XFOIL Version 6.94 Calculated polar for: GOE 619 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 0.5127 0.01095 0.00399 -0.1092 0.6828 0.3626 0.500 0.5638 0.01089 0.00398 -0.1078 0.6661 0.3963 1.000 0.6139 0.01079 0.00401 -0.1063 0.6481 0.4408 1.500 0.6628 0.01061 0.00401 -0.1045 0.6297 0.5104 2.500 0.8095 0.00987 0.00426 -0.1110 0.5818 1.0000 3.000 0.8491 0.01012 0.00433 -0.1073 0.5470 1.0000 3.500 0.8723 0.01075 0.00441 -0.1004 0.4598 1.0000 4.000 0.8911 0.01184 0.00489 -0.0932 0.3703 1.0000 4.500 0.9199 0.01272 0.00542 -0.0880 0.3214 1.0000 5.000 0.9445 0.01364 0.00601 -0.0822 0.2751 1.0000 5.500 0.9697 0.01456 0.00664 -0.0766 0.2356 1.0000 6.000 1.0008 0.01535 0.00728 -0.0722 0.2096 1.0000 6.500 1.0257 0.01648 0.00811 -0.0672 0.1670 1.0000 7.000 1.0202 0.01934 0.01023 -0.0583 0.0531 1.0000 7.500 1.0382 0.02119 0.01189 -0.0532 0.0072 1.0000 8.000 1.0690 0.02238 0.01314 -0.0499 0.0066 1.0000 8.500 1.0983 0.02372 0.01459 -0.0467 0.0064 1.0000 9.000 1.1254 0.02529 0.01627 -0.0435 0.0063 1.0000 9.500 1.1502 0.02709 0.01821 -0.0404 0.0063 1.0000 10.000 1.1718 0.02925 0.02052 -0.0374 0.0064 1.0000 10.500 1.1904 0.03176 0.02321 -0.0346 0.0064 1.0000 11.000 1.2052 0.03472 0.02635 -0.0319 0.0066 1.0000 11.500 1.2168 0.03818 0.03001 -0.0296 0.0067 1.0000 12.000 1.2232 0.04234 0.03438 -0.0276 0.0068 1.0000 12.500 1.2252 0.04726 0.03952 -0.0261 0.0069 1.0000 13.000 1.2221 0.05310 0.04560 -0.0254 0.0070 1.0000 13.500 1.2235 0.05883 0.05152 -0.0252 0.0071 1.0000 14.000 1.2223 0.06520 0.05810 -0.0256 0.0074 1.0000 14.500 1.2138 0.07295 0.06609 -0.0268 0.0075 1.0000 15.000 1.2007 0.08180 0.07517 -0.0289 0.0077 1.0000 15.500 1.1838 0.09170 0.08529 -0.0318 0.0079 1.0000 16.000 1.1669 0.10187 0.09567 -0.0351 0.0081 1.0000 16.500 1.1524 0.11189 0.10585 -0.0387 0.0082 1.0000 17.000 1.1424 0.12105 0.11512 -0.0420 0.0084 1.0000 17.500 1.1427 0.12824 0.12234 -0.0445 0.0086 1.0000 18.000 1.1546 0.13311 0.12719 -0.0458 0.0089 1.0000 18.500 1.1615 0.13983 0.13410 -0.0487 0.0093 1.0000 19.000 1.1777 0.14404 0.13837 -0.0500 0.0100 1.0000 19.500 1.2247 0.14076 0.13482 -0.0458 0.0108 1.0000 20.000 1.2223 0.14972 0.14410 -0.0510 0.0113 1.0000 20.500 1.2805 0.14447 0.13868 -0.0453 0.0129 1.0000 21.000 1.2689 0.15530 0.14991 -0.0521 0.0135 1.0000 21.500 1.3117 0.15364 0.14828 -0.0492 0.0152 1.0000 22.000 1.2997 0.16419 0.15927 -0.0560 0.0160 1.0000 22.500 1.3200 0.16755 0.16290 -0.0570 0.0180 1.0000 23.000 1.2986 0.17995 0.17581 -0.0651 0.0191 1.0000 23.500 1.2972 0.18784 0.18401 -0.0697 0.0207 1.0000 24.000 1.2464 0.20795 0.20461 -0.0838 0.0210 1.0000 24.500 1.1881 0.23201 0.22901 -0.1002 0.0206 1.0000 25.000 0.8776 0.31389 0.31179 -0.1408 0.0304 1.0000 25.500 0.8796 0.32474 0.32265 -0.1453 0.0272 1.0000 26.000 0.8844 0.33461 0.33253 -0.1491 0.0250 1.0000 26.500 0.8937 0.34111 0.33906 -0.1517 0.0234 1.0000 27.000 0.8964 0.35211 0.35008 -0.1559 0.0211 1.0000 27.500 0.9057 0.35822 0.35622 -0.1582 0.0203 1.0000 28.000 0.9071 0.37014 0.36815 -0.1625 0.0182 1.0000 28.500 0.9163 0.37585 0.37391 -0.1646 0.0175 1.0000 29.000 0.9161 0.38905 0.38711 -0.1691 0.0162 1.0000 29.500 0.9215 0.39685 0.39495 -0.1721 0.0154 1.0000 30.000 0.9263 0.40541 0.40353 -0.1750 0.0150 1.0000 30.500 0.9282 0.41690 0.41504 -0.1787 0.0141 1.0000 31.000 0.9319 0.42560 0.42377 -0.1818 0.0134 1.0000 31.500 0.9358 0.43343 0.43164 -0.1847 0.0130 1.0000 32.000 0.9404 0.44048 0.43872 -0.1872 0.0128 1.0000 32.500 0.9407 0.45228 0.45053 -0.1908 0.0126 1.0000 33.000 0.9423 0.46240 0.46069 -0.1940 0.0123 1.0000 33.500 0.9442 0.47160 0.46992 -0.1970 0.0119 1.0000 34.000 0.9458 0.48041 0.47876 -0.1999 0.0115 1.0000 34.500 0.9471 0.48887 0.48726 -0.2028 0.0113 1.0000 35.000 0.9482 0.49717 0.49559 -0.2056 0.0111 1.0000 35.500 0.9490 0.50492 0.50337 -0.2084 0.0109 1.0000 36.000 0.9496 0.51247 0.51096 -0.2110 0.0108 1.0000 37.000 0.9489 0.52949 0.52804 -0.2164 0.0107 1.0000 37.500 0.9478 0.53842 0.53700 -0.2193 0.0106 1.0000 38.000 0.9465 0.54775 0.54636 -0.2221 0.0105 1.0000 38.500 0.9452 0.55642 0.55507 -0.2247 0.0102 1.0000 39.000 0.9436 0.56465 0.56333 -0.2273 0.0097 1.0000 39.500 0.9416 0.57196 0.57068 -0.2297 0.0092 1.0000 40.000 0.9395 0.57883 0.57758 -0.2322 0.0090 1.0000 40.500 0.9372 0.58429 0.58308 -0.2343 0.0088 1.0000 41.000 0.9338 0.59531 0.59412 -0.2370 0.0086 1.0000 41.500 0.9309 0.60420 0.60305 -0.2393 0.0080 1.0000 42.000 0.9275 0.61114 0.61002 -0.2416 0.0075 1.0000 42.500 0.9237 0.61722 0.61613 -0.2438 0.0072 1.0000 43.000 0.9196 0.62197 0.62092 -0.2459 0.0070 1.0000 43.500 0.9153 0.63219 0.63116 -0.2481 0.0069 1.0000 44.000 0.9111 0.64027 0.63928 -0.2502 0.0063 1.0000 44.500 0.9064 0.64661 0.64564 -0.2523 0.0058 1.0000 45.000 0.9011 0.65159 0.65066 -0.2543 0.0055 1.0000 45.500 0.8954 0.65536 0.65445 -0.2563 0.0054 1.0000 46.000 0.8901 0.66445 0.66357 -0.2581 0.0052 1.0000 46.500 0.8846 0.67132 0.67046 -0.2599 0.0049 1.0000 47.000 0.8786 0.67669 0.67587 -0.2617 0.0044 1.0000 47.500 0.8722 0.68082 0.68002 -0.2635 0.0041 1.0000 48.000 0.8653 0.68392 0.68315 -0.2653 0.0039 1.0000 49.000 0.8516 0.69422 0.69349 -0.2685 0.0038 1.0000 49.500 0.8449 0.69971 0.69901 -0.2699 0.0035 1.0000 50.000 0.8376 0.70338 0.70271 -0.2714 0.0032 1.0000 50.500 0.8299 0.70611 0.70547 -0.2729 0.0029 1.0000 51.000 0.8218 0.70805 0.70743 -0.2743 0.0027 1.0000 51.500 0.8134 0.70921 0.70861 -0.2758 0.0025 1.0000 53.000 0.7880 0.71578 0.71524 -0.2795 0.0024 1.0000 53.500 0.7796 0.71765 0.71714 -0.2805 0.0023 1.0000 54.000 0.7707 0.71851 0.71803 -0.2816 0.0022 1.0000 54.500 0.7617 0.71891 0.71844 -0.2826 0.0020 1.0000 55.000 0.7523 0.71845 0.71800 -0.2836 0.0018 1.0000 55.500 0.7428 0.71749 0.71707 -0.2845 0.0016 1.0000 56.000 0.7329 0.71574 0.71534 -0.2855 0.0015 1.0000 56.500 0.7229 0.71341 0.71303 -0.2864 0.0013 1.0000 57.000 0.7125 0.71022 0.70986 -0.2873 0.0012 1.0000 58.500 0.6823 0.70437 0.70406 -0.2892 0.0011 1.0000 59.000 0.6721 0.70133 0.70104 -0.2897 0.0010 1.0000 59.500 0.6614 0.69721 0.69694 -0.2903 0.0008 1.0000 60.000 0.6506 0.69231 0.69206 -0.2907 0.0008 1.0000