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Assessment of the post-impact damage propagation in a carbon-fibre composite under cyclic loading

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    SYSNO ASEP0432603
    Document TypeJ - Journal Article
    R&D Document TypeJournal Article
    Subsidiary JČlánek ve WOS
    TitleAssessment of the post-impact damage propagation in a carbon-fibre composite under cyclic loading
    Author(s) Kytýř, Daniel (UTAM-F) SAI, RID, ORCID
    Fíla, T. (CZ)
    Šleichrt, J. (CZ)
    Doktor, Tomáš (UTAM-F) RID, SAI, ORCID
    Šperl, Martin (UTAM-F) RID, SAI
    Number of authors5
    Source TitleMateriali in Tehnologije. - : Institut za Kovinske Materiale in Tehnologije - ISSN 1580-2949
    Roč. 48, č. 5 (2014), s. 777-780
    Number of pages4 s.
    Publication formPrint - P
    Languageeng - English
    CountrySI - Slovenia
    Keywordscarbon-fibre composites ; post-impact damage ; laser profilometry
    Subject RIVJI - Composite Materials
    R&D ProjectsTA03010209 GA TA ČR - Technology Agency of the Czech Republic (TA ČR)
    Institutional supportUTAM-F - RVO:68378297
    UT WOS000344718900027
    EID SCOPUS84908090496
    AnnotationCarbon fibre in polyphenylene sulfide composites (C/PPS) became a popular material in the aircraft industry but its fragility and low impact resistance limits its application in primary aircraft structures. This study is focused on damage propagation in the laminated composites reinforced with carbon fibres. The damage may be inflicted during the ground maintenance, by an inflight bird strike or during a flight in severe meteorological conditions (heavy storms). The initial damage was created by a drop-weight out-of-plane impact using a spherical indenter. The response of the material was analysed by monitoring the impacted zones and their propagation history. The influenced area and specimen thickness in the centres of indents were chosen as the degradation parameters. The post-impact damage propagation induced by cyclic loading was assessed using a custom-designed computer-controlled laser-profilometery device. Both the upper and lower profiles of the specimen were scanned during the interruptions of the fatigue test. Global deformation was described with an analytically determined centroidal-axis curve. Local topography changes were obtained with a subtraction of this curve. Surface-deformation maps were created and used for a demonstration of the damage propagation in the specimen.
    WorkplaceInstitute of Theoretical and Applied Mechanics
    ContactKulawiecová Kateřina, kulawiecova@itam.cas.cz, Tel.: 225 443 285
    Year of Publishing2015
    Electronic addresshttp://mit.imt.si/Revija/izvodi/mit145/kytyr.pdf
Number of the records: 1  

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