Details
Original language | English |
---|---|
Pages (from-to) | 513-525 |
Number of pages | 13 |
Journal | Composite structures |
Volume | 136 |
Publication status | Published - 8 Oct 2015 |
Abstract
This paper is concerned with the development of a novel FE-based two-way loose coupling approach for the analysis of stiffened composite panels. The aim of this numerical strategy is to investigate the global postbuckling behaviour as well as the local damage progression of composite structures using separated FE models with different levels of fidelity: (i) a relatively simple global model of the complete structure, and (ii) more complex local models of certain details that incorporate damage capabilities to simulate damage events. In the coupling process, information is exchanged between these diverse models to simulate the overall structural behaviour including geometrical as well as material nonlinearities. The two-way loose coupling character of the methodology allows, firstly, a direct interaction between the global and the local levels along the solution process and, secondly, a highly versatile adaption with regard to the definition of the local models. In addition, the separation of the models and analyses in the approach enables the use of standard FE software without complex implementations or modifications of the source code. The developed coupling procedure is assessed through two applications: (i) an academic composite stiffened panel, and (ii) a real stiffened panel taken from literature. The results of the proposed coupling approach are compared with the numerical and experimental reference data, exhibiting a satisfactory level of accuracy.
Keywords
- Buckling and postbuckling, Composite structures, Damage mechanics, Loose coupling, Multiscale analysis, Stiffened panels
ASJC Scopus subject areas
- Materials Science(all)
- Ceramics and Composites
- Engineering(all)
- Civil and Structural Engineering
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In: Composite structures, Vol. 136, 08.10.2015, p. 513-525.
Research output: Contribution to journal › Article › Research › peer review
}
TY - JOUR
T1 - A two-way loose coupling procedure for investigating the buckling and damage behaviour of stiffened composite panels
AU - Hühne, Sina
AU - Reinoso, José
AU - Jansen, Eelco
AU - Rolfes, Raimund
N1 - Funding information: Parts of the research leading to these results has received funding from the European Community’s Seventh Framework Programme (FP7/2007-2013) under Grant agreement number 234147 . JR gratefully acknowledges the research projects funded by the Spanish Ministry of Economy and Competitiveness/FEDER (DPI2012-37187) and the Andalusian Government (Projects of Excellence No. TEP-7093 and P12-TEP-1050).
PY - 2015/10/8
Y1 - 2015/10/8
N2 - This paper is concerned with the development of a novel FE-based two-way loose coupling approach for the analysis of stiffened composite panels. The aim of this numerical strategy is to investigate the global postbuckling behaviour as well as the local damage progression of composite structures using separated FE models with different levels of fidelity: (i) a relatively simple global model of the complete structure, and (ii) more complex local models of certain details that incorporate damage capabilities to simulate damage events. In the coupling process, information is exchanged between these diverse models to simulate the overall structural behaviour including geometrical as well as material nonlinearities. The two-way loose coupling character of the methodology allows, firstly, a direct interaction between the global and the local levels along the solution process and, secondly, a highly versatile adaption with regard to the definition of the local models. In addition, the separation of the models and analyses in the approach enables the use of standard FE software without complex implementations or modifications of the source code. The developed coupling procedure is assessed through two applications: (i) an academic composite stiffened panel, and (ii) a real stiffened panel taken from literature. The results of the proposed coupling approach are compared with the numerical and experimental reference data, exhibiting a satisfactory level of accuracy.
AB - This paper is concerned with the development of a novel FE-based two-way loose coupling approach for the analysis of stiffened composite panels. The aim of this numerical strategy is to investigate the global postbuckling behaviour as well as the local damage progression of composite structures using separated FE models with different levels of fidelity: (i) a relatively simple global model of the complete structure, and (ii) more complex local models of certain details that incorporate damage capabilities to simulate damage events. In the coupling process, information is exchanged between these diverse models to simulate the overall structural behaviour including geometrical as well as material nonlinearities. The two-way loose coupling character of the methodology allows, firstly, a direct interaction between the global and the local levels along the solution process and, secondly, a highly versatile adaption with regard to the definition of the local models. In addition, the separation of the models and analyses in the approach enables the use of standard FE software without complex implementations or modifications of the source code. The developed coupling procedure is assessed through two applications: (i) an academic composite stiffened panel, and (ii) a real stiffened panel taken from literature. The results of the proposed coupling approach are compared with the numerical and experimental reference data, exhibiting a satisfactory level of accuracy.
KW - Buckling and postbuckling
KW - Composite structures
KW - Damage mechanics
KW - Loose coupling
KW - Multiscale analysis
KW - Stiffened panels
UR - http://www.scopus.com/inward/record.url?scp=84946606559&partnerID=8YFLogxK
U2 - 10.1016/j.compstruct.2015.09.056
DO - 10.1016/j.compstruct.2015.09.056
M3 - Article
AN - SCOPUS:84946606559
VL - 136
SP - 513
EP - 525
JO - Composite structures
JF - Composite structures
SN - 0263-8223
ER -