Simulation of multiple delaminations in composite laminates under mixed-mode deformations

2003 ◽  
Vol 11 (5-6) ◽  
pp. 483-500 ◽  
Author(s):  
Paolo Lonetti ◽  
Raffaele Zinno
Keyword(s):  
Composite Laminates ◽  
Mixed Mode

Mixed-Mode Ply Cracking in Multidirectional Continuous Fiber Composite Laminates

2000 ◽  
Vol 183-187 ◽  
pp. 1141-1146
Author(s):  
Jun Qian Zhang ◽  
K.P. Herrmann ◽  
Xiang Guo Zeng
Keyword(s):  
Composite Laminates ◽  
Mixed Mode ◽  
Fiber Composite ◽  
Continuous Fiber

Test and Analysis of Modes I, II and Mixed-Mode I/II Delamination for Carbon/Epoxy Composite Laminates

2019 ◽  
Vol 20 (3) ◽  
pp. 636-652 ◽  
Author(s):  
Hongsu Bae ◽  
Minsong Kang ◽  
Kyeongsik Woo ◽  
In-Gul Kim ◽  
Kyung-hwan In
Keyword(s):  
Composite Laminates ◽  
Mixed Mode ◽  
Epoxy Composite ◽  
Mode I

Fatigue Delamination Analysis of Composite Laminates with a Central Hole Using Interface Elements

2011 ◽  
Vol 471-472 ◽  
pp. 568-571
Author(s):  
Hossein Hosseini-Toudeshky ◽  
A. Jasemzadeh ◽  
Bijan Mohammadi
Keyword(s):  
Cyclic Loading ◽  
Composite Laminates ◽  
Mixed Mode ◽  
Composite Laminate ◽  
Constitutive Law ◽  
Central Hole ◽  
Interface Element ◽  
Interface Elements

In this paper a solid like interface element along with a fatigue constitutive law is used to study the damage behaviour of holed composite laminates under cyclic loading. For this purpose a user element routine and a material routine was developed include the interface element and to handle the formulation of progressive fatigue damages. The developed procedure is used to predict delamination initiation and growth in mixed-mode condition for a typical composite laminate. The obtained results for damage and stresses are compared with the available results in the literature.

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