A new approach to model delamination growth in fatigue using the Virtual Crack Closure Technique without re-meshing-Reference-Cited by-同舟云学术

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A new approach to model delamination growth in fatigue using the Virtual Crack Closure Technique without re-meshing

Published:2019-12 Issue: Volume:222 Page:106614
ISSN:0013-7944
Container-title:Engineering Fracture Mechanics
language:en
Short-container-title:Engineering Fracture Mechanics

Author:

De Carvalho N.V.,Mabson G.E.,Krueger R.,Deobald L.R.

Funder

NASA

National Aeronautics and Space Administration

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference27 articles.

1. Characterization and analysis of delamination fracture in composites: an overview of developments from 1990 to 2001;Tay;Appl Mech Rev,2003

2. A finite element calculation of stress intensity factors by a modified crack closure integral;Rybicki;Eng Fract Mech,1977

3. Virtual crack closure technique: history, approach, and applications;Krueger;Appl Mech Rev,2004

4. Modeling compression failure after low velocity impact on laminated composites using interface elements;De Moura;J Compos Mater,1997

5. Camanho PP, Dávila CG. Mixed-mode decohesion finite elements for the simulation of delamination in composite materials. Technical report. NASA-TM-2002-211737. National Aeronautics and Space Administration; 2002.

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