摘要
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.
For many years, a comprehensive research program of turbomachinery aerodynamicsand CFD methods has been conducted by the authors. In this paper the advances in nu-merical analysis and design method including quasi-and full-three-dimensional numericalcalcu1ations, code calibrations, aerodynamic design system for multi stage axial turbines aresummarized. Further development in this field is also discussed.
出处
《工程热物理学报》
EI
CAS
CSCD
北大核心
1998年第3期310-314,共5页
Journal of Engineering Thermophysics
基金
国家攀登B项目