XFOIL Version 6.96 Calculated polar for: FX 74-130 WP1 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -10.250 -0.1271 0.08430 0.08083 -0.1184 0.8158 0.0107 -10.000 -0.1291 0.07931 0.07587 -0.1206 0.8145 0.0090 -9.750 -0.1279 0.07587 0.07244 -0.1222 0.8130 0.0088 -9.500 -0.1300 0.07175 0.06837 -0.1241 0.8114 0.0084 -9.250 -0.1340 0.06728 0.06392 -0.1266 0.8097 0.0082 -9.000 -0.1415 0.06220 0.05889 -0.1304 0.8077 0.0080 -8.750 -0.1563 0.05690 0.05356 -0.1340 0.8056 0.0077 -8.500 -0.1760 0.05282 0.04942 -0.1338 0.8036 0.0075 -8.000 -0.2246 0.03816 0.03425 -0.1300 0.7993 0.0067 -7.750 -0.2312 0.03230 0.02802 -0.1273 0.7975 0.0066 -7.500 -0.2263 0.02864 0.02404 -0.1254 0.7960 0.0068 -7.250 -0.2160 0.02553 0.02058 -0.1238 0.7945 0.0069 -7.000 -0.1983 0.02389 0.01870 -0.1230 0.7931 0.0072 -6.750 -0.1806 0.02171 0.01619 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3.000 0.8446 0.00883 0.00405 -0.1216 0.7252 0.8420 3.250 0.8728 0.00876 0.00400 -0.1219 0.7204 0.8428 3.500 0.8992 0.00874 0.00404 -0.1219 0.7137 0.8436 3.750 0.9266 0.00868 0.00398 -0.1220 0.7064 0.8443 4.000 0.9525 0.00867 0.00401 -0.1218 0.6962 0.8451 4.250 0.9782 0.00865 0.00400 -0.1215 0.6828 0.8460 4.500 1.0026 0.00869 0.00398 -0.1210 0.6647 0.8470 4.750 1.0241 0.00884 0.00404 -0.1199 0.6370 0.8478 5.000 1.0383 0.00922 0.00420 -0.1173 0.5842 0.8487 5.250 1.0330 0.01018 0.00471 -0.1110 0.4990 0.8499 5.500 1.0239 0.01114 0.00534 -0.1042 0.4336 0.8514 5.750 1.0181 0.01211 0.00606 -0.0983 0.3787 0.8529 6.000 1.0168 0.01310 0.00683 -0.0936 0.3292 0.8546 6.250 1.0166 0.01419 0.00769 -0.0894 0.2796 0.8563 6.500 1.0205 0.01525 0.00854 -0.0861 0.2343 0.8576 6.750 1.0244 0.01640 0.00945 -0.0830 0.1857 0.8588 7.000 1.0321 0.01744 0.01030 -0.0805 0.1471 0.8599 7.250 1.0420 0.01840 0.01111 -0.0784 0.1156 0.8610 7.500 1.0527 0.01935 0.01195 -0.0765 0.0880 0.8620 8.000 1.0769 0.02115 0.01357 -0.0731 0.0487 0.8638 8.250 1.0908 0.02196 0.01435 -0.0716 0.0387 0.8647 8.500 1.1058 0.02270 0.01511 -0.0704 0.0321 0.8656 8.750 1.1207 0.02348 0.01591 -0.0691 0.0277 0.8667 9.000 1.1358 0.02425 0.01673 -0.0679 0.0245 0.8679 9.250 1.1496 0.02514 0.01764 -0.0666 0.0216 0.8692 9.500 1.1644 0.02596 0.01853 -0.0654 0.0202 0.8703 9.750 1.1798 0.02677 0.01940 -0.0644 0.0188 0.8714 10.000 1.1945 0.02763 0.02031 -0.0633 0.0171 0.8725 10.250 1.2072 0.02867 0.02137 -0.0620 0.0155 0.8737 10.500 1.2205 0.02967 0.02246 -0.0609 0.0143 0.8748 10.750 1.2355 0.03056 0.02342 -0.0599 0.0133 0.8760 11.250 1.2619 0.03261 0.02562 -0.0578 0.0115 0.8783 11.500 1.2731 0.03382 0.02688 -0.0565 0.0106 0.8796 11.750 1.2837 0.03512 0.02826 -0.0553 0.0098 0.8811 12.000 1.2966 0.03623 0.02947 -0.0544 0.0092 0.8826 12.250 1.3094 0.03736 0.03068 -0.0535 0.0083 0.8843 12.500 1.3213 0.03861 0.03200 -0.0525 0.0076 0.8861 12.750 1.3309 0.04010 0.03356 -0.0515 0.0070 0.8880 13.000 1.3397 0.04170 0.03527 -0.0504 0.0066 0.8899 13.250 1.3490 0.04327 0.03695 -0.0494 0.0063 0.8919 13.500 1.3576 0.04491 0.03872 -0.0485 0.0059 0.8944 13.750 1.3662 0.04658 0.04049 -0.0476 0.0055 0.8974 14.000 1.3735 0.04840 0.04242 -0.0466 0.0053 0.9010 14.500 1.3856 0.05237 0.04662 -0.0449 0.0048 0.9105 14.750 1.3876 0.05484 0.04922 -0.0439 0.0046 0.9175 15.000 1.3878 0.05730 0.05186 -0.0427 0.0045 0.9318 15.250 1.3884 0.05972 0.05445 -0.0417 0.0044 1.0000 15.500 1.3911 0.06250 0.05738 -0.0414 0.0042 1.0000 15.750 1.3926 0.06550 0.06053 -0.0412 0.0041 1.0000 16.000 1.3936 0.06862 0.06380 -0.0411 0.0040 1.0000 16.250 1.3923 0.07214 0.06747 -0.0412 0.0039 1.0000 16.500 1.3902 0.07586 0.07135 -0.0415 0.0038 1.0000 16.750 1.3870 0.07986 0.07551 -0.0421 0.0038 1.0000 17.000 1.3831 0.08409 0.07990 -0.0429 0.0037 1.0000 17.250 1.3775 0.08868 0.08465 -0.0439 0.0036 1.0000 17.500 1.3706 0.09363 0.08977 -0.0453 0.0035 1.0000 17.750 1.3630 0.09888 0.09518 -0.0471 0.0035 1.0000 18.000 1.3544 0.10445 0.10092 -0.0493 0.0034 1.0000 18.250 1.3451 0.11032 0.10696 -0.0518 0.0034 1.0000 18.500 1.3343 0.11665 0.11345 -0.0548 0.0034 1.0000 18.750 1.3226 0.12336 0.12033 -0.0583 0.0033 1.0000 19.000 1.3094 0.13059 0.12773 -0.0623 0.0033 1.0000 19.250 1.2953 0.13827 0.13558 -0.0668 0.0033 1.0000