Experimental investigation of the damage propagation in composite specimens under biaxial loading

被引：9

作者：

Bisagni, Chiara ^{[1
,2
]}

Walters, Carey ^{[1
]}

机构：

[1] MIT, Impact & Crashworthiness Lab, Dept Mech Engn, Cambridge, MA 02139 USA

[2] Politecn Milan, Dept Aerosp Engn, I-20156 Milan, Italy

来源：

COMPOSITE STRUCTURES | 2008年 / 85卷 / 04期

关键词：

composite material; damage propagation; delamination; failure; combined loads;

D O I：

10.1016/j.compstruct.2007.10.029

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

This paper deals with biaxial testing of flat specimens made of graphite-epoxy. Using a dual actuator hydraulic testing machine, combinations of axial and transverse loading are applied to the specimens. The corresponding strain fields are determined from digital image correlation. Two test series were performed with two different graphite-epoxy materials. Half of the specimens were manufactured containing artificial delaminations for the purpose of evaluating the effect of the reduction in the resistance given by the out-of-plane displacements, and of investigating the damage propagation. The results of this study can be used to improve the understanding of the different failure modes of composite structures, and to guide the development of finite element models able to predict their failure mechanism. (C) 2007 Elsevier Ltd. All rights reserved.

引用

页码：293 / 310

页数：18

共 20 条

[1] Progressive failure analyses of compression-loaded composite curved panels with and without cutouts [J].

Ambur, DR ;

Jaunky, N ;

Hilburger, M ;

Dávila, CG .

COMPOSITE STRUCTURES, 2004, 65 (02) :143-155

[2] Post-buckling and collapse experiments of stiffened composite cylindrical shells subjected to axial loading and torque [J].

Bisagni, C ;

Cordisco, P .

COMPOSITE STRUCTURES, 2006, 73 (02) :138-149

[3]

Bisagni C, 2006, P 47 AIAA ASME ASCE, P1, DOI [10.2514/6.2006-2178, DOI 10.2514/6.2006-2178]

[4]

Camanho PP, 2003, J COMPOS MATER, V37, P1415, DOI [10.1177/0021998303034505, 10.1177/002199803034505]

[5] DAMAGE TOLERANCE OF LAMINATED COMPOSITES CONTAINING AN OPEN HOLE AND SUBJECTED TO COMPRESSIVE LOADINGS .1. ANALYSIS [J].

CHANG, FK ;

LESSARD, LB .

JOURNAL OF COMPOSITE MATERIALS, 1991, 25 (01) :2-43

[6] Failure criteria for FRP laminates [J].

Dávila, CG ;

Camanho, PP ;

Rose, CA .

JOURNAL OF COMPOSITE MATERIALS, 2005, 39 (04) :323-345

[7] Post-buckling behavior of composite panels in the presence of unstable delaminations [J].

Gaudenzi, P ;

Perugini, P ;

Riccio, A .

COMPOSITE STRUCTURES, 2001, 51 (03) :301-309

[8] Recent advances to assess mono- and multi-delaminations behaviour of aerospace composites [J].

Guédra-Degeorges, D .

COMPOSITES SCIENCE AND TECHNOLOGY, 2006, 66 (06) :796-806

[9] FAILURE CRITERIA FOR UNIDIRECTIONAL FIBER COMPOSITES [J].

HASHIN, Z .

JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1980, 47 (02) :329-334

[10] Predicting failure in composite laminates: The background to the exercise [J].

Hinton, MJ ;

Soden, PD .

COMPOSITES SCIENCE AND TECHNOLOGY, 1998, 58 (07) :1001-1010

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