Limit states of thin-walled composite structures with closed sections under axial compression
The subjects of the study were thin-walled composite columns with closed cross sections manufactured using the autoclave technique. The composite profiles were characterized by the fact that they had a constant height and arrangement of laminate layers, however, varied cross-sectional shapes. The st...
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| Published in | Composites. Part B, Engineering Vol. 287; p. 111813 |
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| Main Author | |
| Format | Journal Article |
| Language | English |
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01.12.2024
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| Abstract | The subjects of the study were thin-walled composite columns with closed cross sections manufactured using the autoclave technique. The composite profiles were characterized by the fact that they had a constant height and arrangement of laminate layers, however, varied cross-sectional shapes. The study was conducted using several interdisciplinary experimental research methods and advanced numerical simulations. In the course of the research, both forms of structural stability loss were registered, and damage to composite structures was assessed. In the course of the research, the influence of the shape of the cross-section on the stability and load-carrying capacity of the structure was evaluated. A measurable effect of the conducted research was the determination of the structure's post-buckling equilibrium paths, which made it possible to determine the structure's behavior in the full range of loading. In addition, the author's numerical models developed enabled validation of parallel experimental studies. The developed numerical models were based on a failure criterion known as progressive failure analysis - which allowed a thorough assessment of the failure mechanism of the composite material. |
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| AbstractList | The subjects of the study were thin-walled composite columns with closed cross sections manufactured using the autoclave technique. The composite profiles were characterized by the fact that they had a constant height and arrangement of laminate layers, however, varied cross-sectional shapes. The study was conducted using several interdisciplinary experimental research methods and advanced numerical simulations. In the course of the research, both forms of structural stability loss were registered, and damage to composite structures was assessed. In the course of the research, the influence of the shape of the cross-section on the stability and load-carrying capacity of the structure was evaluated. A measurable effect of the conducted research was the determination of the structure's post-buckling equilibrium paths, which made it possible to determine the structure's behavior in the full range of loading. In addition, the author's numerical models developed enabled validation of parallel experimental studies. The developed numerical models were based on a failure criterion known as progressive failure analysis - which allowed a thorough assessment of the failure mechanism of the composite material. |
| ArticleNumber | 111813 |
| Author | Rozylo, Patryk |
| Author_xml | – sequence: 1 givenname: Patryk orcidid: 0000-0003-1997-3235 surname: Rozylo fullname: Rozylo, Patryk email: p.rozylo@pollub.pl organization: Department of Machine Design and Mechatronics, Faculty of Mechanical Engineering, Lublin University of Technology, Nadbystrzycka 36, 20-618, Lublin, Poland |
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| Cites_doi | 10.1016/j.compositesb.2021.109346 10.1080/09243046.2014.915105 10.1016/j.tws.2020.107019 10.1016/j.compstruct.2016.12.041 10.1016/0266-3538(96)00005-X 10.1016/j.compstruct.2020.113342 10.1016/j.tws.2016.06.022 10.1007/s10443-017-9583-y 10.1061/(ASCE)AS.1943-5525.0000036 10.1115/1.3443689 10.1016/j.mechmat.2005.10.003 10.1016/j.compstruct.2021.113650 10.12913/22998624/161598 10.3390/ma16216835 10.1016/j.compositesb.2017.01.001 10.12913/22998624/174193 10.1016/j.engstruct.2014.12.028 10.1016/0045-7949(87)90130-1 10.1002/nme.6757 10.1016/j.compstruct.2021.113751 10.1016/j.tws.2015.03.009 10.1007/s10443-013-9315-x 10.1016/j.tws.2022.109869 10.1016/j.compstruct.2015.07.039 10.1016/j.compstruct.2021.114298 10.1177/002199837300700404 10.1016/0167-6636(94)00053-0 10.1016/j.compstruct.2016.10.029 10.1115/1.3153664 10.1016/j.compstruct.2015.08.023 10.1016/j.compstruct.2023.117530 10.1016/0167-6636(83)90032-7 10.1177/0021998303034505 10.3390/aerospace9100541 10.1016/j.compositesa.2007.01.017 10.1016/j.compstruct.2019.111407 10.3390/ma13132956 10.1016/j.ijmecsci.2021.106747 |
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| Keywords | Progressive failure analysis Composite structures Load-carrying capacity Buckling Failure |
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| SubjectTerms | Buckling Composite structures Failure Load-carrying capacity Progressive failure analysis |
| Title | Limit states of thin-walled composite structures with closed sections under axial compression |
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