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 = 0.200 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -13.250 -0.0970 0.11361 0.10853 -0.1230 0.7918 0.0217 -13.000 -0.0858 0.11170 0.10660 -0.1239 0.7903 0.0223 -12.750 -0.0975 0.10250 0.09739 -0.1276 0.7893 0.0168 -12.500 -0.0998 0.09711 0.09202 -0.1300 0.7879 0.0168 -12.250 -0.0945 0.09400 0.08888 -0.1317 0.7864 0.0166 -12.000 -0.0936 0.08991 0.08481 -0.1337 0.7849 0.0165 -11.750 -0.0952 0.08541 0.08036 -0.1358 0.7831 0.0163 -11.500 -0.0932 0.08190 0.07686 -0.1377 0.7813 0.0158 -11.250 -0.1198 0.07018 0.06520 -0.1440 0.7797 0.0158 -11.000 -0.1431 0.06109 0.05603 -0.1504 0.7780 0.0150 -10.750 -0.1766 0.05375 0.04853 -0.1545 0.7759 0.0150 -10.500 -0.2029 0.04874 0.04332 -0.1558 0.7738 0.0149 -10.250 -0.2196 0.04529 0.03969 -0.1557 0.7720 0.0149 -10.000 -0.2393 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0.01804 0.01088 -0.1208 0.7041 0.6889 -0.250 0.4712 0.01821 0.01100 -0.1200 0.7014 0.6914 0.000 0.4955 0.01829 0.01103 -0.1199 0.6994 0.6938 0.250 0.5208 0.01836 0.01106 -0.1198 0.6979 0.6955 0.500 0.5471 0.01840 0.01108 -0.1198 0.6965 0.6968 0.750 0.5749 0.01841 0.01105 -0.1200 0.6953 0.6980 1.000 0.6036 0.01839 0.01100 -0.1204 0.6943 0.6993 1.250 0.6330 0.01837 0.01095 -0.1210 0.6934 0.7008 1.500 0.6358 0.01911 0.01178 -0.1171 0.6883 0.7027 1.750 0.6529 0.01941 0.01210 -0.1157 0.6853 0.7042 2.000 0.6766 0.01951 0.01219 -0.1153 0.6832 0.7056 2.250 0.7026 0.01957 0.01224 -0.1153 0.6817 0.7071 2.500 0.7300 0.01961 0.01226 -0.1156 0.6805 0.7088 3.000 0.7900 0.01953 0.01218 -0.1169 0.6786 0.7115 3.500 0.7866 0.02106 0.01386 -0.1075 0.6677 0.7141 3.750 0.8141 0.02104 0.01386 -0.1077 0.6663 0.7153 4.000 0.8438 0.02098 0.01384 -0.1082 0.6652 0.7165 4.250 0.8764 0.02085 0.01374 -0.1093 0.6642 0.7177 4.500 0.9102 0.02070 0.01362 -0.1106 0.6634 0.7194 5.000 0.8484 0.02426 0.01728 -0.0928 0.6435 0.7238 5.250 0.9026 0.02301 0.01608 -0.0965 0.6461 0.7250 5.500 0.9573 0.02198 0.01509 -0.1007 0.6478 0.7262 6.000 0.9377 0.02471 0.01795 -0.0906 0.6312 0.7291 6.250 0.9902 0.02333 0.01666 -0.0938 0.6329 0.7302 6.750 0.9894 0.02579 0.01926 -0.0873 0.6165 0.7337 7.000 1.0492 0.02375 0.01731 -0.0910 0.6189 0.7354 7.500 1.0265 0.02777 0.02145 -0.0827 0.5942 0.7398 7.750 1.0624 0.02690 0.02066 -0.0836 0.5914 0.7417 8.250 1.0886 0.02803 0.02196 -0.0807 0.5706 0.7449 8.750 1.1382 0.02755 0.02160 -0.0800 0.5447 0.7487 9.000 1.1511 0.02822 0.02230 -0.0787 0.5235 0.7508 9.250 1.1875 0.02709 0.02109 -0.0792 0.4942 0.7532 9.500 1.2139 0.02663 0.02038 -0.0786 0.4528 0.7554 9.750 1.2202 0.02768 0.02120 -0.0764 0.4135 0.7577 10.000 1.2159 0.02954 0.02282 -0.0735 0.3712 0.7599 10.250 1.2128 0.03155 0.02466 -0.0709 0.3364 0.7622 10.500 1.2076 0.03385 0.02678 -0.0685 0.3004 0.7651 10.750 1.2043 0.03616 0.02892 -0.0664 0.2664 0.7677 11.000 1.2028 0.03846 0.03106 -0.0647 0.2350 0.7706 11.500 1.2028 0.04313 0.03546 -0.0618 0.1739 0.7756 11.750 1.2046 0.04547 0.03766 -0.0608 0.1462 0.7785 12.000 1.2085 0.04765 0.03977 -0.0599 0.1235 0.7817 12.250 1.2132 0.04981 0.04185 -0.0591 0.1042 0.7852 12.750 1.2260 0.05404 0.04604 -0.0580 0.0754 0.7929 13.000 1.2341 0.05609 0.04812 -0.0577 0.0676 0.7977 13.250 1.2412 0.05823 0.05029 -0.0574 0.0596 0.8029 13.500 1.2500 0.06036 0.05253 -0.0573 0.0542 0.8092 13.750 1.2578 0.06262 0.05484 -0.0572 0.0491 0.8167 14.000 1.2667 0.06493 0.05726 -0.0574 0.0453 0.8273 14.250 1.2773 0.06726 0.05975 -0.0580 0.0420 0.8433 14.500 1.2878 0.07024 0.06289 -0.0595 0.0386 0.8796 14.750 1.2915 0.07218 0.06494 -0.0585 0.0367 1.0000 15.000 1.2968 0.07454 0.06741 -0.0581 0.0347 1.0000 15.250 1.3018 0.07698 0.06991 -0.0579 0.0326 1.0000 15.500 1.3032 0.07984 0.07281 -0.0576 0.0309 1.0000 15.750 1.3079 0.08234 0.07542 -0.0574 0.0293 1.0000 16.000 1.3124 0.08485 0.07805 -0.0573 0.0279 1.0000 16.250 1.3160 0.08753 0.08081 -0.0572 0.0264 1.0000 16.500 1.3180 0.09042 0.08377 -0.0572 0.0252 1.0000 16.750 1.3180 0.09359 0.08698 -0.0573 0.0239 1.0000 17.000 1.3218 0.09631 0.08984 -0.0574 0.0229 1.0000 17.250 1.3246 0.09918 0.09283 -0.0576 0.0218 1.0000 17.500 1.3274 0.10214 0.09590 -0.0581 0.0205 1.0000 17.750 1.3277 0.10538 0.09923 -0.0586 0.0197 1.0000 18.000 1.3259 0.10892 0.10281 -0.0591 0.0190 1.0000 18.250 1.3278 0.11202 0.10607 -0.0597 0.0182 1.0000 18.500 1.3289 0.11524 0.10943 -0.0603 0.0175 1.0000 18.750 1.3294 0.11866 0.11297 -0.0613 0.0166 1.0000 19.000 1.3292 0.12216 0.11658 -0.0623 0.0161 1.0000 19.250 1.3287 0.12575 0.12027 -0.0635 0.0157 1.0000