XFOIL Version 6.94 Calculated polar for: SD8000-089-88 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 0.2315 0.00710 0.00295 -0.0522 0.8834 0.9617 0.500 0.3225 0.00687 0.00263 -0.0588 0.8580 1.0000 1.000 0.3655 0.00681 0.00243 -0.0557 0.8214 1.0000 1.500 0.4121 0.00687 0.00229 -0.0532 0.7788 1.0000 2.000 0.4608 0.00706 0.00227 -0.0511 0.7263 1.0000 2.500 0.5098 0.00739 0.00232 -0.0492 0.6621 1.0000 3.000 0.5589 0.00786 0.00250 -0.0475 0.5876 1.0000 3.500 0.6075 0.00848 0.00276 -0.0459 0.5061 1.0000 4.000 0.6560 0.00921 0.00316 -0.0445 0.4228 1.0000 4.500 0.7043 0.01004 0.00364 -0.0431 0.3423 1.0000 5.000 0.7529 0.01091 0.00424 -0.0420 0.2701 1.0000 5.500 0.8014 0.01184 0.00492 -0.0408 0.2116 1.0000 6.000 0.8500 0.01279 0.00571 -0.0397 0.1663 1.0000 6.500 0.8977 0.01384 0.00663 -0.0385 0.1305 1.0000 7.000 0.9455 0.01484 0.00757 -0.0373 0.1011 1.0000 7.500 0.9919 0.01600 0.00875 -0.0359 0.0790 1.0000 8.500 1.0758 0.01931 0.01208 -0.0319 0.0421 1.0000 9.000 1.1152 0.02117 0.01410 -0.0295 0.0343 1.0000 10.000 1.1842 0.02611 0.01950 -0.0238 0.0270 1.0000 10.500 1.2119 0.02947 0.02309 -0.0206 0.0249 1.0000 11.000 1.2308 0.03414 0.02824 -0.0167 0.0233 1.0000 11.500 1.2415 0.03736 0.03188 -0.0118 0.0220 1.0000 12.000 1.2378 0.04201 0.03698 -0.0068 0.0213 1.0000 12.500 1.2242 0.04766 0.04306 -0.0033 0.0206 1.0000 13.000 1.2024 0.05487 0.05068 -0.0026 0.0202 1.0000 13.500 1.1676 0.06534 0.06158 -0.0061 0.0201 1.0000 14.000 1.1148 0.08166 0.07837 -0.0161 0.0205 1.0000 14.500 1.0297 0.11014 0.10730 -0.0361 0.0220 1.0000 16.500 0.9021 0.20284 0.20000 -0.0827 0.0335 1.0000 17.000 0.9106 0.21429 0.21142 -0.0869 0.0322 1.0000 17.500 0.9144 0.22385 0.22095 -0.0955 0.0301 1.0000 18.000 0.9279 0.23180 0.22890 -0.1002 0.0270 1.0000 18.500 0.9455 0.23802 0.23514 -0.1032 0.0252 1.0000 19.000 0.9638 0.24748 0.24461 -0.1050 0.0239 1.0000 19.500 0.9702 0.25548 0.25257 -0.1137 0.0221 1.0000 20.000 0.9853 0.26294 0.26003 -0.1183 0.0198 1.0000 20.500 1.0020 0.26918 0.26630 -0.1220 0.0184 1.0000 21.000 1.0214 0.27797 0.27511 -0.1234 0.0174 1.0000 21.500 1.0338 0.28521 0.28234 -0.1292 0.0173 1.0000 22.000 1.0457 0.29255 0.28965 -0.1365 0.0160 1.0000 22.500 1.0610 0.29957 0.29667 -0.1411 0.0147 1.0000 23.000 1.0765 0.30600 0.30312 -0.1455 0.0137 1.0000 23.500 1.0923 0.31161 0.30875 -0.1489 0.0128 1.0000 24.000 1.1085 0.32031 0.31747 -0.1520 0.0125 1.0000 24.500 1.1208 0.32643 0.32357 -0.1593 0.0119 1.0000 25.000 1.1358 0.33331 0.33045 -0.1642 0.0107 1.0000 25.500 1.1503 0.33952 0.33668 -0.1688 0.0099 1.0000 26.000 1.1645 0.34533 0.34250 -0.1733 0.0094 1.0000 26.500 1.1781 0.35082 0.34801 -0.1773 0.0090 1.0000 27.000 1.1927 0.35899 0.35620 -0.1804 0.0087 1.0000 27.500 1.2050 0.36382 0.36104 -0.1862 0.0087 1.0000 28.000 1.2182 0.36873 0.36594 -0.1919 0.0085 1.0000 28.500 1.2323 0.37426 0.37149 -0.1971 0.0082 1.0000 29.000 1.2456 0.37956 0.37680 -0.2020 0.0076 1.0000 29.500 1.2581 0.38451 0.38176 -0.2067 0.0072 1.0000 30.000 1.2702 0.38928 0.38655 -0.2116 0.0069 1.0000 30.500 1.2817 0.39387 0.39116 -0.2163 0.0065 1.0000 31.000 1.2926 0.39821 0.39554 -0.2211 0.0062 1.0000 31.500 1.3025 0.40237 0.39973 -0.2254 0.0060 1.0000 32.500 1.3232 0.41246 0.40984 -0.2352 0.0058 1.0000 33.000 1.3336 0.41685 0.41424 -0.2405 0.0057 1.0000 33.500 1.3448 0.42197 0.41937 -0.2456 0.0054 1.0000 34.000 1.3542 0.42654 0.42396 -0.2505 0.0050 1.0000 34.500 1.3628 0.43085 0.42831 -0.2554 0.0047 1.0000 35.000 1.3708 0.43502 0.43250 -0.2602 0.0045 1.0000 35.500 1.3785 0.43908 0.43658 -0.2652 0.0042 1.0000 36.000 1.3857 0.44300 0.44054 -0.2701 0.0041 1.0000 36.500 1.3921 0.44672 0.44428 -0.2751 0.0039 1.0000 37.000 1.3975 0.45029 0.44788 -0.2799 0.0038 1.0000 39.000 1.4184 0.46598 0.46366 -0.2995 0.0037 1.0000 39.500 1.4232 0.46968 0.46739 -0.3046 0.0037 1.0000 40.000 1.4279 0.47348 0.47122 -0.3097 0.0036 1.0000 40.500 1.4322 0.47737 0.47515 -0.3146 0.0035 1.0000 41.000 1.4357 0.48113 0.47893 -0.3195 0.0034 1.0000 41.500 1.4387 0.48472 0.48255 -0.3245 0.0032 1.0000 42.000 1.4407 0.48805 0.48591 -0.3294 0.0030 1.0000 42.500 1.4424 0.49130 0.48920 -0.3343 0.0028 1.0000 43.000 1.4435 0.49439 0.49232 -0.3392 0.0027 1.0000 43.500 1.4441 0.49746 0.49542 -0.3442 0.0026 1.0000 44.000 1.4439 0.50027 0.49826 -0.3490 0.0024 1.0000 44.500 1.4434 0.50303 0.50105 -0.3540 0.0023 1.0000 45.000 1.4421 0.50560 0.50366 -0.3588 0.0023 1.0000 45.500 1.4400 0.50788 0.50596 -0.3638 0.0022 1.0000