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Equivalent stress concept to account for the effect of local cyclic stress ratio on transverse cracking in tension–tension fatigue
Luleå University of Technology, Department of Engineering Sciences and Mathematics, Material Science.ORCID iD: 0000-0002-7524-0661
Department of Management and Engineering, Linköping University, SE-58183 Linköping, Sweden.
Luleå University of Technology, Department of Engineering Sciences and Mathematics, Material Science.ORCID iD: 0000-0002-5948-7525
Luleå University of Technology, Department of Engineering Sciences and Mathematics, Material Science. Laboratory of Experimental Mechanics of Materials, Riga Technical University, LV-1048 Riga, Latvia.ORCID iD: 0000-0001-9649-8621
2024 (English)In: International Journal of Fatigue, ISSN 0142-1123, E-ISSN 1879-3452, Vol. 187, article id 108482Article in journal (Refereed) Published
Abstract [en]

Presented test results on transverse cracking in cross-ply laminates upon tension–tension cyclic loading show that the increase of crack density depends not only on the maximum transverse stress in the cycle but also on the local cyclic stress ratio RTloc in the analyzed layer. To include the effect of the RTloc in the model with statistical failure stress distribution for crack initiation (based on Weibull distribution) adapted for fatigue, an equivalent stress is introduced in a similar manner as the equivalent strain energy release rate has been used for delamination crack propagation. The equivalent stress in the layer is defined as a power function of the maximum stress and the stress ratio in the layer. It was found, testing laminates with two different fiber contents that higher the local stress ratio in 90-layer, higher the transverse cracking resistance. Transverse crack density simulation using the developed equivalent stress model has been validated against test results. 

Place, publisher, year, edition, pages
Elsevier, 2024. Vol. 187, article id 108482
Keywords [en]
Fatigue, Polymer-matrix composites, Statistical methods, Transverse cracking
National Category
Applied Mechanics Composite Science and Engineering
Research subject
Polymeric Composite Materials
Identifiers
URN: urn:nbn:se:ltu:diva-108399DOI: 10.1016/j.ijfatigue.2024.108482ISI: 001269306200001Scopus ID: 2-s2.0-85197612883OAI: oai:DiVA.org:ltu-108399DiVA, id: diva2:1886268
Note

Validerad;2024;Nivå 2;2024-07-31 (signyg);

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

Full text license: CC BY

Available from: 2024-07-31 Created: 2024-07-31 Last updated: 2024-07-31Bibliographically approved

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Pakkam Gabriel, Vivek RichardsFernberg, PatrikVarna, Janis

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