XFOIL Version 6.94 Calculated polar for: GOE 526 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 0.4259 0.01103 0.00399 -0.0822 0.7229 0.2517 0.500 0.4604 0.00969 0.00386 -0.0778 0.7078 0.6086 1.000 0.6630 0.00946 0.00427 -0.1066 0.6835 0.9947 1.500 0.7270 0.00944 0.00410 -0.1081 0.6591 1.0000 2.000 0.7689 0.00953 0.00405 -0.1049 0.6327 1.0000 2.500 0.8088 0.00967 0.00407 -0.1015 0.6004 1.0000 3.000 0.8462 0.00994 0.00413 -0.0975 0.5612 1.0000 3.500 0.8821 0.01034 0.00431 -0.0933 0.5216 1.0000 4.000 0.9182 0.01081 0.00460 -0.0892 0.4900 1.0000 4.500 0.9546 0.01131 0.00497 -0.0853 0.4645 1.0000 5.000 0.9916 0.01183 0.00539 -0.0814 0.4440 1.0000 5.500 1.0223 0.01238 0.00579 -0.0765 0.4126 1.0000 6.000 1.0500 0.01300 0.00623 -0.0710 0.3813 1.0000 6.500 1.0806 0.01351 0.00668 -0.0661 0.3564 1.0000 7.000 1.1009 0.01417 0.00717 -0.0593 0.3157 1.0000 7.500 1.1219 0.01481 0.00773 -0.0527 0.2834 1.0000 8.000 1.1344 0.01592 0.00857 -0.0452 0.2299 1.0000 8.500 1.1435 0.01755 0.00986 -0.0381 0.1790 1.0000 9.000 1.1585 0.01921 0.01133 -0.0323 0.1486 1.0000 9.500 1.1817 0.02061 0.01271 -0.0281 0.1298 1.0000 10.000 1.2033 0.02223 0.01424 -0.0241 0.1051 1.0000 10.500 1.2192 0.02436 0.01624 -0.0200 0.0812 1.0000 11.000 1.2314 0.02693 0.01871 -0.0161 0.0609 1.0000 11.500 1.2487 0.02932 0.02112 -0.0130 0.0506 1.0000 12.000 1.2655 0.03190 0.02374 -0.0104 0.0424 1.0000 12.500 1.2795 0.03485 0.02675 -0.0079 0.0358 1.0000 13.000 1.2874 0.03849 0.03042 -0.0057 0.0273 1.0000 13.500 1.2951 0.04238 0.03439 -0.0039 0.0208 1.0000 14.000 1.2871 0.04811 0.04012 -0.0024 0.0053 1.0000 14.500 1.2857 0.05358 0.04575 -0.0016 0.0039 1.0000 15.000 1.2866 0.05913 0.05151 -0.0015 0.0035 1.0000 15.500 1.2850 0.06527 0.05786 -0.0019 0.0033 1.0000 16.000 1.2821 0.07187 0.06468 -0.0028 0.0032 1.0000 16.500 1.2769 0.07900 0.07203 -0.0042 0.0032 1.0000 17.000 1.2697 0.08663 0.07990 -0.0060 0.0032 1.0000 17.500 1.2582 0.09509 0.08860 -0.0084 0.0031 1.0000 18.000 1.2461 0.10382 0.09757 -0.0111 0.0031 1.0000 18.500 1.2331 0.11292 0.10691 -0.0144 0.0031 1.0000 19.000 1.2173 0.12276 0.11699 -0.0183 0.0031 1.0000 19.500 1.2006 0.13308 0.12757 -0.0229 0.0031 1.0000 20.000 1.1822 0.14409 0.13883 -0.0283 0.0031 1.0000 20.500 1.1614 0.15605 0.15104 -0.0346 0.0031 1.0000 21.000 1.1402 0.16866 0.16391 -0.0417 0.0032 1.0000 21.500 1.1189 0.18175 0.17724 -0.0494 0.0032 1.0000 22.000 1.0935 0.19663 0.19235 -0.0582 0.0033 1.0000 22.500 1.0738 0.21097 0.20691 -0.0668 0.0034 1.0000 23.000 1.0612 0.22413 0.22023 -0.0747 0.0035 1.0000 23.500 1.0575 0.23501 0.23122 -0.0814 0.0036 1.0000 24.000 1.0599 0.24400 0.24028 -0.0872 0.0036 1.0000 24.500 1.0669 0.25145 0.24778 -0.0924 0.0036 1.0000 25.000 1.0762 0.25788 0.25426 -0.0971 0.0036 1.0000 25.500 1.0871 0.26364 0.26006 -0.1015 0.0036 1.0000 26.000 1.0987 0.26902 0.26549 -0.1059 0.0037 1.0000 26.500 1.1107 0.27411 0.27062 -0.1102 0.0036 1.0000 27.000 1.1223 0.27925 0.27583 -0.1146 0.0037 1.0000 27.500 1.1331 0.28464 0.28130 -0.1192 0.0038 1.0000 28.000 1.1417 0.29109 0.28786 -0.1243 0.0038 1.0000 28.500 1.1332 0.30892 0.30586 -0.1337 0.0044 1.0000 29.000 0.8600 0.36135 0.35926 -0.1386 0.0143 1.0000 29.500 0.8613 0.37337 0.37128 -0.1430 0.0140 1.0000 30.000 0.8657 0.38293 0.38088 -0.1466 0.0131 1.0000 30.500 0.8705 0.39136 0.38934 -0.1499 0.0124 1.0000 31.000 0.8752 0.39919 0.39720 -0.1532 0.0120 1.0000 31.500 0.8809 0.40629 0.40434 -0.1560 0.0117 1.0000 32.000 0.8824 0.41739 0.41546 -0.1599 0.0115 1.0000 32.500 0.8855 0.42688 0.42499 -0.1633 0.0111 1.0000 33.000 0.8886 0.43563 0.43377 -0.1666 0.0105 1.0000 33.500 0.8914 0.44381 0.44199 -0.1698 0.0101 1.0000 34.000 0.8940 0.45161 0.44982 -0.1729 0.0097 1.0000 34.500 0.8965 0.45887 0.45712 -0.1758 0.0096 1.0000 35.000 0.8980 0.46768 0.46596 -0.1790 0.0095 1.0000 35.500 0.8988 0.47717 0.47548 -0.1823 0.0094 1.0000 36.000 0.8998 0.48615 0.48450 -0.1855 0.0092 1.0000 36.500 0.9005 0.49443 0.49282 -0.1885 0.0090 1.0000 37.000 0.9009 0.50268 0.50110 -0.1915 0.0087 1.0000 37.500 0.9011 0.51061 0.50907 -0.1945 0.0084 1.0000 38.000 0.9008 0.51821 0.51671 -0.1974 0.0083 1.0000 38.500 0.9002 0.52569 0.52423 -0.2004 0.0080 1.0000 39.000 0.8993 0.53285 0.53143 -0.2032 0.0078 1.0000 39.500 0.8981 0.53940 0.53801 -0.2060 0.0076 1.0000 40.500 0.8945 0.55520 0.55388 -0.2116 0.0075 1.0000 41.000 0.8926 0.56374 0.56246 -0.2142 0.0071 1.0000 41.500 0.8902 0.57104 0.56979 -0.2169 0.0066 1.0000 42.000 0.8875 0.57772 0.57651 -0.2195 0.0062 1.0000 42.500 0.8843 0.58354 0.58237 -0.2221 0.0060 1.0000 43.000 0.8809 0.59097 0.58983 -0.2246 0.0058 1.0000 43.500 0.8777 0.59955 0.59844 -0.2270 0.0055 1.0000 44.000 0.8739 0.60632 0.60524 -0.2293 0.0051 1.0000 44.500 0.8698 0.61211 0.61107 -0.2317 0.0047 1.0000 45.000 0.8650 0.61673 0.61572 -0.2341 0.0045 1.0000 45.500 0.8604 0.62402 0.62304 -0.2363 0.0044 1.0000 46.000 0.8559 0.63153 0.63058 -0.2384 0.0041 1.0000 46.500 0.8508 0.63713 0.63621 -0.2406 0.0037 1.0000 47.000 0.8453 0.64185 0.64097 -0.2427 0.0034 1.0000 47.500 0.8391 0.64505 0.64419 -0.2449 0.0032 1.0000 48.000 0.8333 0.65132 0.65049 -0.2469 0.0031 1.0000 48.500 0.8277 0.65755 0.65675 -0.2487 0.0030 1.0000 49.000 0.8215 0.66235 0.66158 -0.2505 0.0027 1.0000 49.500 0.8148 0.66606 0.66531 -0.2524 0.0024 1.0000 50.000 0.8076 0.66835 0.66763 -0.2543 0.0022 1.0000 51.000 0.7930 0.67541 0.67474 -0.2578 0.0021 1.0000 51.500 0.7860 0.67956 0.67891 -0.2592 0.0020 1.0000 52.000 0.7786 0.68269 0.68208 -0.2608 0.0018 1.0000 52.500 0.7706 0.68454 0.68394 -0.2623 0.0016 1.0000 53.000 0.7623 0.68569 0.68512 -0.2638 0.0015 1.0000 53.500 0.7538 0.68610 0.68556 -0.2653 0.0013 1.0000 54.000 0.7447 0.68552 0.68500 -0.2669 0.0013 1.0000 55.000 0.7274 0.68838 0.68790 -0.2693 0.0012 1.0000 55.500 0.7187 0.68917 0.68872 -0.2705 0.0012 1.0000 56.000 0.7099 0.68951 0.68908 -0.2715 0.0011 1.0000 56.500 0.7006 0.68880 0.68839 -0.2726 0.0010 1.0000 57.000 0.6911 0.68745 0.68706 -0.2736 0.0009 1.0000 57.500 0.6814 0.68562 0.68525 -0.2746 0.0008 1.0000 58.000 0.6715 0.68321 0.68286 -0.2756 0.0007 1.0000 58.500 0.6614 0.68028 0.67995 -0.2765 0.0006 1.0000 59.000 0.6510 0.67646 0.67615 -0.2775 0.0006 1.0000 59.500 0.6402 0.67191 0.67162 -0.2784 0.0005 1.0000 60.000 0.6305 0.67060 0.67032 -0.2789 0.0005 1.0000