Tension-after-impact (TAI) performance and 3D damage visualization of carbon-fiber epoxy composites with adhesively bonded patch repairs-Reference-Cited by-同舟云学术

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Tension-after-impact (TAI) performance and 3D damage visualization of carbon-fiber epoxy composites with adhesively bonded patch repairs

Published:2023-10 Issue: Volume:322 Page:117338
ISSN:0263-8223
Container-title:Composite Structures
language:en
Short-container-title:Composite Structures

Author:

Roeper Florian,Sommacal Silvano^ORCID,Compston Paul,Tauchner Jürgen,Wolfahrt Markus^ORCID,Pinter Gerald^ORCID

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference57 articles.

1. On the durability of FRP composites for aircraft structures in hygrothermal conditioning;Guermazi;Compos B,2016

2. Effect of hydrothermal ageing on the thermal and delamination fracture behaviour of CFRP composites;Alessi;Compos B,2014

3. Environmental and chemical degradation of carbon/epoxy and structural adhesive for aerospace applications: Fickian and anomalous diffusion, Arrhenius kinetics;La Saponara;Compos Struct,2011

4. Stepped flush repairs for primary composite structures;Wang;J Adhes,2015

5. Parametric study on static and fatigue strength recovery of scarf-patch-repaired composite laminates;Yoo;Compos Struct,2016

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Barely visible impact damage evaluation of composite laminates using acoustic emission;Non-destructive Testing of Impact Damage in Fiber-Reinforced Polymer Composites;2024

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