XFOIL Version 6.94 Calculated polar for: GOE 79 (PFALZ 11) AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.450 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.5740 0.01963 0.01408 -0.1030 0.5953 0.0312 0.500 0.6365 0.01765 0.01170 -0.1036 0.5728 0.0344 1.000 0.6960 0.01603 0.00976 -0.1040 0.5482 0.0383 1.500 0.7544 0.01502 0.00839 -0.1041 0.5195 0.0453 2.000 0.8116 0.01388 0.00700 -0.1042 0.4839 0.0512 2.500 0.8670 0.01336 0.00610 -0.1040 0.4259 0.0660 3.500 0.9542 0.00420 -0.00358 -0.0985 0.3281 0.0602 4.000 1.0072 0.00408 -0.00378 -0.0977 0.3077 0.0472 4.500 1.0595 0.00412 -0.00380 -0.0972 0.2895 0.0481 5.000 1.1117 0.00419 -0.00380 -0.0967 0.2617 0.0544 5.500 1.1601 0.00368 -0.00301 -0.0957 0.2364 1.0000 6.000 1.2079 0.00413 -0.00296 -0.0947 0.1900 1.0000 6.500 1.2474 0.00528 -0.00245 -0.0928 0.0930 1.0000 7.000 1.2901 0.00621 -0.00168 -0.0910 0.0706 1.0000 7.500 1.3356 0.00684 -0.00109 -0.0897 0.0570 1.0000 8.000 1.3755 0.00793 -0.00021 -0.0877 0.0296 1.0000 8.500 1.4070 0.00967 0.00142 -0.0844 0.0026 1.0000 9.000 1.4448 0.01069 0.00256 -0.0820 0.0023 1.0000 9.500 1.4785 0.01187 0.00389 -0.0790 0.0022 1.0000 10.000 1.5049 0.01325 0.00545 -0.0751 0.0022 1.0000 10.500 1.5183 0.01488 0.00729 -0.0694 0.0022 1.0000 11.000 1.5241 0.01717 0.00983 -0.0639 0.0022 1.0000 11.500 1.5237 0.02053 0.01346 -0.0595 0.0022 1.0000 12.000 1.5181 0.02537 0.01858 -0.0561 0.0022 1.0000 12.500 1.5064 0.03204 0.02554 -0.0538 0.0023 1.0000 13.000 1.4883 0.04064 0.03442 -0.0525 0.0023 1.0000 13.500 1.4633 0.05097 0.04505 -0.0518 0.0023 1.0000 14.000 1.4322 0.06267 0.05703 -0.0519 0.0023 1.0000 14.500 1.3981 0.07507 0.06972 -0.0529 0.0024 1.0000 15.000 1.3627 0.08761 0.08254 -0.0548 0.0024 1.0000 15.500 1.3274 0.09973 0.09492 -0.0573 0.0024 1.0000 16.000 1.2916 0.11116 0.10661 -0.0603 0.0024 1.0000 16.500 1.2534 0.12152 0.11721 -0.0633 0.0024 1.0000 17.000 1.2085 0.13007 0.12602 -0.0658 0.0025 1.0000 17.500 1.1749 0.13882 0.13500 -0.0693 0.0025 1.0000 18.000 1.1437 0.14799 0.14439 -0.0735 0.0025 1.0000 18.500 1.1135 0.15750 0.15412 -0.0782 0.0025 1.0000 19.000 1.0804 0.16824 0.16509 -0.0836 0.0026 1.0000 19.500 1.0427 0.18079 0.17787 -0.0899 0.0026 1.0000 20.000 1.0040 0.19495 0.19224 -0.0966 0.0026 1.0000 20.500 0.9780 0.20738 0.20480 -0.1022 0.0026 1.0000 21.000 0.9649 0.21715 0.21466 -0.1064 0.0027 1.0000 21.500 0.9603 0.22477 0.22235 -0.1097 0.0028 1.0000 22.000 0.9622 0.23042 0.22804 -0.1123 0.0029 1.0000 22.500 0.9685 0.23452 0.23218 -0.1144 0.0029 1.0000 23.000 0.9775 0.23757 0.23525 -0.1161 0.0031 1.0000 23.500 0.9883 0.23976 0.23746 -0.1175 0.0032 1.0000 24.000 0.9966 0.24278 0.24052 -0.1192 0.0033 1.0000 24.500 0.9910 0.25092 0.24877 -0.1226 0.0034 1.0000 25.000 0.9796 0.26200 0.26002 -0.1268 0.0036 1.0000 26.000 0.9134 0.32253 0.32071 -0.1377 0.0129 1.0000 26.500 0.9166 0.32914 0.32734 -0.1398 0.0123 1.0000 27.000 0.9216 0.33431 0.33255 -0.1413 0.0119 1.0000 27.500 0.9194 0.34566 0.34389 -0.1448 0.0105 1.0000 28.000 0.9221 0.35173 0.35000 -0.1469 0.0099 1.0000 28.500 0.9232 0.35995 0.35823 -0.1493 0.0095 1.0000 29.000 0.9244 0.36828 0.36658 -0.1517 0.0084 1.0000 29.500 0.9264 0.37435 0.37268 -0.1539 0.0079 1.0000 30.000 0.9276 0.38138 0.37974 -0.1560 0.0077 1.0000 30.500 0.9278 0.39114 0.38952 -0.1587 0.0069 1.0000 31.000 0.9287 0.39818 0.39659 -0.1610 0.0064 1.0000 31.500 0.9296 0.40431 0.40276 -0.1632 0.0061 1.0000 32.000 0.9304 0.41029 0.40877 -0.1651 0.0060 1.0000 32.500 0.9296 0.41976 0.41826 -0.1678 0.0059 1.0000 33.000 0.9295 0.42800 0.42653 -0.1701 0.0056 1.0000 33.500 0.9292 0.43530 0.43386 -0.1724 0.0053 1.0000 34.000 0.9287 0.44231 0.44090 -0.1746 0.0051 1.0000 34.500 0.9280 0.44916 0.44778 -0.1769 0.0049 1.0000 35.000 0.9269 0.45580 0.45446 -0.1791 0.0048 1.0000 35.500 0.9257 0.46226 0.46095 -0.1814 0.0047 1.0000 36.000 0.9241 0.46850 0.46723 -0.1836 0.0046 1.0000 36.500 0.9222 0.47432 0.47309 -0.1857 0.0045 1.0000 38.000 0.9152 0.49450 0.49338 -0.1924 0.0045 1.0000 38.500 0.9126 0.50154 0.50046 -0.1946 0.0045 1.0000 39.000 0.9101 0.50926 0.50821 -0.1967 0.0044 1.0000 39.500 0.9073 0.51625 0.51523 -0.1988 0.0038 1.0000 40.000 0.9040 0.52210 0.52112 -0.2009 0.0034 1.0000 40.500 0.8998 0.52670 0.52575 -0.2030 0.0033 1.0000 41.000 0.8973 0.53734 0.53640 -0.2048 0.0030 1.0000 41.500 0.8935 0.54370 0.54280 -0.2068 0.0025 1.0000 42.000 0.8889 0.54853 0.54767 -0.2089 0.0023 1.0000 42.500 0.8841 0.55436 0.55352 -0.2108 0.0022 1.0000 43.000 0.8813 0.56434 0.56351 -0.2124 0.0020 1.0000 43.500 0.8769 0.57076 0.56996 -0.2143 0.0016 1.0000 44.000 0.8717 0.57571 0.57494 -0.2163 0.0014 1.0000 44.500 0.8654 0.57922 0.57849 -0.2184 0.0013 1.0000 45.000 0.8607 0.58701 0.58629 -0.2200 0.0013 1.0000 45.500 0.8566 0.59508 0.59438 -0.2216 0.0012 1.0000 46.000 0.8515 0.60146 0.60078 -0.2232 0.0010 1.0000 46.500 0.8458 0.60682 0.60616 -0.2250 0.0008 1.0000 47.000 0.8397 0.61145 0.61083 -0.2268 0.0007 1.0000 47.500 0.8331 0.61547 0.61487 -0.2286 0.0006 1.0000 48.000 0.8256 0.61840 0.61784 -0.2305 0.0006 1.0000 48.500 0.8198 0.62505 0.62450 -0.2320 0.0005 1.0000 49.000 0.8143 0.63102 0.63049 -0.2333 0.0004 1.0000 49.500 0.8074 0.63500 0.63449 -0.2350 0.0003 1.0000 50.000 0.7996 0.63757 0.63709 -0.2367 0.0003 1.0000 51.000 0.7859 0.64684 0.64640 -0.2396 0.0002 1.0000 51.500 0.7785 0.65053 0.65011 -0.2410 0.0002 1.0000 52.000 0.7709 0.65364 0.65324 -0.2425 0.0001 1.0000 52.500 0.7628 0.65602 0.65564 -0.2440 0.0000 1.0000 53.000 0.7544 0.65764 0.65729 -0.2455 0.0000 1.0000 54.000 0.7375 0.66148 0.66117 -0.2484 0.0000 1.0000 54.500 0.7292 0.66361 0.66332 -0.2497 0.0000 1.0000 55.000 0.7207 0.66541 0.66515 -0.2510 0.0000 1.0000 55.500 0.7120 0.66689 0.66665 -0.2523 0.0000 1.0000 56.000 0.7031 0.66795 0.66773 -0.2535 0.0001 1.0000 56.500 0.6940 0.66855 0.66834 -0.2548 0.0002 1.0000 57.000 0.6847 0.66880 0.66862 -0.2560 0.0004 1.0000 57.500 0.6752 0.66849 0.66833 -0.2573 0.0007 1.0000 58.000 0.6654 0.66768 0.66754 -0.2585 0.0010 1.0000 58.500 0.6555 0.66652 0.66641 -0.2598 0.0012 1.0000 59.000 0.6452 0.66466 0.66457 -0.2610 0.0014 1.0000 59.500 0.6347 0.66245 0.66238 -0.2623 0.0016 1.0000