XFOIL Version 6.96 Calculated polar for: GOE 8K AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -14.000 -0.3615 0.03654 0.03407 -0.2187 0.9434 0.0127 -13.750 -0.3990 0.03116 0.02844 -0.2195 0.9349 0.0130 -13.500 -0.3994 0.02761 0.02461 -0.2221 0.9325 0.0131 -13.250 -0.3870 0.02489 0.02161 -0.2246 0.9308 0.0133 -13.000 -0.4043 0.02416 0.02077 -0.2174 0.9237 0.0134 -12.750 -0.3918 0.02272 0.01914 -0.2170 0.9212 0.0136 -12.500 -0.3710 0.02147 0.01770 -0.2178 0.9193 0.0139 -12.250 -0.3681 0.02060 0.01668 -0.2142 0.9155 0.0140 -12.000 -0.3861 0.01946 0.01536 -0.2063 0.9098 0.0143 -11.750 -0.3717 0.01830 0.01406 -0.2050 0.9072 0.0148 -11.500 -0.3430 0.01762 0.01329 -0.2064 0.9056 0.0153 -11.250 -0.3115 0.01698 0.01255 -0.2084 0.9040 0.0160 -11.000 -0.3319 0.01685 0.01238 -0.1983 0.8987 0.0159 -10.750 -0.3168 0.01631 0.01174 -0.1963 0.8960 0.0165 -10.500 -0.2966 0.01573 0.01103 -0.1955 0.8939 0.0169 -10.250 -0.2694 0.01510 0.01025 -0.1962 0.8921 0.0175 -10.000 -0.2399 0.01425 0.00929 -0.1976 0.8904 0.0184 -9.750 -0.2536 0.01420 0.00924 -0.1887 0.8858 0.0188 -9.500 -0.2423 0.01385 0.00882 -0.1855 0.8827 0.0192 -9.250 -0.2198 0.01353 0.00844 -0.1848 0.8806 0.0201 -9.000 -0.1944 0.01317 0.00798 -0.1848 0.8787 0.0209 -8.750 -0.1649 0.01261 0.00732 -0.1858 0.8771 0.0220 -8.500 -0.1303 0.01237 0.00706 -0.1879 0.8755 0.0232 -8.250 -0.1512 0.01236 0.00704 -0.1771 0.8706 0.0235 -8.000 -0.1336 0.01219 0.00684 -0.1751 0.8680 0.0244 -7.750 -0.1092 0.01201 0.00658 -0.1747 0.8659 0.0254 -7.500 -0.0837 0.01164 0.00618 -0.1746 0.8639 0.0271 -7.250 -0.0466 0.01158 0.00610 -0.1770 0.8623 0.0288 -7.000 -0.0374 0.01161 0.00612 -0.1730 0.8591 0.0300 -6.750 -0.0326 0.01153 0.00600 -0.1680 0.8554 0.0305 -6.500 -0.0140 0.01130 0.00574 -0.1663 0.8527 0.0320 -6.250 0.0121 0.01134 0.00578 -0.1661 0.8506 0.0333 -6.000 0.0441 0.01135 0.00577 -0.1674 0.8489 0.0348 -5.750 0.0818 0.01137 0.00574 -0.1699 0.8472 0.0364 -5.500 0.0759 0.01143 0.00578 -0.1624 0.8430 0.0367 -5.250 0.0867 0.01109 0.00541 -0.1589 0.8396 0.0383 -5.000 0.1082 0.01101 0.00533 -0.1577 0.8370 0.0393 -4.750 0.1366 0.01091 0.00520 -0.1581 0.8350 0.0405 -4.500 0.1724 0.01085 0.00509 -0.1603 0.8332 0.0423 -4.250 0.1737 0.01090 0.00514 -0.1544 0.8292 0.0431 -4.000 0.1869 0.01085 0.00505 -0.1513 0.8257 0.0438 -3.750 0.2072 0.01071 0.00487 -0.1498 0.8229 0.0448 -3.500 0.2320 0.01022 0.00438 -0.1495 0.8206 0.0468 -3.250 0.2659 0.01006 0.00420 -0.1513 0.8187 0.0483 -3.000 0.2710 0.01009 0.00423 -0.1463 0.8150 0.0494 -2.750 0.2830 0.00998 0.00411 -0.1429 0.8115 0.0502 -2.500 0.3020 0.00986 0.00397 -0.1412 0.8087 0.0513 -2.250 0.3291 0.00975 0.00383 -0.1412 0.8066 0.0525 -2.000 0.3626 0.00963 0.00368 -0.1429 0.8047 0.0534 -1.750 0.3728 0.00956 0.00360 -0.1391 0.8015 0.0542 -1.500 0.3824 0.00937 0.00340 -0.1351 0.7981 0.0551 -1.250 0.4002 0.00921 0.00322 -0.1331 0.7953 0.0563 -1.000 0.4239 0.00908 0.00307 -0.1324 0.7930 0.0576 -0.750 0.4543 0.00896 0.00294 -0.1333 0.7910 0.0590 -0.500 0.4825 0.00889 0.00285 -0.1337 0.7889 0.0606 -0.250 0.4915 0.00892 0.00289 -0.1296 0.7859 0.0618 0.000 0.5097 0.00890 0.00287 -0.1277 0.7833 0.0625 0.250 0.5313 0.00888 0.00284 -0.1266 0.7810 0.0639 0.500 0.5562 0.00885 0.00281 -0.1262 0.7790 0.0649 0.750 0.5876 0.00875 0.00269 -0.1273 0.7768 0.0686 1.000 0.6150 0.00873 0.00266 -0.1274 0.7742 0.0715 1.250 0.6193 0.00879 0.00276 -0.1223 0.7703 0.0756 1.500 0.6381 0.00879 0.00279 -0.1206 0.7671 0.0883 1.750 0.9463 0.00759 0.00399 -0.1875 0.7748 0.9899 2.000 1.0059 0.00770 0.00411 -0.1952 0.7735 0.9960 2.250 1.0480 0.00770 0.00413 -0.1990 0.7711 0.9994 2.500 1.0691 0.00774 0.00417 -0.1979 0.7681 1.0000 2.750 1.0855 0.00778 0.00421 -0.1957 0.7645 1.0000 3.000 1.1162 0.00780 0.00418 -0.1967 0.7606 1.0000 3.250 1.1067 0.00797 0.00439 -0.1885 0.7542 1.0000 3.500 1.1209 0.00805 0.00444 -0.1857 0.7485 1.0000 3.750 1.1411 0.00813 0.00451 -0.1844 0.7444 1.0000 4.000 1.1441 0.00830 0.00472 -0.1791 0.7384 1.0000 4.250 1.1613 0.00841 0.00479 -0.1770 0.7324 1.0000 4.500 1.1749 0.00855 0.00496 -0.1742 0.7282 1.0000 4.750 1.1809 0.00875 0.00516 -0.1696 0.7197 1.0000 5.000 1.1912 0.00896 0.00537 -0.1660 0.7125 1.0000 5.250 1.2000 0.00920 0.00560 -0.1622 0.7038 1.0000 5.500 1.2078 0.00948 0.00590 -0.1581 0.6937 1.0000 5.750 1.2175 0.00977 0.00617 -0.1545 0.6845 1.0000 6.000 1.2233 0.01016 0.00653 -0.1501 0.6710 1.0000 6.250 1.2271 0.01063 0.00698 -0.1454 0.6549 1.0000 6.500 1.2306 0.01116 0.00748 -0.1406 0.6338 1.0000 6.750 1.2108 0.01242 0.00853 -0.1313 0.5866 1.0000 7.000 1.1865 0.01407 0.00991 -0.1214 0.5358 1.0000 7.250 1.1806 0.01526 0.01095 -0.1154 0.5030 1.0000 7.500 1.1763 0.01646 0.01200 -0.1099 0.4681 1.0000 7.750 1.1718 0.01775 0.01311 -0.1045 0.4306 1.0000 8.000 1.1741 0.01880 0.01404 -0.1004 0.3998 1.0000 8.250 1.1660 0.02039 0.01536 -0.0947 0.3489 1.0000 8.500 1.1566 0.02211 0.01679 -0.0890 0.2897 1.0000 8.750 1.1517 0.02369 0.01808 -0.0842 0.2372 1.0000 9.000 1.1511 0.02510 0.01928 -0.0802 0.1951 1.0000 9.250 1.1542 0.02637 0.02035 -0.0769 0.1576 1.0000 9.500 1.1555 0.02776 0.02152 -0.0734 0.1165 1.0000 9.750 1.1572 0.02918 0.02274 -0.0701 0.0804 1.0000 10.000 1.1643 0.03033 0.02380 -0.0676 0.0629 1.0000 10.250 1.1734 0.03138 0.02478 -0.0654 0.0467 1.0000 10.500 1.1823 0.03245 0.02577 -0.0632 0.0349 1.0000 10.750 1.1924 0.03346 0.02675 -0.0613 0.0291 1.0000 11.000 1.2046 0.03436 0.02767 -0.0596 0.0261 1.0000 11.250 1.2165 0.03529 0.02861 -0.0580 0.0242 1.0000 11.500 1.2267 0.03635 0.02970 -0.0562 0.0227 1.0000 11.750 1.2382 0.03734 0.03074 -0.0545 0.0216 1.0000 12.000 1.2510 0.03824 0.03167 -0.0531 0.0205 1.0000 12.250 1.2617 0.03929 0.03275 -0.0516 0.0192 1.0000 12.500 1.2713 0.04044 0.03393 -0.0498 0.0184 1.0000 12.750 1.2771 0.04189 0.03544 -0.0477 0.0173 1.0000 13.000 1.2890 0.04291 0.03651 -0.0463 0.0166 1.0000 13.250 1.2995 0.04403 0.03768 -0.0449 0.0160 1.0000 13.500 1.3105 0.04513 0.03880 -0.0436 0.0153 1.0000 13.750 1.3185 0.04648 0.04021 -0.0420 0.0149 1.0000 14.000 1.3260 0.04788 0.04165 -0.0403 0.0143 1.0000 14.250 1.3284 0.04972 0.04355 -0.0383 0.0137 1.0000 14.500 1.3351 0.05124 0.04514 -0.0367 0.0134 1.0000 14.750 1.3457 0.05244 0.04640 -0.0355 0.0129 1.0000 15.000 1.3545 0.05381 0.04782 -0.0343 0.0125 1.0000 15.250 1.3613 0.05537 0.04943 -0.0329 0.0121 1.0000 15.500 1.3684 0.05692 0.05104 -0.0316 0.0118 1.0000 15.750 1.3733 0.05869 0.05286 -0.0302 0.0114 1.0000 16.000 1.3738 0.06088 0.05511 -0.0286 0.0110 1.0000 16.250 1.3701 0.06351 0.05782 -0.0267 0.0106 1.0000 16.500 1.3745 0.06543 0.05982 -0.0255 0.0105 1.0000 16.750 1.3824 0.06702 0.06147 -0.0246 0.0103 1.0000 17.000 1.3849 0.06918 0.06371 -0.0234 0.0101 1.0000 17.250 1.3863 0.07146 0.06609 -0.0223 0.0100 1.0000 17.500 1.3928 0.07327 0.06796 -0.0216 0.0095 1.0000 17.750 1.3946 0.07556 0.07032 -0.0207 0.0095 1.0000 18.000 1.3936 0.07819 0.07304 -0.0197 0.0093 1.0000 18.250 1.3971 0.08039 0.07531 -0.0191 0.0092 1.0000 18.500 1.4016 0.08251 0.07745 -0.0187 0.0087 1.0000 18.750 1.3989 0.08547 0.08051 -0.0180 0.0088 1.0000 19.000 1.3954 0.08857 0.08369 -0.0175 0.0086 1.0000