A stage - by - stage simulation method is introduced for analysis of inlet total pressure distortion effect on the multistageaxialflowcompressor characteristics.
介绍了1种分析进口总压畸变对多级轴流压气机特性影响的逐级模拟方法。
2
In this paper, virtual prototype technology of turbo-machinery, multistageaxialflowcompressor numerical simulation, and integrated design of turbo-machinery and engine have been introduced.
介绍了叶轮机虚拟样机技术、多级轴流压气机数值仿真和叶轮机与发动机一体化设计。
3
This paper details the experimental methods and results using the airfoil sensors to measure total pressure and total temperature distributions behind the rotors in a multistageaxial-flowcompressor.