XFOIL Version 6.96 Calculated polar for: GOE 383 AIRFOIL 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 ------ -------- --------- --------- -------- -------- -------- -12.750 -0.0985 0.11419 0.11105 -0.0663 0.7750 0.0499 -12.500 -0.6887 0.03824 0.03333 -0.1047 0.8654 0.0398 -12.250 -0.6886 0.03635 0.03119 -0.1025 0.8478 0.0397 -12.000 -0.6823 0.03460 0.02921 -0.1007 0.8307 0.0398 -11.750 -0.6723 0.03300 0.02739 -0.0992 0.8143 0.0399 -11.500 -0.6590 0.03159 0.02577 -0.0980 0.7983 0.0400 -11.250 -0.6435 0.03030 0.02431 -0.0969 0.7828 0.0401 -11.000 -0.6256 0.02916 0.02304 -0.0960 0.7687 0.0403 -10.750 -0.6066 0.02816 0.02187 -0.0952 0.7559 0.0405 -10.500 -0.5865 0.02717 0.02078 -0.0944 0.7441 0.0407 -10.250 -0.5659 0.02633 0.01979 -0.0937 0.7342 0.0409 -10.000 -0.5443 0.02551 0.01887 -0.0931 0.7254 0.0413 -9.750 -0.5227 0.02472 0.01793 -0.0924 0.7175 0.0417 -9.500 -0.5004 0.02390 0.01698 -0.0918 0.7108 0.0420 -9.250 -0.4773 0.02304 0.01600 -0.0913 0.7044 0.0422 -9.000 -0.4538 0.02227 0.01509 -0.0908 0.6980 0.0425 -8.750 -0.4299 0.02159 0.01426 -0.0902 0.6915 0.0428 -8.500 -0.4051 0.02091 0.01350 -0.0898 0.6860 0.0430 -8.250 -0.3801 0.02032 0.01280 -0.0894 0.6802 0.0433 -8.000 -0.3550 0.01983 0.01219 -0.0890 0.6747 0.0436 -7.750 -0.3295 0.01931 0.01156 -0.0886 0.6694 0.0439 -7.500 -0.3038 0.01840 0.01069 -0.0884 0.6652 0.0443 -7.250 -0.2780 0.01782 0.01012 -0.0882 0.6610 0.0448 -7.000 -0.2521 0.01736 0.00965 -0.0879 0.6569 0.0453 -6.750 -0.2262 0.01698 0.00922 -0.0875 0.6529 0.0458 -6.500 -0.2002 0.01664 0.00883 -0.0872 0.6488 0.0464 -6.250 -0.1737 0.01627 0.00845 -0.0870 0.6461 0.0471 -6.000 -0.1471 0.01595 0.00811 -0.0868 0.6429 0.0478 -5.750 -0.1201 0.01570 0.00781 -0.0865 0.6394 0.0485 -5.500 -0.0953 0.01515 0.00727 -0.0861 0.6359 0.0493 -5.250 -0.0696 0.01480 0.00692 -0.0857 0.6322 0.0501 -5.000 -0.0433 0.01457 0.00665 -0.0854 0.6282 0.0510 -4.750 -0.0165 0.01430 0.00638 -0.0852 0.6254 0.0520 -4.500 0.0105 0.01405 0.00613 -0.0850 0.6225 0.0531 -4.250 0.0367 0.01373 0.00581 -0.0847 0.6192 0.0543 -4.000 0.0631 0.01343 0.00554 -0.0844 0.6158 0.0559 -3.750 0.0903 0.01323 0.00531 -0.0842 0.6123 0.0577 -3.500 0.1173 0.01305 0.00509 -0.0840 0.6085 0.0600 -3.250 0.1444 0.01286 0.00491 -0.0839 0.6048 0.0633 -3.000 0.1714 0.01260 0.00470 -0.0837 0.6015 0.0679 -2.750 0.1982 0.01232 0.00450 -0.0834 0.5979 0.0789 -2.500 0.2234 0.01187 0.00434 -0.0831 0.5942 0.1409 -2.250 0.2497 0.01159 0.00421 -0.0829 0.5905 0.1820 -2.000 0.2757 0.01133 0.00415 -0.0827 0.5864 0.2441 -1.750 0.3024 0.01111 0.00412 -0.0825 0.5828 0.2960 -1.500 0.3292 0.01089 0.00406 -0.0824 0.5788 0.3373 -1.250 0.3557 0.01066 0.00400 -0.0822 0.5743 0.3841 -1.000 0.3812 0.01038 0.00394 -0.0818 0.5698 0.4542 -0.750 0.4065 0.01017 0.00393 -0.0813 0.5649 0.5330 -0.500 0.4314 0.00991 0.00398 -0.0807 0.5607 0.6088 -0.250 0.4575 0.00978 0.00402 -0.0802 0.5557 0.6649 0.000 0.4841 0.00972 0.00403 -0.0798 0.5505 0.7019 0.250 0.5106 0.00972 0.00406 -0.0794 0.5451 0.7338 0.500 0.5368 0.00966 0.00411 -0.0789 0.5395 0.7673 0.750 0.5629 0.00962 0.00415 -0.0783 0.5330 0.7951 1.000 0.5889 0.00965 0.00416 -0.0778 0.5266 0.8163 1.250 0.6152 0.00965 0.00424 -0.0773 0.5201 0.8374 1.500 0.6409 0.00968 0.00429 -0.0767 0.5128 0.8582 1.750 0.6659 0.00977 0.00435 -0.0760 0.5060 0.8781 2.000 0.6913 0.00981 0.00446 -0.0753 0.4984 0.8998 2.250 0.7158 0.00994 0.00455 -0.0744 0.4910 0.9227 2.500 0.7431 0.01008 0.00468 -0.0741 0.4842 0.9415 2.750 0.7742 0.01024 0.00481 -0.0748 0.4769 0.9554 3.000 0.8070 0.01048 0.00495 -0.0759 0.4694 0.9676 3.250 0.8425 0.01066 0.00511 -0.0776 0.4614 0.9783 3.500 0.8843 0.01094 0.00528 -0.0807 0.4530 0.9830 3.750 0.9257 0.01115 0.00546 -0.0837 0.4467 0.9884 4.000 0.9659 0.01137 0.00564 -0.0866 0.4407 0.9933 4.250 1.0085 0.01166 0.00583 -0.0900 0.4350 0.9975 4.500 1.0414 0.01184 0.00600 -0.0914 0.4305 1.0000 4.750 1.0546 0.01194 0.00609 -0.0889 0.4265 1.0000 5.000 1.0680 0.01209 0.00621 -0.0863 0.4224 1.0000 5.250 1.0818 0.01229 0.00636 -0.0838 0.4183 1.0000 5.500 1.0977 0.01251 0.00654 -0.0817 0.4145 1.0000 5.750 1.1151 0.01265 0.00670 -0.0799 0.4113 1.0000 6.000 1.1332 0.01282 0.00688 -0.0782 0.4077 1.0000 6.250 1.1500 0.01304 0.00708 -0.0764 0.4038 1.0000 6.500 1.1668 0.01332 0.00731 -0.0746 0.3999 1.0000 6.750 1.1861 0.01361 0.00757 -0.0733 0.3961 1.0000 7.000 1.2055 0.01382 0.00782 -0.0720 0.3929 1.0000 7.250 1.2254 0.01407 0.00810 -0.0709 0.3894 1.0000 7.500 1.2449 0.01437 0.00839 -0.0698 0.3857 1.0000 7.750 1.2642 0.01474 0.00872 -0.0687 0.3818 1.0000 8.000 1.2842 0.01510 0.00908 -0.0678 0.3780 1.0000 8.250 1.3035 0.01540 0.00944 -0.0668 0.3741 1.0000 8.500 1.3221 0.01576 0.00982 -0.0657 0.3696 1.0000 8.750 1.3394 0.01622 0.01024 -0.0645 0.3649 1.0000 9.000 1.3571 0.01670 0.01072 -0.0634 0.3603 1.0000 9.250 1.3756 0.01711 0.01120 -0.0625 0.3559 1.0000 9.500 1.3929 0.01761 0.01171 -0.0615 0.3511 1.0000 9.750 1.4083 0.01823 0.01231 -0.0603 0.3464 1.0000 10.000 1.4252 0.01881 0.01293 -0.0594 0.3419 1.0000 10.250 1.4421 0.01940 0.01356 -0.0585 0.3366 1.0000 10.500 1.4553 0.02020 0.01435 -0.0573 0.3308 1.0000 10.750 1.4692 0.02101 0.01519 -0.0562 0.3248 1.0000 11.000 1.4823 0.02190 0.01610 -0.0552 0.3174 1.0000 11.250 1.4915 0.02307 0.01724 -0.0539 0.3102 1.0000 11.500 1.5036 0.02411 0.01833 -0.0529 0.3020 1.0000 11.750 1.5106 0.02553 0.01972 -0.0516 0.2942 1.0000 12.000 1.5203 0.02682 0.02104 -0.0507 0.2860 1.0000 12.250 1.5253 0.02848 0.02268 -0.0494 0.2787 1.0000 12.500 1.5339 0.02993 0.02415 -0.0485 0.2714 1.0000 12.750 1.5365 0.03189 0.02608 -0.0473 0.2647 1.0000 13.000 1.5453 0.03342 0.02766 -0.0466 0.2585 1.0000 13.250 1.5484 0.03542 0.02966 -0.0456 0.2525 1.0000 13.500 1.5541 0.03723 0.03149 -0.0448 0.2472 1.0000 13.750 1.5593 0.03914 0.03343 -0.0441 0.2418 1.0000 14.000 1.5603 0.04143 0.03571 -0.0432 0.2366 1.0000 14.250 1.5667 0.04329 0.03761 -0.0426 0.2319 1.0000 14.500 1.5702 0.04542 0.03977 -0.0420 0.2269 1.0000 14.750 1.5707 0.04783 0.04217 -0.0413 0.2223 1.0000 15.000 1.5761 0.04985 0.04425 -0.0408 0.2184 1.0000 15.250 1.5810 0.05193 0.04638 -0.0404 0.2143 1.0000 15.500 1.5814 0.05445 0.04891 -0.0399 0.2101 1.0000 15.750 1.5832 0.05684 0.05133 -0.0395 0.2063 1.0000 16.000 1.5882 0.05899 0.05355 -0.0392 0.2023 1.0000 16.250 1.5887 0.06161 0.05621 -0.0389 0.1982 1.0000 16.500 1.5865 0.06450 0.05910 -0.0385 0.1942 1.0000 16.750 1.5909 0.06679 0.06148 -0.0384 0.1904 1.0000 17.000 1.5916 0.06947 0.06420 -0.0383 0.1859 1.0000 17.250 1.5849 0.07300 0.06774 -0.0381 0.1811 1.0000 17.500 1.5875 0.07558 0.07040 -0.0382 0.1760 1.0000 17.750 1.5804 0.07927 0.07412 -0.0382 0.1704 1.0000 18.000 1.5763 0.08265 0.07755 -0.0383 0.1640 1.0000 18.250 1.5652 0.08692 0.08183 -0.0386 0.1567 1.0000 18.500 1.5534 0.09137 0.08630 -0.0389 0.1468 1.0000 18.750 1.5343 0.09676 0.09168 -0.0395 0.1333 1.0000 19.000 1.5023 0.10390 0.09874 -0.0404 0.1124 1.0000 19.250 1.4611 0.11244 0.10718 -0.0418 0.0915 1.0000