Modelling competitive delamination and debonding phenomena in composite T-Joints

被引：21

作者：

Baldi, A. ^{[1
]}

Airoldi, A. ^{[1
]}

Crespi, M. ^{[1
]}

Iavarone, P. ^{[1
]}

Bettini, P. ^{[1
]}

机构：

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

来源：

11TH INTERNATIONAL CONFERENCE ON THE MECHANICAL BEHAVIOR OF MATERIALS (ICM11) | 2011年 / 10卷

关键词：

Composite T-Joints; Delamination; Debonding; Damage Tolerace; Explicit Numerical Analysis; Cohesive Elements; SIMULATION;

D O I：

10.1016/j.proeng.2011.04.574

中图分类号：

T [工业技术];

学科分类号：

08 ;

摘要：

Experimental studies on the failure mode of composite T-joint specimens, in the presence of adhesive interlaminar layers, are presented. Tests underline the role played by the interaction between delamination and debonding phenomena. Quasi static analyses of the tests are performed by means of explicit FE models. A modelling technique based on a cohesive zone approach is adopted to simulate damage propagation both in the adhesive interface and in the most critical interlaminar layers of laminates. All the numerical results are compared against the experimental evidences in terms of fracture patterns, of load vs. displacement responses and local strain levels. (C) 2011 Published by Elsevier Ltd. Selection and peer-review under responsibility of ICM11

引用

页码：3483 / 3489

页数：7

共 14 条

[1]

Abaqus&REG, 2004, AB THEOR US MAN

[2]

Airoldi A, COMPOSITES IN PRESS, DOI [10.1016/j.compscitech.2009.10.011, DOI 10.1016/J.COMPSCITECH.2009.10.011]

[3]

Airoldi A, 2009, P 20 AIDAA C MIL JUN

[4]

Baldi A, 2010, P 14 EUR C COMP MAT

[5] Composite chiral structures for morphing airfoils: Numerical analyses and development of a manufacturing process [J].

Bettini, Paolo ;

Airoldi, Alessandro ;

Sala, Giuseppe ;

Di Landro, Luca ;

Ruzzene, Massimo ;

Spadoni, Alessandro .

COMPOSITES PART B-ENGINEERING, 2010, 41 (02) :133-147

[6]

Bish J, 1997, NSWCCD95TR199811CR

[7] The strength of adhesively bonded T-joints [J].

da Silva, LFM ;

Adams, RD .

INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2002, 22 (04) :311-315

[8]

Davila CG, 2001, P 42 AIAA ASME ASCII

[9]

Davila CG, 2001, P 16 TECHN C AM SOC

[10] Crack equivalent concept applied to the fracture characterization of bonded joints under pure mode I loading [J].

de Moura, M. F. S. F. ;

Campilho, R. D. S. G. ;

Goncalves, J. P. M. .

COMPOSITES SCIENCE AND TECHNOLOGY, 2008, 68 (10-11) :2224-2230

← 1 2 →