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  • 史治宇 ( 教授 )

    的个人主页 http://faculty.nuaa.edu.cn/szy/zh_CN/index.htm

  •   教授   博士生导师
  • 招生学科专业:
    力学 -- 【招收博士、硕士研究生】 -- 航空学院
    航空宇航科学与技术 -- 【招收硕士研究生】 -- 航空学院
    机械 -- 【招收博士、硕士研究生】 -- 航空学院
论文成果 当前位置: 中文主页 >> 科学研究 >> 论文成果
A scaled boundary finite element method for static and dynamic analyses of cylindrical shells

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所属单位:航空学院
发表刊物:Eng Anal Boundary Elem
摘要:A modeling technique based on the scaled boundary finite element method is developed for both static and dynamic analyses of cylindrical shells. A new scaling strategy is employed to ensure that the shell boundaries and the cross sections at the element inferfaces are accurately represented through the scaling process. The formulation starts directly from the three-dimensional linear elasticity theory for cylindrical shells. The principle of virtual work involving the inertial force is applied to derive the scaled boundary finite element equation. Only the in-plane dimensions of the structure are discretized with finite elements while the solution through the thickness is expressed analytically as a Padé expansion. A variable transformation procedure facilitates the development of the dynamic stiffness matrix, which leads to the static stiffness matrix and mass matrix naturally. A laminate model with arbitrary number of layers can readily be constructed. Numerical examples demonstrate the accuracy, applicability and efficiency of the two-layer model. © 2018 Elsevier Ltd
ISSN号:0955-7997
是否译文:否
发表时间:2019-01-01
合写作者:Liu, Lei
通讯作者:史治宇

 

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