XFOIL Version 6.94 Calculated polar for: NACA 65(1)-212 a=0.6 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.300 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.1416 0.01005 0.00503 -0.0300 0.7612 0.7973 0.500 0.1964 0.01046 0.00543 -0.0307 0.7506 0.8172 1.000 0.2512 0.01049 0.00557 -0.0307 0.7456 0.8396 1.500 0.3031 0.01080 0.00601 -0.0298 0.7390 0.8564 2.000 0.3562 0.01108 0.00638 -0.0293 0.7314 0.8725 2.500 0.4075 0.01103 0.00633 -0.0288 0.7219 0.9108 3.000 0.4647 0.01068 0.00593 -0.0279 0.7000 0.9278 3.500 0.5238 0.00968 0.00489 -0.0273 0.6693 0.9435 4.000 0.5838 0.00923 0.00416 -0.0275 0.6009 0.9578 4.500 0.6254 0.01207 0.00509 -0.0275 0.1992 0.9734 5.000 0.6636 0.01500 0.00727 -0.0264 0.0318 0.9886 5.500 0.7039 0.01718 0.00971 -0.0248 0.0270 0.9984 6.000 0.7260 0.01913 0.01180 -0.0193 0.0263 1.0000 6.500 0.7705 0.02227 0.01543 -0.0172 0.0258 1.0000 7.000 0.8052 0.02405 0.01738 -0.0142 0.0216 1.0000 7.500 0.8411 0.02596 0.01946 -0.0113 0.0204 1.0000 8.000 0.8762 0.02870 0.02246 -0.0083 0.0198 1.0000 8.500 0.9024 0.03162 0.02566 -0.0041 0.0191 1.0000 9.000 0.9183 0.03460 0.02895 0.0014 0.0185 1.0000 9.500 0.9148 0.03457 0.02898 0.0101 0.0156 1.0000 10.000 0.9131 0.03597 0.03052 0.0174 0.0144 1.0000 10.500 0.9106 0.03762 0.03226 0.0237 0.0134 1.0000 11.000 0.9011 0.04088 0.03573 0.0297 0.0125 1.0000 11.500 0.8695 0.04701 0.04227 0.0360 0.0119 1.0000 12.000 0.8234 0.05460 0.05030 0.0409 0.0116 1.0000 12.500 0.7808 0.06228 0.05833 0.0429 0.0115 1.0000 13.000 0.7421 0.07071 0.06705 0.0423 0.0114 1.0000 13.500 0.7060 0.08066 0.07724 0.0388 0.0115 1.0000 14.000 0.6797 0.09147 0.08823 0.0332 0.0116 1.0000 14.500 0.6570 0.10510 0.10201 0.0253 0.0118 1.0000 15.000 0.6356 0.12270 0.11967 0.0172 0.0123 1.0000 16.500 0.5876 0.17228 0.16911 0.0000 0.0233 1.0000 17.000 0.5961 0.18046 0.17728 -0.0031 0.0232 1.0000 17.500 0.6056 0.18809 0.18489 -0.0062 0.0230 1.0000 18.000 0.6168 0.19401 0.19083 -0.0092 0.0221 1.0000 18.500 0.6264 0.19954 0.19634 -0.0125 0.0201 1.0000 19.000 0.6362 0.20632 0.20310 -0.0157 0.0185 1.0000 19.500 0.6466 0.21311 0.20988 -0.0187 0.0173 1.0000 20.000 0.6575 0.21976 0.21653 -0.0217 0.0163 1.0000 20.500 0.6686 0.22621 0.22297 -0.0246 0.0154 1.0000 21.000 0.6800 0.23211 0.22885 -0.0273 0.0147 1.0000 21.500 0.6916 0.23772 0.23446 -0.0300 0.0141 1.0000 22.000 0.7034 0.24332 0.24005 -0.0327 0.0135 1.0000 22.500 0.7175 0.24889 0.24563 -0.0351 0.0127 1.0000 23.000 0.7312 0.26240 0.25911 -0.0377 0.0112 1.0000 23.500 0.7393 0.26642 0.26313 -0.0408 0.0111 1.0000 24.000 0.7457 0.26856 0.26525 -0.0441 0.0105 1.0000 24.500 0.7557 0.27328 0.26997 -0.0471 0.0091 1.0000 25.000 0.7666 0.27905 0.27574 -0.0500 0.0082 1.0000 25.500 0.7774 0.28473 0.28150 -0.0529 0.0076 1.0000 26.000 0.7881 0.29027 0.28705 -0.0558 0.0071 1.0000 26.500 0.7999 0.29620 0.29297 -0.0586 0.0067 1.0000 27.000 0.8132 0.30621 0.30299 -0.0612 0.0064 1.0000 27.500 0.8193 0.31055 0.30733 -0.0644 0.0063 1.0000 28.000 0.8259 0.31490 0.31168 -0.0676 0.0061 1.0000 28.500 0.8354 0.32070 0.31749 -0.0705 0.0053 1.0000 29.000 0.8445 0.32640 0.32320 -0.0735 0.0047 1.0000 29.500 0.8532 0.33181 0.32861 -0.0766 0.0043 1.0000 30.000 0.8618 0.33725 0.33406 -0.0796 0.0041 1.0000 30.500 0.8710 0.34406 0.34086 -0.0825 0.0040 1.0000 31.000 0.8780 0.34979 0.34659 -0.0855 0.0040 1.0000 31.500 0.8849 0.35550 0.35232 -0.0885 0.0040 1.0000 32.000 0.8918 0.36123 0.35806 -0.0915 0.0040 1.0000 32.500 0.8984 0.36692 0.36376 -0.0945 0.0040 1.0000 33.000 0.9048 0.37260 0.36951 -0.0975 0.0040 1.0000 33.500 0.9110 0.37823 0.37516 -0.1005 0.0039 1.0000 34.000 0.9169 0.38382 0.38077 -0.1035 0.0039 1.0000 34.500 0.9224 0.38937 0.38633 -0.1065 0.0039 1.0000 35.000 0.9277 0.39485 0.39184 -0.1095 0.0039 1.0000 35.500 0.9326 0.40027 0.39728 -0.1124 0.0039 1.0000 36.000 0.9372 0.40563 0.40265 -0.1154 0.0039 1.0000 36.500 0.9415 0.41091 0.40795 -0.1184 0.0039 1.0000 37.000 0.9454 0.41615 0.41321 -0.1214 0.0039 1.0000 37.500 0.9489 0.42128 0.41836 -0.1244 0.0039 1.0000 38.000 0.9521 0.42636 0.42346 -0.1274 0.0039 1.0000 38.500 0.9550 0.43134 0.42849 -0.1303 0.0039 1.0000 39.000 0.9575 0.43626 0.43343 -0.1333 0.0039 1.0000 39.500 0.9597 0.44107 0.43827 -0.1363 0.0039 1.0000 40.000 0.9615 0.44583 0.44305 -0.1392 0.0038 1.0000 40.500 0.9629 0.45048 0.44773 -0.1422 0.0038 1.0000 41.000 0.9640 0.45506 0.45233 -0.1452 0.0038 1.0000 41.500 0.9648 0.45952 0.45682 -0.1481 0.0038 1.0000 42.000 0.9653 0.46394 0.46126 -0.1510 0.0038 1.0000 42.500 0.9654 0.46824 0.46558 -0.1540 0.0038 1.0000 43.000 0.9652 0.47248 0.46988 -0.1569 0.0038 1.0000 43.500 0.9646 0.47662 0.47405 -0.1598 0.0038 1.0000 44.000 0.9638 0.48069 0.47814 -0.1627 0.0038 1.0000 44.500 0.9626 0.48470 0.48218 -0.1656 0.0037 1.0000 45.000 0.9611 0.48868 0.48618 -0.1684 0.0037 1.0000 45.500 0.9596 0.49286 0.49038 -0.1712 0.0036 1.0000 46.000 0.9580 0.49752 0.49504 -0.1737 0.0035 1.0000 46.500 0.9560 0.50205 0.49959 -0.1763 0.0033 1.0000 47.000 0.9536 0.50625 0.50380 -0.1790 0.0033 1.0000 47.500 0.9509 0.51031 0.50788 -0.1816 0.0032 1.0000 48.000 0.9479 0.51423 0.51181 -0.1843 0.0032 1.0000 48.500 0.9445 0.51804 0.51564 -0.1869 0.0031 1.0000 49.000 0.9408 0.52156 0.51917 -0.1896 0.0031 1.0000 49.500 0.9368 0.52501 0.52265 -0.1923 0.0031 1.0000 50.000 0.9325 0.52846 0.52611 -0.1949 0.0031 1.0000 50.500 0.9279 0.53168 0.52939 -0.1976 0.0031 1.0000 51.000 0.9231 0.53483 0.53256 -0.2003 0.0031 1.0000 51.500 0.9180 0.53790 0.53566 -0.2029 0.0030 1.0000 52.000 0.9126 0.54080 0.53858 -0.2056 0.0030 1.0000 52.500 0.9070 0.54362 0.54142 -0.2083 0.0030 1.0000 53.000 0.9008 0.54618 0.54400 -0.2108 0.0030 0.9994 53.500 0.8943 0.54857 0.54641 -0.2133 0.0030 0.9986 54.000 0.8876 0.55090 0.54875 -0.2157 0.0030 0.9978 54.500 0.8806 0.55303 0.55091 -0.2182 0.0030 0.9970 55.000 0.8734 0.55507 0.55297 -0.2207 0.0030 0.9962 55.500 0.8659 0.55695 0.55486 -0.2231 0.0030 0.9955 56.000 0.8582 0.55879 0.55673 -0.2256 0.0030 0.9948 56.500 0.8503 0.56055 0.55851 -0.2280 0.0030 0.9941 57.000 0.8421 0.56207 0.56008 -0.2305 0.0030 0.9934 57.500 0.8338 0.56359 0.56162 -0.2329 0.0030 0.9927 58.000 0.8252 0.56497 0.56302 -0.2354 0.0030 0.9920 58.500 0.8165 0.56623 0.56431 -0.2378 0.0029 0.9914 59.000 0.8076 0.56744 0.56555 -0.2403 0.0029 0.9907 59.500 0.7984 0.56854 0.56666 -0.2428 0.0029 0.9901 60.000 0.7892 0.56954 0.56769 -0.2452 0.0029 0.9895