Numerical investigation into the buckling behavior of advanced grid stiffened composite cylindrical shell

被引:50
|
作者
Ren, Mingfa [1 ]
Li, Tong [2 ]
Huang, Qizhong [3 ]
Wang, Bo [1 ]
机构
[1] Dalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Dalian 116024, Peoples R China
[2] Queensland Univ Technol, Sch Chem Phys & Mech Engn, Brisbane, Qld 4001, Australia
[3] Beijing Composite Mat Co Ltd, State Key Lab Special Reinforce Fiber Composite M, Beijing 102101, Peoples R China
基金
中国国家自然科学基金;
关键词
Advanced grid stiffened; composite; finite element model; equivalent stiffness model; buckling; PLATE ELEMENT; LATTICE STRUCTURES; CYLINDERS; DESIGN;
D O I
10.1177/0731684414537881
中图分类号
TB33 [复合材料];
学科分类号
摘要
Advanced grid stiffened composite cylindrical shell is widely adopted in advanced structures due to its exceptional mechanical properties. Buckling is a main failure mode of advanced grid stiffened structures in engineering, which calls for increasing attention. In this paper, the buckling response of advanced grid stiffened structure is investigated by three different means including equivalent stiffness model, finite element model and a hybrid model (H-model) that combines equivalent stiffness model with finite element model. Buckling experiment is carried out on an advanced grid stiffened structure to validate the efficiency of different modeling methods. Based on the comparison, the characteristics of different methods are independently evaluated. It is arguable that, by considering the defects of material, finite element model is a suitable numerical tool for the buckling analysis of advanced grid stiffened structures.
引用
收藏
页码:1508 / 1519
页数:12
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