XFOIL Version 6.94 Calculated polar for: GOE 535 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 0.6500 0.01081 0.00385 -0.1282 0.4757 0.3947 0.500 0.7029 0.01108 0.00405 -0.1269 0.4627 0.4216 1.000 0.7557 0.01136 0.00432 -0.1257 0.4513 0.4423 1.500 0.8081 0.01160 0.00454 -0.1244 0.4405 0.4601 2.000 0.8599 0.01198 0.00482 -0.1231 0.4294 0.4755 2.500 0.9113 0.01217 0.00506 -0.1217 0.4187 0.4913 3.000 0.9613 0.01259 0.00538 -0.1202 0.4069 0.5049 3.500 1.0124 0.01277 0.00563 -0.1188 0.3996 0.5177 4.000 1.0617 0.01302 0.00586 -0.1172 0.3905 0.5277 4.500 1.1101 0.01340 0.00622 -0.1154 0.3810 0.5395 5.000 1.1580 0.01358 0.00649 -0.1136 0.3725 0.5511 5.500 1.2027 0.01400 0.00684 -0.1112 0.3628 0.5643 6.000 1.2471 0.01424 0.00721 -0.1088 0.3546 0.5788 6.500 1.2855 0.01452 0.00753 -0.1053 0.3449 0.5949 7.000 1.3235 0.01493 0.00800 -0.1019 0.3352 0.6143 7.500 1.3602 0.01527 0.00846 -0.0983 0.3251 0.6387 8.000 1.3928 0.01566 0.00904 -0.0942 0.3124 0.6894 9.000 1.4945 0.01705 0.01068 -0.0945 0.2764 1.0000 9.500 1.5266 0.01805 0.01164 -0.0912 0.2622 1.0000 10.000 1.5525 0.01941 0.01291 -0.0874 0.2429 1.0000 10.500 1.5784 0.02092 0.01439 -0.0839 0.2269 1.0000 11.000 1.6045 0.02257 0.01605 -0.0809 0.2151 1.0000 11.500 1.6253 0.02468 0.01815 -0.0777 0.2039 1.0000 12.000 1.6409 0.02734 0.02081 -0.0747 0.1908 1.0000 12.500 1.6598 0.02997 0.02350 -0.0724 0.1805 1.0000 13.000 1.6698 0.03351 0.02706 -0.0701 0.1682 1.0000 13.500 1.6747 0.03777 0.03137 -0.0681 0.1575 1.0000 14.000 1.6776 0.04248 0.03613 -0.0666 0.1471 1.0000 14.500 1.6773 0.04775 0.04150 -0.0655 0.1362 1.0000 15.000 1.6691 0.05412 0.04793 -0.0649 0.1239 1.0000 15.500 1.6467 0.06245 0.05631 -0.0648 0.1073 1.0000 16.000 1.6128 0.07257 0.06646 -0.0655 0.0904 1.0000 16.500 1.5847 0.08229 0.07627 -0.0666 0.0799 1.0000 17.000 1.5513 0.09305 0.08714 -0.0684 0.0703 1.0000 17.500 1.5236 0.10324 0.09743 -0.0704 0.0633 1.0000 18.000 1.5070 0.11210 0.10642 -0.0725 0.0603 1.0000 18.500 1.4914 0.12096 0.11541 -0.0749 0.0567 1.0000 19.000 1.4759 0.13003 0.12459 -0.0779 0.0533 1.0000 19.500 1.4673 0.13816 0.13285 -0.0809 0.0506 1.0000 20.000 1.4583 0.14641 0.14122 -0.0843 0.0477 1.0000 20.500 1.4536 0.15405 0.14896 -0.0877 0.0454 1.0000 21.000 1.4511 0.16137 0.15639 -0.0912 0.0431 1.0000 21.500 1.4453 0.16934 0.16445 -0.0955 0.0395 1.0000 22.000 1.4423 0.17677 0.17196 -0.0996 0.0364 1.0000 22.500 1.4437 0.18338 0.17867 -0.1035 0.0343 1.0000 23.000 1.4396 0.19110 0.18644 -0.1083 0.0298 1.0000 23.500 1.4394 0.19807 0.19349 -0.1128 0.0273 1.0000 24.000 1.4376 0.20537 0.20082 -0.1178 0.0225 1.0000 24.500 1.4313 0.21363 0.20910 -0.1236 0.0161 1.0000 25.000 1.4059 0.22628 0.22168 -0.1326 0.0030 1.0000 25.500 1.4036 0.23400 0.22952 -0.1384 0.0023 1.0000 26.000 1.4036 0.24124 0.23690 -0.1440 0.0021 1.0000 26.500 1.4041 0.24842 0.24421 -0.1497 0.0020 1.0000 27.000 1.4045 0.25573 0.25165 -0.1556 0.0020 1.0000 27.500 1.4004 0.26435 0.26044 -0.1626 0.0019 1.0000 28.000 1.3972 0.27298 0.26923 -0.1696 0.0019 1.0000 28.500 1.3896 0.28311 0.27955 -0.1777 0.0018 1.0000 29.000 1.3840 0.29306 0.28967 -0.1857 0.0019 1.0000 29.500 1.3783 0.30344 0.30020 -0.1939 0.0019 1.0000 30.000 1.3758 0.31291 0.30981 -0.2016 0.0018 1.0000 30.500 1.3785 0.32045 0.31744 -0.2081 0.0019 1.0000 31.000 1.3817 0.32772 0.32480 -0.2144 0.0019 1.0000 31.500 1.3873 0.33375 0.33089 -0.2201 0.0019 1.0000 32.000 1.3935 0.33930 0.33649 -0.2255 0.0019 1.0000 32.500 1.4011 0.34401 0.34124 -0.2306 0.0018 1.0000 33.000 1.4088 0.34818 0.34545 -0.2354 0.0018 1.0000 33.500 1.4174 0.35172 0.34901 -0.2399 0.0018 1.0000 34.000 1.4258 0.35501 0.35233 -0.2444 0.0018 1.0000 34.500 1.4345 0.35797 0.35532 -0.2488 0.0018 1.0000 35.000 1.4433 0.36050 0.35787 -0.2530 0.0018 1.0000 35.500 1.4517 0.36307 0.36046 -0.2573 0.0018 1.0000 36.000 1.4595 0.36559 0.36301 -0.2616 0.0018 1.0000 36.500 1.4667 0.36815 0.36561 -0.2659 0.0018 1.0000 37.000 1.4741 0.37073 0.36823 -0.2705 0.0018 1.0000 37.500 1.4799 0.37345 0.37099 -0.2750 0.0018 1.0000 38.000 1.4850 0.37659 0.37420 -0.2800 0.0018 1.0000 38.500 1.4890 0.37986 0.37755 -0.2849 0.0018 1.0000 39.000 1.4918 0.38330 0.38107 -0.2901 0.0019 1.0000 39.500 1.4927 0.38775 0.38564 -0.2960 0.0019 1.0000 40.500 0.9860 0.61372 0.61280 -0.2573 0.0057 1.0000 41.000 0.9804 0.62845 0.62754 -0.2596 0.0055 1.0000 41.500 0.9762 0.63705 0.63617 -0.2616 0.0050 1.0000 42.000 0.9718 0.64314 0.64228 -0.2635 0.0047 1.0000 42.500 0.9672 0.64717 0.64634 -0.2654 0.0044 1.0000 43.000 0.9626 0.65076 0.64996 -0.2671 0.0044 1.0000 43.500 0.9566 0.66625 0.66547 -0.2690 0.0038 1.0000 44.000 0.9511 0.67138 0.67063 -0.2708 0.0034 1.0000 44.500 0.9453 0.67462 0.67390 -0.2725 0.0033 1.0000 45.000 0.9391 0.68407 0.68337 -0.2741 0.0032 1.0000 45.500 0.9331 0.69254 0.69186 -0.2756 0.0027 1.0000 46.000 0.9265 0.69625 0.69559 -0.2772 0.0024 1.0000 46.500 0.9196 0.69793 0.69730 -0.2788 0.0023 1.0000 47.000 0.9128 0.70899 0.70838 -0.2801 0.0022 1.0000 47.500 0.9058 0.71494 0.71435 -0.2815 0.0018 1.0000 48.000 0.8983 0.71749 0.71692 -0.2829 0.0016 1.0000 48.500 0.8904 0.71832 0.71778 -0.2844 0.0015 1.0000 49.000 0.8824 0.72342 0.72289 -0.2856 0.0015 1.0000 49.500 0.8751 0.73235 0.73185 -0.2866 0.0013 1.0000 50.000 0.8669 0.73508 0.73459 -0.2878 0.0011 1.0000 50.500 0.8582 0.73570 0.73523 -0.2890 0.0010 1.0000 51.000 0.8492 0.73505 0.73461 -0.2902 0.0009 1.0000 51.500 0.8403 0.73784 0.73742 -0.2912 0.0009 1.0000 52.000 0.8323 0.74611 0.74570 -0.2919 0.0008 1.0000 52.500 0.8232 0.74793 0.74754 -0.2928 0.0007 1.0000 53.000 0.8138 0.74801 0.74764 -0.2937 0.0006 1.0000 53.500 0.8041 0.74697 0.74662 -0.2946 0.0005 1.0000 54.000 0.7941 0.74470 0.74437 -0.2956 0.0005 1.0000 55.000 0.7742 0.74515 0.74485 -0.2970 0.0005 1.0000 55.500 0.7647 0.74714 0.74685 -0.2974 0.0004 1.0000 56.000 0.7549 0.74751 0.74724 -0.2980 0.0004 1.0000 56.500 0.7447 0.74613 0.74588 -0.2985 0.0003 1.0000 57.000 0.7342 0.74334 0.74311 -0.2990 0.0003 1.0000 57.500 0.7235 0.73986 0.73964 -0.2995 0.0002 1.0000 58.000 0.7125 0.73523 0.73503 -0.3000 0.0002 1.0000 58.500 0.7012 0.72938 0.72920 -0.3006 0.0002 1.0000 59.500 0.6800 0.72606 0.72590 -0.3009 0.0001 1.0000 60.000 0.6691 0.72185 0.72171 -0.3010 0.0001 1.0000