XFOIL Version 6.94 Calculated polar for: NACA 63-206 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 0.1500 0.00608 0.00119 -0.0329 0.7002 1.0000 0.500 0.2037 0.00615 0.00119 -0.0336 0.7002 1.0000 1.000 0.2557 0.00661 0.00125 -0.0336 0.6718 1.0000 1.500 0.3102 0.00704 0.00148 -0.0340 0.6309 1.0000 2.000 0.3656 0.00736 0.00189 -0.0347 0.6027 1.0000 3.000 0.4569 0.01078 0.00334 -0.0325 0.0302 1.0000 3.500 0.5070 0.01224 0.00496 -0.0316 0.0297 1.0000 4.000 0.5539 0.01505 0.00790 -0.0302 0.0258 1.0000 4.500 0.6057 0.01630 0.00919 -0.0296 0.0187 1.0000 5.000 0.6610 0.02566 0.01974 -0.0243 0.0330 1.0000 5.500 0.7041 0.03319 0.02807 -0.0211 0.0331 1.0000 6.000 0.7378 0.04023 0.03550 -0.0191 0.0291 1.0000 6.500 0.7477 0.05212 0.04785 -0.0176 0.0254 1.0000 7.000 0.7377 0.06498 0.06122 -0.0162 0.0243 1.0000 7.500 0.7325 0.07219 0.06873 -0.0146 0.0243 1.0000 8.000 0.7116 0.07815 0.07486 -0.0123 0.0242 1.0000 8.500 0.6818 0.08412 0.08090 -0.0125 0.0242 1.0000 9.000 0.6665 0.09307 0.08988 -0.0183 0.0242 1.0000 9.500 0.6628 0.10223 0.09901 -0.0235 0.0242 1.0000 10.000 0.6639 0.11078 0.10753 -0.0278 0.0240 1.0000 10.500 0.6693 0.11838 0.11510 -0.0319 0.0234 1.0000 11.000 0.6788 0.12529 0.12199 -0.0358 0.0219 1.0000 11.500 0.6860 0.13324 0.12992 -0.0400 0.0203 1.0000 12.000 0.6942 0.14135 0.13800 -0.0442 0.0178 1.0000 12.500 0.7042 0.14948 0.14612 -0.0480 0.0155 1.0000 13.000 0.7221 0.15771 0.15434 -0.0501 0.0130 1.0000 13.500 0.7274 0.17067 0.16727 -0.0549 0.0119 1.0000 14.000 0.7383 0.17716 0.17375 -0.0592 0.0114 1.0000 14.500 0.6983 0.16577 0.16331 -0.1074 0.0116 1.0000 15.000 0.7121 0.17426 0.17181 -0.1128 0.0099 1.0000 15.500 0.7314 0.18703 0.18459 -0.1165 0.0082 1.0000 16.000 0.7561 0.20423 0.20176 -0.1182 0.0070 1.0000 16.500 0.7676 0.21410 0.21163 -0.1237 0.0066 1.0000 17.000 0.7851 0.22603 0.22358 -0.1274 0.0051 1.0000 17.500 0.8043 0.24030 0.23783 -0.1296 0.0046 1.0000 18.000 0.8193 0.25280 0.25033 -0.1336 0.0045 1.0000 18.500 0.8347 0.26521 0.26275 -0.1372 0.0045 1.0000 19.000 0.8502 0.27754 0.27508 -0.1407 0.0044 1.0000 19.500 0.8657 0.28995 0.28749 -0.1440 0.0044 1.0000 20.000 0.8808 0.30212 0.29966 -0.1472 0.0043 1.0000 20.500 0.8954 0.31419 0.31173 -0.1503 0.0043 1.0000 21.000 0.9094 0.32598 0.32351 -0.1535 0.0043 1.0000 21.500 0.9231 0.33768 0.33521 -0.1565 0.0042 1.0000 22.000 0.9362 0.34917 0.34671 -0.1594 0.0042 1.0000 22.500 0.9490 0.36053 0.35806 -0.1623 0.0042 1.0000 23.000 0.9612 0.37175 0.36927 -0.1653 0.0041 1.0000 23.500 0.9731 0.38278 0.38030 -0.1681 0.0041 1.0000 24.000 0.9846 0.39367 0.39125 -0.1710 0.0041 1.0000 24.500 0.9956 0.40447 0.40206 -0.1738 0.0041 1.0000 25.000 1.0062 0.41508 0.41267 -0.1767 0.0040 1.0000 25.500 1.0165 0.42559 0.42318 -0.1795 0.0040 1.0000 26.000 1.0264 0.43598 0.43358 -0.1823 0.0040 1.0000 26.500 1.0358 0.44627 0.44388 -0.1851 0.0040 1.0000 27.000 1.0450 0.45634 0.45395 -0.1879 0.0040 1.0000 27.500 1.0538 0.46633 0.46394 -0.1907 0.0039 1.0000 28.000 1.0620 0.47641 0.47404 -0.1936 0.0039 1.0000 28.500 1.0700 0.48617 0.48381 -0.1963 0.0039 1.0000 29.000 1.0776 0.49586 0.49351 -0.1991 0.0039 1.0000 29.500 1.0848 0.50551 0.50317 -0.2020 0.0039 1.0000 30.000 1.0916 0.51490 0.51257 -0.2047 0.0039 1.0000 30.500 1.0980 0.52435 0.52204 -0.2076 0.0039 1.0000 31.000 1.1040 0.53363 0.53139 -0.2104 0.0039 1.0000 31.500 1.1096 0.54274 0.54051 -0.2132 0.0039 1.0000 32.000 1.1148 0.55174 0.54954 -0.2159 0.0039 1.0000 32.500 1.1196 0.56079 0.55861 -0.2188 0.0039 1.0000 33.000 1.1240 0.56973 0.56757 -0.2216 0.0039 1.0000 33.500 1.1280 0.57841 0.57628 -0.2244 0.0039 1.0000 34.000 1.1315 0.58717 0.58507 -0.2272 0.0039 1.0000 34.500 1.1348 0.59556 0.59347 -0.2299 0.0039 1.0000 35.000 1.1376 0.60397 0.60191 -0.2327 0.0039 1.0000 35.500 1.1399 0.61241 0.61041 -0.2355 0.0039 1.0000 36.000 1.1418 0.62071 0.61874 -0.2383 0.0039 1.0000 36.500 1.1433 0.62876 0.62682 -0.2411 0.0039 1.0000 37.000 1.1444 0.63687 0.63496 -0.2439 0.0039 1.0000 37.500 1.1451 0.64488 0.64300 -0.2466 0.0039 1.0000 38.000 1.1453 0.65284 0.65099 -0.2494 0.0039 1.0000 38.500 1.1452 0.66042 0.65861 -0.2521 0.0039 1.0000 39.000 1.1445 0.66825 0.66647 -0.2549 0.0039 1.0000 39.500 1.1435 0.67581 0.67409 -0.2576 0.0039 1.0000 40.000 1.1421 0.68337 0.68169 -0.2603 0.0039 1.0000 40.500 1.1403 0.69064 0.68899 -0.2630 0.0039 1.0000 41.000 1.1381 0.69795 0.69634 -0.2657 0.0039 1.0000 41.500 1.1353 0.70541 0.70383 -0.2684 0.0039 1.0000 42.000 1.1322 0.71250 0.71095 -0.2710 0.0039 1.0000 42.500 1.1287 0.71962 0.71811 -0.2737 0.0040 1.0000 43.000 1.1248 0.72672 0.72525 -0.2763 0.0039 1.0000 43.500 1.1206 0.73370 0.73227 -0.2789 0.0039 1.0000 44.000 1.1160 0.74054 0.73914 -0.2814 0.0039 1.0000 44.500 1.1114 0.74721 0.74584 -0.2839 0.0039 1.0000 45.000 1.1063 0.75500 0.75365 -0.2863 0.0038 1.0000 45.500 1.1015 0.76271 0.76138 -0.2887 0.0036 1.0000 46.000 1.0961 0.77055 0.76924 -0.2910 0.0035 1.0000 46.500 1.0902 0.77767 0.77642 -0.2933 0.0035 1.0000 47.000 1.0840 0.78461 0.78338 -0.2955 0.0034 1.0000 47.500 1.0772 0.79182 0.79062 -0.2978 0.0034 1.0000 48.000 1.0700 0.79845 0.79727 -0.3000 0.0034 1.0000 48.500 1.0622 0.80567 0.80452 -0.3023 0.0034 1.0000 49.000 1.0544 0.81206 0.81093 -0.3044 0.0034 1.0000 49.500 1.0457 0.81923 0.81813 -0.3066 0.0033 1.0000 50.000 1.0371 0.82523 0.82416 -0.3087 0.0033 1.0000 50.500 1.0277 0.83190 0.83086 -0.3108 0.0033 1.0000 51.000 1.0181 0.83818 0.83716 -0.3128 0.0033 1.0000 51.500 1.0087 0.84316 0.84217 -0.3147 0.0033 1.0000 52.000 0.9979 0.85004 0.84910 -0.3167 0.0033 1.0000 52.500 0.9873 0.85568 0.85477 -0.3186 0.0033 1.0000 53.000 0.9761 0.86160 0.86072 -0.3204 0.0033 1.0000 53.500 0.9647 0.86709 0.86624 -0.3221 0.0033 1.0000 54.000 0.9532 0.87197 0.87115 -0.3238 0.0033 1.0000 54.500 0.9405 0.87787 0.87707 -0.3255 0.0033 1.0000 55.000 0.9282 0.88263 0.88186 -0.3271 0.0033 1.0000 55.500 0.9152 0.88765 0.88692 -0.3286 0.0033 1.0000 56.000 0.9021 0.89218 0.89148 -0.3300 0.0033 1.0000 56.500 0.8886 0.89645 0.89578 -0.3313 0.0033 1.0000 57.000 0.8744 0.90102 0.90039 -0.3326 0.0033 1.0000 57.500 0.8607 0.90424 0.90365 -0.3338 0.0033 1.0000 58.000 0.8457 0.90832 0.90775 -0.3348 0.0033 1.0000 58.500 0.8310 0.91147 0.91093 -0.3358 0.0033 1.0000 59.000 0.8160 0.91440 0.91389 -0.3366 0.0032 1.0000 59.500 0.8007 0.91685 0.91636 -0.3373 0.0032 1.0000 60.000 0.7851 0.91881 0.91835 -0.3379 0.0032 1.0000