NACA 2414-Mod, Re=50000 Mach=0.0000-NCrit=9.00 Upper part Cp Vs X (pressure coefficient)for Alpha=2.0 degrees Lower part 2.0 1.0 0.5 0.0 0. 0.00 0.100.200.30 0.40 0.500.600.700.800.901.001.10120130140 1.50 Page 21 of 43.Drawn by Profili 2.15b on dats proceased by XFoil-Copyright (C)1995-2004-All rights reserved. ACA2414MOd Re=50000 Mach=0.0000.ici9.00 Cp distribution for Alpha=2.0 degrees 11 TTTTTT Page 21 of 43 Drawn by Profili 2.156 on data processed by XFoil.Copyright (C)1995-2004.All rights reserved 攻角为2时周围气体压强曲线与模拟图攻角为 2°时周围气体压强曲线与模拟图