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轴压下玻/碳纤维混杂复合材料薄壁圆筒屈曲分析

王强强 孙双双 张哲

宇航材料工艺2025,Vol.55Issue(4):34-40,7.
宇航材料工艺2025,Vol.55Issue(4):34-40,7.DOI:10.12044/j.issn.1007-2330.2025.04.005

轴压下玻/碳纤维混杂复合材料薄壁圆筒屈曲分析

Buckling Analysis of Thin-walled Cylinder of Glass/Carbon Fiber Hybrid Composites Under Axial Pressure

王强强 1孙双双 1张哲1

作者信息

  • 1. 青岛科技大学机电工程学院,青岛 266061
  • 折叠

摘要

Abstract

Thin-walled cylindrical structures were prone to buckling under axial compression.In this paper,the thin-walled cylinders made of glass/carbon fiber hybrid composites(G/CFHC)were taken as the object of study,six lay-up sequences were designed,and with the help of ABAQUS finite element analysis software,the effects of the position of the single-layer carbon fiber composite boards,the thickness of lay-ups,and the mixing ratio of the glass/carbon fibers on the buckling loads of the thin-walled cylinders made of G/CFHC were designed.The results show that under the same layup angle,the change of the position of the single-layer carbon fiber plate will lead to the change of the structural buckling load,and for the unidirectional layup of G/CFHC thin-walled cylinders,the influence on the buckling load is consistent,the maximum buckling load occurs in the single-layer carbon fiber plate located in the outermost layer,and the increase of the single-layer carbon fiber plate in the multi-directional layup even makes the structural buckling load decrease.For the different layup sequences of the thin-walled cylinders,the corresponding buckling load increases gradually with the increase of the layup thickness.When the thickness and the number of layers of the structure are certain,the increase of the single-layer carbon fiber composite and the reasonable change of the mixing method of the glass/carbon fibers will increase the buckling critical load of the structure and improve the stability of the structure.

关键词

玻/碳纤维混杂复合材料/轴向压缩/薄壁圆筒/屈曲载荷

Key words

Glass/carbon fiber hybrid composites/Axial compression/Thin-walled cylinders/Buckling loads

分类

通用工业技术

引用本文复制引用

王强强,孙双双,张哲..轴压下玻/碳纤维混杂复合材料薄壁圆筒屈曲分析[J].宇航材料工艺,2025,55(4):34-40,7.

基金项目

山东省自然科学基金(No.ZR2014AL011) (No.ZR2014AL011)

宇航材料工艺

OA北大核心

1007-2330

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