XFOIL Version 6.94 Calculated polar for: GOE 279 (DAIMLER X) 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 0.5587 0.01058 0.00378 -0.1079 0.8411 0.0338 0.500 0.6125 0.01046 0.00361 -0.1068 0.8100 0.0420 1.500 0.7180 0.00996 0.00280 -0.1044 0.6991 0.0693 2.000 0.7686 0.01016 0.00269 -0.1030 0.6274 0.1082 4.000 0.9596 0.01102 0.00394 -0.0971 0.3903 1.0000 4.500 1.0091 0.01174 0.00443 -0.0962 0.3540 1.0000 5.000 1.0523 0.01296 0.00508 -0.0945 0.2526 1.0000 5.500 1.0968 0.01418 0.00582 -0.0931 0.1618 1.0000 6.000 1.1387 0.01575 0.00692 -0.0914 0.0961 1.0000 6.500 1.1773 0.01764 0.00839 -0.0890 0.0281 1.0000 7.000 1.2236 0.01851 0.00937 -0.0876 0.0238 1.0000 7.500 1.2689 0.01942 0.01037 -0.0861 0.0169 1.0000 8.000 1.3097 0.02074 0.01174 -0.0839 0.0049 1.0000 8.500 1.3503 0.02197 0.01319 -0.0815 0.0052 1.0000 9.000 1.3891 0.02322 0.01469 -0.0788 0.0059 1.0000 9.500 1.4221 0.02479 0.01651 -0.0753 0.0065 1.0000 10.000 1.4495 0.02641 0.01843 -0.0708 0.0074 1.0000 10.500 1.4653 0.02894 0.02129 -0.0653 0.0076 1.0000 11.000 1.4704 0.03239 0.02507 -0.0594 0.0078 1.0000 11.500 1.4658 0.03697 0.02996 -0.0540 0.0080 1.0000 12.000 1.4546 0.04278 0.03605 -0.0498 0.0082 1.0000 12.500 1.4424 0.04943 0.04297 -0.0471 0.0083 1.0000 13.000 1.4362 0.05613 0.05000 -0.0457 0.0087 1.0000 13.500 1.4258 0.06377 0.05802 -0.0442 0.0092 1.0000 14.000 1.4141 0.07196 0.06659 -0.0425 0.0099 1.0000 14.500 1.4051 0.08029 0.07524 -0.0413 0.0105 1.0000 15.000 1.3573 0.09622 0.09203 -0.0461 0.0119 1.0000 15.500 1.3262 0.10985 0.10604 -0.0519 0.0124 1.0000 16.000 1.2993 0.12382 0.12034 -0.0589 0.0132 1.0000 16.500 1.2567 0.14331 0.14026 -0.0725 0.0133 1.0000 17.000 1.2216 0.16307 0.16031 -0.0863 0.0133 1.0000 17.500 1.1893 0.18453 0.18198 -0.1011 0.0132 1.0000 18.000 0.9534 0.16116 0.15866 -0.0660 0.0114 1.0000 18.500 0.9087 0.17732 0.17500 -0.0748 0.0112 1.0000 19.000 0.8693 0.19424 0.19196 -0.0825 0.0107 1.0000 19.500 0.8303 0.21531 0.21295 -0.0893 0.0110 1.0000 20.000 0.8213 0.22923 0.22684 -0.0922 0.0225 1.0000 20.500 0.8176 0.23886 0.23646 -0.0959 0.0229 1.0000 21.000 0.8192 0.24678 0.24439 -0.0986 0.0229 1.0000 21.500 0.8232 0.25394 0.25157 -0.1007 0.0226 1.0000 22.000 0.8311 0.26084 0.25848 -0.1019 0.0223 1.0000 22.500 0.8262 0.27024 0.26787 -0.1065 0.0212 1.0000 23.000 0.8300 0.27753 0.27517 -0.1089 0.0199 1.0000 23.500 0.8359 0.28394 0.28160 -0.1106 0.0190 1.0000 24.000 0.8370 0.29245 0.29012 -0.1137 0.0180 1.0000 24.500 0.8409 0.29960 0.29729 -0.1160 0.0164 1.0000 25.000 0.8476 0.30614 0.30385 -0.1173 0.0156 1.0000 25.500 0.8477 0.31461 0.31233 -0.1209 0.0140 1.0000 26.000 0.8529 0.32085 0.31860 -0.1226 0.0129 1.0000 26.500 0.8546 0.32950 0.32727 -0.1256 0.0118 1.0000 27.000 0.8583 0.33618 0.33398 -0.1278 0.0106 1.0000 27.500 0.8608 0.34414 0.34195 -0.1303 0.0100 1.0000 28.000 0.8639 0.35154 0.34938 -0.1326 0.0088 1.0000 28.500 0.8672 0.35801 0.35588 -0.1345 0.0083 1.0000 29.000 0.8690 0.36659 0.36448 -0.1374 0.0075 1.0000 29.500 0.8715 0.37353 0.37144 -0.1396 0.0067 1.0000 30.000 0.8736 0.38041 0.37835 -0.1418 0.0064 1.0000 30.500 0.8754 0.38871 0.38667 -0.1443 0.0059 1.0000 31.000 0.8772 0.39597 0.39397 -0.1467 0.0054 1.0000 31.500 0.8787 0.40255 0.40058 -0.1489 0.0050 1.0000 32.000 0.8797 0.40981 0.40787 -0.1512 0.0048 1.0000 32.500 0.8810 0.41784 0.41593 -0.1536 0.0046 1.0000 33.000 0.8819 0.42519 0.42331 -0.1559 0.0043 1.0000 33.500 0.8825 0.43223 0.43038 -0.1582 0.0040 1.0000 34.000 0.8828 0.43902 0.43721 -0.1605 0.0038 1.0000 34.500 0.8825 0.44537 0.44359 -0.1628 0.0036 1.0000 35.500 0.8815 0.45909 0.45739 -0.1673 0.0035 1.0000 36.000 0.8809 0.46605 0.46438 -0.1696 0.0035 1.0000 36.500 0.8802 0.47289 0.47125 -0.1719 0.0034 1.0000 37.000 0.8791 0.47954 0.47794 -0.1741 0.0034 1.0000 37.500 0.8778 0.48610 0.48454 -0.1764 0.0033 1.0000 38.000 0.8761 0.49225 0.49073 -0.1786 0.0033 1.0000 38.500 0.8741 0.49840 0.49692 -0.1808 0.0032 1.0000 39.000 0.8719 0.50439 0.50295 -0.1830 0.0032 1.0000 39.500 0.8694 0.51015 0.50875 -0.1852 0.0032 1.0000 40.000 0.8668 0.51600 0.51463 -0.1874 0.0032 1.0000 40.500 0.8637 0.52143 0.52011 -0.1896 0.0031 1.0000 41.000 0.8604 0.52671 0.52543 -0.1917 0.0031 1.0000 41.500 0.8570 0.53207 0.53083 -0.1939 0.0031 1.0000 42.000 0.8532 0.53706 0.53586 -0.1960 0.0031 1.0000 42.500 0.8493 0.54199 0.54082 -0.1982 0.0031 1.0000 43.000 0.8450 0.54656 0.54544 -0.2003 0.0031 1.0000 43.500 0.8405 0.55116 0.55008 -0.2023 0.0031 1.0000 44.000 0.8359 0.55568 0.55463 -0.2044 0.0031 1.0000 44.500 0.8311 0.56001 0.55900 -0.2064 0.0030 1.0000 45.000 0.8261 0.56425 0.56327 -0.2084 0.0029 1.0000 45.500 0.8208 0.56826 0.56732 -0.2104 0.0027 1.0000 46.000 0.8154 0.57237 0.57147 -0.2124 0.0026 1.0000 46.500 0.8095 0.57580 0.57493 -0.2144 0.0025 1.0000 47.000 0.8029 0.57876 0.57793 -0.2164 0.0024 1.0000 48.000 0.7912 0.58695 0.58617 -0.2200 0.0023 1.0000 48.500 0.7855 0.59086 0.59010 -0.2217 0.0023 1.0000 49.000 0.7793 0.59429 0.59356 -0.2234 0.0023 1.0000 49.500 0.7729 0.59746 0.59677 -0.2252 0.0021 1.0000 50.000 0.7661 0.60018 0.59952 -0.2269 0.0020 1.0000 50.500 0.7590 0.60250 0.60186 -0.2286 0.0018 1.0000 51.000 0.7517 0.60450 0.60389 -0.2303 0.0017 1.0000 51.500 0.7441 0.60614 0.60556 -0.2320 0.0016 1.0000 52.000 0.7361 0.60740 0.60686 -0.2338 0.0015 1.0000 52.500 0.7274 0.60833 0.60782 -0.2355 0.0014 1.0000 54.000 0.7045 0.61362 0.61317 -0.2400 0.0014 1.0000 54.500 0.6966 0.61472 0.61430 -0.2414 0.0014 1.0000 55.000 0.6884 0.61558 0.61518 -0.2428 0.0014 1.0000 55.500 0.6801 0.61602 0.61564 -0.2442 0.0013 1.0000 56.000 0.6715 0.61621 0.61586 -0.2456 0.0013 1.0000 56.500 0.6626 0.61573 0.61541 -0.2470 0.0012 1.0000 57.000 0.6537 0.61548 0.61518 -0.2484 0.0010 1.0000 57.500 0.6445 0.61462 0.61434 -0.2497 0.0010 1.0000 58.000 0.6353 0.61358 0.61332 -0.2510 0.0009 1.0000 58.500 0.6257 0.61191 0.61168 -0.2523 0.0008 1.0000 59.000 0.6161 0.61019 0.60998 -0.2537 0.0007 1.0000 59.500 0.6063 0.60816 0.60798 -0.2550 0.0007 1.0000 60.000 0.5960 0.60543 0.60528 -0.2563 0.0007 1.0000