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 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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