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Transverse cracking in non-crimp fabric cross-ply laminate under tension–tension cyclic loading at room and elevated temperature
Luleå University of Technology, Department of Engineering Sciences and Mathematics, Material Science.ORCID iD: 0000-0002-7524-0661
Luleå University of Technology, Department of Engineering Sciences and Mathematics, Material Science.ORCID iD: 0000-0002-5948-7525
Laboratory of Experimental Mechanics of Materials, Riga Technical University, LV-1048 Riga, Latvia.ORCID iD: 0000-0001-9649-8621
2025 (English)In: Composites. Part A, Applied science and manufacturing, ISSN 1359-835X, E-ISSN 1878-5840, Vol. 192, article id 108796Article in journal (Refereed) Published
Abstract [en]

The effect of test temperature, maximum stress, and stress-ratio on transverse cracking development in cross-ply laminates subjected to tension–tension cyclic loading was analysed. A two-parameter Weibull distribution model was used to predict transverse cracking, wherein the Weibull scale parameter was assumed to be test temperature and number of cycles dependent. By introducing an equivalent stress in the model, it was possible to account for the effect of the stress ratio in cyclic loading over a range of different loading conditions. To verify the model, tests on temperature resistant cross-ply composites were performed at room temperature and at 150 °C with different stress levels and local 90-layer stress ratios. For both test temperatures, increase in stress level increased the transverse cracking tendency. At 150 °C, despite the lower maximum thermo-mechanical ply-stress level compared to room temperature, transverse cracking tendency was found to be higher.

Place, publisher, year, edition, pages
Elsevier, 2025. Vol. 192, article id 108796
Keywords [en]
Polymer-matrix composites, Transverse cracking, Fatigue, Statistical methods
National Category
Composite Science and Engineering
Research subject
Polymeric Composite Materials
Identifiers
URN: urn:nbn:se:ltu:diva-111726DOI: 10.1016/j.compositesa.2025.108796Scopus ID: 2-s2.0-85217927472OAI: oai:DiVA.org:ltu-111726DiVA, id: diva2:1940446
Note

Validerad;2025;Nivå 2;2025-02-26 (u4);

Funder: Swedish Aeronautical Research Program NFFP 7 (2019–02777); NFFP 8 (2023–01199); GKN Aerospace, Sweden;

Fulltext license: CC BY

Available from: 2025-02-26 Created: 2025-02-26 Last updated: 2025-02-26Bibliographically approved

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Pakkam Gabriel, Vivek RichardsFernberg, PatrikVarna, Janis

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