XFOIL Version 6.96 Calculated polar for: Marsden 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -18.250 -0.1865 0.08708 0.08118 -0.1550 0.4301 0.0352 -18.000 -0.2289 0.07774 0.07168 -0.1612 0.4301 0.0353 -17.750 -0.2499 0.07163 0.06547 -0.1653 0.4300 0.0355 -17.500 -0.2621 0.06681 0.06057 -0.1686 0.4299 0.0356 -17.250 -0.2697 0.06263 0.05632 -0.1714 0.4297 0.0357 -17.000 -0.2747 0.05885 0.05248 -0.1740 0.4295 0.0359 -16.750 -0.2770 0.05542 0.04899 -0.1764 0.4293 0.0360 -16.500 -0.2774 0.05229 0.04580 -0.1785 0.4291 0.0360 -16.250 -0.2760 0.04944 0.04290 -0.1803 0.4288 0.0361 -16.000 -0.2729 0.04683 0.04024 -0.1820 0.4285 0.0362 -15.750 -0.2686 0.04444 0.03779 -0.1835 0.4281 0.0363 -15.500 -0.2630 0.04225 0.03555 -0.1847 0.4277 0.0363 -15.250 -0.2565 0.04023 0.03349 -0.1858 0.4274 0.0364 -15.000 -0.2491 0.03839 0.03160 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-10.250 -0.0348 0.02163 0.01441 -0.1743 0.4226 0.0382 -10.000 -0.0284 0.02120 0.01398 -0.1716 0.4225 0.0383 -9.750 -0.0275 0.02079 0.01356 -0.1679 0.4224 0.0384 -9.500 -0.0393 0.02040 0.01318 -0.1619 0.4223 0.0385 -9.250 -0.0351 0.01995 0.01273 -0.1587 0.4222 0.0386 -9.000 -0.0242 0.01951 0.01228 -0.1567 0.4221 0.0387 -8.750 -0.0087 0.01910 0.01186 -0.1554 0.4220 0.0388 -8.500 0.0100 0.01869 0.01145 -0.1547 0.4218 0.0389 -8.250 0.0315 0.01831 0.01105 -0.1543 0.4217 0.0391 -8.000 0.0554 0.01796 0.01069 -0.1544 0.4215 0.0392 -7.750 0.0811 0.01762 0.01034 -0.1547 0.4213 0.0393 -7.500 0.1085 0.01731 0.01002 -0.1553 0.4211 0.0395 -7.250 0.1373 0.01703 0.00973 -0.1560 0.4209 0.0396 -7.000 0.1673 0.01676 0.00945 -0.1570 0.4207 0.0397 -6.750 0.1986 0.01646 0.00914 -0.1582 0.4205 0.0400 -6.500 0.2313 0.01615 0.00883 -0.1597 0.4203 0.0403 -6.250 0.2645 0.01591 0.00858 -0.1613 0.4201 0.0407 -6.000 0.2976 0.01571 0.00839 -0.1626 0.4199 0.0411 -5.750 0.3307 0.01556 0.00824 -0.1640 0.4196 0.0415 -5.500 0.3637 0.01542 0.00811 -0.1652 0.4194 0.0419 -5.250 0.3969 0.01531 0.00799 -0.1665 0.4192 0.0423 -5.000 0.4302 0.01520 0.00788 -0.1678 0.4189 0.0426 -4.750 0.4635 0.01509 0.00778 -0.1690 0.4186 0.0429 -4.500 0.4969 0.01500 0.00769 -0.1703 0.4183 0.0433 -4.250 0.5304 0.01493 0.00761 -0.1716 0.4179 0.0437 -4.000 0.5642 0.01487 0.00756 -0.1730 0.4177 0.0441 -3.750 0.5981 0.01483 0.00752 -0.1743 0.4174 0.0444 -3.500 0.6322 0.01480 0.00749 -0.1757 0.4172 0.0448 -3.250 0.6671 0.01475 0.00746 -0.1773 0.4169 0.0456 -3.000 0.7016 0.01473 0.00745 -0.1788 0.4166 0.0465 -2.750 0.7358 0.01473 0.00746 -0.1803 0.4164 0.0474 -2.500 0.7697 0.01474 0.00748 -0.1816 0.4161 0.0484 -2.250 0.8033 0.01475 0.00750 -0.1830 0.4158 0.0494 -2.000 0.8372 0.01475 0.00751 -0.1844 0.4154 0.0507 -1.750 0.8712 0.01475 0.00753 -0.1858 0.4151 0.0526 -1.500 0.9044 0.01475 0.00755 -0.1871 0.4146 0.0548 -1.250 0.9381 0.01476 0.00758 -0.1884 0.4142 0.0578 -1.000 0.9714 0.01478 0.00762 -0.1897 0.4139 0.0617 -0.750 1.0057 0.01481 0.00768 -0.1913 0.4136 0.0680 -0.500 1.0414 0.01483 0.00775 -0.1932 0.4133 0.0798 -0.250 1.0796 0.01482 0.00784 -0.1956 0.4130 0.1056 0.000 1.1196 0.01481 0.00794 -0.1985 0.4128 0.1423 0.250 1.1619 0.01478 0.00805 -0.2019 0.4125 0.1906 0.500 1.2037 0.01477 0.00818 -0.2052 0.4122 0.2417 0.750 1.2461 0.01477 0.00832 -0.2086 0.4120 0.2946 1.000 1.3013 0.01467 0.00847 -0.2148 0.4116 0.3994 1.250 1.3631 0.01459 0.00876 -0.2223 0.4113 0.5552 1.500 1.3938 0.01474 0.00898 -0.2231 0.4109 0.5897 1.750 1.4212 0.01491 0.00917 -0.2233 0.4105 0.6039 2.000 1.4481 0.01509 0.00934 -0.2234 0.4101 0.6105 2.250 1.4747 0.01529 0.00955 -0.2235 0.4098 0.6157 2.500 1.5008 0.01551 0.00978 -0.2235 0.4094 0.6208 2.750 1.5269 0.01575 0.01002 -0.2235 0.4090 0.6254 3.000 1.5531 0.01603 0.01029 -0.2235 0.4085 0.6302 3.250 1.5794 0.01634 0.01060 -0.2237 0.4079 0.6339 3.500 1.6053 0.01662 0.01090 -0.2238 0.4076 0.6374 3.750 1.6302 0.01680 0.01111 -0.2236 0.4074 0.6390 4.000 1.6548 0.01700 0.01133 -0.2235 0.4073 0.6405 4.250 1.6791 0.01720 0.01154 -0.2233 0.4071 0.6421 4.500 1.7031 0.01741 0.01178 -0.2230 0.4070 0.6438 4.750 1.7265 0.01763 0.01202 -0.2227 0.4068 0.6455 5.000 1.7495 0.01786 0.01228 -0.2223 0.4065 0.6471 5.250 1.7722 0.01810 0.01255 -0.2219 0.4063 0.6485 5.500 1.7947 0.01835 0.01282 -0.2216 0.4061 0.6499 5.750 1.8171 0.01861 0.01310 -0.2212 0.4058 0.6512 6.000 1.8391 0.01888 0.01340 -0.2207 0.4055 0.6525 6.250 1.8602 0.01917 0.01372 -0.2202 0.4051 0.6537 6.500 1.8810 0.01947 0.01405 -0.2196 0.4048 0.6549 6.750 1.9017 0.01979 0.01439 -0.2191 0.4044 0.6560 7.000 1.9219 0.02012 0.01475 -0.2184 0.4040 0.6569 7.250 1.9417 0.02046 0.01513 -0.2178 0.4036 0.6583 7.500 1.9612 0.02082 0.01552 -0.2172 0.4032 0.6599 7.750 1.9804 0.02119 0.01593 -0.2165 0.4027 0.6614 8.000 1.9988 0.02158 0.01636 -0.2158 0.4022 0.6629 8.250 2.0172 0.02197 0.01679 -0.2150 0.4017 0.6642 8.500 2.0350 0.02239 0.01725 -0.2143 0.4012 0.6655 8.750 2.0524 0.02281 0.01771 -0.2135 0.4006 0.6668 9.000 2.0698 0.02327 0.01820 -0.2128 0.4001 0.6681 9.250 2.0861 0.02378 0.01875 -0.2120 0.3996 0.6694 9.500 2.1027 0.02430 0.01930 -0.2112 0.3991 0.6709 9.750 2.1183 0.02487 0.01991 -0.2104 0.3986 0.6725 10.000 2.1336 0.02547 0.02055 -0.2096 0.3981 0.6740 10.250 2.1482 0.02611 0.02123 -0.2088 0.3976 0.6752 10.500 2.1621 0.02682 0.02198 -0.2080 0.3971 0.6764 10.750 2.1755 0.02760 0.02279 -0.2073 0.3965 0.6775 11.000 2.1886 0.02842 0.02365 -0.2065 0.3960 0.6785 11.250 2.2011 0.02932 0.02458 -0.2058 0.3953 0.6794 11.500 2.2128 0.03029 0.02557 -0.2051 0.3944 0.6802 11.750 2.2221 0.03147 0.02678 -0.2042 0.3934 0.6809 12.000 2.2225 0.03335 0.02877 -0.2029 0.3927 0.6820 12.250 2.2183 0.03574 0.03128 -0.2015 0.3915 0.6835 12.500 2.2086 0.03877 0.03443 -0.2001 0.3897 0.6848 12.750 2.1930 0.04252 0.03830 -0.1988 0.3876 0.6860 13.000 2.1553 0.04864 0.04457 -0.1971 0.3845 0.6868 13.250 2.0967 0.05705 0.05307 -0.1949 0.3798 0.6873