东篱科研大数据发现系统（DRDS）

位置：成果数据库 > 期刊 > 期刊详情页

Effect of tip geometry and tip clearance on aerodynamic performance of a linear compressor cascade

ISSN号：1000-9361
期刊名称：《中国航空学报：英文版》
时间：0
分类：V23[航空宇航科学与技术—航空宇航推进理论与工程;航空宇航科学技术] TB651[一般工业技术—制冷工程]
作者机构：Marine Engineering College, Dalian Maritime University, Dalian 116026, China
相关基金：Acknowledgement This research was supported by the National Natural Science Foundation of China （Grant No.： 51076018）, the Fundamental Research Funds for the Central Universities, and Special- ized Research Fund for the Doctoral Program of Higher Education.

作者： Zhong Jingjun Han Shaobing Lu Huawei Kan Xiaoxu

关键词：线性压缩机, 叶尖间隙, 气动性能, 几何形状, 级联, 压气机叶片, 叶尖泄漏涡, 空气动力场, Compressor cascade, Experimental investigation, Tip clearance, Tip geometry, Tip leakage vortex

中文摘要：

Zhong Jingjun is a professor and Ph.D. advisor in the Marine Engineering College at Dalian Maritime University. His current research interest lies in the area of turbomachinery aerodynamic. Corresponding author. Tel.：＋ 86 411 84726935. E-mail addresses： zhongjj@dlmu.edu.cn （J. Zhong） Han Shaobing is a Ph.D. student in the Marine Engineering College at Dalian Maritime University. His research interest lies in the area of turbomachinery aerodynamic. E-mail addresses： hanshaobing@ 126.com （S. Han）.

同期刊论文项目