Model Reduction for Dynamic Analysis to Rod Component with Frequency-Dependent Damping

被引:4
作者
Tang, Guo-An [1 ]
Chen, Bin [2 ]
Liu, Jing-Hua [3 ]
Zhang, Mei-Yan [4 ]
机构
[1] Fudan Univ, Dept Mech & Engn Sci, Shanghai 200433, Peoples R China
[2] Fudan Univ, Shanghai 200433, Peoples R China
[3] Shanghai Aerosp Syst Engn Inst, Dept Launch Vehicle, Shanghai 201109, Peoples R China
[4] Fudan Univ, Dept Mech & Engn Sci, Shanghai 200433, Peoples R China
基金
中国国家自然科学基金;
关键词
STRUCTURAL SYSTEMS; TIME-DOMAIN;
D O I
10.2514/1.J053419
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper proposes a dynamic model-reduction method for damping rods that vary stiffness and damping characteristics with frequency. The damping rod considered in the paper is an elongated cylindrical body with two orthogonal symmetric planes, which can withstand tension, compression, bending, and torsion. The cross-sectional geometric shapes and the material properties are nonuniform along the rod axis. By performing numerical approximations on the frequency responses calculated from a three-dimensional finite element model, an analytical expression for the interface dynamic stiffness of the damping rod is obtained in the form of rational fractions. Based on this expression, a reduced dynamic model of only 22 degrees of freedom is established through an equivalent mathematical transformation. Examples of a single damping rod component and a satellite-bracket adapter assembly constructed using multiple damping rods demonstrate that the reduced model achieves satisfactory numerical results after degrees of freedom are substantially reduced.
引用
收藏
页码:2489 / 2498
页数:10
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