XFOIL Version 6.96 Calculated polar for: FX 78-K-140/20 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -12.250 -0.1736 0.12444 0.12044 -0.0790 0.8215 0.0302 -12.000 -0.1850 0.12316 0.11922 -0.0835 0.8203 0.0349 -11.750 -0.1821 0.11983 0.11590 -0.0848 0.8191 0.0350 -11.500 -0.1726 0.11609 0.11217 -0.0854 0.8180 0.0347 -11.250 -0.1734 0.11380 0.10993 -0.0882 0.8166 0.0351 -11.000 -0.1715 0.11067 0.10684 -0.0902 0.8154 0.0352 -10.750 -0.1667 0.10746 0.10366 -0.0916 0.8141 0.0352 -10.500 -0.1540 0.10195 0.09815 -0.0890 0.8133 0.0387 -10.250 -0.1505 0.09922 0.09543 -0.0903 0.8120 0.0386 -10.000 -0.1464 0.09645 0.09267 -0.0911 0.8106 0.0403 -9.750 -0.1461 0.09338 0.08962 -0.0921 0.8090 0.0426 -9.500 -0.1475 0.09023 0.08651 -0.0936 0.8078 0.0443 -9.250 -0.1476 0.08736 0.08364 -0.0949 0.8067 0.0446 -9.000 -0.1571 0.08390 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