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 = 0.450 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.6005 0.01200 0.00491 -0.1371 0.5504 0.3018 0.500 0.6520 0.01204 0.00484 -0.1358 0.5302 0.3050 1.000 0.7035 0.01216 0.00487 -0.1345 0.5098 0.3076 1.500 0.7541 0.01198 0.00464 -0.1332 0.4914 0.3124 2.000 0.8041 0.01210 0.00470 -0.1317 0.4743 0.3161 2.500 0.8537 0.01229 0.00484 -0.1301 0.4581 0.3203 3.000 0.9036 0.01246 0.00499 -0.1286 0.4426 0.3246 3.500 0.9520 0.01271 0.00518 -0.1268 0.4279 0.3281 4.000 0.9985 0.01295 0.00535 -0.1247 0.4120 0.3316 4.500 1.0385 0.01313 0.00547 -0.1214 0.3818 0.3376 5.000 1.0779 0.01345 0.00574 -0.1181 0.3627 0.3435 5.500 1.1136 0.01388 0.00604 -0.1141 0.3275 0.3488 6.000 1.1513 0.01440 0.00648 -0.1106 0.3049 0.3535 6.500 1.1849 0.01505 0.00704 -0.1066 0.2714 0.3623 7.000 1.1915 0.01704 0.00844 -0.0988 0.1784 0.3692 7.500 1.2158 0.01830 0.00957 -0.0938 0.1532 0.3777 8.000 1.2431 0.01937 0.01068 -0.0896 0.1374 0.3941 8.500 1.2536 0.02137 0.01246 -0.0835 0.0845 0.4150 9.000 1.2551 0.02397 0.01502 -0.0769 0.0503 0.4608 10.000 1.2932 0.02781 0.01973 -0.0703 0.0191 1.0000 10.500 1.2990 0.03117 0.02312 -0.0662 0.0040 1.0000 11.000 1.3160 0.03396 0.02599 -0.0636 0.0036 1.0000 11.500 1.3301 0.03723 0.02937 -0.0613 0.0035 1.0000 12.000 1.3420 0.04096 0.03322 -0.0595 0.0034 1.0000 12.500 1.3514 0.04528 0.03768 -0.0582 0.0033 1.0000 13.000 1.3583 0.05014 0.04269 -0.0573 0.0033 1.0000 13.500 1.3632 0.05547 0.04817 -0.0570 0.0032 1.0000 14.000 1.3649 0.06145 0.05432 -0.0571 0.0032 1.0000 14.500 1.3646 0.06792 0.06096 -0.0576 0.0032 1.0000 15.000 1.3633 0.07481 0.06804 -0.0586 0.0032 1.0000 15.500 1.3601 0.08226 0.07568 -0.0601 0.0032 1.0000 16.000 1.3564 0.09008 0.08369 -0.0620 0.0032 1.0000 16.500 1.3525 0.09812 0.09191 -0.0643 0.0032 1.0000 17.000 1.3481 0.10644 0.10043 -0.0670 0.0032 1.0000 17.500 1.3440 0.11483 0.10900 -0.0700 0.0032 1.0000 18.000 1.3390 0.12348 0.11785 -0.0734 0.0032 1.0000 18.500 1.3345 0.13213 0.12668 -0.0771 0.0032 1.0000 19.000 1.3288 0.14103 0.13577 -0.0813 0.0033 1.0000 19.500 1.3220 0.15021 0.14515 -0.0858 0.0033 1.0000 20.000 1.3141 0.15964 0.15476 -0.0908 0.0033 1.0000 20.500 1.3049 0.16937 0.16468 -0.0963 0.0033 1.0000 21.000 1.2953 0.17919 0.17468 -0.1020 0.0034 1.0000 21.500 1.2854 0.18920 0.18486 -0.1081 0.0034 1.0000 22.000 1.2770 0.19893 0.19474 -0.1141 0.0034 1.0000 22.500 1.2699 0.20837 0.20431 -0.1202 0.0034 1.0000 23.000 1.2662 0.21704 0.21308 -0.1258 0.0035 1.0000 23.500 1.2656 0.22491 0.22103 -0.1311 0.0035 1.0000 24.000 1.2691 0.23165 0.22782 -0.1357 0.0036 1.0000 24.500 1.2744 0.23785 0.23406 -0.1401 0.0036 1.0000 25.000 1.2825 0.24322 0.23945 -0.1440 0.0036 1.0000 25.500 1.2927 0.24787 0.24412 -0.1475 0.0037 1.0000 26.000 1.3050 0.25181 0.24806 -0.1507 0.0037 1.0000 26.500 1.3187 0.25515 0.25140 -0.1536 0.0037 1.0000 27.000 1.3338 0.25791 0.25415 -0.1562 0.0038 1.0000 27.500 1.3446 0.26192 0.25820 -0.1596 0.0038 1.0000 28.000 1.3522 0.26686 0.26322 -0.1637 0.0039 1.0000 28.500 1.3578 0.27225 0.26869 -0.1681 0.0039 1.0000 29.000 1.3635 0.27754 0.27408 -0.1725 0.0040 1.0000 29.500 1.3685 0.28292 0.27958 -0.1770 0.0041 1.0000 30.000 1.3740 0.28795 0.28473 -0.1814 0.0043 1.0000 30.500 1.3763 0.29382 0.29075 -0.1863 0.0044 1.0000 31.000 1.3770 0.30006 0.29713 -0.1916 0.0046 1.0000 31.500 1.3750 0.30713 0.30434 -0.1973 0.0048 1.0000 32.000 1.3712 0.31463 0.31198 -0.2033 0.0050 1.0000 32.500 1.3724 0.32061 0.31805 -0.2084 0.0052 1.0000 33.000 1.0082 0.48913 0.48786 -0.2254 0.0102 1.0000 33.500 1.0052 0.50615 0.50488 -0.2290 0.0097 1.0000 34.000 1.0057 0.51606 0.51481 -0.2316 0.0092 1.0000 34.500 1.0061 0.52502 0.52379 -0.2341 0.0089 1.0000 35.000 1.0062 0.53341 0.53221 -0.2365 0.0086 1.0000 35.500 1.0062 0.54120 0.54002 -0.2388 0.0085 1.0000 36.000 1.0060 0.54832 0.54716 -0.2411 0.0084 1.0000 37.000 1.0037 0.56593 0.56481 -0.2457 0.0082 1.0000 37.500 1.0014 0.57623 0.57513 -0.2482 0.0082 1.0000 38.000 0.9991 0.58648 0.58541 -0.2506 0.0081 1.0000 38.500 0.9968 0.59586 0.59482 -0.2529 0.0077 1.0000 39.000 0.9943 0.60382 0.60281 -0.2550 0.0074 1.0000 39.500 0.9916 0.61127 0.61028 -0.2572 0.0071 1.0000 40.000 0.9887 0.61771 0.61675 -0.2592 0.0068 1.0000 40.500 0.9855 0.62318 0.62224 -0.2612 0.0067 1.0000 41.000 0.9820 0.62971 0.62879 -0.2630 0.0066 1.0000 41.500 0.9775 0.64339 0.64249 -0.2652 0.0061 1.0000 42.000 0.9733 0.65047 0.64960 -0.2672 0.0056 1.0000 42.500 0.9688 0.65572 0.65487 -0.2690 0.0053 1.0000 43.000 0.9642 0.65955 0.65873 -0.2708 0.0051 1.0000 43.500 0.9589 0.67193 0.67113 -0.2726 0.0049 1.0000 44.000 0.9538 0.67961 0.67883 -0.2743 0.0044 1.0000 44.500 0.9482 0.68474 0.68398 -0.2760 0.0040 1.0000 45.000 0.9423 0.68819 0.68746 -0.2777 0.0039 1.0000 45.500 0.9362 0.69067 0.68996 -0.2793 0.0038 1.0000 46.000 0.9304 0.70510 0.70441 -0.2807 0.0034 1.0000 46.500 0.9238 0.70987 0.70920 -0.2822 0.0030 1.0000 47.000 0.9170 0.71314 0.71250 -0.2838 0.0028 1.0000 47.500 0.9097 0.71542 0.71479 -0.2853 0.0027 1.0000 48.500 0.8955 0.72896 0.72837 -0.2878 0.0025 1.0000 49.000 0.8881 0.73408 0.73350 -0.2890 0.0021 1.0000 49.500 0.8803 0.73689 0.73633 -0.2902 0.0019 1.0000 50.000 0.8720 0.73827 0.73774 -0.2915 0.0017 1.0000 50.500 0.8634 0.73844 0.73792 -0.2927 0.0017 1.0000 51.500 0.8462 0.74433 0.74384 -0.2948 0.0016 1.0000 52.000 0.8381 0.74948 0.74901 -0.2956 0.0015 1.0000 52.500 0.8293 0.75160 0.75115 -0.2965 0.0014 1.0000 53.000 0.8203 0.75263 0.75220 -0.2974 0.0012 1.0000 53.500 0.8110 0.75288 0.75247 -0.2983 0.0010 1.0000 54.000 0.8013 0.75170 0.75130 -0.2991 0.0009 1.0000 54.500 0.7915 0.75005 0.74967 -0.2999 0.0009 1.0000 55.000 0.7813 0.74707 0.74671 -0.3008 0.0008 1.0000 55.500 0.7709 0.74334 0.74299 -0.3016 0.0007 1.0000 56.000 0.7618 0.74802 0.74768 -0.3019 0.0007 1.0000 56.500 0.7518 0.74641 0.74609 -0.3024 0.0006 1.0000 57.000 0.7414 0.74352 0.74321 -0.3030 0.0005 1.0000 57.500 0.7308 0.73961 0.73931 -0.3035 0.0004 1.0000 59.000 0.6989 0.73004 0.72979 -0.3046 0.0003 1.0000 59.500 0.6881 0.72603 0.72580 -0.3049 0.0002 1.0000 60.000 0.6771 0.72069 0.72047 -0.3052 0.0001 1.0000