Progressive Failure Analysis of Laminated Composite Plates With Two Serial Pinned Joints

被引：19

作者：

Turan, Kadir ^{[1
]}

Kaman, Mete Onur ^{[2
]}

Gur, Mustafa ^{[2
]}

机构：

[1] Dicle Univ, Dept Mech Engn, TR-21280 Diyarbakir, Turkey

[2] Firat Univ, Dept Engn Mech, TR-23169 Elazig, Turkey

来源：

MECHANICS OF ADVANCED MATERIALS AND STRUCTURES | 2015年 / 22卷 / 10期

关键词：

progressive failure analysis; pinned joints; finite element method; laminated composites; GEOMETRIC PARAMETERS; BOLTED JOINTS; DAMAGE MODEL; STRENGTH; BEHAVIOR;

D O I：

10.1080/15376494.2012.761302

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

This study presents experimental and numerical failure analyses for two serial pin loaded holes in unidirectional carbon fiber/epoxy resin composite laminates. The failure loads and failure modes of composite laminates are determined for different geometrical parameters and different stacking sequences. Three-dimensional ANSYS Parametric Design Language codes are developed in the ANSYS (R) finite element software. Hashin Failure Criteria and material degradation rules are used to determine failure loads and failure modes in the numerical analysis. Experimental and numerical results show that failure loads and failure modes were affected with geometrical parameters.

引用

页码：839 / 849

页数：11

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