XFOIL Version 6.96 Calculated polar for: NACA 2415 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -13.500 -0.8013 0.06679 0.06013 -0.0667 1.0000 0.0572 -13.250 -0.8380 0.05901 0.05206 -0.0716 1.0000 0.0573 -13.000 -0.8601 0.05413 0.04695 -0.0734 1.0000 0.0576 -12.750 -0.8769 0.05048 0.04308 -0.0734 1.0000 0.0581 -12.500 -0.8908 0.04758 0.03996 -0.0721 1.0000 0.0587 -12.250 -0.9034 0.04524 0.03740 -0.0695 1.0000 0.0593 -12.000 -0.9148 0.04327 0.03522 -0.0658 1.0000 0.0600 -11.750 -0.9209 0.04134 0.03302 -0.0625 1.0000 0.0607 -11.500 -0.9143 0.04002 0.03171 -0.0603 1.0000 0.0614 -11.250 -0.9078 0.03883 0.03050 -0.0579 1.0000 0.0623 -11.000 -0.9017 0.03769 0.02929 -0.0553 1.0000 0.0633 -10.750 -0.8954 0.03653 0.02804 -0.0527 1.0000 0.0646 -10.500 -0.8888 0.03532 0.02668 -0.0501 1.0000 0.0661 -10.250 -0.8813 0.03407 0.02522 -0.0474 1.0000 0.0677 -10.000 -0.8716 0.03297 0.02405 -0.0450 1.0000 0.0691 -9.750 -0.8606 0.03209 0.02318 -0.0428 1.0000 0.0706 -9.500 -0.8493 0.03119 0.02224 -0.0405 1.0000 0.0722 -9.250 -0.8375 0.03028 0.02123 -0.0382 1.0000 0.0742 -9.000 -0.8250 0.02937 0.02015 -0.0360 1.0000 0.0767 -8.750 -0.8123 0.02859 0.01940 -0.0340 1.0000 0.0789 -8.500 -0.7989 0.02790 0.01870 -0.0319 1.0000 0.0815 -8.250 -0.7845 0.02718 0.01788 -0.0300 1.0000 0.0848 -8.000 -0.7699 0.02647 0.01712 -0.0281 1.0000 0.0879 -7.750 -0.7395 0.02574 0.01638 -0.0294 0.9961 0.0927 -7.500 -0.7062 0.02500 0.01556 -0.0311 0.9916 0.0988 -7.250 -0.6737 0.02435 0.01489 -0.0327 0.9862 0.1056 -7.000 -0.6387 0.02371 0.01425 -0.0347 0.9818 0.1135 -6.750 -0.6073 0.02315 0.01362 -0.0358 0.9754 0.1226 -6.500 -0.5724 0.02260 0.01308 -0.0378 0.9703 0.1327 -6.250 -0.5413 0.02207 0.01258 -0.0388 0.9637 0.1432 -6.000 -0.5070 0.02157 0.01210 -0.0405 0.9579 0.1556 -5.750 -0.4734 0.02112 0.01164 -0.0420 0.9520 0.1690 -5.500 -0.4417 0.02069 0.01124 -0.0430 0.9447 0.1833 -5.250 -0.4041 0.02025 0.01084 -0.0452 0.9402 0.2000 -5.000 -0.3759 0.01989 0.01051 -0.0454 0.9314 0.2160 -4.750 -0.3404 0.01948 0.01017 -0.0471 0.9258 0.2349 -4.500 -0.3095 0.01912 0.00986 -0.0477 0.9183 0.2539 -4.250 -0.2780 0.01876 0.00955 -0.0485 0.9106 0.2740 -4.000 -0.2434 0.01838 0.00922 -0.0498 0.9048 0.2961 -3.750 -0.2164 0.01807 0.00897 -0.0495 0.8947 0.3168 -3.500 -0.1812 0.01768 0.00864 -0.0508 0.8890 0.3413 -3.250 -0.1559 0.01740 0.00845 -0.0502 0.8779 0.3639 -3.000 -0.1219 0.01701 0.00814 -0.0512 0.8715 0.3922 -2.750 -0.0968 0.01673 0.00799 -0.0505 0.8600 0.4196 -2.500 -0.0652 0.01638 0.00775 -0.0509 0.8521 0.4536 -2.250 -0.0389 0.01611 0.00763 -0.0503 0.8407 0.4894 -2.000 -0.0105 0.01584 0.00749 -0.0500 0.8307 0.5289 -1.750 0.0182 0.01558 0.00735 -0.0497 0.8204 0.5695 -1.500 0.0448 0.01540 0.00728 -0.0489 0.8085 0.6088 -1.250 0.0746 0.01517 0.00715 -0.0486 0.7986 0.6488 -1.000 0.1010 0.01504 0.00712 -0.0477 0.7857 0.6865 -0.750 0.1286 0.01494 0.00710 -0.0470 0.7735 0.7232 -0.500 0.1585 0.01484 0.00704 -0.0466 0.7624 0.7583 -0.250 0.1857 0.01483 0.00708 -0.0457 0.7490 0.7913 0.000 0.2150 0.01485 0.00711 -0.0453 0.7360 0.8215 0.250 0.2461 0.01487 0.00710 -0.0452 0.7239 0.8496 0.500 0.2789 0.01492 0.00713 -0.0456 0.7108 0.8744 0.750 0.3122 0.01501 0.00718 -0.0462 0.6971 0.8973 1.000 0.3477 0.01510 0.00720 -0.0473 0.6840 0.9180 1.250 0.3854 0.01519 0.00720 -0.0489 0.6711 0.9365 1.500 0.4242 0.01531 0.00726 -0.0508 0.6571 0.9535 1.750 0.4671 0.01543 0.00733 -0.0537 0.6428 0.9683 2.000 0.5130 0.01554 0.00737 -0.0573 0.6285 0.9817 2.250 0.5598 0.01562 0.00736 -0.0612 0.6127 0.9941 2.500 0.5936 0.01570 0.00735 -0.0626 0.5965 1.0000 2.750 0.6138 0.01581 0.00734 -0.0612 0.5820 1.0000 3.000 0.6335 0.01594 0.00744 -0.0597 0.5676 1.0000 3.250 0.6538 0.01610 0.00755 -0.0584 0.5548 1.0000 3.500 0.6747 0.01628 0.00765 -0.0570 0.5429 1.0000 3.750 0.6954 0.01647 0.00780 -0.0557 0.5306 1.0000 4.000 0.7160 0.01668 0.00799 -0.0544 0.5182 1.0000 4.250 0.7371 0.01691 0.00815 -0.0530 0.5066 1.0000 4.500 0.7579 0.01714 0.00836 -0.0517 0.4944 1.0000 4.750 0.7784 0.01739 0.00859 -0.0503 0.4816 1.0000 5.000 0.7989 0.01765 0.00881 -0.0489 0.4687 1.0000 5.250 0.8191 0.01792 0.00902 -0.0474 0.4547 1.0000 5.500 0.8388 0.01819 0.00926 -0.0458 0.4397 1.0000 5.750 0.8585 0.01848 0.00954 -0.0443 0.4245 1.0000 6.000 0.8784 0.01879 0.00985 -0.0428 0.4099 1.0000 6.250 0.8983 0.01912 0.01016 -0.0414 0.3956 1.0000 6.500 0.9179 0.01948 0.01048 -0.0399 0.3811 1.0000 6.750 0.9371 0.01985 0.01082 -0.0384 0.3662 1.0000 7.000 0.9557 0.02026 0.01120 -0.0368 0.3505 1.0000 7.250 0.9736 0.02069 0.01161 -0.0351 0.3340 1.0000 7.500 0.9909 0.02115 0.01204 -0.0334 0.3168 1.0000 7.750 1.0073 0.02166 0.01252 -0.0316 0.2990 1.0000 8.000 1.0231 0.02219 0.01304 -0.0297 0.2804 1.0000 8.250 1.0379 0.02278 0.01359 -0.0278 0.2618 1.0000 8.500 1.0515 0.02344 0.01419 -0.0257 0.2438 1.0000 8.750 1.0638 0.02416 0.01486 -0.0235 0.2272 1.0000 9.000 1.0740 0.02493 0.01557 -0.0210 0.2121 1.0000 9.250 1.0834 0.02576 0.01636 -0.0184 0.1982 1.0000 9.500 1.0924 0.02668 0.01724 -0.0160 0.1849 1.0000 9.750 1.1018 0.02764 0.01820 -0.0138 0.1719 1.0000 10.000 1.1113 0.02865 0.01922 -0.0118 0.1597 1.0000 10.250 1.1198 0.02976 0.02033 -0.0097 0.1488 1.0000 10.500 1.1268 0.03101 0.02157 -0.0078 0.1395 1.0000 10.750 1.1335 0.03235 0.02291 -0.0059 0.1309 1.0000 11.000 1.1402 0.03375 0.02435 -0.0042 0.1233 1.0000 11.250 1.1446 0.03537 0.02597 -0.0026 0.1169 1.0000 11.500 1.1509 0.03695 0.02761 -0.0012 0.1108 1.0000 11.750 1.1548 0.03875 0.02943 0.0001 0.1056 1.0000 12.000 1.1590 0.04062 0.03134 0.0013 0.1010 1.0000 12.250 1.1639 0.04250 0.03331 0.0023 0.0964 1.0000 12.500 1.1660 0.04465 0.03547 0.0032 0.0930 1.0000 12.750 1.1706 0.04669 0.03759 0.0040 0.0895 1.0000 13.000 1.1749 0.04880 0.03979 0.0046 0.0863 1.0000 13.250 1.1779 0.05107 0.04210 0.0051 0.0837 1.0000 13.500 1.1806 0.05337 0.04441 0.0056 0.0815 1.0000 13.750 1.1849 0.05566 0.04685 0.0060 0.0789 1.0000 14.000 1.1882 0.05806 0.04935 0.0063 0.0766 1.0000 14.250 1.1908 0.06053 0.05188 0.0064 0.0746 1.0000 14.500 1.1939 0.06296 0.05431 0.0066 0.0730 1.0000 14.750 1.1973 0.06550 0.05697 0.0067 0.0714 1.0000 15.000 1.1996 0.06825 0.05989 0.0066 0.0698 1.0000 15.250 1.2012 0.07109 0.06285 0.0064 0.0683 1.0000 15.500 1.2027 0.07396 0.06581 0.0061 0.0669 1.0000 15.750 1.2049 0.07674 0.06863 0.0058 0.0656 1.0000 16.000 1.2098 0.07912 0.07100 0.0057 0.0645 1.0000 16.250 1.2060 0.08296 0.07504 0.0048 0.0634 1.0000 16.500 1.2004 0.08716 0.07946 0.0035 0.0623 1.0000 16.750 1.1943 0.09150 0.08400 0.0021 0.0613 1.0000 17.000 1.1876 0.09603 0.08869 0.0005 0.0605 1.0000 17.250 1.1801 0.10076 0.09358 -0.0014 0.0596 1.0000 17.500 1.1731 0.10548 0.09843 -0.0033 0.0588 1.0000 17.750 1.1689 0.10975 0.10280 -0.0052 0.0580 1.0000 18.000 1.1726 0.11258 0.10563 -0.0061 0.0571 1.0000 18.250 1.1580 0.11899 0.11222 -0.0094 0.0565 1.0000 18.500 1.1204 0.13042 0.12398 -0.0164 0.0562 1.0000