摘要
研究了离心式压缩机蜗壳中各特性参数沿周向流动的变化规律，建立了在蜗壳内总气动损失为最小的计算方程。
Change rule of various characteristic parameters for the volute of the centrifugal compressor along circumferential direction flow is researched.A computing equation taking the total aerodynamic loss in the volute is established,i.e.optimal volute design principle.
出处
《风机技术》
北大核心
1997年第5期7-11,共5页
Chinese Journal of Turbomachinery
