XFOIL Version 6.94 Calculated polar for: GOE 626 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 0.6003 0.01430 0.00672 -0.1371 0.5815 0.3209 0.500 0.6516 0.01423 0.00658 -0.1358 0.5617 0.3251 1.000 0.7032 0.01431 0.00654 -0.1346 0.5423 0.3289 1.500 0.7537 0.01418 0.00627 -0.1333 0.5232 0.3331 2.000 0.8036 0.01416 0.00620 -0.1318 0.5050 0.3374 2.500 0.8541 0.01425 0.00630 -0.1304 0.4887 0.3425 3.000 0.9042 0.01445 0.00643 -0.1290 0.4736 0.3475 3.500 0.9532 0.01468 0.00657 -0.1273 0.4583 0.3518 4.000 1.0025 0.01480 0.00673 -0.1258 0.4450 0.3567 4.500 1.0507 0.01509 0.00699 -0.1242 0.4311 0.3637 5.000 1.0918 0.01530 0.00719 -0.1211 0.4118 0.3705 5.500 1.1253 0.01560 0.00739 -0.1167 0.3854 0.3766 6.000 1.1594 0.01582 0.00765 -0.1124 0.3656 0.3847 6.500 1.1908 0.01627 0.00810 -0.1078 0.3420 0.3945 7.000 1.2258 0.01677 0.00863 -0.1040 0.3218 0.4073 7.500 1.2547 0.01747 0.00933 -0.0994 0.2900 0.4253 8.000 1.2742 0.01861 0.01038 -0.0937 0.2454 0.4550 8.500 1.2884 0.01996 0.01190 -0.0878 0.1982 0.5892 9.500 1.3230 0.02354 0.01569 -0.0787 0.1463 1.0000 10.000 1.3431 0.02549 0.01761 -0.0748 0.1314 1.0000 10.500 1.3524 0.02828 0.02024 -0.0704 0.0968 1.0000 11.000 1.3334 0.03347 0.02515 -0.0649 0.0575 1.0000 11.500 1.3397 0.03727 0.02899 -0.0621 0.0494 1.0000 12.000 1.3485 0.04120 0.03300 -0.0600 0.0445 1.0000 12.500 1.3584 0.04536 0.03726 -0.0586 0.0398 1.0000 13.000 1.3618 0.05049 0.04245 -0.0577 0.0300 1.0000 13.500 1.3388 0.05908 0.05104 -0.0576 0.0065 1.0000 14.000 1.3368 0.06564 0.05777 -0.0580 0.0054 1.0000 14.500 1.3362 0.07234 0.06465 -0.0588 0.0051 1.0000 15.000 1.3349 0.07942 0.07191 -0.0601 0.0049 1.0000 15.500 1.3325 0.08694 0.07964 -0.0618 0.0048 1.0000 16.000 1.3300 0.09469 0.08758 -0.0639 0.0047 1.0000 16.500 1.3277 0.10260 0.09568 -0.0663 0.0047 1.0000 17.000 1.3248 0.11073 0.10401 -0.0690 0.0046 1.0000 17.500 1.3224 0.11887 0.11235 -0.0720 0.0046 1.0000 18.000 1.3197 0.12714 0.12081 -0.0753 0.0045 1.0000 18.500 1.3179 0.13526 0.12912 -0.0789 0.0045 1.0000 19.000 1.3161 0.14339 0.13744 -0.0826 0.0045 1.0000 19.500 1.3138 0.15164 0.14588 -0.0867 0.0045 1.0000 20.000 1.3107 0.16004 0.15448 -0.0911 0.0045 1.0000 20.500 1.3066 0.16868 0.16331 -0.0959 0.0045 1.0000 21.000 1.3007 0.17770 0.17253 -0.1012 0.0045 1.0000 21.500 1.2932 0.18715 0.18219 -0.1069 0.0045 1.0000 22.000 1.2847 0.19692 0.19216 -0.1131 0.0046 1.0000 22.500 1.2731 0.20748 0.20292 -0.1198 0.0046 1.0000 23.000 1.2613 0.21825 0.21389 -0.1269 0.0047 1.0000 23.500 1.2471 0.22982 0.22566 -0.1345 0.0047 1.0000 24.000 1.2353 0.24107 0.23706 -0.1418 0.0048 1.0000 24.500 1.2327 0.24995 0.24603 -0.1477 0.0048 1.0000 25.000 1.2381 0.25651 0.25263 -0.1524 0.0049 1.0000 25.500 1.2484 0.26139 0.25754 -0.1561 0.0049 1.0000 26.000 1.2626 0.26492 0.26106 -0.1592 0.0049 1.0000 26.500 1.2780 0.26784 0.26397 -0.1619 0.0049 1.0000 27.000 1.2942 0.27046 0.26658 -0.1645 0.0049 1.0000 27.500 1.3110 0.27263 0.26872 -0.1670 0.0049 1.0000 28.000 1.3268 0.27494 0.27103 -0.1695 0.0050 1.0000 28.500 1.3407 0.27769 0.27380 -0.1724 0.0050 1.0000 29.000 1.3540 0.28048 0.27661 -0.1753 0.0050 1.0000 29.500 1.3672 0.28306 0.27923 -0.1782 0.0051 1.0000 30.000 1.3792 0.28588 0.28209 -0.1813 0.0051 1.0000 30.500 1.3820 0.29173 0.28807 -0.1863 0.0052 1.0000 31.000 1.3808 0.29890 0.29542 -0.1921 0.0053 1.0000 31.500 1.3730 0.30843 0.30521 -0.1992 0.0056 1.0000 33.000 1.0022 0.49175 0.49020 -0.2239 0.0146 1.0000 33.500 1.0009 0.50525 0.50372 -0.2272 0.0142 1.0000 34.000 1.0013 0.51550 0.51399 -0.2299 0.0134 1.0000 34.500 1.0019 0.52434 0.52286 -0.2324 0.0129 1.0000 35.000 1.0024 0.53244 0.53099 -0.2348 0.0126 1.0000 35.500 1.0029 0.53963 0.53820 -0.2370 0.0123 1.0000 36.000 1.0029 0.54778 0.54637 -0.2391 0.0122 1.0000 36.500 1.0005 0.55966 0.55829 -0.2420 0.0121 1.0000 37.000 0.9990 0.56961 0.56826 -0.2445 0.0117 1.0000 37.500 0.9975 0.57826 0.57695 -0.2468 0.0114 1.0000 38.000 0.9958 0.58651 0.58522 -0.2491 0.0110 1.0000 38.500 0.9938 0.59419 0.59293 -0.2513 0.0106 1.0000 39.000 0.9916 0.60084 0.59962 -0.2534 0.0103 1.0000 39.500 0.9898 0.60624 0.60504 -0.2552 0.0101 1.0000 40.000 0.9857 0.61706 0.61589 -0.2577 0.0100 1.0000 40.500 0.9822 0.62698 0.62584 -0.2598 0.0094 1.0000 41.000 0.9788 0.63432 0.63321 -0.2619 0.0088 1.0000 41.500 0.9750 0.64033 0.63925 -0.2638 0.0085 1.0000 42.000 0.9713 0.64492 0.64388 -0.2655 0.0083 1.0000 42.500 0.9663 0.65731 0.65629 -0.2676 0.0079 1.0000 43.000 0.9617 0.66457 0.66358 -0.2695 0.0072 1.0000 43.500 0.9568 0.66991 0.66895 -0.2713 0.0068 1.0000 44.000 0.9515 0.67413 0.67319 -0.2730 0.0066 1.0000 44.500 0.9460 0.68456 0.68365 -0.2747 0.0064 1.0000 45.000 0.9405 0.69153 0.69064 -0.2763 0.0058 1.0000 45.500 0.9345 0.69626 0.69540 -0.2780 0.0054 1.0000 46.000 0.9281 0.69923 0.69840 -0.2795 0.0052 1.0000 46.500 0.9217 0.70841 0.70759 -0.2810 0.0050 1.0000 47.000 0.9153 0.71466 0.71387 -0.2824 0.0045 1.0000 47.500 0.9084 0.71875 0.71799 -0.2839 0.0042 1.0000 48.000 0.9011 0.72158 0.72085 -0.2853 0.0039 1.0000 48.500 0.8934 0.72262 0.72191 -0.2867 0.0038 1.0000 49.000 0.8862 0.73124 0.73054 -0.2879 0.0037 1.0000 49.500 0.8787 0.73619 0.73552 -0.2891 0.0033 1.0000 50.000 0.8708 0.73890 0.73826 -0.2903 0.0030 1.0000 50.500 0.8624 0.74028 0.73966 -0.2915 0.0028 1.0000 51.000 0.8537 0.74043 0.73983 -0.2926 0.0027 1.0000 52.000 0.8366 0.74720 0.74664 -0.2946 0.0026 1.0000 52.500 0.8280 0.74959 0.74905 -0.2955 0.0024 1.0000 53.000 0.8189 0.75064 0.75012 -0.2964 0.0022 1.0000 53.500 0.8097 0.75087 0.75037 -0.2973 0.0019 1.0000 54.000 0.8001 0.74973 0.74925 -0.2981 0.0018 1.0000 54.500 0.7902 0.74797 0.74751 -0.2990 0.0017 1.0000 55.000 0.7800 0.74488 0.74444 -0.2998 0.0016 1.0000 56.000 0.7604 0.74519 0.74478 -0.3010 0.0016 1.0000 56.500 0.7504 0.74415 0.74376 -0.3015 0.0016 1.0000 57.000 0.7403 0.74237 0.74200 -0.3020 0.0015 1.0000 57.500 0.7300 0.73983 0.73948 -0.3024 0.0014 1.0000 58.000 0.7195 0.73652 0.73619 -0.3029 0.0012 1.0000 58.500 0.7087 0.73236 0.73204 -0.3033 0.0011 1.0000 59.000 0.6979 0.72781 0.72751 -0.3036 0.0010 1.0000 59.500 0.6869 0.72262 0.72234 -0.3040 0.0009 1.0000 60.000 0.6758 0.71667 0.71641 -0.3043 0.0008 1.0000