XFOIL Version 6.96 Calculated polar for: NACA 16-018 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.750 -0.9234 0.11596 0.11280 -0.0652 1.0000 0.0188 -19.500 -0.9631 0.10559 0.10218 -0.0699 1.0000 0.0187 -19.250 -0.9863 0.09892 0.09537 -0.0724 1.0000 0.0188 -19.000 -1.0062 0.09311 0.08942 -0.0740 1.0000 0.0189 -18.750 -1.0252 0.08776 0.08393 -0.0752 1.0000 0.0190 -18.500 -1.0404 0.08327 0.07932 -0.0757 1.0000 0.0191 -18.250 -1.0553 0.07904 0.07497 -0.0757 1.0000 0.0192 -18.000 -1.0689 0.07524 0.07105 -0.0754 1.0000 0.0194 -17.750 -1.0820 0.07167 0.06736 -0.0746 1.0000 0.0196 -17.500 -1.0942 0.06839 0.06396 -0.0735 1.0000 0.0198 -17.250 -1.1059 0.06534 0.06079 -0.0721 1.0000 0.0200 -17.000 -1.1162 0.06260 0.05791 -0.0703 1.0000 0.0202 -16.750 -1.1261 0.05999 0.05518 -0.0683 1.0000 0.0205 -16.500 -1.1272 0.05713 0.05215 -0.0680 0.9993 0.0208 -16.250 -1.1259 0.05444 0.04928 -0.0680 0.9983 0.0213 -16.000 -1.1233 0.05205 0.04670 -0.0677 0.9972 0.0216 -15.750 -1.1220 0.04959 0.04404 -0.0670 0.9963 0.0220 -15.500 -1.1150 0.04752 0.04192 -0.0665 0.9955 0.0226 -15.250 -1.1049 0.04599 0.04034 -0.0663 0.9948 0.0231 -15.000 -1.0943 0.04454 0.03882 -0.0661 0.9941 0.0236 -14.750 -1.0857 0.04312 0.03731 -0.0651 0.9928 0.0241 -14.500 -1.0767 0.04173 0.03581 -0.0640 0.9910 0.0247 -14.250 -1.0654 0.04040 0.03435 -0.0632 0.9895 0.0253 -14.000 -1.0529 0.03919 0.03299 -0.0625 0.9880 0.0259 -13.750 -1.0393 0.03784 0.03150 -0.0619 0.9870 0.0265 -13.500 -1.0233 0.03654 0.03019 -0.0616 0.9862 0.0274 -13.250 -1.0066 0.03560 0.02922 -0.0614 0.9853 0.0282 -13.000 -0.9885 0.03472 0.02828 -0.0614 0.9845 0.0291 -12.750 -0.9690 0.03385 0.02731 -0.0615 0.9839 0.0300 -12.500 -0.9480 0.03305 0.02640 -0.0617 0.9833 0.0308 -12.250 -0.9409 0.03235 0.02562 -0.0588 0.9792 0.0313 -12.000 -0.9248 0.03109 0.02433 -0.0579 0.9778 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-0.0448 0.9461 0.0980 -7.000 -0.5369 0.01891 0.01196 -0.0449 0.9453 0.1266 -6.750 -0.5445 0.01875 0.01187 -0.0379 0.9381 0.1430 -6.500 -0.5302 0.01821 0.01150 -0.0358 0.9354 0.1773 -6.250 -0.5137 0.01751 0.01104 -0.0344 0.9337 0.2283 -6.000 -0.4991 0.01661 0.01049 -0.0326 0.9323 0.3012 -5.750 -0.4889 0.01553 0.00983 -0.0300 0.9309 0.3913 -5.500 -0.4836 0.01437 0.00911 -0.0262 0.9296 0.4892 -4.750 -0.5635 0.01346 0.00878 0.0091 0.9054 0.6214 -4.500 -0.5649 0.01287 0.00849 0.0156 0.9027 0.6901 -4.250 -0.5466 0.01261 0.00839 0.0178 0.9014 0.7370 -4.000 -0.5741 0.01289 0.00872 0.0300 0.8916 0.7533 -3.750 -0.5528 0.01282 0.00868 0.0315 0.8897 0.7790 -3.500 -0.5237 0.01280 0.00868 0.0312 0.8886 0.7971 -3.250 -0.4949 0.01283 0.00870 0.0310 0.8876 0.8128 -3.000 -0.4671 0.01290 0.00877 0.0311 0.8867 0.8273 -2.750 -0.4816 0.01324 0.00911 0.0404 0.8779 0.8377 -2.500 -0.4445 0.01349 0.00935 0.0382 0.8766 0.8446 -2.250 -0.4183 0.01355 0.00937 0.0385 0.8749 0.8516 -2.000 -0.3707 0.01412 0.00995 0.0342 0.8748 0.8594 -1.750 -0.2278 0.01532 0.01114 0.0093 0.8864 0.8598 -1.500 -0.2727 0.01551 0.01133 0.0254 0.8746 0.8715 -1.250 -0.2258 0.01574 0.01155 0.0209 0.8744 0.8720 -1.000 -0.1802 0.01593 0.01171 0.0166 0.8741 0.8724 -0.750 -0.1343 0.01603 0.01180 0.0123 0.8739 0.8727 -0.500 -0.0890 0.01609 0.01185 0.0081 0.8737 0.8729 -0.250 -0.0443 0.01612 0.01187 0.0040 0.8735 0.8731 0.000 0.0000 0.01613 0.01188 0.0000 0.8733 0.8733 0.250 0.0444 0.01612 0.01187 -0.0040 0.8731 0.8735 0.500 0.0890 0.01608 0.01184 -0.0081 0.8729 0.8737 0.750 0.1343 0.01603 0.01180 -0.0123 0.8727 0.8739 1.000 0.1801 0.01593 0.01171 -0.0166 0.8724 0.8741 1.250 0.2258 0.01574 0.01155 -0.0209 0.8720 0.8744 1.500 0.2727 0.01551 0.01133 -0.0254 0.8715 0.8746 1.750 0.2278 0.01532 0.01114 -0.0093 0.8598 0.8864 2.000 0.3123 0.01434 0.01018 -0.0217 0.8591 0.8837 2.250 0.3653 0.01333 0.00914 -0.0269 0.8505 0.8843 2.500 0.4098 0.01322 0.00905 -0.0306 0.8437 0.8836 2.750 0.4580 0.01303 0.00887 -0.0353 0.8384 0.8831 3.000 0.4670 0.01290 0.00877 -0.0311 0.8274 0.8867 3.250 0.4949 0.01283 0.00870 -0.0310 0.8130 0.8876 3.500 0.5236 0.01280 0.00868 -0.0312 0.7971 0.8886 3.750 0.5528 0.01282 0.00868 -0.0315 0.7791 0.8897 4.000 0.5741 0.01289 0.00872 -0.0301 0.7534 0.8917 4.250 0.5467 0.01260 0.00839 -0.0179 0.7368 0.9014 4.500 0.5649 0.01287 0.00849 -0.0156 0.6897 0.9027 4.750 0.5634 0.01346 0.00878 -0.0090 0.6211 0.9054 5.500 0.4847 0.01441 0.00914 0.0259 0.4868 0.9294 6.750 0.5132 0.01824 0.01148 0.0451 0.1625 0.9446 7.000 0.5373 0.01889 0.01195 0.0448 0.1266 0.9453 7.250 0.5610 0.01951 0.01242 0.0447 0.0979 0.9461 7.500 0.5845 0.02009 0.01289 0.0447 0.0779 0.9470 7.750 0.6079 0.02064 0.01338 0.0447 0.0664 0.9481 8.000 0.6300 0.02118 0.01391 0.0451 0.0600 0.9495 8.250 0.6512 0.02165 0.01439 0.0456 0.0560 0.9514 8.500 0.6437 0.02191 0.01465 0.0525 0.0540 0.9586 8.750 0.6685 0.02246 0.01523 0.0521 0.0511 0.9592 9.000 0.6938 0.02295 0.01576 0.0516 0.0488 0.9600 9.250 0.7178 0.02354 0.01636 0.0513 0.0467 0.9608 9.500 0.7361 0.02449 0.01731 0.0520 0.0444 0.9620 9.750 0.7602 0.02496 0.01784 0.0518 0.0432 0.9633 10.000 0.7805 0.02550 0.01844 0.0523 0.0418 0.9651 10.250 0.7937 0.02602 0.01899 0.0543 0.0406 0.9681 10.500 0.8012 0.02652 0.01951 0.0575 0.0396 0.9719 10.750 0.8218 0.02745 0.02044 0.0574 0.0379 0.9725 11.000 0.8442 0.02827 0.02133 0.0572 0.0368 0.9732 11.250 0.8675 0.02891 0.02204 0.0569 0.0358 0.9741 11.500 0.8888 0.02959 0.02278 0.0569 0.0347 0.9751 11.750 0.9085 0.03028 0.02350 0.0571 0.0336 0.9764 12.000 0.9260 0.03106 0.02430 0.0577 0.0325 0.9779 12.250 0.9419 0.03232 0.02558 0.0586 0.0313 0.9794 12.500 0.9498 0.03302 0.02637 0.0614 0.0308 0.9834 12.750 0.9708 0.03382 0.02728 0.0611 0.0300 0.9839 13.000 0.9902 0.03468 0.02823 0.0610 0.0291 0.9846 13.250 1.0084 0.03556 0.02917 0.0611 0.0282 0.9854 13.500 1.0251 0.03649 0.03014 0.0612 0.0274 0.9863 13.750 1.0413 0.03790 0.03155 0.0616 0.0264 0.9870 14.000 1.0546 0.03914 0.03294 0.0622 0.0259 0.9882 14.250 1.0671 0.04036 0.03430 0.0629 0.0253 0.9896 14.500 1.0784 0.04167 0.03575 0.0637 0.0247 0.9913 14.750 1.0873 0.04306 0.03725 0.0648 0.0241 0.9930 15.000 1.0966 0.04448 0.03876 0.0657 0.0235 0.9941 15.250 1.1072 0.04593 0.04028 0.0659 0.0230 0.9949 15.500 1.1174 0.04746 0.04185 0.0660 0.0226 0.9957 15.750 1.1239 0.04964 0.04409 0.0667 0.0220 0.9964 16.000 1.1257 0.05201 0.04666 0.0673 0.0216 0.9974 16.250 1.1283 0.05440 0.04924 0.0675 0.0212 0.9985 16.500 1.1298 0.05709 0.05211 0.0676 0.0208 0.9995 16.750 1.1272 0.05984 0.05502 0.0682 0.0205 1.0000 17.000 1.1176 0.06240 0.05771 0.0703 0.0202 1.0000 17.250 1.1072 0.06515 0.06059 0.0721 0.0200 1.0000 17.500 1.0953 0.06823 0.06380 0.0735 0.0198 1.0000 17.750 1.0833 0.07146 0.06715 0.0747 0.0196 1.0000 18.000 1.0701 0.07503 0.07084 0.0754 0.0194 1.0000 18.250 1.0566 0.07882 0.07475 0.0758 0.0192 1.0000 18.500 1.0426 0.08291 0.07895 0.0757 0.0191 1.0000 18.750 1.0270 0.08745 0.08361 0.0752 0.0190 1.0000 19.000 1.0088 0.09266 0.08896 0.0742 0.0189 1.0000 19.250 0.9888 0.09847 0.09491 0.0725 0.0188 1.0000