Tensile and flexural damage response of symmetric angle‐ply carbon fiber‐reinforced epoxy laminates: Non‐linear response and effects of thickness and ply‐stacking sequence-Reference-Cited by-同舟云学术

Tensile and flexural damage response of symmetric angle‐ply carbon fiber‐reinforced epoxy laminates: Non‐linear response and effects of thickness and ply‐stacking sequence

Published:2019-02-19 Issue:9 Volume:40 Page:3678-3690
ISSN:0272-8397
Container-title:Polymer Composites
language:en
Short-container-title:Polym Compos

Author:

Caminero Miguel Angel¹^ORCID,Rodríguez Gloria Patricia¹,Chacón Jesus Miguel²,García‐Moreno Irene¹

Affiliation:

1. Escuela Técnica Superior de Ingenieros Industriales, INEIUniversidad de Castilla‐La Mancha, Campus Universitario s/n Ciudad Real 13071 Spain

2. Escuela Técnica Superior de Ingenieros Industriales, IMACIUniversidad de Castilla‐La Mancha, Campus Universitario s/n Ciudad Real 13071 Spain

Funder

Secretaría de Estado de Investigación, Desarrollo e Innovación

European Regional Development Fund

Publisher

Wiley

Subject

Materials Chemistry,Polymers and Plastics,General Chemistry,Ceramics and Composites

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/pc.25230

Reference68 articles.

1. Fibre reinforced composites in aircraft construction

2. Strength prediction of patch-repaired CFRP laminates loaded in compression

3. A Graphical Method Predicting the Compressive Strength of Toughened Unidirectional Composite Laminates

4. Modelling damage evolution in composite laminates subjected to low velocity impact

5. Continuous debonding monitoring of a patch repaired helicopter stabilizer: Damage assessment and analysis

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