Framework of Physically Consistent Homogenization and Multiscale Modeling of Shell Structures

被引:1
作者
Zhang, Zewei [1 ,2 ]
Lu, Zhiyuan [1 ,2 ]
Yang, Yu [3 ]
Dong, Leiting [1 ,2 ]
Atluri, Satya N. [4 ,5 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Natl Key Lab Strength & Struct Integr, Beijing 100191, Peoples R China
[2] Tianmushan Lab, Hangzhou 310023, Peoples R China
[3] Aircraft Strength Res Inst China, Natl Key Lab Strength & Struct Integr, Xian 710065, Shaanxi, Peoples R China
[4] Texas Tech Univ, Dept Mech Engn, Lubbock, TX 79409 USA
[5] AIAA, Reston, VA 20191 USA
基金
中国国家自然科学基金;
关键词
Structural Modeling and Simulation; Shell Structures; Homogenization; Multiscale Modeling; Boundary Condition; COMPOSITE; PLATES;
D O I
10.2514/1.J064645
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A framework of physically consistent homogenization and multiscale modeling (PCHMM) for reduced-order analysis of plate/shell structures is developed in this paper. To address the inapplicability of conventional periodic boundary conditions and Hill's condition involved in homogenization of shear-deformable shell structures, the paper proposes physically consistent boundary conditions and modified Hill's condition for plate/shells. Unlike the PCHMM method for beams, considering the contradiction between high-order displacement fields induced by shear forces and low-order kinematic assumptions, additional constraints are applied to the plate/shell structure sectional strains during the solution of perturbation fields. The correctness and effectiveness of the proposed plate/shell PCHMM framework and method are verified by typical numerical examples. The proposed theory can also be conveniently embedded into commercial finite element software for homogenization and multiscale analysis of structures such as microscale metamaterials like lattice plates and large complex structures like aircraft fuselage sections.
引用
收藏
页码:260 / 273
页数:14
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