XFOIL Version 6.94 Calculated polar for: GOE 190 (MVA MK.18) AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.450 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.6461 0.01047 0.00354 -0.1455 0.5628 0.3458 0.500 0.6988 0.01074 0.00366 -0.1445 0.5471 0.3527 1.000 0.7517 0.01078 0.00367 -0.1436 0.5338 0.3593 1.500 0.8043 0.01101 0.00383 -0.1426 0.5209 0.3651 2.000 0.8576 0.01118 0.00400 -0.1418 0.5101 0.3715 2.500 0.9097 0.01140 0.00415 -0.1408 0.4981 0.3775 3.000 0.9606 0.01154 0.00438 -0.1395 0.4843 0.3856 3.500 1.0051 0.01165 0.00443 -0.1369 0.4543 0.3931 4.000 1.0501 0.01186 0.00452 -0.1344 0.4250 0.4003 4.500 1.0869 0.01236 0.00471 -0.1305 0.3603 0.4088 5.000 1.1295 0.01288 0.00512 -0.1278 0.3296 0.4185 5.500 1.1621 0.01376 0.00568 -0.1234 0.2696 0.4277 6.000 1.1957 0.01464 0.00634 -0.1192 0.2183 0.4375 6.500 1.2148 0.01635 0.00755 -0.1128 0.1351 0.4465 7.000 1.2064 0.01948 0.00996 -0.1022 0.0036 0.4538 7.500 1.2397 0.02031 0.01088 -0.0984 0.0029 0.4653 8.000 1.2706 0.02122 0.01193 -0.0943 0.0028 0.4781 8.500 1.2997 0.02226 0.01313 -0.0901 0.0028 0.4906 9.000 1.3258 0.02350 0.01452 -0.0858 0.0029 0.5040 9.500 1.3489 0.02493 0.01615 -0.0813 0.0029 0.5192 10.000 1.3693 0.02662 0.01806 -0.0769 0.0030 0.5386 10.500 1.3859 0.02867 0.02040 -0.0726 0.0032 0.5710 12.000 1.4587 0.04021 0.03316 -0.0734 0.0037 1.0000 12.500 1.4563 0.04586 0.03902 -0.0716 0.0038 1.0000 13.000 1.4604 0.05111 0.04445 -0.0706 0.0040 1.0000 13.500 1.4586 0.05738 0.05092 -0.0702 0.0042 1.0000 14.000 1.4487 0.06504 0.05881 -0.0705 0.0044 1.0000 14.500 1.4337 0.07372 0.06770 -0.0714 0.0046 1.0000 15.000 1.4154 0.08307 0.07728 -0.0728 0.0048 1.0000 15.500 1.3964 0.09283 0.08724 -0.0747 0.0049 1.0000 16.000 1.3756 0.10310 0.09767 -0.0770 0.0051 1.0000 16.500 1.3646 0.11212 0.10683 -0.0794 0.0052 1.0000 17.000 1.3649 0.11969 0.11458 -0.0816 0.0055 1.0000 17.500 1.3647 0.12717 0.12224 -0.0837 0.0061 1.0000 18.000 1.3656 0.13408 0.12924 -0.0856 0.0065 1.0000 18.500 1.3762 0.13930 0.13454 -0.0868 0.0071 1.0000 19.000 1.4106 0.13830 0.13357 -0.0826 0.0087 1.0000 19.500 1.4388 0.13984 0.13539 -0.0803 0.0110 1.0000 20.000 1.2077 0.16795 0.16478 -0.1080 0.0088 1.0000 20.500 1.1840 0.18100 0.17830 -0.1163 0.0095 1.0000 21.000 1.1643 0.19297 0.19062 -0.1229 0.0107 1.0000 21.500 1.1300 0.21121 0.20924 -0.1340 0.0112 1.0000 22.000 0.9922 0.28070 0.27921 -0.1647 0.0107 1.0000 22.500 0.9774 0.31033 0.30882 -0.1722 0.0195 1.0000 23.000 0.9779 0.32424 0.32272 -0.1769 0.0179 1.0000 23.500 0.9846 0.33319 0.33169 -0.1799 0.0166 1.0000 24.000 0.9879 0.34527 0.34377 -0.1837 0.0152 1.0000 24.500 0.9942 0.35410 0.35262 -0.1866 0.0137 1.0000 25.000 0.9975 0.36631 0.36483 -0.1902 0.0123 1.0000 25.500 1.0032 0.37525 0.37379 -0.1930 0.0111 1.0000 26.000 1.0066 0.38740 0.38595 -0.1964 0.0102 1.0000 26.500 1.0112 0.39709 0.39565 -0.1994 0.0091 1.0000 27.000 1.0177 0.40398 0.40256 -0.2014 0.0087 1.0000 27.500 1.0185 0.41947 0.41805 -0.2055 0.0077 1.0000 28.000 1.0225 0.42876 0.42736 -0.2082 0.0071 1.0000 28.500 1.0269 0.43641 0.43503 -0.2105 0.0068 1.0000 29.000 1.0281 0.45105 0.44967 -0.2140 0.0064 1.0000 29.500 1.0308 0.46216 0.46080 -0.2168 0.0059 1.0000 30.000 1.0333 0.47234 0.47100 -0.2195 0.0056 1.0000 30.500 1.0355 0.48144 0.48013 -0.2221 0.0053 1.0000 31.000 1.0384 0.48876 0.48747 -0.2240 0.0051 1.0000 31.500 1.0386 0.50159 0.50031 -0.2271 0.0051 1.0000 32.000 1.0394 0.51345 0.51219 -0.2300 0.0050 1.0000 32.500 1.0404 0.52538 0.52414 -0.2326 0.0048 1.0000 33.000 1.0409 0.53600 0.53478 -0.2351 0.0045 1.0000 33.500 1.0411 0.54609 0.54489 -0.2376 0.0044 1.0000 34.000 1.0410 0.55613 0.55495 -0.2401 0.0044 1.0000 34.500 1.0405 0.56585 0.56469 -0.2425 0.0043 1.0000 35.000 1.0396 0.57558 0.57445 -0.2448 0.0043 1.0000 35.500 1.0385 0.58505 0.58394 -0.2472 0.0042 1.0000 36.000 1.0370 0.59445 0.59336 -0.2495 0.0041 1.0000 36.500 1.0352 0.60356 0.60250 -0.2517 0.0041 1.0000 37.000 1.0331 0.61264 0.61161 -0.2540 0.0041 1.0000 37.500 1.0306 0.62141 0.62041 -0.2562 0.0040 1.0000 38.000 1.0278 0.62994 0.62896 -0.2583 0.0040 1.0000 38.500 1.0247 0.63832 0.63736 -0.2604 0.0039 1.0000 39.000 1.0213 0.64650 0.64557 -0.2625 0.0039 1.0000 39.500 1.0175 0.65453 0.65364 -0.2645 0.0039 1.0000 40.000 1.0134 0.66211 0.66124 -0.2665 0.0039 1.0000 40.500 1.0091 0.66968 0.66884 -0.2685 0.0039 1.0000 41.000 1.0043 0.67651 0.67570 -0.2704 0.0038 1.0000 41.500 0.9992 0.68281 0.68202 -0.2723 0.0038 1.0000 43.000 0.9833 0.70680 0.70608 -0.2777 0.0037 1.0000 43.500 0.9778 0.71438 0.71368 -0.2793 0.0036 1.0000 44.000 0.9720 0.72165 0.72099 -0.2809 0.0033 1.0000 44.500 0.9657 0.72795 0.72731 -0.2825 0.0030 1.0000 45.000 0.9590 0.73336 0.73274 -0.2840 0.0028 1.0000 45.500 0.9517 0.73773 0.73713 -0.2856 0.0027 1.0000 46.000 0.9437 0.74081 0.74024 -0.2871 0.0026 1.0000 47.000 0.9293 0.75376 0.75322 -0.2899 0.0025 1.0000 47.500 0.9221 0.75965 0.75913 -0.2911 0.0025 1.0000 48.000 0.9147 0.76510 0.76460 -0.2922 0.0023 1.0000 48.500 0.9066 0.76907 0.76860 -0.2934 0.0020 1.0000 49.000 0.8980 0.77185 0.77140 -0.2946 0.0018 1.0000 49.500 0.8891 0.77394 0.77351 -0.2958 0.0017 1.0000 50.000 0.8796 0.77490 0.77450 -0.2970 0.0016 1.0000 50.500 0.8699 0.77554 0.77515 -0.2981 0.0015 1.0000 51.500 0.8522 0.78329 0.78293 -0.2998 0.0015 1.0000 52.000 0.8432 0.78574 0.78540 -0.3006 0.0015 1.0000 52.500 0.8338 0.78721 0.78688 -0.3014 0.0014 1.0000 53.000 0.8243 0.78846 0.78815 -0.3021 0.0013 1.0000 53.500 0.8143 0.78875 0.78847 -0.3028 0.0012 1.0000 54.000 0.8041 0.78820 0.78793 -0.3035 0.0011 1.0000 54.500 0.7936 0.78676 0.78650 -0.3042 0.0009 1.0000 55.000 0.7830 0.78498 0.78475 -0.3048 0.0008 1.0000 55.500 0.7720 0.78228 0.78206 -0.3055 0.0008 1.0000 56.000 0.7607 0.77878 0.77858 -0.3061 0.0007 1.0000 56.500 0.7490 0.77465 0.77447 -0.3067 0.0007 1.0000 57.500 0.7284 0.77323 0.77307 -0.3072 0.0006 1.0000 58.000 0.7175 0.77002 0.76988 -0.3075 0.0006 1.0000 58.500 0.7063 0.76623 0.76610 -0.3077 0.0005 1.0000 59.000 0.6948 0.76145 0.76134 -0.3080 0.0004 1.0000 59.500 0.6831 0.75590 0.75581 -0.3082 0.0004 1.0000 60.000 0.6711 0.74968 0.74960 -0.3085 0.0003 1.0000