Evaluating the compressive strength of stepped scarf repaired single stiffener composite panels
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Published:2023-05-30
Issue:18
Volume:57
Page:2887-2898
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ISSN:0021-9983
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Container-title:Journal of Composite Materials
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language:en
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Short-container-title:Journal of Composite Materials
Author:
Psarras Spyridon1ORCID,
Loutas Theodoros1,
Sotiriadis George1,
Kostopoulos Vassilis1ORCID
Affiliation:
1. Laboratory of Applied Mechanics, Mechanical Engineering and Aeronautics Department, University of Patras, Patra, Greece
Abstract
In this study, tests were carried out on repaired 300 × 250 mm composite stiffened panels. The initial damage was assumed to be extended in a depth of the first six plies and a repair with scarf ratio of 1:50 was employed. A circular repair took place, utilizing laser-assisted ablation and the wet patches approach. The panels were tested in compression and Digital Image Correlation (DIC) and Acoustic Emission (AE) were used in order to monitor the damage initiation and propagation of the panels. In addition, Phased Array (PA) was used in order to monitor the patch failure. Detailed Finite Elements (FE) models were validated against the test findings and their performance as a prediction tool for the performance of repairs on composite aeronautical structures was assessed.
Funder
European Union’s H2020 Framework Programme, call FET-OPEN
Publisher
SAGE Publications
Subject
Materials Chemistry,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites