XFOIL Version 6.96 Calculated polar for: MH 104 15.28% 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.100 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -11.750 -0.6041 0.08759 0.08291 -0.0276 1.0000 0.0518 -11.500 -0.6220 0.08018 0.07548 -0.0322 1.0000 0.0507 -11.250 -0.6469 0.07276 0.06799 -0.0373 1.0000 0.0493 -11.000 -0.6787 0.06601 0.06108 -0.0416 1.0000 0.0479 -10.750 -0.7091 0.06094 0.05580 -0.0432 1.0000 0.0472 -10.500 -0.7776 0.05682 0.05097 -0.0388 1.0000 0.0438 -10.250 -0.7863 0.05448 0.04832 -0.0362 1.0000 0.0434 -10.000 -0.7886 0.05150 0.04506 -0.0342 1.0000 0.0433 -9.750 -0.7885 0.04728 0.04061 -0.0326 1.0000 0.0439 -9.500 -0.7831 0.04432 0.03735 -0.0308 1.0000 0.0440 -9.250 -0.7727 0.04140 0.03428 -0.0294 1.0000 0.0449 -9.000 -0.7591 0.03897 0.03171 -0.0281 1.0000 0.0459 -8.750 -0.7450 0.03651 0.02901 -0.0266 1.0000 0.0466 -8.500 -0.7284 0.03419 0.02648 -0.0252 1.0000 0.0474 -8.250 -0.7099 0.03212 0.02425 -0.0239 1.0000 0.0486 -8.000 -0.6920 0.03032 0.02231 -0.0224 1.0000 0.0504 -7.750 -0.6835 0.02932 0.02114 -0.0196 1.0000 0.0524 -7.500 -0.6899 0.02829 0.02022 -0.0152 0.9995 0.0541 -7.250 -0.6387 0.02617 0.01809 -0.0202 0.9839 0.0630 -7.000 -0.5939 0.02369 0.01580 -0.0243 0.9680 0.0770 -6.750 -0.5593 0.02138 0.01377 -0.0267 0.9471 0.1112 -6.500 -0.5376 0.01923 0.01252 -0.0268 0.9254 0.2490 -6.250 -0.5135 0.01925 0.01249 -0.0260 0.9021 0.3018 -6.000 -0.4918 0.01933 0.01245 -0.0244 0.8811 0.3338 -5.750 -0.4721 0.01941 0.01244 -0.0223 0.8620 0.3607 -5.500 -0.4534 0.01950 0.01239 -0.0201 0.8428 0.3869 -5.250 -0.4329 0.01950 0.01239 -0.0182 0.8256 0.4102 -5.000 -0.4125 0.01944 0.01218 -0.0163 0.8096 0.4326 -4.750 -0.3900 0.01926 0.01197 -0.0148 0.7947 0.4518 -4.500 -0.3671 0.01906 0.01170 -0.0134 0.7806 0.4706 -4.250 -0.3440 0.01884 0.01141 -0.0120 0.7676 0.4897 -4.000 -0.3207 0.01864 0.01111 -0.0108 0.7547 0.5100 -3.750 -0.2966 0.01843 0.01089 -0.0098 0.7418 0.5303 -3.500 -0.2722 0.01825 0.01070 -0.0088 0.7298 0.5515 -3.250 -0.2486 0.01808 0.01046 -0.0076 0.7192 0.5755 -3.000 -0.2237 0.01790 0.01033 -0.0065 0.7084 0.5990 -2.750 -0.1993 0.01780 0.01024 -0.0056 0.6975 0.6257 -2.500 -0.1749 0.01769 0.01012 -0.0044 0.6890 0.6550 -2.250 -0.1497 0.01761 0.01013 -0.0034 0.6787 0.6852 -2.000 -0.1243 0.01760 0.01016 -0.0024 0.6696 0.7182 -1.750 -0.0970 0.01760 0.01020 -0.0015 0.6613 0.7519 -1.500 -0.0675 0.01777 0.01045 -0.0011 0.6524 0.7862 -1.250 -0.0340 0.01797 0.01059 -0.0011 0.6451 0.8196 -1.000 0.0033 0.01836 0.01097 -0.0021 0.6362 0.8498 -0.750 0.0432 0.01869 0.01116 -0.0034 0.6290 0.8772 -0.500 0.0937 0.01925 0.01166 -0.0071 0.6202 0.8964 -0.250 0.1474 0.01964 0.01187 -0.0113 0.6134 0.9132 0.000 0.2013 0.02010 0.01226 -0.0162 0.6049 0.9297 0.250 0.2544 0.02032 0.01232 -0.0208 0.5980 0.9462 0.500 0.3075 0.02064 0.01260 -0.0261 0.5905 0.9627 0.750 0.3615 0.02072 0.01257 -0.0314 0.5836 0.9788 1.000 0.4175 0.02077 0.01256 -0.0376 0.5766 0.9937 1.250 0.4540 0.02079 0.01257 -0.0404 0.5701 1.0000 1.500 0.4721 0.02084 0.01251 -0.0394 0.5659 1.0000 1.750 0.4901 0.02121 0.01295 -0.0388 0.5597 1.0000 2.000 0.5087 0.02146 0.01317 -0.0379 0.5543 1.0000 2.250 0.5281 0.02161 0.01325 -0.0367 0.5502 1.0000 2.500 0.5458 0.02220 0.01393 -0.0360 0.5439 1.0000 2.750 0.5648 0.02256 0.01428 -0.0350 0.5386 1.0000 3.000 0.5853 0.02275 0.01439 -0.0338 0.5346 1.0000 3.250 0.6021 0.02354 0.01530 -0.0329 0.5282 1.0000 3.500 0.6213 0.02397 0.01574 -0.0318 0.5228 1.0000 3.750 0.6431 0.02414 0.01583 -0.0306 0.5189 1.0000 4.000 0.6580 0.02516 0.01701 -0.0296 0.5120 1.0000 4.250 0.6779 0.02556 0.01741 -0.0284 0.5067 1.0000 4.500 0.7015 0.02565 0.01742 -0.0273 0.5030 1.0000 4.750 0.7129 0.02698 0.01895 -0.0260 0.4950 1.0000 5.000 0.7350 0.02721 0.01916 -0.0249 0.4901 1.0000 5.250 0.7559 0.02764 0.01959 -0.0237 0.4853 1.0000 5.500 0.7679 0.02882 0.02092 -0.0222 0.4774 1.0000 5.750 0.7944 0.02869 0.02074 -0.0213 0.4732 1.0000 6.000 0.8034 0.03016 0.02238 -0.0196 0.4651 1.0000 6.250 0.8266 0.03029 0.02251 -0.0185 0.4596 1.0000 6.500 0.8503 0.03048 0.02270 -0.0175 0.4544 1.0000 6.750 0.8596 0.03176 0.02414 -0.0157 0.4458 1.0000 7.000 0.8932 0.03106 0.02336 -0.0152 0.4416 1.0000 7.250 0.8944 0.03295 0.02548 -0.0129 0.4318 1.0000 7.500 0.9290 0.03215 0.02462 -0.0124 0.4270 1.0000 7.750 0.9315 0.03387 0.02653 -0.0101 0.4176 1.0000 8.000 0.9667 0.03297 0.02559 -0.0097 0.4122 1.0000 8.250 0.9710 0.03446 0.02725 -0.0074 0.4031 1.0000 8.500 1.0071 0.03345 0.02622 -0.0071 0.3971 1.0000 8.750 1.0122 0.03478 0.02771 -0.0048 0.3879 1.0000 9.000 1.0510 0.03355 0.02644 -0.0047 0.3815 1.0000 9.250 1.0552 0.03482 0.02789 -0.0023 0.3720 1.0000 9.500 1.1009 0.03310 0.02607 -0.0027 0.3653 1.0000 9.750 1.1006 0.03451 0.02770 0.0001 0.3550 1.0000 10.000 1.1339 0.03362 0.02679 0.0005 0.3468 1.0000 10.250 1.1535 0.03352 0.02676 0.0020 0.3370 1.0000 10.500 1.1621 0.03414 0.02754 0.0043 0.3270 1.0000 10.750 1.1929 0.03327 0.02664 0.0049 0.3171 1.0000 11.000 1.2161 0.03279 0.02615 0.0062 0.3061 1.0000 11.250 1.2176 0.03362 0.02714 0.0091 0.2952 1.0000 11.500 1.2293 0.03382 0.02738 0.0113 0.2842 1.0000 11.750 1.2444 0.03379 0.02734 0.0131 0.2727 1.0000 12.000 1.2580 0.03385 0.02733 0.0151 0.2607 1.0000 12.250 1.2481 0.03506 0.02864 0.0190 0.2510 1.0000 12.500 1.2442 0.03632 0.02993 0.0216 0.2410 1.0000 12.750 1.2481 0.03730 0.03086 0.0234 0.2299 1.0000 13.000 1.2539 0.03831 0.03176 0.0249 0.2181 1.0000 13.250 1.2385 0.04097 0.03458 0.0264 0.2094 1.0000 13.500 1.2350 0.04303 0.03665 0.0274 0.1994 1.0000 13.750 1.2378 0.04467 0.03820 0.0282 0.1887 1.0000 14.000 1.2263 0.04768 0.04130 0.0285 0.1800 1.0000 14.250 1.2191 0.05054 0.04420 0.0287 0.1712 1.0000 14.500 1.2208 0.05251 0.04608 0.0291 0.1610 1.0000 14.750 1.2048 0.05650 0.05023 0.0285 0.1537 1.0000 15.000 1.2003 0.05938 0.05309 0.0283 0.1451 1.0000 15.250 1.2049 0.06121 0.05474 0.0287 0.1349 1.0000 15.500 1.1825 0.06651 0.06032 0.0271 0.1299 1.0000 15.750 1.1856 0.06865 0.06231 0.0271 0.1207 1.0000 16.000 1.1651 0.07416 0.06805 0.0251 0.1156 1.0000 16.250 1.1683 0.07645 0.07021 0.0250 0.1073 1.0000 16.500 1.1484 0.08230 0.07629 0.0227 0.1029 1.0000 16.750 1.1550 0.08421 0.07804 0.0228 0.0949 1.0000 17.000 1.1330 0.09079 0.08488 0.0200 0.0919 1.0000 17.250 1.1480 0.09145 0.08529 0.0208 0.0836 1.0000 17.500 1.1230 0.09877 0.09292 0.0174 0.0818 1.0000 17.750 1.0988 0.10635 0.10075 0.0138 0.0801 1.0000 18.000 1.0700 0.11509 0.10971 0.0094 0.0790 1.0000 18.250 1.0168 0.12933 0.12421 0.0017 0.0812 1.0000