XFOIL Version 6.96 Calculated polar for: WORTMANN FX 76-120 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 ------ -------- --------- --------- -------- -------- -------- -19.000 -1.2330 0.09690 0.09355 -0.0153 1.0000 0.0107 -18.750 -1.2676 0.08756 0.08406 -0.0202 1.0000 0.0108 -18.500 -1.3012 0.07857 0.07491 -0.0248 1.0000 0.0106 -18.250 -1.3294 0.07058 0.06678 -0.0289 1.0000 0.0108 -18.000 -1.3528 0.06344 0.05949 -0.0327 1.0000 0.0107 -17.750 -1.3734 0.05684 0.05274 -0.0361 1.0000 0.0108 -17.500 -1.3871 0.05145 0.04722 -0.0389 1.0000 0.0109 -17.250 -1.3963 0.04690 0.04254 -0.0410 1.0000 0.0110 -17.000 -1.4042 0.04276 0.03828 -0.0427 1.0000 0.0110 -16.750 -1.4053 0.03969 0.03510 -0.0437 1.0000 0.0113 -16.500 -1.4092 0.03652 0.03182 -0.0444 1.0000 0.0114 -16.250 -1.4070 0.03422 0.02942 -0.0446 1.0000 0.0115 -16.000 -1.4054 0.03203 0.02713 -0.0443 1.0000 0.0116 -15.750 -1.4006 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0.00403 -0.0073 0.9700 0.0649 -6.250 -0.6664 0.00966 0.00378 -0.0082 0.9666 0.0740 -6.000 -0.6346 0.00936 0.00354 -0.0091 0.9628 0.0847 -5.750 -0.6004 0.00907 0.00330 -0.0106 0.9589 0.0969 -5.500 -0.5667 0.00875 0.00306 -0.0119 0.9521 0.1127 -5.250 -0.5310 0.00847 0.00284 -0.0137 0.9434 0.1285 -5.000 -0.5009 0.00825 0.00267 -0.0142 0.9331 0.1419 -4.750 -0.4708 0.00808 0.00252 -0.0146 0.9240 0.1530 -4.500 -0.4425 0.00792 0.00237 -0.0147 0.9136 0.1641 -4.250 -0.4152 0.00777 0.00224 -0.0144 0.9000 0.1749 -4.000 -0.3884 0.00766 0.00211 -0.0141 0.8832 0.1852 -3.750 -0.3628 0.00755 0.00199 -0.0134 0.8635 0.1985 -3.500 -0.3380 0.00745 0.00188 -0.0127 0.8426 0.2112 -3.250 -0.3134 0.00736 0.00177 -0.0118 0.8206 0.2239 -3.000 -0.2890 0.00730 0.00168 -0.0109 0.7983 0.2359 -2.750 -0.2651 0.00726 0.00159 -0.0099 0.7712 0.2494 -2.500 -0.2418 0.00724 0.00151 -0.0088 0.7393 0.2634 -2.250 -0.2183 0.00724 0.00145 -0.0077 0.7066 0.2771 -2.000 -0.1946 0.00723 0.00139 -0.0067 0.6762 0.2920 -1.750 -0.1706 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0.7985 3.250 0.3134 0.00737 0.00177 0.0118 0.2230 0.8200 3.500 0.3379 0.00746 0.00188 0.0127 0.2107 0.8426 4.000 0.3885 0.00766 0.00211 0.0140 0.1859 0.8830 4.250 0.4153 0.00777 0.00224 0.0144 0.1756 0.9004 4.500 0.4425 0.00792 0.00237 0.0147 0.1645 0.9135 4.750 0.4707 0.00810 0.00252 0.0146 0.1518 0.9243 5.000 0.5007 0.00827 0.00268 0.0142 0.1400 0.9330 5.250 0.5309 0.00848 0.00284 0.0137 0.1277 0.9433 5.500 0.5669 0.00874 0.00306 0.0119 0.1140 0.9522 5.750 0.6009 0.00905 0.00329 0.0105 0.0985 0.9590 6.000 0.6346 0.00937 0.00354 0.0091 0.0845 0.9628 6.250 0.6664 0.00967 0.00378 0.0082 0.0737 0.9667 6.500 0.6979 0.00995 0.00402 0.0073 0.0650 0.9699 6.750 0.7300 0.01024 0.00428 0.0063 0.0582 0.9727 7.000 0.7590 0.01054 0.00455 0.0059 0.0521 0.9770 7.250 0.7893 0.01082 0.00481 0.0053 0.0478 0.9800 7.500 0.8213 0.01115 0.00511 0.0043 0.0434 0.9821 7.750 0.8525 0.01145 0.00541 0.0035 0.0400 0.9850 8.000 0.8823 0.01179 0.00573 0.0029 0.0371 0.9881 8.250 0.9133 0.01207 0.00603 0.0021 0.0351 0.9901 8.500 0.9429 0.01241 0.00635 0.0016 0.0329 0.9924 8.750 0.9717 0.01276 0.00671 0.0012 0.0310 0.9948 9.000 1.0017 0.01307 0.00703 0.0005 0.0295 0.9971 9.250 1.0318 0.01343 0.00739 -0.0002 0.0279 0.9988 9.500 1.0617 0.01384 0.00781 -0.0009 0.0262 1.0000 9.750 1.0800 0.01412 0.00812 0.0009 0.0255 1.0000 10.000 1.0981 0.01443 0.00845 0.0027 0.0244 1.0000 10.250 1.1161 0.01477 0.00880 0.0045 0.0235 1.0000 10.500 1.1339 0.01515 0.00919 0.0063 0.0224 1.0000 10.750 1.1516 0.01555 0.00962 0.0081 0.0217 1.0000 11.000 1.1702 0.01589 0.01000 0.0097 0.0210 1.0000 11.250 1.1885 0.01627 0.01040 0.0113 0.0201 1.0000 11.500 1.2063 0.01669 0.01084 0.0130 0.0194 1.0000 11.750 1.2236 0.01714 0.01132 0.0147 0.0187 1.0000 12.000 1.2400 0.01764 0.01185 0.0165 0.0179 1.0000 12.250 1.2573 0.01808 0.01233 0.0182 0.0175 1.0000 12.500 1.2737 0.01856 0.01285 0.0200 0.0170 1.0000 12.750 1.2896 0.01907 0.01340 0.0218 0.0164 1.0000 13.000 1.3022 0.01960 0.01398 0.0242 0.0160 1.0000 13.250 1.3133 0.02017 0.01458 0.0267 0.0155 1.0000 13.500 1.3239 0.02082 0.01527 0.0291 0.0149 1.0000 13.750 1.3355 0.02147 0.01597 0.0313 0.0144 1.0000 14.000 1.3475 0.02213 0.01669 0.0332 0.0141 1.0000 14.250 1.3585 0.02290 0.01752 0.0351 0.0138 1.0000 14.500 1.3687 0.02375 0.01843 0.0368 0.0134 1.0000 14.750 1.3779 0.02472 0.01948 0.0385 0.0130 1.0000 15.000 1.3862 0.02581 0.02063 0.0400 0.0128 1.0000 15.250 1.3937 0.02702 0.02190 0.0414 0.0125 1.0000 15.500 1.3984 0.02854 0.02348 0.0426 0.0121 1.0000 15.750 1.4030 0.03018 0.02520 0.0435 0.0119 1.0000 16.000 1.4058 0.03210 0.02721 0.0441 0.0117 1.0000 16.250 1.4087 0.03417 0.02938 0.0443 0.0115 1.0000 16.500 1.4097 0.03662 0.03192 0.0442 0.0113 1.0000 16.750 1.4094 0.03938 0.03479 0.0436 0.0112 1.0000 17.000 1.4061 0.04272 0.03824 0.0425 0.0110 1.0000 17.250 1.3992 0.04673 0.04238 0.0408 0.0109 1.0000 17.500 1.3899 0.05130 0.04707 0.0386 0.0108 1.0000 17.750 1.3767 0.05665 0.05254 0.0359 0.0107 1.0000 18.000 1.3572 0.06308 0.05912 0.0325 0.0107 1.0000 18.250 1.3350 0.07006 0.06624 0.0288 0.0106 1.0000 18.500 1.3020 0.07881 0.07516 0.0243 0.0107 1.0000 18.750 1.2687 0.08779 0.08429 0.0196 0.0106 1.0000 19.000 1.2362 0.09680 0.09345 0.0149 0.0107 1.0000