摘要
本文在考虑旋转和曲率的条件下,采用微分法对离心叶轮内的边界层进行了数值计算,并分析了叶片压力面和吸力面上边界层发展的不同趋势。
In this paper, a differential method is used to calculate the centrifugal impeller boundary layer, where the rotation and curvature are considered. The tendency of the development of boundary layer in pressure surface ands uction surface in impeller are analysed.
出处
《农业机械学报》
EI
CAS
CSCD
北大核心
1990年第1期83-89,共7页
Transactions of the Chinese Society for Agricultural Machinery
