Effects of endwall boundary layer suction position on the flow field and load in a high-turning compressor cascade

被引:0
作者
Guo, Shuang [1 ]
Chen, Fu [1 ]
Lu, Hua-Wei [2 ]
Chen, Shao-Wen [1 ]
Song, Yu-Fei [3 ]
Song, Yan-Ping [1 ]
Wang, Zhong-Qi [1 ]
机构
[1] School of Energy Science and Engineering, Harbin Inst. of Technology, Harbin 150001, China
[2] Marine Engineering Coll., Dalian Maritime Univ., Dalian 116026, China
[3] China Nuclear Power Design Company, Shenzhen 518049, China
来源
Tuijin Jishu/Journal of Propulsion Technology | 2011年 / 32卷 / 03期
关键词
D O I
暂无
中图分类号
学科分类号
摘要
12
引用
收藏
页码:323 / 328
相关论文
empty
未找到相关数据