XFOIL Version 6.96 Calculated polar for: MH 113 14.62% 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 ------ -------- --------- --------- -------- -------- -------- -10.750 0.0516 0.10641 0.10238 -0.1147 0.9275 0.0333 -10.500 0.0571 0.10227 0.09822 -0.1204 0.9215 0.0357 -10.250 0.0695 0.09778 0.09371 -0.1260 0.9173 0.0358 -9.750 0.0978 0.08828 0.08415 -0.1320 0.9070 0.0270 -9.250 0.1203 0.07850 0.07428 -0.1403 0.8951 0.0229 -9.000 0.1336 0.07597 0.07173 -0.1423 0.8875 0.0227 -8.750 0.1474 0.07246 0.06817 -0.1458 0.8814 0.0224 -8.500 0.1498 0.06920 0.06491 -0.1472 0.8720 0.0223 -8.250 0.1557 0.06532 0.06098 -0.1501 0.8649 0.0221 -8.000 0.1510 0.06166 0.05735 -0.1511 0.8552 0.0219 -7.750 0.1448 0.05676 0.05240 -0.1538 0.8472 0.0217 -7.500 0.0387 0.03065 0.02530 -0.1772 0.8268 0.0202 -7.250 0.0534 0.02811 0.02241 -0.1785 0.8201 0.0204 -7.000 0.0766 0.02616 0.02013 -0.1800 0.8153 0.0209 -6.750 0.1005 0.02453 0.01818 -0.1811 0.8106 0.0216 -6.500 0.1225 0.02296 0.01625 -0.1813 0.8046 0.0224 -6.250 0.1490 0.02153 0.01442 -0.1820 0.7998 0.0229 -6.000 0.1781 0.02045 0.01320 -0.1829 0.7961 0.0234 -5.750 0.2016 0.01971 0.01237 -0.1826 0.7903 0.0238 -5.500 0.2279 0.01897 0.01152 -0.1826 0.7850 0.0244 -5.250 0.2569 0.01823 0.01064 -0.1831 0.7808 0.0252 -5.000 0.2845 0.01760 0.00988 -0.1833 0.7760 0.0260 -4.750 0.3103 0.01706 0.00924 -0.1831 0.7704 0.0269 -4.500 0.3386 0.01657 0.00871 -0.1834 0.7655 0.0280 -4.000 0.3945 0.01581 0.00784 -0.1838 0.7555 0.0324 -3.750 0.4224 0.01546 0.00742 -0.1839 0.7501 0.0349 -3.500 0.4529 0.01508 0.00696 -0.1845 0.7457 0.0385 -3.250 0.4801 0.01478 0.00665 -0.1845 0.7400 0.0441 -3.000 0.5076 0.01450 0.00638 -0.1845 0.7343 0.0554 -2.750 0.5375 0.01421 0.00610 -0.1850 0.7294 0.0738 -2.500 0.5653 0.01401 0.00594 -0.1851 0.7239 0.0961 -2.250 0.5922 0.01381 0.00585 -0.1851 0.7177 0.1283 -2.000 0.6216 0.01360 0.00571 -0.1855 0.7125 0.1701 -1.750 0.6493 0.01347 0.00565 -0.1856 0.7068 0.2075 -1.500 0.6761 0.01336 0.00562 -0.1855 0.7004 0.2444 -1.250 0.7053 0.01324 0.00554 -0.1858 0.6950 0.2843 -1.000 0.7319 0.01317 0.00556 -0.1856 0.6886 0.3255 -0.750 0.7590 0.01311 0.00557 -0.1855 0.6820 0.3689 -0.250 0.8129 0.01305 0.00563 -0.1851 0.6693 0.4543 0.000 0.8401 0.01303 0.00566 -0.1849 0.6628 0.4954 0.250 0.8665 0.01303 0.00572 -0.1846 0.6563 0.5353 0.500 0.8917 0.01305 0.00580 -0.1840 0.6491 0.5738 0.750 0.9185 0.01306 0.00582 -0.1837 0.6428 0.6125 1.000 0.9420 0.01311 0.00596 -0.1827 0.6350 0.6497 1.250 0.9671 0.01314 0.00601 -0.1821 0.6280 0.6885 1.500 0.9898 0.01318 0.00612 -0.1809 0.6206 0.7286 1.750 1.0118 0.01320 0.00620 -0.1796 0.6131 0.7736 2.000 1.0312 0.01320 0.00626 -0.1776 0.6058 0.8295 2.250 1.0481 0.01305 0.00622 -0.1750 0.5980 1.0000 2.500 1.0743 0.01324 0.00629 -0.1748 0.5905 1.0000 2.750 1.0987 0.01343 0.00643 -0.1742 0.5819 1.0000 3.000 1.1240 0.01363 0.00653 -0.1738 0.5743 1.0000 3.250 1.1474 0.01385 0.00670 -0.1731 0.5655 1.0000 3.500 1.1717 0.01407 0.00683 -0.1725 0.5577 1.0000 3.750 1.1941 0.01431 0.00703 -0.1716 0.5488 1.0000 4.000 1.2171 0.01456 0.00720 -0.1708 0.5406 1.0000 4.250 1.2385 0.01481 0.00743 -0.1697 0.5317 1.0000 4.500 1.2597 0.01508 0.00763 -0.1685 0.5235 1.0000 4.750 1.2792 0.01536 0.00789 -0.1671 0.5144 1.0000 5.000 1.2991 0.01567 0.00814 -0.1658 0.5062 1.0000 5.250 1.3180 0.01599 0.00843 -0.1643 0.4972 1.0000 5.500 1.3370 0.01634 0.00873 -0.1628 0.4888 1.0000 5.750 1.3552 0.01670 0.00908 -0.1612 0.4799 1.0000 6.000 1.3734 0.01708 0.00942 -0.1597 0.4715 1.0000 6.250 1.3905 0.01749 0.00981 -0.1580 0.4625 1.0000 6.500 1.4079 0.01792 0.01022 -0.1564 0.4542 1.0000 6.750 1.4241 0.01838 0.01067 -0.1547 0.4453 1.0000 7.000 1.4405 0.01887 0.01114 -0.1530 0.4369 1.0000 7.250 1.4559 0.01939 0.01164 -0.1512 0.4282 1.0000 7.500 1.4714 0.01993 0.01218 -0.1495 0.4199 1.0000 7.750 1.4860 0.02053 0.01277 -0.1476 0.4114 1.0000 8.000 1.5007 0.02113 0.01338 -0.1459 0.4032 1.0000 8.250 1.5143 0.02180 0.01404 -0.1441 0.3948 1.0000 8.500 1.5283 0.02249 0.01475 -0.1423 0.3869 1.0000 8.750 1.5410 0.02324 0.01550 -0.1404 0.3784 1.0000 9.000 1.5540 0.02401 0.01628 -0.1387 0.3706 1.0000 9.250 1.5660 0.02485 0.01713 -0.1369 0.3623 1.0000 9.500 1.5782 0.02571 0.01802 -0.1351 0.3547 1.0000 9.750 1.5897 0.02664 0.01897 -0.1334 0.3466 1.0000 10.000 1.6006 0.02762 0.01996 -0.1316 0.3391 1.0000 10.250 1.6116 0.02863 0.02101 -0.1299 0.3311 1.0000 10.500 1.6214 0.02974 0.02214 -0.1282 0.3238 1.0000 10.750 1.6315 0.03087 0.02332 -0.1266 0.3157 1.0000 11.000 1.6401 0.03212 0.02456 -0.1248 0.3087 1.0000 11.250 1.6497 0.03334 0.02586 -0.1233 0.3007 1.0000 11.500 1.6568 0.03477 0.02729 -0.1216 0.2936 1.0000 11.750 1.6661 0.03609 0.02869 -0.1202 0.2858 1.0000 12.000 1.6718 0.03771 0.03031 -0.1186 0.2785 1.0000 12.250 1.6805 0.03917 0.03185 -0.1173 0.2710 1.0000 12.500 1.6856 0.04094 0.03364 -0.1158 0.2637 1.0000 12.750 1.6927 0.04260 0.03538 -0.1146 0.2563 1.0000 13.000 1.6973 0.04452 0.03733 -0.1132 0.2490 1.0000 13.250 1.7029 0.04641 0.03928 -0.1121 0.2419 1.0000 13.500 1.7067 0.04852 0.04143 -0.1109 0.2344 1.0000 13.750 1.7111 0.05063 0.04361 -0.1099 0.2275 1.0000 14.000 1.7140 0.05294 0.04597 -0.1089 0.2201 1.0000 14.250 1.7169 0.05531 0.04839 -0.1080 0.2135 1.0000 14.500 1.7196 0.05777 0.05092 -0.1072 0.2063 1.0000 14.750 1.7203 0.06050 0.05369 -0.1064 0.1999 1.0000 15.000 1.7229 0.06308 0.05636 -0.1058 0.1929 1.0000 15.250 1.7214 0.06618 0.05948 -0.1052 0.1867 1.0000 15.500 1.7237 0.06893 0.06234 -0.1049 0.1800 1.0000 15.750 1.7215 0.07225 0.06570 -0.1045 0.1739 1.0000 16.000 1.7225 0.07526 0.06880 -0.1043 0.1678 1.0000 16.250 1.7204 0.07871 0.07231 -0.1042 0.1617 1.0000 16.500 1.7187 0.08216 0.07583 -0.1042 0.1563 1.0000 16.750 1.7175 0.08561 0.07937 -0.1044 0.1505 1.0000 17.250 1.7126 0.09298 0.08690 -0.1050 0.1401 1.0000 17.500 1.7086 0.09695 0.09094 -0.1055 0.1350 1.0000 17.750 1.7052 0.10086 0.09492 -0.1061 0.1304 1.0000 18.000 1.7031 0.10464 0.09880 -0.1068 0.1254 1.0000 18.250 1.6977 0.10894 0.10316 -0.1078 0.1210 1.0000 18.500 1.6954 0.11278 0.10711 -0.1087 0.1167 1.0000 18.750 1.6924 0.11677 0.11118 -0.1098 0.1122 1.0000