XFOIL Version 6.96 Calculated polar for: NACA M6 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 ------ -------- --------- --------- -------- -------- -------- -10.250 -0.5197 0.08321 0.07779 -0.0415 1.0000 0.0478 -10.000 -0.5271 0.07830 0.07289 -0.0442 1.0000 0.0475 -9.750 -0.5399 0.07351 0.06809 -0.0459 1.0000 0.0472 -9.500 -0.5575 0.06905 0.06358 -0.0460 1.0000 0.0470 -9.250 -0.5780 0.06509 0.05955 -0.0442 1.0000 0.0467 -9.000 -0.5975 0.06180 0.05619 -0.0409 1.0000 0.0465 -8.750 -0.6152 0.05819 0.05245 -0.0374 1.0000 0.0464 -8.500 -0.6311 0.05461 0.04868 -0.0334 1.0000 0.0464 -8.250 -0.6448 0.05124 0.04507 -0.0290 1.0000 0.0466 -8.000 -0.6564 0.04815 0.04169 -0.0243 1.0000 0.0469 -7.750 -0.6655 0.04544 0.03869 -0.0194 1.0000 0.0472 -7.500 -0.6727 0.04315 0.03614 -0.0144 1.0000 0.0474 -7.250 -0.6711 0.04071 0.03337 -0.0109 0.9959 0.0475 -7.000 -0.6484 0.03752 0.02969 -0.0115 0.9829 0.0476 -6.750 -0.6229 0.03482 0.02651 -0.0120 0.9713 0.0478 -6.500 -0.5948 0.03252 0.02395 -0.0129 0.9603 0.0483 -6.250 -0.5639 0.03061 0.02178 -0.0141 0.9500 0.0488 -6.000 -0.5305 0.02907 0.02005 -0.0157 0.9407 0.0498 -5.750 -0.4978 0.02780 0.01861 -0.0170 0.9298 0.0514 -5.500 -0.4651 0.02647 0.01705 -0.0181 0.9186 0.0528 -5.250 -0.4292 0.02506 0.01539 -0.0197 0.9091 0.0538 -5.000 -0.3954 0.02384 0.01398 -0.0208 0.8975 0.0547 -4.750 -0.3628 0.02278 0.01275 -0.0216 0.8855 0.0557 -4.500 -0.3307 0.02184 0.01169 -0.0224 0.8738 0.0568 -4.250 -0.3008 0.02098 0.01082 -0.0228 0.8623 0.0583 -4.000 -0.2746 0.02036 0.01018 -0.0224 0.8493 0.0604 -3.750 -0.2490 0.01984 0.00960 -0.0218 0.8366 0.0635 -3.500 -0.2232 0.01934 0.00900 -0.0212 0.8249 0.0670 -3.250 -0.1982 0.01875 0.00840 -0.0206 0.8143 0.0707 -3.000 -0.1747 0.01832 0.00792 -0.0196 0.8021 0.0757 -2.750 -0.1506 0.01784 0.00744 -0.0186 0.7913 0.0838 -2.500 -0.1254 0.01734 0.00699 -0.0179 0.7816 0.1020 -2.250 -0.1013 0.01690 0.00672 -0.0172 0.7705 0.1407 -2.000 -0.0758 0.01641 0.00645 -0.0167 0.7612 0.1975 -1.750 0.0452 0.01469 0.00733 -0.0342 0.7539 0.8494 -1.500 0.0907 0.01554 0.00800 -0.0360 0.7444 0.9034 -1.250 0.1453 0.01618 0.00843 -0.0402 0.7343 0.9325 -1.000 0.1927 0.01656 0.00864 -0.0436 0.7240 0.9530 -0.750 0.2509 0.01668 0.00855 -0.0494 0.7146 0.9707 -0.500 0.3130 0.01648 0.00821 -0.0564 0.7031 0.9883 -0.250 0.3542 0.01623 0.00784 -0.0593 0.6933 0.9960 0.000 0.3862 0.01605 0.00755 -0.0605 0.6836 0.9997 0.250 0.4086 0.01603 0.00747 -0.0596 0.6738 1.0000 0.500 0.4302 0.01603 0.00737 -0.0585 0.6655 1.0000 0.750 0.4515 0.01605 0.00735 -0.0574 0.6553 1.0000 1.000 0.4732 0.01608 0.00730 -0.0563 0.6473 1.0000 1.250 0.4946 0.01612 0.00732 -0.0552 0.6376 1.0000 1.500 0.5164 0.01616 0.00731 -0.0541 0.6293 1.0000 1.750 0.5380 0.01622 0.00734 -0.0531 0.6201 1.0000 2.000 0.5597 0.01629 0.00739 -0.0520 0.6115 1.0000 2.250 0.5814 0.01636 0.00744 -0.0509 0.6027 1.0000 2.500 0.6031 0.01644 0.00752 -0.0498 0.5936 1.0000 2.750 0.6249 0.01652 0.00759 -0.0486 0.5849 1.0000 3.000 0.6463 0.01663 0.00771 -0.0475 0.5751 1.0000 3.250 0.6680 0.01671 0.00775 -0.0463 0.5660 1.0000 3.500 0.6891 0.01681 0.00790 -0.0450 0.5547 1.0000 3.750 0.7102 0.01691 0.00802 -0.0438 0.5438 1.0000 4.000 0.7318 0.01701 0.00809 -0.0425 0.5343 1.0000 4.250 0.7526 0.01715 0.00830 -0.0413 0.5228 1.0000 4.500 0.7738 0.01729 0.00848 -0.0400 0.5125 1.0000 4.750 0.7951 0.01742 0.00861 -0.0387 0.5027 1.0000 5.000 0.8157 0.01760 0.00888 -0.0374 0.4914 1.0000 5.250 0.8365 0.01778 0.00911 -0.0361 0.4810 1.0000 5.500 0.8574 0.01794 0.00928 -0.0348 0.4705 1.0000 5.750 0.8771 0.01813 0.00953 -0.0333 0.4565 1.0000 6.000 0.8965 0.01833 0.00978 -0.0317 0.4417 1.0000 6.250 0.9155 0.01855 0.01003 -0.0301 0.4260 1.0000 6.500 0.9340 0.01879 0.01029 -0.0284 0.4093 1.0000 6.750 0.9515 0.01906 0.01056 -0.0265 0.3900 1.0000 7.000 0.9677 0.01939 0.01090 -0.0245 0.3661 1.0000 7.250 0.9829 0.01978 0.01125 -0.0223 0.3412 1.0000 7.500 0.9971 0.02026 0.01166 -0.0201 0.3146 1.0000 7.750 1.0110 0.02080 0.01217 -0.0178 0.2885 1.0000 8.000 1.0234 0.02143 0.01275 -0.0154 0.2624 1.0000 8.250 1.0336 0.02218 0.01340 -0.0127 0.2345 1.0000 8.500 1.0418 0.02306 0.01416 -0.0097 0.2067 1.0000 8.750 1.0486 0.02402 0.01503 -0.0067 0.1794 1.0000 9.000 1.0531 0.02509 0.01599 -0.0033 0.1529 1.0000 9.250 1.0549 0.02627 0.01704 0.0003 0.1285 1.0000 9.500 1.0545 0.02749 0.01818 0.0042 0.1105 1.0000 9.750 1.0503 0.02866 0.01928 0.0087 0.0996 1.0000 10.000 1.0434 0.02995 0.02050 0.0133 0.0925 1.0000 10.250 1.0402 0.03128 0.02188 0.0169 0.0860 1.0000 10.500 1.0344 0.03295 0.02353 0.0203 0.0812 1.0000 10.750 1.0341 0.03449 0.02514 0.0228 0.0765 1.0000 11.000 1.0333 0.03621 0.02693 0.0250 0.0723 1.0000 11.250 1.0298 0.03825 0.02896 0.0271 0.0690 1.0000 11.500 1.0320 0.04000 0.03082 0.0287 0.0659 1.0000 11.750 1.0342 0.04184 0.03275 0.0301 0.0626 1.0000 12.000 1.0351 0.04384 0.03479 0.0313 0.0598 1.0000 12.250 1.0355 0.04595 0.03689 0.0325 0.0576 1.0000 12.500 1.0403 0.04778 0.03887 0.0336 0.0551 1.0000 12.750 1.0439 0.04975 0.04093 0.0345 0.0528 1.0000 13.000 1.0463 0.05185 0.04308 0.0353 0.0507 1.0000 13.250 1.0486 0.05400 0.04523 0.0360 0.0490 1.0000 13.500 1.0536 0.05602 0.04737 0.0368 0.0473 1.0000 13.750 1.0578 0.05817 0.04967 0.0375 0.0456 1.0000 14.000 1.0607 0.06046 0.05207 0.0380 0.0439 1.0000 14.250 1.0628 0.06283 0.05450 0.0383 0.0425 1.0000 14.500 1.0660 0.06509 0.05675 0.0386 0.0412 1.0000 14.750 1.0681 0.06766 0.05944 0.0389 0.0400 1.0000 15.000 1.0662 0.07084 0.06285 0.0388 0.0388 1.0000 15.250 1.0642 0.07408 0.06629 0.0386 0.0378 1.0000 15.500 1.0615 0.07747 0.06984 0.0382 0.0370 1.0000 15.750 1.0573 0.08110 0.07361 0.0375 0.0361 1.0000 16.000 1.0536 0.08472 0.07734 0.0367 0.0353 1.0000 16.250 1.0509 0.08823 0.08093 0.0359 0.0346 1.0000 16.500 1.0513 0.09127 0.08395 0.0354 0.0338 1.0000 16.750 1.0345 0.09738 0.09034 0.0328 0.0334 1.0000 17.000 1.0187 0.10359 0.09678 0.0301 0.0332 1.0000 17.250 0.9975 0.11114 0.10457 0.0264 0.0329 1.0000 17.500 0.9744 0.11947 0.11313 0.0221 0.0329 1.0000 17.750 0.9458 0.12953 0.12340 0.0166 0.0330 1.0000 18.000 0.9077 0.14278 0.13684 0.0092 0.0333 1.0000