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 = 1.000 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.250 -0.7255 0.11528 0.11142 -0.0537 0.8684 0.0136 -19.000 -0.7304 0.11092 0.10696 -0.0560 0.8589 0.0138 -18.750 -0.7343 0.10670 0.10266 -0.0584 0.8491 0.0140 -18.500 -0.7389 0.10244 0.09829 -0.0607 0.8399 0.0142 -18.250 -0.7412 0.09855 0.09433 -0.0628 0.8318 0.0144 -18.000 -0.7450 0.09445 0.09014 -0.0651 0.8233 0.0146 -17.750 -0.7462 0.09077 0.08637 -0.0671 0.8158 0.0149 -17.500 -0.7490 0.08688 0.08240 -0.0693 0.8082 0.0151 -17.250 -0.7496 0.08335 0.07878 -0.0712 0.7999 0.0154 -17.000 -0.7509 0.07972 0.07507 -0.0733 0.7931 0.0156 -16.750 -0.7512 0.07628 0.07156 -0.0752 0.7863 0.0159 -16.500 -0.7509 0.07293 0.06812 -0.0771 0.7787 0.0161 -16.250 -0.7520 0.06944 0.06455 -0.0791 0.7720 0.0165 -16.000 -0.7538 0.06589 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0.4487 0.3175 -1.250 0.6567 0.00978 0.00341 -0.1721 0.4445 0.3224 -1.000 0.6881 0.00981 0.00344 -0.1729 0.4414 0.3273 -0.750 0.7195 0.00985 0.00348 -0.1736 0.4381 0.3323 -0.500 0.7503 0.00992 0.00353 -0.1742 0.4341 0.3360 -0.250 0.7812 0.00999 0.00358 -0.1749 0.4299 0.3412 0.000 0.8118 0.01007 0.00366 -0.1756 0.4257 0.3466 0.250 0.8426 0.01014 0.00372 -0.1763 0.4228 0.3518 0.500 0.8733 0.01020 0.00379 -0.1769 0.4201 0.3565 0.750 0.9043 0.01026 0.00386 -0.1777 0.4170 0.3636 1.000 0.9348 0.01034 0.00394 -0.1783 0.4135 0.3702 1.250 0.9646 0.01046 0.00404 -0.1788 0.4096 0.3756 1.500 0.9942 0.01059 0.00416 -0.1793 0.4054 0.3813 1.750 1.0248 0.01065 0.00425 -0.1800 0.4030 0.3884 2.000 1.0548 0.01074 0.00434 -0.1805 0.4001 0.3953 2.250 1.0846 0.01084 0.00445 -0.1811 0.3971 0.4022 2.500 1.1143 0.01095 0.00458 -0.1816 0.3939 0.4106 2.750 1.1431 0.01110 0.00472 -0.1820 0.3906 0.4176 3.000 1.1717 0.01126 0.00487 -0.1823 0.3871 0.4239 3.250 1.2014 0.01135 0.00500 -0.1828 0.3849 0.4319 3.500 1.2303 0.01147 0.00514 -0.1832 0.3820 0.4391 3.750 1.2588 0.01161 0.00529 -0.1836 0.3788 0.4461 4.000 1.2871 0.01176 0.00546 -0.1839 0.3757 0.4554 4.250 1.3143 0.01196 0.00565 -0.1841 0.3725 0.4632 4.500 1.3413 0.01216 0.00586 -0.1842 0.3693 0.4707 4.750 1.3694 0.01229 0.00603 -0.1845 0.3673 0.4787 5.000 1.3967 0.01245 0.00621 -0.1846 0.3648 0.4856 5.250 1.4235 0.01263 0.00641 -0.1847 0.3618 0.4928 5.500 1.4495 0.01284 0.00664 -0.1847 0.3588 0.5018 5.750 1.4742 0.01308 0.00689 -0.1844 0.3560 0.5094 6.000 1.4964 0.01335 0.00717 -0.1837 0.3528 0.5172 6.250 1.5192 0.01359 0.00744 -0.1832 0.3505 0.5248 6.500 1.5434 0.01382 0.00771 -0.1829 0.3483 0.5318 6.750 1.5673 0.01409 0.00801 -0.1826 0.3458 0.5399 7.000 1.5902 0.01439 0.00835 -0.1822 0.3433 0.5483 7.250 1.6116 0.01477 0.00874 -0.1816 0.3404 0.5553 7.500 1.6320 0.01520 0.00919 -0.1808 0.3372 0.5632 7.750 1.6516 0.01569 0.00970 -0.1801 0.3342 0.5711 8.000 1.6738 0.01604 0.01009 -0.1796 0.3326 0.5782 8.250 1.6955 0.01644 0.01054 -0.1792 0.3305 0.5857 8.500 1.7160 0.01690 0.01105 -0.1786 0.3279 0.5936 8.750 1.7353 0.01744 0.01161 -0.1779 0.3253 0.6008 9.000 1.7533 0.01807 0.01226 -0.1771 0.3225 0.6074 9.250 1.7701 0.01879 0.01302 -0.1762 0.3195 0.6147 9.500 1.7870 0.01951 0.01377 -0.1754 0.3167 0.6218 9.750 1.8065 0.02009 0.01439 -0.1748 0.3148 0.6279 10.000 1.8246 0.02078 0.01514 -0.1742 0.3122 0.6347 10.250 1.8414 0.02155 0.01595 -0.1734 0.3092 0.6417 10.500 1.8554 0.02252 0.01694 -0.1724 0.3060 0.6480 10.750 1.8681 0.02360 0.01804 -0.1714 0.3027 0.6537 11.000 1.8816 0.02466 0.01915 -0.1704 0.3001 0.6601 11.250 1.8982 0.02548 0.02003 -0.1698 0.2980 0.6668 11.500 1.9121 0.02651 0.02110 -0.1689 0.2954 0.6726 11.750 1.9252 0.02761 0.02225 -0.1680 0.2926 0.6784 12.000 1.9352 0.02897 0.02365 -0.1670 0.2895 0.6846 12.250 1.9435 0.03046 0.02517 -0.1658 0.2863 0.6906 12.750 1.9651 0.03314 0.02795 -0.1639 0.2812 0.7014 13.000 1.9751 0.03458 0.02946 -0.1630 0.2784 0.7074 13.250 1.9834 0.03618 0.03110 -0.1620 0.2753 0.7132 13.750 1.9909 0.04025 0.03524 -0.1597 0.2682 0.7229 14.000 1.9994 0.04192 0.03698 -0.1589 0.2657 0.7284 14.250 2.0070 0.04368 0.03879 -0.1581 0.2626 0.7339 14.500 2.0098 0.04590 0.04105 -0.1570 0.2590 0.7385 14.750 2.0091 0.04847 0.04366 -0.1559 0.2550 0.7430 15.000 2.0097 0.05098 0.04623 -0.1549 0.2516 0.7476 15.250 2.0153 0.05298 0.04829 -0.1541 0.2483 0.7529 15.500 2.0147 0.05566 0.05102 -0.1532 0.2445 0.7575 15.750 2.0099 0.05874 0.05412 -0.1521 0.2400 0.7614 16.000 2.0062 0.06179 0.05724 -0.1512 0.2363 0.7656 16.250 2.0079 0.06428 0.05978 -0.1505 0.2324 0.7701 16.500 2.0009 0.06774 0.06329 -0.1496 0.2279 0.7743 16.750 1.9875 0.07190 0.06748 -0.1486 0.2230 0.7780 17.000 1.9871 0.07468 0.07031 -0.1481 0.2189 0.7819 17.250 1.9766 0.07863 0.07431 -0.1473 0.2136 0.7857 17.500 1.9623 0.08302 0.07873 -0.1466 0.2079 0.7891 17.750 1.9537 0.08681 0.08257 -0.1461 0.2026 0.7928 18.000 1.9348 0.09187 0.08766 -0.1456 0.1964 0.7959 18.250 1.9270 0.09565 0.09147 -0.1454 0.1911 0.7993 18.500 1.9113 0.10042 0.09628 -0.1452 0.1852 0.8024 18.750 1.8983 0.10487 0.10076 -0.1451 0.1798 0.8058 19.000 1.8866 0.10926 0.10519 -0.1452 0.1740 0.8092