XFOIL Version 6.96 Calculated polar for: SD7062 (14%) 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 ------ -------- --------- --------- -------- -------- -------- -14.000 -0.7847 0.05436 0.05160 -0.0715 1.0000 0.0107 -13.750 -0.8129 0.04574 0.04280 -0.0784 1.0000 0.0107 -13.500 -0.8281 0.03960 0.03650 -0.0837 1.0000 0.0107 -13.250 -0.8415 0.03454 0.03129 -0.0879 1.0000 0.0107 -13.000 -0.8541 0.03103 0.02764 -0.0897 1.0000 0.0107 -12.750 -0.8594 0.02866 0.02515 -0.0900 0.9900 0.0108 -12.500 -0.8350 0.02662 0.02294 -0.0934 0.9779 0.0109 -12.250 -0.8089 0.02488 0.02105 -0.0961 0.9628 0.0109 -12.000 -0.7857 0.02357 0.01957 -0.0973 0.9416 0.0110 -11.750 -0.7702 0.02249 0.01832 -0.0965 0.9161 0.0111 -11.500 -0.7544 0.02162 0.01727 -0.0953 0.8935 0.0112 -11.250 -0.7372 0.02078 0.01628 -0.0943 0.8753 0.0112 -11.000 -0.7182 0.02003 0.01538 -0.0934 0.8597 0.0113 -10.750 -0.6977 0.01935 0.01456 -0.0926 0.8460 0.0114 -10.500 -0.6761 0.01874 0.01382 -0.0919 0.8340 0.0115 -10.250 -0.6534 0.01817 0.01314 -0.0914 0.8222 0.0115 -10.000 -0.6330 0.01722 0.01207 -0.0907 0.8117 0.0117 -9.750 -0.6105 0.01655 0.01130 -0.0901 0.8008 0.0119 -9.500 -0.5864 0.01600 0.01067 -0.0897 0.7910 0.0120 -9.250 -0.5621 0.01550 0.01007 -0.0893 0.7812 0.0122 -9.000 -0.5368 0.01504 0.00955 -0.0889 0.7719 0.0123 -8.750 -0.5115 0.01462 0.00905 -0.0886 0.7628 0.0124 -8.500 -0.4858 0.01419 0.00855 -0.0883 0.7537 0.0126 -8.250 -0.4599 0.01381 0.00808 -0.0880 0.7447 0.0127 -8.000 -0.4336 0.01342 0.00763 -0.0877 0.7356 0.0129 -7.750 -0.4073 0.01306 0.00719 -0.0874 0.7268 0.0131 -7.500 -0.3806 0.01271 0.00678 -0.0872 0.7177 0.0133 -7.250 -0.3539 0.01239 0.00638 -0.0870 0.7092 0.0134 -7.000 -0.3268 0.01207 0.00600 -0.0868 0.7002 0.0136 -6.750 -0.2997 0.01179 0.00565 -0.0866 0.6916 0.0138 -6.500 -0.2723 0.01151 0.00532 -0.0864 0.6825 0.0140 -6.250 -0.2449 0.01128 0.00501 -0.0862 0.6737 0.0142 -6.000 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0.3165 0.00825 0.00165 -0.0846 0.4884 0.1553 -1.000 0.3446 0.00811 0.00161 -0.0846 0.4795 0.1988 -0.750 0.3725 0.00801 0.00160 -0.0846 0.4698 0.2443 -0.500 0.4006 0.00788 0.00159 -0.0846 0.4606 0.2929 -0.250 0.4285 0.00781 0.00160 -0.0846 0.4511 0.3392 0.000 0.4565 0.00769 0.00162 -0.0846 0.4419 0.3972 0.250 0.4845 0.00767 0.00166 -0.0845 0.4326 0.4362 0.500 0.5126 0.00767 0.00169 -0.0845 0.4232 0.4649 0.750 0.5406 0.00769 0.00174 -0.0844 0.4141 0.4949 1.000 0.5686 0.00771 0.00180 -0.0844 0.4051 0.5261 1.250 0.5966 0.00774 0.00186 -0.0843 0.3964 0.5526 1.500 0.6244 0.00779 0.00193 -0.0842 0.3870 0.5772 1.750 0.6523 0.00784 0.00199 -0.0841 0.3789 0.6021 2.000 0.6799 0.00791 0.00208 -0.0840 0.3697 0.6266 2.250 0.7077 0.00795 0.00216 -0.0839 0.3615 0.6528 2.500 0.7350 0.00804 0.00226 -0.0837 0.3529 0.6792 2.750 0.7625 0.00809 0.00236 -0.0836 0.3446 0.7072 3.000 0.7894 0.00818 0.00247 -0.0833 0.3357 0.7353 3.250 0.8165 0.00823 0.00258 -0.0831 0.3281 0.7651 3.500 0.8428 0.00833 0.00271 -0.0827 0.3194 0.7964 3.750 0.8690 0.00838 0.00283 -0.0823 0.3118 0.8307 4.000 0.8935 0.00846 0.00297 -0.0815 0.3035 0.8703 4.250 0.9164 0.00847 0.00308 -0.0803 0.2964 0.9214 4.500 0.9494 0.00859 0.00321 -0.0813 0.2877 1.0000 4.750 0.9765 0.00875 0.00333 -0.0812 0.2804 1.0000 5.250 1.0296 0.00914 0.00364 -0.0808 0.2651 1.0000 5.500 1.0556 0.00937 0.00381 -0.0805 0.2566 1.0000 5.750 1.0821 0.00955 0.00396 -0.0802 0.2504 1.0000 6.000 1.1078 0.00979 0.00415 -0.0799 0.2425 1.0000 6.250 1.1338 0.00999 0.00433 -0.0796 0.2358 1.0000 6.500 1.1594 0.01022 0.00453 -0.0793 0.2291 1.0000 6.750 1.1848 0.01045 0.00473 -0.0789 0.2228 1.0000 7.000 1.2099 0.01070 0.00495 -0.0785 0.2153 1.0000 7.250 1.2346 0.01096 0.00518 -0.0781 0.2091 1.0000 7.500 1.2596 0.01119 0.00540 -0.0777 0.2032 1.0000 7.750 1.2831 0.01151 0.00567 -0.0770 0.1956 1.0000 8.000 1.3077 0.01174 0.00589 -0.0766 0.1909 1.0000 8.250 1.3311 0.01204 0.00617 -0.0759 0.1845 1.0000 8.500 1.3542 0.01234 0.00645 -0.0753 0.1786 1.0000 8.750 1.3772 0.01263 0.00673 -0.0746 0.1729 1.0000 9.000 1.3987 0.01299 0.00706 -0.0737 0.1668 1.0000 9.250 1.4210 0.01328 0.00735 -0.0729 0.1616 1.0000 9.500 1.4414 0.01365 0.00770 -0.0718 0.1558 1.0000 9.750 1.4619 0.01400 0.00804 -0.0708 0.1510 1.0000 10.000 1.4805 0.01435 0.00839 -0.0694 0.1457 1.0000 10.250 1.4957 0.01479 0.00880 -0.0674 0.1401 1.0000 10.500 1.5125 0.01515 0.00918 -0.0658 0.1361 1.0000 10.750 1.5274 0.01560 0.00963 -0.0639 0.1312 1.0000 11.000 1.5415 0.01612 0.01013 -0.0620 0.1264 1.0000 11.250 1.5564 0.01661 0.01064 -0.0603 0.1219 1.0000 11.500 1.5692 0.01723 0.01125 -0.0584 0.1172 1.0000 11.750 1.5828 0.01782 0.01186 -0.0567 0.1134 1.0000 12.000 1.5959 0.01847 0.01252 -0.0550 0.1094 1.0000 12.250 1.6069 0.01926 0.01332 -0.0532 0.1052 1.0000 12.500 1.6189 0.02004 0.01412 -0.0516 0.1018 1.0000 12.750 1.6305 0.02088 0.01498 -0.0501 0.0983 1.0000 13.000 1.6399 0.02189 0.01600 -0.0485 0.0945 1.0000 13.250 1.6496 0.02294 0.01707 -0.0471 0.0910 1.0000 13.500 1.6597 0.02400 0.01816 -0.0458 0.0880 1.0000 13.750 1.6672 0.02529 0.01947 -0.0445 0.0845 1.0000 14.000 1.6747 0.02664 0.02085 -0.0432 0.0816 1.0000 14.250 1.6837 0.02793 0.02219 -0.0422 0.0793 1.0000 14.500 1.6904 0.02945 0.02374 -0.0412 0.0765 1.0000 14.750 1.6950 0.03119 0.02551 -0.0402 0.0738 1.0000 15.000 1.7006 0.03291 0.02728 -0.0393 0.0713 1.0000 15.250 1.7056 0.03475 0.02916 -0.0386 0.0688 1.0000 15.500 1.7082 0.03685 0.03130 -0.0380 0.0664 1.0000 15.750 1.7089 0.03922 0.03371 -0.0374 0.0638 1.0000 16.000 1.7130 0.04134 0.03590 -0.0370 0.0623 1.0000 16.250 1.7141 0.04384 0.03846 -0.0368 0.0598 1.0000 16.500 1.7116 0.04680 0.04146 -0.0367 0.0572 1.0000 16.750 1.7103 0.04974 0.04446 -0.0367 0.0551 1.0000 17.000 1.7097 0.05270 0.04748 -0.0369 0.0533 1.0000 17.250 1.7065 0.05603 0.05088 -0.0373 0.0513 1.0000 17.500 1.7002 0.05986 0.05476 -0.0379 0.0491 1.0000 17.750 1.6969 0.06343 0.05840 -0.0386 0.0474 1.0000 18.000 1.6928 0.06715 0.06221 -0.0394 0.0460 1.0000 18.250 1.6865 0.07129 0.06642 -0.0404 0.0446 1.0000 18.500 1.6775 0.07589 0.07109 -0.0417 0.0430 1.0000 18.750 1.6705 0.08030 0.07559 -0.0431 0.0420 1.0000 19.000 1.6634 0.08482 0.08019 -0.0446 0.0406 1.0000 19.250 1.6547 0.08966 0.08512 -0.0463 0.0393 1.0000