XFOIL Version 6.96 Calculated polar for: WORTMANN FX 75-193 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -16.000 -0.3708 0.08335 0.08005 -0.1341 0.7883 0.0080 -15.750 -0.4008 0.07262 0.06913 -0.1418 0.7880 0.0078 -15.500 -0.4230 0.06403 0.06034 -0.1487 0.7877 0.0080 -15.250 -0.4362 0.05783 0.05397 -0.1536 0.7873 0.0078 -15.000 -0.4489 0.05227 0.04821 -0.1576 0.7869 0.0077 -14.750 -0.4525 0.04829 0.04408 -0.1606 0.7864 0.0077 -14.500 -0.4554 0.04470 0.04032 -0.1631 0.7858 0.0079 -14.250 -0.4592 0.04127 0.03671 -0.1649 0.7851 0.0078 -14.000 -0.4544 0.03896 0.03428 -0.1664 0.7843 0.0080 -13.750 -0.4489 0.03689 0.03209 -0.1675 0.7834 0.0081 -13.500 -0.4483 0.03479 0.02985 -0.1671 0.7831 0.0080 -13.250 -0.4426 0.03334 0.02831 -0.1667 0.7827 0.0082 -13.000 -0.4366 0.03200 0.02686 -0.1662 0.7823 0.0084 -12.750 -0.4294 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0.7087 7.000 1.1171 0.01276 0.00804 -0.0987 0.4703 0.7093 7.250 1.1123 0.01390 0.00910 -0.0941 0.4503 0.7098 7.500 1.1060 0.01514 0.01023 -0.0894 0.4277 0.7102 7.750 1.1064 0.01603 0.01104 -0.0857 0.4075 0.7111 8.000 1.1029 0.01713 0.01201 -0.0816 0.3808 0.7118 8.250 1.0965 0.01841 0.01314 -0.0771 0.3516 0.7126 8.500 1.0928 0.01963 0.01421 -0.0731 0.3208 0.7133 8.750 1.0880 0.02096 0.01537 -0.0692 0.2875 0.7139 9.000 1.0813 0.02248 0.01666 -0.0651 0.2478 0.7144 9.250 1.0751 0.02410 0.01806 -0.0613 0.2072 0.7147 9.500 1.0640 0.02608 0.01972 -0.0571 0.1541 0.7150 9.750 1.0621 0.02770 0.02116 -0.0542 0.1200 0.7153 10.000 1.0602 0.02939 0.02266 -0.0514 0.0848 0.7158 10.250 1.0606 0.03106 0.02418 -0.0490 0.0580 0.7163 10.500 1.0657 0.03248 0.02550 -0.0472 0.0402 0.7166 10.750 1.0700 0.03401 0.02693 -0.0454 0.0223 0.7171 11.000 1.0801 0.03519 0.02810 -0.0442 0.0171 0.7175 11.250 1.0904 0.03639 0.02929 -0.0430 0.0123 0.7178 11.500 1.1010 0.03761 0.03051 -0.0420 0.0104 0.7179 11.750 1.1135 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0.06712 -0.0311 0.0082 0.7203 16.750 1.2628 0.07602 0.07003 -0.0312 0.0082 0.7204 17.000 1.2671 0.07863 0.07270 -0.0314 0.0081 0.7205 17.250 1.2689 0.08160 0.07575 -0.0317 0.0081 0.7206 17.500 1.2721 0.08441 0.07863 -0.0320 0.0081 0.7208 17.750 1.2745 0.08739 0.08169 -0.0325 0.0081 0.7209 18.000 1.2771 0.09037 0.08474 -0.0330 0.0081 0.7211