Comparison of numerical analyses of a composite wing component subjected to 4-point bending
2022
Authors
Bisagni, C.Raimondo, A.
Atanasovska, Ivana
Milić, M.
Troian, R.
Frulla, G.
Polla, A.
Cora, Ö.N.
Bekci, M.L.
Henriques, B.
de Moura, M.F.S.F.
Almudaihesh, F.
Grigg, S.
Article (Published version)
Metadata
Show full item recordAbstract
In this paper, a comparison between six finite element models of a representative wing structural component performed in the context of Optimised Design for Inspection (ODIN) project of the European Cooperation in Science and Technology (COST) is presented. Six partners from six different countries involved in the project received the drawing of the structure, the material properties, the loading and boundary conditions. Each partner, based on their background and experience in numerical analyses, developed a finite element model with different levels of details and accuracy and performed a blind prediction of the structural behaviour of the wing component. The numerical results are presented and compared with the experimental test data conducted at Cardiff University.
Keywords:
Wing structure / Numerical benchmark / Aerospace composite structureSource:
Composites Part C: Open Access, 2022, 8Publisher:
- Elsevier B.V.
Funding / projects:
- This publication is based upon work from COST Action CA18203 - Optimizing Design for Inspection (ODIN ? www.odin-cost.com) supported by COST (European Cooperation in Science and Technology - www.cost.eu).
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Mašinski fakultetTY - JOUR AU - Bisagni, C. AU - Raimondo, A. AU - Atanasovska, Ivana AU - Milić, M. AU - Troian, R. AU - Frulla, G. AU - Polla, A. AU - Cora, Ö.N. AU - Bekci, M.L. AU - Henriques, B. AU - de Moura, M.F.S.F. AU - Almudaihesh, F. AU - Grigg, S. PY - 2022 UR - https://machinery.mas.bg.ac.rs/handle/123456789/3824 AB - In this paper, a comparison between six finite element models of a representative wing structural component performed in the context of Optimised Design for Inspection (ODIN) project of the European Cooperation in Science and Technology (COST) is presented. Six partners from six different countries involved in the project received the drawing of the structure, the material properties, the loading and boundary conditions. Each partner, based on their background and experience in numerical analyses, developed a finite element model with different levels of details and accuracy and performed a blind prediction of the structural behaviour of the wing component. The numerical results are presented and compared with the experimental test data conducted at Cardiff University. PB - Elsevier B.V. T2 - Composites Part C: Open Access T1 - Comparison of numerical analyses of a composite wing component subjected to 4-point bending VL - 8 DO - 10.1016/j.jcomc.2022.100264 ER -
@article{ author = "Bisagni, C. and Raimondo, A. and Atanasovska, Ivana and Milić, M. and Troian, R. and Frulla, G. and Polla, A. and Cora, Ö.N. and Bekci, M.L. and Henriques, B. and de Moura, M.F.S.F. and Almudaihesh, F. and Grigg, S.", year = "2022", abstract = "In this paper, a comparison between six finite element models of a representative wing structural component performed in the context of Optimised Design for Inspection (ODIN) project of the European Cooperation in Science and Technology (COST) is presented. Six partners from six different countries involved in the project received the drawing of the structure, the material properties, the loading and boundary conditions. Each partner, based on their background and experience in numerical analyses, developed a finite element model with different levels of details and accuracy and performed a blind prediction of the structural behaviour of the wing component. The numerical results are presented and compared with the experimental test data conducted at Cardiff University.", publisher = "Elsevier B.V.", journal = "Composites Part C: Open Access", title = "Comparison of numerical analyses of a composite wing component subjected to 4-point bending", volume = "8", doi = "10.1016/j.jcomc.2022.100264" }
Bisagni, C., Raimondo, A., Atanasovska, I., Milić, M., Troian, R., Frulla, G., Polla, A., Cora, Ö.N., Bekci, M.L., Henriques, B., de Moura, M.F.S.F., Almudaihesh, F.,& Grigg, S.. (2022). Comparison of numerical analyses of a composite wing component subjected to 4-point bending. in Composites Part C: Open Access Elsevier B.V.., 8. https://doi.org/10.1016/j.jcomc.2022.100264
Bisagni C, Raimondo A, Atanasovska I, Milić M, Troian R, Frulla G, Polla A, Cora Ö, Bekci M, Henriques B, de Moura M, Almudaihesh F, Grigg S. Comparison of numerical analyses of a composite wing component subjected to 4-point bending. in Composites Part C: Open Access. 2022;8. doi:10.1016/j.jcomc.2022.100264 .
Bisagni, C., Raimondo, A., Atanasovska, Ivana, Milić, M., Troian, R., Frulla, G., Polla, A., Cora, Ö.N., Bekci, M.L., Henriques, B., de Moura, M.F.S.F., Almudaihesh, F., Grigg, S., "Comparison of numerical analyses of a composite wing component subjected to 4-point bending" in Composites Part C: Open Access, 8 (2022), https://doi.org/10.1016/j.jcomc.2022.100264 . .