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 = 0.500 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -15.000 -0.5409 0.08503 0.08234 -0.0897 1.0000 0.0254 -14.750 -0.5659 0.07892 0.07621 -0.0916 1.0000 0.0252 -14.500 -0.6006 0.06798 0.06503 -0.1010 0.9971 0.0251 -14.250 -0.6271 0.05962 0.05641 -0.1082 0.9883 0.0250 -14.000 -0.6454 0.05298 0.04951 -0.1137 0.9813 0.0250 -13.750 -0.6637 0.04703 0.04318 -0.1190 0.9723 0.0252 -13.500 -0.6690 0.04259 0.03837 -0.1241 0.9641 0.0255 -13.250 -0.6582 0.03822 0.03380 -0.1280 0.9573 0.0260 -13.000 -0.6291 0.03693 0.03252 -0.1312 0.9497 0.0265 -12.750 -0.6057 0.03506 0.03052 -0.1344 0.9398 0.0269 -12.500 -0.5918 0.03348 0.02878 -0.1355 0.9258 0.0275 -12.250 -0.5865 0.03173 0.02679 -0.1347 0.9116 0.0278 -12.000 -0.5826 0.03028 0.02511 -0.1331 0.8988 0.0283 -11.500 -0.5751 0.02787 0.02224 -0.1286 0.8766 0.0292 -11.250 -0.5728 0.02708 0.02122 -0.1256 0.8672 0.0296 -11.000 -0.5618 0.02562 0.01956 -0.1239 0.8591 0.0302 -10.750 -0.5348 0.02420 0.01807 -0.1245 0.8537 0.0309 -10.500 -0.5166 0.02335 0.01716 -0.1236 0.8468 0.0313 -10.250 -0.4982 0.02266 0.01640 -0.1227 0.8399 0.0319 -10.000 -0.4784 0.02199 0.01563 -0.1219 0.8337 0.0325 -9.750 -0.4602 0.02140 0.01497 -0.1209 0.8269 0.0333 -9.500 -0.4395 0.02074 0.01418 -0.1201 0.8211 0.0340 -9.250 -0.4187 0.02017 0.01349 -0.1194 0.8157 0.0345 -9.000 -0.3990 0.01970 0.01292 -0.1184 0.8096 0.0349 -8.750 -0.3702 0.01845 0.01166 -0.1188 0.8049 0.0358 -8.500 -0.3493 0.01786 0.01105 -0.1181 0.7998 0.0366 -8.250 -0.3303 0.01735 0.01054 -0.1170 0.7940 0.0374 -8.000 -0.3107 0.01692 0.01006 -0.1161 0.7885 0.0383 -7.750 -0.2904 0.01649 0.00954 -0.1152 0.7836 0.0391 -7.500 -0.2712 0.01603 0.00907 -0.1142 0.7785 0.0399 -7.250 -0.2510 0.01564 0.00862 -0.1133 0.7735 0.0405 -7.000 -0.2327 0.01508 0.00800 -0.1122 0.7689 0.0414 -6.750 -0.2150 0.01451 0.00741 -0.1110 0.7644 0.0426 -6.500 -0.1944 0.01411 0.00701 -0.1103 0.7595 0.0439 -6.250 -0.1721 0.01378 0.00664 -0.1097 0.7550 0.0456 -6.000 -0.1486 0.01348 0.00626 -0.1093 0.7508 0.0471 -5.750 -0.1268 0.01305 0.00581 -0.1088 0.7466 0.0489 -5.500 -0.1035 0.01269 0.00545 -0.1084 0.7424 0.0516 -5.250 -0.0785 0.01242 0.00515 -0.1083 0.7385 0.0549 -5.000 -0.0537 0.01208 0.00480 -0.1082 0.7349 0.0615 -4.750 -0.0291 0.01168 0.00447 -0.1081 0.7313 0.0810 -4.500 -0.0098 0.01048 0.00392 -0.1080 0.7273 0.2239 -4.250 0.0113 0.00896 0.00333 -0.1087 0.7233 0.4562 -4.000 0.0396 0.00878 0.00333 -0.1091 0.7199 0.5321 -3.750 0.0691 0.00883 0.00335 -0.1096 0.7166 0.5601 -3.500 0.0979 0.00887 0.00339 -0.1099 0.7135 0.5768 -3.250 0.1266 0.00890 0.00342 -0.1102 0.7101 0.5885 -3.000 0.1559 0.00897 0.00342 -0.1105 0.7068 0.5998 -2.750 0.1851 0.00911 0.00353 -0.1108 0.7037 0.6152 -2.500 0.2139 0.00932 0.00374 -0.1109 0.7007 0.6305 -2.250 0.2420 0.00951 0.00397 -0.1109 0.6977 0.6426 -2.000 0.2708 0.00964 0.00406 -0.1112 0.6946 0.6505 -1.750 0.2994 0.00961 0.00402 -0.1115 0.6916 0.6538 -1.500 0.3283 0.00961 0.00401 -0.1118 0.6887 0.6564 -1.250 0.3576 0.00964 0.00400 -0.1123 0.6861 0.6592 -1.000 0.3875 0.00970 0.00401 -0.1129 0.6834 0.6622 -0.750 0.4164 0.00974 0.00402 -0.1133 0.6806 0.6651 -0.500 0.4454 0.00976 0.00402 -0.1138 0.6777 0.6679 -0.250 0.4741 0.00974 0.00401 -0.1142 0.6749 0.6706 0.000 0.5029 0.00976 0.00403 -0.1145 0.6723 0.6731 0.250 0.5321 0.00979 0.00406 -0.1150 0.6699 0.6756 0.500 0.5617 0.00986 0.00410 -0.1156 0.6674 0.6784 0.750 0.5910 0.00995 0.00418 -0.1161 0.6648 0.6815 1.000 0.6193 0.00999 0.00423 -0.1164 0.6622 0.6846 1.250 0.6480 0.01003 0.00428 -0.1168 0.6596 0.6873 1.500 0.6765 0.01005 0.00434 -0.1172 0.6570 0.6899 1.750 0.7053 0.01009 0.00440 -0.1176 0.6545 0.6926 2.000 0.7345 0.01016 0.00447 -0.1181 0.6521 0.6957 2.250 0.7645 0.01030 0.00459 -0.1187 0.6497 0.6991 2.500 0.7925 0.01038 0.00471 -0.1190 0.6473 0.7025 2.750 0.8203 0.01043 0.00480 -0.1193 0.6446 0.7055 3.000 0.8480 0.01047 0.00491 -0.1195 0.6418 0.7085 3.250 0.8764 0.01053 0.00501 -0.1198 0.6391 0.7116 3.500 0.9053 0.01058 0.00508 -0.1202 0.6360 0.7150 3.750 0.9352 0.01073 0.00520 -0.1209 0.6326 0.7188 4.000 0.9610 0.01076 0.00531 -0.1207 0.6289 0.7225 4.250 0.9875 0.01077 0.00541 -0.1206 0.6250 0.7261 4.500 1.0151 0.01080 0.00547 -0.1208 0.6210 0.7296 4.750 1.0442 0.01088 0.00553 -0.1212 0.6160 0.7335 5.000 1.0669 0.01083 0.00558 -0.1203 0.6090 0.7378 5.250 1.0930 0.01079 0.00552 -0.1201 0.6014 0.7417 5.500 1.1148 0.01076 0.00560 -0.1190 0.5927 0.7456 5.750 1.1380 0.01077 0.00559 -0.1182 0.5826 0.7502 6.000 1.1590 0.01078 0.00569 -0.1170 0.5724 0.7552 6.250 1.1804 0.01084 0.00578 -0.1159 0.5617 0.7599 6.500 1.2005 0.01094 0.00590 -0.1145 0.5505 0.7643 6.750 1.2193 0.01105 0.00607 -0.1130 0.5373 0.7695 7.000 1.2363 0.01123 0.00625 -0.1111 0.5215 0.7750 7.250 1.2462 0.01144 0.00647 -0.1078 0.5013 0.7802 7.500 1.2504 0.01185 0.00682 -0.1036 0.4735 0.7864 7.750 1.2469 0.01262 0.00743 -0.0982 0.4336 0.7936 8.000 1.2353 0.01377 0.00839 -0.0919 0.3888 0.8006 8.250 1.2221 0.01527 0.00966 -0.0859 0.3441 0.8088 8.500 1.2103 0.01689 0.01111 -0.0805 0.3010 0.8163 8.750 1.1996 0.01871 0.01273 -0.0758 0.2586 0.8251 9.000 1.1893 0.02064 0.01448 -0.0714 0.2185 0.8333 9.250 1.1818 0.02263 0.01629 -0.0678 0.1800 0.8428 9.500 1.1741 0.02466 0.01817 -0.0643 0.1442 0.8522 9.750 1.1668 0.02684 0.02018 -0.0611 0.1081 0.8630 10.000 1.1601 0.02905 0.02224 -0.0581 0.0771 0.8748 10.250 1.1566 0.03107 0.02417 -0.0555 0.0549 0.8880 10.500 1.1576 0.03275 0.02585 -0.0532 0.0451 0.9042 10.750 1.1600 0.03420 0.02735 -0.0509 0.0401 0.9274 11.000 1.1653 0.03582 0.02903 -0.0497 0.0365 1.0000 11.250 1.1770 0.03735 0.03059 -0.0493 0.0339 1.0000 11.500 1.1840 0.03925 0.03250 -0.0486 0.0318 1.0000 11.750 1.1928 0.04101 0.03430 -0.0480 0.0301 1.0000 12.000 1.2021 0.04276 0.03609 -0.0475 0.0287 1.0000 12.250 1.2100 0.04464 0.03800 -0.0469 0.0275 1.0000 12.500 1.2117 0.04714 0.04053 -0.0461 0.0265 1.0000 12.750 1.2210 0.04895 0.04241 -0.0457 0.0257 1.0000 13.000 1.2294 0.05089 0.04440 -0.0453 0.0248 1.0000 13.250 1.2372 0.05291 0.04646 -0.0450 0.0242 1.0000 13.500 1.2439 0.05506 0.04865 -0.0446 0.0235 1.0000 13.750 1.2486 0.05744 0.05107 -0.0442 0.0228 1.0000 14.000 1.2492 0.06026 0.05392 -0.0437 0.0223 1.0000 14.250 1.2587 0.06223 0.05596 -0.0436 0.0218 1.0000 14.500 1.2677 0.06425 0.05806 -0.0435 0.0213 1.0000 14.750 1.2755 0.06644 0.06032 -0.0435 0.0208 1.0000 15.000 1.2832 0.06864 0.06257 -0.0434 0.0203 1.0000 15.250 1.2908 0.07088 0.06486 -0.0435 0.0199 1.0000 15.500 1.2979 0.07320 0.06722 -0.0435 0.0196 1.0000 15.750 1.3051 0.07548 0.06953 -0.0436 0.0192 1.0000 16.000 1.3124 0.07765 0.07171 -0.0434 0.0188 1.0000 16.250 1.3215 0.07961 0.07372 -0.0432 0.0185 1.0000 16.500 1.3291 0.08198 0.07620 -0.0434 0.0183 1.0000 16.750 1.3371 0.08429 0.07859 -0.0436 0.0181 1.0000 17.000 1.3450 0.08663 0.08103 -0.0439 0.0178 1.0000 17.250 1.3523 0.08904 0.08354 -0.0442 0.0176 1.0000 17.500 1.3593 0.09150 0.08608 -0.0445 0.0174 1.0000 17.750 1.3661 0.09398 0.08866 -0.0449 0.0172 1.0000 18.000 1.3724 0.09656 0.09133 -0.0454 0.0170 1.0000 18.250 1.3780 0.09927 0.09414 -0.0460 0.0168 1.0000 18.500 1.3825 0.10214 0.09710 -0.0467 0.0166 1.0000 18.750 1.3858 0.10521 0.10026 -0.0476 0.0164 1.0000 19.000 1.3890 0.10831 0.10345 -0.0486 0.0162 1.0000