XFOIL Version 6.94 Calculated polar for: WB-135/35 13.5% smoothed 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 0.4041 0.01042 0.00361 -0.0871 0.7034 0.4950 0.500 0.4560 0.01034 0.00366 -0.0861 0.6915 0.5393 1.000 0.5076 0.01021 0.00367 -0.0851 0.6791 0.5931 1.500 0.5557 0.00989 0.00366 -0.0832 0.6647 0.6776 2.000 0.6999 0.00932 0.00377 -0.1019 0.6453 1.0000 2.500 0.7471 0.00945 0.00383 -0.1000 0.6263 1.0000 3.000 0.7930 0.00958 0.00391 -0.0977 0.6017 1.0000 3.500 0.8373 0.00977 0.00403 -0.0952 0.5707 1.0000 4.000 0.8771 0.01010 0.00419 -0.0917 0.5204 1.0000 4.500 0.9071 0.01089 0.00456 -0.0866 0.4436 1.0000 5.000 0.9395 0.01181 0.00517 -0.0822 0.3965 1.0000 5.500 0.9757 0.01263 0.00582 -0.0786 0.3679 1.0000 6.000 1.0118 0.01340 0.00649 -0.0750 0.3428 1.0000 6.500 1.0484 0.01413 0.00716 -0.0716 0.3232 1.0000 7.000 1.0841 0.01479 0.00784 -0.0680 0.3036 1.0000 7.500 1.1148 0.01539 0.00847 -0.0635 0.2790 1.0000 8.000 1.1410 0.01616 0.00918 -0.0584 0.2466 1.0000 8.500 1.1531 0.01778 0.01036 -0.0518 0.1666 1.0000 9.000 1.1272 0.02219 0.01382 -0.0416 0.0302 1.0000 9.500 1.1451 0.02440 0.01618 -0.0373 0.0227 1.0000 10.000 1.1604 0.02698 0.01901 -0.0333 0.0203 1.0000 10.500 1.1678 0.03034 0.02264 -0.0293 0.0188 1.0000 11.000 1.1729 0.03416 0.02669 -0.0261 0.0178 1.0000 11.500 1.1715 0.03887 0.03162 -0.0233 0.0171 1.0000 12.000 1.1687 0.04402 0.03698 -0.0212 0.0168 1.0000 12.500 1.1641 0.04967 0.04282 -0.0195 0.0164 1.0000 13.000 1.1639 0.05508 0.04843 -0.0181 0.0161 1.0000 13.500 1.1668 0.06027 0.05376 -0.0166 0.0156 1.0000 14.000 1.1721 0.06535 0.05896 -0.0156 0.0146 1.0000 14.500 1.1851 0.06958 0.06338 -0.0138 0.0146 1.0000 15.000 1.1988 0.07406 0.06807 -0.0121 0.0145 1.0000 15.500 1.2076 0.07968 0.07408 -0.0109 0.0154 1.0000 16.000 1.2045 0.08754 0.08241 -0.0103 0.0172 1.0000 16.500 0.9404 0.09375 0.08966 -0.0160 0.0160 1.0000 17.000 0.9265 0.10189 0.09816 -0.0201 0.0168 1.0000 17.500 0.9016 0.11230 0.10893 -0.0263 0.0176 1.0000 18.000 0.8692 0.12479 0.12176 -0.0342 0.0184 1.0000 18.500 0.7236 0.17443 0.17210 -0.0622 0.0368 1.0000 19.000 0.7036 0.19326 0.19090 -0.0705 0.0475 1.0000 19.500 0.7212 0.19931 0.19697 -0.0710 0.0438 1.0000 20.000 0.7131 0.20953 0.20718 -0.0782 0.0377 1.0000 20.500 0.7332 0.21316 0.21086 -0.0790 0.0352 1.0000 21.000 0.7246 0.22597 0.22362 -0.0859 0.0304 1.0000 21.500 0.7400 0.23078 0.22849 -0.0877 0.0276 1.0000 22.000 0.7408 0.24144 0.23914 -0.0924 0.0257 1.0000 22.500 0.7450 0.25067 0.24838 -0.0968 0.0225 1.0000 23.000 0.7566 0.25661 0.25434 -0.0993 0.0203 1.0000 23.500 0.7666 0.26556 0.26330 -0.1017 0.0191 1.0000 24.000 0.7687 0.27510 0.27285 -0.1066 0.0185 1.0000 24.500 0.7737 0.28474 0.28250 -0.1107 0.0166 1.0000 25.000 0.7811 0.29311 0.29089 -0.1141 0.0154 1.0000 25.500 0.7888 0.30108 0.29890 -0.1173 0.0145 1.0000 26.000 0.7972 0.30851 0.30636 -0.1202 0.0136 1.0000 26.500 0.8073 0.31572 0.31360 -0.1226 0.0131 1.0000 27.000 0.8140 0.32684 0.32472 -0.1256 0.0126 1.0000 27.500 0.8193 0.33557 0.33347 -0.1292 0.0125 1.0000 28.000 0.8213 0.34506 0.34298 -0.1337 0.0120 1.0000 28.500 0.8271 0.35415 0.35209 -0.1372 0.0111 1.0000 29.000 0.8328 0.36289 0.36087 -0.1404 0.0102 1.0000 29.500 0.8383 0.37143 0.36943 -0.1436 0.0097 1.0000 30.000 0.8440 0.37948 0.37751 -0.1466 0.0091 1.0000 30.500 0.8492 0.38744 0.38550 -0.1495 0.0089 1.0000 31.500 0.8590 0.40633 0.40443 -0.1553 0.0084 1.0000 32.000 0.8618 0.41525 0.41338 -0.1587 0.0084 1.0000 32.500 0.8646 0.42486 0.42302 -0.1622 0.0081 1.0000 33.000 0.8681 0.43391 0.43209 -0.1653 0.0077 1.0000 33.500 0.8712 0.44284 0.44105 -0.1684 0.0072 1.0000 34.000 0.8740 0.45159 0.44983 -0.1713 0.0068 1.0000 34.500 0.8765 0.45995 0.45822 -0.1743 0.0063 1.0000 35.000 0.8785 0.46808 0.46638 -0.1772 0.0061 1.0000 35.500 0.8802 0.47561 0.47395 -0.1800 0.0059 1.0000 37.000 0.8833 0.50200 0.50041 -0.1886 0.0056 1.0000 37.500 0.8837 0.51054 0.50897 -0.1915 0.0056 1.0000 38.000 0.8841 0.51927 0.51774 -0.1942 0.0053 1.0000 38.500 0.8841 0.52723 0.52574 -0.1970 0.0051 1.0000 39.000 0.8837 0.53538 0.53391 -0.1996 0.0048 1.0000 39.500 0.8829 0.54306 0.54162 -0.2023 0.0045 1.0000 40.000 0.8817 0.55032 0.54890 -0.2050 0.0044 1.0000 40.500 0.8801 0.55733 0.55595 -0.2076 0.0041 1.0000 41.000 0.8781 0.56411 0.56277 -0.2101 0.0039 1.0000 41.500 0.8757 0.57042 0.56910 -0.2127 0.0038 1.0000 43.500 0.8644 0.59803 0.59682 -0.2225 0.0036 1.0000 44.000 0.8607 0.60362 0.60244 -0.2248 0.0036 1.0000 44.500 0.8571 0.60968 0.60852 -0.2270 0.0035 1.0000 45.000 0.8530 0.61530 0.61417 -0.2293 0.0034 1.0000 45.500 0.8485 0.62016 0.61907 -0.2315 0.0033 1.0000 46.000 0.8438 0.62515 0.62409 -0.2336 0.0031 1.0000 46.500 0.8387 0.62974 0.62870 -0.2358 0.0029 1.0000 47.000 0.8335 0.63414 0.63313 -0.2379 0.0027 1.0000 47.500 0.8278 0.63773 0.63675 -0.2400 0.0026 1.0000 48.000 0.8218 0.64124 0.64029 -0.2420 0.0026 1.0000 48.500 0.8156 0.64439 0.64346 -0.2440 0.0024 1.0000 49.000 0.8089 0.64696 0.64607 -0.2459 0.0023 1.0000 49.500 0.8018 0.64914 0.64827 -0.2479 0.0023 1.0000 51.500 0.7737 0.65817 0.65740 -0.2548 0.0022 1.0000 52.000 0.7661 0.65934 0.65860 -0.2564 0.0022 1.0000 52.500 0.7586 0.66072 0.66000 -0.2579 0.0021 1.0000 53.000 0.7504 0.66064 0.65994 -0.2594 0.0021 1.0000 53.500 0.7422 0.66080 0.66013 -0.2609 0.0020 1.0000 54.000 0.7336 0.66029 0.65964 -0.2623 0.0019 1.0000 54.500 0.7251 0.65981 0.65919 -0.2637 0.0017 1.0000 55.000 0.7162 0.65855 0.65795 -0.2651 0.0016 1.0000 55.500 0.7072 0.65708 0.65651 -0.2664 0.0015 1.0000 56.000 0.6979 0.65509 0.65454 -0.2676 0.0014 1.0000 56.500 0.6885 0.65268 0.65215 -0.2688 0.0013 1.0000 57.000 0.6787 0.64973 0.64922 -0.2700 0.0012 1.0000 57.500 0.6686 0.64642 0.64593 -0.2712 0.0012 1.0000 59.000 0.6399 0.63766 0.63723 -0.2739 0.0011 1.0000 59.500 0.6298 0.63337 0.63296 -0.2747 0.0011 1.0000 60.000 0.6197 0.62906 0.62867 -0.2755 0.0011 1.0000