摘要
一、前言 本文是作者继文献[1]之后在叶轮机中推广应用边界元法解决气动问题的又一次尝试。文中应用边界元法求解了任意迴转面叶栅气动正问题。计算了一个压气机叶栅和一个透平叶栅。
In this paper a boundary element method for solving direct aerodynamic problem of aerofoil cascades on an arbitrary stream surface of revolution is presented. By this method the parameters of the flow fields past a compressor cascade and a turbine cascade are computed. The results have a good agreement with those of the experiment or other computational methods.
出处
《工程热物理学报》
EI
CAS
CSCD
北大核心
1990年第1期41-43,共3页
Journal of Engineering Thermophysics
