摘要
用一维理论对轴流压气机的初步设计作进一步的研究,导出了多级轴流压气机特性关系,建立了在给定轴向分速时最优化设计的数学模型,得到了解析关系.所得结论具有普适性,对多级轴流压气机的初步设计有一定的指导作用.
The preliminary design of a multistage axial flow compressor using one\|dimensional flow theory is studied. The characteristic relation of an axial flow compressor stage is obtained. The model for the optimum design of a multistage axial flow compressor for the fixed distribution of axial velocity is presented. The analytical relations are obtained. The results are universal and can provide some guides for the optimum design of multistage compressor.
出处
《海军工程大学学报》
CAS
2002年第6期100-103,111,共5页
Journal of Naval University of Engineering
基金
海军工程大学2001年度科研基金项目(69773021)
关键词
一维
多级
轴流压气机
性能
效率
优化
multistage axial flow compressor
efficiency
optimization
