XFOIL Version 6.96 Calculated polar for: WB-135/35 13.5% smoothed 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 -0.7488 0.08435 0.08172 -0.0557 1.0000 0.0041 -15.250 -0.7653 0.07821 0.07550 -0.0589 1.0000 0.0041 -15.000 -0.7925 0.07087 0.06804 -0.0627 1.0000 0.0040 -14.750 -0.8035 0.06615 0.06325 -0.0651 1.0000 0.0039 -14.500 -0.8236 0.06024 0.05727 -0.0682 1.0000 0.0040 -14.250 -0.8459 0.05421 0.05116 -0.0713 1.0000 0.0040 -14.000 -0.8751 0.04754 0.04437 -0.0747 1.0000 0.0040 -13.750 -0.8950 0.04206 0.03881 -0.0774 1.0000 0.0041 -13.500 -0.9266 0.03497 0.03157 -0.0816 1.0000 0.0040 -13.250 -0.9237 0.02915 0.02557 -0.0906 0.9965 0.0041 -13.000 -0.9177 0.02648 0.02274 -0.0922 0.9837 0.0041 -12.750 -0.8975 0.02468 0.02082 -0.0942 0.9754 0.0041 -12.500 -0.8714 0.02348 0.01953 -0.0960 0.9678 0.0043 -12.250 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2.500 0.6369 0.00877 0.00207 -0.0763 0.3385 0.4362 2.750 0.6617 0.00886 0.00219 -0.0757 0.3293 0.4551 3.250 0.7106 0.00906 0.00243 -0.0744 0.3107 0.4945 3.500 0.7347 0.00918 0.00256 -0.0737 0.3015 0.5129 3.750 0.7587 0.00927 0.00269 -0.0730 0.2936 0.5379 4.000 0.7826 0.00933 0.00283 -0.0723 0.2879 0.5678 4.250 0.8067 0.00937 0.00295 -0.0716 0.2839 0.5974 4.500 0.8295 0.00942 0.00309 -0.0706 0.2781 0.6347 4.750 0.8469 0.00927 0.00325 -0.0685 0.2701 0.7493 5.250 0.9802 0.00957 0.00392 -0.0864 0.2405 1.0000 5.500 1.0014 0.00980 0.00410 -0.0851 0.2299 1.0000 5.750 1.0219 0.01007 0.00430 -0.0838 0.2159 1.0000 6.000 1.0407 0.01040 0.00454 -0.0821 0.1958 1.0000 6.250 1.0515 0.01110 0.00498 -0.0791 0.1542 1.0000 6.500 1.0525 0.01226 0.00575 -0.0744 0.0888 1.0000 6.750 1.0487 0.01363 0.00677 -0.0688 0.0174 1.0000 7.000 1.0641 0.01396 0.00709 -0.0665 0.0138 1.0000 7.250 1.0806 0.01425 0.00740 -0.0645 0.0125 1.0000 7.500 1.0969 0.01457 0.00775 -0.0624 0.0112 1.0000 7.750 1.1131 0.01494 0.00813 -0.0605 0.0102 1.0000 8.000 1.1285 0.01538 0.00860 -0.0584 0.0091 1.0000 8.250 1.1457 0.01575 0.00900 -0.0568 0.0087 1.0000 8.500 1.1621 0.01618 0.00945 -0.0551 0.0082 1.0000 8.750 1.1786 0.01662 0.00992 -0.0534 0.0077 1.0000 9.000 1.1941 0.01714 0.01045 -0.0517 0.0070 1.0000 9.250 1.2080 0.01777 0.01111 -0.0498 0.0065 1.0000 9.500 1.2241 0.01829 0.01166 -0.0483 0.0062 1.0000 9.750 1.2390 0.01890 0.01231 -0.0468 0.0059 1.0000 10.000 1.2534 0.01957 0.01303 -0.0452 0.0057 1.0000 10.250 1.2679 0.02025 0.01374 -0.0437 0.0054 1.0000 10.500 1.2813 0.02102 0.01456 -0.0422 0.0052 1.0000 10.750 1.2940 0.02186 0.01544 -0.0407 0.0051 1.0000 11.000 1.3060 0.02277 0.01638 -0.0393 0.0047 1.0000 11.250 1.3142 0.02400 0.01767 -0.0375 0.0045 1.0000 11.500 1.3248 0.02509 0.01881 -0.0361 0.0044 1.0000 11.750 1.3371 0.02607 0.01984 -0.0349 0.0043 1.0000 12.000 1.3465 0.02732 0.02117 -0.0336 0.0041 1.0000 12.250 1.3579 0.02843 0.02233 -0.0326 0.0040 1.0000 12.500 1.3662 0.02983 0.02379 -0.0315 0.0039 1.0000 12.750 1.3716 0.03153 0.02556 -0.0302 0.0037 1.0000 13.000 1.3806 0.03294 0.02703 -0.0293 0.0036 1.0000 13.250 1.3833 0.03495 0.02912 -0.0282 0.0036 1.0000 13.500 1.3914 0.03653 0.03075 -0.0275 0.0034 1.0000 13.750 1.3952 0.03856 0.03285 -0.0267 0.0034 1.0000 14.000 1.3982 0.04072 0.03506 -0.0260 0.0032 1.0000 14.250 1.4025 0.04280 0.03722 -0.0254 0.0032 1.0000 14.500 1.3978 0.04593 0.04045 -0.0248 0.0031 1.0000 14.750 1.3973 0.04870 0.04331 -0.0245 0.0031 1.0000 15.000 1.3918 0.05211 0.04682 -0.0243 0.0030 1.0000 15.250 1.3899 0.05524 0.05003 -0.0243 0.0030 1.0000 15.500 1.3831 0.05908 0.05399 -0.0244 0.0029 1.0000 15.750 1.3785 0.06272 0.05773 -0.0248 0.0029 1.0000 16.000 1.3724 0.06669 0.06180 -0.0253 0.0029 1.0000 16.250 1.3653 0.07093 0.06614 -0.0260 0.0029 1.0000 16.500 1.3569 0.07545 0.07076 -0.0269 0.0029 1.0000 16.750 1.3461 0.08042 0.07585 -0.0281 0.0029 1.0000 17.000 1.3360 0.08541 0.08094 -0.0294 0.0029 1.0000 17.250 1.3267 0.09039 0.08602 -0.0308 0.0028 1.0000 17.500 1.3210 0.09481 0.09053 -0.0321 0.0028 1.0000 17.750 1.3058 0.10079 0.09662 -0.0340 0.0028 1.0000 18.000 1.2989 0.10549 0.10142 -0.0355 0.0027 1.0000