Delamination onset in symmetric cross-ply laminates under static loads: Theory, numerics and experiments

被引：30

作者：

Carraro, Paolo Andrea ^{[1
]}

Novello, Elisa ^{[1
]}

Quaresimin, Marino ^{[1
]}

Zappalorto, Michele ^{[1
]}

机构：

[1] Univ Padua, Dept Management & Engn, Str S Nicola 3, Vicenza, Italy

来源：

COMPOSITE STRUCTURES | 2017年 / 176卷

关键词：

Delamination; Transverse cracks; Cross ply laminates; Generalized Stress Intensity Factors; STRESS INTENSITY FACTOR; CRACK INDUCED DELAMINATION; INTERFACE RELATED DAMAGE; MIXED-MODE DELAMINATION; LAP BONDED JOINTS; FATIGUE DELAMINATION; TRANSVERSE CRACKING; FRACTURE INITIATION; SHARP NOTCHES; PART II;

D O I：

10.1016/j.compstruct.2017.05.030

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

In this paper, the delamination onset from transverse cracks in composite cross-ply laminates under static loadings is thoroughly investigated. Initially, an analytical solution is presented for the local mode I, II and III stress fields arising in the close neighbourhoods of a transverse crack, stresses being written as a function of Generalized Stress Intensity Factors (GSIFs). Then, a fracture criterion for the delamination onset in cross-ply laminates under tension, based on a critical value for the mode 1 GSIF, is proposed and validated taking advantage of the results from an experimental campaign carried out in the present work, as well as reconsidering some data taken from the literature. (C) 2017 Elsevier Ltd. All rights reserved.

引用

页码：420 / 432

页数：13

共 76 条

[1] THE INFLUENCE OF LOCAL GEOMETRY ON THE STRENGTH OF ADHESIVE JOINTS [J].

ADAMS, RD ;

HARRIS, JA .

INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 1987, 7 (02) :69-80

[2] A mechanistic model for fatigue damage evolution in composite laminates [J].

Akshantala, NV ;

Talreja, R .

MECHANICS OF MATERIALS, 1998, 29 (02) :123-140

[3] A micromechanics based model for predicting fatigue life of composite laminates [J].

Akshantala, NV ;

Talreja, R .

MATERIALS SCIENCE AND ENGINEERING A-STRUCTURAL MATERIALS PROPERTIES MICROSTRUCTURE AND PROCESSING, 2000, 285 (1-2) :303-313

[4] A non-linear damage evolution model for mode II fatigue delamination onset and growth [J].

Allegri, G. ;

Wisnom, M. R. .

INTERNATIONAL JOURNAL OF FATIGUE, 2012, 43 :226-234

[5] Empirical model for stress ratio effect on fatigue delamination growth rate in composite laminates [J].

Andersons, J ;

Hojo, M ;

Ochiai, S .

INTERNATIONAL JOURNAL OF FATIGUE, 2004, 26 (06) :597-604

[6] Model of delamination propagation in brittle-matrix composites under cyclic loading [J].

Andersons, J ;

Hojo, M ;

Ochiai, S .

JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2001, 20 (05) :431-450

[7] ORTHOTROPIC LAMINATE COMPOSITE CONTAINING A LAYER WITH A CRACK [J].

ARIN, K .

INTERNATIONAL JOURNAL OF ENGINEERING SCIENCE, 1977, 15 (9-10) :545-559

[8]

Berthelot J.-M., 2003, Applied Mechanics Review, V56, P111, DOI 10.1115/1.1519557

[9] A model for transverse cracking and delamination in cross-ply laminates [J].

Berthelot, JM ;

Le Corre, JF .

COMPOSITES SCIENCE AND TECHNOLOGY, 2000, 60 (07) :1055-1066

[10] BEM analysis of damage progress in 0/90 laminates [J].

Blazquez, A. ;

Mantic, V. ;

Paris, F. ;

McCartney, N. L. .

ENGINEERING ANALYSIS WITH BOUNDARY ELEMENTS, 2009, 33 (06) :762-769

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