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Nonlinear dynamic properties of disk-bolt rotor with interfacial cutting faults on assembly surfaces 期刊论文
JOURNAL OF VIBRATION AND CONTROL, 2018, 卷号: 24, 页码: 4369-4382
作者:  Liu, Yi;  Liu, Heng;  Fan, BoWen
收藏  |  浏览/下载:3/0  |  提交时间:2019/11/19
Numerical analysis on the static-dynamic coupling influences of parallelism flaw in disc-rod rotor ball bearing system 期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART K-JOURNAL OF MULTI-BODY DYNAMICS, 2018, 卷号: 232, 页码: 103-112
作者:  Liu, Yi;  Liu, Heng;  Fan, Bowen
收藏  |  浏览/下载:5/0  |  提交时间:2019/11/19
Analytical study of the low frequency multi-direction isolator with high-static-low-dynamic stiffness struts and spatial pendulum 期刊论文
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2018, 卷号: 110, 页码: 521-539
作者:  Dong, Guangxu;  Zhang, Xinong;  Luo, Yajun;  Zhang, Yahong;  Xie, Shilin
收藏  |  浏览/下载:7/0  |  提交时间:2019/11/26
A Quasi-Static Method for Predicting Vehicle-Road Coupling Vibration Generated by Pavement Unevenness 期刊论文
JOURNAL OF VIBRATION ENGINEERING & TECHNOLOGIES, 2015, 卷号: 3, 期号: 2, 页码: 223-236
作者:  Lu, Zheng;  Wang, Hua;  Yao, Hailin;  Liu, Jie;  Hu, Zhi
收藏  |  浏览/下载:18/0  |  提交时间:2018/06/05
EXPERIMENTAL RESEARCH ON ACOUSTIC EMISSION ENERGY AND ROCK CRUSHING EFFECT UNDER STATIC-DYNAMIC COUPLING LOADING 期刊论文
Chinese Journal of Rock Mechanics and Engineering, 2012, 卷号: Vol.31 No.7, 页码: 1363-1368
作者:  Zhao, Fujun;  Wang, Hongyu;  Peng, Yun;  Wang, Guoju
收藏  |  浏览/下载:5/0  |  提交时间:2020/01/05
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:62/0  |  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.  
Thermo-Mechanical Coupling Statics Analysis and Transient Dynamics Analysis for Diesel Engine Piston 期刊论文
ADVANCED SCIENCE LETTERS, 2011, 卷号: 4, 期号: 8-10, 页码: 2566-2572
作者:  Wang, Yanxia;  Gao, Hui
收藏  |  浏览/下载:6/0  |  提交时间:2019/12/23
地下结构抗震设计中的静力弹塑性分析方法 期刊论文
2010, 2010
刘晶波; 李彬; 刘祥庆; Liu Jingbo; Li Bin; Liu Xiangqing
收藏  |  浏览/下载:3/0
Electro-mechanical coupling performances of a piezoelectric bimorph 期刊论文
2010, 2010
Shaoze Yan; Fuxing Zhang; Shizhu Wen
收藏  |  浏览/下载:3/0
Correlation between power and data in CMOS gates 期刊论文
2010, 2010
Li Xiangyu; Sun Yihe
收藏  |  浏览/下载:4/0


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