XFOIL Version 6.94 Calculated polar for: GOE 615 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 0.5782 0.01103 0.00404 -0.1069 0.6091 0.3945 0.500 0.7085 0.00988 0.00433 -0.1221 0.5935 1.0000 1.000 0.7552 0.01018 0.00437 -0.1200 0.5807 1.0000 1.500 0.8005 0.01041 0.00449 -0.1177 0.5681 1.0000 2.000 0.8473 0.01075 0.00465 -0.1157 0.5552 1.0000 2.500 0.8923 0.01101 0.00482 -0.1133 0.5418 1.0000 3.000 0.9374 0.01135 0.00505 -0.1110 0.5273 1.0000 3.500 0.9813 0.01171 0.00526 -0.1085 0.5099 1.0000 4.000 1.0203 0.01192 0.00546 -0.1049 0.4903 1.0000 4.500 1.0593 0.01221 0.00571 -0.1015 0.4689 1.0000 5.000 1.0829 0.01257 0.00583 -0.0950 0.4198 1.0000 5.500 1.0877 0.01353 0.00630 -0.0853 0.3513 1.0000 6.000 1.1008 0.01471 0.00714 -0.0778 0.3055 1.0000 6.500 1.1264 0.01567 0.00796 -0.0729 0.2783 1.0000 7.000 1.1473 0.01691 0.00897 -0.0676 0.2424 1.0000 7.500 1.1714 0.01815 0.01006 -0.0631 0.2148 1.0000 8.000 1.1836 0.02012 0.01170 -0.0576 0.1664 1.0000 8.500 1.1937 0.02247 0.01377 -0.0525 0.1226 1.0000 9.000 1.1758 0.02699 0.01783 -0.0455 0.0489 1.0000 9.500 1.1968 0.02920 0.02007 -0.0427 0.0406 1.0000 10.000 1.2019 0.03283 0.02360 -0.0393 0.0051 1.0000 10.500 1.2212 0.03551 0.02642 -0.0372 0.0045 1.0000 11.000 1.2385 0.03853 0.02957 -0.0354 0.0043 1.0000 11.500 1.2526 0.04199 0.03321 -0.0338 0.0042 1.0000 12.000 1.2643 0.04591 0.03730 -0.0325 0.0042 1.0000 12.500 1.2724 0.05040 0.04198 -0.0315 0.0042 1.0000 13.000 1.2774 0.05544 0.04723 -0.0309 0.0042 1.0000 13.500 1.2790 0.06112 0.05312 -0.0307 0.0043 1.0000 14.000 1.2776 0.06734 0.05956 -0.0309 0.0043 1.0000 14.500 1.2732 0.07414 0.06659 -0.0314 0.0044 1.0000 15.000 1.2665 0.08143 0.07411 -0.0323 0.0044 1.0000 15.500 1.2565 0.08947 0.08239 -0.0336 0.0045 1.0000 16.000 1.2458 0.09786 0.09102 -0.0355 0.0046 1.0000 16.500 1.2347 0.10661 0.10000 -0.0378 0.0046 1.0000 17.000 1.2220 0.11587 0.10949 -0.0407 0.0047 1.0000 17.500 1.2086 0.12548 0.11933 -0.0441 0.0047 1.0000 18.000 1.1944 0.13546 0.12953 -0.0481 0.0048 1.0000 18.500 1.1813 0.14544 0.13972 -0.0526 0.0048 1.0000 19.000 1.1743 0.15444 0.14889 -0.0568 0.0049 1.0000 19.500 1.1705 0.16295 0.15756 -0.0610 0.0050 1.0000 20.000 1.1702 0.17080 0.16556 -0.0651 0.0052 1.0000 20.500 1.1684 0.17896 0.17387 -0.0696 0.0053 1.0000 21.000 1.1687 0.18668 0.18169 -0.0740 0.0054 1.0000 21.500 1.1754 0.19278 0.18783 -0.0776 0.0057 1.0000 22.000 1.1902 0.19667 0.19167 -0.0800 0.0060 1.0000 22.500 1.2216 0.19600 0.19082 -0.0795 0.0063 1.0000 23.000 1.2289 0.20225 0.19725 -0.0835 0.0066 1.0000 23.500 1.2486 0.20502 0.20011 -0.0854 0.0072 1.0000 24.000 1.2946 0.20042 0.19531 -0.0821 0.0079 1.0000 24.500 1.2947 0.20852 0.20374 -0.0878 0.0085 1.0000 25.000 1.3435 0.20334 0.19844 -0.0840 0.0096 1.0000 25.500 1.3333 0.21387 0.20940 -0.0916 0.0104 1.0000 26.000 1.3648 0.21318 0.20878 -0.0912 0.0117 1.0000 26.500 1.3477 0.22519 0.22123 -0.1001 0.0123 1.0000 27.000 1.3588 0.22979 0.22608 -0.1036 0.0139 1.0000 27.500 1.3248 0.24686 0.24361 -0.1161 0.0142 1.0000 28.000 0.9149 0.36758 0.36565 -0.1593 0.0230 1.0000 28.500 0.9226 0.37411 0.37221 -0.1618 0.0214 1.0000 29.000 0.9239 0.38565 0.38377 -0.1658 0.0191 1.0000 29.500 0.9271 0.39575 0.39390 -0.1692 0.0175 1.0000 30.000 0.9320 0.40329 0.40147 -0.1721 0.0161 1.0000 30.500 0.9337 0.41486 0.41306 -0.1756 0.0147 1.0000 31.000 0.9382 0.42220 0.42043 -0.1784 0.0137 1.0000 31.500 0.9392 0.43387 0.43212 -0.1819 0.0128 1.0000 32.000 0.9418 0.44304 0.44133 -0.1850 0.0119 1.0000 32.500 0.9454 0.44966 0.44799 -0.1876 0.0115 1.0000 33.000 0.9453 0.46279 0.46114 -0.1911 0.0108 1.0000 33.500 0.9467 0.47206 0.47044 -0.1940 0.0102 1.0000 34.000 0.9483 0.48037 0.47878 -0.1969 0.0098 1.0000 34.500 0.9503 0.48697 0.48543 -0.1994 0.0095 1.0000 35.000 0.9494 0.49884 0.49731 -0.2026 0.0094 1.0000 35.500 0.9493 0.50887 0.50738 -0.2056 0.0092 1.0000 36.000 0.9491 0.51841 0.51695 -0.2084 0.0087 1.0000 36.500 0.9488 0.52721 0.52579 -0.2112 0.0084 1.0000 37.000 0.9481 0.53534 0.53395 -0.2138 0.0081 1.0000 37.500 0.9471 0.54333 0.54197 -0.2165 0.0080 1.0000 38.000 0.9461 0.55023 0.54892 -0.2190 0.0078 1.0000 39.000 0.9422 0.56707 0.56582 -0.2242 0.0077 1.0000 39.500 0.9396 0.57597 0.57475 -0.2268 0.0077 1.0000 40.000 0.9368 0.58448 0.58330 -0.2293 0.0077 1.0000 40.500 0.9341 0.59327 0.59212 -0.2318 0.0074 1.0000 41.000 0.9309 0.60112 0.60001 -0.2342 0.0071 1.0000 41.500 0.9275 0.60846 0.60738 -0.2365 0.0068 1.0000 42.000 0.9237 0.61489 0.61386 -0.2388 0.0065 1.0000 42.500 0.9195 0.61998 0.61899 -0.2410 0.0063 1.0000 43.000 0.9152 0.62840 0.62742 -0.2432 0.0062 1.0000 43.500 0.9110 0.63777 0.63683 -0.2453 0.0059 1.0000 44.000 0.9063 0.64463 0.64372 -0.2474 0.0055 1.0000 44.500 0.9011 0.65031 0.64943 -0.2494 0.0051 1.0000 45.000 0.8955 0.65486 0.65401 -0.2515 0.0049 1.0000 45.500 0.8898 0.66118 0.66036 -0.2534 0.0048 1.0000 46.000 0.8845 0.66997 0.66917 -0.2552 0.0046 1.0000 46.500 0.8786 0.67598 0.67521 -0.2570 0.0043 1.0000 47.000 0.8723 0.68061 0.67987 -0.2588 0.0039 1.0000 47.500 0.8655 0.68424 0.68353 -0.2606 0.0037 1.0000 48.500 0.8517 0.69467 0.69401 -0.2639 0.0036 1.0000 49.000 0.8450 0.70047 0.69983 -0.2653 0.0033 1.0000 49.500 0.8376 0.70409 0.70348 -0.2668 0.0030 1.0000 50.000 0.8298 0.70687 0.70629 -0.2683 0.0028 1.0000 50.500 0.8215 0.70820 0.70765 -0.2699 0.0026 1.0000 51.500 0.8050 0.71406 0.71355 -0.2726 0.0025 1.0000 52.000 0.7974 0.71859 0.71810 -0.2736 0.0024 1.0000 52.500 0.7890 0.72078 0.72031 -0.2748 0.0022 1.0000 53.000 0.7802 0.72188 0.72144 -0.2760 0.0020 1.0000 53.500 0.7711 0.72232 0.72190 -0.2771 0.0018 1.0000 54.000 0.7617 0.72190 0.72150 -0.2782 0.0017 1.0000 54.500 0.7517 0.72023 0.71986 -0.2793 0.0016 1.0000 56.000 0.7231 0.72027 0.71995 -0.2819 0.0016 1.0000 56.500 0.7135 0.71965 0.71935 -0.2826 0.0015 1.0000 57.000 0.7037 0.71835 0.71806 -0.2833 0.0014 1.0000 57.500 0.6936 0.71613 0.71587 -0.2839 0.0013 1.0000 58.000 0.6833 0.71341 0.71317 -0.2845 0.0012 1.0000 58.500 0.6727 0.71005 0.70982 -0.2851 0.0011 1.0000 59.000 0.6620 0.70595 0.70574 -0.2856 0.0010 1.0000 59.500 0.6511 0.70146 0.70127 -0.2861 0.0009 1.0000 60.000 0.6400 0.69623 0.69606 -0.2866 0.0008 1.0000