XFOIL Version 6.96 Calculated polar for: GOE 738 AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.000 -0.9962 0.12258 0.11933 0.0002 1.0000 0.0285 -18.750 -1.0321 0.11139 0.10795 -0.0069 1.0000 0.0287 -18.500 -1.0607 0.10197 0.09838 -0.0129 1.0000 0.0288 -18.250 -1.0859 0.09350 0.08976 -0.0182 1.0000 0.0290 -18.000 -1.1086 0.08569 0.08181 -0.0231 1.0000 0.0292 -17.750 -1.1287 0.07857 0.07454 -0.0275 1.0000 0.0293 -17.500 -1.1460 0.07199 0.06782 -0.0316 1.0000 0.0295 -17.250 -1.1621 0.06591 0.06160 -0.0353 1.0000 0.0296 -17.000 -1.1743 0.06055 0.05611 -0.0384 1.0000 0.0298 -16.750 -1.1837 0.05577 0.05118 -0.0412 1.0000 0.0300 -16.500 -1.1918 0.05142 0.04669 -0.0435 1.0000 0.0302 -16.250 -1.1971 0.04763 0.04277 -0.0452 1.0000 0.0303 -16.000 -1.2003 0.04432 0.03933 -0.0465 1.0000 0.0305 -15.750 -1.2032 0.04127 0.03618 -0.0474 1.0000 0.0307 -15.500 -1.2060 0.03847 0.03330 -0.0478 1.0000 0.0309 -15.250 -1.2063 0.03609 0.03086 -0.0478 1.0000 0.0312 -15.000 -1.2046 0.03407 0.02877 -0.0475 1.0000 0.0314 -14.750 -1.2021 0.03224 0.02687 -0.0468 1.0000 0.0316 -14.500 -1.1966 0.03078 0.02535 -0.0459 1.0000 0.0320 -14.250 -1.1902 0.02946 0.02397 -0.0447 1.0000 0.0323 -14.000 -1.1832 0.02826 0.02270 -0.0433 1.0000 0.0326 -13.750 -1.1756 0.02716 0.02153 -0.0417 1.0000 0.0329 -13.500 -1.1667 0.02618 0.02049 -0.0400 1.0000 0.0332 -13.250 -1.1411 0.02518 0.01933 -0.0414 0.8991 0.0337 -13.000 -1.1324 0.02455 0.01847 -0.0389 0.8519 0.0340 -12.750 -1.1231 0.02392 0.01768 -0.0364 0.8297 0.0343 -12.500 -1.1125 0.02330 0.01692 -0.0340 0.8140 0.0347 -12.250 -1.1007 0.02273 0.01622 -0.0317 0.8010 0.0350 -12.000 -1.0910 0.02205 0.01548 -0.0290 0.7895 0.0354 -11.750 -1.0779 0.02150 0.01486 -0.0268 0.7800 0.0359 -11.500 -1.0613 0.02097 0.01426 -0.0251 0.7708 0.0364 -11.250 -1.0434 0.02047 0.01369 -0.0236 0.7628 0.0369 -11.000 -1.0244 0.01998 0.01313 -0.0222 0.7548 0.0374 -10.500 -0.9845 0.01906 0.01205 -0.0197 0.7403 0.0386 -10.250 -0.9635 0.01862 0.01153 -0.0186 0.7331 0.0392 -10.000 -0.9419 0.01822 0.01104 -0.0175 0.7267 0.0397 -9.750 -0.9210 0.01771 0.01050 -0.0164 0.7199 0.0405 -9.500 -0.8991 0.01729 0.01004 -0.0154 0.7134 0.0413 -9.250 -0.8762 0.01692 0.00962 -0.0145 0.7074 0.0422 -9.000 -0.8527 0.01656 0.00922 -0.0137 0.7009 0.0432 -8.750 -0.8290 0.01624 0.00882 -0.0128 0.6945 0.0443 -8.500 -0.8050 0.01592 0.00843 -0.0121 0.6888 0.0451 -8.250 -0.7814 0.01552 0.00802 -0.0113 0.6824 0.0463 -8.000 -0.7572 0.01520 0.00766 -0.0106 0.6763 0.0476 -7.750 -0.7325 0.01490 0.00732 -0.0099 0.6708 0.0489 -7.500 -0.7073 0.01462 0.00700 -0.0093 0.6644 0.0504 -7.250 -0.6822 0.01435 0.00668 -0.0087 0.6583 0.0519 -7.000 -0.6572 0.01405 0.00637 -0.0081 0.6530 0.0538 -6.750 -0.6315 0.01379 0.00610 -0.0075 0.6471 0.0559 -6.500 -0.6055 0.01358 0.00583 -0.0070 0.6408 0.0579 -6.250 -0.5801 0.01331 0.00554 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0.00238 0.0012 0.5135 0.2734 -1.000 -0.0212 0.00961 0.00232 0.0016 0.5078 0.3082 -0.750 0.0048 0.00939 0.00225 0.0020 0.5014 0.3505 -0.500 0.0301 0.00917 0.00219 0.0026 0.4951 0.4020 -0.250 0.0552 0.00894 0.00216 0.0032 0.4898 0.4581 0.000 0.0797 0.00870 0.00214 0.0040 0.4839 0.5226 0.250 0.1045 0.00854 0.00213 0.0047 0.4773 0.5745 0.500 0.1304 0.00843 0.00213 0.0053 0.4706 0.6114 0.750 0.1564 0.00836 0.00214 0.0059 0.4629 0.6438 1.000 0.1823 0.00832 0.00216 0.0065 0.4569 0.6751 1.250 0.2087 0.00825 0.00220 0.0070 0.4517 0.7046 1.500 0.2352 0.00823 0.00224 0.0075 0.4462 0.7332 1.750 0.2615 0.00821 0.00229 0.0081 0.4409 0.7600 2.000 0.2885 0.00820 0.00235 0.0085 0.4359 0.7835 2.250 0.3157 0.00820 0.00240 0.0088 0.4302 0.8051 2.500 0.3428 0.00819 0.00248 0.0093 0.4245 0.8359 2.750 0.3730 0.00818 0.00259 0.0091 0.4190 0.8738 3.000 0.4111 0.00824 0.00273 0.0072 0.4122 0.9062 3.250 0.4537 0.00840 0.00287 0.0043 0.4050 0.9250 3.500 0.4922 0.00851 0.00299 0.0023 0.3974 0.9357 4.000 0.5648 0.00882 0.00323 -0.0011 0.3770 0.9494 4.250 0.5972 0.00899 0.00336 -0.0020 0.3658 0.9560 4.500 0.6305 0.00920 0.00350 -0.0031 0.3527 0.9613 4.750 0.6592 0.00943 0.00366 -0.0034 0.3355 0.9685 5.000 0.6935 0.00969 0.00384 -0.0048 0.3167 0.9720 5.250 0.7253 0.00999 0.00405 -0.0058 0.2971 0.9767 5.500 0.7550 0.01034 0.00430 -0.0064 0.2784 0.9817 5.750 0.7891 0.01066 0.00453 -0.0080 0.2636 0.9846 6.000 0.8217 0.01099 0.00479 -0.0093 0.2503 0.9882 6.250 0.8534 0.01132 0.00506 -0.0103 0.2406 0.9918 6.500 0.8873 0.01156 0.00529 -0.0118 0.2335 0.9945 6.750 0.9217 0.01185 0.00555 -0.0135 0.2256 0.9973 7.000 0.9564 0.01212 0.00580 -0.0152 0.2193 0.9996 7.250 0.9805 0.01236 0.00604 -0.0147 0.2138 1.0000 7.500 1.0012 0.01265 0.00632 -0.0135 0.2088 1.0000 7.750 1.0219 0.01293 0.00659 -0.0124 0.2044 1.0000 8.000 1.0430 0.01318 0.00686 -0.0113 0.1983 1.0000 8.250 1.0627 0.01353 0.00718 -0.0100 0.1918 1.0000 8.500 1.0830 0.01381 0.00748 -0.0088 0.1865 1.0000 8.750 1.1026 0.01414 0.00780 -0.0076 0.1788 1.0000 9.000 1.1212 0.01452 0.00815 -0.0062 0.1706 1.0000 9.250 1.1381 0.01496 0.00856 -0.0047 0.1590 1.0000 9.500 1.1522 0.01554 0.00905 -0.0028 0.1434 1.0000 9.750 1.1636 0.01621 0.00964 -0.0005 0.1300 1.0000 10.000 1.1733 0.01690 0.01029 0.0019 0.1202 1.0000 10.250 1.1810 0.01760 0.01096 0.0046 0.1128 1.0000 10.500 1.1817 0.01833 0.01170 0.0083 0.1077 1.0000 10.750 1.1859 0.01922 0.01260 0.0108 0.1025 1.0000 11.000 1.1903 0.02036 0.01374 0.0128 0.0973 1.0000 11.250 1.1992 0.02139 0.01480 0.0141 0.0920 1.0000 11.500 1.2054 0.02270 0.01611 0.0154 0.0861 1.0000 11.750 1.2133 0.02398 0.01740 0.0164 0.0806 1.0000 12.000 1.2196 0.02545 0.01886 0.0173 0.0760 1.0000 12.250 1.2264 0.02694 0.02037 0.0181 0.0723 1.0000 12.500 1.2328 0.02851 0.02196 0.0188 0.0698 1.0000 12.750 1.2391 0.03014 0.02362 0.0194 0.0677 1.0000 13.000 1.2460 0.03176 0.02528 0.0200 0.0663 1.0000 13.250 1.2513 0.03354 0.02711 0.0204 0.0647 1.0000 13.500 1.2561 0.03542 0.02903 0.0208 0.0635 1.0000 13.750 1.2590 0.03751 0.03116 0.0210 0.0622 1.0000 14.000 1.2598 0.03986 0.03355 0.0212 0.0607 1.0000 14.250 1.2647 0.04185 0.03561 0.0214 0.0597 1.0000 14.500 1.2687 0.04396 0.03778 0.0214 0.0589 1.0000 14.750 1.2721 0.04623 0.04011 0.0213 0.0576 1.0000 15.000 1.2747 0.04864 0.04259 0.0212 0.0570 1.0000 15.250 1.2759 0.05125 0.04526 0.0209 0.0561 1.0000 15.500 1.2767 0.05398 0.04804 0.0205 0.0554 1.0000 15.750 1.2772 0.05677 0.05089 0.0201 0.0549 1.0000 16.000 1.2735 0.06010 0.05426 0.0195 0.0537 1.0000 16.250 1.2731 0.06310 0.05733 0.0189 0.0530 1.0000 16.500 1.2759 0.06574 0.06005 0.0183 0.0525 1.0000 16.750 1.2767 0.06866 0.06305 0.0177 0.0520 1.0000 17.000 1.2776 0.07157 0.06604 0.0170 0.0514 1.0000 17.250 1.2783 0.07458 0.06912 0.0163 0.0508 1.0000 17.500 1.2776 0.07779 0.07241 0.0154 0.0503 1.0000 17.750 1.2769 0.08102 0.07570 0.0145 0.0494 1.0000 18.000 1.2740 0.08459 0.07933 0.0134 0.0486 1.0000 18.250 1.2708 0.08826 0.08305 0.0123 0.0478 1.0000 18.500 1.2671 0.09201 0.08686 0.0110 0.0472 1.0000