学术论文

[1]Tian Guo, Zili Xu. Structural health monitoring using DOG multi-scale space: An approach for analyzing damage characteristics[J]. Smart Materials and Structures, 27(3),1361-665, 2018.
[2]Tian Guo, Zili Xu. Data fusion of multi-scale representations for structural damage detection[J]. Mechanical Systems and Signal Processing, 98(5): 1020-1033. 2018.
[3]Jize Zhong, Zili Xu. A reduced mesh movement method based on pseudo elastic solid for fluid structure interaction. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, 2018.232(6):973-986.
[4]Jize Zhong, Zili Xu. A time-space synchronized fluid structure coupling algorithm for the prediction of wing flutter[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2018,232(5):922-931
[5]Xuanen Kan, Zili Xu. Vibration localization for a rotating mistuning bladed disk with the Coriolis effect by a state space decoupling method[J]. Pro. ImechE Part G: Journal of Aerospace Engineering. 2017, DOI:101177/0954410017744238.
[6]Jize Zhong, Zili Xu. A reduced mesh movement method based on pseudo elastic solid for fluid structure interaction. Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science.2017, DOI: 10.1177/0954 406 217700177.
[7]Tian Guo, Zili Xu. Data fusion of multi-scale representations for structural damage detection[J]. Mechanical Systems and Signal Processing.98:1020-1033.2017.
[8]Xuanen Kan, Zili Xu, Bo Zhao, Jize Zhong. Effect of Coriolis Force on Forced Response Magnification of Intentionally Mistuned Bladed Disk[J].Journal of Sound and Vibration.399(7): 124-136. 2017.
[9]Jize Zhong, Zili Xu. A modal approach for coupled fluid structure computations of wing flutter[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.231(1):72-81.2017.
[10]Jize Zhong, Zili Xu,An energy method for flutter analysis of wing using one-way fluid structure coupling[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering.231(14): 2560–2569, 2017.

[11]Jize Zhong, Zili Xu, Coupled fluid structure analysis for wing 445.6 flutter using a fast dynamic mesh technology[J].International Journal of Computational Fluid Dynamics, 30(7-10): 531-542, 2016.

[12]Bo Zhao, Xuanen Kan, Jize Zhong, Tian Guo. Structural damage detection by using single natural frequency and the corresponding mode shape[J]. Shock and Vibration2016(1):1-8. 2016.

[13]Jize Zhong, Zili Xu. Effect of the coverage of dynamic mesh region on the efficiency and accuracy of coupled fluid structure simulation for blade flutter[C]. Proceedings of ASME Turbo Expo 2015, GT2015-43147. June 15-19, 2015, Montréal, Canada. SCI: UT CSCD:6075444.

[14]Xuanen Kan, Zili Xu, Yu Zhao, Baitong Dou, Wenbin Zhao. Tiejun Wang. Transient response of control stage blade disk due to partial admission by a reduced method[C]. Proceedings of ASME Turbo Expo 2015, GT2015-43194. June 15-19, 2015, Montréal, Canada. EI: 20160301830532.

[15]Chen Dexiang, Xu Zili,Shi Liu, Xiong-xin Feng. Least Squares Finite Element Method with High Continuity NURBS Basis for Incompressible Navier-Stokes Equations[J].  Journal of computational physics,260:204-221. 2014.

[16]Xu Zili, Yang Yi, Zhang chunmei. Modeling contact interface between rough surfaces based on fractal contact model and thin layer elements[C]. 20th International Congress on Sound and Vibration (ICSV20), Bangkok, Thailand, 7-11 July 2013, ICSV20-593

[17]Yalin Liu,Bo Shangguan, Zili Xu. A friction contact stiffness model of fractal geometry in forced response analysis of shrouded blade[J]. Nonlinear Dynamics, 70(3):2247-2257. 2012.

[18]Shangguan Bo, Xu Zili. Experimental study of friction damping of blade with loosely assembled dovetail attachment[J]. Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy,226(6) 738–750. 2012.

[19]Gu Weiwei, Xu Zili, Liu Yalin. A method to predict the nonlinear vibratory response of bladed disk system with shrouded dampers[J]. Proceedings of the Institution of Mechanical Engineers(Proc. IMechE),Part C, Journal of Mechanical Engineering Science. 2012,226(6):1620-1632.

[20]Weiwei Gu, Zili Xu, Shangjin Wang. Advanced modeling of friction contact in three-dimensional motion when analysing of the forced response of a shrouded blade. Proc. IMechE Part A: Journal of Power and Energy.,224:573-582.2010.

论文期刊
论文标题 作者 发表/完成日期 期刊名称
基于遗传算法的汽轮机转子启动优化研究 李猛,徐自力2017-09-15西安交通大学学报
拉杆转子界面局部脱开识别的改进广义柔度矩阵法 赵 博,徐自力,阚选恩2017-06-05振动工程学报
Data fusion of multi-scale representations for structural damage detection Tian Guo, Zili Xu2017-05-31Mechanical Systems and Signal Processing
Effect of Coriolis Force on Forced Response Magnification of Intentionally Mistuned Bladed Disk Xuanen Kan, Zili Xu, Bo Zhao, Jize Zhong2017-03-05Journal of Sound and Vibration
A reduced mesh movement method based on pseudo elastic solid for fluid structure interaction Jize Zhong, Zili Xu2017-02-28Journal of Mechanical Engineering Science
基于虚拟弹性体的快速动网格方法 仲继泽,徐自力,陶磊2016-10-30西安交通大学学报
超超临界汽轮机高压转子冷态启动优化 李猛,徐自力2016-10-262016年中国动力工程学会透平专业委员会学术研讨会
核电汽轮机2米等级超长叶片动应力计算分析 23. 王蕤,仲继泽,徐自力,范志飞,范小平,方宇,王建录2016-10-262016年中国动力工程学会透平专业委员会学术研讨会
Coupled fluid structure analysis for wing 445.6 flutter using a fast dynamic mesh technology Zhong J, Xu Z2016-10-25International Journal of Computational Fluid Dynamics
大容量汽轮机阀序改造后调节级叶片强度安全性分析 常东锋, 谷伟伟, 徐自力2016-10-12汽轮机技术
大容量汽轮机不同阀序工况下调节级叶片的动应力数值分析 谷伟伟,常东锋,江浩,徐自力2016-09-28汽轮机技术
一种求解含围带阻尼成圈叶片振动响应的高效方法 邱恒斌,徐自力,刘雅琳,上官博2016-09-20西安交通大学学报
基于快速动网格技术的时空同步流固耦合算法 仲继泽,徐自力2016-09-19振动工程学报
Structural damage detection by using single natural frequency and the corresponding mode shape Bo Zhao, Xuanen Kan, Jize Zhong, Tian Guo2016-08-19Shock and Vibration
叶片弯曲与轴扭转耦合振动机理 徐自力,赵 宇 ,周子宣2016-08-08第12届全国转子动力学学术研讨会下册
An energy method for flutter analysis of wing using one-way fluid structure coupling Zhong J, Xu Z2016-06-24Journal of Aerospace Engineering
动网格区域对叶片颤振流固耦合计算效率及精度的影响 王蕤,仲继泽,徐自力,阚选恩2016-06-23推进技术
一种正压力随时间变化的微滑移干摩擦模型 上官博, 徐自力, 肖俊峰, 高松, 于飞龙2016-06-08振动工程学报
基于热固双向耦合模型的二次再热超超临界汽轮机超高压转子热应力研究 袁建宝,徐自力,李溶江,刘金芳,张晓东,刘东旗2016-03-30东方汽轮机
A modal approach for coupled fluid structure computations of wing flutter Jieze Zhong, Zili Xu2016-03-23Journal of Aerospace Engineering
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