XFOIL Version 6.96 Calculated polar for: NACA 0024 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 -1.2119 0.08663 0.08133 -0.0434 1.0000 0.0959 -19.500 -1.2128 0.08353 0.07821 -0.0443 1.0000 0.0976 -19.250 -1.2140 0.08032 0.07494 -0.0453 1.0000 0.0994 -19.000 -1.2126 0.07743 0.07196 -0.0461 1.0000 0.1011 -18.750 -1.2135 0.07441 0.06890 -0.0468 1.0000 0.1029 -18.500 -1.2149 0.07138 0.06588 -0.0474 1.0000 0.1048 -18.250 -1.2158 0.06837 0.06283 -0.0481 1.0000 0.1067 -18.000 -1.2132 0.06574 0.06014 -0.0486 1.0000 0.1086 -17.750 -1.2100 0.06318 0.05749 -0.0491 1.0000 0.1104 -17.500 -1.2112 0.06034 0.05465 -0.0494 1.0000 0.1125 -17.250 -1.2116 0.05753 0.05183 -0.0498 1.0000 0.1146 -17.000 -1.2093 0.05501 0.04926 -0.0501 1.0000 0.1168 -16.750 -1.2034 0.05287 0.04706 -0.0503 1.0000 0.1191 -16.500 -1.2013 0.05044 0.04458 -0.0504 1.0000 0.1213 -16.250 -1.2007 0.04792 0.04207 -0.0504 1.0000 0.1237 -16.000 -1.1967 0.04574 0.03986 -0.0503 1.0000 0.1263 -15.750 -1.1895 0.04387 0.03793 -0.0503 1.0000 0.1288 -15.500 -1.1841 0.04191 0.03594 -0.0501 1.0000 0.1314 -15.250 -1.1819 0.03973 0.03376 -0.0497 1.0000 0.1341 -15.000 -1.1758 0.03792 0.03193 -0.0493 1.0000 0.1371 -14.750 -1.1656 0.03651 0.03046 -0.0490 1.0000 0.1400 -14.500 -1.1609 0.03472 0.02866 -0.0483 1.0000 0.1430 -14.250 -1.1557 0.03303 0.02698 -0.0475 1.0000 0.1461 -14.000 -1.1469 0.03170 0.02562 -0.0467 1.0000 0.1495 -13.750 -1.1361 0.03057 0.02443 -0.0459 1.0000 0.1526 -13.500 -1.1329 0.02905 0.02294 -0.0444 1.0000 0.1560 -13.250 -1.1266 0.02786 0.02175 -0.0429 1.0000 0.1595 -13.000 -1.1182 0.02695 0.02081 -0.0413 1.0000 0.1630 -12.750 -1.1148 0.02595 0.01980 -0.0390 1.0000 0.1664 -12.500 -1.1147 0.02496 0.01884 -0.0360 1.0000 0.1698 -12.250 -1.1143 0.02421 0.01808 -0.0327 1.0000 0.1733 -12.000 -1.1132 0.02368 0.01751 -0.0292 1.0000 0.1764 -11.750 -1.1217 0.02300 0.01683 -0.0244 1.0000 0.1795 -11.500 -1.1177 0.02225 0.01610 -0.0217 0.9991 0.1835 -11.250 -1.0870 0.02154 0.01538 -0.0236 0.9965 0.1890 -11.000 -1.0580 0.02071 0.01457 -0.0253 0.9937 0.1946 -10.750 -1.0270 0.01999 0.01387 -0.0273 0.9915 0.2007 -10.500 -0.9962 0.01939 0.01325 -0.0288 0.9882 0.2063 -10.250 -0.9686 0.01862 0.01254 -0.0300 0.9838 0.2127 -10.000 -0.9344 0.01811 0.01201 -0.0321 0.9809 0.2189 -9.750 -0.9019 0.01740 0.01135 -0.0341 0.9784 0.2258 -9.500 -0.8668 0.01685 0.01081 -0.0363 0.9760 0.2327 -9.250 -0.8425 0.01634 0.01031 -0.0362 0.9680 0.2387 -9.000 -0.8145 0.01578 0.00979 -0.0369 0.9622 0.2456 -8.750 -0.7893 0.01542 0.00940 -0.0368 0.9540 0.2516 -8.500 -0.7700 0.01489 0.00892 -0.0355 0.9443 0.2583 -8.250 -0.7508 0.01453 0.00855 -0.0341 0.9335 0.2647 -8.000 -0.7302 0.01419 0.00818 -0.0328 0.9235 0.2708 -7.750 -0.7135 0.01382 0.00784 -0.0309 0.9111 0.2776 -7.500 -0.6924 0.01354 0.00751 -0.0296 0.9007 0.2843 -7.250 -0.6737 0.01324 0.00722 -0.0280 0.8879 0.2909 -7.000 -0.6538 0.01295 0.00692 -0.0266 0.8766 0.2981 -6.750 -0.6313 0.01278 0.00669 -0.0255 0.8640 0.3047 -6.500 -0.6126 0.01248 0.00641 -0.0238 0.8519 0.3123 -6.250 -0.5916 0.01229 0.00619 -0.0225 0.8390 0.3198 -6.000 -0.5711 0.01212 0.00599 -0.0210 0.8266 0.3268 -5.750 -0.5521 0.01195 0.00580 -0.0193 0.8138 0.3345 -5.500 -0.5298 0.01185 0.00566 -0.0181 0.8009 0.3419 -5.250 -0.5089 0.01167 0.00546 -0.0167 0.7884 0.3499 -5.000 -0.4862 0.01154 0.00533 -0.0157 0.7753 0.3582 -4.750 -0.4628 0.01144 0.00518 -0.0148 0.7628 0.3659 -4.500 -0.4404 0.01129 0.00505 -0.0137 0.7497 0.3745 -4.250 -0.4156 0.01125 0.00493 -0.0130 0.7374 0.3824 -4.000 -0.3932 0.01110 0.00480 -0.0119 0.7244 0.3910 -3.750 -0.3689 0.01103 0.00470 -0.0111 0.7123 0.3997 -3.500 -0.3450 0.01095 0.00459 -0.0102 0.6994 0.4080 -3.250 -0.3212 0.01086 0.00451 -0.0094 0.6875 0.4170 -3.000 -0.2961 0.01084 0.00442 -0.0087 0.6750 0.4253 -2.750 -0.2726 0.01073 0.00435 -0.0078 0.6633 0.4345 -2.500 -0.2477 0.01072 0.00428 -0.0071 0.6510 0.4435 -2.250 -0.2233 0.01063 0.00422 -0.0063 0.6396 0.4525 -2.000 -0.1989 0.01061 0.00416 -0.0055 0.6276 0.4621 -1.750 -0.1737 0.01057 0.00412 -0.0049 0.6165 0.4711 -1.500 -0.1496 0.01054 0.00407 -0.0041 0.6048 0.4809 -1.250 -0.1238 0.01053 0.00404 -0.0036 0.5939 0.4901 -1.000 -0.1000 0.01048 0.00401 -0.0027 0.5826 0.5001 -0.750 -0.0743 0.01049 0.00400 -0.0021 0.5721 0.5098 -0.500 -0.0500 0.01045 0.00397 -0.0013 0.5609 0.5196 -0.250 -0.0248 0.01046 0.00397 -0.0007 0.5508 0.5300 0.000 0.0000 0.01045 0.00396 0.0000 0.5399 0.5399 0.250 0.0248 0.01046 0.00397 0.0007 0.5300 0.5508 0.500 0.0501 0.01045 0.00397 0.0013 0.5196 0.5609 0.750 0.0743 0.01049 0.00400 0.0021 0.5098 0.5721 1.000 0.1000 0.01048 0.00401 0.0027 0.5001 0.5826 1.250 0.1239 0.01053 0.00404 0.0036 0.4900 0.5939 1.500 0.1497 0.01054 0.00407 0.0041 0.4809 0.6048 1.750 0.1738 0.01057 0.00412 0.0049 0.4711 0.6165 2.000 0.1990 0.01061 0.00416 0.0055 0.4621 0.6276 2.250 0.2234 0.01063 0.00422 0.0063 0.4525 0.6396 2.500 0.2477 0.01072 0.00428 0.0071 0.4435 0.6510 2.750 0.2726 0.01073 0.00435 0.0078 0.4345 0.6633 3.000 0.2962 0.01084 0.00442 0.0087 0.4252 0.6750 3.250 0.3213 0.01086 0.00451 0.0093 0.4170 0.6875 3.500 0.3451 0.01095 0.00459 0.0102 0.4079 0.6994 3.750 0.3691 0.01103 0.00470 0.0110 0.3997 0.7123 4.000 0.3934 0.01110 0.00480 0.0118 0.3910 0.7244 4.250 0.4157 0.01125 0.00493 0.0129 0.3824 0.7374 4.500 0.4406 0.01129 0.00505 0.0136 0.3745 0.7498 4.750 0.4630 0.01144 0.00518 0.0147 0.3659 0.7628 5.000 0.4864 0.01154 0.00533 0.0157 0.3582 0.7753 5.250 0.5092 0.01167 0.00546 0.0167 0.3499 0.7884 5.500 0.5302 0.01185 0.00566 0.0181 0.3419 0.8009 5.750 0.5525 0.01195 0.00580 0.0192 0.3345 0.8138 6.000 0.5716 0.01213 0.00599 0.0209 0.3267 0.8265 6.250 0.5920 0.01229 0.00619 0.0224 0.3197 0.8390 6.500 0.6131 0.01247 0.00641 0.0237 0.3122 0.8519 6.750 0.6318 0.01278 0.00669 0.0254 0.3047 0.8639 7.000 0.6543 0.01295 0.00692 0.0264 0.2981 0.8765 7.250 0.6742 0.01324 0.00722 0.0279 0.2909 0.8879 7.500 0.6930 0.01354 0.00751 0.0295 0.2843 0.9007 7.750 0.7142 0.01382 0.00784 0.0308 0.2775 0.9110 8.000 0.7308 0.01419 0.00817 0.0327 0.2708 0.9234 8.250 0.7515 0.01453 0.00855 0.0340 0.2647 0.9335 8.500 0.7707 0.01489 0.00891 0.0354 0.2582 0.9443 8.750 0.7901 0.01541 0.00939 0.0366 0.2516 0.9539 9.000 0.8153 0.01577 0.00978 0.0368 0.2456 0.9622 9.250 0.8432 0.01633 0.01030 0.0361 0.2386 0.9681 9.500 0.8677 0.01684 0.01080 0.0362 0.2327 0.9760 9.750 0.9028 0.01739 0.01134 0.0339 0.2257 0.9784 10.000 0.9353 0.01809 0.01199 0.0319 0.2189 0.9809 10.250 0.9695 0.01861 0.01252 0.0299 0.2126 0.9839 10.500 0.9971 0.01937 0.01324 0.0287 0.2063 0.9883 10.750 1.0281 0.01997 0.01385 0.0271 0.2006 0.9916 11.000 1.0592 0.02069 0.01455 0.0251 0.1945 0.9938 11.250 1.0883 0.02151 0.01535 0.0234 0.1889 0.9966 11.500 1.1191 0.02222 0.01608 0.0215 0.1834 0.9992 11.750 1.1217 0.02296 0.01679 0.0244 0.1795 1.0000 12.000 1.1132 0.02364 0.01746 0.0293 0.1765 1.0000 12.250 1.1146 0.02416 0.01803 0.0327 0.1733 1.0000 12.500 1.1152 0.02492 0.01879 0.0360 0.1698 1.0000 12.750 1.1154 0.02590 0.01975 0.0389 0.1663 1.0000 13.000 1.1192 0.02690 0.02075 0.0412 0.1630 1.0000 13.250 1.1278 0.02781 0.02170 0.0428 0.1594 1.0000 13.500 1.1344 0.02900 0.02289 0.0442 0.1559 1.0000 13.750 1.1376 0.03053 0.02439 0.0457 0.1525 1.0000 14.000 1.1489 0.03164 0.02555 0.0464 0.1494 1.0000 14.250 1.1578 0.03297 0.02691 0.0472 0.1460 1.0000 14.500 1.1629 0.03467 0.02860 0.0480 0.1429 1.0000 14.750 1.1681 0.03643 0.03038 0.0486 0.1399 1.0000 15.000 1.1784 0.03785 0.03185 0.0490 0.1370 1.0000 15.250 1.1844 0.03967 0.03369 0.0493 0.1340 1.0000 15.500 1.1866 0.04186 0.03587 0.0497 0.1313 1.0000 15.750 1.1925 0.04377 0.03783 0.0499 0.1288 1.0000 16.000 1.1997 0.04566 0.03977 0.0499 0.1262 1.0000 16.250 1.2037 0.04784 0.04198 0.0500 0.1236 1.0000 16.500 1.2043 0.05037 0.04451 0.0500 0.1212 1.0000 16.750 1.2069 0.05277 0.04695 0.0499 0.1190 1.0000 17.000 1.2128 0.05490 0.04915 0.0496 0.1167 1.0000 17.250 1.2151 0.05745 0.05174 0.0493 0.1145 1.0000 17.500 1.2146 0.06026 0.05456 0.0490 0.1124 1.0000 17.750 1.2138 0.06307 0.05738 0.0486 0.1103 1.0000 18.000 1.2171 0.06564 0.06003 0.0481 0.1085 1.0000 18.250 1.2196 0.06828 0.06273 0.0476 0.1065 1.0000 18.500 1.2187 0.07130 0.06579 0.0469 0.1047 1.0000 18.750 1.2173 0.07433 0.06881 0.0463 0.1028 1.0000 19.000 1.2166 0.07734 0.07187 0.0456 0.1010 1.0000 19.250 1.2181 0.08023 0.07484 0.0447 0.0993 1.0000