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本文对多级汽轮机通流部分气动热力学数值计算方法与设计体系研究所取得的进展进行了回顾，主要内容包括通流部分气动热力准三维、全三维计算方法进展、程序的校准方法、多级轴流透平气动热力设计体系研制等，并提出了今后进一步开发的设想．
In this paper, the progress made in the research on numerical thermodynamic numerical method and design system for the flow through the multi-stage steam turbine is reviewed. The main contents include the progress of quasi-three-dimensional and full three-dimensional calculation of the flow through the aerodynamic part, the calibration method of the program, Flow through the aerodynamic and thermal design system development, and put forward the idea of further development.