XFOIL Version 6.96 Calculated polar for: NACA 2414 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -17.500 -1.0317 0.08950 0.08559 -0.0404 1.0000 0.0206 -17.250 -1.0560 0.08197 0.07794 -0.0445 1.0000 0.0206 -17.000 -1.0803 0.07457 0.07041 -0.0486 1.0000 0.0207 -16.750 -1.1030 0.06746 0.06316 -0.0526 1.0000 0.0208 -16.500 -1.1230 0.06070 0.05626 -0.0566 1.0000 0.0208 -16.250 -1.1389 0.05453 0.04994 -0.0604 1.0000 0.0209 -16.000 -1.1506 0.04906 0.04433 -0.0639 1.0000 0.0211 -15.750 -1.1582 0.04437 0.03950 -0.0669 1.0000 0.0212 -15.500 -1.1625 0.04041 0.03541 -0.0693 1.0000 0.0214 -15.250 -1.1638 0.03714 0.03200 -0.0709 1.0000 0.0217 -15.000 -1.1631 0.03444 0.02918 -0.0718 1.0000 0.0219 -14.750 -1.1605 0.03224 0.02685 -0.0721 1.0000 0.0221 -14.500 -1.1584 0.03028 0.02479 -0.0716 1.0000 0.0224 -14.250 -1.1559 0.02861 0.02305 -0.0705 1.0000 0.0227 -14.000 -1.1517 0.02730 0.02167 -0.0688 1.0000 0.0230 -13.750 -1.1470 0.02625 0.02055 -0.0666 1.0000 0.0233 -13.500 -1.1431 0.02539 0.01964 -0.0636 1.0000 0.0237 -13.250 -1.1367 0.02464 0.01882 -0.0608 1.0000 0.0241 -13.000 -1.1282 0.02394 0.01805 -0.0582 1.0000 0.0246 -12.750 -1.1186 0.02329 0.01733 -0.0556 1.0000 0.0251 -12.500 -1.1084 0.02269 0.01665 -0.0530 1.0000 0.0256 -12.250 -1.0987 0.02205 0.01596 -0.0502 1.0000 0.0261 -12.000 -1.0889 0.02142 0.01529 -0.0475 1.0000 0.0266 -11.750 -1.0701 0.02078 0.01461 -0.0465 0.9991 0.0272 -11.500 -1.0420 0.02013 0.01390 -0.0473 0.9971 0.0281 -11.250 -1.0129 0.01952 0.01323 -0.0481 0.9951 0.0290 -11.000 -0.9829 0.01896 0.01259 -0.0491 0.9934 0.0298 -10.750 -0.9560 0.01830 0.01191 -0.0496 0.9905 0.0308 -10.500 -0.9269 0.01776 0.01135 -0.0503 0.9878 0.0320 -10.250 -0.8964 0.01728 0.01081 -0.0513 0.9856 0.0334 -10.000 -0.8650 0.01677 0.01026 -0.0524 0.9837 0.0347 -9.750 -0.8329 0.01625 0.00972 -0.0537 0.9822 0.0362 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0.1151 -4.750 -0.2739 0.01015 0.00340 -0.0551 0.8466 0.1248 -4.500 -0.2467 0.00998 0.00322 -0.0549 0.8358 0.1355 -4.250 -0.2197 0.00982 0.00306 -0.0547 0.8237 0.1479 -4.000 -0.1926 0.00965 0.00291 -0.0544 0.8117 0.1614 -3.750 -0.1655 0.00951 0.00277 -0.0542 0.7996 0.1756 -3.500 -0.1385 0.00937 0.00264 -0.0539 0.7863 0.1903 -3.250 -0.1113 0.00925 0.00253 -0.0537 0.7730 0.2061 -3.000 -0.0841 0.00913 0.00242 -0.0534 0.7598 0.2232 -2.750 -0.0571 0.00903 0.00233 -0.0532 0.7460 0.2411 -2.500 -0.0301 0.00894 0.00224 -0.0529 0.7316 0.2601 -2.250 -0.0029 0.00885 0.00217 -0.0527 0.7170 0.2796 -2.000 0.0242 0.00877 0.00210 -0.0525 0.7021 0.2999 -1.750 0.0512 0.00869 0.00204 -0.0522 0.6876 0.3217 -1.500 0.0782 0.00863 0.00200 -0.0520 0.6727 0.3459 -1.000 0.1318 0.00850 0.00192 -0.0514 0.6432 0.3987 -0.750 0.1586 0.00841 0.00190 -0.0512 0.6287 0.4310 -0.500 0.1852 0.00832 0.00190 -0.0509 0.6143 0.4689 -0.250 0.2118 0.00825 0.00190 -0.0505 0.6006 0.5080 0.000 0.2382 0.00820 0.00192 -0.0502 0.5866 0.5457 0.250 0.2647 0.00816 0.00194 -0.0498 0.5730 0.5817 0.500 0.2913 0.00812 0.00198 -0.0495 0.5595 0.6171 0.750 0.3178 0.00809 0.00202 -0.0491 0.5465 0.6518 1.000 0.3441 0.00809 0.00208 -0.0487 0.5339 0.6852 1.500 0.3966 0.00808 0.00221 -0.0477 0.5092 0.7530 1.750 0.4225 0.00809 0.00229 -0.0471 0.4981 0.7861 2.000 0.4481 0.00812 0.00239 -0.0465 0.4862 0.8187 2.250 0.4740 0.00816 0.00249 -0.0458 0.4750 0.8504 2.500 0.4995 0.00823 0.00260 -0.0451 0.4636 0.8801 2.750 0.5259 0.00835 0.00272 -0.0445 0.4511 0.9058 3.000 0.5542 0.00847 0.00284 -0.0444 0.4383 0.9276 3.250 0.5843 0.00862 0.00296 -0.0447 0.4251 0.9449 3.500 0.6159 0.00880 0.00309 -0.0455 0.4111 0.9588 3.750 0.6485 0.00899 0.00323 -0.0465 0.3956 0.9709 4.000 0.6836 0.00921 0.00338 -0.0480 0.3786 0.9826 4.250 0.7211 0.00945 0.00354 -0.0502 0.3589 0.9899 4.500 0.7552 0.00971 0.00371 -0.0517 0.3382 0.9946 4.750 0.7891 0.00998 0.00389 -0.0532 0.3175 0.9983 5.000 0.8155 0.01027 0.00407 -0.0530 0.2977 1.0000 5.250 0.8361 0.01053 0.00425 -0.0517 0.2790 1.0000 5.500 0.8568 0.01082 0.00445 -0.0503 0.2603 1.0000 5.750 0.8774 0.01111 0.00467 -0.0490 0.2423 1.0000 6.000 0.8980 0.01143 0.00490 -0.0476 0.2246 1.0000 6.250 0.9188 0.01177 0.00516 -0.0464 0.2070 1.0000 6.500 0.9397 0.01214 0.00543 -0.0451 0.1893 1.0000 6.750 0.9605 0.01253 0.00573 -0.0439 0.1720 1.0000 7.000 0.9815 0.01293 0.00605 -0.0427 0.1562 1.0000 7.250 1.0026 0.01333 0.00638 -0.0416 0.1416 1.0000 7.500 1.0237 0.01375 0.00673 -0.0405 0.1285 1.0000 7.750 1.0449 0.01415 0.00708 -0.0395 0.1170 1.0000 8.000 1.0660 0.01456 0.00745 -0.0384 0.1069 1.0000 8.250 1.0867 0.01499 0.00784 -0.0373 0.0977 1.0000 8.500 1.1069 0.01544 0.00825 -0.0361 0.0895 1.0000 8.750 1.1268 0.01590 0.00868 -0.0349 0.0821 1.0000 9.000 1.1467 0.01633 0.00911 -0.0337 0.0759 1.0000 9.250 1.1655 0.01682 0.00957 -0.0323 0.0703 1.0000 9.500 1.1833 0.01729 0.01004 -0.0308 0.0654 1.0000 9.750 1.1999 0.01778 0.01053 -0.0290 0.0613 1.0000 10.000 1.2162 0.01830 0.01106 -0.0273 0.0572 1.0000 10.250 1.2324 0.01886 0.01162 -0.0256 0.0539 1.0000 10.500 1.2485 0.01943 0.01221 -0.0240 0.0508 1.0000 10.750 1.2634 0.02008 0.01287 -0.0223 0.0481 1.0000 11.000 1.2791 0.02070 0.01352 -0.0208 0.0457 1.0000 11.250 1.2934 0.02142 0.01427 -0.0192 0.0434 1.0000 11.500 1.3074 0.02218 0.01506 -0.0177 0.0415 1.0000 11.750 1.3214 0.02295 0.01587 -0.0162 0.0396 1.0000 12.000 1.3340 0.02385 0.01679 -0.0147 0.0379 1.0000 12.250 1.3459 0.02481 0.01780 -0.0132 0.0365 1.0000 12.500 1.3585 0.02577 0.01882 -0.0119 0.0352 1.0000 12.750 1.3697 0.02684 0.01994 -0.0106 0.0339 1.0000 13.000 1.3794 0.02808 0.02122 -0.0093 0.0326 1.0000 13.250 1.3889 0.02938 0.02258 -0.0082 0.0316 1.0000 13.500 1.3986 0.03071 0.02398 -0.0071 0.0306 1.0000 13.750 1.4071 0.03219 0.02552 -0.0062 0.0296 1.0000 14.000 1.4141 0.03385 0.02724 -0.0053 0.0287 1.0000 14.250 1.4190 0.03576 0.02921 -0.0045 0.0279 1.0000 14.500 1.4251 0.03764 0.03117 -0.0039 0.0273 1.0000 14.750 1.4305 0.03965 0.03327 -0.0034 0.0266 1.0000 15.000 1.4346 0.04184 0.03554 -0.0031 0.0259 1.0000 15.250 1.4373 0.04424 0.03803 -0.0028 0.0253 1.0000 15.500 1.4386 0.04689 0.04075 -0.0028 0.0248 1.0000 15.750 1.4380 0.04983 0.04377 -0.0029 0.0243 1.0000 16.000 1.4356 0.05307 0.04709 -0.0032 0.0239 1.0000 16.250 1.4355 0.05613 0.05026 -0.0036 0.0234 1.0000 16.500 1.4340 0.05943 0.05367 -0.0042 0.0230 1.0000 16.750 1.4315 0.06292 0.05726 -0.0049 0.0226 1.0000 17.000 1.4277 0.06665 0.06109 -0.0057 0.0221 1.0000 17.250 1.4224 0.07065 0.06518 -0.0067 0.0218 1.0000 17.500 1.4159 0.07491 0.06954 -0.0079 0.0214 1.0000 17.750 1.4079 0.07942 0.07414 -0.0093 0.0211 1.0000 18.000 1.3984 0.08422 0.07904 -0.0109 0.0209 1.0000 18.250 1.3876 0.08932 0.08423 -0.0126 0.0206 1.0000