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北京大学 [5]
北京航空航天大学 [5]
西安交通大学 [4]
大连理工大学 [2]
金属研究所 [2]
山东大学 [2]
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期刊论文 [15]
会议论文 [6]
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2017 [21]
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Investigation and simulation of the shear lip phenomenon observed in a high-speed abradable seal for use in aero-engines
期刊论文
WEAR, 2017, 卷号: 386-387, 页码: 195-203
Xue, Weihai
;
Gao, Siyang
;
Duan, Deli
;
Zheng, Hailiang
;
Li, Shu
收藏
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浏览/下载:41/0
  |  
提交时间:2017/08/17
Seal coating
High-speed rubbing
GH4169 blade
Compressor blades
Blade shear lip
An integrated polishing method for compressor blade surfaces
期刊论文
2017, 卷号: 88, 页码: 1723-1733
作者:
Xiao, Guijian[1]
;
Huang, Yun[1]
;
Yin, Jiachao[1]
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  |  
浏览/下载:3/0
  |  
提交时间:2019/11/28
Multidisciplinary Analysis Transient Flow Effects on the Impeller in a Semi-open Centrifugal Impeller Stage
会议论文
2017 IEEE 21ST INTERNATIONAL CONFERENCE ON COMPUTER SUPPORTED COOPERATIVE WORK IN DESIGN (CSCWD), 2017-01-01
作者:
Xie, Rong
;
Hao, Muting
;
Guan, Liang
;
Shi, Yanjun
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  |  
浏览/下载:5/0
  |  
提交时间:2019/12/03
Centrifugal compressor
Semi-open impeller stage
Transient Flow
Numerical simulation
Vortex shedding
low-energy group
blade failure
Multidisciplinary analysis
BLADE INCIPIENT CRACK DETERMINATION FOR CENTRIFUGAL COMPRESSOR BASED ON CWT-STOCHASTIC RESONANCE METHOD
会议论文
ASME Turbo Expo: Turbine Technical Conference and Exposition, Charlotte, NC, 2017-06-26
作者:
Li, Hongkun
;
He, Changbo
;
Zhou, Qiang
;
Lu, Fuan
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  |  
浏览/下载:2/0
  |  
提交时间:2019/12/03
Influence of geometrical modeling on the results of numerical prediction for the centrifugal compressor with shrouded impeller
期刊论文
Zhongguo Kexue Jishu Kexue/Scientia Sinica Technologica, 2017, 卷号: 47, 页码: 618-631
作者:
Tang, Yonghong
;
Tian, Yubao
;
Wang, Zhiheng
;
Xi, Guang
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  |  
浏览/下载:2/0
  |  
提交时间:2019/11/26
Blade thickness
Fillet
Mass flow rate
Shroud gap
Shrouded impeller
Impact of Defective Blades on Aerodynamic Performance of Transonic Compressor Rotor
期刊论文
Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2017, 卷号: 38, 页码: 2357-2362
作者:
Jiang, Wei
;
Ju, Ya-Ping
;
Zhang, Chu-Hua
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  |  
浏览/下载:4/0
  |  
提交时间:2019/11/26
Aero-dynamic performance
Defective blade
Geometry parameterization
Performance degradation
Performance variations
Polytropic efficiency
Theoretical values
Transonic compressor rotor
Unsteady flow structures in the tip region for a centrifugal compressor impeller before rotating stall
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 页码: 924-934
作者:
Zhao HuiJing
;
Wang ZhiHeng
;
Xi Guang
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  |  
浏览/下载:7/0
  |  
提交时间:2019/11/26
centrifugal compressor impeller
tip leakage flow
blade loading
flow unsteadiness
Effects of Coverage of Dynamic Mesh Region on Efficiency and Accuracy of Coupled Fluid Structure Simulation for Blade Flutter
期刊论文
Tuijin Jishu/Journal of Propulsion Technology, 2017, 卷号: 38, 页码: 2086-2092
作者:
Wang, Rui
;
Zhong, Ji-Ze
;
Xu, Zi-Li
;
Kan, Xuan-En
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浏览/下载:3/0
  |  
提交时间:2019/11/26
Aeroelastic stability
Blade
Compressor blades
Dynamic mesh
Flutter boundaries
Logarithmic decrement
Maximum displacement
Reynolds Averaged Navier-Stokes Equations
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
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  |  
浏览/下载:6/0
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提交时间:2017/12/03
Axial compressor
Boundary layer suction
Bowed blade
Corner separation
Coupled method
Passage vortex
ADJOINT AERODYNAMIC OPTIMIZATION OF A TRANSONIC FAN ROTOR BLADE WITH A LOCALIZED TWO-LEVEL MESH DEFORMATION METHOD
会议论文
Tang, Xiao
;
Luo, Jiaqi
;
Liu, Feng
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  |  
浏览/下载:5/0
  |  
提交时间:2017/12/03
AXIAL COMPRESSOR ROTOR
FLOW
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