XFOIL Version 6.94 Calculated polar for: NACA 65-410 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 0.3343 0.00715 0.00281 -0.0795 0.7896 0.7971 0.500 0.3892 0.00708 0.00276 -0.0796 0.7787 0.8127 1.000 0.4424 0.00712 0.00279 -0.0792 0.7652 0.8273 1.500 0.4962 0.00725 0.00290 -0.0790 0.7470 0.8416 2.000 0.5473 0.00713 0.00259 -0.0777 0.7067 0.8547 2.500 0.5951 0.00709 0.00256 -0.0759 0.6713 0.8738 3.000 0.6407 0.00735 0.00261 -0.0737 0.6094 0.8901 3.500 0.6724 0.00841 0.00287 -0.0693 0.4217 0.9090 4.000 0.6728 0.01095 0.00391 -0.0595 0.0925 0.9418 4.500 0.7091 0.01267 0.00555 -0.0562 0.0222 0.9807 5.000 0.7540 0.01402 0.00707 -0.0549 0.0211 1.0000 5.500 0.7909 0.01590 0.00912 -0.0520 0.0208 1.0000 6.000 0.8366 0.01864 0.01202 -0.0506 0.0211 1.0000 6.500 0.8957 0.02321 0.01688 -0.0515 0.0220 1.0000 7.000 0.9321 0.02620 0.02032 -0.0488 0.0104 1.0000 7.500 0.9694 0.02511 0.01916 -0.0467 0.0084 1.0000 8.000 1.0029 0.02560 0.01966 -0.0441 0.0074 1.0000 8.500 1.0318 0.02703 0.02117 -0.0408 0.0068 1.0000 9.000 1.0597 0.03289 0.02764 -0.0373 0.0067 1.0000 9.500 0.9756 0.05490 0.05149 -0.0170 0.0158 1.0000 10.000 0.9374 0.05987 0.05673 -0.0085 0.0159 1.0000 10.500 0.8969 0.06589 0.06300 -0.0036 0.0159 1.0000 11.000 0.8505 0.07404 0.07138 -0.0026 0.0162 1.0000 11.500 0.8030 0.08530 0.08283 -0.0065 0.0167 1.0000 12.000 0.7491 0.10592 0.10355 -0.0188 0.0192 1.0000 13.500 0.7356 0.14090 0.13845 -0.0367 0.0173 1.0000 14.000 0.7393 0.15053 0.14805 -0.0414 0.0161 1.0000 14.500 0.7450 0.15962 0.15713 -0.0458 0.0152 1.0000 15.000 0.7522 0.16838 0.16587 -0.0500 0.0144 1.0000 15.500 0.7611 0.17671 0.17418 -0.0538 0.0137 1.0000 16.000 0.7716 0.18465 0.18211 -0.0574 0.0131 1.0000 16.500 0.7834 0.19240 0.18985 -0.0607 0.0125 1.0000 17.000 0.7955 0.20032 0.19777 -0.0640 0.0120 1.0000 17.500 0.8030 0.21064 0.20807 -0.0679 0.0113 1.0000 18.000 0.8070 0.22242 0.21981 -0.0725 0.0109 1.0000 18.500 0.8166 0.22793 0.22533 -0.0761 0.0105 1.0000 19.000 0.8266 0.23327 0.23065 -0.0799 0.0087 1.0000 19.500 0.8385 0.23929 0.23666 -0.0830 0.0075 1.0000 20.000 0.8514 0.24462 0.24198 -0.0858 0.0067 1.0000 20.500 0.8638 0.25311 0.25045 -0.0885 0.0061 1.0000 21.000 0.8712 0.25854 0.25586 -0.0923 0.0058 1.0000 21.500 0.8831 0.26481 0.26213 -0.0955 0.0044 1.0000 22.000 0.8949 0.27027 0.26759 -0.0986 0.0040 1.0000 22.500 0.9073 0.27735 0.27465 -0.1013 0.0038 1.0000 23.000 0.9166 0.28422 0.28151 -0.1046 0.0038 1.0000 23.500 0.9263 0.29109 0.28838 -0.1078 0.0037 1.0000 24.000 0.9363 0.29794 0.29523 -0.1110 0.0037 1.0000 24.500 0.9465 0.30473 0.30203 -0.1141 0.0037 1.0000 25.000 0.9567 0.31150 0.30880 -0.1172 0.0036 1.0000 25.500 0.9667 0.31824 0.31554 -0.1202 0.0036 1.0000 26.000 0.9766 0.32492 0.32229 -0.1233 0.0036 1.0000 26.500 0.9862 0.33159 0.32896 -0.1263 0.0036 1.0000 27.000 0.9955 0.33823 0.33561 -0.1293 0.0035 1.0000 27.500 1.0046 0.34483 0.34223 -0.1324 0.0035 1.0000 28.000 1.0133 0.35141 0.34882 -0.1354 0.0035 1.0000 28.500 1.0218 0.35795 0.35537 -0.1384 0.0035 1.0000 29.000 1.0300 0.36446 0.36189 -0.1414 0.0034 1.0000 29.500 1.0378 0.37094 0.36839 -0.1445 0.0034 1.0000 30.000 1.0453 0.37736 0.37481 -0.1475 0.0034 1.0000 30.500 1.0525 0.38377 0.38124 -0.1505 0.0034 1.0000 31.000 1.0594 0.39009 0.38758 -0.1535 0.0034 1.0000 31.500 1.0659 0.39641 0.39392 -0.1565 0.0033 1.0000 32.000 1.0721 0.40266 0.40018 -0.1595 0.0033 1.0000 32.500 1.0779 0.40886 0.40640 -0.1625 0.0033 1.0000 33.000 1.0833 0.41500 0.41256 -0.1655 0.0033 1.0000 33.500 1.0884 0.42107 0.41870 -0.1685 0.0033 1.0000 34.000 1.0932 0.42709 0.42474 -0.1714 0.0033 1.0000 34.500 1.0976 0.43306 0.43073 -0.1744 0.0033 1.0000 35.000 1.1016 0.43895 0.43664 -0.1774 0.0033 1.0000 35.500 1.1052 0.44476 0.44248 -0.1803 0.0032 1.0000 36.000 1.1085 0.45052 0.44826 -0.1833 0.0032 1.0000 36.500 1.1114 0.45617 0.45394 -0.1862 0.0032 1.0000 37.000 1.1140 0.46173 0.45953 -0.1891 0.0032 1.0000 37.500 1.1162 0.46726 0.46509 -0.1921 0.0032 1.0000 38.000 1.1180 0.47266 0.47051 -0.1950 0.0032 1.0000 38.500 1.1194 0.47798 0.47588 -0.1979 0.0032 1.0000 39.000 1.1205 0.48321 0.48113 -0.2008 0.0032 1.0000 39.500 1.1212 0.48835 0.48631 -0.2036 0.0032 1.0000 40.000 1.1216 0.49339 0.49137 -0.2065 0.0032 1.0000 40.500 1.1215 0.49831 0.49633 -0.2094 0.0032 1.0000 41.000 1.1212 0.50314 0.50119 -0.2122 0.0032 1.0000 41.500 1.1204 0.50788 0.50596 -0.2151 0.0032 1.0000 42.000 1.1193 0.51250 0.51061 -0.2179 0.0032 1.0000 42.500 1.1179 0.51700 0.51514 -0.2207 0.0032 1.0000 43.000 1.1161 0.52140 0.51959 -0.2235 0.0032 1.0000 43.500 1.1139 0.52571 0.52393 -0.2263 0.0032 1.0000 44.000 1.1114 0.52988 0.52813 -0.2291 0.0032 1.0000 44.500 1.1086 0.53393 0.53221 -0.2319 0.0032 1.0000 45.000 1.1054 0.53789 0.53621 -0.2346 0.0031 1.0000 45.500 1.1019 0.54177 0.54011 -0.2374 0.0031 1.0000 46.000 1.0981 0.54550 0.54387 -0.2401 0.0031 1.0000 46.500 1.0940 0.54913 0.54753 -0.2428 0.0031 1.0000 47.000 1.0896 0.55270 0.55114 -0.2455 0.0031 1.0000 47.500 1.0849 0.55631 0.55477 -0.2482 0.0030 1.0000 48.000 1.0804 0.56032 0.55880 -0.2507 0.0029 1.0000 48.500 1.0761 0.56481 0.56331 -0.2531 0.0027 1.0000 49.000 1.0711 0.56879 0.56730 -0.2556 0.0026 1.0000 49.500 1.0656 0.57246 0.57100 -0.2581 0.0025 1.0000 50.000 1.0599 0.57599 0.57455 -0.2606 0.0025 1.0000 50.500 1.0538 0.57938 0.57799 -0.2630 0.0025 1.0000 51.000 1.0475 0.58259 0.58122 -0.2655 0.0024 1.0000 51.500 1.0408 0.58567 0.58432 -0.2680 0.0024 1.0000 52.000 1.0339 0.58860 0.58727 -0.2705 0.0024 1.0000 52.500 1.0266 0.59142 0.59012 -0.2729 0.0024 1.0000 53.000 1.0191 0.59413 0.59284 -0.2754 0.0024 1.0000 53.500 1.0114 0.59670 0.59544 -0.2778 0.0024 1.0000 54.000 1.0033 0.59914 0.59790 -0.2803 0.0024 1.0000 54.500 0.9950 0.60149 0.60028 -0.2827 0.0024 1.0000 55.000 0.9865 0.60371 0.60251 -0.2852 0.0024 1.0000 55.500 0.9777 0.60581 0.60464 -0.2876 0.0024 1.0000 56.000 0.9687 0.60771 0.60656 -0.2901 0.0024 1.0000 56.500 0.9595 0.60957 0.60847 -0.2925 0.0024 1.0000 57.000 0.9500 0.61141 0.61032 -0.2950 0.0024 1.0000 57.500 0.9403 0.61298 0.61192 -0.2974 0.0024 1.0000 58.000 0.9304 0.61451 0.61347 -0.2999 0.0024 1.0000 58.500 0.9203 0.61601 0.61499 -0.3023 0.0024 1.0000 59.000 0.9100 0.61731 0.61632 -0.3048 0.0024 1.0000 59.500 0.8995 0.61854 0.61757 -0.3072 0.0024 1.0000 60.000 0.8888 0.61967 0.61872 -0.3097 0.0024 1.0000