From this point the work establishes aerodynamic optimization design system that is applicable to heavy-duty gas turbine compressor by introducing optimization theory to heavy-duty gas turbine compressor blade design. 本文的工作就是从这一方面着手,将优化理论引入到地面重型燃气轮机压气机叶型设计中,建立可用于地面重型燃气轮机压气机的二维气动优化设计体系。