Intra-laminar progressive failure analysis of composite laminates with a large notch damage-Reference-Cited by-同舟云学术

Intra-laminar progressive failure analysis of composite laminates with a large notch damage

Published:2017-03 Issue: Volume:73 Page:97-112
ISSN:1350-6307
Container-title:Engineering Failure Analysis
language:en
Short-container-title:Engineering Failure Analysis

Author:

Riccio A.^ORCID,Di Costanzo C.,Di Gennaro P.,Sellitto A.,Raimondo A.

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference35 articles.

1. A study on skin delaminations growth in stiffened composite panels by a novel numerical approach;Riccio;Appl. Compos. Mater.,2013

2. Influence of contact phenomena on embedded delamination growth in composites;Riccio;AIAA J.,2003

3. Delaminations buckling and growth phenomena in stiffened composite panels under compression. Part I: An experimental study;Riccio;J. Compos. Mater.,2013

4. Delaminations buckling and growth phenomena in stiffened composite panels under compression. Part II: a numerical study;Riccio;J. Compos. Mater.,2013

5. Three-dimensional BEM and FEM Submodelling in a cracked FML full scale aeronautic panel;Citarella;Appl. Compos. Mater.,2014

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