Influence of Blade Tip Winglet Combined With Tip Groove on the Leakage Flow of Transonic Compressor Rotor

被引：0
|
作者：
Han, Shaobing [1 ]
Zhao, Ao [1 ]
Zhao, Yuzhou [1 ]
Zhong, Jingjun [2 ]
机构：
[1] Naval Architecture and Ocean Engineering College, Dalian Maritime University, Dalian,116026, China
[2] Merchant Marine College, Shanghai Maritime University, Shanghai,201306, China
来源：
Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics | 2022年 / 43卷 / 07期
关键词：
Compendex;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Shock waves
引用
收藏
页码：1859 / 1869
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