XFOIL Version 6.96 Calculated polar for: S1012 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 ------ -------- --------- --------- -------- -------- -------- -18.250 -0.9917 0.11846 0.11553 -0.0108 1.0000 0.0197 -18.000 -1.0230 0.10720 0.10409 -0.0180 1.0000 0.0196 -17.750 -1.0500 0.09740 0.09412 -0.0242 1.0000 0.0196 -17.500 -1.0740 0.08840 0.08494 -0.0300 1.0000 0.0196 -17.250 -1.0990 0.07974 0.07609 -0.0354 1.0000 0.0197 -17.000 -1.1188 0.07241 0.06859 -0.0398 1.0000 0.0197 -16.750 -1.1383 0.06563 0.06163 -0.0435 1.0000 0.0198 -16.500 -1.1521 0.06018 0.05603 -0.0462 1.0000 0.0200 -16.250 -1.1642 0.05534 0.05106 -0.0481 1.0000 0.0202 -16.000 -1.1721 0.05143 0.04703 -0.0493 1.0000 0.0205 -15.750 -1.1765 0.04822 0.04374 -0.0500 1.0000 0.0208 -15.500 -1.1780 0.04553 0.04097 -0.0502 1.0000 0.0211 -15.250 -1.1791 0.04302 0.03836 -0.0501 1.0000 0.0214 -15.000 -1.1780 0.04087 0.03612 -0.0497 1.0000 0.0219 -14.750 -1.1777 0.03870 0.03382 -0.0490 1.0000 0.0223 -14.500 -1.1745 0.03687 0.03188 -0.0482 1.0000 0.0228 -14.250 -1.1708 0.03514 0.03002 -0.0471 1.0000 0.0232 -14.000 -1.1655 0.03359 0.02834 -0.0460 1.0000 0.0236 -13.750 -1.1582 0.03226 0.02686 -0.0447 1.0000 0.0240 -13.500 -1.1591 0.03003 0.02453 -0.0428 1.0000 0.0247 -13.250 -1.1530 0.02862 0.02308 -0.0413 1.0000 0.0255 -13.000 -1.1432 0.02756 0.02196 -0.0399 1.0000 0.0260 -12.750 -1.1323 0.02658 0.02093 -0.0385 1.0000 0.0268 -12.500 -1.1198 0.02574 0.02002 -0.0371 1.0000 0.0277 -12.250 -1.1067 0.02490 0.01908 -0.0357 1.0000 0.0286 -12.000 -1.0924 0.02416 0.01822 -0.0344 1.0000 0.0292 -11.750 -1.0849 0.02273 0.01674 -0.0323 1.0000 0.0304 -11.500 -1.0717 0.02192 0.01592 -0.0307 1.0000 0.0315 -11.250 -1.0562 0.02129 0.01526 -0.0294 1.0000 0.0327 -11.000 -1.0397 0.02071 0.01462 -0.0281 1.0000 0.0342 -10.750 -1.0215 0.02028 0.01411 -0.0269 1.0000 0.0354 -10.500 -1.0116 0.01932 0.01314 -0.0247 1.0000 0.0373 -10.250 -0.9811 0.01870 0.01252 -0.0262 0.9844 0.0396 -10.000 -0.9488 0.01817 0.01192 -0.0278 0.9743 0.0420 -9.750 -0.9214 0.01736 0.01104 -0.0286 0.9643 0.0446 -9.500 -0.8967 0.01686 0.01052 -0.0286 0.9550 0.0472 -9.250 -0.8749 0.01656 0.01016 -0.0278 0.9462 0.0498 -9.000 -0.8543 0.01622 0.00972 -0.0267 0.9394 0.0521 -8.750 -0.8367 0.01564 0.00916 -0.0252 0.9328 0.0553 -8.500 -0.8156 0.01536 0.00882 -0.0242 0.9278 0.0582 -8.250 -0.7928 0.01514 0.00853 -0.0234 0.9235 0.0608 -8.000 -0.7735 0.01460 0.00799 -0.0221 0.9188 0.0648 -7.750 -0.7511 0.01432 0.00770 -0.0213 0.9151 0.0686 -7.500 -0.7274 0.01415 0.00745 -0.0206 0.9121 0.0719 -7.250 -0.7065 0.01368 0.00701 -0.0196 0.9091 0.0769 -7.000 -0.6824 0.01342 0.00675 -0.0192 0.9063 0.0817 -6.750 -0.6585 0.01316 0.00644 -0.0186 0.9036 0.0862 -6.500 -0.6358 0.01281 0.00613 -0.0179 0.9010 0.0926 -6.250 -0.6107 0.01265 0.00592 -0.0174 0.8988 0.0978 -6.000 -0.5886 0.01229 0.00562 -0.0165 0.8964 0.1060 -5.750 -0.5639 0.01209 0.00539 -0.0161 0.8942 0.1136 -5.500 -0.5394 0.01181 0.00517 -0.0156 0.8921 0.1236 -5.250 -0.5149 0.01154 0.00496 -0.0152 0.8900 0.1344 -5.000 -0.4902 0.01130 0.00477 -0.0148 0.8880 0.1475 -4.750 -0.4657 0.01105 0.00458 -0.0143 0.8861 0.1634 -4.500 -0.4413 0.01080 0.00441 -0.0138 0.8841 0.1827 -4.250 -0.4175 0.01052 0.00424 -0.0132 0.8822 0.2077 -4.000 -0.3941 0.01022 0.00409 -0.0126 0.8805 0.2421 -3.750 -0.3711 0.00989 0.00395 -0.0119 0.8789 0.2877 -3.500 -0.3490 0.00944 0.00379 -0.0112 0.8768 0.3509 -3.250 -0.3291 0.00889 0.00361 -0.0100 0.8744 0.4366 -3.000 -0.3113 0.00824 0.00343 -0.0084 0.8721 0.5426 -2.750 -0.2943 0.00770 0.00347 -0.0062 0.8697 0.6689 -2.500 -0.2690 0.00776 0.00366 -0.0054 0.8679 0.7240 -2.250 -0.2419 0.00786 0.00376 -0.0050 0.8662 0.7456 -2.000 -0.2148 0.00800 0.00389 -0.0046 0.8645 0.7611 -1.750 -0.1873 0.00813 0.00401 -0.0044 0.8625 0.7728 -1.500 -0.1598 0.00825 0.00412 -0.0042 0.8600 0.7833 -1.250 -0.1321 0.00832 0.00422 -0.0040 0.8568 0.7904 -1.000 -0.1053 0.00836 0.00422 -0.0034 0.8524 0.7983 -0.750 -0.0793 0.00834 0.00418 -0.0024 0.8456 0.8046 -0.500 -0.0535 0.00822 0.00404 -0.0013 0.8356 0.8106 -0.250 -0.0272 0.00819 0.00395 -0.0006 0.8279 0.8167 0.000 0.0000 0.00816 0.00396 0.0000 0.8217 0.8217 0.250 0.0272 0.00819 0.00396 0.0006 0.8168 0.8279 0.500 0.0535 0.00822 0.00404 0.0013 0.8106 0.8356 0.750 0.0793 0.00833 0.00418 0.0024 0.8045 0.8456 1.000 0.1054 0.00836 0.00422 0.0034 0.7984 0.8524 1.250 0.1321 0.00833 0.00422 0.0040 0.7905 0.8568 1.500 0.1598 0.00825 0.00412 0.0042 0.7833 0.8600 1.750 0.1872 0.00813 0.00401 0.0044 0.7728 0.8625 2.000 0.2147 0.00800 0.00388 0.0046 0.7609 0.8645 2.250 0.2419 0.00786 0.00376 0.0050 0.7457 0.8662 2.500 0.2690 0.00776 0.00366 0.0054 0.7240 0.8679 2.750 0.2944 0.00770 0.00347 0.0062 0.6701 0.8697 3.000 0.3113 0.00824 0.00343 0.0084 0.5431 0.8721 3.250 0.3290 0.00889 0.00361 0.0100 0.4363 0.8744 3.500 0.3490 0.00944 0.00379 0.0112 0.3502 0.8768 3.750 0.3711 0.00988 0.00395 0.0119 0.2878 0.8789 4.000 0.3941 0.01022 0.00409 0.0126 0.2423 0.8805 4.250 0.4175 0.01052 0.00424 0.0132 0.2078 0.8822 4.500 0.4413 0.01080 0.00441 0.0138 0.1827 0.8841 4.750 0.4657 0.01105 0.00458 0.0143 0.1633 0.8861 5.000 0.4902 0.01130 0.00477 0.0148 0.1474 0.8880 5.250 0.5149 0.01154 0.00496 0.0152 0.1344 0.8900 5.500 0.5394 0.01181 0.00517 0.0156 0.1235 0.8921 5.750 0.5639 0.01209 0.00539 0.0161 0.1136 0.8942 6.000 0.5885 0.01229 0.00562 0.0165 0.1059 0.8964 6.250 0.6108 0.01265 0.00592 0.0174 0.0978 0.8988 6.500 0.6358 0.01281 0.00613 0.0179 0.0926 0.9010 6.750 0.6586 0.01315 0.00644 0.0186 0.0863 0.9036 7.000 0.6823 0.01343 0.00675 0.0192 0.0817 0.9063 7.250 0.7065 0.01368 0.00700 0.0197 0.0768 0.9091 7.500 0.7275 0.01414 0.00745 0.0206 0.0719 0.9121 7.750 0.7511 0.01432 0.00770 0.0213 0.0686 0.9151 8.000 0.7735 0.01460 0.00799 0.0222 0.0649 0.9188 8.250 0.7926 0.01515 0.00854 0.0234 0.0609 0.9235 8.500 0.8157 0.01536 0.00883 0.0241 0.0582 0.9278 8.750 0.8367 0.01564 0.00916 0.0252 0.0554 0.9328 9.000 0.8544 0.01621 0.00972 0.0267 0.0521 0.9393 9.250 0.8753 0.01655 0.01014 0.0278 0.0497 0.9461 9.500 0.8970 0.01685 0.01051 0.0286 0.0472 0.9549 9.750 0.9217 0.01735 0.01103 0.0286 0.0445 0.9643 10.000 0.9490 0.01817 0.01191 0.0278 0.0420 0.9743 10.250 0.9813 0.01871 0.01252 0.0262 0.0396 0.9844 10.500 1.0117 0.01932 0.01315 0.0247 0.0374 1.0000 10.750 1.0214 0.02031 0.01414 0.0269 0.0354 1.0000 11.000 1.0398 0.02072 0.01463 0.0281 0.0342 1.0000 11.250 1.0563 0.02130 0.01527 0.0293 0.0328 1.0000 11.500 1.0719 0.02193 0.01593 0.0307 0.0316 1.0000 11.750 1.0852 0.02272 0.01674 0.0322 0.0305 1.0000 12.000 1.0925 0.02418 0.01823 0.0344 0.0293 1.0000 12.250 1.1071 0.02490 0.01908 0.0357 0.0285 1.0000 12.500 1.1203 0.02571 0.01999 0.0371 0.0276 1.0000 12.750 1.1322 0.02664 0.02099 0.0385 0.0269 1.0000 13.000 1.1440 0.02752 0.02192 0.0398 0.0260 1.0000 13.250 1.1533 0.02863 0.02308 0.0412 0.0254 1.0000 13.500 1.1592 0.03006 0.02456 0.0428 0.0247 1.0000 13.750 1.1592 0.03220 0.02680 0.0446 0.0240 1.0000 14.000 1.1663 0.03357 0.02831 0.0459 0.0237 1.0000 14.250 1.1712 0.03518 0.03006 0.0470 0.0233 1.0000 14.500 1.1754 0.03684 0.03185 0.0481 0.0227 1.0000 14.750 1.1781 0.03872 0.03384 0.0489 0.0223 1.0000 15.000 1.1799 0.04073 0.03596 0.0496 0.0218 1.0000 15.250 1.1796 0.04304 0.03838 0.0500 0.0215 1.0000 15.500 1.1804 0.04532 0.04073 0.0501 0.0210 1.0000 15.750 1.1785 0.04804 0.04354 0.0499 0.0207 1.0000 16.000 1.1740 0.05128 0.04687 0.0493 0.0204 1.0000 16.250 1.1650 0.05531 0.05103 0.0480 0.0202 1.0000 16.500 1.1531 0.06011 0.05595 0.0461 0.0199 1.0000 16.750 1.1383 0.06573 0.06174 0.0434 0.0198 1.0000 17.000 1.1193 0.07244 0.06862 0.0397 0.0197 1.0000 17.250 1.0978 0.08009 0.07645 0.0350 0.0196 1.0000 17.500 1.0764 0.08817 0.08471 0.0299 0.0196 1.0000 17.750 1.0516 0.09720 0.09391 0.0242 0.0196 1.0000 18.000 1.0200 0.10799 0.10489 0.0173 0.0196 1.0000 18.250 0.9916 0.11867 0.11574 0.0106 0.0197 1.0000