Study of stability of moderately thick composite laminates under axial compression loading and shear loading

Xiaojun Shao; Zhufeng Yue; Lizhou Li; Qingmao Zhang

Study of stability of moderately thick composite laminates under axial compression loading and shear loading

Xiaojun Shao
, Zhufeng Yue
, Lizhou Li
, Qingmao Zhang

力学与土木建筑学院

Northwestern Polytechnical University Xian
China Aviation Industry Corporation

科研成果: 期刊稿件 › 文章 › 同行评审

7 引用（Scopus）

摘要

The stability of moderately thick composite laminates under axial compression loading and shear loading is analyzed by means of linear buckling analytical method and arc-length method. The first order buckling mode and buckling equilibrium path are presented. Under axial compression loading, the laminates can not take on any increasing load after they lost stability, but Laminates are impossible lost stability under shear loading.

源语言	英语
页（从-至）	716-720
页数	5
期刊	Jixie Qiangdu/Journal of Mechanical Strength
卷	28
期	5
出版状态	已出版 - 10月 2006

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引用此

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title = "Study of stability of moderately thick composite laminates under axial compression loading and shear loading",

abstract = "The stability of moderately thick composite laminates under axial compression loading and shear loading is analyzed by means of linear buckling analytical method and arc-length method. The first order buckling mode and buckling equilibrium path are presented. Under axial compression loading, the laminates can not take on any increasing load after they lost stability, but Laminates are impossible lost stability under shear loading.",

keywords = "Arc-length method, Buckling, Moderately thick composite laminates",

author = "Xiaojun Shao and Zhufeng Yue and Lizhou Li and Qingmao Zhang",

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T1 - Study of stability of moderately thick composite laminates under axial compression loading and shear loading

AU - Shao, Xiaojun

AU - Yue, Zhufeng

AU - Li, Lizhou

AU - Zhang, Qingmao

PY - 2006/10

Y1 - 2006/10

N2 - The stability of moderately thick composite laminates under axial compression loading and shear loading is analyzed by means of linear buckling analytical method and arc-length method. The first order buckling mode and buckling equilibrium path are presented. Under axial compression loading, the laminates can not take on any increasing load after they lost stability, but Laminates are impossible lost stability under shear loading.

AB - The stability of moderately thick composite laminates under axial compression loading and shear loading is analyzed by means of linear buckling analytical method and arc-length method. The first order buckling mode and buckling equilibrium path are presented. Under axial compression loading, the laminates can not take on any increasing load after they lost stability, but Laminates are impossible lost stability under shear loading.

KW - Arc-length method

KW - Buckling

KW - Moderately thick composite laminates

UR - https://www.scopus.com/pages/publications/33751564209

M3 - 文章

AN - SCOPUS:33751564209

SN - 1001-9669

VL - 28

SP - 716

EP - 720

JO - Jixie Qiangdu/Journal of Mechanical Strength

JF - Jixie Qiangdu/Journal of Mechanical Strength

IS - 5

ER -

Study of stability of moderately thick composite laminates under axial compression loading and shear loading

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