XFOIL Version 6.96 Calculated polar for: ONERA HOR20 AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -14.500 -1.0092 0.05586 0.05017 -0.0680 1.0000 0.1041 -14.250 -1.0492 0.04806 0.04202 -0.0747 1.0000 0.1052 -14.000 -1.0434 0.04570 0.03965 -0.0758 1.0000 0.1068 -13.750 -1.0210 0.04533 0.03942 -0.0753 1.0000 0.1087 -13.500 -1.0204 0.04251 0.03653 -0.0775 1.0000 0.1104 -13.250 -1.0312 0.03903 0.03287 -0.0801 1.0000 0.1119 -13.000 -1.0410 0.03648 0.03007 -0.0804 1.0000 0.1134 -12.750 -1.0334 0.03474 0.02822 -0.0802 1.0000 0.1152 -12.500 -1.0113 0.03408 0.02770 -0.0798 1.0000 0.1170 -12.250 -0.9949 0.03315 0.02678 -0.0795 1.0000 0.1190 -12.000 -0.9827 0.03192 0.02544 -0.0791 1.0000 0.1213 -11.750 -0.9741 0.03057 0.02384 -0.0784 1.0000 0.1235 -11.500 -0.9560 0.02981 0.02323 -0.0774 1.0000 0.1256 -11.250 -0.9435 0.02939 0.02290 -0.0757 1.0000 0.1277 -11.000 -0.9415 0.02897 0.02248 -0.0727 0.9996 0.1297 -10.750 -0.9017 0.02773 0.02092 -0.0770 0.9919 0.1337 -10.500 -0.8600 0.02695 0.02034 -0.0800 0.9848 0.1370 -10.250 -0.8177 0.02619 0.01954 -0.0835 0.9774 0.1410 -10.000 -0.7803 0.02513 0.01826 -0.0865 0.9667 0.1450 -9.750 -0.7411 0.02447 0.01774 -0.0889 0.9568 0.1485 -9.500 -0.7076 0.02387 0.01708 -0.0903 0.9429 0.1523 -9.250 -0.6817 0.02321 0.01617 -0.0903 0.9254 0.1560 -9.000 -0.6569 0.02262 0.01569 -0.0897 0.9085 0.1592 -8.750 -0.6325 0.02226 0.01532 -0.0889 0.8924 0.1628 -8.500 -0.6089 0.02183 0.01469 -0.0882 0.8775 0.1672 -8.250 -0.5849 0.02133 0.01418 -0.0874 0.8630 0.1711 -8.000 -0.5591 0.02107 0.01392 -0.0869 0.8485 0.1754 -7.750 -0.5340 0.02074 0.01339 -0.0862 0.8360 0.1803 -7.500 -0.5077 0.02030 0.01297 -0.0859 0.8218 0.1847 -7.250 -0.4812 0.02012 0.01274 -0.0854 0.8098 0.1895 -7.000 -0.4539 0.01985 0.01228 -0.0853 0.7967 0.1951 -6.750 -0.4270 0.01955 0.01201 -0.0849 0.7856 0.1999 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0.3220 -1.750 0.1540 0.01681 0.00837 -0.0852 0.5961 0.3288 -1.500 0.1839 0.01687 0.00841 -0.0853 0.5893 0.3363 -1.250 0.2139 0.01682 0.00832 -0.0855 0.5817 0.3440 -1.000 0.2434 0.01677 0.00830 -0.0855 0.5749 0.3509 -0.750 0.2732 0.01688 0.00833 -0.0856 0.5685 0.3591 -0.500 0.3030 0.01682 0.00830 -0.0858 0.5612 0.3669 -0.250 0.3326 0.01682 0.00833 -0.0858 0.5544 0.3743 0.000 0.3625 0.01694 0.00832 -0.0859 0.5484 0.3832 0.250 0.3920 0.01693 0.00840 -0.0860 0.5418 0.3913 0.500 0.4216 0.01700 0.00850 -0.0861 0.5350 0.4002 0.750 0.4515 0.01706 0.00847 -0.0862 0.5291 0.4102 1.000 0.4807 0.01721 0.00864 -0.0862 0.5233 0.4189 1.250 0.5103 0.01731 0.00876 -0.0863 0.5167 0.4300 1.500 0.5395 0.01735 0.00885 -0.0862 0.5107 0.4392 1.750 0.5691 0.01752 0.00894 -0.0863 0.5052 0.4502 2.000 0.5982 0.01765 0.00911 -0.0863 0.4993 0.4601 2.250 0.6270 0.01776 0.00929 -0.0862 0.4929 0.4703 2.500 0.6564 0.01786 0.00934 -0.0863 0.4872 0.4808 2.750 0.6857 0.01807 0.00950 -0.0863 0.4819 0.4900 3.000 0.7143 0.01822 0.00969 -0.0863 0.4758 0.5007 3.250 0.7426 0.01823 0.00981 -0.0861 0.4696 0.5096 3.500 0.7718 0.01835 0.00987 -0.0861 0.4643 0.5198 3.750 0.8008 0.01853 0.01000 -0.0862 0.4592 0.5286 4.000 0.8284 0.01860 0.01020 -0.0860 0.4529 0.5381 4.250 0.8570 0.01867 0.01026 -0.0859 0.4468 0.5480 4.500 0.8856 0.01872 0.01030 -0.0858 0.4416 0.5573 4.750 0.9137 0.01892 0.01052 -0.0857 0.4359 0.5672 5.000 0.9409 0.01896 0.01067 -0.0855 0.4295 0.5762 5.250 0.9690 0.01903 0.01074 -0.0854 0.4238 0.5870 5.500 0.9977 0.01923 0.01088 -0.0853 0.4185 0.5979 5.750 1.0236 0.01934 0.01116 -0.0849 0.4122 0.6097 6.000 1.0507 0.01942 0.01130 -0.0846 0.4062 0.6218 6.250 1.0786 0.01955 0.01140 -0.0845 0.4010 0.6364 6.500 1.1044 0.01976 0.01175 -0.0841 0.3954 0.6538 6.750 1.1296 0.01986 0.01203 -0.0835 0.3893 0.6781 7.000 1.1549 0.01988 0.01218 -0.0828 0.3838 0.7150 7.250 1.1768 0.01979 0.01236 -0.0812 0.3786 0.8245 7.500 1.2023 0.01986 0.01263 -0.0808 0.3722 1.0000 7.750 1.2289 0.02014 0.01283 -0.0805 0.3663 1.0000 8.000 1.2569 0.02050 0.01303 -0.0805 0.3611 1.0000 8.250 1.2800 0.02090 0.01351 -0.0798 0.3552 1.0000 8.500 1.3043 0.02124 0.01385 -0.0793 0.3494 1.0000 8.750 1.3301 0.02158 0.01409 -0.0789 0.3443 1.0000 9.000 1.3537 0.02207 0.01457 -0.0782 0.3389 1.0000 9.250 1.3750 0.02246 0.01502 -0.0773 0.3329 1.0000 9.500 1.3983 0.02282 0.01532 -0.0765 0.3275 1.0000 9.750 1.4222 0.02333 0.01575 -0.0760 0.3222 1.0000 10.000 1.4400 0.02383 0.01636 -0.0745 0.3165 1.0000 10.250 1.4603 0.02426 0.01679 -0.0734 0.3112 1.0000 10.500 1.4859 0.02478 0.01714 -0.0731 0.3062 1.0000 10.750 1.4986 0.02541 0.01793 -0.0710 0.3010 1.0000 11.000 1.5143 0.02596 0.01853 -0.0694 0.2958 1.0000 11.250 1.5337 0.02648 0.01897 -0.0682 0.2910 1.0000 11.500 1.5469 0.02721 0.01973 -0.0663 0.2862 1.0000 11.750 1.5532 0.02799 0.02061 -0.0634 0.2812 1.0000 12.000 1.5648 0.02871 0.02133 -0.0615 0.2765 1.0000 12.250 1.5848 0.02939 0.02189 -0.0606 0.2717 1.0000 12.500 1.5856 0.03061 0.02328 -0.0579 0.2671 1.0000 12.750 1.5933 0.03168 0.02440 -0.0560 0.2623 1.0000 13.000 1.6084 0.03252 0.02516 -0.0549 0.2579 1.0000 13.250 1.6166 0.03381 0.02651 -0.0534 0.2535 1.0000 13.500 1.6183 0.03541 0.02824 -0.0516 0.2489 1.0000 13.750 1.6261 0.03674 0.02958 -0.0504 0.2445 1.0000 14.000 1.6461 0.03746 0.03015 -0.0497 0.2400 1.0000 14.250 1.6396 0.03984 0.03276 -0.0481 0.2361 1.0000 14.500 1.6412 0.04179 0.03479 -0.0471 0.2317 1.0000 14.750 1.6497 0.04323 0.03620 -0.0462 0.2276 1.0000 15.000 1.6576 0.04483 0.03779 -0.0453 0.2234 1.0000 15.250 1.6493 0.04779 0.04094 -0.0446 0.2191 1.0000 15.500 1.6502 0.05000 0.04319 -0.0440 0.2149 1.0000 15.750 1.6668 0.05080 0.04383 -0.0432 0.2106 1.0000 16.000 1.6524 0.05463 0.04789 -0.0429 0.2069 1.0000 16.250 1.6469 0.05775 0.05112 -0.0428 0.2030 1.0000 16.500 1.6505 0.05994 0.05332 -0.0425 0.1993 1.0000 16.750 1.6611 0.06138 0.05469 -0.0419 0.1956 1.0000 17.000 1.6441 0.06609 0.05962 -0.0425 0.1919 1.0000 17.250 1.6394 0.06948 0.06309 -0.0429 0.1880 1.0000 17.500 1.6473 0.07129 0.06484 -0.0427 0.1846 1.0000 17.750 1.6458 0.07435 0.06796 -0.0429 0.1813 1.0000 18.000 1.6303 0.07935 0.07315 -0.0439 0.1779 1.0000 18.250 1.6271 0.08277 0.07663 -0.0445 0.1745 1.0000 18.500 1.6393 0.08404 0.07782 -0.0443 0.1714 1.0000 18.750 1.6314 0.08814 0.08203 -0.0451 0.1684 1.0000 19.000 1.6120 0.09400 0.08808 -0.0469 0.1650 1.0000 19.250 1.6092 0.09750 0.09163 -0.0478 0.1618 1.0000