中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
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过程工程研究所 [2]
力学研究所 [1]
长春光学精密机械与物... [1]
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武汉岩土力学研究所 [1]
地球环境研究所 [1]
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OAI收割 [9]
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期刊论文 [7]
会议论文 [2]
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2022 [1]
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2019 [1]
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CFD-DEM simulation of the force acting on immersed baffles during the start-up stage of a gas-solid fluidized bed
期刊论文
OAI收割
Huagong Xuebao/CIESC Journal, 2022, 卷号: 73, 期号: 6, 页码: 2649-2661
作者:
Li, Tienan
;
Zhao, Bidan
;
Zhao, Peng
;
Zhang, Yongmin
;
Wang, Junwu
  |  
收藏
  |  
浏览/下载:0/0
  |  
提交时间:2023/06/26
Computational fluid dynamics - Dynamic loads - Numerical methods
Size segregation mechanism of reclamation fill sand due to rainbowing operations in hydraulic dredging activities
期刊论文
OAI收割
OCEAN ENGINEERING, 2021, 卷号: 242, 页码: 20
作者:
Dong, Youkou
;
Liu, Chengli
;
Wei, Houzhen
;
Meng, Qingshan
;
Zhou, Haoran
  |  
收藏
  |  
浏览/下载:37/0
  |  
提交时间:2022/02/17
Computational fluid dynamic
Discrete element method
Coupling analysis
Size segregation
Hydraulic dredging
Rainbowing
Effects of Clamping Pressure on Cold Start Behavior of Polymer Electrolyte Fuel Cells
期刊论文
OAI收割
FUEL CELLS, 2019, 卷号: 19, 期号: 3, 页码: 221-230
作者:
Dafalla, A. M.
;
Wei, L.
;
Liao, Z. H.
;
Jiang, F. M.
  |  
收藏
  |  
浏览/下载:24/0
  |  
提交时间:2020/10/29
Clamping Pressure
Cold Start
Computational Fluid Dynamic Analysis
Deformation
Fuel Cells
Hydrodynamic analysis of a gliding robotic dolphin based on Computational Fluid Dynamics
会议论文
OAI收割
35th Chinese Control Conference, CCC 2016, Chengdu, China, July 27, 2016 - July 29, 2016
作者:
Li, Kang
;
Yu, Junzhi
;
Wu, Zhengxing
;
Tan, Min
收藏
  |  
浏览/下载:43/0
  |  
提交时间:2017/01/23
Hydrodynamic Analysis
Gliding Robotic Dolphin
Computational Fluid Dynamics (CFD)
Dynamic Mesh
高压捕获翼前缘型线优化和分析
期刊论文
OAI收割
力学学报, 2016, 卷号: 48, 期号: 4, 页码: 877-885
作者:
李广利
;
崔凯
;
肖尧
;
徐应洲
收藏
  |  
浏览/下载:32/0
  |  
提交时间:2016/12/16
high pressure capturing wing
computational fluid dynamic
surrogate model
shape optimization
Analysis on the heat transfer characteristics of a micro-channel type porous-sheets Stirling regenerator
期刊论文
OAI收割
INTERNATIONAL JOURNAL OF THERMAL SCIENCES, 2015, 卷号: 94, 页码: 37-49
作者:
Li, Zhigang
;
Haramura, Yoshihiko
;
Tang, Dawei
;
Guo, Chaohong
收藏
  |  
浏览/下载:23/0
  |  
提交时间:2015/10/27
Stirling engine
Porous-sheets regenerator
Micro-channel
Heat transfer characteristics
Analytical solution
Dynamic mesh computational fluid dynamics
Modeling micro-particle deposition in human upper respiratory tract under steady inhalation
期刊论文
OAI收割
PARTICUOLOGY, 2011, 卷号: 9, 期号: 1, 页码: 39-43
作者:
Huang, JH (Huang, Jianhua)[1]
;
Zhang, LZ (Zhang, Lianzhong)[1,2]
;
Yu, SY (Yu, Suyuan)[3]
  |  
收藏
  |  
浏览/下载:25/0
  |  
提交时间:2019/01/07
Human upper airway model
Asymmetric tracheobronchial (TB) airway
Particle deposition
Computational fluid-particle dynamic
simulations
Numerical simulation of single bubble motion in ionic liquids
期刊论文
OAI收割
CHEMICAL ENGINEERING SCIENCE, 2010, 卷号: 65, 期号: 22, 页码: 6036-6047
作者:
Wang, Xiaoling
;
Dong, Haifeng
;
Zhang, Xiangping
;
Yu, Liang
;
Zhang, Suojiang
收藏
  |  
浏览/下载:22/0
  |  
提交时间:2013/11/12
Multiphase flow
Bubble
Ionic liquids
Volume-of-fluid
Computational fluid dynamic
Bubble column
The design of missile's dome that fits both optical and aerodynamic needs (EI CONFERENCE)
会议论文
OAI收割
5th International Symposium on Advanced Optical Manufacturing and Testing Technologies: Smart Structures and Materials in Manufacturing and Testing, April 26, 2010 - April 29, 2010, Dalian, China
作者:
Zhang X.
;
Zhang X.
;
Zhang X.
收藏
  |  
浏览/下载:14/0
  |  
提交时间:2013/03/25
Optical guidance missiles requires a dome which fits both optical and aerodynamic needs when they attack at 3 Ma. In this study
ellipse is the figure chosen to be the dome's shape. The ellipticity is the main variable should to be decided. The optimized function was built by optical and aerodynamic performance function multiply by their weights. The optical and aerodynamic functions were all obtained by computational fluid dynamic (CFD) simulation's results after normalization. In this study
the optical and aerodynamic performances have equal weights
after optimzing the ellipticity is 2 for the missile. 2010 SPIE.