Cohesive element for analysis of delamination growth under arbitrary mixed-mode II and II failure condition

被引：0

作者：

Kondo A. ^{[1
]}

Suematsu H. ^{[1
]}

Aoki Y. ^{[1
]}

Nagashima T. ^{[1
]}

机构：

[1] Department of Mechanical Engineering, Sophia University, Chiyoda-ku, Tokyo, 102-8554

来源：

Nihon Kikai Gakkai Ronbunshu, A Hen/Transactions of the Japan Society of Mechanical Engineers, Part A | 2010年 / 76卷 / 765期

关键词：

Composite material; Delamination; Finite element method; Fracture mechanics;

D O I：

10.1299/kikaia.76.557

中图分类号：

学科分类号：

摘要：

Novel cohesive element which can deal with non-self-similar crack growth under mixed-mode II and III failure condition is proposed. The local coordinate system based on the crack front direction is determined in terms of relative displacement of the cohesive elements. Traction-relative displacement relation of the element is determined as a function of mode components calculated on the local coordinate system. This formulation allows us to simulate delamination growth when the non-self-similar crack growth occurs and the fracture toughness depends on the mode ratio. The numerical examples revealed that the crack growth strongly depends on its history when the mode II and III fracture toughness is different and the present formulation is valid even for the simulation of such history dependent crack growth.

引用

页码：557 / 563

页数：6

共 50 条

[21] A novel mixed-mode cohesive formulation for crack growth analysis
Nhung Nguyen
Waas, Anthony M.
COMPOSITE STRUCTURES, 2016, 156 : 253 - 262
[22] Computational analysis of residual stress effects on fatigue crack growth under mode I, II and mixed-mode I/II loadings
Wang, H
Buchholz, FG
Richard, HA
FATIGUE '99: PROCEEDINGS OF THE SEVENTH INTERNATIONAL FATIGUE CONGRESS, VOLS 1-4, 1999, : 1213 - 1218
[23] Effects of Stitching on Delamination of Satin Weave Carbon-Epoxy Laminates Under Mode I, Mode II and Mixed-Mode I/II Loadings
Trabelsi, Walid
Michel, Laurent
Othomene, Renaud
APPLIED COMPOSITE MATERIALS, 2010, 17 (06) : 575 - 595
[24] Effects of Stitching on Delamination of Satin Weave Carbon-Epoxy Laminates Under Mode I, Mode II and Mixed-Mode I/II Loadings
Walid Trabelsi
Laurent Michel
Renaud Othomene
Applied Composite Materials, 2010, 17 : 575 - 595
[25] Prediction of Cohesive Zone Length and Accurate Numerical Simulation of Delamination under Mixed-mode Loading
Chetan H. C.
Subhaschandra Kattimani
S. M. Murigendrappa
Applied Composite Materials, 2021, 28 : 1861 - 1898
[26] An energy based approach for reliability analysis of delamination growth under mode I, mode II and mixed mode I/II loading in composite laminates
Delbariani-Nejad, Ali
Farrokhabadi, Amin
Jafari, Sepideh Rezaei
INTERNATIONAL JOURNAL OF MECHANICAL SCIENCES, 2018, 145 : 287 - 298
[27] Prediction of Cohesive Zone Length and Accurate Numerical Simulation of Delamination under Mixed-mode Loading
Chetan, H. C.
Kattimani, Subhaschandra
Murigendrappa, S. M.
APPLIED COMPOSITE MATERIALS, 2021, 28 (06) : 1861 - 1898
[28] Assessment of energy dissipation during mixed-mode delamination growth using cohesive zone models
Sarrado, C.
Turon, A.
Renart, J.
Urresti, I.
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2012, 43 (11) : 2128 - 2136
[29] A THERMODYNAMICALLY CONSISTENT COHESIVE DAMAGE MODEL FOR THE SIMULATION OF MIXED-MODE DELAMINATION
Confalonieri, Federica
Perego, Umberto
COMPUTATIONAL PLASTICITY XIV: FUNDAMENTALS AND APPLICATIONS, 2017, : 151 - 162
[30] A new framework for the formulation and validation of cohesive mixed-mode delamination models
Confalonieri, Federica
Perego, Umberto
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2019, 164 : 168 - 190

← 1 2 3 4 5 →