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Equivalent stress concept to account for the effect of local cyclic stress ratio on transverse cracking in tension–tension fatigue
Department of Engineering Sciences and Mathematics, Luleå University of Technology, Luleå, Sweden.
Linköpings universitet, Institutionen för ekonomisk och industriell utveckling, Konstruktionsmaterial. Linköpings universitet, Tekniska fakulteten.ORCID-id: 0000-0003-4472-1742
Department of Engineering Sciences and Mathematics, Luleå University of Technology, Luleå, Sweden.ORCID-id: 0000-0002-5948-7525
Department of Engineering Sciences and Mathematics, Luleå University of Technology, Luleå, Sweden; .
2024 (engelsk)Inngår i: International Journal of Fatigue, ISSN 0142-1123, E-ISSN 1879-3452, Vol. 187, artikkel-id 108482Artikkel i tidsskrift (Fagfellevurdert) 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 RlocT in the analyzed layer. To include the effect of the RlocT 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.

sted, utgiver, år, opplag, sider
Elsevier BV , 2024. Vol. 187, artikkel-id 108482
Emneord [en]
Fatigue; Polymer-matrix composites; Statistical methods; Transverse cracking
HSV kategori
Identifikatorer
URN: urn:nbn:se:liu:diva-206212DOI: 10.1016/j.ijfatigue.2024.108482ISI: 001269306200001Scopus ID: 2-s2.0-85197612883OAI: oai:DiVA.org:liu-206212DiVA, id: diva2:1888277
Merknad

Funding Agencies|Swedish Aeronautical Research Program NFFP 7 [2019-02777]; Swedish Aeronautical Research Program NFFP 8 [2023-01199]; GKN Aerospace, Sweden

Tilgjengelig fra: 2024-08-12 Laget: 2024-08-12 Sist oppdatert: 2025-04-10bibliografisk kontrollert

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Sahbi Loukil, Mohamed

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