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 = 0.300 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.6498 0.01261 0.00516 -0.1283 0.5052 0.4298 0.500 0.7025 0.01288 0.00542 -0.1270 0.4918 0.4528 1.000 0.7555 0.01336 0.00574 -0.1259 0.4788 0.4743 1.500 0.8074 0.01363 0.00606 -0.1245 0.4671 0.4921 2.000 0.8602 0.01412 0.00643 -0.1233 0.4551 0.5091 2.500 0.9108 0.01436 0.00671 -0.1218 0.4446 0.5257 3.000 0.9625 0.01484 0.00706 -0.1206 0.4320 0.5403 3.500 1.0117 0.01498 0.00727 -0.1189 0.4221 0.5498 4.000 1.0617 0.01530 0.00754 -0.1175 0.4119 0.5609 4.500 1.1119 0.01568 0.00794 -0.1162 0.4027 0.5729 5.000 1.1589 0.01594 0.00824 -0.1143 0.3927 0.5863 5.500 1.2077 0.01641 0.00867 -0.1128 0.3824 0.6013 6.000 1.2509 0.01660 0.00904 -0.1103 0.3733 0.6188 6.500 1.2950 0.01697 0.00943 -0.1080 0.3634 0.6420 7.000 1.3357 0.01727 0.00996 -0.1052 0.3535 0.6747 7.500 1.3997 0.01742 0.01054 -0.1073 0.3414 1.0000 8.000 1.4348 0.01803 0.01119 -0.1036 0.3312 1.0000 8.500 1.4661 0.01872 0.01178 -0.0994 0.3195 1.0000 9.000 1.4961 0.01945 0.01260 -0.0952 0.3078 1.0000 9.500 1.5239 0.02045 0.01352 -0.0910 0.2957 1.0000 10.000 1.5452 0.02155 0.01462 -0.0863 0.2807 1.0000 10.500 1.5673 0.02292 0.01602 -0.0822 0.2658 1.0000 11.000 1.5889 0.02460 0.01773 -0.0785 0.2542 1.0000 11.500 1.6052 0.02674 0.01983 -0.0747 0.2419 1.0000 12.000 1.6204 0.02917 0.02231 -0.0715 0.2274 1.0000 12.500 1.6355 0.03191 0.02514 -0.0688 0.2173 1.0000 13.000 1.6437 0.03539 0.02863 -0.0663 0.2072 1.0000 13.500 1.6569 0.03878 0.03216 -0.0645 0.1983 1.0000 14.000 1.6597 0.04324 0.03666 -0.0628 0.1905 1.0000 14.500 1.6681 0.04749 0.04109 -0.0617 0.1825 1.0000 15.000 1.6634 0.05322 0.04688 -0.0609 0.1732 1.0000 15.500 1.6564 0.05962 0.05340 -0.0608 0.1627 1.0000 16.000 1.6497 0.06616 0.06009 -0.0609 0.1537 1.0000 16.500 1.6362 0.07374 0.06777 -0.0615 0.1457 1.0000 17.000 1.6212 0.08184 0.07602 -0.0626 0.1349 1.0000 17.500 1.5983 0.09126 0.08555 -0.0645 0.1222 1.0000 18.000 1.5735 0.10114 0.09552 -0.0668 0.1095 1.0000 18.500 1.5395 0.11271 0.10715 -0.0702 0.0949 1.0000 19.000 1.5085 0.12414 0.11863 -0.0742 0.0847 1.0000 19.500 1.4867 0.13441 0.12899 -0.0782 0.0778 1.0000 20.000 1.4696 0.14403 0.13867 -0.0824 0.0728 1.0000 20.500 1.4599 0.15253 0.14726 -0.0864 0.0683 1.0000 21.000 1.4543 0.16033 0.15512 -0.0903 0.0646 1.0000 21.500 1.4506 0.16785 0.16272 -0.0943 0.0609 1.0000 22.000 1.4498 0.17476 0.16969 -0.0982 0.0580 1.0000 22.500 1.4535 0.18086 0.17591 -0.1018 0.0556 1.0000 23.000 1.4532 0.18764 0.18270 -0.1060 0.0526 1.0000 23.500 1.4586 0.19340 0.18860 -0.1097 0.0507 1.0000 24.000 1.4580 0.20035 0.19565 -0.1144 0.0477 1.0000 24.500 1.4634 0.20592 0.20127 -0.1183 0.0460 1.0000 25.000 1.4638 0.21265 0.20818 -0.1231 0.0435 1.0000 25.500 1.4658 0.21891 0.21452 -0.1278 0.0416 1.0000 26.000 1.4684 0.22502 0.22075 -0.1325 0.0397 1.0000 26.500 1.4680 0.23178 0.22767 -0.1378 0.0377 1.0000 27.000 1.4685 0.23828 0.23422 -0.1430 0.0359 1.0000 27.500 1.4639 0.24610 0.24225 -0.1493 0.0333 1.0000 28.000 1.4618 0.25332 0.24960 -0.1553 0.0318 1.0000 28.500 1.4533 0.26226 0.25872 -0.1626 0.0297 1.0000 29.000 1.4417 0.27231 0.26898 -0.1708 0.0288 1.0000 29.500 1.4157 0.28728 0.28416 -0.1825 0.0266 1.0000 30.000 1.3814 0.30718 0.30425 -0.1970 0.0229 1.0000 30.500 1.3727 0.31943 0.31659 -0.2062 0.0203 1.0000 31.000 1.3746 0.32747 0.32471 -0.2129 0.0169 1.0000 31.500 1.3741 0.33711 0.33444 -0.2205 0.0123 1.0000 32.500 1.3965 0.34212 0.33915 -0.2284 0.0045 1.0000 33.000 1.4026 0.34732 0.34436 -0.2338 0.0041 1.0000 33.500 1.4094 0.35196 0.34902 -0.2389 0.0038 1.0000 34.000 1.4170 0.35583 0.35292 -0.2437 0.0037 1.0000 34.500 1.4247 0.35940 0.35652 -0.2484 0.0036 1.0000 35.000 1.4325 0.36259 0.35973 -0.2530 0.0034 1.0000 35.500 1.4404 0.36541 0.36258 -0.2574 0.0034 1.0000 36.000 1.4485 0.36774 0.36493 -0.2616 0.0033 1.0000 36.500 1.4561 0.37010 0.36733 -0.2659 0.0032 1.0000 37.000 1.4635 0.37265 0.36993 -0.2705 0.0032 1.0000 37.500 1.4692 0.37550 0.37286 -0.2751 0.0032 1.0000 38.000 1.4746 0.37857 0.37600 -0.2800 0.0032 1.0000 38.500 1.4772 0.38269 0.38023 -0.2855 0.0032 1.0000 40.000 0.9857 0.61334 0.61218 -0.2543 0.0090 1.0000 40.500 0.9820 0.62209 0.62097 -0.2564 0.0085 1.0000 41.000 0.9782 0.62936 0.62827 -0.2584 0.0079 1.0000 41.500 0.9742 0.63538 0.63432 -0.2604 0.0076 1.0000 42.000 0.9704 0.63926 0.63823 -0.2621 0.0073 1.0000 42.500 0.9648 0.65220 0.65120 -0.2642 0.0069 1.0000 43.000 0.9598 0.65918 0.65821 -0.2660 0.0064 1.0000 43.500 0.9548 0.66448 0.66354 -0.2678 0.0059 1.0000 44.000 0.9497 0.66743 0.66653 -0.2695 0.0057 1.0000 44.500 0.9435 0.68003 0.67915 -0.2713 0.0053 1.0000 45.000 0.9376 0.68591 0.68507 -0.2729 0.0048 1.0000 45.500 0.9314 0.68950 0.68868 -0.2746 0.0045 1.0000 46.000 0.9248 0.69642 0.69563 -0.2761 0.0043 1.0000 46.500 0.9183 0.70445 0.70368 -0.2775 0.0038 1.0000 47.000 0.9114 0.70849 0.70775 -0.2790 0.0035 1.0000 47.500 0.9041 0.71029 0.70958 -0.2805 0.0033 1.0000 48.000 0.8969 0.71837 0.71768 -0.2818 0.0031 1.0000 48.500 0.8895 0.72406 0.72339 -0.2831 0.0027 1.0000 49.000 0.8817 0.72681 0.72618 -0.2844 0.0025 1.0000 49.500 0.8734 0.72755 0.72694 -0.2857 0.0023 1.0000 50.000 0.8653 0.73306 0.73247 -0.2868 0.0022 1.0000 50.500 0.8574 0.73864 0.73808 -0.2878 0.0020 1.0000 51.000 0.8488 0.74072 0.74018 -0.2889 0.0017 1.0000 51.500 0.8399 0.74110 0.74059 -0.2900 0.0016 1.0000 52.000 0.8305 0.73940 0.73891 -0.2912 0.0015 1.0000 52.500 0.8217 0.74505 0.74458 -0.2920 0.0015 1.0000 53.000 0.8128 0.74810 0.74765 -0.2927 0.0013 1.0000 53.500 0.8035 0.74885 0.74842 -0.2935 0.0012 1.0000 54.000 0.7938 0.74816 0.74775 -0.2944 0.0010 1.0000 54.500 0.7837 0.74570 0.74532 -0.2953 0.0009 1.0000 55.500 0.7636 0.74486 0.74452 -0.2966 0.0009 1.0000 56.000 0.7539 0.74567 0.74535 -0.2971 0.0008 1.0000 56.500 0.7438 0.74479 0.74448 -0.2975 0.0007 1.0000 57.000 0.7333 0.74239 0.74211 -0.2981 0.0007 1.0000 57.500 0.7227 0.73909 0.73882 -0.2985 0.0006 1.0000 58.000 0.7118 0.73473 0.73449 -0.2990 0.0005 1.0000 58.500 0.7006 0.72922 0.72899 -0.2995 0.0005 1.0000 60.000 0.6679 0.71961 0.71943 -0.3001 0.0004 1.0000