中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
机构
采集方式
内容类型
发表日期
学科主题
筛选

浏览/检索结果: 共14条,第1-10条 帮助

条数/页: 排序方式:
Load-bearing behaviors of the composite gravity-type anchorage: Insights from physical model and numerical tests 期刊论文  OAI收割
ENGINEERING FAILURE ANALYSIS, 2025, 卷号: 167, 页码: 21
作者:  
Wang, Chengtang;  Han, Hongju;  Wang, Hao;  Zhang, Xiuli;  Liu, Xinhua
  |  收藏  |  浏览/下载:6/0  |  提交时间:2025/06/27
Aseismic performances of constrained damping lining structures made of rubber-sand-concrete 期刊论文  OAI收割
JOURNAL OF ROCK MECHANICS AND GEOTECHNICAL ENGINEERING, 2024, 卷号: 16, 期号: 5, 页码: 1522-1537
作者:  
Mei, Xiancheng;  Sheng, Qian;  Chen, Jian;  Cui, Zhen;  Li, Jianhe
  |  收藏  |  浏览/下载:4/0  |  提交时间:2025/06/27
Conceptual design and heat transfer performance of a flat-tile water-cooled divertor target 期刊论文  OAI收割
PLASMA SCIENCE & TECHNOLOGY, 2021, 卷号: 23
作者:  
LI, Lei;  Han, Le;  Zi, Pengfei;  Cao, Lei;  Xu, Tiejun
  |  收藏  |  浏览/下载:49/0  |  提交时间:2021/08/30
Modelling the scores and performance statistics of NBA basketball games 期刊论文  OAI收割
COMMUNICATIONS IN STATISTICS-SIMULATION AND COMPUTATION, 2020, 卷号: 49, 期号: 10, 页码: 2604-2616
作者:  
Song, Kai;  Zou, Qingrong;  Shi, Jian
  |  收藏  |  浏览/下载:36/0  |  提交时间:2021/01/14
Performance of the insulation mock-ups for the ITER PF6 coil 期刊论文  OAI收割
FUSION ENGINEERING AND DESIGN, 2018, 卷号: 137, 期号: 无, 页码: 362-372
作者:  
Wu, Huan;  Song, Yuntao;  Lu, Kun;  Wei, Jing;  Shen, Guang
  |  收藏  |  浏览/下载:38/0  |  提交时间:2020/03/31
Development of fast response freezing valve for liquid lithium application in tokamak 期刊论文  OAI收割
VACUUM, 2016, 卷号: 127, 期号: 无, 页码: 73-81
作者:  
Chen, Zhaoxi;  Yang, Qingxi;  Song, Yuntao;  Hu, Jiansheng;  Zuo, Guizhong
收藏  |  浏览/下载:41/0  |  提交时间:2017/07/19
爆轰驱动膨胀管性能研究 期刊论文  OAI收割
航空学报, 2016, 卷号: 37, 期号: 3, 页码: 810-816
作者:  
周凯;  汪球;  胡宗民;  姜宗林
收藏  |  浏览/下载:36/0  |  提交时间:2016/12/16
Investigation of pipe separation technology in the oilfield 会议论文  OAI收割
2nd International Conference on Energy, Environment and Sustainable Development, EESD 2012, Jilin, PEOPLES R CHINA, OCT 12-14, 2012
作者:  
Zhong XF(钟兴福);  Wu YX(吴应湘);  Li SM;  Wei PJ
收藏  |  浏览/下载:35/0  |  提交时间:2013/02/26
Aerodynamic design on China new high-speed trains 会议论文  OAI收割
1st International Workshop on High-Speed and Intercity Railways, IWHIR 2011, Shenzhen, Hong Kong, China, JULY 19-22, 2011
作者:  
Yang GW(杨国伟);  Yang GW(杨国伟)
收藏  |  浏览/下载:43/0  |  提交时间:2013/02/06
Modular aircraft simulation platform based on simulink (EI CONFERENCE) 会议论文  OAI收割
2010 IEEE International Conference on Mechatronics and Automation, ICMA 2010, August 4, 2010 - August 7, 2010, Xi'an, China
Chen C.-Q.; Ji Y.
收藏  |  浏览/下载:30/0  |  提交时间:2013/03/25
Aircraft simulation platform is the most important supporting technology in the aircraft development process. This simulation platform can be used for validating the design of subsystem and also it provides the necessary data for the Aircraft design. Wind has great impact on the flight parameter. In order to accurately simulate the wind model and calculate the flight parameters  a simulation modeling method for flight parameter simulation platform under wind field environment is established. Firstly  the various sub-systems which affecting flight parameters are analyzed  some mathematical models of the flight parameter simulation platform is established. Secondly  the atmospheric wind field is studied to analyze the impact on its trajectory. Then the model is built in the Simulink toolbox in the Matlab which is based on the principles of hierarchy and modularity  using C MEX S-function for the complex kinetic equations. Finally  when the models have been established  encapsulating models for several subsystem and assembling them for the Aircraft simulation platform based on the unified interface. The simulation tests (including the performance test of a certain gliding Aircraft  the wind influence test of a certain uncontrolled aircraft) prove the simulation capability of the platform  and its calculating step can reach 1 ms. Comparing simulation with field test data of a certain uncontrolled aircraft  it shows that the relative deviation of range is 0.47%  the relative deviation of maximal altitude is 2.1%. Taking relevant standards as a reference standard  it is demonstrated the platform is reliable  meets the engineering accuracy requirements. 2010 IEEE.