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Study on a new numerical method for solving heat conduction problems 会议论文
Shanghai, China, November 22-24, 2019
作者:  Liu PJ(刘朋杰);  Pan FC(潘福成);  Xu, Gangfeng;  Shi, Weidong;  Wang, Ning
收藏  |  浏览/下载：0/0  |  提交时间：2020/03/31
Disturbance Rejection control for Discrete Time-delay Nonlinear System 会议论文
作者:  Ma Hui;  Tang Gong-You;  Hu Wei;  Zhang Bao-Lin;  Su Hao
收藏  |  浏览/下载：2/0  |  提交时间：2019/08/19
Disturbance Rejection control for Discrete Time-delay Nonlinear System 会议论文
作者:  Ma Hui;  Tang Gong-You;  Hu Wei;  Zhang Bao-Lin;  Su Hao
收藏  |  浏览/下载：3/0  |  提交时间：2018/12/07
Application of differential transform method to buckling problems at pined-pined boundary conditions 会议论文
2012 2nd International Conference on Machinery Electronics and Control Engineering, ICMECE 2012, December 29, 2012 - December 30, 2012
作者:  Han, Ling Feng;  Wu, Shi Yuan
收藏  |  浏览/下载：1/0  |  提交时间：2019/12/31
Positive solutions for nonlinear lidstone boundary value problems 会议论文
2012 2nd International Conference on Machinery Electronics and Control Engineering, ICMECE 2012, December 29, 2012 - December 30, 2012
作者:  Wang, Lei;  Li, Li
收藏  |  浏览/下载：2/0  |  提交时间：2019/12/31
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.  
Modal analysis of cantilever beams with an edge notch using asymptotic transfer function method 会议论文
DYNAMICS OF CONTINUOUS DISCRETE AND IMPULSIVE SYSTEMS-SERIES B-APPLICATIONS & ALGORITHMS, 2nd International Conference on Dynamics, Vibration and Control, Beijing, PEOPLES R CHINA, Web of Science
Yu, Zhigang; Feng, Xiang; Wu, Xun; Chu, Fulei
收藏  |  浏览/下载：4/0
New inverse method of centrifugal pump blade and its optimization 会议论文
Nanjing, China, October 20, 2008 - October 23, 2008
作者:  Zhang, Renhui;  Yang, Junhu;  Li, Rennian
收藏  |  浏览/下载：0/0  |  提交时间：2020/11/15
Consensus behavior of agents in networked systems under general communication topologies 会议论文
Xiao, Feng; Wang, Long
收藏  |  浏览/下载：2/0  |  提交时间：2015/11/13
Consensus behavior of agents in networked systems under general communication topologies 会议论文
Xiao, Feng; Wang, Long
收藏  |  浏览/下载：5/0  |  提交时间：2015/11/13

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