XFOIL Version 6.94 Calculated polar for: NACA 6412 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.300 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.6556 0.01070 0.00361 -0.1404 0.6905 0.3130 0.500 0.7046 0.01033 0.00365 -0.1390 0.6690 0.4647 1.000 0.7795 0.00950 0.00376 -0.1430 0.6476 0.9999 1.500 0.8315 0.00984 0.00387 -0.1420 0.6284 0.9999 2.000 0.8832 0.01019 0.00405 -0.1411 0.6101 0.9999 2.500 0.9349 0.01055 0.00428 -0.1402 0.5935 0.9999 3.000 0.9870 0.01095 0.00458 -0.1394 0.5789 0.9999 3.500 1.0392 0.01139 0.00490 -0.1387 0.5652 0.9999 4.000 1.0906 0.01179 0.00525 -0.1379 0.5519 0.9999 4.500 1.1418 0.01223 0.00569 -0.1371 0.5394 0.9999 5.000 1.1937 0.01273 0.00612 -0.1364 0.5273 0.9999 5.500 1.2434 0.01316 0.00661 -0.1353 0.5155 0.9999 6.000 1.2932 0.01367 0.00715 -0.1343 0.5031 0.9999 6.500 1.3429 0.01422 0.00767 -0.1333 0.4898 0.9999 7.000 1.3866 0.01463 0.00816 -0.1311 0.4738 0.9999 7.500 1.4259 0.01510 0.00863 -0.1280 0.4528 0.9999 8.000 1.4640 0.01560 0.00922 -0.1248 0.4339 0.9999 8.500 1.4980 0.01618 0.00987 -0.1210 0.4138 0.9999 9.000 1.5266 0.01683 0.01064 -0.1162 0.3906 0.9999 9.500 1.5518 0.01779 0.01164 -0.1111 0.3622 0.9999 10.000 1.5696 0.01925 0.01304 -0.1054 0.3239 0.9999 10.500 1.5780 0.02152 0.01514 -0.0990 0.2730 0.9999 11.000 1.5744 0.02493 0.01827 -0.0921 0.2147 0.9999 11.500 1.5626 0.02946 0.02250 -0.0854 0.1553 0.9999 12.000 1.5486 0.03477 0.02758 -0.0799 0.1105 0.9999 12.500 1.5367 0.04045 0.03320 -0.0756 0.0831 0.9999 13.000 1.5267 0.04652 0.03928 -0.0725 0.0674 0.9999 13.500 1.5184 0.05289 0.04576 -0.0703 0.0576 0.9999 14.000 1.5077 0.05989 0.05289 -0.0687 0.0508 0.9999 14.500 1.4962 0.06730 0.06041 -0.0677 0.0456 0.9999 15.000 1.4898 0.07431 0.06762 -0.0671 0.0414 0.9999 15.500 1.4808 0.08176 0.07517 -0.0669 0.0380 0.9999 16.000 1.4741 0.08892 0.08250 -0.0667 0.0352 0.9999 16.500 1.4725 0.09560 0.08933 -0.0669 0.0328 0.9999 17.000 1.4690 0.10216 0.09593 -0.0669 0.0308 0.9999 17.500 1.4721 0.10787 0.10185 -0.0668 0.0292 0.9999 18.000 1.4749 0.11398 0.10815 -0.0675 0.0276 0.9999 18.500 1.4782 0.11998 0.11426 -0.0686 0.0262 0.9999 19.000 1.4863 0.12418 0.11850 -0.0680 0.0247 0.9999 19.500 1.4855 0.13119 0.12583 -0.0700 0.0241 0.9999 20.000 1.4835 0.13842 0.13337 -0.0724 0.0233 0.9999 20.500 1.4793 0.14622 0.14144 -0.0755 0.0227 0.9999 21.000 1.4721 0.15485 0.15034 -0.0797 0.0220 0.9999 21.500 1.4639 0.16388 0.15961 -0.0847 0.0214 0.9999 22.000 1.4576 0.17260 0.16852 -0.0898 0.0208 0.9999 22.500 1.4425 0.18340 0.17957 -0.0965 0.0204 0.9999 23.000 1.4091 0.20021 0.19678 -0.1081 0.0203 0.9999 24.000 0.7916 0.25333 0.25084 -0.1014 0.0343 0.9999 24.500 0.7972 0.25980 0.25733 -0.1038 0.0319 0.9999 25.000 0.8112 0.26384 0.26141 -0.1043 0.0306 0.9999 25.500 0.8037 0.27538 0.27295 -0.1093 0.0284 0.9999 26.000 0.8086 0.28204 0.27965 -0.1117 0.0262 0.9999 26.500 0.8178 0.28703 0.28467 -0.1131 0.0251 0.9999 27.000 0.8156 0.29748 0.29513 -0.1170 0.0237 0.9999 27.500 0.8195 0.30453 0.30221 -0.1195 0.0215 0.9999 28.000 0.8262 0.30992 0.30764 -0.1213 0.0205 0.9999 28.500 0.8293 0.31823 0.31596 -0.1238 0.0200 0.9999 29.000 0.8292 0.32756 0.32532 -0.1272 0.0180 0.9999 29.500 0.8335 0.33359 0.33138 -0.1294 0.0168 0.9999 30.000 0.8409 0.33949 0.33732 -0.1308 0.0162 0.9999 30.500 0.8378 0.35011 0.34795 -0.1347 0.0150 0.9999 31.000 0.8406 0.35710 0.35497 -0.1371 0.0138 0.9999 31.500 0.8439 0.36300 0.36090 -0.1392 0.0131 0.9999 32.000 0.8474 0.37004 0.36797 -0.1412 0.0129 0.9999 32.500 0.8465 0.37985 0.37781 -0.1445 0.0117 0.9999 33.000 0.8483 0.38670 0.38469 -0.1469 0.0108 0.9999 33.500 0.8502 0.39263 0.39065 -0.1491 0.0102 0.9999 34.000 0.8526 0.39911 0.39716 -0.1510 0.0100 0.9999 34.500 0.8516 0.40873 0.40681 -0.1540 0.0096 0.9999 35.000 0.8522 0.41604 0.41415 -0.1564 0.0088 0.9999 35.500 0.8527 0.42267 0.42081 -0.1587 0.0082 0.9999 36.000 0.8530 0.42861 0.42679 -0.1610 0.0078 0.9999 37.000 0.8522 0.44319 0.44143 -0.1657 0.0074 0.9999 37.500 0.8517 0.45039 0.44866 -0.1680 0.0068 0.9999 38.000 0.8508 0.45676 0.45506 -0.1702 0.0063 0.9999 38.500 0.8497 0.46257 0.46091 -0.1725 0.0059 0.9999 39.000 0.8482 0.46767 0.46604 -0.1747 0.0056 0.9999 39.500 0.8464 0.47431 0.47271 -0.1769 0.0055 0.9999 40.000 0.8445 0.48175 0.48018 -0.1792 0.0054 0.9999 40.500 0.8426 0.48817 0.48664 -0.1813 0.0049 0.9999 41.000 0.8402 0.49380 0.49230 -0.1835 0.0045 0.9999 41.500 0.8374 0.49887 0.49741 -0.1856 0.0041 0.9999 42.000 0.8342 0.50334 0.50192 -0.1878 0.0039 0.9999 43.000 0.8277 0.51513 0.51376 -0.1920 0.0038 0.9999 43.500 0.8244 0.52080 0.51946 -0.1940 0.0035 0.9999 44.000 0.8205 0.52559 0.52429 -0.1960 0.0031 0.9999 44.500 0.8163 0.52988 0.52862 -0.1980 0.0028 0.9999 45.000 0.8116 0.53348 0.53225 -0.2001 0.0026 0.9999 46.000 0.8020 0.54195 0.54078 -0.2040 0.0025 0.9999 46.500 0.7974 0.54671 0.54558 -0.2058 0.0024 0.9999 47.000 0.7923 0.55058 0.54948 -0.2076 0.0022 0.9999 47.500 0.7868 0.55388 0.55281 -0.2095 0.0019 0.9999 48.000 0.7809 0.55652 0.55548 -0.2114 0.0017 0.9999 48.500 0.7747 0.55862 0.55762 -0.2133 0.0015 0.9999 50.000 0.7559 0.56680 0.56589 -0.2184 0.0014 0.9999 50.500 0.7494 0.56901 0.56813 -0.2200 0.0013 0.9999 51.000 0.7425 0.57072 0.56988 -0.2217 0.0011 0.9999 51.500 0.7353 0.57186 0.57104 -0.2234 0.0010 0.9999 52.000 0.7279 0.57240 0.57161 -0.2250 0.0008 0.9999 52.500 0.7200 0.57230 0.57155 -0.2267 0.0007 0.9999 54.000 0.6969 0.57427 0.57359 -0.2311 0.0007 0.9999 54.500 0.6889 0.57432 0.57368 -0.2325 0.0006 0.9999 55.000 0.6807 0.57384 0.57323 -0.2339 0.0005 0.9999 55.500 0.6723 0.57293 0.57234 -0.2353 0.0004 0.9999 56.000 0.6636 0.57151 0.57095 -0.2367 0.0003 0.9999 56.500 0.6547 0.56965 0.56912 -0.2381 0.0003 0.9999 57.000 0.6455 0.56716 0.56666 -0.2395 0.0002 0.9999 58.500 0.6184 0.56143 0.56100 -0.2432 0.0002 0.9999 59.000 0.6092 0.55902 0.55862 -0.2443 0.0002 0.9999 59.500 0.5999 0.55613 0.55576 -0.2454 0.0002 0.9999 60.000 0.5904 0.55293 0.55258 -0.2465 0.0001 0.9999