XFOIL Version 6.96 Calculated polar for: WORTMANN FX 75-141 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 ------ -------- --------- --------- -------- -------- -------- -15.750 -0.7627 0.07353 0.07064 -0.0818 0.8556 0.0117 -15.500 -0.7998 0.06213 0.05898 -0.0904 0.8499 0.0116 -15.250 -0.8099 0.05576 0.05244 -0.0959 0.8444 0.0116 -15.000 -0.8227 0.04947 0.04596 -0.1014 0.8403 0.0117 -14.750 -0.8259 0.04486 0.04121 -0.1057 0.8366 0.0118 -14.500 -0.8256 0.04070 0.03688 -0.1099 0.8330 0.0119 -14.250 -0.8176 0.03732 0.03334 -0.1141 0.8298 0.0120 -14.000 -0.8089 0.03415 0.02999 -0.1181 0.8266 0.0122 -13.750 -0.7946 0.03234 0.02808 -0.1202 0.8244 0.0125 -13.500 -0.7862 0.02982 0.02542 -0.1226 0.8221 0.0125 -13.250 -0.7667 0.02862 0.02412 -0.1243 0.8200 0.0129 -13.000 -0.7527 0.02678 0.02215 -0.1261 0.8178 0.0130 -12.750 -0.7339 0.02552 0.02078 -0.1276 0.8157 0.0132 -12.500 -0.7264 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0.00626 0.00202 -0.1257 0.6893 0.7032 2.000 0.7476 0.00626 0.00202 -0.1254 0.6783 0.7069 2.250 0.7735 0.00629 0.00201 -0.1249 0.6639 0.7106 2.500 0.7993 0.00637 0.00203 -0.1244 0.6490 0.7140 2.750 0.8249 0.00644 0.00207 -0.1239 0.6360 0.7173 3.000 0.8503 0.00654 0.00215 -0.1234 0.6238 0.7203 3.250 0.8754 0.00667 0.00224 -0.1228 0.6103 0.7232 3.500 0.9006 0.00680 0.00234 -0.1222 0.5969 0.7263 3.750 0.9258 0.00695 0.00245 -0.1217 0.5844 0.7292 4.000 0.9509 0.00709 0.00256 -0.1212 0.5726 0.7319 4.250 0.9751 0.00723 0.00268 -0.1205 0.5594 0.7347 4.500 0.9983 0.00742 0.00283 -0.1196 0.5410 0.7372 4.750 1.0202 0.00766 0.00300 -0.1184 0.5187 0.7398 5.000 1.0423 0.00791 0.00317 -0.1173 0.4995 0.7427 5.250 1.0648 0.00814 0.00334 -0.1163 0.4793 0.7453 5.500 1.0861 0.00841 0.00354 -0.1151 0.4566 0.7475 5.750 1.1054 0.00872 0.00376 -0.1135 0.4297 0.7501 6.000 1.1224 0.00913 0.00403 -0.1115 0.3955 0.7527 6.250 1.1364 0.00965 0.00437 -0.1090 0.3561 0.7553 6.500 1.1470 0.01029 0.00479 -0.1059 0.3105 0.7579 6.750 1.1572 0.01090 0.00521 -0.1027 0.2710 0.7605 7.000 1.1642 0.01147 0.00560 -0.0989 0.2377 0.7628 7.250 1.1736 0.01198 0.00601 -0.0955 0.2112 0.7658 7.500 1.1831 0.01252 0.00645 -0.0923 0.1885 0.7688 7.750 1.1945 0.01302 0.00688 -0.0895 0.1707 0.7721 8.000 1.2052 0.01355 0.00734 -0.0866 0.1526 0.7758 8.250 1.2156 0.01410 0.00782 -0.0838 0.1362 0.7796 8.500 1.2238 0.01475 0.00840 -0.0808 0.1178 0.7833 8.750 1.2318 0.01546 0.00903 -0.0779 0.1008 0.7864 9.000 1.2402 0.01622 0.00973 -0.0752 0.0851 0.7897 9.250 1.2488 0.01703 0.01048 -0.0727 0.0722 0.7929 9.500 1.2583 0.01784 0.01126 -0.0704 0.0620 0.7962 9.750 1.2681 0.01867 0.01207 -0.0682 0.0543 0.8001 10.000 1.2797 0.01945 0.01286 -0.0664 0.0489 0.8044 10.250 1.2914 0.02027 0.01368 -0.0646 0.0441 0.8087 10.500 1.3030 0.02109 0.01453 -0.0629 0.0405 0.8135 10.750 1.3141 0.02199 0.01546 -0.0612 0.0372 0.8194 11.000 1.3280 0.02273 0.01626 -0.0598 0.0355 0.8262 11.250 1.3396 0.02362 0.01720 -0.0583 0.0333 0.8366 11.500 1.3490 0.02468 0.01834 -0.0566 0.0307 0.8547 11.750 1.3796 0.02550 0.01939 -0.0589 0.0291 0.9148 12.000 1.4272 0.02706 0.02099 -0.0655 0.0264 1.0000 12.250 1.4381 0.02831 0.02228 -0.0644 0.0249 1.0000 12.500 1.4522 0.02934 0.02336 -0.0636 0.0238 1.0000 12.750 1.4643 0.03050 0.02454 -0.0626 0.0227 1.0000 13.000 1.4746 0.03180 0.02587 -0.0615 0.0218 1.0000 13.250 1.4797 0.03353 0.02763 -0.0601 0.0205 1.0000 13.500 1.4908 0.03479 0.02896 -0.0591 0.0200 1.0000 13.750 1.5016 0.03609 0.03030 -0.0582 0.0193 1.0000 14.000 1.5116 0.03747 0.03173 -0.0573 0.0184 1.0000 14.250 1.5195 0.03907 0.03337 -0.0563 0.0178 1.0000 14.500 1.5244 0.04097 0.03530 -0.0552 0.0171 1.0000 14.750 1.5252 0.04327 0.03768 -0.0539 0.0164 1.0000 15.000 1.5346 0.04484 0.03931 -0.0533 0.0160 1.0000 15.250 1.5423 0.04661 0.04114 -0.0526 0.0155 1.0000 15.500 1.5491 0.04849 0.04308 -0.0519 0.0150 1.0000 15.750 1.5539 0.05061 0.04527 -0.0512 0.0146 1.0000 16.000 1.5576 0.05285 0.04757 -0.0506 0.0142 1.0000 16.250 1.5582 0.05546 0.05023 -0.0500 0.0136 1.0000 16.500 1.5542 0.05866 0.05351 -0.0494 0.0133 1.0000 16.750 1.5546 0.06143 0.05637 -0.0490 0.0129 1.0000 17.000 1.5575 0.06395 0.05897 -0.0487 0.0127 1.0000 17.250 1.5591 0.06663 0.06173 -0.0485 0.0124 1.0000 17.500 1.5577 0.06971 0.06490 -0.0484 0.0122 1.0000 17.750 1.5578 0.07267 0.06794 -0.0484 0.0119 1.0000 18.000 1.5566 0.07583 0.07118 -0.0485 0.0117 1.0000 18.250 1.5543 0.07919 0.07462 -0.0487 0.0114 1.0000 18.500 1.5494 0.08289 0.07840 -0.0490 0.0112 1.0000 18.750 1.5438 0.08678 0.08237 -0.0495 0.0110 1.0000 19.000 1.5354 0.09114 0.08682 -0.0503 0.0108 1.0000 19.250 1.5246 0.09596 0.09174 -0.0514 0.0107 1.0000