01586 -0.1355 0.7678 0.2154
-9.500 -0.3999 0.02143 0.01519 -0.1379 0.7606 0.2267
-9.250 -0.3702 0.02122 0.01498 -0.1389 0.7549 0.2364
-9.000 -0.3403 0.02097 0.01465 -0.1404 0.7486 0.2463
-8.750 -0.3102 0.02087 0.01451 -0.1416 0.7413 0.2556
-8.500 -0.2798 0.02062 0.01419 -0.1426 0.7354 0.2642
-8.250 -0.2485 0.02059 0.01405 -0.1435 0.7302 0.2727
-8.000 -0.2187 0.02036 0.01377 -0.1446 0.7229 0.2809
-7.750 -0.1893 0.02036 0.01378 -0.1449 0.7164 0.2879
-7.500 -0.1552 0.02017 0.01331 -0.1468 0.7110 0.2968
-7.250 -0.1275 0.02010 0.01334 -0.1466 0.7054 0.3029
-7.000 -0.0979 0.02009 0.01332 -0.1472 0.6984 0.3100
-6.750 -0.0648 0.01983 0.01285 -0.1487 0.6924 0.3177
-6.500 -0.0357 0.01978 0.01280 -0.1486 0.6874 0.3233
-6.250 -0.0063 0.01978 0.01280 -0.1491 0.6809 0.3297
-6.000 0.0272 0.01960 0.01242 -0.1508 0.6746 0.3368
-5.750 0.0555 0.01942 0.01228 -0.1507 0.6693 0.3420
-5.500 0.0859 0.01944 0.01224 -0.1511 0.6641 0.3477
-5.250 0.1172 0.01934 0.01205 -0.1522 0.6573 0.3543
-5.000 0.1481 0.01910 0.01174 -0.1530 0.6515 0.3598
-4.750 0.1778 0.01905 0.01167 -0.1532 0.6466 0.3648
-4.500 0.2082 0.01906 0.01163 -0.1538 0.6411 0.3706
-4.250 0.2408 0.01897 0.01141 -0.1552 0.6346 0.3768
-4.000 0.2705 0.01876 0.01118 -0.1556 0.6291 0.3818
-3.750 0.3009 0.01875 0.01112 -0.1559 0.6245 0.3869
-3.500 0.3310 0.01878 0.01113 -0.1566 0.6189 0.3927
-3.250 0.3640 0.01873 0.01094 -0.1580 0.6128 0.3989
-3.000 0.3931 0.01855 0.01079 -0.1582 0.6076 0.4039
-2.750 0.4240 0.01858 0.01074 -0.1587 0.6031 0.4092
-2.500 0.4539 0.01862 0.01078 -0.1594 0.5976 0.4153
-2.250 0.4863 0.01858 0.01065 -0.1606 0.5920 0.4214
-2.000 0.5155 0.01848 0.01057 -0.1609 0.5872 0.4263
-1.750 0.5466 0.01854 0.01055 -0.1614 0.5828 0.4322
-1.500 0.5768 0.01862 0.01062 -0.1622 0.5774 0.4390
-1.250 0.6074 0.01859 0.01057 -0.1630 0.5719 0.4451
-1.000 0.6367 0.01860 0.01060 -0.1633 0.5673 0.4506
-0.750 0.6682 0.01868 0.01059 -0.1640 0.5633 0.4576
-0.500 0.7003 0.01883 0.01066 -0.1652 0.5587 0.4655
-0.250 0.7269 0.01890 0.01086 -0.1651 0.5535 0.4715
0.000 0.7564 0.01897 0.01093 -0.1655 0.5486 0.4786
0.250 0.7898 0.01903 0.01085 -0.1667 0.5444 0.4871
0.500 0.8193 0.01920 0.01101 -0.1671 0.5404 0.4939
0.750 0.8456 0.01941 0.01133 -0.1671 0.5357 0.5018
1.000 0.8763 0.01956 0.01145 -0.1679 0.5310 0.5111
1.250 0.9041 0.01966 0.01161 -0.1679 0.5270 0.5181
1.500 0.9351 0.01982 0.01169 -0.1686 0.5232 0.5268
1.750 0.9652 0.02007 0.01191 -0.1693 0.5190 0.5357
2.000 0.9895 0.02031 0.01229 -0.1688 0.5144 0.5431
2.250 1.0182 0.02052 0.01251 -0.1692 0.5100 0.5530
2.500 1.0473 0.02068 0.01265 -0.1696 0.5063 0.5613
2.750 1.0765 0.02091 0.01286 -0.1698 0.5030 0.5696
3.000 1.1068 0.02129 0.01319 -0.1707 0.4993 0.5798
3.250 1.1286 0.02158 0.01365 -0.1698 0.4950 0.5865
3.500 1.1541 0.02185 0.01397 -0.1696 0.4908 0.5952
3.750 1.1842 0.02204 0.01411 -0.1703 0.4871 0.6052
4.000 1.2114 0.02228 0.01435 -0.1701 0.4839 0.6123
4.250 1.2401 0.02272 0.01476 -0.1705 0.4806 0.6216
4.500 1.2622 0.02313 0.01530 -0.1700 0.4768 0.6299
4.750 1.2834 0.02352 0.01579 -0.1690 0.4730 0.6369
5.000 1.3103 0.02381 0.01609 -0.1692 0.4694 0.6467
5.250 1.3382 0.02402 0.01628 -0.1693 0.4662 0.6543
5.500 1.3664 0.02435 0.01656 -0.1693 0.4631 0.6618
5.750 1.3900 0.02492 0.01719 -0.1693 0.4597 0.6718
6.000 1.4065 0.02543 0.01786 -0.1677 0.4562 0.6780
6.250 1.4261 0.02589 0.01840 -0.1666 0.4528 0.6852
6.500 1.4545 0.02623 0.01871 -0.1673 0.4494 0.6957
6.750 1.4786 0.02645 0.01895 -0.1665 0.4466 0.7013
7.000 1.5085 0.02681 0.01924 -0.1669 0.4437 0.7092
7.250 1.5267 0.02753 0.02007 -0.1662 0.4405 0.7185
7.500 1.5359 0.02822 0.02094 -0.1636 0.4372 0.7238
7.750 1.5514 0.02879 0.02160 -0.1621 0.4339 0.7313
8.000 1.5756 0.02918 0.02199 -0.1621 0.4307 0.7403
8.250 1.5990 0.02941 0.02223 -0.1613 0.4279 0.7463
8.500 1.6319 0.02970 0.02245 -0.1623 0.4254 0.7548
8.750 1.6476 0.03053 0.02337 -0.1611 0.4225 0.7622
9.000 1.6401 0.03157 0.02462 -0.1565 0.4192 0.7681
9.250 1.6461 0.03256 0.02573 -0.1543 0.4157 0.7765
9.500 1.6606 0.03318 0.02640 -0.1529 0.4126 0.7833
9.750 1.6830 0.03349 0.02673 -0.1523 0.4101 0.7906
10.000 1.7198 0.03356 0.02672 -0.1538 0.4076 0.7996
10.250 1.7442 0.03408 0.02724 -0.1535 0.4048 0.8060
10.500 1.7174 0.03639 0.02983 -0.1480 0.4013 0.8133
10.750 1.7043 0.03851 0.03214 -0.1445 0.3975 0.8199
11.000 1.7094 0.03970 0.03342 -0.1426 0.3944 0.8270
11.250 1.7367 0.03987 0.03357 -0.1429 0.3917 0.8356
11.500 1.7730 0.03939 0.03303 -0.1435 0.3894 0.8435
11.750 1.8092 0.03950 0.03308 -0.1447 0.3868 0.8524
12.000 1.7278 0.04585 0.03989 -0.1367 0.3817 0.8563
12.250 1.6936 0.05037 0.04461 -0.1334 0.3768 0.8622
12.500 1.7193 0.05034 0.04458 -0.1334 0.3742 0.8705
12.750 1.7632 0.04900 0.04316 -0.1342 0.3722 0.8808
13.000 1.8153 0.04714 0.04121 -0.1355 0.3703 0.8912
13.250 1.5592 0.07354 0.06837 -0.1265 0.3547 0.8815
13.500 1.6148 0.06971 0.06450 -0.1264 0.3545 0.8934
13.750 1.6742 0.06577 0.06049 -0.1267 0.3541 0.9060
14.000 1.7340 0.06207 0.05670 -0.1273 0.3534 0.9198
14.250 1.7939 0.05867 0.05322 -0.1280 0.3522 0.9358
14.500 1.5557 0.08766 0.08276 -0.1243 0.3345 0.9199
14.750 1.6076 0.08364 0.07873 -0.1238 0.3345 0.9371
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