中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
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Graphical models of dominant topologies of polymer-substrate adhesive-interfacial strength and toughness 期刊论文  OAI收割
ACTA MECHANICA SINICA, 2025, 卷号: 41, 期号: 3, 页码: 11
作者:  
王新天洋;  Liao LJ(廖丽涓);  Wu XQ(吴先前);  Huang CG(黄晨光)
  |  收藏  |  浏览/下载:15/0  |  提交时间:2024/11/01
Graphical models of dominant topologies of polymer-substrate adhesive-interfacial strength and toughness 期刊论文  OAI收割
ACTA MECHANICA SINICA, 2025, 卷号: 41
作者:  
Wang, Xintianyang;  Liao, Lijuan;  Wu, Xianqian;  Huang, Chenguang
  |  收藏  |  浏览/下载:46/0  |  提交时间:2024/11/20
Hand-drawn sketch and vector map matching based on topological features 期刊论文  OAI收割
FRONTIERS IN EARTH SCIENCE, 2023, 卷号: 11
作者:  
Lu, Yuefeng;  Sun, Ying;  Liu, Shuo;  Li, Jing;  Liu, Yanru
  |  收藏  |  浏览/下载:35/0  |  提交时间:2023/04/06
Dependence of Field Splitting Characteristics on Metallic Components Topological Configuration in Multilaminar Plasmonic Films 期刊论文  OAI收割
IEEE Transactions on Nanotechnology, 2021, 卷号: 20, 页码: 715-725
作者:  
Kang, Yifan;  Yang, Hongtao;  Wang, Chao;  Li, Yongfeng;  Cao, Weiwei
  |  收藏  |  浏览/下载:25/0  |  提交时间:2021/10/11
Influence of the topological structures of the nose of high-speed maglev train on aerodynamic performances 会议论文  OAI收割
Virtual, Online, 10 August 2021 到 12 August 2021
作者:  
Wang YT(王业腾);  Sun ZX(孙振旭)
  |  收藏  |  浏览/下载:20/0  |  提交时间:2021/11/30
Structure optimization of strap-down inertial navigation system support (EI CONFERENCE) 会议论文  OAI收割
2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China
作者:  
Wang J.;  Sun H.;  Sun H.
收藏  |  浏览/下载:31/0  |  提交时间:2013/03/25
In order to meet the requirement of inertial navigation components and minimizing the system's weight  and topological optimization was conducted. Then  topological optimization and size optimization were conducted under conditions of random vibration and impact. Firstly  according to the dynamic characteristics of missile and requirement of inertial navigation system  the structure of inertial navigation support was designed according to types of missile connection and space arrangement of electronic components  the method of transforming multi-loading cases to multi-loading constraints was used to optimizing the size of the support under conditions of random vibration and impact. Comparing to the original support structures  RMS accelerations in installed points reduced by 25.2% under random vibration  the weight of optimal structures reduced by 28.1%  the structures also met the requirement of inertial navigation system under condition of impact. The support structure shows improvements in both dynamic characteristic and light weight comparing with the original one. 2011 IEEE.