Please use this identifier to cite or link to this item: https://dspace.iiti.ac.in/handle/123456789/11755
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dc.contributor.authorJoshi, Suhas S.en_US
dc.date.accessioned2023-06-08T11:34:50Z-
dc.date.available2023-06-08T11:34:50Z-
dc.date.issued2023-
dc.identifier.citationDivse, V., Marla, D., & Joshi, S. S. (2023). Progressive damage analysis in an open hole compression of FRP laminates including fiber kinking and pre-existing damage. Composites Part A: Applied Science and Manufacturing, 169 doi:10.1016/j.compositesa.2023.107523en_US
dc.identifier.issn1359-835X-
dc.identifier.otherEID(2-s2.0-85151039394)-
dc.identifier.urihttps://doi.org/10.1016/j.compositesa.2023.107523-
dc.identifier.urihttps://dspace.iiti.ac.in/handle/123456789/11755-
dc.description.abstractProgressive damage and strength analysis in an open hole compression (OHC) test is crucial in designing components made of fiber reinforced plastics (FRPs) composites. In this work, a continuum damage mechanics based 3D progressive damage model (PDM) incorporating LaRC05 failure criteria is developed. It considers identification of fracture and kink-band plane, shear non-linearity, in-situ strengths, and mixed-mode fracture in the formulation. The proposed PDM is validated through single element tests and applied to analyze the damage patterns and strength during open hole compression (OHC) tests of three different layups with two different hole sizes and a pre-existing damage. It is observed that fiber kinking in 0∘ plies initiates at the location of maximum in-plane shear stress and propagates due to a combined action of longitudinal compression and in-plane shear stress. The final failure of 0∘ dominant and quasi-isotropic layup is governed by fiber kinking in 0∘ plies, whereas matrix cracking in ±45∘ plies is responsible for the final failure of the shear dominant layup. Furthermore, OHC strength of the layups reduces by 15%–20%, when the hole size increases from 6.35 mm to 9.525 mm. In the presence of a pre-existing kink or matrix damage, fiber kinking initiates at locations of the pre-existing damage. A small pre-existing damage reduces OHC strength of the layups up to 7%–11%. The results predicted by the model match well with the experimental results in the literature. © 2023 Elsevier Ltden_US
dc.language.isoenen_US
dc.publisherElsevier Ltden_US
dc.sourceComposites Part A: Applied Science and Manufacturingen_US
dc.subjectFiber kinkingen_US
dc.subjectOpen hole compressionen_US
dc.subjectPre-existing damageen_US
dc.subjectProgressive damageen_US
dc.titleProgressive damage analysis in an open hole compression of FRP laminates including fiber kinking and pre-existing damageen_US
dc.typeJournal Articleen_US
Appears in Collections:Department of Mechanical Engineering

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