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清华大学 [4]
北京航空航天大学 [4]
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大连理工大学 [2]
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期刊论文 [14]
会议论文 [1]
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An improved inverse method for multirow blades of turbomachinery
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2020, 页码: 11
作者:
Li AT
;
Zhu YL
;
Li W
;
Wang X
;
Qin W(秦伟)
收藏
  |  
浏览/下载:65/0
  |  
提交时间:2020/06/15
Inverse design method
multirow blades
turbomachinery
load distribution
transonic compressor
A method for controlled circulation trailing edge design of compressor blade [一种压气机叶型的可控环量尾缘造型方法]
期刊论文
Hangkong Dongli Xuebao/Journal of Aerospace Power, 2019, 卷号: 34, 页码: 142-155
作者:
Ning, F.
;
Li, Y.
收藏
  |  
浏览/下载:6/0
  |  
提交时间:2019/12/30
Design
Reynolds number
Circulation control
Compressor blades
Design condition
Geometrical modelling
High loadings
Numerical results
Total-pressure loss
Trailing edges
Compressors
High blade lift generation through short rotor-stator axial spacing in a tiny pump
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 79, 页码: 328-335
作者:
Xu, Han
;
Jin, Donghai
;
Wang, Mengyu
;
Du, Lin
;
Sun, Dakun
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  |  
浏览/下载:4/0
  |  
提交时间:2019/12/30
Turbomachine blades
Aero-dynamic performance
Axial spacing
Design process
Downstream stators
PIV measurements
Potential field
Subsonic compressor
Two Dimensional (2 D)
Stators
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
  |  
浏览/下载:42/0
  |  
提交时间:2017/08/17
Seal coating
High-speed rubbing
GH4169 blade
Compressor blades
Blade shear lip
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:4/0
  |  
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
Development of a Preliminary Design Method for Subsonic Splittered Blades in Highly Loaded Axial-Flow Compressors
期刊论文
APPLIED SCIENCES-BASEL, 2017, 卷号: 7
作者:
Liu, Baojie
;
Fu, Du
;
Yu, Xianjun
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  |  
浏览/下载:9/0
  |  
提交时间:2019/12/30
incidence and deviation model
compressor aerodynamics
blade-to-blade design
blades with splitter vanes
axial compressors
Fatigue life assessment of centrifugal compressor impeller based on FEA
期刊论文
ENGINEERING FAILURE ANALYSIS, 2016, 卷号: 60, 页码: 383-390
作者:
Liu, Shujie
;
Liu, Chi
;
Hu, Yawei
;
Gao, Sibo
;
Wang, Yifan
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  |  
浏览/下载:5/0
  |  
提交时间:2019/12/09
Impeller failures
Compressor blades
Fatigue life
S-N curves
Fatigue life assessment of the centrifugal compressor impeller with cracks based on the properties of FV520B
期刊论文
ENGINEERING FAILURE ANALYSIS, 2016, 卷号: 66, 页码: 177-186
作者:
Liu, Chi
;
Liu, Shujie
;
Gao, Sibo
;
Hu, Yawei
;
Zhang, Shixin
收藏
  |  
浏览/下载:7/0
  |  
提交时间:2019/12/09
Impeller failures
Fatigue life
Compressor blades
Research on meta-model based global design optimization and data mining methods
会议论文
作者:
Guo, Zhendong
;
Song, Liming
;
Li, Jun
;
Li, Guojun
;
Feng, Zhenping
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/12/02
Aero-dynamic performance
Computational resources
Isentropic efficiency
Modified differential evolution algorithms
Optimization strategy
Parameterization method
Performance indicators
Transonic compressor blades
转子叶栅非同步振荡发声特性研究
期刊论文
航空学报, 2015, 卷号: 36, 页码: 737-748
作者:
周迪
;
王晓宇
;
陈俊
;
洪志亮
;
孙晓峰
收藏
  |  
浏览/下载:5/0
  |  
提交时间:2020/01/06
压气机噪声 转子叶栅振荡 叶片间相角 转子叶片非定常载荷 三维升力面理论 compressor noise rotor blades vibration inter-blade phase angle unsteady aerodynamic force on rotor blades three-dimensional lifting surface theory
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