摘要
本文概要介绍了株洲航空动力机械研究所在９０年代中期引进每秒１０亿次运算速度的计算机后，建立了以二维叶片造型和三维粘性数值计算为核心的小发压气机ＣＦＤ设计系统。用新建立的ＣＦＤ设计系统进行了单级和双级压气机设计并进行了试验验证．试验结果证明，使用该系统能够完成高性能小型轴流压气机设计。
A new CFD design system for small flow axial compressors has been createdin Zhuzhou Aviation Power -- Plant Research Institute. The design system is comprised ofthe one-dimensional optimum calculation code, the S2 stream surface calculation code, theblade design code and three-dimensional N-S calculation code. To testify the design system,the authors designed a single stage compressor and a two-stage compressor. In this paper,the main content of this system is introduced in detail. The design and experiment resultsof these two compressors are also described.
出处
《工程热物理学报》
EI
CAS
CSCD
北大核心
2000年第1期38-41,共4页
Journal of Engineering Thermophysics
