XFOIL Version 6.94 Calculated polar for: GOE 604 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 ------- -------- --------- --------- -------- ------- ------- 0.500 0.5119 0.00284 -0.00319 -0.0654 0.4655 0.8698 1.000 0.6068 0.00289 -0.00319 -0.0728 0.4526 0.9506 1.500 0.6960 0.00301 -0.00327 -0.0795 0.4403 0.9783 2.000 0.7919 0.00300 -0.00345 -0.0880 0.4274 0.9977 2.500 0.8378 0.00317 -0.00340 -0.0867 0.4173 1.0000 3.000 0.8726 0.00334 -0.00330 -0.0831 0.4082 1.0000 3.500 0.9108 0.00367 -0.00316 -0.0802 0.3998 1.0000 4.000 0.9471 0.00390 -0.00288 -0.0769 0.3930 1.0000 4.500 0.9847 0.00417 -0.00267 -0.0739 0.3859 1.0000 5.000 1.0261 0.00460 -0.00238 -0.0716 0.3785 1.0000 5.500 1.0610 0.00486 -0.00204 -0.0681 0.3724 1.0000 6.000 1.0841 0.00499 -0.00207 -0.0625 0.3564 1.0000 6.500 1.0984 0.00507 -0.00196 -0.0553 0.3436 1.0000 7.000 1.1082 0.00525 -0.00185 -0.0480 0.3251 1.0000 7.500 1.1309 0.00570 -0.00147 -0.0434 0.3161 1.0000 8.000 1.1535 0.00609 -0.00100 -0.0392 0.3042 1.0000 8.500 1.1677 0.00679 -0.00030 -0.0344 0.2885 1.0000 9.000 1.1814 0.00783 0.00073 -0.0302 0.2766 1.0000 9.500 1.1902 0.00935 0.00228 -0.0262 0.2593 1.0000 10.000 1.1830 0.01223 0.00513 -0.0219 0.2276 1.0000 10.500 1.1521 0.01799 0.01079 -0.0177 0.1875 1.0000 11.000 1.1259 0.02506 0.01787 -0.0151 0.1681 1.0000 11.500 1.1023 0.03300 0.02588 -0.0132 0.1553 1.0000 12.000 1.0865 0.04085 0.03384 -0.0121 0.1457 1.0000 12.500 1.0673 0.04965 0.04274 -0.0115 0.1356 1.0000 13.000 1.0512 0.05841 0.05160 -0.0113 0.1279 1.0000 14.000 1.0241 0.07557 0.06896 -0.0123 0.1065 1.0000 14.500 0.9885 0.08712 0.08047 -0.0142 0.0747 1.0000 15.000 0.9461 0.09916 0.09245 -0.0170 0.0376 1.0000 15.500 0.9138 0.10925 0.10256 -0.0204 0.0042 1.0000 16.000 0.9074 0.11477 0.10829 -0.0231 0.0034 1.0000 16.500 0.9029 0.11985 0.11359 -0.0261 0.0033 1.0000 17.000 0.8992 0.12534 0.11930 -0.0293 0.0032 1.0000 17.500 0.8948 0.13120 0.12536 -0.0329 0.0031 1.0000 18.000 0.8894 0.13744 0.13183 -0.0369 0.0031 1.0000 18.500 0.8824 0.14414 0.13875 -0.0411 0.0031 1.0000 19.000 0.8745 0.15121 0.14604 -0.0457 0.0030 1.0000 19.500 0.8672 0.15849 0.15353 -0.0504 0.0031 1.0000 20.000 0.8622 0.16563 0.16086 -0.0551 0.0031 1.0000 20.500 0.8599 0.17243 0.16784 -0.0596 0.0031 1.0000 21.000 0.8603 0.17887 0.17442 -0.0638 0.0031 1.0000 21.500 0.8626 0.18505 0.18075 -0.0679 0.0031 1.0000 22.000 0.8652 0.19125 0.18709 -0.0720 0.0032 1.0000 22.500 0.8681 0.19749 0.19347 -0.0761 0.0032 1.0000 23.000 0.8710 0.20382 0.19992 -0.0802 0.0032 1.0000 23.500 0.8749 0.20996 0.20617 -0.0842 0.0033 1.0000 24.000 0.8801 0.21583 0.21213 -0.0881 0.0033 1.0000 24.500 0.8882 0.22082 0.21718 -0.0916 0.0034 1.0000 25.000 0.9005 0.22445 0.22083 -0.0946 0.0035 1.0000 25.500 0.9167 0.22670 0.22308 -0.0970 0.0036 1.0000 26.000 0.9375 0.22743 0.22377 -0.0988 0.0036 1.0000 26.500 0.9594 0.22762 0.22393 -0.1003 0.0037 1.0000 27.000 0.9646 0.23308 0.22954 -0.1041 0.0038 1.0000 27.500 0.9688 0.23882 0.23545 -0.1080 0.0040 1.0000 28.000 0.9752 0.24386 0.24067 -0.1114 0.0042 1.0000 28.500 0.9786 0.24971 0.24670 -0.1152 0.0044 1.0000 29.000 0.9787 0.25666 0.25383 -0.1193 0.0047 1.0000 29.500 0.9821 0.26235 0.25965 -0.1228 0.0049 1.0000 30.000 0.9631 0.27727 0.27487 -0.1293 0.0051 1.0000 30.500 0.8518 0.36941 0.36745 -0.1445 0.0180 1.0000 31.000 0.8530 0.38112 0.37919 -0.1482 0.0167 1.0000 31.500 0.8570 0.38940 0.38749 -0.1515 0.0154 1.0000 32.000 0.8642 0.39477 0.39290 -0.1541 0.0148 1.0000 32.500 0.8623 0.40875 0.40689 -0.1582 0.0132 1.0000 33.000 0.8666 0.41563 0.41381 -0.1612 0.0125 1.0000 33.500 0.8717 0.42199 0.42020 -0.1639 0.0122 1.0000 34.000 0.8696 0.43590 0.43412 -0.1678 0.0109 1.0000 34.500 0.8725 0.44292 0.44118 -0.1708 0.0103 1.0000 35.000 0.8771 0.44800 0.44630 -0.1733 0.0100 1.0000 35.500 0.8744 0.46237 0.46068 -0.1771 0.0094 1.0000 36.000 0.8755 0.47093 0.46927 -0.1801 0.0088 1.0000 36.500 0.8767 0.47839 0.47676 -0.1830 0.0084 1.0000 37.000 0.8781 0.48438 0.48278 -0.1857 0.0081 1.0000 37.500 0.8788 0.49196 0.49040 -0.1885 0.0080 1.0000 38.000 0.8768 0.50366 0.50212 -0.1917 0.0078 1.0000 38.500 0.8762 0.51231 0.51080 -0.1945 0.0075 1.0000 39.000 0.8754 0.52006 0.51858 -0.1973 0.0072 1.0000 39.500 0.8745 0.52750 0.52606 -0.2001 0.0069 1.0000 40.000 0.8732 0.53434 0.53293 -0.2028 0.0068 1.0000 40.500 0.8717 0.54061 0.53923 -0.2054 0.0066 1.0000 41.000 0.8702 0.54610 0.54475 -0.2080 0.0065 1.0000 41.500 0.8686 0.55131 0.55000 -0.2104 0.0064 1.0000 42.000 0.8653 0.55914 0.55785 -0.2130 0.0064 1.0000 42.500 0.8620 0.56670 0.56544 -0.2156 0.0064 1.0000 43.000 0.8586 0.57386 0.57264 -0.2182 0.0063 1.0000 43.500 0.8551 0.58055 0.57936 -0.2206 0.0062 1.0000 44.000 0.8513 0.58660 0.58544 -0.2229 0.0061 1.0000 44.500 0.8475 0.59262 0.59149 -0.2253 0.0059 1.0000 45.000 0.8432 0.59787 0.59678 -0.2275 0.0056 1.0000 45.500 0.8387 0.60268 0.60161 -0.2297 0.0054 1.0000 46.000 0.8340 0.60660 0.60556 -0.2319 0.0051 1.0000 46.500 0.8290 0.60933 0.60833 -0.2340 0.0050 1.0000 47.000 0.8236 0.61494 0.61396 -0.2361 0.0049 1.0000 47.500 0.8181 0.62179 0.62085 -0.2380 0.0048 1.0000 48.000 0.8125 0.62654 0.62562 -0.2399 0.0044 1.0000 48.500 0.8066 0.63011 0.62922 -0.2418 0.0041 1.0000 49.000 0.8003 0.63268 0.63182 -0.2437 0.0039 1.0000 49.500 0.7937 0.63424 0.63341 -0.2456 0.0038 1.0000 50.500 0.7804 0.64291 0.64212 -0.2489 0.0036 1.0000 51.000 0.7734 0.64586 0.64510 -0.2504 0.0033 1.0000 51.500 0.7661 0.64769 0.64695 -0.2520 0.0031 1.0000 52.000 0.7586 0.64872 0.64800 -0.2536 0.0029 1.0000 52.500 0.7506 0.64849 0.64780 -0.2551 0.0027 1.0000 53.500 0.7346 0.65132 0.65067 -0.2578 0.0026 1.0000 54.000 0.7268 0.65340 0.65277 -0.2590 0.0025 1.0000 54.500 0.7185 0.65381 0.65321 -0.2602 0.0023 1.0000 55.000 0.7099 0.65314 0.65256 -0.2614 0.0021 1.0000 55.500 0.7010 0.65159 0.65103 -0.2626 0.0019 1.0000 56.000 0.6918 0.64900 0.64846 -0.2638 0.0018 1.0000 56.500 0.6823 0.64545 0.64494 -0.2650 0.0018 1.0000 57.500 0.6642 0.64488 0.64440 -0.2666 0.0017 1.0000 58.000 0.6551 0.64367 0.64320 -0.2673 0.0017 1.0000 58.500 0.6457 0.64111 0.64066 -0.2681 0.0016 1.0000 59.000 0.6359 0.63785 0.63742 -0.2688 0.0014 1.0000 59.500 0.6260 0.63389 0.63348 -0.2695 0.0013 1.0000 60.000 0.6160 0.62941 0.62902 -0.2702 0.0012 1.0000