XFOIL Version 6.96 Calculated polar for: NACA 65(3)-618 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -12.500 -0.2931 0.11126 0.10770 -0.0820 0.9815 0.0790 -12.250 -0.2831 0.10678 0.10321 -0.0861 0.9767 0.0824 -12.000 -0.3301 0.09065 0.08715 -0.1028 0.9720 0.0880 -11.750 -0.2875 0.09197 0.08842 -0.1001 0.9704 0.0896 -11.500 -0.1500 0.07578 0.07226 -0.1160 0.9459 0.1031 -11.250 -0.1312 0.07293 0.06938 -0.1177 0.9416 0.1070 -10.500 -0.4950 0.04298 0.03718 -0.1271 0.9132 0.0547 -10.250 -0.4830 0.03963 0.03358 -0.1269 0.9071 0.0541 -10.000 -0.4788 0.03772 0.03137 -0.1245 0.8980 0.0543 -9.750 -0.4677 0.03566 0.02897 -0.1232 0.8912 0.0546 -9.500 -0.4513 0.03352 0.02654 -0.1223 0.8857 0.0545 -9.250 -0.4371 0.03180 0.02459 -0.1207 0.8778 0.0545 -9.000 -0.4160 0.03021 0.02270 -0.1201 0.8727 0.0549 -8.750 -0.3973 0.02899 0.02122 -0.1190 0.8668 0.0556 -8.500 -0.3724 0.02707 0.01928 -0.1189 0.8610 0.0569 -8.250 -0.3454 0.02584 0.01797 -0.1190 0.8566 0.0579 -8.000 -0.3163 0.02474 0.01677 -0.1193 0.8532 0.0589 -7.750 -0.2953 0.02402 0.01602 -0.1183 0.8467 0.0601 -7.500 -0.2708 0.02329 0.01521 -0.1178 0.8415 0.0618 -7.250 -0.2441 0.02260 0.01440 -0.1177 0.8375 0.0636 -7.000 -0.2198 0.02184 0.01361 -0.1171 0.8328 0.0652 -6.750 -0.2006 0.02110 0.01295 -0.1159 0.8269 0.0671 -6.500 -0.1797 0.02051 0.01237 -0.1150 0.8225 0.0694 -6.250 -0.1568 0.01996 0.01176 -0.1144 0.8190 0.0727 -6.000 -0.1418 0.01961 0.01141 -0.1127 0.8133 0.0758 -5.750 -0.1268 0.01903 0.01087 -0.1111 0.8079 0.0800 -5.500 -0.1055 0.01852 0.01030 -0.1104 0.8040 0.0860 -5.250 -0.0841 0.01781 0.00960 -0.1099 0.8009 0.0978 -5.000 -0.0744 0.01713 0.00923 -0.1079 0.7945 0.1369 -4.750 -0.0716 0.01476 0.00867 -0.1062 0.7896 0.4987 -4.500 -0.0437 0.01503 0.00899 -0.1058 0.7866 0.5729 -4.250 -0.0135 0.01533 0.00920 -0.1059 0.7842 0.6012 -4.000 0.0079 0.01580 0.00967 -0.1046 0.7790 0.6185 -3.750 0.0334 0.01614 0.00993 -0.1040 0.7746 0.6337 -3.500 0.0602 0.01656 0.01036 -0.1031 0.7714 0.6467 -3.250 0.0868 0.01733 0.01111 -0.1016 0.7688 0.6679 -3.000 0.1122 0.01834 0.01214 -0.0994 0.7666 0.6865 -2.750 0.1261 0.01923 0.01317 -0.0955 0.7615 0.6936 -2.500 0.1504 0.01940 0.01328 -0.0950 0.7575 0.7021 -2.250 0.1779 0.01934 0.01313 -0.0951 0.7545 0.7069 -2.000 0.2065 0.01936 0.01309 -0.0950 0.7520 0.7101 -1.750 0.2366 0.01936 0.01301 -0.0955 0.7500 0.7140 -1.500 0.2551 0.01950 0.01315 -0.0948 0.7452 0.7193 -1.250 0.2799 0.01948 0.01308 -0.0951 0.7414 0.7237 -1.000 0.3059 0.01949 0.01307 -0.0949 0.7384 0.7262 -0.750 0.3351 0.01945 0.01297 -0.0952 0.7360 0.7291 -0.500 0.3663 0.01938 0.01284 -0.0961 0.7340 0.7325 -0.250 0.3898 0.01953 0.01298 -0.0962 0.7305 0.7367 0.000 0.4109 0.01974 0.01318 -0.0960 0.7261 0.7411 0.250 0.4343 0.01986 0.01332 -0.0954 0.7228 0.7436 0.500 0.4626 0.01985 0.01330 -0.0957 0.7203 0.7463 0.750 0.4939 0.01980 0.01321 -0.0966 0.7183 0.7494 1.000 0.5267 0.01978 0.01315 -0.0979 0.7166 0.7532 1.250 0.5410 0.02036 0.01379 -0.0968 0.7115 0.7582 1.500 0.5597 0.02065 0.01413 -0.0956 0.7074 0.7607 1.750 0.5864 0.02072 0.01422 -0.0956 0.7046 0.7636 2.000 0.6161 0.02076 0.01426 -0.0962 0.7025 0.7669 2.250 0.6490 0.02075 0.01424 -0.0975 0.7008 0.7709 2.500 0.6860 0.02072 0.01417 -0.0997 0.6993 0.7755 2.750 0.6761 0.02198 0.01562 -0.0941 0.6911 0.7789 3.000 0.7026 0.02210 0.01577 -0.0942 0.6883 0.7822 3.250 0.7343 0.02206 0.01576 -0.0951 0.6861 0.7860 3.500 0.7701 0.02195 0.01566 -0.0968 0.6844 0.7904 3.750 0.8069 0.02183 0.01554 -0.0986 0.6828 0.7944 4.000 0.7886 0.02340 0.01729 -0.0918 0.6732 0.7991 4.250 0.8224 0.02321 0.01715 -0.0928 0.6707 0.8033 4.500 0.8608 0.02295 0.01691 -0.0948 0.6687 0.8079 4.750 0.9002 0.02262 0.01660 -0.0969 0.6670 0.8118 5.000 0.8822 0.02418 0.01834 -0.0901 0.6576 0.8171 5.250 0.9175 0.02389 0.01810 -0.0913 0.6548 0.8222 5.500 0.9603 0.02339 0.01764 -0.0939 0.6525 0.8276 5.750 1.0033 0.02267 0.01697 -0.0959 0.6504 0.8313 6.000 0.9952 0.02372 0.01818 -0.0906 0.6414 0.8380 6.250 1.0413 0.02285 0.01734 -0.0933 0.6375 0.8435 6.500 1.0970 0.02139 0.01589 -0.0970 0.6338 0.8471 6.750 1.1016 0.02152 0.01615 -0.0930 0.6239 0.8542 7.000 1.1488 0.01977 0.01435 -0.0951 0.6116 0.8605 7.250 1.1809 0.01860 0.01315 -0.0947 0.5991 0.8659 7.500 1.1895 0.01847 0.01314 -0.0912 0.5874 0.8745 7.750 1.1990 0.01830 0.01307 -0.0877 0.5768 0.8824 8.000 1.2167 0.01799 0.01280 -0.0856 0.5654 0.8915 8.250 1.2150 0.01796 0.01288 -0.0802 0.5536 0.9029 8.500 1.2132 0.01811 0.01313 -0.0750 0.5402 0.9169 8.750 1.2137 0.01824 0.01334 -0.0704 0.5244 0.9339 9.000 1.2136 0.01839 0.01354 -0.0659 0.5052 0.9581 9.250 1.2221 0.01898 0.01409 -0.0643 0.4710 1.0000 9.500 1.2240 0.02028 0.01512 -0.0620 0.4173 1.0000 10.000 1.1982 0.02519 0.01930 -0.0552 0.3109 1.0000 10.250 1.1815 0.02824 0.02202 -0.0520 0.2610 1.0000 10.500 1.1641 0.03157 0.02502 -0.0491 0.2105 1.0000 10.750 1.1461 0.03518 0.02827 -0.0465 0.1582 1.0000 11.000 1.1299 0.03888 0.03157 -0.0443 0.1085 1.0000 11.250 1.1203 0.04220 0.03463 -0.0426 0.0810 1.0000 11.500 1.1178 0.04503 0.03736 -0.0414 0.0690 1.0000 11.750 1.1204 0.04746 0.03981 -0.0406 0.0620 1.0000 12.000 1.1211 0.05013 0.04244 -0.0398 0.0574 1.0000 12.250 1.1279 0.05225 0.04461 -0.0393 0.0534 1.0000 12.500 1.1304 0.05478 0.04711 -0.0387 0.0506 1.0000 12.750 1.1375 0.05690 0.04928 -0.0382 0.0482 1.0000 13.000 1.1462 0.05888 0.05130 -0.0378 0.0461 1.0000 13.250 1.1549 0.06084 0.05325 -0.0374 0.0443 1.0000 13.500 1.1659 0.06249 0.05484 -0.0367 0.0425 1.0000 13.750 1.1785 0.06412 0.05658 -0.0364 0.0409 1.0000 14.000 1.1921 0.06564 0.05814 -0.0361 0.0393 1.0000 14.250 1.2072 0.06697 0.05947 -0.0357 0.0380 1.0000 14.500 1.2367 0.06693 0.05927 -0.0349 0.0366 1.0000 14.750 1.2525 0.06842 0.06091 -0.0346 0.0360 1.0000 15.000 1.2691 0.06991 0.06254 -0.0342 0.0352 1.0000 15.250 1.2866 0.07141 0.06418 -0.0339 0.0345 1.0000 15.500 1.3025 0.07310 0.06601 -0.0337 0.0339 1.0000 15.750 1.3173 0.07491 0.06792 -0.0335 0.0331 1.0000 16.000 1.3309 0.07683 0.06992 -0.0335 0.0324 1.0000 16.250 1.3498 0.07848 0.07160 -0.0335 0.0317 1.0000 16.500 1.3772 0.08056 0.07378 -0.0334 0.0311 1.0000 16.750 1.3754 0.08402 0.07749 -0.0333 0.0310 1.0000 17.000 1.3715 0.08779 0.08151 -0.0334 0.0309 1.0000 17.250 1.3660 0.09183 0.08581 -0.0337 0.0309 1.0000 17.500 1.3591 0.09616 0.09038 -0.0342 0.0309 1.0000 17.750 1.3509 0.10072 0.09517 -0.0350 0.0309 1.0000 18.000 1.3410 0.10559 0.10027 -0.0361 0.0309 1.0000 18.250 1.3309 0.11067 0.10558 -0.0374 0.0310 1.0000 18.500 1.3228 0.11583 0.11092 -0.0389 0.0311 1.0000 18.750 1.3041 0.12147 0.11680 -0.0413 0.0313 1.0000 19.000 1.2697 0.12969 0.12539 -0.0456 0.0317 1.0000 19.250 1.1391 0.15912 0.15572 -0.0639 0.0342 1.0000