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Numerical calculation and model experiment of a novel external buoy type wave energy converter for navigation lighted buoys numerical study of a novel wave energy converter 期刊论文
IET RENEWABLE POWER GENERATION, 2021, 页码: 10
作者:  Huang, Shuo;  Liu, Weiqi;  Zhang, Chao;  Sheng, Songwei;  You, Yage
收藏  |  浏览/下载：35/0  |  提交时间：2021/10/27
Design and Experiment of Triangular Prism Mast with Tape-Spring Hyperelastic Hinges 期刊论文
Chinese Journal of Mechanical Engineering, 2018, 卷号: Vol.31 No.1
作者:  Liu, RQ;  Yang, H;  Li, M;  Wang, Y;  Guo, HW
收藏  |  浏览/下载：10/0  |  提交时间：2019/04/24
Theoretical and experimental research of frequency tuning characteristics of NiTi-Al MMCs beam 期刊论文
Shanghai Jiaotong Daxue Xuebao/Journal of Shanghai Jiaotong University, 2015, 卷号: 49, 期号: [db:dc_citation_issue], 页码: 1300-1305
作者:  Wang, Yi-Qing;  Zhang, Teng;  Kuang, Xin-Bin;  Lu, Bing-Heng;  Hong, Jun
收藏  |  浏览/下载：5/0  |  提交时间：2019/12/02
Dynamic characteristics optimization for a whole vertical machining center based on the configuration of joint stiffness 期刊论文
The International Journal of Advanced Manufacturing Technology, 2015, 卷号: Vol.76 No.5-8, 页码: 1225-1242
作者:  Congying Deng;  Guofu Yin;  Hui Fang;  Zhaoyuxi Meng
收藏  |  浏览/下载：3/0  |  提交时间：2019/03/26
Dynamic properties and seismic responses of the masonry structure model strengthened with BFRP laminates 会议论文
作者:  Zhang Si;  Hu Xiao-bin;  Zhang Ming-jie;  Yang Fan;  Cai Yin-liang
收藏  |  浏览/下载：4/0  |  提交时间：2019/12/05
Effects of Machine Tool Configuration on Its Dynamics Based on Orthogonal Experiment Method 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2012, 卷号: 25, 页码: 285-291
作者:  Gao Xiangsheng;  Zhang Yidu;  Zhang Hongwei;  Wu Qiong
收藏  |  浏览/下载：2/0  |  提交时间：2020/01/06
A strong coupled CFD-CSD method on computational aeroelastity (EI CONFERENCE) 会议论文
2011 2nd International Conference on Mechanic Automation and Control Engineering, MACE 2011, July 15, 2011 - July 17, 2011, Inner Mongolia, China
Xi R.; Jia H.
收藏  |  浏览/下载：64/0  |  提交时间：2013/03/25
In this paper  a strong coupled CFD-CSD method is developed to simulate the aeroelastic phenomena. The CFD solver is based on the finite-volume algorithm for the Navier-Stokes equations on unstructured grid. The CSD solver solves the aeroelastic governing equations in the modal space. Their coupling is realized by a dual-time method. The spring-based smoothing method is adopted to deform and regenerate the aerodynamic grid. Two test cases are selected to validate the authors' method for static and dynamic aeroelastity .The results of the simulation for the static aeroelastic problems of a missile wing show that the Lift Coefficient and Drag Coefficient are severally 7% and 5% lower than those don't consider the elasticity of the wing. The results for the flutter boundary prediction of the AGARD 445.6 wing have been proved much closer to the experiment than using the DLM. This method can describe the effects of fluid viscosity more exactly for highly nonlinear transonic flight conditions. The calculation has proved reliable in the subsonic regime  but not accurate enough in the supersonic regime. 2011 IEEE.  
汽车排放测试模态试验及分析方法研究 期刊论文
2010, 2010
金振华; 黄开胜; 卢青春; 聂圣芳; JIN Zhen-hua; HUANG Kai-sheng; LU Qing-chun; NIE Sheng-fang
收藏  |  浏览/下载：2/0
Modal analysis for filament wound pressure vessels filled with fluid 期刊论文
15th International Conference on Composite Structures, 2010, 卷号: 92, 页码: 1994-1998
作者:  Wu, Z.;  Zhou, W.;  Li, H.
收藏  |  浏览/下载：1/0  |  提交时间：2019/12/24
PHYSICAL PARAMETER IDENTIFICATION OF AN RC FRAME STRUCTURE ON ELASTIC FOUNDATION 期刊论文
International Journal of Structural Stability and Dynamics, 2009, 卷号: Vol.9 No.4, 页码: 627-648
作者:  Zhou, Yun;  Yi, Wei-Jian
收藏  |  浏览/下载：4/0  |  提交时间：2020/01/13

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