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工程热物理研究所 [30]
大连理工大学 [7]
北京航空航天大学 [6]
北京大学 [2]
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会议论文 [26]
期刊论文 [19]
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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
Turbulence anisotropy analysis in a highly loaded linear compressor cascade
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 91, 页码: 241-254
作者:
Yan, Hao
;
Liu, Yangwei
;
Lu, Lipeng
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  |  
浏览/下载:9/0
  |  
提交时间:2019/12/30
Budget control
Compressors
Kinetic energy
Kinetics
Reynolds number
Tensors
Turbulence models
Turbulent flow
Vortex flow
Aero-dynamic performance
Anisotropy invariant map
Delayed detached eddy simulation (DDES)
Linear compressors
Small scale turbulence
Threedimensional (3-d)
Turbulence anisotropy
Turbulence kinetic energy
Anisotropy
Effect of BLS via streamwise endwallslot in an annular cascade of highly loaded compressor
会议论文
Proceedings of The Third Chinese International Turbo-machinery Conference
-
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  |  
浏览/下载:2/0
  |  
提交时间:2019/12/02
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
Turbulence characteristics in corner separation in a highly loaded linear compressor cascade
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 75, 页码: 139-154
作者:
Yan, Hao
;
Liu, Yangwei
;
Li, Qiushi
;
Lu, Lipeng
收藏
  |  
浏览/下载:8/0
  |  
提交时间:2019/12/30
Anisotropy
Navier Stokes equations
Numerical methods
Shear stress
Statistical methods
Velocity
Velocity distribution
Accurate prediction
Anisotropy invariant map
Linear compressors
Structure of vortices
Threedimensional (3-d)
Turbulence anisotropy
Turbulence characteristics
Velocity histograms
Turbulence
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
Influence of coupled boundary layer suction and bowed blade on flow field and performance of a diffusion cascade
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2017
Cao Zhiyuan
;
Liu Bo
;
Zhang Ting
;
Yang Xiqiong
;
Chen Pingping
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2017/12/03
Axial compressor
Boundary layer suction
Bowed blade
Corner separation
Coupled method
Passage vortex
Comparison of aerodynamic characteristics between a novel highly loaded injected blade with curvature induced pressure-recovery concept and one with conventional design
期刊论文
中国航空学报(英文版), 2017
Zhiyuan CAO
;
Chao ZHOU
;
Zhili SUN
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2017/12/03
Axial compressor Air injection Curvature induced ‘Shock’ Flow control Separation
Axial compressor
Air injection
Curvature induced ‘Shock’
Flow control
Separation
COMPRESSOR
AIRFOILS
FLOW
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