XFOIL Version 6.96 Calculated polar for: WORTMANN FX 057-816 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 ------ -------- --------- --------- -------- -------- -------- -15.500 -0.8607 0.04783 0.04377 -0.0908 0.5731 0.0067 -15.250 -0.9029 0.04106 0.03678 -0.0925 0.5728 0.0066 -15.000 -0.9196 0.03743 0.03298 -0.0918 0.5724 0.0067 -14.750 -0.9303 0.03476 0.03016 -0.0903 0.5718 0.0067 -14.500 -0.9368 0.03261 0.02787 -0.0884 0.5712 0.0068 -14.250 -0.9374 0.03093 0.02606 -0.0864 0.5705 0.0068 -14.000 -0.9378 0.02943 0.02444 -0.0840 0.5702 0.0069 -13.750 -0.9353 0.02826 0.02317 -0.0813 0.5698 0.0069 -13.500 -0.9325 0.02690 0.02168 -0.0788 0.5694 0.0070 -13.250 -0.9231 0.02560 0.02027 -0.0771 0.5690 0.0072 -13.000 -0.9094 0.02453 0.01910 -0.0758 0.5686 0.0073 -12.750 -0.8939 0.02352 0.01798 -0.0746 0.5681 0.0075 -12.500 -0.8764 0.02263 0.01700 -0.0736 0.5675 0.0077 -12.250 -0.8577 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0.8418 7.000 1.2659 0.00836 0.00404 -0.0857 0.4971 0.8426 7.250 1.2928 0.00845 0.00408 -0.0859 0.4770 0.8434 7.500 1.2978 0.01017 0.00526 -0.0831 0.3745 0.8447 7.750 1.2897 0.01259 0.00722 -0.0787 0.2863 0.8464 8.000 1.2974 0.01373 0.00824 -0.0765 0.2585 0.8475 8.250 1.3024 0.01482 0.00928 -0.0739 0.2382 0.8492 8.500 1.2957 0.01611 0.01056 -0.0696 0.2231 0.8514 8.750 1.2726 0.01980 0.01435 -0.0666 0.2139 0.8549 9.000 1.2509 0.02310 0.01766 -0.0631 0.2039 0.8578 9.250 1.2338 0.02591 0.02044 -0.0599 0.1912 0.8603 9.500 1.2149 0.02884 0.02330 -0.0567 0.1736 0.8625 9.750 1.2029 0.03135 0.02574 -0.0541 0.1544 0.8647 10.000 1.1824 0.03449 0.02874 -0.0511 0.1249 0.8672 10.250 1.1756 0.03688 0.03102 -0.0493 0.1049 0.8693 10.500 1.1797 0.03864 0.03275 -0.0483 0.0949 0.8713 10.750 1.1869 0.04020 0.03428 -0.0475 0.0868 0.8732 11.000 1.1963 0.04162 0.03569 -0.0468 0.0802 0.8751 11.250 1.2049 0.04316 0.03721 -0.0463 0.0732 0.8772 11.750 1.2254 0.04600 0.04007 -0.0453 0.0624 0.8818 12.000 1.2341 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0.08522 -0.0457 0.0061 1.0000 17.750 1.4218 0.09319 0.08799 -0.0463 0.0059 1.0000 18.000 1.4262 0.09594 0.09080 -0.0469 0.0057 1.0000 18.250 1.4299 0.09883 0.09375 -0.0476 0.0056 1.0000 18.500 1.4348 0.10158 0.09657 -0.0483 0.0054 1.0000 18.750 1.4395 0.10437 0.09942 -0.0491 0.0053 1.0000 19.000 1.4427 0.10744 0.10256 -0.0500 0.0052 1.0000 19.250 1.4460 0.11047 0.10566 -0.0509 0.0050 1.0000