XFOIL Version 6.96 Calculated polar for: WORTMANN FX 73-170 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -12.500 -0.0759 0.10061 0.09691 -0.1318 0.7821 0.0233 -12.250 -0.0834 0.09271 0.08902 -0.1367 0.7809 0.0238 -12.000 -0.0787 0.08860 0.08492 -0.1394 0.7798 0.0238 -11.750 -0.0733 0.08554 0.08188 -0.1409 0.7785 0.0240 -11.500 -0.0644 0.08352 0.07987 -0.1419 0.7771 0.0244 -11.250 -0.0623 0.07918 0.07555 -0.1448 0.7758 0.0246 -11.000 -0.0580 0.07566 0.07205 -0.1472 0.7743 0.0251 -10.750 -0.0076 0.05060 0.04714 -0.1509 0.7678 0.0283 -10.500 -0.0316 0.04305 0.03953 -0.1556 0.7667 0.0280 -10.250 -0.0590 0.03715 0.03353 -0.1588 0.7654 0.0279 -10.000 -0.0815 0.03303 0.02933 -0.1599 0.7639 0.0278 -9.750 -0.1055 0.02977 0.02597 -0.1596 0.7623 0.0280 -9.500 -0.1348 0.02757 0.02361 -0.1577 0.7603 0.0285 -9.250 -0.1639 0.02757 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-0.1324 0.7053 0.6952 0.500 0.6215 0.01286 0.00745 -0.1330 0.7042 0.6968 0.750 0.6501 0.01290 0.00747 -0.1335 0.7029 0.6979 1.000 0.6721 0.01293 0.00755 -0.1326 0.7010 0.6991 1.250 0.6954 0.01301 0.00766 -0.1320 0.6991 0.7003 1.500 0.7199 0.01307 0.00775 -0.1317 0.6972 0.7014 1.750 0.7457 0.01310 0.00778 -0.1316 0.6954 0.7025 2.000 0.7726 0.01310 0.00780 -0.1317 0.6938 0.7037 2.250 0.8002 0.01311 0.00780 -0.1319 0.6924 0.7050 2.500 0.8285 0.01311 0.00779 -0.1323 0.6911 0.7064 2.750 0.8580 0.01310 0.00777 -0.1329 0.6898 0.7076 3.000 0.8879 0.01315 0.00781 -0.1336 0.6886 0.7087 3.250 0.9111 0.01328 0.00798 -0.1331 0.6867 0.7099 3.500 0.9305 0.01340 0.00816 -0.1317 0.6840 0.7111 3.750 0.9539 0.01346 0.00825 -0.1312 0.6815 0.7122 4.000 0.9799 0.01343 0.00825 -0.1311 0.6794 0.7134 4.250 1.0082 0.01332 0.00816 -0.1314 0.6774 0.7146 4.500 1.0396 0.01316 0.00802 -0.1323 0.6755 0.7156 4.750 1.0743 0.01303 0.00787 -0.1338 0.6735 0.7166 5.000 1.0892 0.01310 0.00805 -0.1315 0.6696 0.7178 5.250 1.1110 0.01302 0.00803 -0.1305 0.6658 0.7190 5.500 1.1411 0.01271 0.00774 -0.1310 0.6621 0.7202 5.750 1.1766 0.01245 0.00744 -0.1326 0.6589 0.7215 6.000 1.1893 0.01247 0.00757 -0.1298 0.6539 0.7229 6.250 1.2124 0.01221 0.00735 -0.1289 0.6481 0.7245 6.500 1.2366 0.01194 0.00707 -0.1281 0.6416 0.7260 6.750 1.2489 0.01180 0.00697 -0.1250 0.6333 0.7275 7.000 1.2632 0.01168 0.00687 -0.1223 0.6249 0.7287 7.250 1.2731 0.01162 0.00688 -0.1188 0.6177 0.7301 7.500 1.2825 0.01165 0.00697 -0.1153 0.6096 0.7315 7.750 1.2949 0.01174 0.00709 -0.1124 0.6012 0.7331 8.000 1.3015 0.01197 0.00739 -0.1085 0.5907 0.7348 8.250 1.3098 0.01224 0.00770 -0.1051 0.5791 0.7365 8.500 1.3145 0.01267 0.00812 -0.1013 0.5630 0.7383 8.750 1.3148 0.01336 0.00876 -0.0971 0.5415 0.7402 9.000 1.3135 0.01437 0.00970 -0.0931 0.5157 0.7422 9.250 1.3007 0.01614 0.01129 -0.0880 0.4782 0.7442 9.500 1.2897 0.01830 0.01327 -0.0840 0.4390 0.7462 9.750 1.2769 0.02077 0.01555 -0.0801 0.3997 0.7481 10.000 1.2630 0.02344 0.01800 -0.0765 0.3582 0.7499 10.250 1.2565 0.02577 0.02018 -0.0737 0.3226 0.7519 10.500 1.2522 0.02809 0.02234 -0.0714 0.2876 0.7539 10.750 1.2460 0.03061 0.02464 -0.0691 0.2494 0.7559 11.000 1.2441 0.03288 0.02673 -0.0672 0.2135 0.7579 11.250 1.2432 0.03515 0.02881 -0.0655 0.1792 0.7598 11.500 1.2465 0.03734 0.03085 -0.0645 0.1485 0.7619 11.750 1.2495 0.03953 0.03289 -0.0634 0.1192 0.7642 12.000 1.2533 0.04166 0.03488 -0.0624 0.0946 0.7666 12.250 1.2592 0.04363 0.03678 -0.0616 0.0767 0.7693 12.500 1.2661 0.04553 0.03864 -0.0608 0.0640 0.7721 12.750 1.2735 0.04743 0.04051 -0.0601 0.0557 0.7750 13.000 1.2836 0.04935 0.04244 -0.0600 0.0491 0.7782 13.250 1.2945 0.05116 0.04432 -0.0599 0.0448 0.7820 13.500 1.3046 0.05307 0.04629 -0.0597 0.0416 0.7860 13.750 1.3103 0.05531 0.04854 -0.0592 0.0377 0.7903 14.000 1.3245 0.05711 0.05047 -0.0597 0.0355 0.7952 14.250 1.3358 0.05912 0.05255 -0.0600 0.0332 0.8012 14.500 1.3385 0.06191 0.05540 -0.0597 0.0308 0.8074 14.750 1.3534 0.06383 0.05745 -0.0605 0.0290 0.8165 15.000 1.3675 0.06599 0.05975 -0.0615 0.0273 0.8297 15.250 1.3800 0.06903 0.06291 -0.0634 0.0253 0.8521 15.500 1.4063 0.07290 0.06706 -0.0689 0.0234 0.9256 15.750 1.4145 0.07523 0.06945 -0.0684 0.0221 1.0000 16.000 1.4201 0.07754 0.07180 -0.0681 0.0210 1.0000 16.250 1.4207 0.08043 0.07472 -0.0677 0.0198 1.0000 16.500 1.4190 0.08360 0.07796 -0.0672 0.0189 1.0000 16.750 1.4246 0.08599 0.08045 -0.0671 0.0182 1.0000 17.000 1.4285 0.08861 0.08315 -0.0670 0.0174 1.0000 17.250 1.4321 0.09129 0.08590 -0.0669 0.0165 1.0000 17.500 1.4330 0.09428 0.08893 -0.0670 0.0158 1.0000 17.750 1.4273 0.09805 0.09276 -0.0668 0.0153 1.0000