An experimental investigation of tensile residual strength of repaired composite laminates after low velocity impact-Reference-Cited by-同舟云学术

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An experimental investigation of tensile residual strength of repaired composite laminates after low velocity impact

Published:2024-07 Issue: Volume:200 Page:111896
ISSN:0263-8231
Container-title:Thin-Walled Structures
language:en
Short-container-title:Thin-Walled Structures

Author:

Damghani M.^ORCID,Atkinson G.A.^ORCID,Thapa P.^ORCID,Joy J.,Monaghan M.,Maleki P.,Ward C.^ORCID

Publisher

Elsevier BV

Reference46 articles.

1. A study on low velocity impact damage evaluation and repair technique of small aircraft composite structure;Park;Compos. Part A Appl. Sci. Manuf.,2011

2. Experimental investigation on different positional impact damages and shear-after-impact (SAI) behaviors of stiffened composite panels;Feng;Compos. Struct.,2017

3. Experimental evaluation of residual tensile strength of hybrid composite aerospace materials after low velocity impact;Damghani;Compos. B Eng.,2019

4. Numerical shape, thickness and stacking sequence optimisation and experimental study of hybrid composite plates under in-plane shear loading;Damghani;Structures,2023

5. A comparative study of failure features in aerospace grade unidirectional and bidirectional woven CFRP composite laminates under four-point bend fatigue loads;Suresh Kumar;Materwiss. Werksttech.,2015

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