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科研机构
大连理工大学 [4]
北京航空航天大学 [2]
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期刊论文 [6]
发表日期
2019 [2]
2018 [3]
2014 [1]
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Control of corner separation via dimpled surface for a highly loaded compressor cascade under different inlet Mach number
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 85, 页码: 48-60
作者:
Lu, Huawei
;
Yang, Yi
;
Guo, Shuang
;
Pang, Wenxuan
;
Yang, Fan
收藏
  |  
浏览/下载:8/0
  |  
提交时间:2019/12/02
Highly loaded compressor cascade
Dimple
Flow loss
Variation of inlet Mach number
Control of corner separation via dimpled surface for a highly loaded compressor cascade under different inlet Mach number
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 85, 页码: 48-60
作者:
Lu, Huawei
;
Yang, Yi
;
Guo, Shuang
;
Pang, Wenxuan
;
Yang, Fan
收藏
  |  
浏览/下载:9/0
  |  
提交时间:2019/12/30
Highly loaded compressor cascade
Dimple
Flow loss
Variation of inlet Mach number
Flow control in linear compressor cascades by inclusion of suction side dimples at varying locations
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2018, 卷号: 232, 页码: 706-721
作者:
Lu, Hua-wei
;
Yang, Yi
;
Guo, Shang
;
Huang, Yu-xuan
;
Wang, Hong
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/02
Highly loaded compressor cascade
dimples
flow control
numerical simulation
The effect of dimpled surface on loss reduction and vortices in a highly loaded compressor cascade
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2018, 卷号: 232, 页码: 374-387
作者:
Lu, Hua-wei
;
Yang, Yi
;
Guo, Shuang
;
Huang, Yu-xuan
;
Wang, Hong
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/02
Dimpled surface
highly loaded compressor cascade
flow control
topological structure
numerical simulation
Experimental investigation on separation control by slot jet in highly loaded compressor cascade
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2018, 卷号: 232, 页码: 1704-1714
作者:
Hu Jiaguo
;
Wang Rugen
;
Li Renkang
;
He Chen
;
Li Qiushi
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Compressor cascade
highly loaded
flow control
trailing edge separation
corner separation
slot jet
THE EFFECTS OF CAVITY GEOMETRY ON AN ASPIRATED COMPRESSOR CASCADE
期刊论文
JOURNAL OF THEORETICAL AND APPLIED MECHANICS, 2014, 卷号: 52, 页码: 117-128
作者:
Guo, Shuang
;
Lu, Hua-Wei
;
Liu, Jie
;
Wu, Chui-Jie
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/09
highly loaded compressor cascade
boundary layer suction
suction flow distribution
off-take cavity
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